A320 Amm Ch12
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__________ HIGHLIGHTS REVISION NO. 32 Jan 01/07 Pages which have been revised are outlined below, together with the Highlights of the Revision -------------------------------------------------------------------------------------CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES -------------------------------------------------------------------------------------CHAPTER 12 __________
L.E.P. 1-12 Revised to Reflect this revision indicating new,revised, and/or deleted pages T. OF C. Revised to reflect this revision 12, 5, 78, 1116 12-00-00 CORRECTION/ADDITION/AMPLIFICATION 202, 206 ADDED NOTE.
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12-11-28 301, 303304, 308309, 315B308
Effectivity updated CORRECTION/ADDITION/AMPLIFICATION NOTE ADDED TO INCLUDE REFUEL WITH ONE ENGINE RUNNING LAYOUT IMPROVED/MATERIAL RELOCATED
12-12-29 302- 304, 306, 309312, 317
CORRECTION/ADDITION/AMPLIFICATION REMOVED NOTE RELATED TO THE RESET OF THE C/B 5JR
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12-12-32 313, 331, 334
CORRECTION/ADDITION/AMPLIFICATION ILLUSTRATION RE-ISSUED TOOL DESIGNATION(S) DATA UPDATED
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ALL ALL
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12-13-80 01 TITLE OF TASK(S) DATA UPDATED 311, 323
001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499,
12-14-29 301- 302, 305- 306, 309- 310
CORRECTION/ADDITION/AMPLIFICATION ADDED A NOTE (TEMPERATURE COMPENSATION TIME OF THE ACCUMULATOR). TOOL DESIGNATION(S) DATA UPDATED
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12-14-32 301- 302, 304, 318,
Effectivity updated CORRECTION/ADDITION/AMPLIFICATION FINS CHANGED TO 5490GG AND 5491GG
ALL ALL 12-HIGHLIGHTS Page REVISION NO. 32
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1 of 3 Jan 01/07
-------------------------------------------------------------------------------------CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES -------------------------------------------------------------------------------------323- 325, 327, 329330, 335
TOOL DESIGNATION(S) DATA UPDATED TITLE OF TASK(S) DATA UPDATED
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12-16-38 303
TECHNICAL CORRECTIONS CLERICAL CORRECTION
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12-21-11 301- 311
TECHNICAL CORRECTIONS ADDED WARNING FOR HEALTH RECOMMENDATION CORRECTION/ADDITION/AMPLIFICATION ADDED ADHESIVE-TAPE WARNING WARNING/NOTE/REASON FOR THE JOB AMENDED
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12-21-12 323- 324, 326- 328, 345, 353, 365- 366
12-21-13 701- 720
Effectivity updated MOD.45794D41610 REMOVED EQUIPMENT/FURNISHINGS-PAX COMPARTMENTINSTALL A 3 CLASS LAYOUT FOR SWR1 VERSION CORRECTION/ADDITION/AMPLIFICATION MINOR CHANGE CORRECTION/ADDITION/AMPLIFICATION ADDED CROSS REFERENCE TO ILS RECEIVER TITLE OF TASK(S) DATA UPDATED WARNING/NOTE/REASON FOR THE JOB AMENDED
ALL ALL 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, ALL ALL ALL ALL
12-22-27 305- 306, 345- 346, 348, 350390
Effectivity updated CORRECTION/ADDITION/AMPLIFICATION CAUTION ADDED.
12-22-32 312- 317, 322- 323, 328- 336, 339, 349, 356, 360365
CORRECTION/ADDITION/AMPLIFICATION ITEM 1 (2 ON ONE SIDE, 1ON THE OTHER) CHANGED TO (3 ON ONE SIDE, 2ON THE OTHER) LAYOUT IMPROVED/MATERIAL RELOCATED
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12-31-00 3
CORRECTION/ADDITION/AMPLIFICATION NOTE IN ITEM B.(4) UPDATED.
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12-31-11 201- 204, 208- 210
CORRECTION/ADDITION/AMPLIFICATION ANTI-ICING FLUID REPLACED BY ANTI-ICING/DE-ICING FLUID. TOOL DESIGNATION(S) DATA UPDATED WARNING/NOTE/REASON FOR THE JOB AMENDED
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ALL
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ALL ALL 12-HIGHLIGHTS Page REVISION NO. 32
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-------------------------------------------------------------------------------------CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES -------------------------------------------------------------------------------------12-31-12 201- 203, 209- 213
TECHNICAL CORRECTIONS CLERICAL CORRECTION. CORRECTION/ADDITION/AMPLIFICATION ADDED NOTE. TOOL DESIGNATION(S) DATA UPDATED
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TECHNICAL CORRECTIONS CLERICAL CORRECTION. WARNING/NOTE/REASON FOR THE JOB AMENDED
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12-31-27 201- 203
TECHNICAL CORRECTIONS CLERICAL CORRECTION.
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12-31-32 203- 207
LAYOUT IMPROVED/MATERIAL RELOCATED
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12-31-35 202
TECHNICAL CORRECTIONS CLERICAL CORRECTION.
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12-31-38 201
WARNING/NOTE/REASON FOR THE JOB AMENDED
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12-32-28 302, 308309, 311314, 338, 341- 344
TECHNICAL CORRECTIONS CLERICAL CHANGE CORRECTION/ADDITION/AMPLIFICATION CLERICAL CHANGE WARNING/NOTE/REASON FOR THE JOB AMENDED
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12-32-29 301- 302, 304- 305
CORRECTION/ADDITION/AMPLIFICATION ADDED PLASTIC SAMPLE BOTTLE EXCLUSIVELY MADE FROM POLY-ETHYLENE
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12-34-24 201- 202, 205- 207
TECHNICAL CORRECTIONS CLERICAL CORRECTION. CORRECTION/ADDITION/AMPLIFICATION WORK-STAND REPLACED BY ACCESS PLATFORM OR STE P LADDER. WARNING/NOTE/REASON FOR THE JOB AMENDED
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12-31-24 201
12-36-29 327, 332, 335,A328A329,A351C361
Effectivity updated CORRECTION/ADDITION/AMPLIFICATION REMOVED STEPS RELATED TO THE HCU FILTER LAYOUT IMPROVED/MATERIAL RELOCATED WARNING/NOTE/REASON FOR THE JOB AMENDED
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12-HIGHLIGHTS Page REVISION NO. 32 SROS
3 of 3 Jan 01/07
CHAPTER 12 __________ SERVICING LIST OF EFFECTIVE PAGES _______________________ N, R or D indicates pages which are New, Revised or Deleted respectively Remove and insert the affected pages and complete the Record of Revisions and the Record of Temporary Revisions as necessary CH/SE/SU
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RECORD OF TEMP. REVISION L.E.P. T. of C. T. of C. T. of C. T. of C. T. of C. T. of C. T. of C. T. of C. T. of C. T. of C. T. of C. T. of C. T. of C. T. of C. T. of C. T. of C. 12-00-00 12-00-00 12-00-00 12-00-00 12-00-00 12-00-00 12-00-00 12-00-00 12-00-00 12-00-00 12-00-00 12-00-00 12-00-00 12-00-00 12-00-00 12-00-00 12-00-00 12-00-00 12-10-00
R 1-12 Jan01/07 R 1 Jan01/07 R 2 Jan01/07 3 Jul01/06 4 Jul01/05 R 5 Jan01/07 6 Jul01/05 R 7 Jan01/07 R 8 Jan01/07 9 Jul01/06 10 Jul01/06 R 11 Jan01/07 R 12 Jan01/07 R 13 Jan01/07 R 14 Jan01/07 R 15 Jan01/07 R 16 Jan01/07
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1 2 3 4 5 6 7 8 9 10 11 201 202 203 204 205 206 207
Jul01/05 Apr01/98 Apr01/98 Jul01/05 Jul01/05 Oct01/00 Oct01/00 Oct01/00 Oct01/00 Oct01/00 Oct01/00 Jan01/02 Jan01/07 Apr01/98 Jan01/02 Apr01/98 Jan01/07 Apr01/98
1 Apr01/98
CH/SE/SU 12-11-00 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28
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1 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315 316 317 318 319 320 321 322 323 324 325 326 327 328 329 330 331 332 333 334 335 336 337 338 339 340 341
DATE Jul01/06 Jan01/07 Apr01/00 Jan01/07 Jan01/07 Jul01/06 Jul01/06 Jul01/04 Jan01/07 Jan01/07 Jul01/04 Jul01/04 Jul01/04 Jan01/06 Apr01/05 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07
CH/SE/SU 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28
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342 343 344 345 346 347 348 349 350 351 352 353 354 355 356 357 358 359 360 361 362 363 364 365 366 367 368 369 370 371 372 373 374 375 376 377 378 379 380 381 382 383
DATE Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07
12-L.E.P. Page 1 Jan 01/07 SROS
CH/SE/SU 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28
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384 385 386 387 388 389 390 391 392 393 394 395 396 397 398 399 A300 A301 A302 A303 A304 A305 A306 A307 A308 A309 A310 A311 A312 A313 A314 A315 A316 A317 A318 A319 A320 A321 A322 A323 A324 A325 A326 A327 A328 A329 A330 A331 A332 A333 A334
DATE Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07
CH/SE/SU 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28
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A335 A336 A337 A338 A339 A340 A341 A342 A343 A344 A345 A346 A347 A348 A349 A350 A351 A352 A353 A354 A355 A356 A357 A358 A359 A360 A361 A362 A363 A364 A365 A366 A367 A368 A369 A370 A371 A372 A373 A374 A375 A376 A377 A378 A379 A380 A381 A382 A383 A384 A385
DATE Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07
CH/SE/SU 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-12-00 12-12-00 12-12-00 12-12-00 12-12-00 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29
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R R R R R R R R
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A386 A387 A388 A389 A390 A391 A392 A393 A394 A395 A396 A397 A398 A399 B300 B301 B302 B303 B304 B305 B306 B307 B308
Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07
1 2 3 4 5 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315 316 317 318 319 320 321 322
Jan01/05 Jan01/05 Jan01/04 Jul01/03 Apr01/98 Jan01/05 Jan01/07 Jan01/07 Jan01/07 Apr01/98 Jan01/07 Apr01/98 Jan01/05 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Apr01/98 Jan01/05 Jan01/05 Jul01/06 Jan01/07 Jan01/05 Jan01/05 Jan01/05 Jan01/05 Jan01/05
12-L.E.P. Page 2 Jan 01/07 SROS
CH/SE/SU 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32
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323 324 325 326 327 328 329 330 331 332 333 334 335 336 337 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315 316 317 318 319 320 321 322 323 324 325 326 327 328 329 330 331 332 333 334 335 336
DATE Jan01/05 Jan01/05 Jan01/05 Jan01/05 Jan01/05 Jan01/05 Jul01/06 Jan01/05 Jan01/05 Jan01/05 Jan01/05 Jan01/05 Jan01/05 Jan01/05 Jan01/05 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jan01/04 Jan01/04 Jan01/04 Jan01/04 Jul01/06 Jul01/06 Jul01/06 Jan01/07 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jan01/07 Jul01/06 Jul01/06 Jan01/07 Jul01/06 Jul01/06
CH/SE/SU
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12-12-32 12-12-32 12-12-32 12-12-32 12-13-00 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24
01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 02 02 02 02 02 02 02 02 02 02 02 02 02 02
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337 338 339 340
Jul01/06 Jul01/06 Jul01/06 Jul01/06
1 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315 316 317 318 319 320 321 322 323 324 325 326 327 328 329 330 331 301 302 303 304 305 306 307 308 309 310 311 312 313 314
Apr01/98 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jan01/06 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jan01/02 Jan01/06 Jan01/06 Jan01/06 Oct01/00 Jan01/06 Jan01/06 Jan01/06 Jan01/02 Jan01/02 Jan01/02 Jan01/02 Jan01/02 Jan01/02
CH/SE/SU
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12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27
02 02 02 02 02 02 02 02 02 02 02 02 02 02 02
315 316 317 318 319 320 321 322 323 324 325 326 327 328 329 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315 316 317 318 319 320 321 322 323 324 325 326 327 328 329 330 331 332 333 334 335 336
DATE Jul01/05 Jul01/05 Jan01/06 Apr01/04 Jan01/06 Jan01/06 Jan01/02 Jan01/02 Jan01/02 Jan01/02 Jan01/02 Jan01/02 Apr01/03 Apr01/03 Jan01/02 Jan01/05 Jul01/02 Apr01/02 Apr01/02 Jul01/06 Jan01/05 Jan01/06 Jul01/02 Oct01/01 Apr01/01 Jan01/06 Jan01/06 Jan01/05 Jul01/02 Jul01/06 Jul01/01 Apr01/02 Apr01/05 Jul01/06 Apr01/02 Jan01/06 Jul01/06 Jul01/01 Jul01/01 Apr01/05 Oct01/01 Oct01/01 Jan01/05 Jan01/02 Jul01/06 Jul01/01 Jul01/02 Oct01/01 Jul01/06 Jan01/02 Jan01/02
12-L.E.P. Page 3 Jan 01/07 SROS
CH/SE/SU 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-29 12-13-29 12-13-29 12-13-29 12-13-29 12-13-29 12-13-29 12-13-49 12-13-49 12-13-49 12-13-49 12-13-49 12-13-49 12-13-49 12-13-49 12-13-49 12-13-49 12-13-49 12-13-49 12-13-49 12-13-49 12-13-49
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DATE Jul01/06 Jan01/02 Jan01/02 Jan01/06 Jul01/05 Jul01/05 Jul01/05 Jul01/06 Jul01/06 Jul01/06 Jul01/05 Jul01/05 Jan01/05 Jan01/06 Jan01/06 Jan01/06 Jul01/06 Jan01/03 Jul01/06 Jul01/06 Jan01/03 Jul01/06 Jan01/03 Jul01/06 Jan01/05 Jan01/03 Jan01/03 Jan01/03 Jan01/03 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/05 Jul01/02 Apr01/02 Apr01/98 Apr01/98 Apr01/02 Jul01/02 Apr01/02 Jan01/05 Jan01/05 Jul01/02 Apr01/02 Apr01/02 Apr01/02 Apr01/02
CH/SE/SU
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12-13-49 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79
01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 02 02 02 02 02 02 02 02 02
316 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315 316 317 318 319 320 321 322 323 324 325 326 327 328 329 330 331 332 333 334 335 336 337 338 339 340 341 301 302 303 304 305 306 307 308 309
DATE Apr01/02 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/01 Apr01/02 Jul01/01 Apr01/05 Apr01/05 Apr01/05 Apr01/05 Apr01/05 Apr01/05
CH/SE/SU
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12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80
02 02 02 02 02 02 02 02 02 02 02 02 02 02 02 01 01 01 01 01 01 01 01 01 01 01 R 01 01 01 01 01 01 01 01 01 01 01 01 R 01 01 01 01 01 01 01 01 01 01 01 01 01
310 311 312 313 314 315 316 317 318 319 320 321 322 323 324 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315 316 317 318 319 320 321 322 323 324 325 326 327 328 329 330 331 332 333 334 335 336
DATE Apr01/05 Oct01/00 Oct01/04 Jul01/03 Jul01/03 Apr01/02 Oct01/00 Jul01/04 Oct01/00 Oct01/00 Jul01/03 Oct01/00 Jul01/03 Jul01/03 Jul01/03 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jan01/07 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jan01/07 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jan01/06
12-L.E.P. Page 4 Jan 01/07 SROS
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12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80
01 01 01 01 01 01 02 02 02 02 02 02 02 02 02 02 02 02 02
337 338 339 340 341 342 301 302 303 304 305 306 307 308 309 310 311 312 313
Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Apr01/05 Oct01/00 Oct01/00 Oct01/00 Oct01/00 Oct01/00 Oct01/00 Oct01/00 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04
1 301 302 303 304 305 306 307 308 309 310 311 312 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315 316 317 318
Apr01/98 Jan01/07 Jan01/07 Apr01/98 Jul01/06 Jan01/07 Jan01/07 Apr01/98 Jul01/06 Jan01/07 Jan01/07 Apr01/98 Jul01/06 Jan01/07 Jan01/07 Jan01/03 Jan01/07 Jul01/06 Apr01/04 Jul01/06 Apr01/98 Apr01/04 Jul01/04 Jul01/04 Jul01/06 Jul01/06 Jul01/06 Apr01/03 Apr01/03 Apr01/03 Jan01/07
12-14-00 12-14-29 12-14-29 12-14-29 12-14-29 12-14-29 12-14-29 12-14-29 12-14-29 12-14-29 12-14-29 12-14-29 12-14-29 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32
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CH/SE/SU 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-35 12-14-35 12-14-35 12-14-35 12-14-35 12-14-35 12-15-00 12-15-38 12-15-38 12-15-38 12-15-38
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319 320 321 322 323 324 325 326 327 328 329 330 331 332 333 334 335 336 337 338 339 340 341 342 343 344 345 346 347 348 349 350 351 352 353 354 355 356 357 301 302 303 304 305 306
Jul01/06 Jul01/06 Apr01/04 Apr01/04 Jan01/07 Jan01/07 Jan01/07 Apr01/04 Jan01/07 Apr01/04 Jan01/07 Jan01/07 Apr01/05 Apr01/04 Jul01/06 Apr01/04 Jan01/07 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jan01/05 Apr01/04 Apr01/04 Apr01/04 Apr01/04 Apr01/04 Apr01/04 Jul01/03 Jan01/05 Apr01/05 Apr01/04 Apr01/04 Jul01/03 Apr01/04 Apr01/05 Apr01/04 Jan01/06 Jul01/03 Oct01/04 Oct01/04 Apr01/00 Apr01/02 Apr01/98 Apr01/02
1 301 302 303 304
Apr01/98 Jul01/05 Jul01/06 Jul01/05 Jul01/03
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12-15-38 12-15-38 12-15-38 12-15-38 12-15-38 12-15-38 12-15-38 12-15-38 12-15-38 12-15-38
305 306 307 308 309 310 311 312 313 314
Jul01/98 Jul01/05 Jul01/05 Jul01/03 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05
12-16-00 12-16-25 12-16-25 12-16-25 12-16-25 12-16-25 12-16-38 12-16-38 12-16-38 12-16-38 12-16-38 12-16-38 12-16-38 12-16-38
1 301 302 303 304 305 301 302 303 304 305 306 307 308
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12-L.E.P. Page 5 Jan 01/07 SROS
CH/SE/SU 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12
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DATE Apr01/05 Jul01/05 Jul01/05 Apr01/05 Apr01/05 Apr01/05 Jul01/06 Apr01/05 Apr01/05 Apr01/05 Apr01/05 Jul01/06 Jul01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/07 Jan01/07 Jan01/06 Jan01/07 Jan01/07 Jan01/07 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Apr01/05 Apr01/05 Apr01/05 Apr01/05 Apr01/05 Apr01/05 Jan01/06 Jul01/06 Jul01/06 Jan01/07 Jul01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jul01/06 Jul01/06 Jan01/07 Jul01/06 Jul01/06 Jan01/06
CH/SE/SU 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-22-00 12-22-00 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27
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357 358 359 360 361 362 363 364 365 366 367 368 369 701 702 703 704 705 706 707 708 709 710 711 712 713 714 715 716 717 718 719 720
Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/07 Jan01/07 Jan01/06 Jan01/06 Jan01/06 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07
1 2 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315
Apr01/98 Apr01/98 Jan01/05 Apr01/05 Jul01/06 Jan01/04 Jan01/07 Jan01/07 Jul01/06 Jul01/06 Jul01/06 Apr01/03 Jul01/02 Jan01/02 Jan01/02 Jul01/06 Jul01/06
CH/SE/SU 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27
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316 317 318 319 320 321 322 323 324 325 326 327 328 329 330 331 332 333 334 335 336 337 338 339 340 341 342 343 344 345 346 347 348 349 350 351 352 353 354 355 356 357 358 359 360 361 362 363 364 365 366
DATE Jan01/06 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jan01/06 Jan01/06 Jul01/06 Jul01/06 Jul01/06 Apr01/04 Apr01/04 Jan01/05 Jul01/04 Apr01/04 Jul01/04 Jul01/04 Jan01/05 Jan01/06 Oct01/03 Oct01/03 Apr01/04 Jan01/05 Jan01/06 Oct01/04 Oct01/04 Oct01/03 Oct01/03 Jan01/07 Jan01/07 Jan01/06 Jan01/07 Jan01/06 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07
12-L.E.P. Page 6 Jan 01/07 SROS
CH/SE/SU 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32
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DATE Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jan01/07 Jan01/07 Jul01/06 Jul01/06 Jul01/06 Jul01/06
CH/SE/SU 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52
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328 329 330 331 332 333 334 335 336 337 338 339 340 341 342 343 344 345 346 347 348 349 350 351 352 353 354 355 356 357 358 359 360 361 362 363 364 365 366 367 368 369 370 371 372 373 301 302 303 304 305
DATE Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jul01/06 Jul01/06 Jan01/07 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jan01/07 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jan01/07 Jul01/06 Jul01/06 Jul01/06 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07
Jan01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/99
CH/SE/SU 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52
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DATE Jul01/05 Jul01/99 Apr01/04 Apr01/04 Jul01/05 Jul01/99 Apr01/04 Apr01/04 Jul01/05 Apr01/04 Apr01/04 Apr01/04 Apr01/04 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Oct01/99 Jul01/06 Oct01/99 Oct01/99 Oct01/99 Jul01/06 Oct01/99 Jan01/05 Apr01/03 Apr01/03 Apr01/03 Jan01/05 Jul01/05 Jul01/05 Apr01/03 Jul01/05 Jul01/06 Apr01/04 Apr01/04 Apr01/04 Apr01/04 Apr01/04 Jul01/05 Apr01/04 Apr01/03 Jul01/05 Jul01/05 Jul01/05 Apr01/03 Jul01/05
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12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-53 12-22-53 12-22-53 12-22-53 12-22-53 12-22-53 12-22-53 12-22-53 12-22-55 12-22-55 12-22-55 12-22-55 12-22-56 12-22-56 12-22-56
357 358 359 360 361 362 363 364 301 302 303 304 305 306 307 308 301 302 303 304 301 302 303
Jul01/05 Jul01/05 Jul01/05 Jul01/05 Apr01/05 Jul01/05 Apr01/05 Apr01/05 Jul01/04 Apr01/03 Jul01/04 Jul01/04 Jul01/04 Jan01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/00 Jul01/00 Oct01/04 Apr01/98 Apr01/98
12-24-00 12-24-29 12-24-29 12-24-29 12-24-29 12-24-29 12-24-34 12-24-34 12-24-38 12-24-38 12-24-38 12-24-38 12-24-38 12-24-38 12-24-38 12-24-38 12-24-38 12-24-38 12-24-38 12-24-38 12-24-38 12-24-38 12-24-38 12-24-38 12-24-38 12-24-38 12-24-38
1 301 302 303 304 305 301 302 201 202 203 204 205 206 207 208 209 210 211 212 213 214 215 216 217 218 219
Apr01/98 Jul01/06 Apr01/04 Apr01/04 Oct01/01 Jul01/06 Apr01/98 Apr01/98 Oct01/01 Jul01/06 Jan01/06 Jul01/06 Jul01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06
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220 221 222 223
DATE Jan01/06 Jan01/06 Jan01/06 Jan01/06
12-28-00
1 Jul01/06
12-30-00
1 Apr01/98
12-31-00 12-31-00 12-31-00 12-31-00 12-31-00 12-31-00 12-31-11 12-31-11 12-31-11 12-31-11 12-31-11 12-31-11 12-31-11 12-31-11 12-31-11 12-31-11 12-31-12 12-31-12 12-31-12 12-31-12 12-31-12 12-31-12 12-31-12 12-31-12 12-31-12 12-31-12 12-31-12 12-31-12 12-31-12 12-31-12 12-31-12 12-31-12 12-31-12 12-31-12 12-31-12 12-31-21 12-31-21 12-31-21 12-31-24 12-31-24 12-31-25 12-31-25
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1 2 3 4 5 6 201 202 203 204 205 206 207 208 209 210 201 202 203 204 205 206 207 208 209 210 211 212 213 214 215 216 217 218 219 201 202 203 201 202 201 202
Oct01/04 Oct01/04 Jan01/07 Oct01/04 Oct01/04 Oct01/04 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Oct01/04 Oct01/04 Oct01/04 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Oct01/04 Oct01/04 Oct01/04 Oct01/04 Jul01/06 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Oct01/01 Oct01/01 Apr01/98 Jan01/07 Apr01/98 Apr01/02 Jan01/01
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12-31-25 12-31-25 12-31-25 12-31-27 12-31-27 12-31-27 12-31-28 12-31-28 12-31-28 12-31-28 12-31-28 12-31-31 12-31-31 12-31-32 12-31-32 12-31-32 12-31-32 12-31-32 12-31-32 12-31-32 12-31-35 12-31-35 12-31-38 12-31-38 12-31-38 12-31-38 12-31-38 12-31-38 12-31-38 12-31-38 12-31-38 12-31-49 12-31-49 12-31-49 12-31-49 12-31-51 12-31-51 12-31-51 12-31-52 12-31-52 12-31-52 12-31-52 12-31-52 12-31-52 12-31-52 12-31-52 12-31-71 12-31-71 12-32-00 12-32-24 01
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1 Jul01/05 301 Jul01/05
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12-32-24 12-32-24 12-32-24 12-32-24 12-32-24 12-32-24 12-32-24 12-32-24 12-32-24 12-32-24 12-32-24 12-32-24 12-32-24 12-32-24 12-32-24 12-32-24 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28
01 01 01 01 01 01 01 01 02 02 02 02 02 02 02 02
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CH/SE/SU 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-28 12-32-29 12-32-29 12-32-29 12-32-29 12-32-29 12-32-29 12-32-29 12-32-29 12-32-29 12-32-29 12-32-29 12-32-29 12-32-29 12-32-49 12-32-49 12-32-49 12-32-49 12-32-49 12-32-79 12-32-79 12-32-79 12-32-79 12-32-79 12-32-79 12-32-79 12-32-79 12-32-79 12-32-79 12-33-00 12-33-21 12-33-21 12-33-21 12-33-21 12-33-21 12-33-21 12-33-21 12-33-21 12-33-21 12-33-21 12-33-21 12-33-21
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336 337 338 339 340 341 342 343 344 301 302 303 304 305 306 307 308 309 310 311 312 313 301 302 303 304 305 301 302 303 304 305 306 301 302 303 304
Jul01/06 Jul01/06 Jan01/07 Jan01/06 Jan01/06 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/06 Jan01/07 Jan01/07 Apr01/98 Apr01/98 Jan01/06 Jan01/06 Jul01/06 Jan01/06 Jul01/06 Jan01/06 Oct01/00 Jul01/00 Oct01/00 Jul01/00 Oct01/00 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Apr01/02 Apr01/02 Apr01/02 Apr01/02
1 201 202 203 204 205 206 207 208 209 210 211 212
Jul01/06 Jan01/03 Jan01/03 Apr01/98 Jan01/03 Jan01/03 Jan01/03 Jan01/03 Jan01/06 Jan01/03 Jan01/03 Jan01/03 Jan01/03
R R R R R R R R R
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12-33-21 12-33-21 12-33-21 12-33-21 12-34-00 12-34-24 12-34-24 12-34-24 12-34-24 12-34-24 12-34-24 12-34-24 12-36-00 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29
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213 214 215 216
Jan01/06 Jan01/04 Jan01/03 Jan01/03
1 201 202 203 204 205 206 207
Apr01/98 Jan01/07 Jan01/07 Apr01/98 Apr01/98 Jan01/07 Jan01/07 Jan01/07
1 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315 316 317 318 319 320 321 322 323 324 325 326 327 328 329 330 331 332 333 334 335 336
Apr01/98 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Apr01/02 Apr01/05 Oct01/02 Oct01/04 Oct01/04 Oct01/04 Oct01/04 Oct01/04 Oct01/04 Oct01/04 Apr01/01 Apr01/01 Apr01/01 Jul01/05 Jan01/07 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jan01/07 Jul01/05 Jul01/05 Jan01/07 Jul01/05
12-L.E.P. Page 9 Jan 01/07 SROS
CH/SE/SU 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29
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DATE Apr01/01 Apr01/05 Apr01/01 Apr01/01 Oct01/04 Apr01/01 Apr01/01 Apr01/01 Apr01/01 Apr01/01 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Apr01/01 Apr01/05 Apr01/01 Oct01/04 Apr01/01 Apr01/01 Apr01/01 Apr01/01 Apr01/01 Apr01/01 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Apr01/01 Apr01/05 Apr01/01 Oct01/04 Apr01/01 Apr01/01 Apr01/01 Apr01/01 Apr01/01 Jul01/05
CH/SE/SU 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29
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DATE Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Apr01/01 Apr01/05 Apr01/01 Oct01/04 Apr01/01 Apr01/01 Apr01/01 Apr01/01 Apr01/01 Apr01/01 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Apr01/01 Apr01/05 Apr01/01 Oct01/04 Apr01/01 Apr01/01 Apr01/01 Apr01/01 Apr01/01 Jul01/05 Jan01/07 Jan01/07 Jul01/05 Apr01/01 Apr01/01 Apr01/01 Oct01/04 Jul01/05 Jul01/05 Jul01/05 Jul01/05
CH/SE/SU 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29
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A339 A340 A341 A342 A343 A344 A345 A346 A347 A348 A349 A350 A351 A352 A353 A354 A355 A356 A357 A358 A359 A360 A361 A362 A363 A364 A365 A366 A367 A368 A369 A370 A371 A372 A373 A374 A375 A376 A377 A378 A379 A380 A381 A382 A383 A384 A385 A386 A387 A388 A389
DATE Apr01/01 Apr01/01 Apr01/01 Oct01/04 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Apr01/01 Apr01/01 Apr01/01 Oct01/04 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07
12-L.E.P. Page 10 Jan 01/07 SROS
CH/SE/SU 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29
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A390 A391 A392 A393 A394 A395 A396 A397 A398 A399 B300 B301 B302 B303 B304 B305 B306 B307 B308 B309 B310 B311 B312 B313 B314 B315 B316 B317 B318 B319 B320 B321 B322 B323 B324 B325 B326 B327 B328 B329 B330 B331 B332 B333 B334 B335 B336 B337 B338 B339 B340
DATE Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07
CH/SE/SU 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29
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B341 B342 B343 B344 B345 B346 B347 B348 B349 B350 B351 B352 B353 B354 B355 B356 B357 B358 B359 B360 B361 B362 B363 B364 B365 B366 B367 B368 B369 B370 B371 B372 B373 B374 B375 B376 B377 B378 B379 B380 B381 B382 B383 B384 B385 B386 B387 B388 B389 B390 B391
DATE Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07
CH/SE/SU 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29
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B392 B393 B394 B395 B396 B397 B398 B399 C300 C301 C302 C303 C304 C305 C306 C307 C308 C309 C310 C311 C312 C313 C314 C315 C316 C317 C318 C319 C320 C321 C322 C323 C324 C325 C326 C327 C328 C329 C330 C331 C332 C333 C334 C335 C336 C337 C338 C339 C340 C341 C342
DATE Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07
12-L.E.P. Page 11 Jan 01/07 SROS
CH/SE/SU 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29 12-36-29
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C343 C344 C345 C346 C347 C348 C349 C350 C351 C352 C353 C354 C355 C356 C357 C358 C359 C360 C361
DATE
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DATE
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DATE
Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07
12-L.E.P. Page 12 Jan 01/07 SROS
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ _______ SUBJECT SERVICING - GENERAL ___________________ DESCRIPTION AND OPERATION General NO STEP Areas NO STEP Areas on the Wing NO STEP Areas on the THS Ground Service Connections Drainage Points General Hydraulic Safety Procedures Hydraulic System Pressurization Safety Instructions Applicable to Hydraulic Fluid Technical Safety Instructions
________ CH/SE/SU 12-00-00
____________________ SERVICING - GENERAL MAINTENANCE PRACTICES Installation of the Wing Safety Rope Removal of the Wing Safety Rope
12-00-00
____________ REPLENISHING DESCRIPTION AND OPERATION General
12-10-00
FUEL
12-11-00
DESCRIPTION AND OPERATION General FUEL SYSTEM SERVICING General Refuel/Defuel Safety Procedures Refuel/Defuel Safety Procedures In The Hangar Pressure Refuel with Automatic Control from the Panel 990VU Pressure Refuel With Manual Control Pressure Refuel with Automatic Control from the Cockpit Pressure Refuel with Manual Control and Override of Individual Inlet Valve(s)
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PAGE ___________ ____ EFFECTIVITY 1 1 1 1 1 1 1 1
ALL ALL ALL ALL ALL ALL ALL ALL
1 10
ALL ALL
10
ALL
201 201
ALL ALL
205
ALL
1 1
ALL ALL
1 1
ALL ALL
301 301
ALL ALL
307
ALL
308
ALL
319
ALL
393
201-249, 251-252 255-299, 301-399 401-449, 451-499 701-749, ALL
12-11-28
A301
12-CONTENTS R SROS
Page 1 Jan 01/07
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ _______ SUBJECT Overwing Refuel Procedure Procedure To Use The Fuel Magnetic Level Indicators Procedure To Use The ADIRU to Find the Pitch and Roll Data
CH/SE/SU ________
HYDRAULIC FLUIDS DESCRIPTION AND OPERATION General Specification of Phosphate Ester-Base Fluids Fluid Monitoring Hydraulic Ground Power Cart Hydraulic Fluid Property In-Service Limits Specification of Mineral-Base Fluids Safety Precautions HYDRAULIC POWER SERVICING Fill the Green Hydraulic Reservoir with a Hydraulic Service Cart Fill the Green Hydraulic Reservoir with a Hand Pump Fill the Blue Hydraulic Reservoir with a Hydraulic Service Cart Fill the Blue Hydraulic Reservoir with a Hand Pump Fill the Yellow Hydraulic Reservoir with a Hydraulic Service Cart Fill the Yellow Hydraulic Reservoir with a Hand Pump LANDING GEAR SERVICING Hydraulic Replenishment of the MLG Shock Absorber (Aircraft on Jacks) Hydraulic Replenishment of the MLG Shock Absorber (Weight on Wheels) Hydraulic Replenishment of the NLG Shock Absorber (Aircraft on Jacks)
12-12-00
OIL
12-13-00
DESCRIPTION AND OPERATION General ELECTRICAL POWER
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____ ___________ PAGE EFFECTIVITY A315 ALL A322 ALL B302
ALL
1 1 1
ALL ALL ALL
1 3 3
ALL ALL ALL
3
ALL
3
ALL
301 301
ALL ALL
308
ALL
314
ALL
320
ALL
327
ALL
332
ALL
301 301
ALL ALL
322
ALL
331
ALL
1 1
ALL ALL
12-12-29
12-12-32
12-13-24 12-CONTENTS
R SROS
Page 2 Jan 01/07
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ _______ SUBJECT SERVICING
CH/SE/SU ________
_ C 1
Draining of the Oil from the IDG
IDG Servicing - Filling of the IDG with Oil or Addition of Oil after a Level Check Drain IDG Oil System, Discard Filter Element and Replenish SERVICING Draining of the Oil from the IDG IDG Servicing - Filling of the IDG with Oil or Addition of Oil after Level Check Drain IDG Oil System, Discard Filter Element and Replenish FLIGHT CONTROLS SERVICING Oil Replenishing of the THS Actuator (1CS) Oil Replenishing of the Flap Power Control Unit (PCU) Gearbox (5000CV) Oil Replenishing of the Slat Power Control-Unit (PCU) Gearbox (5000CW) Drain and Refill the Rotary Actuators Oil Replenishing of the Flap System Torque Limiter (5003CV, 5081CV) Oil Replenishing of the Slat System Torque Limiter (5009CW, 5069CW) Semi-Fluid Sampling and Replenishing of the Input Gearbox (5007CV, 5022CV, 5032CV, 5042CV, 5053CV, 5085CV, 5100CV, 5110CV, 5120CV, 5131CV)
2
____ EFFECTIVITY PAGE ___________ 301 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 301 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 309 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 319 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 301 701-749, 301 701-749, 309 701-749, 318
701-749,
301 301
ALL ALL
306
ALL
313
ALL
318
ALL
328
ALL
334
ALL
340
002-049, 202-249 252-252, 255-299 301-399, 451-499 701-749,
12-13-27
12-CONTENTS R SROS
Page 3 Jul 01/06
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ _______ SUBJECT Oil Draining of the Flap/Slat PCU (5000CV, 5000CW) Oil Draining of the Flap/Slat System Torque Limiter (5003CV, 5081CV, 5009CW, 5069CW) Sampling of the SEMIFLUID from the Flap Rotary Actuator HYDRAULIC POWER SERVICING Oil Replenishment of the Ram Air Turbine (RAT) (11JR) APU SERVICING Gravity Servicing of the APU Oil Reservoir Pressure Servicing of the APU Oil Reservoir ENGINE OIL SERVICING
CH/SE/SU ________
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____ ___________ PAGE EFFECTIVITY 349 ALL 354
ALL
360
ALL
301 301
ALL ALL
301 301
ALL ALL
310
ALL
301
001-049, 251-252, 301-399, 451-499, 001-049, 251-252, 301-399, 451-499, 001-049, 251-252, 301-399, 451-499, 001-049, 251-252, 301-399, 451-499, 001-049, 251-252, 301-399, 451-499, 701-749, 701-749, 701-749,
12-13-29
12-13-49
12-13-79 1
Servicing of the Engine Oil System
301
Filling the Engine Oil System after the Replacement of an Oil System Component
311
Changing the Oil in the Engine Oil System
324
Flushing the Oil in the Engine Oil System.
337
SERVICING To Service the Engine Oil System Drain the Engine Oil System ENGINE STARTING SERVICING
2
301 301 311
1
301
SROS
201-249 255-299 401-449 201-249 255-299 401-449 201-249 255-299 401-449 201-249 255-299 401-449
12-13-80 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499,
12-CONTENTS R
201-249 255-299 401-449
Page 4 Jul 01/05
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ _______ SUBJECT Servicing of the Starter (Pressure and Gravity Fill - with Thrust Reverser Cowl Doors Open)
CH/SE/SU ________
C _
Change Starter Oil (with the Threaded Type Starter Magnetic Chip Detector (Vickers/Tedeco)) Change Starter Oil (with the Bayonet Type Starter Magnetic Chip Detector (Lisle)) Check and Replenish Starter Oil by Remote Fill - Through Access Door SERVICING To Service the Pneumatic Starter Oil System To Change the Oil in the Pneumatic Starter GAS DESCRIPTION AND OPERATION General HYDRAULIC POWER SERVICING Fill the Green Power Accumulator (5151JM1) with Nitrogen Fill the Blue Power Accumulator (5151JM2) with Nitrogen Fill the Yellow Power Accumulator (5151JM3) with Nitrogen LANDING GEAR SERVICING Replenishment of the Tires Gas Replenishment of the MLG Shock Absorber Gas Replenishment of the NLG Shock Absorber Pressurization of the Brake Accumulator (5258GG, 5259GG, 5490GG, 5491GG, 5426GG, 5427GG) Depressurization of the Brake Accumulator (5258GG, 5259GG, 5490GG, 5491GG, 5426GG and 5427GG)
2
____ EFFECTIVITY PAGE ___________ 301 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 311 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 323 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 336 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 301 701-749, 301 701-749, 308
701-749,
12-14-00 1 1
ALL ALL
301 301
ALL ALL
305
ALL
309
ALL
301 301 305
ALL ALL ALL
318
ALL
331
ALL
340
ALL
12-14-29
12-14-32
12-CONTENTS R SROS
Page 5 Jan 01/07
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ _______ SUBJECT Depressurization of the Nose Wheel Steering Accumulator 5110GC Pressurization of the Nose Wheel Steering Accumulator 5110GC OXYGEN SERVICING Servicing of the Oxygen Replenishing
CH/SE/SU ________
WATER DESCRIPTION AND OPERATION General POTABLE WATER SERVICING Fill the Potable Water System (Aircraft Electrical Power Available) Fill the Potable Water System (Aircraft Electrical Power not Available)
12-15-00
LAVATORY DESCRIPTION AND OPERATION General LAVATORY ARTICLE SERVICING Servicing of the Liquid Soap Dispenser TOILET SANITARY FLUID SERVICING Servicing of the Toilet System
12-16-00
RAIN REPELLENT DESCRIPTION AND OPERATION General ICE AND RAIN PROTECTION SERVICING Do a Check of Rain Repellent Fluid Can Assy For Correct Fluid Level and Pressure
12-17-00
___________________ SCHEDULED SERVICING DESCRIPTION AND OPERATION General
12-20-00
CLEANING
12-21-00
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____ ___________ PAGE EFFECTIVITY 348 ALL 353
ALL
301 301
ALL ALL
1 1
ALL ALL
301 301
ALL ALL
310
ALL
1 1
ALL ALL
301 301
ALL ALL
301 301
ALL ALL
1 1
ALL ALL
301 301
ALL ALL
1 1
ALL ALL
12-14-35
12-15-38
12-16-25
12-16-38
12-17-30
12-CONTENTS R SROS
Page 6 Jul 01/05
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ _______ SUBJECT DESCRIPTION AND OPERATION General EXTERNAL CLEANING SERVICING External Cleaning INTERNAL CLEANING SERVICING Cleaning of the Cockpit Display-Units Cleaning of the Cockpit Equipment/Furnishings Cleaning of the Carpets and Non-Textile Floor (NTF) Covering Cleaning of the Plastic Surfaces and Mirrors Cleaning of the Curtains Cleaning of Light Alloy and Steel Components Cleaning of the Cargo Compartments Cleaning of the Monitors and Display Screens in the Cabin Cleaning of the Plastic Wash Basin in the Lavatories Cleaning of the Seat Covers Cleaning of the Air Inlet Grids of Galleys and Lavatories Disinfection of the Aircraft Equipment and Furnishing Fumigation of the Aircraft Equipment and Furnishing Fumigation of the Fuselage Pressurized Areas with Carbon-Dioxide (CO2 Gas) Special Precautions to Apply Insecticide Agent in Auxiliary Area Compartments and Cargo Compartments, during Turn-Around DUST REMOVAL CLEANING/PAINTING Dust Removal Cleaning of Relay Box VU Panel Grids
CH/SE/SU ________
LUBRICATION DESCRIPTION AND OPERATION General
12-22-00
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____ ___________ PAGE EFFECTIVITY 1 ALL 1 ALL
12-21-11 301 301
ALL ALL
301 301
ALL ALL
304
ALL
309
ALL
312
ALL
319 321
ALL ALL
323 329
ALL ALL
331
ALL
336 339
ALL ALL
342
ALL
348
ALL
356
ALL
367
ALL
701 701 717
ALL ALL ALL
1 1
ALL ALL
12-21-12
12-21-13
12-CONTENTS R SROS
Page 7 Jan 01/07
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ SUBJECT _______ Lubrication Point Symbols: FLIGHT CONTROLS SERVICING Lubricate the Trimmable Horizontal Stabilizer (THS) Actuator Ball Screw Nut Lubricate the Trimmable Horizontal Stabilizer (THS) Mechanical Control Chains Lubrication of Flap Track/Carriage (1-5) Roller Bearings Lubrication of all Slat Track Roller Bearings, Pinion Bearings, Rack and Pinion Teeth and Slat Track 2 and 3 Lever Bearings Lubrication of all Spoiler Linkage Bearings fitted with Grease Nipples Lubrication of Flap Steady Bearings Lubrication of the Aileron Hinge Bearings Lubrication of Slat Rotary Actuator Type A (Track 2-3) Lubrication of Slat Rotary Actuator Type B (Track 5-16) Lubrication of Rudder Servo-Control Roller-Bearings (Rudder Side) Lubrication of the Aileron Actuator Roller Bearings Lubrication of Slat Steady Bearings Lubrication of the Elevator Actuator Roller Bearings LANDING GEAR SERVICING Lubrication of Main Landing Gear and Doors Lubrication of Nose Gear and Doors Lubrication of MLG Bogie Pivot Pin DOORS SERVICING Lubrication of the FWD Cargo-Compartment Door Hinge Arm Bearings, Locking Mechanism,
CH/SE/SU ________
C _
____ ___________ PAGE EFFECTIVITY 1 ALL
12-22-27 301 301
ALL ALL
307
ALL
316
ALL
322
ALL
329
ALL
334
ALL
339
ALL
345
ALL
352
ALL
367
ALL
373
ALL
379
ALL
385
ALL
301 301
ALL ALL
336 359
ALL ALL
301 301
ALL ALL
12-22-32
12-22-52
12-CONTENTS R SROS
Page 8 Jan 01/07
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ _______ SUBJECT Latching Mechanism and Interlock Mechanism Lubrication of the Telescopic Arm and Exterior Control Handle Lubrication of the Telescopic Arm and Exterior Control Handle Lubrication of the BULK Cargo-Compartment Door Lubrication of the AFT Cargo-Compartment Door Hinge Arm Bearings, Locking, Latching and Interlock Mechanism Lubrication of the Slider Mechanism on all Pax/Crew and Emergency Exit Doors FUSELAGE SERVICING Lubrication of the THS Hinge Line Bearings Lubrication of the THS Upper and Lower Frame Attachment Bearings STABILIZERS SERVICING Lubrication of the Rudder Bearing No. 6 WINDOWS SERVICING Servicing of the Sliding Windows
CH/SE/SU ________
DRAINAGE DESCRIPTION AND OPERATION General HYDRAULIC POWER SERVICING Servicing of the Leakage Recovery Tank (5230JM001, 5230JM002, 5230JM003) AIR DATA SYSTEM SERVICING Draining of the Standby Static Pressure-Lines POTABLE WATER SYSTEM MAINTENANCE PRACTICES Draining of the Potable Water System (with Electrical Power) Draining of the Potable Water
12-24-00
C _
PAGE ___________ ____ EFFECTIVITY 328
ALL
332
ALL
334
ALL
338
ALL
360
ALL
301 301
ALL ALL
305
ALL
301 301
ALL ALL
301 301
ALL ALL
1 1
ALL ALL
301 301
ALL ALL
301 301
ALL ALL
201 201
ALL ALL
217
ALL
12-22-53
12-22-55
12-22-56
12-24-29
12-24-34
12-24-38
12-CONTENTS R SROS
Page 9 Jul 01/06
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ _______ SUBJECT System (without Electrical Power)
CH/SE/SU ________
USE OF MANUAL MAGNETIC FUEL QUANTITY INDICATORS DESCRIPTION AND OPERATION General General
12-28-00
_____________________ UNSCHEDULED SERVICING DESCRIPTION AND OPERATION General
12-30-00
COLD WEATHER MAINTENANCE - AIRCRAFT PROTECTION DESCRIPTION AND OPERATION General Safe operation of aircraft in cold weather conditions raises specific problems. Aircraft downtime and delays in flight schedules caused by cold Procedures for cold weather servicing during cold weather must be developed by the operator. This servicing must meet their specific This topic contains information to assist the operator in defining, developing, and implementing cold weather preventive maintenance Cold Soak Definition De-icing and Anti-icing Guidelines De-Icing and Anti-Icing Glossary An aircraft performance certification is based upon that aircraft having an uncontaminated or clean structure. De-icing and/or Anti-icing Equipment and Materials ANTI-ICING PROTECTION MAINTENANCE PRACTICES Anti-Icing Protection ICE AND SNOW REMOVAL MAINTENANCE PRACTICES
12-31-00
C _
PAGE ___________ ____ EFFECTIVITY
1 1 1
ALL ALL 251-252, 701-749
1 1
ALL ALL
1 1 1
ALL ALL ALL
1
ALL
1
ALL
1 2 2 3
ALL ALL ALL ALL
4
ALL
201 201
ALL ALL
201
ALL
12-31-11 12-31-12 12-CONTENTS
R SROS
Page 10 Jul 01/06
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ _______ SUBJECT De-icing of the Aircraft Parked in an Open Area (Engines Stopped) De-icing of the Aircraft Parked in an Open Area (Engines Running) De-icing of the Aircraft after Landing with Snow on the Runways COLD WEATHER MAINTENANCE - AIR CONDITIONING MAINTENANCE PRACTICES Cold Weather Maintenance Practices for the Air Conditioning COLD WEATHER MAINTENANCE - ELECTRICAL POWER MAINTENANCE PRACTICES Cold Weather Maintenances for Electrical Power COLD WEATHER MAINTENANCE EQUIPMENT/FURNISHINGS MAINTENANCE PRACTICES Cold Weather Maintenance Practices for Equipment/Furnishings COLD WEATHER MAINTENANCE - FLIGHT CONTROLS MAINTENANCE PRACTICES Cold Weather Maintenance Procedures for Flight Controls COLD WEATHER MAINTENANCE - FUEL MAINTENANCE PRACTICES Cold Weather Maintenance Practices for the Fuel System COLD WEATHER MAINTENANCE INDICATING/RECORDING SYSTEMS AND NAVIGATION MAINTENANCE PRACTICES Cold Weather Maintenance Practices for Indicating/Recording and Navigation Systems COLD WEATHER MAINTENANCE - LANDING GEAR MAINTENANCE PRACTICES Cold Weather Maintenance Practices for the Landing Gear Cold Weather Protection for the Landing Gear Axles COLD WEATHER MAINTENANCE - OXYGEN MAINTENANCE PRACTICES
CH/SE/SU ________
C _
____ ___________ PAGE EFFECTIVITY 201 ALL 212
ALL
218
ALL
201 201
ALL ALL
201 201
ALL ALL
201 201
ALL ALL
201 201
ALL ALL
201 201
ALL ALL
201 201
ALL ALL
201 201
ALL ALL
203
ALL
201
ALL
12-31-21
12-31-24
12-31-25
12-31-27
12-31-28
12-31-31
12-31-32
12-31-35 12-CONTENTS
R SROS
Page 11 Jan 01/07
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ _______ SUBJECT Cold Weather Maintenance - Oxygen System COLD WEATHER MAINTENANCE - WATER/ WASTE MAINTENANCE PRACTICES Cold Weather Maintenance Practices for Water/Waste COLD WEATHER MAINTENANCE - AIRBORNE AUXILIARY POWER MAINTENANCE PRACTICES Cold Weather Maintenance Practices for the Auxiliary Power Unit COLD WEATHER MAINTENANCE - STRUCTURE MAINTENANCE PRACTICES Cold Weather Maintenance Practices for the Structure. COLD WEATHER MAINTENANCE - DOORS MAINTENANCE PRACTICES Cold Weather Maintenance Procedures for the Doors System COLD WEATHER MAINTENANCE - POWER PLANT MAINTENANCE PRACTICES Cold Weather Maintenance Practices of Engines
CH/SE/SU ________
SAMPLING FOR ANALYSIS DESCRIPTION AND OPERATION General
12-32-00
General INTEGRATED DRIVE GENERATOR OIL SERVICING
C _
12-31-38 201 201
ALL ALL
201 201
ALL ALL
201 201
ALL ALL
201 201
ALL ALL
201 201
ALL ALL
12-31-49
12-31-51
12-31-52
12-31-71
1 1
1
ALL 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 701-749,
12-32-24 1
Sampling of the IDG Oil for Analysis SERVICING Sampling of the IDG Oil for Analysis FUEL SERVICING
____ ___________ PAGE EFFECTIVITY 201 ALL
301
301 301
001-049, 251-252, 301-399, 451-499, 001-049, 251-252, 301-399, 451-499, 701-749, 701-749,
301
ALL
301
2
SROS
201-249 255-299 401-449
12-32-28 12-CONTENTS
R
201-249 255-299 401-449
Page 12 Jan 01/07
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ _______ SUBJECT Operate Water Drain Valves to Drain Accumulated Water from Center, Inner, Outer and Wing Vent Surge Tanks Operate Water Drain Valves to Drain Accumulated Water from Trim Tank and Trim Vent Surge Tank Draining of the Fuel/Air Separator Operate the Drain Valve of the Fuel/Air Separator to Drain any Accumulated Water Heating of Fuel/Air Separator Warm Fuel Procedure Heating of Fuel/Air Separator Hot Air Procedure Sample Fuel for Microbiological Contamination Analysis HYDRAULIC FLUID SERVICING Sampling for Analysis APU SERVICING Oil Sampling for Analysis ENGINE OIL SERVICING
CH/SE/SU ________
C _
308
ALL
315 320
ALL ALL
327
ALL
330
ALL
333
ALL
301 301
ALL ALL
301 301
ALL ALL
301
001-049, 251-252, 301-399, 451-499, 001-049, 251-252, 301-399, 451-499, 701-749, 701-749,
12-32-29 12-32-49 12-32-79 1
Sampling of the Engine Oil.
301
SERVICING Get a Sample of Engine Oil for Analysis PRE-CONDITIONING DESCRIPTION AND OPERATION General System Description Pre-conditioning with the Low Pressure (LP) Ground Connector Pre-conditioning with the High Pressure (HP) Ground Connector Pre-conditioning with the APU Bleed Air Supply
____ ___________ PAGE EFFECTIVITY 301 ALL
2
301 301
SROS
201-249 255-299 401-449
12-33-00 1 1 1 1
ALL ALL ALL ALL
1
ALL
1
ALL
12-CONTENTS R
201-249 255-299 401-449
Page 13 Jan 01/07
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ _______ SUBJECT GROUND AIR PRE-CONDITIONING MAINTENANCE PRACTICES Pre-conditioning through the Low-Pressure Ground Connection Pre-conditioning through the High-Pressure Ground Connection Pre-conditioning with the APU
________ CH/SE/SU 12-33-21
GROUNDING POINTS DESCRIPTION AND OPERATION General AIRCRAFT GROUNDING MAINTENANCE PRACTICES Aircraft Grounding for the Refuel/Defuel and Oxygen Servicing Operations Aircraft Grounding for the Maintenance Operations
12-34-00
SYSTEM LINE FLUSHING DESCRIPTION AND OPERATION General HYDRAULIC POWER SERVICING Flushing of the Case-Drain line of the Green Hydraulic System
12-36-00
C _
PAGE ___________ ____ EFFECTIVITY 201 201
ALL ALL
207
ALL
212
ALL
1 1
ALL ALL
201 201
ALL ALL
205
ALL
1 1
ALL ALL
12-34-24
12-36-29 301 301
Flushing of the Case-Drain line of the Green Hydraulic System Flushing of the HP line of the Green Hydraulic System
313
Flushing of the HP line of the Green Hydraulic System Flushing of the Case-Drain line of the Blue Hydraulic System
337
Flushing of the Case-Drain line of the Blue Hydraulic System Flushing of the HP line of the Blue Hydraulic System
358
326
347
368
ALL 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 701-749, 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 701-749, 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 701-749, 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499,
12-CONTENTS R SROS
Page 14 Jan 01/07
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ _______ SUBJECT Flushing of the HP line of the Blue Hydraulic System Flushing of the Case-Drain line of the Yellow Hydraulic System Flushing of the Case-Drain line of the Yellow Hydraulic System Flushing of the HP line of the Yellow Hydraulic System
CH/SE/SU ________
C _
____ ___________ PAGE EFFECTIVITY 378 701-749, 387
398 A308
Flushing of the HP line of the Yellow Hydraulic System Flushing of the Green Hydraulic System with the Aircraft Pumps
A318
Flushing of System with Flushing of System with
the the the the
Green Hydraulic Aircraft Pumps Blue Hydraulic Aircraft Pump
A331
Flushing of System with Flushing of System with
the the the the
Blue Hydraulic Aircraft Pump Yellow Hydraulic Aircraft Pump
A339
Flushing of the Yellow Hydraulic System with the Aircraft Pump Flushing of the Suction line of the Green Hydraulic System. Flushing of the Suction line of the Blue Hydraulic System. Flushing of the Suction line of the Yellow Hydraulic System. Replacement of the Hydraulic Fluid of the Green Hydraulic System with a Fluid Replacement and Recovery Bench Replacement of the Hydraulic Fluid of the Green Hydraulic System with a Fluid Replacement and Recovery Bench
A327
A335
A343
001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 701-749, 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 701-749, 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 701-749, 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 701-749,
A347
001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 701-749,
A351
ALL
A358
ALL
A365
ALL
A372
001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 701-749,
A393
12-CONTENTS R SROS
Page 15 Jan 01/07
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ _______ SUBJECT Replacement of the Hydraulic Fluid of the Blue Hydraulic System with a Fluid Replacement and Recovery Bench Replacement of the Hydraulic Fluid of the Blue Hydraulic System with a Fluid Replacement and Recovery Bench Replacement of the Hydraulic Fluid of the Yellow Hydraulic System with a Fluid Replacement and Recovery Bench Replacement of the Hydraulic Fluid of the Yellow Hydraulic System with a Fluid Replacement and Recovery Bench Replacement of the Hydraulic Fluid of the Green Hydraulic System with the Green Electric Pump Replacement of the Hydraulic Fluid of the Blue Hydraulic System with the Blue Electric Pump Replacement of the Hydraulic Fluid of the Yellow Hydraulic System with the Yellow Electric Pump Reclaim the Fluid in the Green Hydraulic System Reclaim the Fluid in the Blue Hydraulic System Reclaim the Fluid in the Yellow Hydraulic System Clean the Fluid in the Green Hydraulic System (with the Pall Purifier) Clean the Fluid in the Blue Hydraulic System (with the Pall Purifier) Clean the Fluid in the Yellow Hydraulic System (with the Pall Purifier)
CH/SE/SU ________
C _
____ EFFECTIVITY PAGE ___________ B313 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, B331 701-749,
B347
B365
001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 701-749,
B381
ALL
C300
ALL
C316
ALL
C332
ALL
C337
ALL
C342
ALL
C347
ALL
C352
ALL
C357
ALL
12-CONTENTS R SROS
Page 16 Jan 01/07
SERVICING - GENERAL - DESCRIPTION AND OPERATION _______________________________________________ 1. _______ General This section gives the information related to the replenishing, scheduled and unscheduled servicing operations applicable to the aircraft. If includes the topics below: 12-10-00/P. Block 001 REPLENISHING 12-20-00/P. Block 001 SCHEDULED SERVICING 12-30-00/P. Block 001 UNSCHEDULED SERVICING 2. _______________ NO STEP Areas A. NO STEP Areas on the Wing (Ref. Fig. 001) B. NO STEP Areas on the THS (Ref. Fig. 002) 3. Ground __________________________ Service Connections The table gives the position of the ground service connection points. R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, (Ref. Fig. 003) **ON A/C 701-749, (Ref. Fig. 003A) **ON A/C ALL 4. Drainage _______________ Points The table gives the position of the drainage points. (Ref. Fig. 004) 5. ___________________________________ General Hydraulic Safety Procedures A. Hydraulic System Pressurization (1) Before you pressurize a hydraulic system: (a) Make sure that no person and no equipment is near flight control surfaces or landing gear doors.
EFF : ALL 12-00-00 SROS
Page 1 Jul 01/05
NO STEP Areas on the Wing Figure 001 EFF : ALL 12-00-00 SROS
Page 2 Apr 01/98
NO STEP Areas on the THS Figure 002 EFF : ALL 12-00-00 SROS
Page 3 Apr 01/98
Ground Service Points Figure 003 (SHEET 1) R EFF : 001-049, 201-249, 251-252, 255-299, 12-00-00 301-399, 401-449, 451-499, SROS
Page 4 Jul 01/05
Ground Service Points Figure 003 (SHEET 2) R EFF : 001-049, 201-249, 251-252, 255-299, 12-00-00 301-399, 401-449, 451-499, SROS
Page 5 Jul 01/05
R R
Ground Service Points Figure 003A (SHEET 1)
R EFF : 701-749, 12-00-00 SROS
Page 6 Oct 01/00
R R
Ground Service Points Figure 003A (SHEET 2)
R EFF : 701-749, 12-00-00 SROS
Page 7 Oct 01/00
Drainage Points Figure 004 (SHEET 1) EFF : ALL 12-00-00 R SROS
Page 8 Oct 01/00
Drainage Points Figure 004 (SHEET 2) EFF : ALL 12-00-00 R SROS
Page 9 Oct 01/00
(b) Use only the interphone system to get permission to pressurize the hydraulic system. B. Safety Instructions Applicable to Hydraulic Fluid (1) Do not mix phosphoric-ester-type hydraulic fluid and mineral-base hydraulic fluid: this mixture causes the formation of a gelatinous substance in the hydraulic system which can damage the system and decrease the aircraft safety. The first of these fluids is used in the hydraulic systems and the second fluid is used in the landing gear. Therefore you must obey safety precautions to prevent any mixture of fluids. (2) Before you start to work with hydraulic fluid, carefully read the following instructions and be sure that you understand them well. (a) Before you start to work, wash you hands, wrists and forearms and apply a protective cream. (b) Apply the protective cream under the finger nails and in the skin folds. (c) Put protective goggles when you do pressurization tests of systems or components or when you can get fluid into your eyes. (d) If you get hydraulic fluid in your eyes, flush it away immediately with a large quantity of clear cold water and make a report of the incident. (e) Wash your hands, wrists and forearms with soap and hot water when you could not prevent contact with hydraulic fluid. (f) Remove the clothes moist with hydraulic fluid as soon as possible. C. Technical Safety Instructions (1) Make sure that the hydraulic fluid does not cause damage to some materials such as rubber, copper, titanium, paint, plastic materials. (2) Make sure that the hydraulic fluid touches the hydraulic system components only, not the other items of the aircraft. Keep accidental spillage of hydraulic fluid to a minimum during maintenance procedures. Remove any sign of hydraulic fluid so that it does not extend to the adjacent areas and subsequently cause incorrect
EFF : ALL 12-00-00 SROS
Page 10 Oct 01/00
indications of leaks. Clean hydraulic-fluid contaminated areas with a dry cloth and solvent. (3) Use only solvent to clean metallic parts before you assemble them. Make sure that there is no more solvent when you assemble the parts. (4) Use only approved hydraulic fluid to fill hydraulic reservoirs, filter bowls, pumps or other hydraulic components before you install them. (5) Make sure that you have obeyed all precautions to prevent contamination of the hydraulic fluid by: - non-approved hydraulic fluids - fuel - oil - water - foreign bodies. (6) If a system is contaminated, keep the hydraulic fluid for analysis. (7) Before you connect the hydraulic service cart to the aircraft make sure that the specifications of the fluids of the service cart and the aircraft are the same.
EFF : ALL 12-00-00 SROS
Page 11 Oct 01/00
SERVICING - GENERAL - MAINTENANCE PRACTICES ___________________________________________ TASK 12-00-00-481-801 Installation of the Wing Safety Rope WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING _______ NOTICES ARE IN POSITION. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED ON THE _______ LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R R
No specific No specific No specific 98D27803000000 98F57004000000
warning notice square drive extension and ratchet handle 0.5 in. (12.6999 mm) access platform 5.8 m (19 ft.) 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER 1 SAFETY ROPE - WING
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------27-50-00-866-802 12-00-00-991-001
Retraction of the Flaps on the Ground Fig. 201
EFF : ALL 12-00-00 SROS
Page 201 Jan 01/02
3. __________ Job Set-up Subtask 12-00-00-866-050 A. Aircraft Maintenance Configuration R
(1) Make sure that the flaps and slats are retracted (Ref. TASK 27-50-00866-802). (2) Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) is correctly installed. Subtask 12-00-00-941-050 B. Safety Precautions (1) Put the warning notice in the cockpit, to tell persons not to operate the flap and slat control lever. Subtask 12-00-00-010-050 C. Get Access (1) Put the access platform at the leading edge. 4. Procedure _________ Subtask 12-00-00-210-050 A. Preparation for Installation (1) Make sure that the SAFETY ROPE - WING (98F57004000000) is serviceable. Subtask 12-00-00-481-050 B. Installation of the Wing Safety Rope (Ref. Fig. 201/TASK 12-00-00-991-001) (1) Put the SAFETY ROPE - WING (98F57004000000) in position on the wing, with the lashing ratchet assembly (10) inboard. (2) Remove and keep the blanking plug from Frame 43 in the fuselage. (3) Install the threaded plug (6) in Frame 43.
EFF : ALL 12-00-00 SROS
Page 202 Jan 01/07
Wing Safety Rope Figure 201/TASK 12-00-00-991-001 EFF : ALL 12-00-00 SROS
Page 203 Apr 01/98
(4) Connect the shackle (7), complete with the anchor plate (9) and the lashing ratchet assembly (10), to the threaded plug (6) with the shackle bolt (8). (5) Remove and keep the plug from the wing tip. R R
(6) Put the washer (2) in position and use the square drive extension and ratchet handle to install the screwed body assembly (1). (7) Install the shackle (5), complete with the safety rope (3), to the screwed body (1) with the shackle bolt (4). NOTE : The rope must not be loose, but do not tighten too much, it ____ can damage the aircraft. (8) Operate the lashing ratchet assembly (10) to tighten the SAFETY ROPEWING (98F57004000000). The tension must not be too loose or too tight. (9) Make sure that the safety lanyard (11) can move freely along the safety rope (3).
EFF : ALL 12-00-00 SROS
Page 204 Jan 01/02
TASK 12-00-00-081-801 Removal of the Wing Safety Rope WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING _______ NOTICES ARE IN POSITION. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED ON THE _______ LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
warning notice square drive extension and ratchet handle 0.5 in. (12.6999 mm) access platform 5.8 m (19 ft.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------27-50-00-866-802 12-00-00-991-001
Retraction of the Flaps on the Ground Fig. 201
EFF : ALL 12-00-00 SROS
Page 205 Apr 01/98
3. __________ Job Set-up Subtask 12-00-00-941-051 A. Safety Precautions R
(1) Make sure that the flaps and slats are retracted (Ref. TASK 27-50-00866-802). (2) Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) is installed. (3) Make sure that the warning notice is in the cockpit, to tell persons not the operate the flap and slat control lever. (4) Make sure that the access platform is at the leading edge at zone 560 and at zone 660. 4. Procedure _________ (Ref. Fig. 201/TASK 12-00-00-991-001) Subtask 12-00-00-081-050 A. Removal of the Wing Safety Rope (1) Operate the lashing ratchet (10) to release the tension of the SAFETY ROPE - WING (98F57004000000). (2) Remove the shackle bolt (4) and remove the shackle (5) from the screwed body (1). (3) Use the square drive extension and ratchet handle to remove the screwed body assembly (1). Remove the washer (2). (4) Install the blanking plug in the wing tip. (5) Carefully make a coil of the SAFETY ROPE - WING (98F57004000000) to the point of access. (6) Remove the shackle bolt (8) to disconnect the lashing ratchet assembly (10). Remove the threaded plug (6). (7) Install the blanking plug in the fuselage. (8) Remove the SAFETY ROPE - WING (98F57004000000) from the wing.
EFF : ALL 12-00-00 SROS
Page 206 Jan 01/07
5. Close-up ________ Subtask 12-00-00-942-050 A. Put the Aircraft back to its Initial Configuration (1) Remove the access platform. (2) Remove the warning notice. (3) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000).
EFF : ALL 12-00-00 SROS
Page 207 Apr 01/98
REPLENISHING - DESCRIPTION AND OPERATION ________________________________________ 1. _______ General This section gives the instructions related to the filling operations. It includes the topics below: 12-11-00/P. 12-12-00/P. 12-13-00/P. 12-14-00/P. 12-15-00/P. 12-16-00/P. 12-17-00/P.
Block Block Block Block Block Block Block
001 001 001 001 001 001 001
FUEL HYDRAULIC FLUIDS OIL GAS WATER TOILET SANITARY FLUID RAIN REPELLENT
EFF : ALL 12-10-00 SROS
Page 1 Apr 01/98
FUEL - DESCRIPTION AND OPERATION ________________________________ R R R R R R R R
1. General _______ This section gives the instructions and the safety precautions when you refuel the aircraft. It includes this topic: 12-11-28/P.Block 301 FUEL SYSTEM SERVICING The types of fuel that you are permitted to use in the fuel system are identified in 28-00-00/P.Block 301 FUEL - GENERAL - SERVICING.
EFF : ALL 12-11-00 SROS
Page 1 Jul 01/06
FUEL SYSTEM - SERVICING _______________________ TASK 12-11-28-650-801 General Refuel/Defuel Safety Procedures 1. __________________ Reason for the Job The procedure that follows contains information as specified in the IATA Guidance Material on Standard Into-Plane Fuelling Procedures 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-34-24-860-801 28-00-00-610-801 29-00-00-863-802 R
FCOM 2.01.30 FM 2.04.00 12-11-28-991-001
Aircraft Grounding for the Refuel/Defuel Operations Fuel Safety Procedures Pressurize the Blue Hydraulic System with the Electric Pump Fig. 301
3. __________ Job Set-up (Ref. Fig. 301/TASK 12-11-28-991-001) Subtask 12-11-28-941-058 A. Not Applicable 4. Procedure _________ Subtask 12-11-28-650-050 A. Safety Precautions R R
(1) You must obey the Fuel safety Procedures (Ref. TASK 28-00-00-610-801) when you refuel/defuel an aircraft. (2) Do not go near the aircraft until the anti-collision lights have been set to OFF.
EFF : ALL 12-11-28 SROS
Page 301 Jan 01/07
R
Refuel Safety Area Figure 301/TASK 12-11-28-991-001
EFF : ALL 12-11-28 SROS
Page 302 Apr 01/00
(3) Before you start the refuel/defuel procedure, make sure that all the electrical circuits in the fuel system are complete. (4) Do not start the refuel/defuel procedure if any part of the landing gear appears unusually hot. You must wait for the landing gear to cool. (5) Ground and bond the aircraft (Ref. TASK 12-34-24-860-801). NOTE : Bonding is essential, grounding is recommended. ____ (6) Move all equipment and material which is not necessary for the refuel/defuel procedure out of the safety area. (7) On panel 312 VU make sure that the ACCU PRESS on the triple indicator has sufficient pressure. If necessary, pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-802). (8) On the panel 117VU, make sure that the PARK BRK is ON. (9) Make sure that the chocks are in this position: (a) If the ramp does not slope: - move the aft NLG chocks away from the tires. During the refuel the NLG tires roll aft as the MLG shock absorber compresses. - make sure that the chocks do not touch the MLG tires. The weight of the fuel can lower the aircraft and cause the tires to catch the chocks (b) If the ramp slopes: - make sure that the chocks down from the tires touch the NLG and MLG tires - make sure that the chocks up from the tires do not touch the NLG and MLG tires. (10) Make sure that there is no equipment below the aircraft which can cause damage. The weight of the fuel can suddenly compress the landing gear and lower the aircraft. (11) Before you start the refuel/defuel procedure make sure that these are available: - a fuelling supervisor or fuelling safety person - the correct fire-fighting equipment - approved persons to use the fire-fighting equipment. (12) Make sure that the overboard vent lines are not blocked. If they are blocked, damage to the fuel tanks can occur. (13) Make sure that the fuel tanker (or hydrant) contains the correct fuel. The correct fuels are shown in the Flight Manual (Ref. FM 2.04.00). EFF : ALL 12-11-28 R SROS
Page 303 Jan 01/07
(14) Make sure that the fuel tanker (or, if you use a hydrant to refuel the aircraft, the pump unit) is in the correct position. (15) Make sure that, if there is an emergency, you can move the fuel tanker/pump unit and the support equipment away quickly. (16) Do not operate the aircraft main engines during a refuel/defuel procedure. R R
NOTE : In an emergency, you are permitted to refuel the aircraft with ____ one engine in operation (Ref. FCOM 2.01.30). (17) APU starts or stutdowns are permitted during refuel/defuel procedures. If it is necessary to operate the APU, the limits that follow apply: (a) An APU start is not permitted during a refuel/defuel procedure if the APU has failed to start or an automatic shutdown has occurred. (b) You must complete a normal APU shutdown if a fuel spill has occurred during the refuel/defuel procedure. (18) Make sure that all electrical equipment you use will not cause a spark. (19) Do not do a refuel/defuel procedure in bad weather conditions and electrical storms. Lightning is dangerous. (20) During the refuel/defuel procedure do not operate the aircraft external lighting. (21) During the refuel/defuel procedure do not fill the oxygen system or change the oxygen bottles. (22) During the refuel/defuel procedure do only essential aircraft maintenance and/or servicing that will not cause a spark. (23) Do not refuel the aircraft if a fire or engine overheat warning is displayed on the flight deck. (24) You are only permitted to replace or do small maintenance work on radio, radar and electrical equipment during refuelling. (25) You are not permitted to remove, install or test aircraft batteries or related equipment during refuelling.
EFF : ALL 12-11-28 SROS
Page 304 Jan 01/07
(26) Do not use the microphone on the High Frequency (HF) transmitter during refuel/defuel or fuel transfer operations. (27) Immediately flush away with water, or remove, fuel leakage. (28) Obey the safety distances for 60 meters (200 ft) from aircraft: (a) Stop the fuel tanker 60 meters (200 ft) from the aircraft nose while the weather radar operates. Do not operate the fuel tanker/pump unit until you stop operation of the weather radar. (29) Obey the safety distances for 30 meters (100 ft) from aircraft: (a) Aircraft must not be refueled/defueled less than 30 meters (100 ft) from radar or HF radio equipment under test or in operation in the aircraft or ground installation. (30) Obey the safety distances for 15 meters (50 ft) from aircraft: (Ref. Fig. 301/TASK 12-11-28-991-001) (a) Put NO SMOKING warning notices around the work area not less than 15 meters (50 ft) from the refueling/defueling equipment and aircraft and aircraft tank vents. (b) Do not connect electrical equipment to a power source less than 15 meters (50 ft) away, unless the power source has spark-proof connectors. (c) Refueling/defueling equipment and aircraft fuel-tank vents must not be nearer than 15 meters (50 ft) to a building during refuelling/defuelling. Make sure the position of the refuelling/defuelling area cannot let this occur. Because of the design of some buildings, you can do refuelling/defuelling operations nearer than 15 meters (50 ft). Examples of this type of building are nose loaders and aerobridges.
R R
(31) Obey the safety distances for 6 meters (20 ft) from aircraft (Ref. Fig. 301/TASK 12-11-28-991-001) (a) Ground power units (GPUs) can be operated when they are put not less than 6 meters (20 ft) from the aircraft filling and venting points, hydrant valves and other refueling/defueling equipment when in use. (b) Photographic flash bulbs or electronic flash equipment must not be used less than 6 meters (20 ft) of the refueling/defueling equipment or any filling or venting points of the aircraft.
EFF : ALL 12-11-28 SROS
Page 305 Jul 01/06
(c) The refueling/defueling zone must be regarded as extending not less than 6 meters (20 ft) radially from the filling and venting points on the aircraft and the fueling/defueling equipment and, when applicable, from the hydrant valve in use for refueling. When defueling is taking place, the vehicle will be venting and will generate a zone radiating from the tank vent. (d) Inside the 6 meter (20 ft) zone, radios, radio telephones (cell phones or mobile phones) and pagers as well as the operation of switches on lighting systems of other than intrinsically safe types are not allowed. Personnel in the refueling/defueling zone and those employed in refueling/defueling must not carry matches or other means of ignition or foot-wear with exposed iron or steel studs, nails or tips.
EFF : ALL 12-11-28 R SROS
Page 306 Jul 01/06
TASK 12-11-28-650-802 Refuel/Defuel Safety Procedures In The Hangar 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information Not Applicable 3. __________ Job Set-up Subtask 12-11-28-941-059 A. Not Applicable 4. Procedure _________ Subtask 12-11-28-650-051 A. Safety Precautions (1) Open all the hangar doors. Do not close the hangar doors until you have completed the refuel/defuel procedure. (2) Make the limits of the hangar the limits of the safety area. (a) The limit of the safety area is usually 15 m. But where the hangar wall is closer than 15 m, then the hangar wall is the limit of the safety area. (b) If a hangar entrance is closer than 15 m, then a safety barrier is to be positioned there. (3) To be prepared to tow the aircraft out of the hangar if an emergency occurs, do these steps: (a) Move all equipment which is not necessary for the refuel/defuel procedure from between the aircraft and the hangar exit. (b) Attach a towing vehicle to the aircraft. (4) Make sure that the driver of the fuel-tanker puts the fuel-tanker in the correct position adjacent to the aircraft. Keep the exit of the hangar clear for the fuel tanker.
EFF : ALL 12-11-28 R SROS
Page 307 Jul 01/04
TASK 12-11-28-650-803 Pressure Refuel with Automatic Control from the Panel 990VU WARNING : MAKE SURE THE AREA AROUND THE AIRCRAFT IS SAFE BEFORE YOU START A _______ REFUEL/DEFUEL PROCEDURE. IN THIS SAFE AREA, DO NOT LET PERSONS: - SMOKE - MAKE SPARKS OR FIRE - USE ANY EQUIPMENT WHICH IS NOT APPROVED FOR THE TASK. AIRCRAFT FUEL IS FLAMMABLE. WARNING : MAKE SURE THAT THE WHEEL CHOCKS ARE IN POSITION. MOVEMENTS OF THE _______ AIRCRAFT COULD BE DANGEROUS. WARNING : DO NOT SPILL FUEL ON THE ENGINES OR THE BRAKES. IF YOU SPILL FUEL ON _______ ENGINES OR BRAKES THAT ARE HOT, IT CAN CAUSE FIRES. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R
12-11-28-650-801 12-11-28-650-802 12-32-28-281-810 12-34-24-860-801 24-41-00-861-801 24-41-00-862-801 28-25-00-650-801
General Refuel/Defuel Safety Procedures Refuel/Defuel Safety Procedures In The Hangar Operate Water Drain Valves to Drain Accumulated Water from Center, Inner, Outer and Wing Vent Surge Tanks Aircraft Grounding for the Refuel/Defuel Operations Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Pressure Defuel Procedure
EFF : ALL 12-11-28 SROS
Page 308 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------28-25-00-869-801 29-00-00-863-802 34-10-00-860-801 34-10-00-860-803 12-11-28-991-001 12-11-28-991-002 12-11-28-991-003 12-11-28-991-026
Ground Fuel Transfer Procedure Pressurize the Blue Hydraulic System with the Electric Pump ADIRS Start Procedure ADIRS Stop Procedure Fig. 301 Fig. 302 Fig. 303 Fig. 304
3. __________ Job Set-up (Ref. Fig. 301/TASK 12-11-28-991-001, 302/TASK 12-11-28-991-002, 303/TASK 12-11-28-991-003, 304/TASK 12-11-28-991-026) Subtask 12-11-28-941-050 A. Safety Precautions WARNING : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND _______ DAMAGE. (1) Obey the safety procedures for the refuel procedure (Ref. TASK 12-1128-650-801) and if applicable (Ref. TASK 12-11-28-650-802). (2) On panel 312 VU make sure that the ACCU PRESS on the triple indicator has sufficiant pressure. If necessary, pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-802). (3) On the panel 117VU, make sure that the PARK BRK is ON. (4) Make sure that the chocks are in position as follows: - move the aft NLG chocks away from the tires. During the refuel the NLG tires roll aft as the MLG shock absorber compresses. - make sure that the chocks do not touch the MLG tires. The weight of the fuel can lower the aircraft and cause the tires to catch the chocks. R R
Subtask 12-11-28-281-052-A B. Water Contamination Check
R R
(1) Get a fuel sample from the fuel tanker/pump unit (Ref. TASK 12-32-28281-810) and do a check for water contamination.
EFF : ALL 12-11-28 SROS
Page 309 Jan 01/07
Refuel/Defuel Couplings Figure 302/TASK 12-11-28-991-002 EFF : ALL 12-11-28 R SROS
Page 310 Jul 01/04
Refuel/Defuel Control Panel 990VU Figure 303/TASK 12-11-28-991-003 EFF : ALL 12-11-28 R SROS
Page 311 Jul 01/04
Refuel Times - Refuel Pressure of 3.45 bar (50 psi) at the Refuel Coupling Figure 304/TASK 12-11-28-991-026 EFF : ALL 12-11-28 R SROS
Page 312 Jul 01/04
Subtask 12-11-28-860-052-A C. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT YOU GROUND THE FUEL TANKER AND THE AIRCRAFT _______ CORRECTLY. IF YOU DO NOT A DANGEROUS ELECTRICAL DISCHARGE CAN OCCUR. (1) Ground the aircraft and the fuel tanker/pump unit (Ref. TASK 12-3424-860-801). Then bond them together electrically. NOTE : Bonding is essential, grounding is recommended. ____ (2) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (3) Do the ADIRS start procedure (Ref. TASK 34-10-00-860-801). NOTE : If external electrical power or APU electrical power is not ____ available, it is possible to use the aircraft batteries to do an automatic refuel. But, on battery, the ADIRS does not send aircraft attitude information to the FCMS. Thus, on battery refuel, there could be a difference of up to 750 kg (1650 lb) between the set fuel quantity and the actual fuel quantity. Subtask 12-11-28-010-050 D. Get Access R R
NOTE : You can use 1, 2, 3 or 4 refuel hoses to do an automatic pressure ____ refuel. This procedure uses the four refuel hoses.
R R
(1) Put 2 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position, one below the access panel 522HB and one below the access panel 622HB. (2) Open the access panels 522HB and 622HB. (3) Remove the refuel/defuel coupling caps 5503QA1, 5503QA2, 5504QA1 and 5504QA2. (4) Examine the aircraft refuel/defuel couplings: WARNING : MAKE SURE THAT THE FUEL SUPPLY HOSE IS CORRECTLY CONNECTED _______ TO THE COUPLING BEFORE YOU REFUEL/DEFUEL THE AIRCRAFT. DO NOT CONNECT THE FUEL SUPPLY HOSE IF THERE ARE SIGNS OF DAMAGE TO THE AIRCRAFT COUPLING LUGS OR SLOTS.
EFF : ALL 12-11-28 SROS
Page 313 Jan 01/06
R R
(a) Visually examine the aircraft coupling lugs and slots for signs of damage or contamination.
R
(5) Make sure that the couplings of the fuel supply hoses are clean. Connect the four hoses to the aircraft refuel/defuel couplings 5502QA1 and 5502QA2.
R
(6) Open the access panel 198DB. Subtask 12-11-28-740-050 E. Do this test: ------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------On the refuel/defuel control panel 990VU: 1. If only the battery power is available, put the PWR SUPPLY switch to BAT. NOTE : During the first 30 ____ seconds after power-up, the indications at the fuel panel must be ignored. 2. Lift the guard, then push (in) and hold the HI LEVEL TEST switch 3QJ.
On the refuel/defuel control panel 990VU: - the hi-level lights (4QJ1, 4QJ2, 5QJ1, 5QJ2, 6QJ and 7QJ) and the OVERFLOW lights (8QJ1, 8QJ2 and 9QJ) go to the opposite condition - the CKPT and END lights come on - the fuel quantity, PRESELECTED and ACTUAL displays show all 8s.
3. Release (out) the HI-LEVEL TEST switch.
Wait for 10 seconds: - the lights go back to their initial condition - the fuel quantity, PRESELECTED and ACTUAL displays go back to their initial condition.
EFF : ALL 12-11-28 SROS
Page 314 Apr 01/05
4. Procedure _________ (Ref. Fig. 304/TASK 12-11-28-991-026) NOTE : An Automatic Refuel is only possible if the fuel quantity in each ____ tank at the start of the refuel is less than the expected quantity after the refuel. Subtask 12-11-28-650-063 A. Reference for Adjustment of the Fuel Distribution (if necessary) (1) If it becomes necessary to adjust the fuel distribution of the aircraft, do the (Ref. TASK 28-25-00-650-801) or the (Ref. TASK 2825-00-869-801). Subtask 12-11-28-650-052 R
B. Pressure Refuel with Automatic Control from the Panel 990VU CAUTION : DO NOT LET THE REFUEL PRESSURE GET TO MORE THAN 3.4 BAR (50 _______ PSI). THIS WILL PREVENT DAMAGE TO THE AIRCRAFT FUEL SYSTEM. (1) On the refuel/defuel control panel 990VU: (a) Put the LOAD switch 7QT to the INC position and hold it there. (b) Make sure that the numbers on the PRESELECTED display increase. (c) When the PRESELECTED display shows the necessary fuel load, release the LOAD switch. NOTE : To do a refuel, the figure set must be a minimum of 200 kg ____ (440.9244 lb) more than the FOB figure. (d) Make sure that the REFUEL VALVES switches (5QU1, 5QU2, 6QU1, 6QU2, 7QU, and 8QU) are in the NORM position and guarded. NOTE : If a switch is moved to SHUT during the automatic refuel, ____ the applicable valve closes. If a switch is moved to OPEN during the automatic refuel, the FCMS ignores the command until the automatic refuel is complete. Then, after approximately 15 seconds, the refuel will continue (in manual mode) into the applicable tank. (2) Start the pump on the fuel tanker/pump unit.
EFF : ALL 12-11-28 SROS
Page 315 Jan 01/07
(3) At the refuel/defuel control panel 990VU: (a) Put the MODE SELECT switch 3QU to the REFUEL position. NOTE : If the following switches are not in the correct ____ configuration, the END light will flash: - One or more of the inlet valve switches is in the OPEN or SHUT position - On the FUEL panel 245VU, the CTR TANK XFR switch is set to MAN - On the FUEL panel 245VU, the T TK FEED switch is set to OPEN or ISOL - On the FUEL panel 245VU, the T TANK MODE switch is set to FWD - On the FUEL panel 245VU, the OUTER TK XFR switch is set to MAN.
R R
(b) Make sure that the numbers on the fuel quantity and the ACTUAL displays increase. NOTE : The refuel times (shown in the illustration) give the ____ estimated time taken (in minutes) to refuel the aircraft from the initial (INIT) fuel quantity to the preselected fuel quantity. Each refuel-time range given makes an allowance for the densities from 0.76 kg/l to 0.82 kg/l, with a fuel pressure of 3.45 bar (50 psi) at the refuel coupling. (c) When the refuel stops, make sure that: - the END light comes on and does not flash - the numbers on the ACTUAL and the PRESELECTED displays are stable and are the same (-200 kg (-440.9244 lb) +200 kg (+440.9244 lb)). (d) Set the MODE SELECT switch to OFF. (e) If the power supply is from the battery, put the PWR SUPPLY switch to NORM. (4) Stop the pump on the fuel tanker/pump unit.
EFF : ALL 12-11-28 SROS
Page 316 Jan 01/07
5. Close-up ________ Subtask 12-11-28-410-050 A. Close Access (1) Disconnect the couplings of the four fuel supply hoses from the aircraft refuel/defuel couplings 5502QA1 and 5502QA2. (2) Install the refuel/defuel coupling caps 5503QA1, 5503QA2, 5504QA1 and 5504QA2. (3) Refuel panel closure CAUTION : DO NOT APPLY TOO MUCH FORCE TO THE OPERATING ROD WHEN YOU _______ CLOSE THE PANEL. THIS PREVENTS DAMAGE TO THE MECHANISM. (a) Close the access panels 522HB and 622HB. (4) Close the access panel 198DB. Subtask 12-11-28-860-053-A B. Aircraft Maintenance Configuration (1) If applicable, do the ADIRS stop procedure (Ref. TASK 34-10-00-860803). (2) If applicable, de-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). (3) Disconnect these ground/bonding cables: - the bonding cable between the aircraft and the fuel tanker/pump unit - if applicable, the grounding cable between the fuel tanker/pump unit and the ground - if applicable, the grounding cable between the aircraft and the ground. NOTE : The outer tank water drain valves have small holes in them to ____ prevent damage due to water freezing in the valve. These holes also let fuel flow from the outer tank to the inner tank at a rate of up to 20 kg/hour. This flow is normal and is to be expected. There is no leakage in the system.
EFF : ALL 12-11-28 R SROS
Page 317 Jan 01/07
Subtask 12-11-28-942-050 C. Removal of Equipment (1) Put the chocks back in their original position. (2) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 12-11-28 R SROS
Page 318 Jan 01/07
TASK 12-11-28-650-804 Pressure Refuel With Manual Control WARNING : MAKE SURE THE AREA AROUND THE AIRCRAFT IS SAFE BEFORE YOU START A _______ REFUEL/DEFUEL PROCEDURE. IN THIS SAFE AREA, DO NOT LET PERSONS: - SMOKE - MAKE SPARKS OR FIRE - USE ANY EQUIPMENT WHICH IS NOT APPROVED FOR THE TASK. AIRCRAFT FUEL IS FLAMMABLE. WARNING : MAKE SURE THAT THE WHEEL CHOCKS ARE IN POSITION. MOVEMENTS OF THE _______ AIRCRAFT COULD BE DANGEROUS. WARNING : DO NOT SPILL FUEL ON THE ENGINES OR THE BRAKES. IF YOU SPILL FUEL ON _______ ENGINES OR BRAKES THAT ARE HOT, IT CAN CAUSE FIRES. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
2 access platforms 5.0 m (16 ft. 5 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R
12-11-28-650-801 12-11-28-650-802 12-32-28-281-810 12-34-24-860-801 24-41-00-861-801 24-41-00-862-801 28-25-00-650-801
General Refuel/Defuel Safety Procedures Refuel/Defuel Safety Procedures In The Hangar Operate Water Drain Valves to Drain Accumulated Water from Center, Inner, Outer and Wing Vent Surge Tanks Aircraft Grounding for the Refuel/Defuel Operations Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Pressure Defuel Procedure
EFF : ALL 12-11-28 SROS
Page 319 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------28-25-00-869-801 29-00-00-863-802 34-10-00-860-801 34-10-00-860-803 12-11-28-991-001 12-11-28-991-002 12-11-28-991-003 12-11-28-991-026 12-11-28-991-020-A
Ground Fuel Transfer Procedure Pressurize the Blue Hydraulic System with the Electric Pump ADIRS Start Procedure ADIRS Stop Procedure Fig. 301 Fig. 302 Fig. 303 Fig. 304 Fig. 305
**ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
12-11-28-991-020-B
Fig. 305A
**ON A/C ALL 12-11-28-991-021-A
Fig. 306
**ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
12-11-28-991-021-B
Fig. 306A
**ON A/C ALL 12-11-28-991-023-A
Fig. 307
**ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
12-11-28-991-023-B
Fig. 307A
EFF : ALL 12-11-28 R SROS
Page 320 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------**ON A/C ALL 12-11-28-991-024-A
Fig. 308
**ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
12-11-28-991-024-B
Fig. 308A
**ON A/C ALL 3. __________ Job Set-up (Ref. Fig. 301/TASK 12-11-28-991-001, 302/TASK 12-11-28-991-002, 303/TASK 12-11-28-991-003) Subtask 12-11-28-941-052 A. Safety Precautions WARNING : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND _______ DAMAGE. (1) Obey the safety procedures for the refuel procedure (Ref. TASK 12-1128-650-801) and if applicable (Ref. TASK 12-11-28-650-802). (2) On panel 312VU make sure that the ACCU PRESS on the triple indicator has sufficient pressure. If necessary, pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-802). (3) On the panel 117VU, make sure that the PARK BRK is ON. (4) Make sure that the chocks are in the position that follows: - move the aft NLG chocks away from the tires. During the refuel the NLG tires roll aft as the MLG shock absorber compresses. - make sure that the chocks do not touch the MLG tires. The weight of the fuel can lower the aircraft and cause the tires to catch the chocks.
EFF : ALL 12-11-28 R SROS
Page 321 Jan 01/07
R R
Subtask 12-11-28-281-054-A B. Fuel Sampling
R R
(1) Get a fuel sample from the fuel tanker/pump unit (Ref. TASK 12-32-28281-810) and do a check for water contamination.
R R
(2) If you use the manual refuel distribution graphs, use the fuel sample from the fuel tanker and measure its Specific Gravity (SG). Subtask 12-11-28-860-054 C. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT YOU GROUND THE FUEL TANKER AND THE AIRCRAFT _______ CORRECTLY. IF YOU DO NOT A DANGEROUS ELECTRICAL DISCHARGE CAN OCCUR. (1) Ground the aircraft and the fuel tanker/pump unit(s) (Ref. TASK 1234-24-860-801). Then bond them together electrically. NOTE : Bonding is essential, grounding is recommended. ____ (2) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (3) Do the ADIRS start procedure (Ref. TASK 34-10-00-860-801). NOTE : If external electrical power or APU electrical power is not ____ available, it is possible to use the aircraft batteries to do a manual refuel. But, on battery, the ADIRS do not send aircraft attitude information to the FCMS. Thus, on battery refuel, there could be a difference of up to 750 kg (1650 lb) between the set fuel quantity and the actual fuel quantity. Subtask 12-11-28-010-052 D. Get Access NOTE : You can use 1, 2, 3 or 4 refuel hoses to do a manual pressure ____ refuel. This procedure uses the four refuel hoses. (1) Put 2 access platforms in position, one below the access panel 522HB and one below the access panel 622HB. (2) Open the access panels 522HB and 622HB.
EFF : ALL 12-11-28 SROS
Page 322 Jan 01/07
(3) Remove the refuel/defuel coupling caps 5503QA1, 5503QA2, 5504QA1 and 5504QA2. (4) Examine the aircraft refuel/defuel couplings: WARNING : MAKE SURE THAT THE FUEL SUPPLY HOSE IS CORRECTLY CONNECTED _______ TO THE COUPLING BEFORE YOU REFUEL/DEFUEL THE AIRCRAFT. DO NOT CONNECT THE FUEL SUPPLY HOSE IF THERE ARE SIGNS OF DAMAGE TO THE AIRCRAFT COUPLING LUGS OR SLOTS. (a) Visually examine the aircraft coupling lugs and slots for signs of damage or contamination. (5) Make sure that the couplings of the fuel supply hoses are clean. Then connect them to the aircraft refuel/defuel couplings 5502QA1 and 5502QA2. (6) Open the access panel 198DB. Subtask 12-11-28-740-051 E. Do this test: ------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------On the refuel/defuel control panel 990VU: 1. If only battery power is available, put the PWR SUPPLY switch to BAT. 2. Lift the guard, then push (in) and hold the HI LEVEL TEST switch 3QJ.
On the refuel/defuel control panel 990VU: - the hi-level lights (4QJ1, 4QJ2, 5QJ1, 5QJ2, 6QJ and 7QJ) and the OVERFLOW lights (8QJ1, 8QJ2 and 9QJ) go to the opposite condition - the CKPT and END lights come on - the fuel quantity, PRESELECTED and ACTUAL displays show all 8s.
3. Release (out) the HI-LEVEL TEST
Wait for 10 seconds:
EFF : ALL 12-11-28 R SROS
Page 323 Jan 01/07
------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------switch. - the lights go back to their initial condition - the fuel quantity, PRESELECTED and ACTUAL displays go back to their initial condition. 4. Procedure _________ (Ref. Fig. 303/TASK 12-11-28-991-003, 304/TASK 12-11-28-991-026, 305/TASK 12-11-28-991-020-A) **ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
(Ref. Fig. 305A/TASK 12-11-28-991-020-B) **ON A/C ALL (Ref. Fig. 306/TASK 12-11-28-991-021-A) **ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
(Ref. Fig. 306A/TASK 12-11-28-991-021-B) **ON A/C ALL (Ref. Fig. 307/TASK 12-11-28-991-023-A) **ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
(Ref. Fig. 307A/TASK 12-11-28-991-023-B)
EFF : ALL 12-11-28 R SROS
Page 324 Jan 01/07
INTENTIONALLY BLANK
R 12-11-28 SROS
Page 325 Jan 01/07
Refuel Distribution Graphs - Density 0.77 to 0.795 Figure 305/TASK 12-11-28-991-020-A18 (SHEET 1) EFF : ALL 12-11-28 R SROS
Page 326 Jan 01/07
Refuel Distribution Graphs - Density 0.77 to 0.795 Figure 305/TASK 12-11-28-991-020-A28 (SHEET 2) EFF : ALL 12-11-28 R SROS
Page 327 Jan 01/07
Refuel Distribution Graphs - Density 0.77 to 0.795 Figure 305/TASK 12-11-28-991-020-A38 (SHEET 3) EFF : ALL 12-11-28 R SROS
Page 328 Jan 01/07
Refuel Distribution Graphs - Density 0.77 to 0.795 Figure 305/TASK 12-11-28-991-020-A48 (SHEET 4) EFF : ALL 12-11-28 R SROS
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Refuel Distribution Graphs - Density 0.76 to 0.795 Figure 305A/TASK 12-11-28-991-020-B18 (SHEET 1) EFF : ALL 12-11-28 R SROS
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Refuel Distribution Graphs - Density 0.76 to 0.795 Figure 305A/TASK 12-11-28-991-020-B28 (SHEET 2) EFF : ALL 12-11-28 R SROS
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Refuel Distribution Graphs - Density 0.76 to 0.795 Figure 305A/TASK 12-11-28-991-020-B38 (SHEET 3) EFF : ALL 12-11-28 R SROS
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Refuel Distribution Graphs - Density 0.76 to 0.795 Figure 305A/TASK 12-11-28-991-020-B48 (SHEET 4) EFF : ALL 12-11-28 R SROS
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Refuel Distribution Graphs - Density 0.76 to 0.795 Figure 305A/TASK 12-11-28-991-020-B58 (SHEET 5) EFF : ALL 12-11-28 R SROS
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Refuel Distribution Graphs - Density 0.76 to 0.795 Figure 305A/TASK 12-11-28-991-020-B68 (SHEET 6) EFF : ALL 12-11-28 R SROS
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Refuel Distribution Graphs - Density 0.76 to 0.795 Figure 305A/TASK 12-11-28-991-020-B78 (SHEET 7) EFF : ALL 12-11-28 R SROS
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Refuel Distribution Graphs - Density 0.76 to 0.795 Figure 305A/TASK 12-11-28-991-020-B88 (SHEET 8) EFF : ALL 12-11-28 R SROS
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Refuel Distribution Graphs - Density 0.8 to 0.83 Figure 306/TASK 12-11-28-991-021-A17 (SHEET 1) EFF : ALL 12-11-28 R SROS
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Refuel Distribution Graphs - Density 0.8 to 0.83 Figure 306A/TASK 12-11-28-991-021-B17 (SHEET 1) EFF : ALL 12-11-28 R SROS
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Refuel Distribution Tables - Density 0.76 to 0.795 Figure 307/TASK 12-11-28-991-023-A18 (SHEET 1) EFF : ALL 12-11-28 R SROS
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Refuel Distribution Tables - Density 0.76 to 0.795 Figure 307/TASK 12-11-28-991-023-A68 (SHEET 6) EFF : ALL 12-11-28 R SROS
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Refuel Distribution Tables - Density 0.76 to 0.795 Figure 307/TASK 12-11-28-991-023-A88 (SHEET 8) EFF : ALL 12-11-28 R SROS
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Manual Refuel Distribution Tables - Density 0.76 To 0.795 Figure 307A/TASK 12-11-28-991-023-B18 (SHEET 1) EFF : ALL 12-11-28 R SROS
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Manual Refuel Distribution Tables - Density 0.76 To 0.795 Figure 307A/TASK 12-11-28-991-023-B28 (SHEET 2) EFF : ALL 12-11-28 R SROS
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Manual Refuel Distribution Tables - Density 0.76 To 0.795 Figure 307A/TASK 12-11-28-991-023-B38 (SHEET 3) EFF : ALL 12-11-28 R SROS
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Manual Refuel Distribution Tables - Density 0.76 To 0.795 Figure 307A/TASK 12-11-28-991-023-B48 (SHEET 4) EFF : ALL 12-11-28 R SROS
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Manual Refuel Distribution Tables - Density 0.76 To 0.795 Figure 307A/TASK 12-11-28-991-023-B58 (SHEET 5) EFF : ALL 12-11-28 R SROS
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Manual Refuel Distribution Tables - Density 0.76 To 0.795 Figure 307A/TASK 12-11-28-991-023-B68 (SHEET 6) EFF : ALL 12-11-28 R SROS
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Manual Refuel Distribution Tables - Density 0.76 To 0.795 Figure 307A/TASK 12-11-28-991-023-B78 (SHEET 7) EFF : ALL 12-11-28 R SROS
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Manual Refuel Distribution Tables - Density 0.76 To 0.795 Figure 307A/TASK 12-11-28-991-023-B88 (SHEET 8) EFF : ALL 12-11-28 R SROS
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**ON A/C ALL (Ref. Fig. 308/TASK 12-11-28-991-024-A) **ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
(Ref. Fig. 308A/TASK 12-11-28-991-024-B) **ON A/C ALL NOTE : During the refuel procedure reference to the refuel graph can include ____ reference to the applicable fuel tables. Subtask 12-11-28-650-064 A. Reference for Adjustment of the Fuel Distribution (if necessary) (1) If it becomes necessary to adjust the fuel distribution of the aircraft, do the (Ref. TASK 28-25-00-650-801) or the (Ref. TASK 2825-00-869-801). Subtask 12-11-28-650-054 B. Pressure Refuel with Manual Control CAUTION : DO NOT LET THE REFUEL PRESSURE GET TO MORE THAN 3.4 BAR (50 _______ PSI). THIS WILL PREVENT DAMAGE TO THE AIRCRAFT FUEL SYSTEM. (1) On the refuel/defuel control panel 990VU, set the switches as follows: (a) Put the REFUEL/DEFUEL VALVE switch(es) for the fuel tank(s) you want to refuel, to the OPEN position. NOTE : To refuel the trim-tank, you must have one of these ____ conditions: - the two inner-tank inlet valves are open - the center-tank inlet valve is open. - the two inner tanks fuel quantities are above 14000 kg (30865 lb).
EFF : ALL 12-11-28 R SROS
Page 374 Jan 01/07
- one inner tank fuel quantity is above 14000 kg (30865 lb) and the other inner-tank inlet valve is open. (b) Put the REFUEL/DEFUEL VALVE switch(es) for the tank(s) you do not want to refuel, to the SHUT position. (2) Start the pump on the fuel tanker/pump unit. (3) On the refuel/defuel control panel 990VU: (a) Put the MODE SELECT switch 3QU to the REFUEL position. (b) If the refuel isolation valve(s) do not open, do the next step. 1 _
On the refuel isolation valve(s), push in and hold the override P/BSW.
(c) Monitor the fuel quantity displays. NOTE : If necessary, use the applicable manual refuel ____ distribution graph to make sure that the fuel distribution is correct for flight. (d) Make sure that the numbers on the fuel quantity and ACTUAL displays increase. (e) If the trim tank is to be refuelled, it must be done in two steps: 1 _
When the trim tank fuel quantity reaches 1000 kg (2200 lb) below that shown on the applicable graph, shut the trim tank inlet valve.
2 _
When the two inner tanks are at the target value (refuel graph), open the trim tank inlet valve. NOTE : If it is necessary to refuel the trim tank, the inner ____ tank quantity will be different from the quantity given in the manual refuel graph. An allowance for this difference must be made in the trim tank fuel quantity. This allowance will also have an effect on the cg of the aircraft (the cg change is approximately 2% MAC for each 1000 kg (2204 lb) difference from the distribution graphs for trim tank fuel quantity).
EFF : ALL 12-11-28 R SROS
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Refuel Distribution Tables - Density 0.8 to 0.83 Figure 308/TASK 12-11-28-991-024-A17 (SHEET 1) EFF : ALL 12-11-28 R SROS
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Refuel Distribution Tables - Density 0.8 to 0.83 Figure 308/TASK 12-11-28-991-024-A67 (SHEET 6) EFF : ALL 12-11-28 R SROS
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INTENTIONALLY BLANK
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Manual Refuel Distribution Tables - Density 0.8 To 0.83 Figure 308A/TASK 12-11-28-991-024-B17 (SHEET 1) EFF : ALL 12-11-28 R SROS
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Manual Refuel Distribution Tables - Density 0.8 To 0.83 Figure 308A/TASK 12-11-28-991-024-B27 (SHEET 2) EFF : ALL 12-11-28 R SROS
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Manual Refuel Distribution Tables - Density 0.8 To 0.83 Figure 308A/TASK 12-11-28-991-024-B37 (SHEET 3) EFF : ALL 12-11-28 R SROS
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Manual Refuel Distribution Tables - Density 0.8 To 0.83 Figure 308A/TASK 12-11-28-991-024-B47 (SHEET 4) EFF : ALL 12-11-28 R SROS
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Manual Refuel Distribution Tables - Density 0.8 To 0.83 Figure 308A/TASK 12-11-28-991-024-B67 (SHEET 6) EFF : ALL 12-11-28 R SROS
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Manual Refuel Distribution Tables - Density 0.8 To 0.83 Figure 308A/TASK 12-11-28-991-024-B77 (SHEET 7) EFF : ALL 12-11-28 R SROS
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(f) When each tank has the correct fuel quantity, put its REFUEL/DEFUEL VALVE switch to the SHUT position. NOTE : Each tank quantity can increase 100 kg (220 lb) to 200 kg ____ (440 lb) after the REFUEL/DEFUEL VALVE switch is set to SHUT. (4) When the fuel tank quantities are correct, set the refuel/defuel control on the panel 990VU as follows: (a) Put the MODE SELECT switch to the OFF position. (b) Put the applicable REFUEL VALVES switch(es) to the NORM position. (c) If the power supply is from the battery, put the PWR SUPPLY switch to NORM. (d) If it was necessary to operate the override P/BSW, do the next step. 1 _
On the refuel isolation valve(s), release the override P/BSW.
(5) Stop the pump on the fuel tanker/pump unit. 5. Close-up ________ Subtask 12-11-28-410-052 A. Close Access (1) Disconnect the couplings of the fuel supply hoses from the aircraft refuel/defuel couplings. (2) Install the refuel/defuel coupling caps 5503QA1, 5503QA2, 5504QA1 and 5504QA2. (3) Refuel panel closure: CAUTION : DO NOT APPLY TOO MUCH FORCE TO THE OPERATING ROD WHEN YOU _______ CLOSE THE PANEL. THIS PREVENTS DAMAGE TO THE MECHANISM. (a) Close the access panels 522HB and 622HB. (4) Close the access panel 198DB.
R EFF : ALL 12-11-28 SROS
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Subtask 12-11-28-860-055 B. Aircraft Maintenance Configuration (1) If applicable, do the ADIRS stop procedure (Ref. TASK 34-10-00-860803). (2) If applicable, de-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). (3) Disconnect these ground/bonding cables: - the bonding cable between the aircraft and the fuel tanker/pump unit - if applicable, the grounding cable between the fuel tanker/pump unit and the ground - if applicable, the grounding cable between the aircraft and the ground. NOTE : The outer tank water drain valves have small holes in them to ____ prevent damage due to water freezing in the valve. These holes also let fuel flow from the outer tank to the inner tank at a rate of up to 20 kg/hour. This flow is normal and is to be expected. There is no leakage in the system. Subtask 12-11-28-942-052 C. Removal of Equipment (1) Put the chocks back in their original position. (2) Remove all the fixtures, tools, test and support equipment used during this procedure.
R EFF : ALL 12-11-28 SROS
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**ON A/C 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 701-749, TASK 12-11-28-650-807 Pressure Refuel with Automatic Control from the Cockpit WARNING : MAKE SURE THE AREA AROUND THE AIRCRAFT IS SAFE BEFORE YOU START A _______ REFUEL/DEFUEL PROCEDURE. IN THIS SAFE AREA, DO NOT LET PERSONS: - SMOKE - MAKE SPARKS OR FIRE - USE ANY EQUIPMENT WHICH IS NOT APPROVED FOR THE TASK. AIRCRAFT FUEL IS FLAMMABLE. WARNING : DO NOT SPILL FUEL ON THE ENGINES OR THE BRAKES. IF YOU SPILL FUEL ON _______ ENGINES OR BRAKES THAT ARE HOT, IT CAN CAUSE FIRES. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
two access platforms 5.0 m (16 ft. 5 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-11-28-650-801 12-11-28-650-802 12-32-28-281-806 12-34-24-860-801 24-41-00-861-801 24-41-00-862-801 28-25-00-650-801
General Refuel/Defuel Safety Procedures Refuel/Defuel Safety Procedures In The Hangar Operate Water Drain Valves to Drain Accumulated Water from Inner, Outer and Wing Vent Surge Tanks Aircraft Grounding for the Refuel/Defuel Operations Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Pressure Defuel Procedure
EFF : 201-249, 251-252, 255-299, 301-399, 12-11-28 401-449, 451-499, 701-749, R SROS
Page 393 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------28-25-00-869-801 29-00-00-863-802 31-60-00-860-801 34-10-00-860-801 34-10-00-860-803 12-11-28-991-009
Ground Fuel Transfer Procedure Pressurize the Blue Hydraulic System with the Electric Pump EIS Start Procedure ADIRS Start Procedure ADIRS Stop Procedure Fig. 309
3. __________ Job Set-up Subtask 12-11-28-941-060-A A. Safety Precautions WARNING : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND _______ DAMAGE. (1) Obey the safety procedures for the refuel procedure (Ref. TASK 12-1128-650-801) and (Ref. TASK 12-11-28-650-802). (2) Make sure that the Parking Brake System is pressurized (Ref. TASK 2900-00-863-802). (3) On the panel 117VU, make sure that the PARK BRK is ON. (4) Make sure that the chocks are in the position that follows: - move the aft NLG chocks away from the tires. During the refuel the NLG tires roll aft as the MLG shock absorber compresses - make sure that the chocks do not touch the MLG tires. The weight of the fuel can lower the aircraft and cause the tires to catch the chocks. Subtask 12-11-28-281-053-A B. Do a check for water contamination in a fuel sample removed from the fuel tanker/pump unit (Ref. TASK 12-32-28-281-806).
EFF : 201-249, 251-252, 255-299, 301-399, 12-11-28 401-449, 451-499, 701-749, R SROS
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Subtask 12-11-28-860-056-A C. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT YOU GROUND THE FUEL TANKER AND THE AIRCRAFT _______ CORRECTLY. IF YOU DO NOT A DANGEROUS ELECTRICAL DISCHARGE CAN OCCUR. (1) Ground the aircraft and the fuel tanker/pump unit (Ref. TASK 12-3424-860-801). Then bond them together electrically. NOTE : Bonding is essential, grounding is recommended. ____ (2) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (3) Do the ADIRS start procedure (Ref. TASK 34-10-00-860-801). (4) Energize the EIS (Ref. TASK 31-60-00-860-801). (5) Press the FUEL P/BSW and make sure that the FUEL page comes into view. Subtask 12-11-28-010-059 D. Get Access NOTE : You can use 1, 2, 3 or 4 refuel hoses to do an automatic pressure ____ refuel. This procedure uses four refuel hoses. (1) Put two access platforms in position, one below the access panel 522HB and one below the access panel 622HB. (2) Open the access panels 522HB and 622HB. (3) Remove the refuel/defuel coupling caps 5503QA1, 5503QA2, 5504QA1 and 5504QA2. (4) Examine the aircraft refuel/defuel couplings: WARNING : MAKE SURE THAT THE FUEL SUPPLY HOSE IS CORRECTLY CONNECTED _______ TO THE COUPLING BEFORE YOU REFUEL/DEFUEL THE AIRCRAFT. DO NOT CONNECT THE FUEL SUPPLY HOSE IF THERE ARE SIGNS OF DAMAGE TO THE AIRCRAFT COUPLING LUGS OR SLOTS. (a) Visually examine the aircraft coupling lugs and slots for signs of damage or contamination.
EFF : 201-249, 251-252, 255-299, 301-399, 12-11-28 401-449, 451-499, 701-749, R SROS
Page 395 Jan 01/07
(5) Make sure that the couplings of the fuel supply hoses are clean. Connect the four hoses to the aircraft refuel/defuel couplings 5502QA1 and 5502QA2. Subtask 12-11-28-740-052 E. Hi-Level Sense Test (1) Do this test: ------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------On the MCDU: 1. Push the line key adjacent to the LEVEL SENSE symbol.
On the MCDU: - the LEVEL SENSE TEST page shows TEST IN PROGRESS - when the test is complete the LEVEL SENSE TEST page shows TEST OK or a fault message.
(2) Push the line key adjacent to RETURN until the MCDU MENU page comes into view again. 4. Procedure _________ (Ref. Fig. 309/TASK 12-11-28-991-009) NOTE : An Automatic Refuel is only possible if the fuel quantity in each ____ tank at the start of the refuel is less than the expected quantity after the refuel. Subtask 12-11-28-650-065 A. Reference for Adjustment of the Fuel Distribution (if necessary) (1) If it becomes necessary to adjust the fuel distribution of the aircraft, do the (Ref. TASK 28-25-00-650-801) or the (Ref. TASK 2825-00-869-801).
EFF : 201-249, 251-252, 255-299, 301-399, 12-11-28 401-449, 451-499, 701-749, R SROS
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Refuel Control Panel in the Cockpit Figure 309/TASK 12-11-28-991-009 EFF : 201-249, 251-252, 255-299, 301-399, 12-11-28 401-449, 451-499, 701-749, R SROS
Page 397 Jan 01/07
Subtask 12-11-28-650-060-A B. To Input the Necessary Total Fuel Quantity (1) On the MCDU: (a) Push the INIT key and make sure that the INIT page comes into view. (b) Push the line key 2R. If a fuel quantity has not been set, an empty amber box is shown on the MCDU. (c) Use the numeric keys to set the necessary total fuel quantity. To do a refuel this quantity must be a minimum of 200 Kg (440 lb) more than the (ECAM) FOB quantity. (d) Push the line key 2R to input the set fuel quantity. To change the input fuel quantity, push the CLEAR key and the line key 2R together and do the procedure again. (e) Make sure that the INIT page now shows the correct total fuel quantity. NOTE : When you input the fuel quantity: ____ - the amber box goes out of view - on the refuel/defuel panel 990VU, the CKPT light comes on. When you have this condition, you cannot control the automatic refuel from the refuel/defuel panel 990VU. NOTE : Alternatively, the crew can use the flight plan to input ____ the necessary total fuel quantity. Subtask 12-11-28-650-061-A C. Pressure Refuel with Control from the Cockpit CAUTION : DO NOT LET THE REFUEL PRESSURE GET TO MORE THAN 3.4 BAR (50 _______ PSI). THIS WILL PREVENT DAMAGE TO THE AIRCRAFT FUEL SYSTEM. (1) Start the pump on the fuel tanker/pump unit.
EFF : 201-249, 251-252, 255-299, 301-399, 12-11-28 401-449, 451-499, 701-749, R SROS
Page 398 Jan 01/07
(2) On the FUEL panel 285VU: (a) Push (in) the REFUEL P/BSW (37QU). (b) Make sure that the ON light comes on. At the refuel/defuel coupling, the ready-to-refuel light also comes on. NOTE : When the REFUEL P/BSW is pushed in, the FCMS does an ____ automatic shut-off test. (3) On the ECAM lower SD, make sure that the tank quantities on the FUEL page increase. (4) When the refuel stops, make sure that: - the END light comes on and does not flash - on the ECAM the FOB and tank quantity displays are stable. (5) Stop the pump on the fuel tanker/pump unit. (6) On the FUEL panel 285VU: (a) Release (out) the REFUEL P/BSW. (b) Make sure that the ON and END lights go off. At the refuel/defuel coupling, the ready-to-refuel light also goes off. 5. Close-up ________ Subtask 12-11-28-410-057 A. Close Access (1) Disconnect the couplings of the four fuel supply hoses from the aircraft refuel/defuel couplings 5502QA1 and 5502QA2. (2) Install the refuel/defuel coupling caps 5503QA1, 5503QA2, 5504QA1 and 5504QA2. (3) Refuel panel closure: CAUTION : DO NOT APPLY TOO MUCH FORCE TO THE OPERATING ROD WHEN YOU _______ CLOSE THE PANEL. THIS PREVENTS DAMAGE TO THE MECHANISM. (a) Close the access panels 522HB and 622HB.
R EFF : 201-249, 251-252, 255-299, 301-399, 12-11-28 401-449, 451-499, 701-749, SROS
Page 399 Jan 01/07
Subtask 12-11-28-860-057-A B. Aircraft Maintenance Configuration (1) Put the aircraft back to its initial configuration. (a) On the ECAM control panel, set the UPPER DISPLAY and the LOWER DISPLAY potentiometers to OFF. (b) Do the ADIRS stop procedure (Ref. TASK 34-10-00-860-803). (c) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). (d) Disconnect these ground/bonding cables: - the bonding cable between the aircraft and the fuel tanker/pump unit - if applicable, the grounding cable between the fuel tanker/pump unit and the ground - if applicable, the grounding cable between the aircraft and the ground. NOTE : The outer tank water drain valves have small holes in them ____ to prevent damage due to water freezing in the valve. These holes also let fuel flow from the outer tank to the inner tank at a rate of up to 20 kg/hour. This flow is normal and is to be expected. There is no leakage in the system. Subtask 12-11-28-942-057 C. Removal of the Ground Support Equipment (1) Put the chocks back in their original position. (2) Make sure that the work area is clean and clear of tools and other items. (3) Remove the access platform(s). (4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
R EFF : 201-249, 251-252, 255-299, 301-399, 12-11-28 401-449, 451-499, 701-749, SROS
Page A300 Jan 01/07
**ON A/C ALL TASK 12-11-28-650-808 Pressure Refuel with Manual Control and Override of Individual Inlet Valve(s) WARNING : DO NOT SPILL FUEL ON THE ENGINES OR THE BRAKES. IF YOU SPILL FUEL ON _______ ENGINES OR BRAKES THAT ARE HOT, IT CAN CAUSE FIRES. 1. __________________ Reason for the Job To refuel with individual inlet valve(s) opened and closed with the deactivation tool. This will let refuel occur if the applicable actuators are inoperative. NOTE : You will need a minimum of three persons to do this task. ____ 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific D97B00-003
variable access platform access platform 3.0 m (9 ft. 10 in.) 2 access platforms 5.0 m (16 ft. 5 in.) 1 ACTUATOR MECHANICAL
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R
12-11-28-650-801 12-11-28-650-802 12-32-28-281-810 12-34-24-860-801 20-28-00-912-802 24-41-00-861-801
General Refuel/Defuel Safety Procedures Refuel/Defuel Safety Procedures In The Hangar Operate Water Drain Valves to Drain Accumulated Water from Center, Inner, Outer and Wing Vent Surge Tanks Aircraft Grounding for the Refuel/Defuel Operations Electrical Bonding of Components with Conductive Screws and Bolts and Bonding Straps Energize the Aircraft Electrical Circuits from the External Power A
EFF : ALL 12-11-28 SROS
Page A301 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-862-801 28-25-00-040-801 28-25-00-040-806 28-25-00-040-807 28-25-00-040-808 28-25-57-000-801 28-25-57-000-802 28-25-57-400-801 28-25-57-400-802 28-26-53-000-801 28-26-53-400-801 28-27-52-000-801 28-27-52-400-801 29-00-00-863-802 32-12-00-010-801 32-12-00-410-801 34-10-00-860-801 34-10-00-860-803 12-11-28-991-001 12-11-28-991-002 12-11-28-991-003 12-11-28-991-020-A
De-energize the Aircraft Electrical Circuits from the External Power A Deactivation of the Center-Tank Inlet Valve 5501QA in the Closed Position Deactivation of the Inner-Tank Inlet Valve 5603QA1(5603QA2) in the Closed Position Deactivation of the Outer-Tank Inlet Valve 5500QA1(5500QA2) in the Closed Position Deactivation of the Trim-Tank Inlet Valve 5705QA in the Closed Position Removal of the Outer-Tank Fuel Inlet-Valve Actuator 500QU1(500QU2) Removal of the Center-Tank Fuel Inlet-Valve Actuator 501QU Installation of the Outer-Tank Fuel Inlet-Valve Actuator 500QU1(500QU2) Installation of the Center-Tank Fuel Inlet-Valve Actuator 501QU Removal of the Fuel Inlet-Valve Actuator (603QL1,603QL2) Installation of the Fuel Inlet-Valve Actuator (603QL1,603QL2) Removal of the Inlet Valve Actuator 705QN Installation of the Inlet Valve Actuator 705QN Pressurize the Blue Hydraulic System with the Electric Pump Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance ADIRS Start Procedure ADIRS Stop Procedure Fig. 301 Fig. 302 Fig. 303 Fig. 305
**ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
12-11-28-991-020-B
Fig. 305A
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------**ON A/C ALL 12-11-28-991-021-A
Fig. 306
**ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
12-11-28-991-021-B
Fig. 306A
**ON A/C ALL 12-11-28-991-023-A
Fig. 307
**ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
12-11-28-991-023-B
Fig. 307A
**ON A/C ALL 12-11-28-991-024-A
Fig. 308
**ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
12-11-28-991-024-B
Fig. 308A
**ON A/C ALL 12-11-28-991-025
Fig. 310
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3. __________ Job Set-up (Ref. Fig. 301/TASK 12-11-28-991-001, 302/TASK 12-11-28-991-002, 303/TASK 12-11-28-991-003) Subtask 12-11-28-941-062 A. Safety Precautions WARNING : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND _______ DAMAGE. (1) Obey the safety procedures for the refuel procedure (Ref. TASK 12-1128-650-801) and if applicable (Ref. TASK 12-11-28-650-802). (2) On panel 312VU make sure that the ACCU PRESS on the triple indicator has sufficient pressure. If necessary, pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-802). (3) On the panel 117VU, make sure that the PARK BRK is ON. (4) Make sure that the chocks are in the position that follows: - move the aft NLG chocks away from the tires. During the refuel the NLG tires roll aft as the MLG shock absorber compresses. - make sure that the chocks do not touch the MLG tires. The weight of the fuel can lower the aircraft and cause the tires to catch the chocks. R R
Subtask 12-11-28-281-056-A B. Fuel Sampling
R R
(1) Get a sample of fuel from the fuel tanker/pump unit (Ref. TASK 12-3228-281-810) and do a check for water contamination.
R R
(2) If you use the manual refuel distribution graphs, use the fuel sample from the fuel tanker and measure its Specific Gravity (SG). Subtask 12-11-28-860-058 C. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT YOU GROUND THE FUEL TANKER AND THE AIRCRAFT _______ CORRECTLY. IF YOU DO NOT A DANGEROUS ELECTRICAL DISCHARGE CAN OCCUR.
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(1) Ground the aircraft and the fuel tanker/pump unit(s) (Ref. TASK 1234-24-860-801). Then bond them together electrically. NOTE : Bonding is essential, grounding is recommended. ____ (2) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (3) Do the ADIRS start procedure (Ref. TASK 34-10-00-860-801). NOTE : If external electrical power or APU electrical power is not ____ available, it is possible to use the aircraft batteries to do a manual refuel. But, on battery, the ADIRS do not send aircraft attitude information to the FCMS. Thus, on battery refuel, there could be a difference of 750 kg (1650 lb) between the set fuel quantity and the actual fuel quantity. Subtask 12-11-28-010-060 D. Get Access NOTE : You can use 1, 2, 3 or 4 refuel hoses to do a manual pressure ____ refuel. This procedure uses the four refuel hoses. (1) Put 2 access platforms in position, one below the access panel 522HB and one below the access panel 622HB. (2) Open the access panels 522HB and 622HB. (3) Remove the refuel/defuel coupling caps 5503QA1, 5503QA2, 5504QA1 and 5504QA2. (4) Examine the aircraft refuel/defuel couplings: WARNING : MAKE SURE THAT THE FUEL SUPPLY HOSE IS CORRECTLY CONNECTED _______ TO THE COUPLING BEFORE YOU REFUEL/DEFUEL THE AIRCRAFT. DO NOT CONNECT THE FUEL SUPPLY HOSE IF THERE ARE SIGNS OF DAMAGE TO THE AIRCRAFT COUPLING LUGS OR SLOTS. (a) Visually examine the aircraft coupling lugs and slots for signs of damage or contamination. (5) Make sure that the couplings of the fuel supply hoses are clean. Then connect them to the aircraft refuel/defuel couplings 5502QA1 and 5502QA2. (6) Open the access panel 198DB.
EFF : ALL 12-11-28 R SROS
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Subtask 12-11-28-740-053 E. Do this test: ------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------On the refuel/defuel control panel 990VU: 1. If only battery power is available, put the PWR SUPPLY switch to BAT. 2. Lift the guard, then push (in) and hold the HI LEVEL TEST switch 3QJ.
On the refuel/defuel control panel 990VU: - the hi-level lights (4QJ1, 4QJ2, 5QJ1, 5QJ2, 6QJ and 7QJ) and the OVERFLOW lights (8QJ1, 8QJ2 and 9QJ) go to the opposite condition - the CKPT and END lights come on - the fuel quantity, PRESELECTED and ACTUAL displays show all 8s.
3. Release (out) the HI-LEVEL TEST switch.
Wait for 10 seconds: - the lights go back to their initial condition - the fuel quantity, PRESELECTED and ACTUAL displays go back to their initial condition.
Subtask 12-11-28-010-061 F. Get Access to the Applicable Refuel Valve(s) (Ref. Fig. 310/TASK 12-11-28-991-025) (1) For the inner tank inlet valve(s), do this step: (a) Open the MLG doors (Ref. TASK 32-12-00-010-801). FOR 5603QA1 open the LH MLG door FOR 5603QA2 open the RH MLG door.
EFF : ALL 12-11-28 R SROS
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Mechanical Actuator - Typical Installation Figure 310/TASK 12-11-28-991-025 EFF : ALL 12-11-28 R SROS
Page A307 Jan 01/07
(2) For the outer tank inlet valve(s), do these steps: (a) Put the access platform in position below the applicable zone 574(674), between STA 1208/RIB 18 and STA 1271/RIB 19. (b) Remove the applicable access panel: FOR the FOR the
5500QA1 panel 574FB 5500QA2 panel 674FB.
(3) For the center tank inlet valve, do this step: (a) Open one of the main landing gear doors (Ref. TASK 32-12-00-010801). (4) For the trim tank inlet valve, do this step: (a) Put the variable access platform in position at zone 319. (b) Remove the access panel 312AR. Subtask 12-11-28-480-050 G. Installation of the Mechanical Actuator Tool (Ref. Fig. 310/TASK 12-11-28-991-025) (1) Remove the applicable inlet valve actuator(s): - for the inner tanks (Ref. TASK 28-26-53-000-801) - for the outer tanks (Ref. TASK 28-25-57-000-801) - for the center tank (Ref. TASK 28-25-57-000-802) - for the trim tank (Ref. TASK 28-27-52-000-801). (2) Temporarily safety the electrical connector (1) away from the valve to prevent unwanted movement. (Ref. Fig. 310/TASK 12-11-28-991-025) (3) Install the ACTUATOR MECHANICAL (D97B00-003) (6), on the studs, with the nuts (2). (4) Connect the bonding strap (4) with the bolt (3) and the nut (5) (Ref. TASK 20-28-00-912-802).
EFF : ALL 12-11-28 R SROS
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4. Procedure _________ (Ref. Fig. 303/TASK 12-11-28-991-003, 305/TASK 12-11-28-991-020-A) **ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
(Ref. Fig. 305A/TASK 12-11-28-991-020-B) **ON A/C ALL (Ref. Fig. 306/TASK 12-11-28-991-021-A) **ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
(Ref. Fig. 306A/TASK 12-11-28-991-021-B) **ON A/C ALL (Ref. Fig. 307/TASK 12-11-28-991-023-A) **ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
(Ref. Fig. 307A/TASK 12-11-28-991-023-B) **ON A/C ALL (Ref. Fig. 308/TASK 12-11-28-991-024-A) **ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
(Ref. Fig. 308A/TASK 12-11-28-991-024-B)
EFF : ALL 12-11-28 R SROS
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**ON A/C ALL Subtask 12-11-28-650-062 A. Pressure Refuel with Manual Control CAUTION : DO NOT LET THE REFUEL PRESSURE GET TO MORE THAN 3.4 BAR (50 _______ PSI). THIS WILL PREVENT DAMAGE TO THE AIRCRAFT FUEL SYSTEM. (1) On the refuel/defuel control panel 990VU, set the switches as follows: (a) Put the REFUEL/DEFUEL VALVE switch(es) for the fuel tank(s) you want to refuel, to the OPEN position. (b) Put the REFUEL/DEFUEL VALVE switch(es) for the tank(s) you do not want to refuel, to the SHUT position. (c) Put the MODE SELECT switch 3QU to the REFUEL position. (2) For the applicable fuel tank(s), turn the ACTUATOR MECHANICAL to OPEN and lock it in that position. NOTE : To refuel the trim-tank, you must have one of these ____ conditions: - the two inner-tank inlet valves are open - the center-tank inlet valve is open - the two inner tanks fuel quantities are above 14,000 kg (30,865 lb) - one inner tank fuel quantity is above 14,000 kg (30,865 lb) and the other inner-tank inlet valve is open. (3) Start the pump on the fuel tanker/pump unit. If the refuel isolation valve(s) do not open, do the next step. (a) On the refuel isolation valve(s), push in and hold the override P/BSW. (4) On the refuel/defuel control panel 990VU: (a) Monitor the fuel quantity displays. NOTE : If necessary, use the applicable manual refuel ____ distribution graph to make sure that the fuel distribution is correct for flight.
EFF : ALL 12-11-28 R SROS
Page A310 Jan 01/07
(b) Make sure that the numbers on the fuel quantity and ACTUAL displays increase. (5) If the trim tank is to be refuelled, it must be done in two steps: (a) When the trim tank fuel quantity reaches 1000 kg (2200 lb) below that shown on the applicable graph, shut the trim tank inlet valve or (if applicable), turn the ACTUATOR MECHANICAL to SHUT and lock it in that position. (b) When the two inner tanks are at the target value (refuel graph), open the trim tank inlet valve or (if applicable), turn the ACTUATOR MECHANICAL to OPEN and lock it in that position. NOTE : If it is necessary to refuel the trim tank, the inner tank ____ quantity will be different from the quantity given in the manual refuel graph. An allowance for this difference must be made in the trim tank fuel quantity. This allowance will also have an effect on the cg of the aircraft (the cg change is approximately 2% MAC for each 1000 kg (2204 lb) difference from the distribution graphs for trim tank fuel quantity). (c) When each tank has the correct fuel quantity, put its REFUEL/DEFUEL VALVE switch to the SHUT position or (if applicable), turn the ACTUATOR MECHANICAL to SHUT and lock it in that position. NOTE : Each tank quantity can increase 100 kg (220 lb) to 200 kg ____ (440 lb) after the REFUEL/DEFUEL VALVE switch is set to SHUT or (if applicable), the ACTUATOR MECHANICAL is set to the SHUT position. (6) When the fuel tank quantities are correct, stop the pump on the fuel tanker/pump unit. If it was necessary to operate the override P/BSW, do the next step. (a) On the refuel isolation valve(s), release the override P/BSW. (7) Set the refuel/defuel control on the panel 990VU as follows: (a) Put the MODE SELECT switch to the OFF position. (b) Put the applicable REFUEL VALVES switch(es) to the NORM position. (c) If the power supply is from the battery, put the PWR SUPPLY switch to NORM.
EFF : ALL 12-11-28 R SROS
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5. Close-up ________ Subtask 12-11-28-080-050 A. Removal of the Mechanical Actuator Tool (Ref. Fig. 310/TASK 12-11-28-991-025) NOTE : Do not ____ one or - MMEL - MMEL - MMEL - MMEL
remove the applicable mechanical actuator tool if you did more of these de-activation procedures: 28-25-04-A (Ref. TASK 28-25-00-040-806) 28-25-04-B (Ref. TASK 28-25-00-040-801) 28-25-04-C (Ref. TASK 28-25-00-040-808) 28-25-04-D (Ref. TASK 28-25-00-040-807).
(1) Remove the temporary attachment from the electrical connector (1). (2) Remove the nut (5) and the bolt (3). (3) Disconnect the bonding strap (4). (4) Remove the nuts (2) and the ACTUATOR MECHANICAL (6). (5) Install the applicable inlet valve actuator(s): - for the inner tanks (Ref. TASK 28-26-53-400-801) - for the outer tanks (Ref. TASK 28-25-57-400-801) - for the center tank (Ref. TASK 28-25-57-400-802) - for the trim tank (Ref. TASK 28-27-52-400-801). Subtask 12-11-28-410-059 B. Close Access to the Applicable Refuel Valve(s) (1) For the inner tank(s) and/or center tank inlet valve(s), close the applicable MLG door (Ref. TASK 32-12-00-410-801). (2) For the outer tank inlet valve(s), do these steps: (a) Install the applicable access panel: FOR the FOR the
5500QA1 panel 574FB 5500QA2 panel 674FB.
(3) For the trim tank inlet valve, install the access panel 312AR.
EFF : ALL 12-11-28 R SROS
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Subtask 12-11-28-410-058 C. Close Access (1) Disconnect the couplings of the fuel supply hoses from the aircraft refuel/defuel couplings. (2) Install the refuel/defuel coupling caps 5503QA1, 5503QA2, 5504QA1 and 5504QA2. (3) Refuel panel closure CAUTION : DO NOT APPLY TOO MUCH FORCE TO THE OPERATING ROD WHEN YOU _______ CLOSE THE PANEL. THIS PREVENTS DAMAGE TO THE MECHANISM. (a) Close the access panels 522HB and 622HB. (4) Close the access panel 198DB. Subtask 12-11-28-860-059 D. Aircraft Maintenance Configuration (1) If applicable, do the ADIRS stop procedure (Ref. TASK 34-10-00-860803). (2) If applicable, de-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). (3) Disconnect these ground/bonding cables: - the bonding cable between the aircraft and the fuel tanker/pump unit - if applicable, the grounding cable between the fuel tanker/pump unit and the ground - if applicable, the grounding cable between the aircraft and the ground. NOTE : The outer tank water drain valves have small holes in them to ____ prevent damage due to water freezing in the valve. These holes also let fuel flow from the outer tank to the inner tank at a rate of up to 20 kg/hour. This flow is normal and is to be expected. There is no leakage in the system.
EFF : ALL 12-11-28 R SROS
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Subtask 12-11-28-942-058 E. Removal of the Ground Support Equipment (1) Put the chocks back in their original position. (2) Remove the access platform(s). (3) Remove the ground support and maintenance equipment, the special and standard tools and all other items. (4) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 12-11-28 R SROS
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TASK 12-11-28-650-805 Overwing Refuel Procedure WARNING : MAKE SURE THE AREA AROUND THE AIRCRAFT IS SAFE BEFORE YOU START A _______ REFUEL/DEFUEL PROCEDURE. IN THIS SAFE AREA, DO NOT LET PERSONS: - SMOKE - MAKE SPARKS OR FIRE - USE ANY EQUIPMENT WHICH IS NOT APPROVED FOR THE TASK. AIRCRAFT FUEL IS FLAMMABLE. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THE WHEEL CHOCKS ARE IN POSITION. MOVEMENTS OF THE _______ AIRCRAFT COULD BE DANGEROUS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific 98D27803000000
2 access platforms 5.8 m (19 ft.) 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
EFF : ALL 12-11-28 R SROS
Page A315 Jan 01/07
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-11-28-650-801 12-11-28-650-802 12-32-28-281-806 12-34-24-860-801 24-41-00-861-801 24-41-00-862-801 27-80-00-866-802 28-25-00-869-801 29-00-00-863-802 31-60-00-860-801 31-60-00-860-802 34-10-00-860-801 34-10-00-860-803 12-11-28-991-001 12-11-28-991-004
General Refuel/Defuel Safety Procedures Refuel/Defuel Safety Procedures In The Hangar Operate Water Drain Valves to Drain Accumulated Water from Inner, Outer and Wing Vent Surge Tanks Aircraft Grounding for the Refuel/Defuel Operations Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Retraction of the Slats on the Ground Ground Fuel Transfer Procedure Pressurize the Blue Hydraulic System with the Electric Pump EIS Start Procedure EIS Stop Procedure ADIRS Start Procedure ADIRS Stop Procedure Fig. 301 Fig. 311
3. __________ Job Set-up (Ref. Fig. 301/TASK 12-11-28-991-001, 311/TASK 12-11-28-991-004) Subtask 12-11-28-941-054 A. Safety Precautions WARNING : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND _______ DAMAGE. (1) Obey the safety procedures for the refuel procedure (Ref. TASK 12-1128-650-801) and if applicable (Ref. TASK 12-11-28-650-802). (2) On panel 312VU make sure that the ACCU PRESS on the triple indicator has sufficiant pressure. If necessary, pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-802). (3) On the panel 117VU, make sure that the PARK BRK is ON.
EFF : ALL 12-11-28 R SROS
Page A316 Jan 01/07
Overwing Refuel-Adaptor Cap Figure 311/TASK 12-11-28-991-004 EFF : ALL 12-11-28 R SROS
Page A317 Jan 01/07
(4) Make sure that the chocks are in the position that follows: - move the aft NLG chocks away from the tires. During the refuel the NLG tires roll aft as the MLG shock absorber compresses. - make sure that the chocks do not touch the MLG tires. The weight of the fuel can lower the aircraft and cause the tires to catch the chocks. Subtask 12-11-28-281-055 B. Make sure that a fuel sampling for water contamination check is done to the fuel in the fuel tanker/pump units (Ref. TASK 12-32-28-281-806). Subtask 12-11-28-860-050 C. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT YOU GROUND THE FUEL TANKER AND THE AIRCRAFT _______ CORRECTLY. IF YOU DO NOT A DANGEROUS ELECTRICAL DISCHARGE CAN OCCUR. (1) Ground the aircraft and the fuel tanker/pump unit(s) (Ref. TASK 1234-24-860-801). Then electrically bond them together. NOTE : Bonding is essential, grounding is recommended. ____ (2) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (3) Do the ADIRS start procedure (Ref. TASK 34-10-00-860-801). (4) Energize the EIS (Ref. TASK 31-60-00-860-801). (5) Push the FUEL pushbutton switch on the ECAM control panel. Read and make a record of the fuel contents. (6) Make sure the slats are retracted (Ref. TASK 27-80-00-866-802). (7) Installation of control locks WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE _______ WARNING NOTICES ARE IN POSITION. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. (a) Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) on the flap/slat control lever.
EFF : ALL 12-11-28 R SROS
Page A318 Jan 01/07
(b) Put a warning notice in the cockpit, to tell persons not to operate the flap/slat control. Subtask 12-11-28-941-055 D. Installation of Ground Support Equipment NOTE : The overwing refuel can be done through the LH wing, the RH wing ____ or the 2 wings. This procedure is through the 2 wings. (1) Position 2 access platforms adjacent to the wing leading edge. Put one near the overwing refuel cap 5508QA1 and one near the overwing refuel cap 5508QA2. 4. Procedure _________ WARNING : DO NOT GET AIRCRAFT FUEL: _______ - IN YOUR MOUTH - IN YOUR EYES - ON YOUR SKIN FOR A LONG TIME. WARNING : DO NOT GET YOUR CLOTHES SOAKED WITH FUEL. _______ AIRCRAFT FUEL IS POISONOUS AND CAN GO THROUGH YOUR SKIN INTO YOUR BODY. IF YOU ARE CONTAMINATED WASH WITH CLEAN WATER AND IF NECESSARY GET MEDICAL HELP. CAUTION : DO NOT LET THE REFUEL HOSE TOUCH THE SLATS. THIS WILL PREVENT _______ DAMAGE TO THE SLATS. Subtask 12-11-28-650-055-A A. Refuel Procedure CAUTION : KEEP THE RATE OF FUEL GROUND TRANSFER THE SAME AS (OR LESS _______ THAN) THE RATE OF FLOW INTO THE INNER TANK. (1) Connect the ground cables of the refuel nozzles to the wing ground connections. (2) Remove the overwing refuel caps 5508QA1 and 5508QA2. (3) Put the fuel nozzles in the overwing refuel points and start the pump on the fuel tanker/pump units.
EFF : ALL 12-11-28 R SROS
Page A319 Jan 01/07
(4) Start a ground fuel transfer from the inner tanks to the other fuel tanks (Ref. TASK 28-25-00-869-801). NOTE : You cannot use this procedure to fill the trim tank. ____ (5) Fill the inner tanks with the necessary amount of fuel. NOTE : Be careful not to overfill the tanks during refuel. There is ____ no automatic cut-out when you do the overwing refuel procedure. (6) When the fuel quantities are correct, stop the pump on the fuel tanker/pump unit. (7) Stop the ground fuel transfer (Ref. TASK 28-25-00-869-801). 5. Close-up ________ Subtask 12-11-28-410-054 A. Close Access (1) Remove the fuel nozzles from the overwing refuel points. (2) Install the overwing refuel caps 5508QA1 and 5508QA2. Make sure each cap is correctly aligned with the indicator arrow on the wing skin. (3) Disconnect the ground cables of the refuel nozzles from the wing ground connections. Subtask 12-11-28-860-051 B. Aircraft Maintenance Configuration (1) Disconnect these ground/bonding cables: - the bonding cable between the aircraft and the fuel tanker/pump unit - if applicable, the grounding cable between the fuel tanker/pump unit and the ground - if applicable, the grounding cable between the aircraft and the ground. (2) On the MCDU, push the line key adjacent to the RETURN indication until the MCDU MENU page comes into view. (3) On the MCDU, set the BRT knob to OFF.
EFF : ALL 12-11-28 R SROS
Page A320 Jan 01/07
(4) Do the EIS stop procedure (Ref. TASK 31-60-00-860-802). (5) Do the ADIRS stop procedure (Ref. TASK 34-10-00-860-803). (6) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). NOTE : The outer tank water drain valves have small holes in them to ____ prevent damage due to water freezing in the valve. These holes also let fuel flow from the outer tank to the inner tank at a rate of up to 20 kg/hour. This flow is normal and is to be expected. There is no leakage in the system. Subtask 12-11-28-942-054 C. Removal of Equipment (1) Put the chocks back in their original position. (2) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) from the flap/slat control lever and the warning notices from the cockpit. (3) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 12-11-28 R SROS
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TASK 12-11-28-650-806 Procedure To Use The Fuel Magnetic Level Indicators 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 4M (13 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-11-28-860-801 R R
12-32-28-281-810 28-51-00-740-803
Procedure To Use The ADIRU to Find the Pitch and Roll Data Operate Water Drain Valves to Drain Accumulated Water from Center, Inner, Outer and Wing Vent Surge Tanks Interrogation of the FCMS Input Parameters Pages
**ON A/C ALL Post SB
28-3078 For A/C 251-252,701-749,
12-11-28-991-007
Fig. 312
**ON A/C ALL 12-11-28-991-006-A 12-11-28-991-005 12-11-28-991-010
Fig. 313 Fig. 314 Fig. 315
EFF : ALL 12-11-28 SROS
Page A322 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------**ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
12-11-28-991-010-A
Fig. 315A
**ON A/C ALL 12-11-28-991-011
Fig. 316
**ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
12-11-28-991-011-A
Fig. 316A
**ON A/C ALL 12-11-28-991-012
Fig. 317
**ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
12-11-28-991-012-A
Fig. 317A
**ON A/C ALL 12-11-28-991-038
Fig. 318
**ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
12-11-28-991-038-A
Fig. 318A
**ON A/C ALL 12-11-28-991-014
Fig. 319
EFF : ALL 12-11-28 R SROS
Page A323 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------**ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
12-11-28-991-014-A
Fig. 319A
**ON A/C ALL 12-11-28-991-015
Fig. 320
**ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
12-11-28-991-015-A
Fig. 320A
**ON A/C ALL 12-11-28-991-016
Fig. 321
**ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
12-11-28-991-016-A
Fig. 321A
**ON A/C ALL 12-11-28-991-017
Fig. 322
**ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
12-11-28-991-017-A
Fig. 322A
**ON A/C ALL 12-11-28-991-018
Fig. 323
EFF : ALL 12-11-28 R SROS
Page A324 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------**ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
12-11-28-991-018-A
Fig. 323A
**ON A/C ALL 3. __________ Job Set-up (Ref. Fig. 312/TASK 12-11-28-991-007) Subtask 12-11-28-860-065 A. Aircraft Maintenance Configuration NOTE : The fuel quantity table for the inner tank MLI gives the fuel ____ value for the inner tank. This value includes the collector cell contents up to the same level as the adjacent inner tank. When the main fuel pumps operate, the collector cell fuel level is higher than for the inner tank. When the pumps operate (and for 10 minutes after they stop) this quantity of fuel cannot be calculated accurately. After 10 minutes, the fuel in the collector cell is at a known level and will decrease at a known rate. The Collector Cells - Correction Factor Graph identifies the quantity of fuel to add to the MLI quantity to get the correct inner tank contents. (1) Make a note of when the pumps were stopped. Use this time as the reference datum when you use the Collector Cells - Correction Factor Graph.
EFF : ALL 12-11-28 R SROS
Page A325 Jan 01/07
Collector Cells - Correction Factor Graph Figure 312/TASK 12-11-28-991-007 EFF : ALL 12-11-28 R SROS
Page A326 Jan 01/07
Subtask 12-11-28-941-061-A B. Get Access (1) Put an ACCESS PLATFORM 4M (13 FT) below the applicable fuel Magnetic Level Indicator (MLI). NOTE : The MLI in the center and inner tanks are accurate to plus or ____ minus 5% of their indication. The MLI in the outer tanks are accurate to plus or minus 7.5% of their indication. MLI values are not as accurate as the values given by the FCMC and you must not use them for comparison. Subtask 12-11-28-010-058 C. Get Access (1) Open the access panel 198DB. R R
Subtask 12-11-28-281-051-A D. Find the Specific Gravity
R R
(1) Get a fuel sample from the aircraft (Ref. TASK 12-32-28-281-810) and measure its Specific Gravity (SG).
R R
NOTE : The SG is also available on the FCMS Input Parameters Page 3 ____ (Ref. TASK 28-51-00-740-803). 4. Procedure _________ (Ref. Fig. 313/TASK 12-11-28-991-006-A, 314/TASK 12-11-28-991-005, 315/TASK 12-11-28-991-010) **ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
(Ref. Fig. 315A/TASK 12-11-28-991-010-A) **ON A/C ALL (Ref. Fig. 316/TASK 12-11-28-991-011)
EFF : ALL 12-11-28 SROS
Page A327 Jan 01/07
Magnetic Level Indicators - Location Figure 313/TASK 12-11-28-991-006-A EFF : ALL 12-11-28 R SROS
Page A328 Jan 01/07
Attitude Monitor - Location Figure 314/TASK 12-11-28-991-005 EFF : ALL 12-11-28 R SROS
Page A329 Jan 01/07
Fuel Quantity Tables - Center Tank MLI Figure 315/TASK 12-11-28-991-010- 17 (SHEET 1) EFF : ALL 12-11-28 R SROS
Page A330 Jan 01/07
Fuel Quantity Tables - Center Tank MLI Figure 315/TASK 12-11-28-991-010- 27 (SHEET 2) EFF : ALL 12-11-28 R SROS
Page A331 Jan 01/07
Fuel Quantity Tables - Center Tank MLI Figure 315/TASK 12-11-28-991-010- 37 (SHEET 3) EFF : ALL 12-11-28 R SROS
Page A332 Jan 01/07
Fuel Quantity Tables - Center Tank MLI Figure 315/TASK 12-11-28-991-010- 47 (SHEET 4) EFF : ALL 12-11-28 R SROS
Page A333 Jan 01/07
Fuel Quantity Tables - Center Tank MLI Figure 315/TASK 12-11-28-991-010- 57 (SHEET 5) EFF : ALL 12-11-28 R SROS
Page A334 Jan 01/07
Fuel Quantity Tables - Center Tank MLI Figure 315/TASK 12-11-28-991-010- 67 (SHEET 6) R EFF : ALL 12-11-28 SROS
Page A335 Jan 01/07
Fuel Quantity Tables - Center Tank MLI Figure 315/TASK 12-11-28-991-010- 77 (SHEET 7) R EFF : ALL 12-11-28 SROS
Page A336 Jan 01/07
INTENTIONALLY BLANK
R 12-11-28 SROS
Page A337 Jan 01/07
R
Fuel Quantity Tables - Center Tank MLI Figure 315A/TASK 12-11-28-991-010-A16 (SHEET 1)
EFF : 251-252, 701-749, 12-11-28 SROS
Page A338 Jan 01/07
R
Fuel Quantity Tables - Center Tank MLI Figure 315A/TASK 12-11-28-991-010-A26 (SHEET 2)
EFF : 251-252, 701-749, 12-11-28 SROS
Page A339 Jan 01/07
R
Fuel Quantity Tables - Center Tank MLI Figure 315A/TASK 12-11-28-991-010-A36 (SHEET 3)
EFF : 251-252, 701-749, 12-11-28 SROS
Page A340 Jan 01/07
R
Fuel Quantity Tables - Center Tank MLI Figure 315A/TASK 12-11-28-991-010-A46 (SHEET 4)
EFF : 251-252, 701-749, 12-11-28 SROS
Page A341 Jan 01/07
R
Fuel Quantity Tables - Center Tank MLI Figure 315A/TASK 12-11-28-991-010-A56 (SHEET 5)
R EFF : 251-252, 701-749, 12-11-28 SROS
Page A342 Jan 01/07
R
Fuel Quantity Tables - Center Tank MLI Figure 315A/TASK 12-11-28-991-010-A66 (SHEET 6)
R EFF : 251-252, 701-749, 12-11-28 SROS
Page A343 Jan 01/07
Fuel Quantity Tables - MLI No. 1 Figure 316/TASK 12-11-28-991-011- 16 (SHEET 1) EFF : ALL 12-11-28 R SROS
Page A344 Jan 01/07
Fuel Quantity Tables - MLI No. 1 Figure 316/TASK 12-11-28-991-011- 26 (SHEET 2) EFF : ALL 12-11-28 R SROS
Page A345 Jan 01/07
Fuel Quantity Tables - MLI No. 1 Figure 316/TASK 12-11-28-991-011- 36 (SHEET 3) EFF : ALL 12-11-28 R SROS
Page A346 Jan 01/07
Fuel Quantity Tables - MLI No. 1 Figure 316/TASK 12-11-28-991-011- 46 (SHEET 4) EFF : ALL 12-11-28 R SROS
Page A347 Jan 01/07
Fuel Quantity Tables - MLI No. 1 Figure 316/TASK 12-11-28-991-011- 56 (SHEET 5) EFF : ALL 12-11-28 R SROS
Page A348 Jan 01/07
Fuel Quantity Tables - MLI No. 1 Figure 316/TASK 12-11-28-991-011- 66 (SHEET 6) EFF : ALL 12-11-28 R SROS
Page A349 Jan 01/07
**ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
(Ref. Fig. 316A/TASK 12-11-28-991-011-A) **ON A/C ALL (Ref. Fig. 317/TASK 12-11-28-991-012) **ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
(Ref. Fig. 317A/TASK 12-11-28-991-012-A) **ON A/C ALL (Ref. Fig. 318/TASK 12-11-28-991-038) **ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
(Ref. Fig. 318A/TASK 12-11-28-991-038-A) **ON A/C ALL (Ref. Fig. 319/TASK 12-11-28-991-014) **ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
(Ref. Fig. 319A/TASK 12-11-28-991-014-A) **ON A/C ALL (Ref. Fig. 320/TASK 12-11-28-991-015)
R EFF : ALL 12-11-28 SROS
Page A350 Jan 01/07
**ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
(Ref. Fig. 320A/TASK 12-11-28-991-015-A) **ON A/C ALL (Ref. Fig. 321/TASK 12-11-28-991-016) **ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
(Ref. Fig. 321A/TASK 12-11-28-991-016-A) **ON A/C ALL (Ref. Fig. 322/TASK 12-11-28-991-017) **ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
(Ref. Fig. 322A/TASK 12-11-28-991-017-A) **ON A/C ALL (Ref. Fig. 323/TASK 12-11-28-991-018) **ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
(Ref. Fig. 323A/TASK 12-11-28-991-018-A)
R EFF : ALL 12-11-28 SROS
Page A351 Jan 01/07
Fuel Quantity Tables - MLI No. 1 Figure 316A/TASK 12-11-28-991-011-A16 (SHEET 1) EFF : 251-252, 701-749, 12-11-28 R SROS
Page A352 Jan 01/07
Fuel Quantity Tables - MLI No. 1 Figure 316A/TASK 12-11-28-991-011-A26 (SHEET 2) EFF : 251-252, 701-749, 12-11-28 R SROS
Page A353 Jan 01/07
Fuel Quantity Tables - MLI No. 1 Figure 316A/TASK 12-11-28-991-011-A36 (SHEET 3) EFF : 251-252, 701-749, 12-11-28 R SROS
Page A354 Jan 01/07
Fuel Quantity Tables - MLI No. 1 Figure 316A/TASK 12-11-28-991-011-A46 (SHEET 4) EFF : 251-252, 701-749, 12-11-28 R SROS
Page A355 Jan 01/07
Fuel Quantity Tables - MLI No. 1 Figure 316A/TASK 12-11-28-991-011-A56 (SHEET 5) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A356 Jan 01/07
Fuel Quantity Tables - MLI No. 1 Figure 316A/TASK 12-11-28-991-011-A66 (SHEET 6) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A357 Jan 01/07
Fuel Quantity Tables - MLI No. 2 Figure 317/TASK 12-11-28-991-012- 14 (SHEET 1) EFF : ALL 12-11-28 R SROS
Page A358 Jan 01/07
Fuel Quantity Tables - MLI No. 2 Figure 317/TASK 12-11-28-991-012- 24 (SHEET 2) EFF : ALL 12-11-28 R SROS
Page A359 Jan 01/07
Fuel Quantity Tables - MLI No. 2 Figure 317/TASK 12-11-28-991-012- 34 (SHEET 3) R EFF : ALL 12-11-28 SROS
Page A360 Jan 01/07
Fuel Quantity Tables - MLI No. 2 Figure 317/TASK 12-11-28-991-012- 44 (SHEET 4) R EFF : ALL 12-11-28 SROS
Page A361 Jan 01/07
Fuel Quantity Tables - MLI No. 2 Figure 317A/TASK 12-11-28-991-012-A14 (SHEET 1) EFF : 251-252, 701-749, 12-11-28 R SROS
Page A362 Jan 01/07
Fuel Quantity Tables - MLI No. 2 Figure 317A/TASK 12-11-28-991-012-A24 (SHEET 2) EFF : 251-252, 701-749, 12-11-28 R SROS
Page A363 Jan 01/07
Fuel Quantity Tables - MLI No. 2 Figure 317A/TASK 12-11-28-991-012-A34 (SHEET 3) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A364 Jan 01/07
Fuel Quantity Tables - MLI No. 2 Figure 317A/TASK 12-11-28-991-012-A44 (SHEET 4) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A365 Jan 01/07
Fuel Quantity Tables - MLI No. 3 Figure 318/TASK 12-11-28-991-038- 13 (SHEET 1) EFF : ALL 12-11-28 R SROS
Page A366 Jan 01/07
Fuel Quantity Tables - MLI No. 3 Figure 318/TASK 12-11-28-991-038- 23 (SHEET 2) R EFF : ALL 12-11-28 SROS
Page A367 Jan 01/07
Fuel Quantity Tables - MLI No. 3 Figure 318/TASK 12-11-28-991-038- 33 (SHEET 3) R EFF : ALL 12-11-28 SROS
Page A368 Jan 01/07
INTENTIONALLY BLANK
R 12-11-28 SROS
Page A369 Jan 01/07
Fuel Quantity Tables - MLI No. 3 Figure 318A/TASK 12-11-28-991-038-A13 (SHEET 1) EFF : 251-252, 701-749, 12-11-28 R SROS
Page A370 Jan 01/07
Fuel Quantity Tables - MLI No. 3 Figure 318A/TASK 12-11-28-991-038-A23 (SHEET 2) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A371 Jan 01/07
Fuel Quantity Tables - MLI No. 3 Figure 318A/TASK 12-11-28-991-038-A33 (SHEET 3) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A372 Jan 01/07
INTENTIONALLY BLANK
R 12-11-28 SROS
Page A373 Jan 01/07
Fuel Quantity Tables - MLI No. 4 Figure 319/TASK 12-11-28-991-014- 13 (SHEET 1) EFF : ALL 12-11-28 R SROS
Page A374 Jan 01/07
Fuel Quantity Tables - MLI No. 4 Figure 319/TASK 12-11-28-991-014- 23 (SHEET 2) R EFF : ALL 12-11-28 SROS
Page A375 Jan 01/07
Fuel Quantity Tables - MLI No. 4 Figure 319/TASK 12-11-28-991-014- 33 (SHEET 3) R EFF : ALL 12-11-28 SROS
Page A376 Jan 01/07
INTENTIONALLY BLANK
R 12-11-28 SROS
Page A377 Jan 01/07
Fuel Quantity Tables - MLI No. 4 Figure 319A/TASK 12-11-28-991-014-A13 (SHEET 1) EFF : 251-252, 701-749, 12-11-28 R SROS
Page A378 Jan 01/07
Fuel Quantity Tables - MLI No. 4 Figure 319A/TASK 12-11-28-991-014-A23 (SHEET 2) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A379 Jan 01/07
Fuel Quantity Tables - MLI No. 4 Figure 319A/TASK 12-11-28-991-014-A33 (SHEET 3) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A380 Jan 01/07
INTENTIONALLY BLANK
R 12-11-28 SROS
Page A381 Jan 01/07
Fuel Quantity Tables - MLI No. 5 Figure 320/TASK 12-11-28-991-015- 12 (SHEET 1) R EFF : ALL 12-11-28 SROS
Page A382 Jan 01/07
Fuel Quantity Tables - MLI No. 5 Figure 320/TASK 12-11-28-991-015- 22 (SHEET 2) R EFF : ALL 12-11-28 SROS
Page A383 Jan 01/07
Fuel Quantity Tables - MLI No. 5 Figure 320A/TASK 12-11-28-991-015-A12 (SHEET 1) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A384 Jan 01/07
Fuel Quantity Tables - MLI No. 5 Figure 320A/TASK 12-11-28-991-015-A22 (SHEET 2) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A385 Jan 01/07
Fuel Quantity Tables - MLI No. 6 Figure 321/TASK 12-11-28-991-016- 12 (SHEET 1) R EFF : ALL 12-11-28 SROS
Page A386 Jan 01/07
Fuel Quantity Tables - MLI No. 6 Figure 321/TASK 12-11-28-991-016- 22 (SHEET 2) R EFF : ALL 12-11-28 SROS
Page A387 Jan 01/07
Fuel Quantity Tables - MLI No. 6 Figure 321A/TASK 12-11-28-991-016-A12 (SHEET 1) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A388 Jan 01/07
Fuel Quantity Tables - MLI No. 6 Figure 321A/TASK 12-11-28-991-016-A22 (SHEET 2) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A389 Jan 01/07
Fuel Quantity Tables - MLI No. 7 Figure 322/TASK 12-11-28-991-017- 12 (SHEET 1) R EFF : ALL 12-11-28 SROS
Page A390 Jan 01/07
Fuel Quantity Tables - MLI No. 7 Figure 322/TASK 12-11-28-991-017- 22 (SHEET 2) R EFF : ALL 12-11-28 SROS
Page A391 Jan 01/07
Fuel Quantity Tables - MLI No. 7 Figure 322A/TASK 12-11-28-991-017-A12 (SHEET 1) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A392 Jan 01/07
Fuel Quantity Tables - MLI No. 7 Figure 322A/TASK 12-11-28-991-017-A22 (SHEET 2) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A393 Jan 01/07
Fuel Quantity Tables - MLI No. 8 Figure 323/TASK 12-11-28-991-018- 12 (SHEET 1) R EFF : ALL 12-11-28 SROS
Page A394 Jan 01/07
Fuel Quantity Tables - MLI No. 8 Figure 323/TASK 12-11-28-991-018- 22 (SHEET 2) R EFF : ALL 12-11-28 SROS
Page A395 Jan 01/07
Fuel Quantity Tables - MLI No. 8 Figure 323A/TASK 12-11-28-991-018-A12 (SHEET 1) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A396 Jan 01/07
Fuel Quantity Tables - MLI No. 8 Figure 323A/TASK 12-11-28-991-018-A22 (SHEET 2) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A397 Jan 01/07
**ON A/C ALL Subtask 12-11-28-869-054-B A. Procedure to Use the Magnetic Level Indicators CAUTION : DO NOT LET THE MLIs FALL FREELY. _______ THE MLIs ARE FRAGILE. CAUTION : RETRACT THE MLIs AS SOON AS POSSIBLE. YOU CAN EASILY CAUSE _______ DAMAGE TO AN EXTENDED MLI. NOTE : Start the procedure with each of the outboard MLIs in the Outer ____ and Inner Tank. If they give no indication move inboard to each subsequent MLI until the MLI gives an indication. At the first MLI that gives an indication, use that MLI for the procedure. NOTE : If the attitude monitor is unservicable, refer to (Ref. TASK 12____ 11-28-860-801). (1) Use a screwdriver to push (in) the applicable MLI and turn it through 90 deg. (2) Hold and carefully lower the MLI fully. Then carefully lift the MLI until you feel the magnets engage. (3) Read the units mark nearest to the bottom skin of the wing and write down the number. (4) Retract the MLI and use a screwdriver to turn it through 90 deg to lock it. (5) Do this procedure for each applicable MLI. NOTE : You will only use one MLI reading from each applicable tank. ____ (6) Calculation Procedure (a) Read and write down the aircraft attitude (grid-square letter and grid-square number shown on the attitude monitor). (b) Use the table for the applicable aircraft attitude (grid-square letter and grid-square number) and the applicable MLI to find the volume of fuel in each tank.
EFF : ALL 12-11-28 R SROS
Page A398 Jan 01/07
(c) For an inner tank, there can be additional fuel in the collector-cells. Use the graph to find the additional fuel quantity in one inner tank. (Ref. Fig. 312/TASK 12-11-28-991-007) NOTE : The fuel quantity in the collector cell will decrease with ____ time. Use the applicable curve for the time since the main fuel pumps were switched off. The data taken from this curve gives a more accurate fuel quantity. (d) Add together the value from each tank to find the total volume of fuel. (e) Multiply the total volume of fuel by the SG of the fuel. The result is the total weight of fuel. NOTE : The trim tank can also contain a fuel quantity of between ____ zero and 4800 kg (10582 lb). **ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
Subtask 12-11-28-869-054-C A. Procedure to Use the Magnetic Level Indicators CAUTION : DO NOT LET THE MLIs FALL FREELY. _______ THE MLIs ARE FRAGILE. CAUTION : RETRACT THE MLIs AS SOON AS POSSIBLE. YOU CAN EASILY CAUSE _______ DAMAGE TO AN EXTENDED MLI. NOTE : Start the procedure with each of the outboard MLIs in the Outer ____ and Inner Tank. If they give no indication move inboard to each subsequent MLI until the MLI gives an indication. At the first MLI that gives an indication, use that MLI for the procedure. (1) Use a screwdriver to push (in) the applicable MLI and turn it through 90 deg. (2) Hold and carefully lower the MLI fully. Then carefully lift the MLI until you feel the magnets engage. (3) Read the units mark nearest to the bottom skin of the wing and write down the number.
EFF : ALL 12-11-28 R SROS
Page A399 Jan 01/07
(4) Retract the MLI and use a screwdriver to turn it through 90 deg to lock it. (5) Do this procedure for each applicable MLI. NOTE : You will only use one MLI reading from each applicable tank. ____ (6) Calculation Procedure (a) Use the table for the applicable ADIRS aircraft attitude data (Ref. TASK 12-11-28-860-801) and MLI to calculate the volume of fuel in each tank. (b) As an option you can use the applicable page of the FCMS Input Parameters to find the aircraft attitude (Ref. TASK 28-51-00-740803). (c) For an inner tank, there can be additional fuel in the collector-cells. Use the graph to find the additional fuel quantity in one inner tank. (Ref. Fig. 312/TASK 12-11-28-991-007) NOTE : The fuel quantity in the collector cell will decrease with ____ time. Use the applicable curve for the time since the main fuel pumps were switched off. The data taken from this curve gives a more accurate fuel quantity. (d) Add together the value from each tank to find the total volume of fuel. (e) Multiply the total volume of fuel by the SG of the fuel. The result is the total weight of fuel. NOTE : The trim tank can also contain a fuel quantity of between ____ zero and 4800 kg (10582 lb). **ON A/C ALL 5. Close-up ________ Subtask 12-11-28-410-056 A. Close Access (1) Close the access panel 198DB.
EFF : ALL 12-11-28 R SROS
Page B300 Jan 01/07
Subtask 12-11-28-942-056 B. Removal of Equipment (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 12-11-28 R SROS
Page B301 Jan 01/07
TASK 12-11-28-860-801 Procedure To Use The ADIRU to Find the Pitch and Roll Data 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
12-11-28-650-806 24-41-00-861-801 24-41-00-862-801 12-11-28-991-027
Procedure To Use The Fuel Magnetic Level Indicators Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Fig. 324
3. __________ Job Set-up Subtask 12-11-28-861-053 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). 4. Procedure _________ Subtask 12-11-28-860-060 A. Procedure (Ref. Fig. 324/TASK 12-11-28-991-027) (1) On the panel 221VU set the 3 ADIRS switches to the NAV position. (2) Do this procedure NOTE : The procedure that follows is only applicable to the MCDU 2 ____ and the MCDU 3. You cannot do this procedure with the MCDU 1. The actions and the results of this procedure occur on the MCDU used.
EFF : ALL 12-11-28 SROS
Page B302 Jan 01/07
INTENTIONALLY BLANK
R 12-11-28 SROS
Page B303 Jan 01/07
Pitch and Roll Data Access from the ADIRUs Figure 324/TASK 12-11-28-991-027- 12 (SHEET 1) EFF : ALL 12-11-28 R SROS
Page B304 Jan 01/07
Pitch and Roll Data Access from the ADIRUs Figure 324/TASK 12-11-28-991-027- 22 (SHEET 2) EFF : ALL 12-11-28 SROS
Page B305 Jan 01/07
------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------1. On the MCDU turn the BRT knob
- the MCDU is on.
2. Push the MCDU MENU mode key
- the MCDU MENU page shows.
3. Push the line key adjacent to the ACMS indication
- the ACMS PARAMETER CALL-UP page shows.
4. Push the line key adjacent to the ALPHA indication
- the ALPHA CALL-UP CTRL page shows.
5. Push the line key adjacent to the LIST indication
- the ALPHA LIST page shows.
6. Use the ALPHA LIST that follows to find the ALPHA CODE for the ROLL and PITCH data. 7. Push the line key adjacent to the RETURN indication
- the ALPHA CALL-UP CTRL page shows.
8. Push the line key adjacent to the ALPHA MENU DISPLAY indication
- the ALPHA CALL-UP page shows.
9. On the MCDU scratchpad enter the alpha code for ROLL, and push the line key adjacent to the first line
- the ALPHA CALL-UP page shows the ROLL data.
10. On the MCDU scratchpad enter the alpha code for PITCH, and push the line key adjacent to the second line
- the ALPHA CALL-UP page shows the PITCH data.
11. If you need to copy the data, push the line key next to the PRINT indication
- after approximately 20 seconds, the screen data is printed.
12. Push the line key next to the RETURN indication
- the ALPHA CALL-UP CTRL page shows.
13. Push the line key adjacent to the CLEAR indication
- the ALPHA CALL-UP CTRL page shows the message ALL ENTRIES CLEARED.
EFF : ALL 12-11-28 SROS
Page B306 Jan 01/07
R R
Subtask 12-11-28-860-064 B. Procedure to Convert Data to Equivalent Attitude Monitor Value
R
(1) Use the table below to find the equivalent attitude monitor value:
R
(a) Use the Pitch data to find the equivalent number.
R
(b) Use the Roll data to find the equivalent letter.
R R R R R R R R R R R
(2) Put together the number and the letter to identify the square to use in the MLI procedure.(Ref. TASK 12-11-28-650-806) Pitch 2.5 2.0 1.5 1.0 0.5 0.0 plus 0.5 minus minus minus minus minus
R
**ON A/C 251-252, 701-749,
R
Post SB
R
Subtask 12-11-28-860-064-A
R R
Roll minus 1.5 minus 1.0 minus 0.5 0.0 plus 0.5 plus 1.0 plus 1.5
Ref A B C D E F G
28-3078 For A/C 251-252,701-749,
B. Procedure to Use Pitch and Roll Data When Attitude Monitor is Not Installed
R R R
Ref 1 2 3 4 5 6 7
(1) Use the pitch and roll data to find the fuel quantity given in the tables of the MLI procedure.(Ref. TASK 12-11-28-650-806) **ON A/C ALL 5. Close-up ________ Subtask 12-11-28-860-061 A. On the panel 221VU set the 3 switching selectors of the ADIRS to the OFF position. (1) On the MCDU push the RETURN key until the PARAMETER CALL-UP PAGE shows.
EFF : ALL 12-11-28 SROS
Page B307 Jan 01/07
(2) On the MCDU control panel, push the K key. (3) Set the BRT knob to the OFF position. Subtask 12-11-28-862-053 B. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
EFF : ALL 12-11-28 SROS
Page B308 Jan 01/07
HYDRAULIC FLUIDS - DESCRIPTION AND OPERATION ____________________________________________ 1. _______ General The hydraulic fluid instructions give specification and special instructions. A. Specification of Phosphate Ester-Base Fluids (1) The aircraft hydraulic systems are filled with one of these hydraulic fluids (Type IV). The Material Numbers (Mat No.) are as follows: - 02-003, - 02-003A, - 02-003B, - 02-003C, - 02-003D, - 02-003E.
R R R
(2) All the fluids are to NSA 307110 specification and can be mixed. (3) Fluid characteristics (Ref. Fig. 001) B. Fluid Monitoring (1) Hydraulic fluid with a high degree of cleanliness is required for the correct operation of the hydraulic systems and equipment. (2) Frequent sampling, particle count (physical contamination) and check of filter clogging indicators permit to monitor the hydraulic fluid. (3) If a filter clogging indicator is out, you must: - depressurize the related hydraulic system, - replace the clogged filter, - take a sample of the system hydraulic fluid and send it for analysis. (4) On results of the analysis record (see contamination analysis by particle count of sampling procedure), clean the hydraulic fluid. NOTE : The number of particles contained in 100 cm3 (6.10 in.3) of ____ hydraulic fluid must not be more than the class 9 requirements of the NAS specification 1638 (final or rejection state). NOTE : The degree of cleanliness of the hydraulic fluid used to fill ____ the hydraulic systems and hydraulic cart reservoirs must agree with the Class 7 of the NAS specification 1638 (initial state).
EFF : ALL 12-12-00 SROS
Page 1 Jan 01/05
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Characteristics of Phosphate Ester-Base Hydraulic Fluids Figure 001
EFF : ALL 12-12-00 SROS
Page 2 Jan 01/05
C. Hydraulic Ground Power Cart Only use a hydraulic ground power cart with a hydraulic reservoir. Do a fluid sampling for contamination of the hydraulic fluid and keep the sample analysis record. D. Hydraulic Fluid Property In-Service Limits The hydraulic fluid property in-service limits are: - the physical properties, - the chemical properties. (Ref. Fig. 002) R R
NOTE : The maximum water contents is 0.8 %. We recommend to decrease the ____ limit to 0.5 % which will increase the life of the hydraulic fluid. (1) The quality of the hydraulic fluid must be in the limits given in Fig. 002. If the sample analysis shows that the properties of the hydraulic fluid are out of the in-service limits, you must replace the hydraulic fluid. E. Specification of Mineral-Base Fluids (1) Each aircraft landing-gear shock-absorber is supplied filled with a hydraulic fluid (Mat. No. 02-001) to the MIL-H-5606 specification. (2) Fluid characteristics (Ref. Fig. 003) F. Safety Precautions When you work on the hydraulic systems obey the safety procedures.
EFF : ALL 12-12-00 SROS
Page 3 Jan 01/04
R
Hydraulic Fluid Property In-Service Limits Figure 002
EFF : ALL 12-12-00 SROS
Page 4 Jul 01/03
Characteristics of Mineral Fluids Figure 003 EFF : ALL 12-12-00 SROS
Page 5 Apr 01/98
HYDRAULIC POWER - SERVICING ___________________________ TASK 12-12-29-611-801 Fill the Green Hydraulic Reservoir with a Hydraulic Service Cart WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE _______ CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM. MOVEMENT OF THE FLIGHT CONTROL SURFACES CAN BE DANGEROUS AND/OR CAUSE DAMAGE. R R R
WARNING : DO NOT GET THE FLUID ON YOUR SKIN OR IN YOUR EYES. IF YOU DO: _______ - FLUSH IT AWAY WITH CLEAN WATER - GET MEDICAL AID. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
circuit breaker(s) safety clip(s) Fill Unit-Hyd Fluid access platform 2.5 m (8 ft. 2 in.)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 02-003
R
Material No. 02-003A
R
Material No. 02-003B
F NSA 307110 TYPE 4 HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00) F NSA 307110 TYPE 4 HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00) F NSA 307-110 TYPE 4 HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00)
EFF : ALL 12-12-29 SROS
Page 301 Jan 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 02-003C Material No. 02-003D Material No. 02-003E
F NSA 307-110 TYPE IV HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00) F NSA 307-110 TYPE IV HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 24-41-00-862-801 R R
29-00-00-210-801 29-00-00-864-801
Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Check for Air in the Green/Blue/Yellow Hydraulic System Depressurize the Green Hydraulic System (Pressurized with the Hydraulic Ground Supply)
R 29-10-00-200-802 29-14-00-614-804 29-14-00-614-804 31-60-00-860-801 12-12-29-991-001
Check of the Nitrogen Charging Pressure on Hydraulic Power Accumulator (5151JM1,5151JM2,5151JM3) Pressurization of the Hydraulic Reservoirs with external bench Pressurization of the Hydraulic Reservoirs with the APU EIS Start Procedure Fig. 301
3. __________ Job Set-up Subtask 12-12-29-861-050 A. Energize the aircraft electrical circuits circuits (Ref. TASK 24-41-00-861-801).
EFF : ALL 12-12-29 SROS
Page 302 Jan 01/07
Subtask 12-12-29-010-050 B. Get Access (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Put the access platform in position at the access door 197CB. (4) Open the Green ground service panel 197CB. Subtask 12-12-29-865-050 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU HYD PUMP G CTL 9JV U09 Subtask 12-12-29-865-051 D. Make sure that this(these) circuit breaker(s) is(are) closed: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU HSMU B + PART G 6JG U10 722VU HSMU Y + PART G 7JG X46 742VU HYD RAT EXT SOL 2 5JR D76 Subtask 12-12-29-860-050 E. Aircraft Maintenance Configuration (1) Make sure that the aircraft is in this configuration: - the speed brakes and the spoilers are retracted, - the thrust reversers are stowed, - the landing gear is extended and the landing gear doors are closed, - all the other hydraulic services are in the normal position.
R R R R
(2) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (3) Make sure that the Green hydraulic system accumulator is pressurized (Ref. TASK 29-10-00-200-802).
EFF : ALL 12-12-29 SROS
Page 303 Jan 01/07
R R
(4) Make sure that the reservoir of the Green hydraulic system is pressurized (Ref. TASK 29-14-00-614-804) or (Ref. TASK 29-14-00-614804). 4. Procedure _________ (Ref. Fig. 301/TASK 12-12-29-991-001) Subtask 12-12-29-611-050 A. Fill the hydraulic reservoir
R R R R R R R R R R R R
(1) If you replace one or more components on the high pressure and/or low pressure side or - if there is a hydraulic-fluid low level which causes loss of the system or - if there is a loss of hydraulic fluid equal to or more than 5 liters - make sure that there is no air in the Green hydraulic system (Ref. TASK 29-00-00-210-801). Use Hydraulic fluid HYDRAULIC FLUIDS (Material No. 02-003), or HYDRAULIC FLUIDS (Material No. 02-003A), or HYDRAULIC FLUIDS (Material No. 02-003B), or HYDRAULIC FLUIDS (Material No. 02-003C), or HYDRAULIC FLUIDS (Material No. 02-003D), or HYDRAULIC FLUIDS (Material No. 02-003E).
R
(2) Remove the blanking cap from the reservoir filling self-sealing ground connector 5203JM.
R
(3) Connect a Fill Unit-Hyd Fluid capable of max pressure 20 bar (290 psi) and flow rate 12l/mn to the self-sealing ground connector 5203JM.
R
(4) On the reservoir-filling manual selector-valve 4JS, select the GREEN position.
R
(5) Operate the hydraulic service cart. CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE ON THE GROUND HYDRAULIC _______ CART IS SET TO A MINIMUM OF 7 BARS (101.53 PSI). Operate the hydraulic service cart and monitor the increase of the fluid level on the reservoir hydraulic quantity indicator 5JS.
EFF : ALL 12-12-29 SROS
Page 304 Jan 01/07
Green Ground Service Panel Figure 301/TASK 12-12-29-991-001 EFF : ALL 12-12-29 SROS
Page 305 Apr 01/98
R
(6) Stop the flow when the pointer is in the center position on the reservoir hydraulic quantity indicator 5JS.
R
(7) Turn the reservoir filling manual selector-valve 4JS to the NEUTRAL position (on the reservoir hydraulic quantity indicator 5JS, the pointer is in the INOP position).
R
(8) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00-860-801).
R
(9) On the ECAM control panel on the center pedestal, press the HYD pushbutton. Make sure that the HYD page is shown on the SD.
R
(10) On the SD: - check that the low indication is not in view for the Green hydraulic system - check that the fluid level index is green.
R
(11) Disconnect the ground hydraulic service cart from the reservoir filling self-sealing ground connector 5203JM and install the blanking cap. 5. Close-up ________ Subtask 12-12-29-865-052 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 9JV. Subtask 12-12-29-862-050 B. Put the Aircraft back to its Initial Configuration (1) On the ECAM control panel, set the UPPER DISPLAY and LOWER DISPLAY potentiometers to OFF. (2) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). Subtask 12-12-29-410-050 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access doors 811.
EFF : ALL 12-12-29 SROS
Page 306 Jan 01/07
(3) Close the Green ground service panel 197CB. (4) Remove the access platform(s).
EFF : ALL 12-12-29 SROS
Page 307 Apr 01/98
TASK 12-12-29-611-802 Fill the Green Hydraulic Reservoir with a Hand Pump WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE _______ CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM. MOVEMENT OF THE FLIGHT CONTROL SURFACES CAN BE DANGEROUS AND/OR CAUSE DAMAGE. R R R
WARNING : DO NOT GET THE FLUID ON YOUR SKIN OR IN YOUR EYES. IF YOU DO: _______ - FLUSH IT AWAY WITH CLEAN WATER - GET MEDICAL AID. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
circuit breaker(s) safety clip(s) hydraulic fluid container access platform 2.5 m (8 ft. 2 in.)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 02-003
R
Material No. 02-003A
R
Material No. 02-003B Material No. 02-003C
F NSA 307110 HYDRAULIC FLUID (Ref. 20-31-00) F NSA 307110 HYDRAULIC FLUID (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00)
TYPE 4 (PHOSPHATE ESTER BASE) TYPE 4 (PHOSPHATE ESTER BASE) TYPE 4 (PHOSPHATE ESTER BASE) TYPE IV (PHOSPHATE ESTER BASE)
EFF : ALL 12-12-29 SROS
Page 308 Jan 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 02-003D Material No. 02-003E
F NSA 307-110 TYPE IV HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 24-41-00-862-801 R R
29-00-00-210-801 29-00-00-864-801
Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Check for Air in the Green/Blue/Yellow Hydraulic System Depressurize the Green Hydraulic System (Pressurized with the Hydraulic Ground Supply)
R 29-10-00-200-802 29-14-00-614-804 29-14-00-614-804 31-60-00-860-801 12-12-29-991-001
Check of the Nitrogen Charging Pressure on Hydraulic Power Accumulator (5151JM1,5151JM2,5151JM3) Pressurization of the Hydraulic Reservoirs with external bench Pressurization of the Hydraulic Reservoirs with the APU EIS Start Procedure Fig. 301
3. __________ Job Set-up Subtask 12-12-29-861-051 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801).
EFF : ALL 12-12-29 SROS
Page 309 Jan 01/07
Subtask 12-12-29-010-051 B. Get Access (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Put the access platform in position at the access door 197CB. (4) Open the Green ground service panel 197CB. Subtask 12-12-29-865-053 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU HYD PUMP G CTL 9JV U09 Subtask 12-12-29-865-054 D. Make sure that this(these) circuit breaker(s) is(are) closed: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU HSMU B + PART G 6JG U10 722VU HSMU Y + PART G 7JG X46 742VU HYD RAT EXT SOL 2 5JR D76 Subtask 12-12-29-860-051 E. Aircraft Maintenance Configuration R R R R
(1) Make sure that the aircraft is in this configuration: - the speed brakes and the spoilers are retracted, - the thrust reversers are stowed, - the landing gear is extended and the landing gear doors are closed, - all the other hydraulic services are in the normal position.
R
(2) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (3) Make sure that the Green hydraulic system accumulator is pressurized (Ref. TASK 29-10-00-200-802).
EFF : ALL 12-12-29 SROS
Page 310 Jan 01/07
(4) Make sure that the reservoir of the Green hydraulic system is pressurized (Ref. TASK 29-14-00-614-804) or (Ref. TASK 29-14-00-614804).
R
4. Procedure _________ (Ref. Fig. 301/TASK 12-12-29-991-001) CAUTION : MAKE SURE THAT YOU OPERATE THE HAND PUMP SLOWLY AND SMOOTHLY. THE _______ HANDLE MUST NOT HIT THE STOPS WITH TOO MUCH FORCE. IF YOU DO NOT OBEY THESE PRECAUTIONS, DAMAGE CAN OCCUR TO THE HAND PUMP AND TO THE SERVICING LINE ON THE OTHER SIDE OF THE SERVICING PANEL. Subtask 12-12-29-611-051 A. Fill the Green hydraulic reservoir R R R R R R R R R R R
(1) If you replace one or more components on the high pressure and/or low pressure side or - if there is a hydraulic-fluid low level which causes loss of the system or - if there is a loss of hydraulic fluid equal to or more than 5 liters - make sure that there is no air in the Green hydraulic system (Ref. TASK 29-00-00-210-801).
R
(2) Remove the hand pump lever 5205JM.
R
(3) Connect the hand pump lever 5205JM to the shaft of the reservoir filling hand pump 5204JM.
R
(4) Remove the reservoir filling hose 5213JM.
R
(5) Remove the blanking cap and connect the filling hose 5213JM to the filling valve 5211JM.
R
(6) Put the other end of the filling hose in the hydraulic fluid container filled with HYDRAULIC FLUIDS (Material No. 02-003), or HYDRAULIC FLUIDS (Material No. 02-003A), or HYDRAULIC FLUIDS (Material No. 02-003B), or HYDRAULIC FLUIDS (Material No. 02-003C), or HYDRAULIC FLUIDS (Material No. 02-003D). HYDRAULIC FLUIDS (Material No. 02-003E)
R
(7) On the reservoir-filling manual selector-valve 4JS, select the GREEN position.
R
(8) Operate the hand pump lever and monitor the increase of the fluid level on the reservoir hydraulic quantity indicator 5JS.
EFF : ALL 12-12-29 SROS
Page 311 Jan 01/07
R
(9) Stop the flow when the pointer is in the center position on the reservoir hydraulic quantity indicator 5JS.
R
(10) Turn the reservoir-filling manual selector-valve 4JS to the NEUTRAL position. (On the reservoir hydraulic quantity indicator 5JS, the pointer is in the INOP position).
R
(11) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00-860-801).
R
(12) On the ECAM control panel on the center pedestal, press the HYD pushbutton. Make sure that the HYD page is shown on SD.
R
(13) On the SD: - check that the low indication is not in view for the Green hydraulic system - check that the fluid level index is green.
R
(14) Remove the filling hose 5213JM and install the blanking cap on the hand pump.
R
(15) Put the filling hose back in position on its mounting.
R
(16) Remove the hand pump lever 5205JM from the hand pump 5204JM and put it in position on the Green ground service panel. 5. Close-up ________ Subtask 12-12-29-865-055 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 9JV. Subtask 12-12-29-862-051 B. Put the Aircraft back to its Initial Configuration (1) On the ECAM control panel, set the UPPER DISPLAY and LOWER DISPLAY potentiometers to OFF. (2) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
EFF : ALL 12-12-29 SROS
Page 312 Jan 01/07
Subtask 12-12-29-410-051 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access doors 811. (3) Close the Green ground service panel 197CB. (4) Remove the access platform(s).
EFF : ALL 12-12-29 SROS
Page 313 Apr 01/98
TASK 12-12-29-611-803 Fill the Blue Hydraulic Reservoir with a Hydraulic Service Cart WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE _______ CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM. MOVEMENT OF THE FLIGHT CONTROL SURFACES CAN BE DANGEROUS AND/OR CAUSE DAMAGE. R R R
WARNING : DO NOT GET THE FLUID ON YOUR SKIN OR IN YOUR EYES. IF YOU DO: _______ - FLUSH IT AWAY WITH CLEAN WATER - GET MEDICAL AID. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No
specific specific specific specific
circuit breaker(s) safety clip(s) Fill Unit-Hyd Fluid access platform 1.8 m (5 ft. 11 in.) access platform 2.5 m (8 ft. 2 in.)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 02-003
R
Material No. 02-003A
R
Material No. 02-003B Material No. 02-003C
F NSA 307110 HYDRAULIC FLUID (Ref. 20-31-00) F NSA 307110 HYDRAULIC FLUID (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00)
TYPE 4 (PHOSPHATE ESTER BASE) TYPE 4 (PHOSPHATE ESTER BASE) TYPE 4 (PHOSPHATE ESTER BASE) TYPE IV (PHOSPHATE ESTER BASE)
EFF : ALL 12-12-29 SROS
Page 314 Jan 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 02-003D
R R
Material No. 02-003E
F NSA 307-110 TYPE IV HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 24-41-00-862-801 29-00-00-863-802 29-00-00-870-805 29-14-00-614-804 29-14-00-614-804 31-60-00-860-801 12-12-29-991-001
Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Pressurize the Blue Hydraulic System with the Electric Pump Bleeding of the Blue Hydraulic System Pressurization of the Hydraulic Reservoirs with external bench Pressurization of the Hydraulic Reservoirs with the APU EIS Start Procedure Fig. 301
3. __________ Job Set-up Subtask 12-12-29-861-052 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). Subtask 12-12-29-010-052 B. Get Access (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Put the access platform in position at the access door 197CB.
EFF : ALL 12-12-29 SROS
Page 315 Jan 01/05
(4) Open the Green ground service panel 197CB. (5) Put the access platform in position at the access door 195BB. (6) Open the Blue ground service panel 195BB. Subtask 12-12-29-865-057 C. Make sure that this(these) circuit breaker(s) is(are) closed: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU HSMU B + PART G 6JG U10 721VU HYD PUMP B CTL 9JC X12 722VU HSMU Y + PART G 7JG X46 Subtask 12-12-29-860-052 D. Aircraft Maintenance Configuration (1) Make sure that the aircraft is in this configuration: - the speed brakes and the spoilers are retracted - the thrust reversers are stowed - the landing gear is extended and the landing gear doors are closed - all the other hydraulic services are in the normal position.
R
(2) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00-860-801). (3) On the ECAM control panel on the center pedestal, press the HYD pushbutton. Make sure that the HYD page is shown on SD. On the SD: Make sure that the Blue hydraulic reservoir do not give LO AIR PRESS indication.
R R R
(4) If necessary, pressurize the Blue hydraulic reservoir (Ref. TASK 2914-00-614-804) or (Ref. TASK 29-14-00-614-804). (5) On the Blue ground service panel, make sure that the pressure of the accumulators are correct according the marking on the ground service panel: - On the pressure gage (5152JS) of the Blue power accumulator. - On the pressure gage (5426GG and 5427GG) of the Blue brake accumulators.
R R
EFF : ALL 12-12-29 SROS
Page 316 Jul 01/06
(6) On the panel 117VU, set the PARK BRAKE selector switch (3GZ) on the ON position (7) Fill the brake accumulator. R R R
NOTE : The nominal fill level of the Blue hydraulic reservoir is ____ obtained with the brake accumulators filled with fluid at 3000 psi (206.8427 bar) (the brake accumulator capacity is approximately 6 liters). (8) On the overhead panel 245VU, push the HYD/BLUE/ELEC pushbutton switch: - the ON legend of this pushbutton switch comes on - the electrical pump of the Blue hydraulic system starts. - the Blue hydraulic system accumulator is filled. (9) On the center instrument panel 312VU: Make sure that the Blue brake-pressure indicator (2GK) show the ACCU PRESS at 3000 psi (206.8427 bar). If necessary pressurize the brake accumulator with Blue pump (Ref. TASK 29-00-00-863-802). (10) On the overhead panel 245VU, release the HYD/BLUE/ELEC pushbutton switch: - the ON legend of this pushbutton switch goes off - the electrical pump of the Blue hydraulic system stop. (11) Pressurize the Hydraulic reservoir during 1 minute to make sure that the nominal pressure is reached (Ref. TASK 29-14-00-614-804). Subtask 12-12-29-865-056 E. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU HYD PUMP B CTL 9JC X12
EFF : ALL 12-12-29 SROS
Page 317 Jan 01/07
4. Procedure _________ (Ref. Fig. 301/TASK 12-12-29-991-001) Subtask 12-12-29-611-052 A. Fill the hydraulic reservoir. NOTE : If you replace one or more components on the high pressure and/or ____ low pressure side, - If there is a hydraulic-fluid low level which causes loss of the system - If there is a large loss of hydraulic fluid - Do the related bleed procedure to make sure that the quantity of fluid in the system is correct:(Ref. TASK 29-00-00-870-805) Use Hydraulic fluid HYDRAULIC FLUIDS (Material No. 02-003), or HYDRAULIC FLUIDS (Material No. 02-003A), or HYDRAULIC FLUIDS (Material No. 02-003B), or HYDRAULIC FLUIDS (Material No. 02003C), or HYDRAULIC FLUIDS (Material No. 02-003D). HYDRAULIC FLUIDS (Material No. 02-003E)
R R R R R
(1) Remove the blanking cap from the reservoir filling self-sealing ground connector 5203JM. (2) Connect a Fill Unit-Hyd Fluid capable of max pressure 20 bar (290psi) and flow rate 12l/mn to the self-sealing ground connector 5203JM. (3) On the reservoir-filling manual selector-valve 4JS, select the BLUE position. (4) Operate the hydraulic service cart. CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE ON THE GROUND HYDRAULIC _______ CART IS SET TO A MINIMUM OF 7 BARS (101.53 PSI). Operate the hydraulic service cart and monitor the increase of the fluid level on the reservoir hydraulic quantity indicator 5JS. (5) Stop the flow when the pointer is in the center position on the reservoir hydraulic quantity indicator 5JS. (6) Turn the reservoir filling manual selector-valve 4JS to the NEUTRAL position (on the reservoir hydraulic quantity indicator 5JS, the pointer is in the INOP position).
EFF : ALL 12-12-29 SROS
Page 318 Jan 01/05
(7) On the ECAM control panel on the center pedestal, make sure that the HYD page is shown On the SD: - check that the low indication is not in view for the Blue hydraulic system - check that the fluid level index is green. (8) Disconnect the ground hydraulic service cart from the reservoir filling self-sealing ground connector 5203JM and install the blanking cap. 5. Close-up ________ Subtask 12-12-29-865-058 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 9JC. Subtask 12-12-29-862-052 B. Put the Aircraft back to its Initial Configuration (1) Get Access (2) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). (3) On the panel 117VU set the Park Brake selector switch (3GZ) on the OFF position. Subtask 12-12-29-410-052 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access doors 811. (3) Close the Green ground service panel 197CB. (4) Close the Blue ground service panel 195BB. (5) Remove the access platform(s).
EFF : ALL 12-12-29 R SROS
Page 319 Jan 01/05
TASK 12-12-29-611-804 Fill the Blue Hydraulic Reservoir with a Hand Pump WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE _______ CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM. MOVEMENT OF THE FLIGHT CONTROL SURFACES CAN BE DANGEROUS AND/OR CAUSE DAMAGE. R R R
WARNING : DO NOT GET THE FLUID ON YOUR SKIN OR IN YOUR EYES. IF YOU DO: _______ - FLUSH IT AWAY WITH CLEAN WATER - GET MEDICAL AID. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No
specific specific specific specific
circuit breaker(s) safety clip(s) hydraulic fluid container access platform 1.8 m (5 ft. 11 in.) access platform 2.5 m (8 ft. 2 in.)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 02-003
R
Material No. 02-003A
R
Material No. 02-003B Material No. 02-003C
F NSA 307110 HYDRAULIC FLUID (Ref. 20-31-00) F NSA 307110 HYDRAULIC FLUID (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00)
TYPE 4 (PHOSPHATE ESTER BASE) TYPE 4 (PHOSPHATE ESTER BASE) TYPE 4 (PHOSPHATE ESTER BASE) TYPE IV (PHOSPHATE ESTER BASE)
EFF : ALL 12-12-29 SROS
Page 320 Jan 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 02-003D
R R
Material No. 02-003E
F NSA 307-110 TYPE IV HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 24-41-00-862-801 29-00-00-863-802 29-00-00-870-805 29-14-00-614-804 29-14-00-614-804 31-60-00-860-801 12-12-29-991-001
Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Pressurize the Blue Hydraulic System with the Electric Pump Bleeding of the Blue Hydraulic System Pressurization of the Hydraulic Reservoirs with external bench Pressurization of the Hydraulic Reservoirs with the APU EIS Start Procedure Fig. 301
3. __________ Job Set-up Subtask 12-12-29-861-053 A. Energize the aircraft electrical circuits circuits (Ref. TASK 24-41-00-861-801). Subtask 12-12-29-010-053 B. Get Access (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Put the access platform in position at the access door 197CB.
EFF : ALL 12-12-29 SROS
Page 321 Jan 01/05
(4) Open the Green ground service panel 197CB. (5) Put the access platform in position at the access door 195BB. (6) Open the Blue ground service panel 195BB. Subtask 12-12-29-865-060 C. Make sure that this(these) circuit breaker(s) is(are) closed: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU HSMU B + PART G 6JG U10 721VU HYD PUMP B CTL 9JC X12 722VU HSMU Y + PART G 7JG X46 Subtask 12-12-29-860-053 D. Aircraft Maintenance Configuration (1) Make sure that the aircraft is in this configuration: - the speed brakes and the spoilers are retracted - the thrust reversers are stowed - the landing gear is extended and the landing gear doors are closed - all the other hydraulic services are in the normal position (2) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00-860-801). (3) On the ECAM control panel on the center pedestal, press the HYD pushbutton. make sure that the HYD page is shown on SD. On the SD: Make sure that the Blue hydraulic reservoir do not give LO AIR PRESS indication. (4) If necessary, pressurize the Blue hydraulic reservoir. (Ref. TASK 2914-00-614-804) or (Ref. TASK 29-14-00-614-804) (5) On the Blue ground service panel, make accumulators are correct according the panel : - On the pressure gage (5152JS) of the - On the two pressure gage (5426GG and accumulators
sure that the pressure of the marking on the ground service Blue power accumulator 5427GG) of the Blue brake
EFF : ALL 12-12-29 R SROS
Page 322 Jan 01/05
(6) On the panel 117VU, set the PARK BRAKE selector switch (3GZ) on the ON position. (7) Fill the brake accumulators 5426GG and 5427GG with the electrical pump of the Blue hydraulic system : NOTE : The capacity of each brake accumulator is approximately 6 ____ liters filled with hydraulic fluid at 3000 psi (206.8427 bar). (a) On the overhead panel 245VU, push the HYD/BLUE/ELEC pushbutton switch: - The ON legend of this pushbutton switch comes on, - The electrical pump of the Blue hydraulic system starts, (b) On the center instrument panel 312VU, make sure that the Blue brake -pressure indicator (2GK) show the ACCU PRESS at 3000 psi (206.8427 bar). If necessary pressurize the brake accumulator with Blue pump.(Ref. TASK 29-00-00-863-802) (c) On the overhead panel 245VU, release the HYD/BLUE/ELEC pushbutton switch: - The ON legend of this pushbutton switch goes off, - The electrical pump of the Blue hydraulic system stop. (8) Pressurize the Blue hydraulic reservoir during 1 minute to make sure that the nominal pressure is reached (Ref. TASK 29-14-00-614-804) NOTE : The nominal fill level of the Blue hydraulic reservoir is ____ obtain with the brake accumulators filled with fluid at 3000 psi (206.8427 bar). Subtask 12-12-29-865-059 E. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU HYD PUMP B CTL 9JC X12
EFF : ALL 12-12-29 R SROS
Page 323 Jan 01/05
4. Procedure _________ (Ref. Fig. 301/TASK 12-12-29-991-001) CAUTION : MAKE SURE THAT YOU OPERATE THE HAND PUMP SLOWLY AND SMOOTHLY. THE _______ HANDLE MUST NOT HIT THE STOPS WITH TOO MUCH FORCE. IF YOU DO NOT OBEY THESE PRECAUTIONS, DAMAGE CAN OCCUR TO THE HAND PUMP AND TO THE SERVICING LINE ON THE OTHER SIDE OF THE SERVICING PANEL. Subtask 12-12-29-611-053 A. Fill the Blue hydraulic reservoir NOTE : If you replace one or more components on the high pressure and/or ____ low pressure side, - If there is a hydraulic-fluid low level which causes loss of the system, - If there is a large loss of hydraulic fluid - Do the related bleed procedure to make sure that the quantity of fluid in the system is correct:(Ref. TASK 29-00-00-870-805) (1) Remove the hand pump lever 5205JM. (2) Connect the hand pump lever 5205JM to the shaft of the reservoir filling hand pump 5204JM. (3) Remove the reservoir filling hose 5213JM. (4) Remove the blanking cap and connect the filling hose 5213JM to the filling valve 5211JM. (5) Put the other end of the filling hose in the hydraulic fluid container filled with HYDRAULIC FLUIDS (Material No. 02-003), or HYDRAULIC FLUIDS (Material No. 02-003A), or HYDRAULIC FLUIDS (Material No. 02-003B), or HYDRAULIC FLUIDS (Material No. 02-003C), or HYDRAULIC FLUIDS (Material No. 02-003D) HYDRAULIC FLUIDS (Material No. 02-003E)
R R R R
(6) On the reservoir-filling manual selector-valve 4JS, select the BLUE position. (7) Operate the hand pump lever and monitor the increase of the fluid level on the reservoir hydraulic quantity indicator 5JS. (8) Stop the flow when the pointer is in the center position on the reservoir hydraulic quantity indicator 5JS.
EFF : ALL 12-12-29 SROS
Page 324 Jan 01/05
(9) Turn the reservoir-filling manual selector-valve 4JS to the NEUTRAL position. (On the reservoir hydraulic quantity indicator 5JS, the pointer is in the INOP position). (10) On the ECAM control panel on the center pedestal, make sure that the HYD page is shown on SD. (11) On the SD: - check that the low indication is not in view for the Blue hydraulic system - check that the fluid level index is green. (12) Remove the filling hose 5213JM and install the blanking cap on the hand pump. (13) Put the filling hose back in position on its mounting. (14) Remove the hand pump lever 5205JM from the hand pump 5204JM and put it in position on the Green ground service panel. 5. Close-up ________ Subtask 12-12-29-865-061 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 9JC. Subtask 12-12-29-862-053 B. Put the Aircraft back to its Initial Configuration (1) On the ECAM control panel, set the UPPER DISPLAY and LOWER DISPLAY potentiometers to OFF. (2) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). Subtask 12-12-29-410-053 C. Close Access ON the panel 117VU, set the PARK BRAKE selector switch (3GZ) on the OFF position. (1) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 12-12-29 R SROS
Page 325 Jan 01/05
(2) Close the access doors 811. (3) Close the Green ground service panel 197CB. (4) Close the Blue ground service panel 195BB. (5) Remove the access platform(s).
EFF : ALL 12-12-29 R SROS
Page 326 Jan 01/05
TASK 12-12-29-611-805 Fill the Yellow Hydraulic Reservoir with a Hydraulic Service Cart WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE _______ CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM. MOVEMENT OF THE FLIGHT CONTROL SURFACES CAN BE DANGEROUS AND/OR CAUSE DAMAGE. R R R
WARNING : DO NOT GET THE FLUID ON YOUR SKIN OR IN YOUR EYES. IF YOU DO: _______ - FLUSH IT AWAY WITH CLEAN WATER - GET MEDICAL AID. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
circuit breaker(s) safety clip(s) Fill-Unit Hyd Fluid access platform 2.5 m (8 ft. 2 in.)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 02-003
R
Material No. 02-003A
R
Material No. 02-003B Material No. 02-003C
F NSA 307110 HYDRAULIC FLUID (Ref. 20-31-00) F NSA 307110 HYDRAULIC FLUID (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00)
TYPE 4 (PHOSPHATE ESTER BASE) TYPE 4 (PHOSPHATE ESTER BASE) TYPE 4 (PHOSPHATE ESTER BASE) TYPE IV (PHOSPHATE ESTER BASE)
EFF : ALL 12-12-29 SROS
Page 327 Jan 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 02-003D
R R
Material No. 02-003E
F NSA 307-110 TYPE IV HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 24-41-00-862-801 29-00-00-864-803 29-00-00-870-806 29-10-00-200-802 29-14-00-614-804 29-14-00-614-804 31-60-00-860-801 12-12-29-991-001
Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Depressurize the Yellow Hydraulic System (Pressurized with the Hydraulic Ground Supply) Bleeding of the Yellow Hydraulic System Check of the Nitrogen Charging Pressure on Hydraulic Power Accumulator (5151JM1,5151JM2,5151JM3) Pressurization of the Hydraulic Reservoirs with external bench Pressurization of the Hydraulic Reservoirs with the APU EIS Start Procedure Fig. 301
3. __________ Job Set-up Subtask 12-12-29-861-054 A. Energize the aircraft electrical circuits circuits (Ref. TASK 24-41-00-861-801). Subtask 12-12-29-010-054 B. Get Access (1) Put the access platform in position at the access door 811. (2) Open the access door 811.
EFF : ALL 12-12-29 SROS
Page 328 Jan 01/05
R
(3) Put the access platform in position at the access door 197CB. (4) Open the Green ground service panel 197CB. Subtask 12-12-29-865-062 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------722VU HYD PUMP Y SVCE 10JJ N46 722VU HYD PUMP Y CTL 9JJ R36 Subtask 12-12-29-865-063 D. Make sure that this(these) circuit breaker(s) is(are) closed: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------722VU HSMU Y + PART G 7JG X46 Subtask 12-12-29-860-054 E. Aircraft Maintenance Configuration (1) Make sure that the aircraft is in this configuration: - the speed brakes and the spoilers are retracted - the thrust reversers are stowed - the landing gear is extended and the landing gear doors are closed - all the other hydraulic services are in the normal position - the FWD and AFT cargo-compartment doors 821, 822 are closed. (2) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803). (3) Make sure that the Yellow hydraulic system accumulator is pressurized (Ref. TASK 29-10-00-200-802). (4) Make sure that the reservoir of the Yellow hydraulic system is pressurized (Ref. TASK 29-14-00-614-804) or (Ref. TASK 29-14-00-614804)
EFF : ALL 12-12-29 SROS
Page 329 Jul 01/06
4. Procedure _________ (Ref. Fig. 301/TASK 12-12-29-991-001) Subtask 12-12-29-611-054 A. Fill the hydraulic reservoir. NOTE : If you replace one or more components on the high pressure and/or ____ low pressure side, - If there is a hydraulic-fluid low level which causes loss of the system, - If there is a large loss of hydraulic fluid, - Do the related bleed procedure to make sure that the quantity of hydraulic fluid in the system is correct (Ref. TASK 29-00-00870-806): Use hydraulic fluid HYDRAULIC FLUIDS (Material No. 02-003), or HYDRAULIC FLUIDS (Material No. 02-003A), or HYDRAULIC FLUIDS (Material No. 02-003B), or HYDRAULIC FLUIDS (Material No. 02003C), or HYDRAULIC FLUIDS (Material No. 02-003D). HYDRAULIC FLUIDS (Material No. 02-003E)
R R R R R
(1) Remove the blanking cap from the reservoir filling self-sealing ground connector (5203JM). (2) Connect a Fill-Unit Hyd Fluid with a capacity of 20 bar (290 psi) maximum and flow rate 12 l/mn to the self-sealing ground connector (5203JM). (3) On the reservoir filling manual selector valve (4JS), select the YELLOW position. (4) Operate the hydraulic service cart. CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE ON THE GROUND HYDRAULIC _______ CART IS SET TO A MINIMUM OF 7 BARS (101.53 PSI). Operate the hydraulic service cart and monitor the increase of the fluid level on the reservoir hydraulic quantity indicator (5JS). (5) Stop the flow when the pointer is in the position 0 on the reservoir hydraulic quantity indicator (5JS). (6) Turn the reservoir filling manual selector valve (4JS) to the NEUTRAL position (on the reservoir hydraulic quantity indicator (5JS), the pointer is in the INOP position).
EFF : ALL 12-12-29 SROS
Page 330 Jan 01/05
(7) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00-860-801). (8) On the ECAM control panel on the center pedestal: - push the HYD pushbutton (on the SD, the HYD page comes into view). (9) On the SD: - make sure that the low indication is not in view for the yellow hydraulic system - make sure that the fluid level index is green. (10) Disconnect the ground hydraulic service cart from the reservoir filling self-sealing ground connector (5203JM) and install the blanking cap. 5. Close-up ________ Subtask 12-12-29-865-064 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 9JJ, 10JJ. Subtask 12-12-29-862-054 B. Put the Aircraft back to its Initial Configuration (1) On the ECAM control panel, set the UPPER DISPLAY and LOWER DISPLAY potentiometers to OFF. (2) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). Subtask 12-12-29-410-054 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access doors 811. (3) Close the Green ground service panel 197CB. (4) Remove the access platform(s).
EFF : ALL 12-12-29 R SROS
Page 331 Jan 01/05
TASK 12-12-29-611-806 Fill the Yellow Hydraulic Reservoir with a Hand Pump WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE _______ CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM. MOVEMENT OF THE FLIGHT CONTROL SURFACES CAN BE DANGEROUS AND/OR CAUSE DAMAGE. R R R
WARNING : DO NOT GET THE FLUID ON YOUR SKIN OR IN YOUR EYES. IF YOU DO: _______ - FLUSH IT AWAY WITH CLEAN WATER - GET MEDICAL AID. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
circuit breaker(s) safety clip(s) hydraulic fluid container access platform 2.5 m (8 ft. 2 in.)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 02-003
R
Material No. 02-003A
R
Material No. 02-003B Material No. 02-003C
F NSA 307110 HYDRAULIC FLUID (Ref. 20-31-00) F NSA 307110 HYDRAULIC FLUID (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00)
TYPE 4 (PHOSPHATE ESTER BASE) TYPE 4 (PHOSPHATE ESTER BASE) TYPE 4 (PHOSPHATE ESTER BASE) TYPE IV (PHOSPHATE ESTER BASE)
EFF : ALL 12-12-29 SROS
Page 332 Jan 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 02-003D
R R
Material No. 02-003E
F NSA 307-110 TYPE IV HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 24-41-00-862-801 29-00-00-864-803 29-00-00-870-806 29-10-00-200-802 29-14-00-614-804 29-14-00-614-804 31-60-00-860-801 12-12-29-991-001
Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Depressurize the Yellow Hydraulic System (Pressurized with the Hydraulic Ground Supply) Bleeding of the Yellow Hydraulic System Check of the Nitrogen Charging Pressure on Hydraulic Power Accumulator (5151JM1,5151JM2,5151JM3) Pressurization of the Hydraulic Reservoirs with external bench Pressurization of the Hydraulic Reservoirs with the APU EIS Start Procedure Fig. 301
3. __________ Job Set-up Subtask 12-12-29-861-055 A. Energize the aircraft electrical circuits circuits (Ref. TASK 24-41-00-861-801). Subtask 12-12-29-010-055 B. Get Access (1) Put the access platform in position at the access door 811. (2) Open the access door 811.
EFF : ALL 12-12-29 SROS
Page 333 Jan 01/05
(3) Put the access platform in position at the access door 197CB. (4) Open the Green ground service panel 197CB. Subtask 12-12-29-865-065 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------722VU HYD PUMP Y SVCE 10JJ N46 722VU HYD PUMP Y CTL 9JJ R36 Subtask 12-12-29-865-066 D. Make sure that this(these) circuit breaker(s) is(are) closed: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU HSMU B + PART G 6JG U10 722VU HSMU Y + PART G 7JG X46 Subtask 12-12-29-860-055 E. Aircraft Maintenance Configuration (1) Make sure that the aircraft is in this configuration: - the speed brakes and the spoilers are retracted - the thrust reversers are stowed - the landing gear is extended and the landing gear doors are closed - all the other hydraulic services are in the normal position - the FWD and AFT cargo compartment doors 821, 822 are closed. (2) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803) (3) Make sure that the Yellow hydraulic system accumulator is pressurized (Ref. TASK 29-10-00-200-802). (4) Make sure that the reservoir of the Yellow hydraulic system is pressurized (Ref. TASK 29-14-00-614-804) or (Ref. TASK 29-14-00-614804)
EFF : ALL 12-12-29 R SROS
Page 334 Jan 01/05
4. Procedure _________ (Ref. Fig. 301/TASK 12-12-29-991-001) CAUTION : MAKE SURE THAT YOU OPERATE THE HAND PUMP SLOWLY AND SMOOTHLY. THE _______ HANDLE MUST NOT HIT THE STOPS WITH TOO MUCH FORCE. IF YOU DO NOT OBEY THESE PRECAUTIONS, DAMAGE CAN OCCUR TO THE HAND PUMP AND TO THE SERVICING LINE ON THE OTHER SIDE OF THE SERVICING PANEL. Subtask 12-12-29-611-055 A. Fill the Yellow hydraulic reservoir NOTE : If you replace one or more components on the high pressure and/or ____ low pressure side, - If there is a hydraulic-fluid low level which causes loss of the system, - If there is a large loss of hydraulic fluid, - Do the related bleed procedure to make sure that the quantity of hydraulic fluid in the system is correct:(Ref. TASK 29-00-00870-806) (1) Remove the hand pump lever 5205JM. (2) Connect the hand pump lever 5205JM to the shaft of the reservoir filling hand pump 5204JM. (3) Remove the reservoir filling hose 5213JM. (4) Remove the blanking cap and connect the filling hose 5213JM to the filling valve 5211JM. (5) Put the other end of the filling hose in the hydraulic fluid container filled with HYDRAULIC FLUIDS (Material No. 02-003), or HYDRAULIC FLUIDS (Material No. 02-003A), or HYDRAULIC FLUIDS (Material No. 02-003B), or HYDRAULIC FLUIDS (Material No. 02-003C), or HYDRAULIC FLUIDS (Material No. 02-003D). HYDRAULIC FLUIDS (Material No. 02-003E)
R R R R
(6) On the reservoir-filling manual selector-valve 4JS, select the YELLOW position. (7) Operate the hand pump lever and monitor the increase of the fluid level on the reservoir hydraulic quantity indicator 5JS. (8) Stop the flow when the pointer is in the center position on the reservoir hydraulic quantity indicator 5JS.
EFF : ALL 12-12-29 SROS
Page 335 Jan 01/05
(9) Turn the reservoir-filling manual selector-valve 4JS to the NEUTRAL position. (On the reservoir hydraulic quantity indicator 5JS, the pointer is in the INOP position). (10) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00-860-801). (11) On the ECAM control panel on the center pedestal, press the HYD pushbutton. Make sure that the HYD page is shown on SD. (12) On the SD: - check that the low indication is not in view for the Yellow hydraulic system - check that the fluid level index is green. (13) Remove the filling hose 5213JM and install the blanking cap on the hand pump. (14) Put the filling hose back in position on its mounting. (15) Remove the hand pump lever 5205JM from the hand pump 5204JM and put it in position on the Green ground service panel. 5. Close-up ________ Subtask 12-12-29-865-067 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 9JJ, 10JJ. Subtask 12-12-29-862-055 B. Put the Aircraft back to its Initial Configuration (1) On the ECAM control panel, set the UPPER DISPLAY and LOWER DISPLAY potentiometers to OFF. (2) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
EFF : ALL 12-12-29 R SROS
Page 336 Jan 01/05
Subtask 12-12-29-410-055 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access doors 811. (3) Close the Green ground service panel 197CB. (4) Remove the access platform(s).
EFF : ALL 12-12-29 SROS
Page 337 Jan 01/05
LANDING GEAR - SERVICING ________________________ TASK 12-12-32-611-801 Hydraulic Replenishment of the MLG Shock Absorber (Aircraft on Jacks) WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED ON THE _______ LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
approved nitrogen supply container hose
R No specific No specific No specific No specific No specific No specific 460007156 98F32104021001
pressure gage 0 - 60 bar thermometer transparent bleed tube warning notice 3-way valve access platform 3.5 m (11 ft. 6 in.) 1 ADAPTER, CHARGING - MLG 1 COMPRESSION TOOL
EFF : ALL 12-12-32 SROS
Page 301 Jul 01/06
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------No specific Material No. 02-001
lockwire, corrosion-resistant steel 0.8 mm (0.032 in) dia. USA MIL-H-5606 OIL, HYDRAULICPETROLEUM FLUID (Ref. 20-31-00)
Material No. 02-004 R R
Material No. 02-006 Material No. 05-004B Material No. 19-010
SHOCK ABSORBER FLUID (Ref. 20-31-00) USA BMS 3-32 TYPE II SHOCK ABSORBER FLUID (Ref. 20-31-00) USA MIL-L-25567 TYPE I OXYGEN LEAK DETECTOR (Ref. 20-31-00) USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------07-11-00-581-801 07-11-00-586-801 29-00-00-864-804 32-00-00-481-801 R
32-11-13-960-801 32-11-15-000-802 32-11-15-400-802 12-12-32-991-002 12-12-32-991-010 12-12-32-991-001 12-12-32-991-016 12-12-32-991-007-A
Lifting of the Aircraft for Maintenance Operations Lowering of the Aircraft for Maintenance Operations Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Installation of the Safety Devices on the Landing Gears Replacement of the MLG Shock Absorber Seals Removal of the MLG Bogie-Alignment Pitch Trimmer (Aircraft on Jacks) Installation of the MLG Bogie-Alignment Pitch Trimmer (Aircraft on Jacks) Fig. 301 Fig. 302 Fig. 303 Fig. 304 Fig. 305
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3. __________ Job Set-up Subtask 12-12-32-941-050 A. Safety Precautions (1) Put the warning notice in the cockpit, to tell persons not to operate the landing gear controls. Subtask 12-12-32-860-050 B. Aircraft Maintenance Configuration (1) Make sure that the Green hydraulic system is depressurized (Ref. TASK 29-00-00-864-804). (2) Make sure that the safety devices are installed on the L/G (Ref. TASK 32-00-00-481-801). Subtask 12-12-32-582-050 C. Lift the Aircraft (1) Lift the aircraft on jacks (Ref. TASK 07-11-00-581-801). (2) Make sure that the wheels of the applicable MLG are clear of the ground (3) Make sure that the applicable MLG shock absorber has fully extended. Subtask 12-12-32-010-050 D. Get Access (1) Put the access platform in position at the applicable zone: - for the LH MLG shock absorber at zone 731 - for the RH MLG shock absorber at zone 741. (2) Remove and discard the lockwire from the bolts (6) (Ref. Fig. 301/TASK 12-12-32-991-002) (3) Remove the bolts (6), the washers (5), the bracket (4) and the panel (3).
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MLG Shock Absorber - Inflation/Bleed Valves Figure 301/TASK 12-12-32-991-002
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Page 304 Jul 01/06
Subtask 12-12-32-480-057 E. Installation of the Compression Tool on the Applicable Gear (COMPRESSION TOOL (98F32104021001)) (Ref. Fig. 302/TASK 12-12-32-991-010) (1) Install the oleo control unit: (a) Install the housing (25) in the right side of the upper torque link bore. (b) Install the spindle (43) in the left side of the upper torque link until it engages the housing (25). (c) Fully install and tighten the bolt (23). NOTE : The housing (25) and spindle (43) must be free to turn in ____ the bore. (d) Install the housing (30) in the right side of the lower torque link bore. (e) Install the spindle (38) in the left side of the lower torque link until it engages the housing (30). (f) Fully install and tighten the bolt (28). NOTE : The housing (30) and spindle (38) must be free to turn in ____ the bore. (2) Installation of the bogie control unit: (a) Make sure that the bogie control cylinder (36) is installed on the yoke (35). (b) Install the adaptor (57) on the bogie beam with the washer (62), the bolt (54), the nut (59) and the locking pin (58). (c) Put the yoke (35) (together with the assembled parts) in position on the spindle (38) and the housing (30). (d) Install the clamps (31) with the bolts (32). (e) Install the cylinder clevis (61) on the rod (63). (f) Connect the hydraulic coupling (64) to the bogie control cylinder (36).
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Compression Tool - Installation and Operation Figure 302/TASK 12-12-32-991-010- 14 (SHEET 1)
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Compression Tool - Installation and Operation Figure 302/TASK 12-12-32-991-010- 24 (SHEET 2)
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Compression Tool - Installation and Operation Figure 302/TASK 12-12-32-991-010- 34 (SHEET 3)
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Compression Tool - Installation and Operation Figure 302/TASK 12-12-32-991-010- 44 (SHEET 4)
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Page 309 Jan 01/04
(g) On the compression-tool hydraulic control-panel, open the bogie beam vent valve. (h) Manually extend the rod (63) until the cylinder clevis (61) aligns with the adaptor (57). (i) Install the pin (60), the washer (55) and the locking pin (56). (3) Install the oleo control cylinders: (a) Attach the cylinder (21) to the housing (25) with the retainer nut (26). (b) Attach the other cylinder (21) to the spindle (43) with the retainer nut (42). NOTE : Make sure that the hydraulic ports (22) point aft. ____ (c) Install the clevis (27) and the clevis (41) on the applicable cylinder rod (24). (d) On the compression tool hydraulic control panel, - set the oleo descent valve to OPEN. - set the oleo directional control valve to DOWN. (e) Operate the hand pump to extend the cylinder rods (24) until: - the clevis (27) aligns with the clevis on the housing (30) - the clevis (41) aligns with the clevis on the spindle (38). (f) Install the pins (29) and (37), the washers (33) and (39) and the lock pins (34) and (40). Subtask 12-12-32-614-050 R
F. Preparation (Ref. Fig. 303/TASK 12-12-32-991-001) (1) Install the ADAPTER, CHARGING - MLG on the bleed/inflation valve (1). (2) Connect the hose between the ADAPTER, CHARGING - MLG and the 3-way valve. (3) Connect a transparent bleed tube between the 3-way valve and the container. Make sure that the free end of the bleed tube is a minimum of 400 mm (16 in.) below the bleed/inflation valve (1). (4) Connect the approved nitrogen supply to the 3-way valve.
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MLG Shock Absorber Charge - Charge and Inflation Details Figure 303/TASK 12-12-32-991-001 EFF : ALL 12-12-32 R SROS
Page 311 Jul 01/06
(5) Make sure that the pressure control valve is closed. (6) On the 3-way valve, open the bleed control valve. (7) Slowly open the bleed/inflation valve (1), to release the nitrogen from the gas chamber. Leave the bleed/inflation valve (1) open for a minimum of 2 hours. This will let the gas separate from the oil. (8) Remove the blanking cap (8). R R R
(9) Connect the hydraulic supply to the filling valve (9). Use HYDRAULIC FLUIDS (Material No. 02-001) or HYDRAULIC FLUIDS (Material No. 02004) or HYDRAULIC FLUIDS (Material No. 02-006).
R R
NOTE : Hydraulic fluids 02-001, 02-004 and 02-006 can be mixed in all ____ applicable maintenance tasks and in all quantities. Subtask 12-12-32-864-050 G. Depressurization of the Pitch Trimmer (1) Depressurize the pitch trimmer (Ref. TASK 32-11-15-000-802). 4. Procedure _________ Subtask 12-12-32-611-050 A. To Fill the Shock Absorber with Hydraulic Fluid (Ref. Fig. 304/TASK 12-12-32-991-016) WARNING : DO NOT GET THE FLUID ON YOUR SKIN OR IN YOUR EYES. IF YOU DO: _______ - FLUSH IT AWAY WITH CLEAN WATER - GET MEDICAL AID. CAUTION : MAKE SURE THAT THE FLUID DOES NOT STAY ON THE AIRCRAFT _______ STRUCTURE. IF THE FLUID GETS ON THE AIRCRAFT STRUCTURE, WASH IT OFF IMMEDIATELY WITH SOAP AND WATER. (1) Operate the COMPRESSION TOOL until the shock absorber is fully compressed. (a) On the hydraulic control panel: - set the oleo descent control valve to CLOSE - set the bogie beam vent valve to CLOSE - set the oleo directional control valve to UP.
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MLG Shock Absorber - Dimension Details Figure 304/TASK 12-12-32-991-016
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Page 313 Jan 01/07
(b) Operate the hand pump until the shock absorber is fully compressed. (2) Measure the dimension H. This should be between 43.5 mm (1.7125 in.) and 52.5 mm (2.0669 in.). NOTE : The dimension H is measured between the inner faces of the ____ torque link lugs. (3) Remove and discard the lockwire from the secondary bleed valve (2). R R R R R
NOTE : Make sure you do not move the seal changeover valve when you ____ remove the lockwire from the secondary bleed valve (2) at step (3). If the seal changeover valve is moved it must be set back counterclockwise to the open position (Ref. TASK 32-11-13-960801). (4) Connect a transparent bleed tube between the secondary bleed valve (2) and the container. (5) Make sure that the bleed screw (7) is closed and correctly torqued. (6) Carefully open the secondary bleed valve (2). (7) Open the hydraulic shut off valve. (8) Open the filling valve (9). (9) Monitor the flow of fluid from the bleed hoses and slowly increase the hydraulic supply to a maximum pressure of 1.7 bar (24.0 psi). (10) When the flow of fluid from the secondary bleed valve (2) is free from air, do these steps: (a) Continue to monitor the fluid until a minimum of 5 l (1.30 USgal) has come out of the shock absorber which is free from air. (b) Close the secondary bleed valve (2). (11) When the flow of fluid from the bleed/inflation valve (1) is free from air, close the filling valve (9). (12) Close the hydraulic shut off valve.
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(13) Continue to monitor the flow of fluid from the bleed/inflation valve (1) for 10 minutes. NOTE : Make sure that the free end of the bleed tube is a minimum of ____ 400 mm (16 in.) below the bleed/inflation valve (1). (14) When the flow of fluid stops, close the bleed/inflation valve (1). (15) On the 3-way valve, close the bleed control valve. (16) Remove the clear bleed tubes and the container. (17) TORQUE the secondary bleed valve (2) to between 0.29 and 0.34 m.daN (25 and 30 lbf.in.). (18) Safety the secondary bleed valve (2) with MISCELLANEOUS (Material No. 19-010). (19) Remove the hydraulic supply line from the filling valve (9). Subtask 12-12-32-614-051 B. Inflation of the Shock Absorber (Ref. Fig. 305/TASK 12-12-32-991-007-A) WARNING : DO NOT PUT COMPRESSED GAS IN CONTACT WITH YOUR SKIN. THE GAS _______ CAN GO THROUGH THE SKIN AND MAKE BUBBLES IN THE BLOOD. THIS CONDITION CAN KILL YOU. CAUTION : DO NOT INFLATE THE MLG SHOCK ABSORBER AT THE LOWER VALVE. IF _______ YOU USE THE LOWER VALVE HYDRAULIC FLUID WILL COME OUT. CAUTION : DO NOT INSTALL A DUST CAP ON THE BLEED/INFLATION VALVE OF THE _______ MLG SHOCK ABSORBER. IF YOU DO, THERE IS A RISK THAT IT WILL FALL INTO THE SHOCK ABSORBER. NOTE : This procedure is only applicable when the hydraulic fluid level ____ was changed. For the applicable procedure to inflate the shock absorber with nitrogen only, Ref. TASK 12-14-32-614-802. (1) Use the ADAPTER, CHARGING - MLG to open the bleed/inflation valve (1). (2) On the 3-way valve, open the bleed control valve.
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MLG Shock Absorber - Pressure Extension Chart Figure 305/TASK 12-12-32-991-007-A12 (SHEET 1) EFF : ALL 12-12-32 R SROS
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MLG Shock Absorber - Pressure Extension Chart Figure 305/TASK 12-12-32-991-007-A22 (SHEET 2) EFF : ALL 12-12-32 R SROS
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(3) Operate the COMPRESSION TOOL to let the shock absorber extend fully: (a) On the hydraulic control panel: - set the oleo directional control valve to DOWN - set the oleo descent control valve to OPEN. NOTE : If the oleo does not extend, operate the hand pump until ____ movement of the oleo occurs. (b) When the shock absorber is fully extended, set the bogie beam control-cylinder vent-valve to OPEN. (c) Set the oleo directional control valve to UP (this will vent the full bore side of the oleo control cylinders (21). (4) Make sure that the shock absorber extends fully to give a dimension H of between 773.5 mm (30.45 in.) and 782.5 mm (30.81 in.). (5) On the 3-way valve, close the bleed control valve. (6) Do these steps: R R
(a) Use a thermometer to measure the surface temperature of the aluminum piston adjacent to the bleed/inflation valve (1). (b) Look at the fully extended inflation chart and find the correct inflation pressure for the temperature you measured at step (a). If your measured value is different from the chart values, use the best approximate value from the chart. (7) At the nitrogen source, set the regulator to the pressure you found at step (6)(b). (8) Open the nitrogen shut off valve. (9) On the 3-way valve, open the pressure control valve. (10) Inflate the shock absorber to the pressure you found at step (6)(b). (Use a pressure gage 0 - 60 bar). (11) Close the nitrogen shut-off valve. (12) After a minimum period of 10 minutes (to let the shock absorber become stable), measure the temperature and pressure again. (13) If the pressure is not in compliance with the fully extended inflation chart, do the steps (7) thru (9) again.
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(14) Close the bleed/inflation valve (1) and release the nitrogen supply pressure. (15) On the 3-way valve, close the pressure control valve. (16) Close the nitrogen shut-off valve. (17) Remove the nitrogen supply from the 3-way valve. (18) Remove the 3-way valve together with the hose. (19) Remove the ADAPTER, CHARGING - MLG from the bleed inflation valve (1). Subtask 12-12-32-942-050 C. Removal of Equipment (Ref. Fig. 302/TASK 12-12-32-991-010) (1) Removal of the COMPRESSION TOOL: (a) Disconnect the hydraulic lines (22) from the cylinders (21). (b) Disconnect the hydraulic line (64) from the cylinder (36). (c) Remove: - the lock pins (34) and pins (29) and (37) - the retainer nut (26), - the retainer nut (42), - the lock pin (56), the
(40), the washers (33) and (39) and the the cylinder (21) and the clevis (27). the cylinder (21) and the clevis (41). washer (55) and the pin (60).
(d) Hold the yoke assembly (35) (together with the bogie beam cylinder (36)) and remove the bolts (32) and the clamps (31). (e) Remove the yoke assembly (35). (f) Remove: - the lock pin (58), the nut (59), the bolt (54) and the adaptor (57) - the bolts (23) and (28), the spindles (38) and (43) and the housings (25) and (30). (2) Make sure that the work area is clean and clear of tools and other items.
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Subtask 12-12-32-870-050 D. Bleeding of the Pitch Trimmer (1) Do the bleed procedure for the pitch trimmer (Ref. TASK 32-11-15-400802). Subtask 12-12-32-586-050 E. Aircraft Maintenance Configuration (1) Lower the aircraft off the jacks (Ref. TASK 07-11-00-586-801). 5. Close-up ________ Subtask 12-12-32-780-050 A. Pressure/Extension Check (Ref. Fig. 305/TASK 12-12-32-991-007-A) (1) Measure: - the nitrogen pressure - the surface temperature of the aluminum piston adjacent to the bleed/inflation valve (1) - the dimension H.
R R
(2) Make sure these measurements agree with the specified data given in the Pressure Extension Chart (Aircraft Weight on Wheels). (3) TORQUE the bleed/inflation valve (1) to between 0.6 and 0.8 m.daN (50 and 70 lbf.in.). (4) Use the SPECIAL MATERIALS (Material No. 05-004B) to do a nitrogen leak test of the bleed/inflation valve (1). Leaks are not permitted. (5) TORQUE the filling valve (9) to between 0.6 and 0.8 m.daN (50 and 70 lbf.in.) (6) Install the blanking cap (8). (7) Examine the filling valve (9) for hydraulic leaks. Leaks are not permitted.
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Subtask 12-12-32-410-051 B. Close Access (1) Install the access panel (3) with the bracket (4), the washers (5) and the bolts (6). (2) Safety the bolts (6) with lockwire, corrosion-resistant steel 0.8 mm (0.032 in) dia. Subtask 12-12-32-942-053 C. Removal of the Ground Support Equipment (1) Remove the access platform(s). (2) Remove the warning notice(s). (3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
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TASK 12-12-32-611-804 Hydraulic Replenishment of the MLG Shock Absorber (Weight on Wheels) WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED ON THE _______ LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
container hose
R No No No No No No No No No
specific specific specific specific specific specific specific specific specific
460007156
pressure gage 0 - 200 bar safety barriers standard charging equipment thermometer transparent bleed tube warning notices 3-way valve adjustable access platform 3.5 m (11 ft. 6 in.) Torque Wrench : range 0.00 to 1.20 m.daN (0.00 to 9.00 lbf.ft) 1 ADAPTER, CHARGING - MLG
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B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 02-001
USA MIL-H-5606 OIL, HYDRAULICPETROLEUM FLUID (Ref. 20-31-00)
Material No. 02-004 R R
Material No. 02-006 Material No. 05-004B Material No. 19-010
SHOCK ABSORBER FLUID (Ref. 20-31-00) USA BMS 3-32 TYPE II SHOCK ABSORBER FLUID (Ref. 20-31-00) USA MIL-L-25567 TYPE I OXYGEN LEAK DETECTOR (Ref. 20-31-00) USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-804 32-00-00-481-801 R
32-11-13-960-801 32-12-00-410-801 12-12-32-991-002 12-12-32-991-001 12-12-32-991-016 12-12-32-991-007-A
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Installation of the Safety Devices on the Landing Gears Replacement of the MLG Shock Absorber Seals Close the MLG Doors after Maintenance Fig. 301 Fig. 303 Fig. 304 Fig. 305
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3. __________ Job Set-up Subtask 12-12-32-941-054 A. Safety Precautions (1) Put the safety barriers in position. (2) Put the warning notices: - in the cockpit to tell persons not to operate the landing gear controls. - at the applicable ground door opening handle to tell persons not to open the MLG door. Subtask 12-12-32-860-053 B. Aircraft Maintenance Configuration (1) Make sure that the Green hydraulic system is depressurized (Ref. TASK 29-00-00-864-804). (2) Make sure that the safety devices are installed on the L/G (Ref. TASK 32-00-00-481-801). (3) MLG door configuration: CAUTION : YOU MUST CLOSE THE MLG DOORS BEFORE YOU DEFLATE THE MAIN _______ LANDING-GEAR SHOCK-ABSORBER. IF THE DOORS STAY OPEN, THEY WILL HIT THE GROUND AND DAMAGE WILL OCCUR. (a) Make sure that the applicable MLG door is closed (Ref. TASK 3212-00-410-801). Subtask 12-12-32-010-057 C. Get Access (Ref. Fig. 301/TASK 12-12-32-991-002) (1) Put the adjustable access platform at the applicable zone: - for the LH MLG shock absorber at zone 731 - for the RH MLG shock absorber at zone 741. (2) Remove and discard the lockwire from the bolts (6). (3) Remove the bolts (6), the washers (5), the bracket (4) and the panel (3).
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Subtask 12-12-32-614-056 R
D. Preparation WARNING : MAKE SURE THAT THE AREA AROUND THE AIRCRAFT IS CLEAR BEFORE YOU _______ PRESSURIZE/DEPRESSURIZE THE SHOCK ABSORBER, WITH THE AIRCRAFT WEIGHT ON THE GROUND. THE MOVEMENT OF THE AIRCRAFT COULD BE DANGEROUS. (Ref. Fig. 303/TASK 12-12-32-991-001, 305/TASK 12-12-32-991-007-A) (1) Install the ADAPTER, CHARGING - MLG on the bleed/inflation valve (1). (2) Connect the hose between the ADAPTER, CHARGING - MLG and the 3-way valve. (3) Connect a transparent bleed tube between the 3-way valve and the container. Make sure that the free end of the bleed tube is a minimum of 400 mm (16 in.) below the bleed inflation valve. (4) On the 3-way valve, make sure that the pressure control valve is closed, then open the bleed control valve. (5) Open the bleed/inflation valve (1) to release the nitrogen pressure from the gas chamber. Let the weight of the aircraft compress the shock absorber. (6) Measure the dimension H. This should be between 43.5 mm (1.7125 in.) and 52.5 mm (2.0669 in.). (7) Let the bleed/inflation valve (1) stay open for a minimum of 2 hours (to let the gas separate from the oil). (8) Remove the blanking cap (8).
R R R
(9) Connect the hydraulic supply to the filling valve (9). Use HYDRAULIC FLUIDS (Material No. 02-001) or HYDRAULIC FLUIDS (Material No. 02004) or HYDRAULIC FLUIDS (Material No. 02-006).
R R
NOTE : Hydraulic fluids 02-001, 02-004 and 02-006 can be mixed in all ____ applicable maintenance tasks and in all quantities.
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4. Procedure _________ Subtask 12-12-32-611-054 A. Filling the Shock Absorber with Hydraulic Fluid WARNING : DO NOT GET THE FLUID ON YOUR SKIN OR IN YOUR EYES. IF YOU DO: _______ - FLUSH IT AWAY WITH CLEAN WATER - GET MEDICAL AID. WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. _______ CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU. CAUTION : MAKE SURE THAT THE FLUID DOES NOT STAY ON THE AIRCRAFT _______ STRUCTURE. IF THE FLUID GETS ON THE AIRCRAFT STRUCTURE, WASH IT OFF IMMEDIATELY WITH SOAP AND WATER. (1) Remove and discard the lockwire from the secondary bleed valve (2). R R R R R
NOTE : Make sure you do not move the seal changeover valve when you ____ remove the lockwire from the secondary bleed valve (2) at step (1). If the seal changeover valve is moved it must be set back counterclockwise to the open position (Ref. TASK 32-11-13-960801). (2) Connect a bleed hose between the secondary bleed valve (2) and the container. (3) Carefully open the secondary bleed valve (2). (4) Open the hydraulic shut off valve. (5) Open the filling valve (9). (6) Monitor the flow of fluid from the bleed hoses and slowly increase the hydraulic pressure to a maximum of 1.7 bar (25 psi). (7) When the flow of fluid from the secondary bleed valve (2) is free from air, do this procedure: (a) Continue to monitor the fluid until a minimum of 5l (1.3 US gal) has come out of the shock absorber which is free from air. (b) Close the secondary bleed valve (2).
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(8) When the flow of fluid from the bleed/inflation valve (1) is free from air, close the filling valve (9). (9) Close the hydraulic shut off valve. (10) Continue to monitor the flow of fluid from the bleed/inflation valve (1) for 10 minutes. (11) When the oil has drained, close the bleed/inflation valve (1). (12) On the 3-way valve, close the bleed control valve. (13) Remove the transparent bleed tubes and the container. (14) TORQUE the secondary bleed valve to between 0.29 and 0.34 m.daN (25 and 30 lbf.in.). (15) Safety the secondary bleed valve (2) with MISCELLANEOUS (Material No. 19-010). (16) Remove the hydraulic supply line from the filling valve (9). Subtask 12-12-32-614-057 R
B. Inflation of the Shock Absorber WARNING : MAKE SURE THAT THE AREA AROUND THE AIRCRAFT IS CLEAR BEFORE YOU _______ PRESSURIZE/DEPRESSURIZE THE SHOCK ABSORBER, WITH THE AIRCRAFT WEIGHT ON THE GROUND. THE MOVEMENT OF THE AIRCRAFT COULD BE DANGEROUS. WARNING : DO NOT PUT COMPRESSED GAS IN CONTACT WITH YOUR SKIN. THE GAS _______ CAN GO THROUGH THE SKIN AND MAKE BUBBLES IN THE BLOOD. THIS CONDITION CAN KILL YOU. CAUTION : DO NOT INFLATE THE MLG SHOCK ABSORBER AT THE LOWER VALVE. IF _______ YOU USE THE LOWER VALVE HYDRAULIC FLUID WILL COME OUT. CAUTION : DO NOT INSTALL A DUST CAP ON THE BLEED/INFLATION VALVE OF THE _______ MLG SHOCK ABSORBER. IF YOU DO, THERE IS A RISK THAT IT WILL FALL INTO THE SHOCK ABSORBER. NOTE : This procedure is only applicable when the hydraulic fluid level ____ was changed. For the applicable procedure to inflate the shock absorber with nitrogen only, Ref. TASK 12-14-32-614-802.
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NOTE : You must use a pressure gage 0 - 200 bar when you do this ____ inflation procedure. R R
(1) Install the standard charging equipment on the ADAPTER, CHARGING MLG and open the nitrogen shut off valve. (2) On the 3-way valve, open the pressure control valve. (3) Use the ADAPTER, CHARGING - MLG to open the bleed/inflation valve (1). (4) Slowly increase the nitrogen supply pressure until the dimension H starts to increase. (5) Do these steps: (a) Use a thermometer to measure the surface temperature of the aluminium piston adjacent to the bleed/inflation valve (1). Write down the temperature. (b) Measure and write down the MLG pressure at the bleed/inflation valve (1). (c) Use the recorded pressure and temperature values to read the dimension H from the inflation chart. (Ref. Fig. 304/TASK 12-12-32-991-016, 305/TASK 12-12-32-991-007A) If your measured values are different from the values given in the chart, use the best approximate chart values. (d) Open the bleed/inflation valve (1) to control the shock absorber pressure. Adjust the pressure to give approximately the dimension H you identified at step (5)(c). (e) Measure and write down the MLG pressure at the bleed/inflation valve (1) (f) Measure and write down the dimension H. (g) Use the inflation chart to find the correct pressure for the dimension H. (6) If the pressure at step (5)(e) is less than the pressure at step (5)(g), do this procedure: (a) Adjust the nitrogen source to give the necessary pressure.
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(b) Slowly open the bleed/inflation valve (1). (c) Inflate the shock absorber to the correct pressure shown on the inflation chart. (d) When the pressure is correct, close the bleed/inflation valve (1). If the dimension H changes before you have the correct pressure, measure dimension H again. Use the new dimension H to do the procedure again from step (5)(e). (e) Close the charge valve on the nitrogen source. Let the shock absorber pressure and its dimension H become stable for a minimum of 10 minutes. (f) Measure the pressure and dimension H again. (g) If the pressure has changed, do the steps (6)(b) thru (6)(d) again. If the dimension H has changed, do the procedure again from step (5)(e). Use the new dimension H. (h) Close the bleed/inflation valve (1). (7) If the pressure at step (5)(e) is more than the pressure at step (5)(g), do this procedure: (a) Slowly open the bleed/inflation valve (1). (b) Deflate the shock absorber to the correct pressure you identified at step (5)(g) from the inflation chart. If the dimension H changes before you have the correct pressure, measure dimension H again. Use the new dimension H to do the procedure again from step (5)(e). (c) Close the charge valve on the nitrogen source. Let the shock absorber pressure and its dimension H become stable for a minimum of 10 minutes. (d) Measure the pressure and dimension H again. (e) If the pressure has changed, do the steps (7)(a) thru (7)(d) again. If the dimension H has changed do the procedure again from step (5)(e). Use the new dimension H. (f) Close the bleed/inflation valve (1). R
(8) Remove the nitrogen source from the standard charging equipment.
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R
(9) Remove the standard charging equipment from the ADAPTER, CHARGING MLG. (10) TORQUE the bleed/inflation valve (1) to between 0.60 and 0.80 m.daN (53.09 and 70.79 lbf.in). (11) Remove the ADAPTER, CHARGING - MLG. (12) Use the SPECIAL MATERIALS (Material No. 05-004B) to do a leak test of the bleed/inflation valve (1) and the bleed screw (7). No leakage is permitted. (13) TORQUE the filling valve (9) 0.60 and 0.80 m.daN (53 and 70 lbf.in.). (14) Install the blanking cap (8). (15) Examine the filling valve (9) for leakage. No leakage is permitted. 5. Close-up ________ Subtask 12-12-32-410-053 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panel (3) with the bracket (4), the washers (5) and the bolts (6). (3) Safety the bolts (6) with MISCELLANEOUS (Material No. 19-010). Subtask 12-12-32-942-056 B. Removal of Equipment (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
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TASK 12-12-32-611-805 Hydraulic Replenishment of the NLG Shock Absorber (Aircraft on Jacks) WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED ON THE _______ LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No R
specific specific specific specific specific specific
U21891000
axle jack with a lift height of 465 mm (18.31 in) transparent bleed tube container 5 l (1.3208 USgal) 1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE 1 WARNING NOTICE Torque Wrench : range 0.00 to 1.20 m.daN (0.00 to 9.00 lbf.ft) 2 ADAPTOR - INFLATION
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B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 02-001
USA MIL-H-5606 OIL, HYDRAULICPETROLEUM FLUID (Ref. 20-31-00)
Material No. 02-004 R R
Material No. 02-006 Material No. 05-004B
SHOCK ABSORBER FLUID (Ref. 20-31-00) USA BMS 3-32 TYPE II SHOCK ABSORBER FLUID (Ref. 20-31-00) USA MIL-L-25567 TYPE I OXYGEN LEAK DETECTOR (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------07-11-00-581-801 07-11-00-581-802 07-11-00-586-801 07-11-00-586-802 12-14-32-614-804 29-00-00-864-804 32-00-00-081-802 32-00-00-481-801 32-21-00-220-803 32-22-00-010-801 32-22-00-410-801 12-12-32-991-005 12-12-32-991-006
Lifting of the Aircraft for Maintenance Operations Lifting of the Aircraft at the Forward Jacking Point, MLG Wheels on the Ground Lowering of the Aircraft for Maintenance Operations Lowering of the Aircraft at the Forward Jacking Point, MLG Wheels on the Ground Gas Replenishment of the NLG Shock Absorber Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Removal of the Safety Devices from the Landing Gear Doors Installation of the Safety Devices on the Landing Gears Check Nose Gear Shock Absorber Nitrogen Charge Pressure Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance Fig. 306 Fig. 307
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3. __________ Job Set-up R R R R R
Subtask 12-12-32-941-064 A. General Information The design of your NLG shock absorber does not permit AIRBUS to give a procedure to service the shock absorber with weight on wheels. Subtask 12-12-32-941-057
R
B. Safety Precautions (1) Put the WARNING NOTICE in the cockpit to tell persons not to operate the landing gear and the nosewheel steering controls. Subtask 12-12-32-860-054
R
C. Aircraft Maintenance Configuration (1) Make sure that the Green hydraulic system is depressurized (Ref. TASK 29-00-00-864-804). (2) Make sure that the safety devices are installed on the L/G (Ref. TASK 32-00-00-481-801). Subtask 12-12-32-582-054
R
D. Lift the Aircraft (1) Make sure that the aircraft is on jacks and that the wheels of the NLG are clear of the ground (Ref. TASK 07-11-00-581-801) or (Ref. TASK 07-11-00-581-802). (2) Make sure that the shock absorber is fully extended. Subtask 12-12-32-582-053
R
E. Put the axle jack with a lift height of 465 mm (18.31 in) below the NLG jacking dome.
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Subtask 12-12-32-010-059 F. Get Access (1) Open the NLG forward doors (Ref. TASK 32-22-00-010-801). (2) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at zone 711. Subtask 12-12-32-614-059 G. Preparation (Ref. Fig. 306/TASK 12-12-32-991-005, 307/TASK 12-12-32-991-006) (1) Remove the blanking caps (1) and (3). R
(2) Install a ADAPTOR - INFLATION (U21891000) on each of the charging valves (2) and (4). (3) Connect the hydraulic filling hose to the FILLING ASSEMBLY at the charging valve (2) and the three-way valve. (4) Connect the transparent bleed tube between the 3-way valve and the container. (5) Connect the hydraulic supply to the 3-way valve and the FILLING ASSEMBLY. Use HYDRAULIC FLUIDS (Material No. 02-001) or HYDRAULIC FLUIDS (Material No. 02-004) or HYDRAULIC FLUIDS (Material No. 02006). NOTE : Hydraulic fluids 02-001, 02-004 and 02-006 can be mixed in all ____ applicable maintenance tasks and in all quantities. (6) Make sure that the pressure control valve on the 3-way valve is closed, then open the bleed control valve. (7) Operate the FILLING ASSEMBLY at the charging valve (4) to decrease the nitrogen pressure in the second stage (HP) pressure chamber to zero. Leave the charging valve (4) open. NOTE : This makes sure that the floating piston is on its lower stop. ____ (8) Operate the FILLING ASSEMBLY at the charging valve (2) to decrease the nitrogen pressure in the first stage (LP) pressure chamber to zero. Leave the charging valve (2) open.
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NLG Shock Absorber - Filling System Figure 306/TASK 12-12-32-991-005 EFF : ALL 12-12-32 R SROS
Page 335 Jul 01/06
NLG Shock Absorber - Inflation/Filling Valves Figure 307/TASK 12-12-32-991-006 EFF : ALL 12-12-32 R SROS
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4. Procedure _________ Subtask 12-12-32-611-055 R
A. Fill the Shock Absorber with Hydraulic Fluid WARNING : DO NOT GET THE FLUID ON YOUR SKIN OR IN YOUR EYES. IF YOU DO: _______ - FLUSH IT AWAY WITH CLEAN WATER - GET MEDICAL AID. CAUTION : MAKE SURE THAT THE FLUID DOES NOT STAY ON THE AIRCRAFT _______ STRUCTURE. IF THE FLUID GETS ON THE AIRCRAFT STRUCTURE, WASH IT OFF IMMEDIATELY WITH SOAP AND WATER. (1) During this step, monitor the flow of hydraulic fluid through the transparent bleed hose. (a) Close the bleed control valve and open the FILLING ASSEMBLY at the charging valve (2).
R R R R
(b) Slowly fill the first stage pressure chamber with HYDRAULIC FLUIDS (Material No. 02-001) or HYDRAULIC FLUIDS (Material No. 02-004) or HYDRAULIC FLUIDS (Material No. 02-006) pressurized to 15 bar (217 psi) maximum.
R R
NOTE : Hydraulic fluids 02-001, 02-004 and 02-006 can be mixed in ____ all applicable maintenance tasks in all quantities. (c) Decrease the pressure to zero and leave the charging valve (2) open. (2) Install a FILLING ASSEMBLY on the charging valve (4) and connect the nitrogen filling hose to the FILLING ASSEMBLY. (3) Connect the nitrogen supply hose to the nitrogen filling hose. (4) Slowly pressurize the second stage pressure chamber (HP) with nitrogen. NOTE : The floating piston goes against the upper stop and hydraulic ____ fluid is pushed out of the first stage pressure chamber (LP). (5) Increase the nitrogen pressure at the charging valve (4) to the correct pressure (Ref. TASK 12-14-32-614-804). (6) Close the charging valve (4) and TORQUE it to between 0.57 and 0.79 m.daN (50.44 and 69.91 lbf.in).
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(7) Use the SPECIAL MATERIALS (Material No. 05-004B) to do a leak check of the charging valve (4). Leakage must not occur. (8) Remove the FILLING ASSEMBLY from the charging valve (4) and disconnect the nitrogen filling hose. (9) Make sure that the first stage pressure chamber is full of hydraulic fluid. If necessary do step (1) again. (10) During this step monitor the flow of hydraulic fluid through the transparent bleed hose: NOTE : During these steps you will use the hydraulic supply to extend ____ the sliding tube. (a) Slowly operate the axle jack to push the sliding tube fully in to the main fitting. (b) Do the procedure in step (1) again and let the sliding tube fully extend. (c) Do the steps (a) and (b) again until the flow of hydraulic fluid from the transparent bleed tube is free from air bubbles. (11) Do the procedure in step (1) again and let the sliding tube fully extend. (12) Operate the axle jack to push the sliding tube in to the main fitting until the dimension H is between 189 and 194 mm (7.44 to 7.64 in). (13) Connect the nitrogen filling hose to the charging valve (2) and connect the nitrogen supply hose to the nitrogen filling hose. (14) Slowly pressurize the first stage pressure chamber (LP) with nitrogen and open the valve on the axle jack, in a controlled manner, to let the shock absorber fully extend. (15) Increase the nitrogen pressure to the correct pressure (Ref. TASK 1214-32-614-804). (16) Make sure that the shock absorber dimension H is between 408 and 416 mm (16.07 and 16.37 in). (17) Close the pressure control valve. (18) Use the FILLING ASSEMBLY to close the charge valve (2).
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(19) Decrease the nitrogen supply pressure to zero. (20) Disconnect the nitrogen supply. (21) Use a SPECIAL MATERIALS (Material No. 05-004B) to do a leak check of the charging valve (2) and (4). Leakage must not occur. (22) Install the blanking caps on the charging valves (2) and (4). (23) Remove the axle jack. (24) Disconnect the hydraulic supply and remove the bleed hose and the container. Subtask 12-12-32-942-057 B. Removal of the Support Equipment (1) Remove the access platform. (2) Make sure that the work area is clean and clear of tools and other items. Subtask 12-12-32-586-053 C. Lower the Aircraft (1) Lower the aircraft off jacks (Ref. TASK 07-11-00-586-801) or (Ref. TASK 07-11-00-586-802). Subtask 12-12-32-780-054 D. Pressure/Extension Check (1) Do a pressure/extension check of the NLG shock absorber (Ref. TASK 32-21-00-220-803). 5. Close-up ________ Subtask 12-12-32-410-054 A. Close Access (1) Remove the safety devices from the NLG doors (Ref. TASK 32-00-00-081802). (2) Close the NLG forward doors (Ref. TASK 32-22-00-410-801).
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Subtask 12-12-32-942-058 B. Removal of the Ground Equipment (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
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OIL - DESCRIPTION AND OPERATION _______________________________ 1. General _______ This section gives the instructions to fill the engine, the accessories (IDG, pneumatic starter) the APU, the flight control components. It includes the topics below: 12-13-24/P. 12-13-27/P. 12-13-49/P. 12-13-79/P. 12-13-80/P.
Block Block Block Block Block
301 301 301 301 301
ELECTRICAL POWER FLIGHT CONTROLS APU ENGINE OIL ENGINE STARTING
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ELECTRICAL POWER - SERVICING ____________________________ TASK 12-13-24-680-804 Draining of the Oil from the IDG WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE COMPONENTS IMMEDIATELY AFTER _______ THE ENGINE IS SHUTDOWN. THE ENGINE COMPONENTS CAN STAY HOT FOR UP TO ONE HOUR. WARNING : WEAR GOGGLES, INSULATED GLOVES AND OTHER PROTECTIVE CLOTHES. _______ HOT OIL CAN BURN YOUR EYES AND SKIN. IF OIL TOUCHES YOUR EYES OR SKIN, GET MEDICAL AID. CAUTION : DO NOT DO THE SERVICING OF A DISCONNECTED IDG. CONTINUED OPERATION OF _______ A DEFECTIVE IDG CAN CAUSE DAMAGE. CAUTION : DO NOT OPERATE THE IDG: _______ - IF IT CONTAINS TOO MUCH OIL - IF IT DOES NOT CONTAIN ENOUGH OIL IF YOU DO, YOU CAN CAUSE DAMAGE TO THE IDG. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No
specific specific specific specific
DH13PM
circuit breaker(s) safety clip(s) container 5.7 l (1.5 USgal) access platform 2.5 m (8 ft. 2 in.) Torque Wrench : range 36.00 to 220.00 lbf.in (0.40 to 2.60 m.daN) 1 TANK - ENGINE OIL FILLING UP
R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-24 Page 301 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
P03-001
Material No.
P05-289
* engine oil (Ref. 70-30-00) * lockwire 0.032 in. (0.80 mm) dia. (Ref. 70-30-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------3
O-ring
24-21-51 42A-060
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-13-24-610-801 12-32-24-281-803 24-21-00-612-810 24-42-00-861-801 24-42-00-862-801 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801 78-30-00-040-804 78-30-00-410-801 78-30-00-440-804 12-13-24-991-008
IDG Servicing - Filling of the IDG with Oil or Addition of Oil after a Level Check Sampling of the IDG Oil for Analysis Servicing of the IDG after Oil Chemical Contamination Energize the Ground Service Network De-energize the Ground Service Network Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Deactivation of the Thrust Reverser for Maintenance Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Reactivation of the Thrust Reverser after Maintenance Fig. 301
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3. __________ Job Set-up Subtask 12-13-24-861-053 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-24-941-059 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure. Subtask 12-13-24-010-062 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU. Subtask 12-13-24-865-056 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU GCU 1 4XU1 Q10 722VU FADEC B ENG 1 13KS1 D44 742VU IDG 1 DISC 1XT1 A76 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 721VU GCU 2 4XU2 N06 722VU FADEC B ENG 2 13KS2 K49 742VU IDG 2 DISC 1XT2 D69 742VU FADEC A ENG 2 12KS2 Q74
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Subtask 12-13-24-010-090 E. Get Access (1) Open the aft fan cowl doors (Ref. TASK 71-13-00-010-802): - FOR 4030EM1 415BL, 416BR, - FOR 4030EM2 425BL, 426BR. Subtask 12-13-24-040-062 F. Deactivation of the Thrust Reverser WARNING : YOU MUST DEACTIVATE THE THRUST REVERSER DIRECTIONAL CONTROL _______ VALVE (DCV) BEFORE YOU WORK ON OR AROUND THE TRANSLATING COWL. IF YOU DO NOT DEACTIVATE THE DCV, YOU CAN CAUSE ACCIDENTAL THRUST REVERSER OPERATION AND INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT. (1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 7830-00-040-804). Subtask 12-13-24-010-063 G. Get Access (1) Open the thrust reverser cowl doors (Ref. TASK 78-30-00-010-801): - FOR 4030EM1 417AL, 418AR, - FOR 4030EM2 427AL, 428AR. 4. Procedure _________ (Ref. Fig. 301/TASK 12-13-24-991-008) Subtask 12-13-24-864-059 A. Depressurization of the IDG Case WARNING : POINT THE OVERFLOW DRAIN HOSE INTO A CONTAINER WHEN YOU CONNECT _______ THE HOSE TO THE OVERFLOW DRAIN VALVE. THIS WILL PREVENT BURNS FROM THE HOT OIL SPRAY. HOT OIL CAN CAUSE BURNS TO EYES AND SKIN.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-24 Page 304 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
IDG Servicing - Overflow Drain Valve and Case Drain of the IDG Figure 301/TASK 12-13-24-991-008 R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-24 Page 305 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
CAUTION : DO NOT USE DEVICES OTHER THAN THE APPROVED OVERFLOW DRAIN-HOSE _______ FITTING. HARD METAL OBJECTS SUCH AS SCREWDRIVERS CAN CAUSE DAMAGE TO THE OVERFLOW DRAIN-VALVE SEAT. (1) Put a container 5.7 l (1.5 USgal) below the IDG (1). (2) Remove the dust cap (7) from the overflow drain valve (6). (3) Put the end of the overflow drain hose (4) of the TANK - ENGINE OIL FILLING UP (DH13PM) in the container (5). (4) Do this step to depressurize the IDG case: (a) Connect the overflow drain hose (4) of the TANK - ENGINE OIL FILLING UP (DH13PM) to the overflow drain valve (6). NOTE : Some oil can come out of the overflow drain hose (4) of ____ the TANK - ENGINE OIL FILLING UP (DH13PM) when you connect it. Subtask 12-13-24-680-059 B. Draining of the Oil WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. _______ CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU. (1) Cut and remove the lockwire from the case drain plug (2). NOTE : Approximately 3.8 l (1 USgal) of oil will flow into the ____ container. (2) Remove the case drain plug (2). (3) Remove the O-ring (3) and discard it. (4) Drain the oil. NOTE : If the drained oil has a fuel odor, do the servicing of the ____ IDG after oil chemical contamination (Ref. TASK 24-21-00-612810). If you think that the condition of the drained oil is not correct, do a sampling of the IDG oil for analysis (Ref. TASK 12-32-24-281-803).
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Subtask 12-13-24-640-056 C. Lubricate the new O-ring (3) with engine oil (Material No. P03-001) Subtask 12-13-24-420-068 D. Installation of the Case Drain Plug (1) Install the new O-ring (3) on the case drain plug (2). (2) Install the case drain plug (2). (3) TORQUE the case drain plug (2) to between 55 and 75 lbf.in (0.62 and 0.84 m.daN). (4) Safety the case drain plug (2) with lockwire 0.032 in. (0.80 mm) dia. (Material No. P05-289). Subtask 12-13-24-420-069 E. Installation of the Dust Cap (1) Disconnect the overflow drain hose (4) of the TANK - ENGINE OIL FILLING UP (DH13PM) from the overflow drain valve (6). (2) Install the dust cap (7) on the overflow drain valve (6). Subtask 12-13-24-612-062 F. Fill the IDG with oil or add oil to the IDG after a level check (Ref. TASK 12-13-24-610-801), if you must not remove the IDG. 5. Close-up ________ Subtask 12-13-24-410-075 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the thrust reverser cowl doors (Ref. TASK 78-30-00-410-801): - FOR 4030EM1 417AL, 418AR, - FOR 4030EM2 427AL, 428AR.
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Subtask 12-13-24-440-062 B. Make the thrust reverser serviceable after maintenance (Ref. TASK 78-3000-440-804). Subtask 12-13-24-865-057 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1, 1XT1, 4XU1 - FOR 4030EM2 12KS2, 13KS2, 1XT2, 4XU2 Subtask 12-13-24-410-059 D. Close Access (1) Close the protective door of the AC/DC emergency power center 740VU. (2) Close the access door 811. (3) Remove the access platform(s). (4) Close the aft fan cowl doors (Ref. TASK 71-13-00-410-802): - FOR 4030EM1 415BL, 416BR, - FOR 4030EM2 425BL, 426BR. Subtask 12-13-24-862-053 E. De-energize the ground service network (Ref. TASK 24-42-00-862-801)
R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-24 Page 308 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
TASK 12-13-24-610-801 IDG Servicing - Filling of the IDG with Oil or Addition of Oil after a Level Check WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE COMPONENTS IMMEDIATELY AFTER _______ THE ENGINE IS SHUTDOWN. THE ENGINE COMPONENTS CAN STAY HOT FOR UP TO ONE HOUR. WARNING : WEAR GOGGLES, INSULATED GLOVES AND OTHER PROTECTIVE CLOTHES. _______ HOT OIL CAN BURN YOUR EYES AND SKIN. IF OIL TOUCHES YOUR EYES OR SKIN, GET MEDICAL AID. CAUTION : DO NOT OPERATE THE IDG: _______ - IF IT CONTAINS TOO MUCH OIL - IF IT DOES NOT CONTAIN ENOUGH OIL IF YOU DO, YOU CAN CAUSE DAMAGE TO THE IDG. CAUTION : USE ONLY NEW CANS OF OIL WHEN YOU FILL THE IDG WITH OIL OR ADD OIL TO _______ THE IDG. THE CONTAMINATION IN OIL THAT STAYS IN OPEN CANS CAN CAUSE FAST DETERIORATION OF THE OIL AND WILL DECREASE THE LIFE OF THE IDG. CAUTION : DO NOT USE SOLVENTS THAT CONTAIN CHLORINE TO CLEAN THE EQUIPMENT _______ (PUMP, HOSES, TANK AND FUNNEL) USED TO FILL THE IDG WITH OIL. CHLORINE CONTAMINATION OF THE OIL CAN CAUSE FAST DETERIORATION OF THE OIL AND WILL DECREASE THE LIFE OF THE IDG. CAUTION : DO NOT DO THE SERVICING OF A DISCONNECTED IDG. CONTINUED OPERATION OF _______ A DEFECTIVE IDG CAN CAUSE DAMAGE. CAUTION : DO NOT LET ENGINE OIL FALL ON THE ENGINE. UNWANTED OIL MUST BE _______ REMOVED IMMEDIATELY. THE OIL CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job You must do this procedure if you: - fill an IDG installed on the aircraft after you drained it, - fill a replacement IDG installed on the aircraft, - add oil when the oil level at the sight-glass is not correct, - add oil after replacement of the scavenge filter element, - add oil after replacement of a component of the IDG oil cooling-system.
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2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific DH13PM
circuit breaker(s) safety clip(s) container 5.7 l (1.5 USgal) access platform 2.5 m (8 ft. 2 in.) 1 TANK - ENGINE OIL FILLING UP
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 03-002
GB DEF-STAN 91-101 LUBRICATING OIL TURBINE ENGINE SYNT BASE (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 71-00-00-720-816 71-00-00-860-818 71-13-00-010-802 71-13-00-410-802 78-30-00-040-804 78-30-00-440-804 12-13-24-991-009 12-13-24-991-019
Energize the Ground Service Network De-energize the Ground Service Network Test No. 2 - Engine Motor Leak Test (Dry Method) Thrust Reverser Cowl Doors Open Normal Engine Automatic Start Procedure Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Deactivation of the Thrust Reverser for Maintenance Reactivation of the Thrust Reverser after Maintenance Fig. 302 Fig. 303
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3. __________ Job Set-up Subtask 12-13-24-861-054 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-24-941-060 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure. Subtask 12-13-24-010-064 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU. Subtask 12-13-24-865-058 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU GCU 1 4XU1 Q10 722VU FADEC B ENG 1 13KS1 D44 742VU IDG 1 DISC 1XT1 A76 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 721VU GCU 2 4XU2 N06 722VU FADEC B ENG 2 13KS2 K49 742VU IDG 2 DISC 1XT2 D69 742VU FADEC A ENG 2 12KS2 Q74
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Subtask 12-13-24-010-086 E. Get Access (1) Open the aft fan cowl doors (Ref. TASK 71-13-00-010-802): - FOR 4030EM1 415BL, 416BR, - FOR 4030EM2 425BL, 426BR. Subtask 12-13-24-040-059 F. Deactivation of the Thrust Reverser WARNING : YOU MUST DEACTIVATE THE THRUST REVERSER DIRECTIONAL CONTROL _______ VALVE (DCV) BEFORE YOU WORK ON OR AROUND THE TRANSLATING COWL. IF YOU DO NOT DEACTIVATE THE DCV, YOU CAN CAUSE ACCIDENTAL THRUST REVERSER OPERATION AND INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT. (1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 7830-00-040-804). Subtask 12-13-24-010-065 G. Get Access (1) Open the lower left thrust reverser access door: - FOR 4030EM1 417EL, - FOR 4030EM2 427EL. 4. Procedure _________ (Ref. Fig. 302/TASK 12-13-24-991-009, 303/TASK 12-13-24-991-019) Subtask 12-13-24-864-060 A. Depressurization of the IDG Case WARNING : POINT THE OVERFLOW DRAIN HOSE INTO A CONTAINER WHEN YOU CONNECT _______ THE HOSE TO THE OVERFLOW DRAIN VALVE. THIS WILL PREVENT BURNS FROM THE HOT OIL SPRAY. HOT OIL CAN CAUSE BURNS TO EYES AND SKIN.
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IDG Servicing - Oil Level System of the IDG Figure 302/TASK 12-13-24-991-009 R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-24 Page 313 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
Correct Filling of the IDG Figure 303/TASK 12-13-24-991-019 R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-24 Page 314 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
CAUTION : DO NOT USE DEVICES OTHER THAN THE APPROVED OVERFLOW DRAIN-HOSE _______ FITTING. HARD METAL OBJECTS SUCH AS SCREWDRIVERS CAN CAUSE DAMAGE TO THE OVERFLOW DRAIN-VALVE SEAT. (1) Put a container 5.7 l (1.5 USgal) below the IDG (1). (2) Remove the dust cap (3) from the overflow drain valve (2). (3) Put the end of the overflow drain hose (4) of the TANK - ENGINE OIL FILLING UP (DH13PM) in the container (5). (4) Do this step to depressurize the IDG case: (a) Connect the overflow drain hose (4) of the TANK - ENGINE OIL FILLING UP (DH13PM) to the overflow drain valve (2). NOTE : Some oil can come out of the overflow drain hose (4) of ____ the TANK - ENGINE OIL FILLING UP (DH13PM) when you connect it. Subtask 12-13-24-612-063 B. Filling of the IDG with Oil CAUTION : USE ONLY APPROVED TYPES/BRANDS OF LUBRICANTS. _______ DO NOT MIX TYPES/BRANDS OF LUBRICANTS. NOTE : In rain, fog or wet conditions, be careful to prevent water ____ contamination of the IDG oil during the filling procedure. (1) Remove the dust cap (7) from the pressure fill valve (8). (2) Connect the pressure fill hose (6) of the TANK - ENGINE OIL FILLING UP (DH13PM) to the pressure fill valve (8). (3) Fill the IDG with filtered OILS (Material No. 03-002) at a maximum pressure of 35 psi (2.41 bar). NOTE : The AMM 20-34-00 gives a list of oil brand names approved for ____ the IDG. (4) Stop the filling procedure when the quantity of oil collected from the overflow drain hose (4) of the TANK - ENGINE OIL FILLING UP (DH13PM) is 0.95 l (0.25 USgal) minimum.
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Subtask 12-13-24-020-059 C. Removal of the Hoses (1) Disconnect the pressure fill hose (6) of the TANK - ENGINE OIL FILLING UP (DH13PM) from the pressure fill valve (8). (2) Install the dust cap (7) on the pressure fill valve (8). (3) When only drops of oil come out of the overflow drain hose (4) of the TANK - ENGINE OIL FILLING UP (DH13PM), remove the hose (4). (4) Install the dust cap (3) on the overflow drain valve (2). Subtask 12-13-24-720-056 D. If you replaced a part of the oil system (filter, external system component, drain plug), do a dry motoring for leak check before inspection (Ref. TASK 71-00-00-720-816). Subtask 12-13-24-210-051 E. Inspection of the Oil Level R R R
NOTE : After an IDG oil servicing, you must do a reset of the oil level ____ sensor. To do this, release then push the related GEN pushbutton switch. NOTE : Before you do a check of the oil level, we recommend that you do ____ dry motoring for two minutes (Ref. TASK 71-00-00-720-816). Alternatively you can do the check after an engine run, at minimum idle (Ref. TASK 71-00-00-860-818). This is to make sure you get maximum filling of the external oil system. (1) Inspection of the oil level with or without a dry motoring. CAUTION : IF YOU DRY-MOTOR THE ENGINE, MAKE SURE THAT THE OIL LEVEL _______ IS STABLE BEFORE YOU DO THE INSPECTION. IN AMBIENT AIR TEMPERATURES OF LESS THAN 20⁰C, THE OIL LEVEL WILL BECOME STABLE ONLY AFTER 30 MINUTES. THUS THE LEVEL INDICATIONS ON THE SIGHTGLASS WILL NOT BE CORRECT BEFORE THE END OF THIS PERIOD. IF YOU ADD OIL WHEN IT IS NOT NECESSARY, THERE IS A RISK THAT YOU WILL CAUSE FAILURE OF THE IDG. (a) Let the oil in the IDG become stable.
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(b) Look at the oil level sight-glass of the IDG: - if the oil level is at or near the top of the green band, oil servicing is not necessary, - if the oil level is below the green band or above the green band , do the steps 4.A. thru 4.D. again. (2) Inspection of the oil level after an engine run (alternative procedure). (a) Let the oil in the IDG become stable for 5 minutes. (b) Look at the oil level sight-glass of the IDG: - if the oil level is in the green or yellow band, oil servicing is not necessary, - if the oil level is below the green band or above the yellow band, do the steps 4.A. thru 4.D. again. 5. Close-up ________ Subtask 12-13-24-410-071 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the lower left thrust reverser access door: - FOR 4030EM1 417EL, - FOR 4030EM2 427EL. Subtask 12-13-24-440-059 B. Make the thrust reverser serviceable after maintenance (Ref. TASK 78-3000-440-804). Subtask 12-13-24-865-059 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1, 1XT1, 4XU1 - FOR 4030EM2 12KS2, 13KS2, 1XT2, 4XU2
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R R R
Subtask 12-13-24-860-050 D. Do a reset of the oil level sensor To do this, release then push the related GEN pushbutton switch. Subtask 12-13-24-410-060
R
E. Close Access (1) Close the protective door of the AC/DC emergency power center 740VU. (2) Close the access door 811. (3) Remove the access platform(s). (4) Close the aft fan cowl doors (Ref. TASK 71-13-00-410-802): - FOR 4030EM1 415BL, 416BR, - FOR 4030EM2 425BL, 426BR. Subtask 12-13-24-862-054
R
F. De-energize the ground service network (Ref. TASK 24-42-00-862-801)
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TASK 12-13-24-612-807 Drain IDG Oil System, Discard Filter Element and Replenish WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE COMPONENTS IMMEDIATELY AFTER _______ THE ENGINE IS SHUTDOWN. THE ENGINE COMPONENTS CAN STAY HOT FOR UP TO ONE HOUR. WARNING : WEAR GOGGLES, INSULATED GLOVES AND OTHER PROTECTIVE CLOTHES. _______ HOT OIL CAN BURN YOUR EYES AND SKIN. IF OIL TOUCHES YOUR EYES OR SKIN, GET MEDICAL AID. CAUTION : USE ONLY NEW CANS OF OIL WHEN YOU FILL THE IDG WITH OIL OR ADD OIL TO _______ THE IDG. THE CONTAMINATION IN OIL THAT STAYS IN OPEN CANS CAN CAUSE FAST DETERIORATION OF THE OIL AND WILL DECREASE THE LIFE OF THE IDG. CAUTION : DO NOT USE SOLVENTS THAT CONTAIN CHLORINE TO CLEAN THE EQUIPMENT _______ (PUMP, HOSES, TANK AND FUNNEL) USED TO FILL THE IDG WITH OIL. CHLORINE CONTAMINATION OF THE OIL CAN CAUSE FAST DETERIORATION OF THE OIL AND WILL DECREASE THE LIFE OF THE IDG. CAUTION : DO NOT OPERATE THE IDG: _______ - IF IT CONTAINS TOO MUCH OIL - IF IT DOES NOT CONTAIN ENOUGH OIL IF YOU DO, YOU CAN CAUSE DAMAGE TO THE IDG. CAUTION : DO NOT DO THE SERVICING OF A DISCONNECTED IDG. CONTINUED OPERATION OF _______ A DEFECTIVE IDG CAN CAUSE DAMAGE. 1. __________________ Reason for the Job Refer to the MPD TASK: 242100-13 To drain the IDG, replace the IDG oil filter element and fill the IDG with oil.
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2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No
specific specific specific specific specific
blanking plug circuit breaker(s) safety clip(s) container 5.7 l (1.5 USgal) access platform 2.5 m (8 ft. 2 in.) Torque Wrench : range 2.00 to 26.00 lbf.ft (0.20 to 3.60 m.daN) Torque Wrench : range 36.00 to 220.00 lbf.in (0.40 to 2.60 m.daN) 1 TANK - ENGINE OIL FILLING UP
No specific DH13PM
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
P05-289
Material No. 03-002
* lockwire 0.032 in. (0.80 mm) dia (Ref. 70-30-00) GB DEF-STAN 91-101 LUBRICATING OIL TURBINE ENGINE SYNT BASE (Ref. 20-31-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------2 3 3 4
O-ring O-ring filter element O-ring
24-21-51 24-21-51 24-21-51 24-21-51
42A-220 42A-060 42A-230 42A-240
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D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-13-24-610-801 12-32-24-281-803 24-21-00-210-814 24-21-00-612-810 24-42-00-861-801 24-42-00-862-801 71-00-00-720-816 71-00-00-860-818 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801 78-30-00-040-804 78-30-00-410-801 78-30-00-440-804 12-13-24-991-011 12-13-24-991-022
IDG Servicing - Filling of the IDG with Oil or Addition of Oil after a Level Check Sampling of the IDG Oil for Analysis Inspection of the Filter Element Servicing of the IDG after Oil Chemical Contamination Energize the Ground Service Network De-energize the Ground Service Network Test No. 2 - Engine Motor Leak Test (Dry Method) Thrust Reverser Cowl Doors Open Normal Engine Automatic Start Procedure Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Deactivation of the Thrust Reverser for Maintenance Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Reactivation of the Thrust Reverser after Maintenance Fig. 304 Fig. 305
3. __________ Job Set-up Subtask 12-13-24-861-058 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-24-941-061 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure.
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Subtask 12-13-24-010-069 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU. Subtask 12-13-24-865-066 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU GCU 1 4XU1 Q10 722VU FADEC B ENG 1 13KS1 D44 742VU IDG 1 DISC 1XT1 A76 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 721VU GCU 2 4XU2 N06 722VU FADEC B ENG 2 13KS2 K49 742VU IDG 2 DISC 1XT2 D69 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-13-24-010-081 E. Get Access (1) Open the aft fan cowl doors (Ref. TASK 71-13-00-010-802): - FOR 4030EM1 415BL, 416BR, - FOR 4030EM2 425BL, 426BR. Subtask 12-13-24-040-057 F. Deactivation of the Thrust Reverser WARNING : YOU MUST DEACTIVATE THE THRUST REVERSER DIRECTIONAL CONTROL _______ VALVE (DCV) BEFORE YOU WORK ON OR AROUND THE TRANSLATING COWL. IF YOU DO NOT DEACTIVATE THE DCV, YOU CAN CAUSE ACCIDENTAL THRUST REVERSER OPERATION AND INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.
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(1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 7830-00-040-804). Subtask 12-13-24-010-070 G. Get Access (1) Open the thrust reverser cowl doors (Ref. TASK 78-30-00-010-801): - FOR 4030EM1 417AL, 418AR, - FOR 4030EM2 427AL, 428AR. 4. Procedure _________ (Ref. Fig. 304/TASK 12-13-24-991-011, 305/TASK 12-13-24-991-022) Subtask 12-13-24-864-061 A. Depressurization of the IDG Case (Ref. Fig. 304/TASK 12-13-24-991-011) WARNING : POINT THE OVERFLOW DRAIN HOSE INTO A CONTAINER WHEN YOU CONNECT _______ THE HOSE TO THE OVERFLOW DRAIN VALVE. THIS WILL PREVENT BURNS FROM THE HOT OIL SPRAY. HOT OIL CAN CAUSE BURNS TO EYES AND SKIN. CAUTION : DO NOT USE DEVICES OTHER THAN THE APPROVED OVERFLOW DRAIN-HOSE _______ FITTING. HARD METAL OBJECTS SUCH AS SCREWDRIVERS CAN CAUSE DAMAGE TO THE OVERFLOW DRAIN-VALVE SEAT. (1) Put a container 5.7 l (1.5 USgal) below the IDG (1). (2) Remove the dust cap (5) from the overflow drain valve (4). (3) Put the end of the overflow drain hose (6) of the TANK - ENGINE OIL FILLING UP (DH13PM) in the container (7). (4) Do this step to depressurize the IDG case: (a) Connect the overflow drain hose (6) of the TANK - ENGINE OIL FILLING UP (DH13PM) to the overflow drain valve (4). NOTE : Some oil may come out of the overflow drain hose (6) of ____ the TANK - ENGINE OIL FILLING UP (DH13PM) when you connect it.
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Draining and Filling of the IDG Figure 304/TASK 12-13-24-991-011 R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-24 Page 324 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
IDG Oil Filter Figure 305/TASK 12-13-24-991-022 R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-24 Page 325 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
Subtask 12-13-24-680-060 B. Draining of the Oil (Ref. Fig. 304/TASK 12-13-24-991-011) WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. _______ CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU. (1) Cut and remove the lockwire from the case drain plug (2). NOTE : Be prepared to catch approximately 3.8 l (1 USgal) of oil in ____ the container. (2) Remove the case drain plug (2). (3) Remove the O-ring (3) and discard it. (4) Drain the oil. NOTE : If the drained oil has a fuel odor, do the servicing of the ____ IDG after oil chemical contamination (Ref. TASK 24-21-00-612810). If you think that the condition of the drained oil is not correct, do a sampling of the IDG oil for analysis (Ref. TASK 12-32-24-281-803). Subtask 12-13-24-020-067 C. Removal of the IDG Oil Filter (Ref. Fig. 305/TASK 12-13-24-991-022) WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. _______ CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU. (1) Cut and remove the lockwire from the filter cover (1). NOTE : Put a container 5.7 l (1.5 USgal) below the filter cavity. ____ (2) Loosen and remove the filter cover (1). (3) Remove and discard the O-ring (2) from the filter cover (1). (4) Remove the filter element (3). (5) Remove and discard the O-ring (4) from the filter element (3).
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(6) Install a blanking plug on the filter cavity port. Subtask 12-13-24-210-064 D. Inspection of the IDG Oil Filter (1) Do the inspection of the filter element (Ref. TASK 24-21-00-210-814). NOTE : We recommend you do a visual inspection of the IDG oil filter ____ for possible contamination, debris. Subtask 12-13-24-640-057 E. Lubrication of the Expendable Parts (1) Lubricate the new O-ring (3) with OILS (Material No. 03-002). (2) Lubricate the new O-ring (4) with OILS (Material No. 03-002). (3) Lubricate the new O-ring (2) with OILS (Material No. 03-002). Subtask 12-13-24-420-071 F. Installation of the Case Drain Plug (Ref. Fig. 304/TASK 12-13-24-991-011) WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. _______ CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU. (1) Install the new O-ring (3) on the case drain plug (2). (2) Install the case drain plug (2). (3) TORQUE the case drain plug (2) to between 55 and 75 lbf.in (0.62 and 0.84 m.daN). (4) Safety the case drain plug (2) with lockwire 0.032 in. (0.80 mm) dia (Material No. P05-289).
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Subtask 12-13-24-420-081 G. Installation of the IDG Oil Filter (Ref. Fig. 305/TASK 12-13-24-991-022) WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. _______ CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU. CAUTION : MAKE SURE THE COMPONENTS ARE SEATED IN THE IDG SCAVENGE FILTER _______ CAVITY BEFORE YOU INSTALL THE FILTER COVER. DO NOT TIGHTEN THE FILTER COVER SCREWS TO FORCE THE FILTER COMPONENTS INTO THE HOUSING. (1) Install the new O-ring (4) on the filter element (3). (2) Install the new O-ring (2) on the filter cover (1). (3) Put the filter element (3) in the filter cavity. (4) Install the filter cover (1). (5) TORQUE the filter cover (1) to between 13 and 15 lbf.ft (1.76 and 2.03 m.daN). (6) Safety the filter cover (1) with lockwire 0.032 in. (0.80 mm) dia (Material No. P05-289). Subtask 12-13-24-612-066 H. Filling of the IDG with Oil (Ref. Fig. 304/TASK 12-13-24-991-011) CAUTION : USE ONLY APPROVED TYPES/BRANDS OF LUBRICANTS. _______ DO NOT MIX TYPES/BRANDS OF LUBRICANTS. NOTE : In rain, fog or wet conditions, be careful to prevent water ____ contamination of the IDG oil during the filling procedure. (1) Remove the dust cap (9) from the pressure fill valve (10). (2) Connect the pressure fill hose (8) of the TANK - ENGINE OIL FILLING UP (DH13PM) to the pressure fill valve (10).
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(3) Fill the IDG with the filtered OILS (Material No. 03-002) at a maximum pressure of 35 psi (2.41 bar). NOTE : The AMM 20-34-00 gives a list of oil brand names approved for ____ IDG. (4) Stop the filling procedure when the quantity of oil collected from the overflow drain hose (6) of the TANK - ENGINE OIL FILLING UP (DH13PM) is 0.95 l (0.25 USgal) minimum. Subtask 12-13-24-020-061 J. Removal of the Hoses (Ref. Fig. 304/TASK 12-13-24-991-011) (1) Disconnect the pressure fill hose (8) of the TANK - ENGINE OIL FILLING UP (DH13PM) from the pressure fill valve (10). (2) Install the dust cap (9) on the pressure fill valve (10). (3) When only drops of oil come out of the overflow drain hose (6) of the TANK - ENGINE OIL FILLING UP (DH13PM), disconnect the hose (6). (4) Install the dust cap (5) on the overflow drain valve (4). Subtask 12-13-24-720-052 K. If you replaced a part of the oil system (filter, external system component, drain plug), do a dry motoring for leak check before inspection (Ref. TASK 71-00-00-720-816). Subtask 12-13-24-210-057 L. Inspection of the Oil Level (Ref. Fig. 304/TASK 12-13-24-991-011) NOTE : Before you do a check of the oil level, we recommend that you do ____ dry motoring for two minutes (Ref. TASK 71-00-00-720-816). Alternatively, you can do the check after an engine start at minimum idle (Ref. TASK 71-00-00-860-818). This is to make sure you get maximum filling of the external oil system.
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(1) Inspection of the oil level after dry motoring. CAUTION : IF YOU DRY-MOTOR THE ENGINE, MAKE SURE THAT THE OIL LEVEL _______ IS STABLE BEFORE YOU DO THE INSPECTION. IN AMBIENT AIR TEMPERATURES OF LESS THAN 20⁰C, THE OIL LEVEL WILL BECOME STABLE ONLY AFTER 30 MINUTES. THUS THE LEVEL INDICATIONS ON THE SIGHTGLASS WILL NOT BE CORRECT BEFORE THE END OF THIS PERIOD. IF YOU ADD OIL WHEN IT IS NOT NECESSARY, THERE IS A RISK THAT YOU WILL CAUSE FAILURE OF THE IDG. (a) Let the oil in the IDG become stable. (b) Look at the oil level sight-glass of the IDG: - if the oil level is at or near the top of the green band, oil servicing is not necessary, - if the oil level is below the green band or above the green band , do the filling of the IDG with oil or addition of oil after level check (Ref. TASK 12-13-24-610-801). (2) Inspection of the oil level after an engine start (alternative procedure). (a) Let the oil in the IDG become stable for 5 minutes. (b) Look at the oil level sight-glass of the IDG: - if the oil level is in the green or yellow band, oil servicing is not necessary, - if the oil level is below the green band or above the yellow band, do the filling of the IDG with oil or addition of oil after level check (Ref. TASK 12-13-24-610-801). 5. Close-up ________ Subtask 12-13-24-410-067 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the thrust reverser cowl doors (Ref. TASK 78-30-00-410-801): - FOR 4030EM1 417AL, 418AR, - FOR 4030EM2 427AL, 428AR.
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Subtask 12-13-24-440-057 B. Make the thrust reverser serviceable after maintenance (Ref. TASK 78-3000-440-804). Subtask 12-13-24-865-067 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1, 1XT1, 4XU1 - FOR 4030EM2 12KS2, 13KS2, 1XT2, 4XU2 Subtask 12-13-24-410-061 D. Close Access (1) Close the protective door of the AC/DC emergency power center 740VU. (2) Close the access door 811. (3) Remove the access platform(s). (4) Close the aft fan cowl doors (Ref. TASK 71-13-00-410-802): - FOR 4030EM1 415BL, 416BR, - FOR 4030EM2 425BL, 426BR. Subtask 12-13-24-862-058 E. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-24 Page 331 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
ELECTRICAL POWER - SERVICING ____________________________ TASK 12-13-24-680-805 R
Draining of the Oil from the IDG WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE COMPONENTS IMMEDIATELY AFTER _______ THE ENGINE IS SHUTDOWN. THE ENGINE COMPONENTS CAN STAY HOT FOR UP TO ONE HOUR. WARNING : WEAR GOGGLES, INSULATED GLOVES AND OTHER PROTECTIVE CLOTHES. _______ HOT OIL CAN BURN YOUR EYES AND SKIN. IF OIL TOUCHES YOUR EYES OR SKIN, GET MEDICAL AID. CAUTION : DO NOT DO THE SERVICING OF A DISCONNECTED IDG. CONTINUED OPERATION OF _______ A DEFECTIVE IDG CAN CAUSE DAMAGE. CAUTION : DO NOT OPERATE THE IDG: _______ - IF IT CONTAINS TOO MUCH OIL - IF IT DOES NOT CONTAIN ENOUGH OIL IF YOU DO, YOU CAN CAUSE DAMAGE TO THE IDG. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No
specific specific specific specific
DH13PM
circuit breaker(s) safety clip(s) container 5.7 l (1.5 USgal) access platform 2.5 m (8 ft. 2 in.) Torque Wrench : range 36.00 to 220.00 lbf.in (0.40 to 2.60 m.daN) 1 TANK - ENGINE OIL FILLING UP
EFF : 701-749, 12-13-24 Page 301 Config-2 Jan 01/02 SROS
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
OMat 1011
Material No.
OMAT 238
* engine oil (Ref. 70-30-00) * lockwire 0.028 to 0.031 in. (0.71 to 0.79 mm) dia. (Ref. 70-30-00)
R R
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-13-24-612-808 12-32-24-281-804 24-21-00-612-814 24-42-00-861-801 24-42-00-862-801 71-13-00-010-805 71-13-00-410-805 78-31-00-040-805 78-31-00-440-805 12-13-24-991-012
IDG Servicing - Filling of the IDG with Addition of Oil after Level Check Sampling of the IDG Oil for Analysis Servicing of the IDG after Oil Chemical Energize the Ground Service Network De-energize the Ground Service Network Open the Fan Cowl Doors Close the Fan Cowl Doors Deactivation of the Thrust Reverser for Activation of the Thrust Reverser after Fig. 301
Oil or Contamination
Maintenance Maintenance
3. __________ Job Set-up Subtask 12-13-24-861-059 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-24-941-062 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure.
EFF : 701-749, 12-13-24 Page 302 Config-2 Jan 01/06 SROS
Subtask 12-13-24-010-071 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU. Subtask 12-13-24-865-068 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU GCU 1 4XU1 Q10 722VU FADEC B ENG 1 13KS1 D44 742VU IDG 1 DISC 1XT1 A76 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 721VU GCU 2 4XU2 N06 722VU FADEC B ENG 2 13KS2 K49 742VU IDG 2 DISC 1XT2 D69 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-13-24-010-072 E. Get Access (1) Open the fan cowl doors (Ref. TASK 71-13-00-010-805): - FOR 4030EM1 415AL, 416AR, - FOR 4030EM2 425AL, 426AR. Subtask 12-13-24-040-063 F. Deactivation of the Thrust Reverser WARNING : YOU MUST DEACTIVATE THE THRUST REVERSER BEFORE YOU DO WORK ON _______ OR AROUND IT. IF YOU DO NOT, THE THRUST REVERSER CAN OPERATE ACCIDENTALLY AND CAUSE INJURY AND/OR DAMAGE.
EFF : 701-749, 12-13-24 Page 303 Config-2 Jan 01/06 R SROS
(1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 7831-00-040-805). 4. Procedure _________ (Ref. Fig. 301/TASK 12-13-24-991-012) Subtask 12-13-24-864-062 A. Depressurization of the IDG Case WARNING : POINT THE OVERFLOW DRAIN HOSE INTO A CONTAINER WHEN YOU CONNECT _______ THE HOSE TO THE OVERFLOW DRAIN VALVE. THIS WILL PREVENT BURNS FROM THE HOT OIL SPRAY. HOT OIL CAN CAUSE BURNS TO EYES AND SKIN. CAUTION : DO NOT USE DEVICES OTHER THAN THE APPROVED OVERFLOW DRAIN-HOSE _______ FITTING. HARD METAL OBJECTS SUCH AS SCREWDRIVERS CAN CAUSE DAMAGE TO THE OVERFLOW DRAIN-VALVE SEAT. (1) Put a container 5.7 l (1.5 USgal) below the IDG (1). (2) Remove the dust cap (3) from the overflow drain valve (2). (3) Put the end of the overflow drain hose (4) of the TANK - ENGINE OIL FILLING UP (DH13PM) in the container (5). (4) Do this step to depressurize the IDG case: (a) Connect the overflow drain hose (4) of the TANK - ENGINE OIL FILLING UP (DH13PM) to the overflow drain valve (2). NOTE : Some oil can come out of the overflow drain hose (4) of ____ the TANK - ENGINE OIL FILLING UP (DH13PM) when you connect it. Subtask 12-13-24-680-061 B. Draining of the Oil WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. _______ CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU.
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IDG Servicing - Overflow Drain Valve and Case Drain of the IDG Figure 301/TASK 12-13-24-991-012 EFF : 701-749, 12-13-24 Page 305 Config-2 Oct 01/00 SROS
(1) Cut and remove the lockwire from the case drain plug (7). NOTE : Approximately 3.8 l (1 USgal) of oil will flow into the ____ container. (2) Remove the case drain plug (7). (3) Remove the O-ring (6) and discard it. (4) Drain the oil. NOTE : If the drained oil has a fuel odor, do the servicing of the ____ IDG after oil chemical contamination (Ref. TASK 24-21-00-612814). If you think that the condition of the drained oil is not correct, do a sampling of the IDG oil for analysis (Ref. TASK 12-32-24-281-804). Subtask 12-13-24-640-058 C. Lubricate the new O-ring (6) with engine oil (Material No. OMat 1011). Subtask 12-13-24-420-074 D. Installation of the Case Drain Plug (1) Install the new O-ring (6) on the case drain plug (7). (2) Install the case drain plug (7). (3) TORQUE the case drain plug (7) to between 55 and 75 lbf.in (0.62 and 0.84 m.daN). (4) Safety the case drain plug (7) with lockwire 0.028 to 0.031 in. (0.71 to 0.79 mm) dia. (Material No. OMAT 238). Subtask 12-13-24-420-075 E. Installation of the Dust Cap (1) Disconnect the overflow drain hose (4) of the TANK - ENGINE OIL FILLING UP (DH13PM) from the overflow drain valve (2). (2) Install the dust cap (3) on the overflow drain valve (2).
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Subtask 12-13-24-612-067 F. Fill the IDG with oil or add oil to the IDG after a level check (Ref. TASK 12-13-24-612-808), if you must not remove the IDG. 5. Close-up ________ Subtask 12-13-24-440-063 A. Make the thrust reverser serviceable after maintenance (Ref. TASK 78-3100-440-805). Subtask 12-13-24-865-069 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1, 1XT1, 4XU1 - FOR 4030EM2 12KS2, 13KS2, 1XT2, 4XU2 Subtask 12-13-24-410-062 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Close the access door 811. (4) Remove the access platform(s). (5) Close the fan cowl doors (Ref. TASK 71-13-00-410-805): - FOR 4030EM1 415AL, 416AR, - FOR 4030EM2 425AL, 426AR. Subtask 12-13-24-862-059 D. De-energize the ground service network (Ref. TASK 24-42-00-862-801)
EFF : 701-749, 12-13-24 Page 307 Config-2 Jan 01/06 R SROS
INTENTIONALLY BLANK
R 12-13-24 Page 308 Config-2 Jan 01/06 SROS
TASK 12-13-24-612-808 R R
IDG Servicing - Filling of the IDG with Oil or Addition of Oil after Level Check WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE COMPONENTS IMMEDIATELY AFTER _______ THE ENGINE IS SHUTDOWN. THE ENGINE COMPONENTS CAN STAY HOT FOR UP TO ONE HOUR. WARNING : WEAR GOGGLES, INSULATED GLOVES AND OTHER PROTECTIVE CLOTHES. _______ HOT OIL CAN BURN YOUR EYES AND SKIN. IF OIL TOUCHES YOUR EYES OR SKIN, GET MEDICAL AID. CAUTION : DO NOT OPERATE THE IDG: _______ - IF IT CONTAINS TOO MUCH OIL - IF IT DOES NOT CONTAIN ENOUGH OIL IF YOU DO, YOU CAN CAUSE DAMAGE TO THE IDG. CAUTION : USE ONLY NEW CANS OF OIL WHEN YOU FILL THE IDG WITH OIL OR ADD OIL TO _______ THE IDG. THE CONTAMINATION IN OIL THAT STAYS IN OPEN CANS CAN CAUSE FAST DETERIORATION OF THE OIL AND WILL DECREASE THE LIFE OF THE IDG. CAUTION : DO NOT USE SOLVENTS THAT CONTAIN CHLORINE TO CLEAN THE EQUIPMENT _______ (PUMP, HOSES, TANK AND FUNNEL) USED TO FILL THE IDG WITH OIL. CHLORINE CONTAMINATION OF THE OIL CAN CAUSE FAST DETERIORATION OF THE OIL AND WILL DECREASE THE LIFE OF THE IDG. CAUTION : DO NOT DO THE SERVICING OF A DISCONNECTED IDG. CONTINUED OPERATION OF _______ A DEFECTIVE IDG CAN CAUSE DAMAGE. 1. __________________ Reason for the Job You must do this procedure if you: - fill an IDG installed on the aircraft after you drained it, - fill a replacement IDG installed on the aircraft, - add oil when the oil level at the sight-glass is not correct, - add oil after replacement of the scavenge filter element, - add oil after replacement of a component of the IDG oil cooling-system.
EFF : 701-749, 12-13-24 Page 309 Config-2 Jan 01/02 SROS
2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific DH13PM
circuit breaker(s) safety clip(s) container 5.7 l (1.5 USgal) access platform 2.5 m (8 ft. 2 in.) 1 TANK - ENGINE OIL FILLING UP
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 03-002
GB DEF-STAN 91-101 LUBRICATING OIL TURBINE ENGINE SYNT BASE (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 71-00-00-720-828 71-00-00-860-810 71-13-00-010-805 71-13-00-410-805 78-31-00-040-805 78-31-00-440-805 12-13-24-991-013 12-13-24-991-020
Energize the Ground Service Network De-energize the Ground Service Network Dry Motoring Engine Engine Automatic Start Open the Fan Cowl Doors Close the Fan Cowl Doors Deactivation of the Thrust Reverser for Maintenance Activation of the Thrust Reverser after Maintenance Fig. 302 Fig. 303
3. __________ Job Set-up Subtask 12-13-24-861-060 A. Energize the ground service network (Ref. TASK 24-42-00-861-801).
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Subtask 12-13-24-941-063 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure. Subtask 12-13-24-010-073 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU. Subtask 12-13-24-865-070 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU GCU 1 4XU1 Q10 722VU FADEC B ENG 1 13KS1 D44 742VU IDG 1 DISC 1XT1 A76 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 721VU GCU 2 4XU2 N06 722VU FADEC B ENG 2 13KS2 K49 742VU IDG 2 DISC 1XT2 D69 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-13-24-010-074 E. Get Access (1) Open the fan cowl doors (Ref. TASK 71-13-00-010-805): - FOR 4030EM1 415AL, 416AR, - FOR 4030EM2 425AL, 426AR.
EFF : 701-749, 12-13-24 Page 311 Config-2 Jan 01/02 R SROS
Subtask 12-13-24-040-060 F. Deactivation of the Thrust Reverser WARNING : YOU MUST DEACTIVATE THE THRUST REVERSER BEFORE YOU DO WORK ON _______ OR AROUND IT. IF YOU DO NOT, THE THRUST REVERSER CAN OPERATE ACCIDENTALLY AND CAUSE INJURY AND/OR DAMAGE. (1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 7831-00-040-805). 4. Procedure _________ (Ref. Fig. 302/TASK 12-13-24-991-013, 303/TASK 12-13-24-991-020) Subtask 12-13-24-864-063 A. Depressurization of the IDG Case WARNING : POINT THE OVERFLOW DRAIN HOSE INTO A CONTAINER WHEN YOU CONNECT _______ THE HOSE TO THE OVERFLOW DRAIN VALVE. THIS WILL PREVENT BURNS FROM THE HOT OIL SPRAY. HOT OIL CAN CAUSE BURNS TO EYES AND SKIN. CAUTION : DO NOT USE DEVICES OTHER THAN THE APPROVED OVERFLOW DRAIN-HOSE _______ FITTING. HARD METAL OBJECTS SUCH AS SCREWDRIVERS CAN CAUSE DAMAGE TO THE OVERFLOW DRAIN-VALVE SEAT. (1) Put a container 5.7 l (1.5 USgal) below the IDG (1). (2) Remove the dust cap (3) from the overflow drain valve (2). (3) Put the end of the overflow drain hose (5) of the TANK - ENGINE OIL FILLING UP (DH13PM) in the container (6). (4) Do this step to depressurize the IDG case: (a) Connect the overflow drain hose (5) of the TANK - ENGINE OIL FILLING UP (DH13PM) to the overflow drain valve (2). NOTE : Some oil can come out of the overflow drain hose (5) of ____ the TANK - ENGINE OIL FILLING UP (DH13PM) when you connect it.
EFF : 701-749, 12-13-24 Page 312 Config-2 Jan 01/02 R SROS
R
IDG Servicing - IDG Drain and Fill Ports Figure 302/TASK 12-13-24-991-013
EFF : 701-749, 12-13-24 Page 313 Config-2 Jan 01/02 SROS
Correct Filling of the IDG Figure 303/TASK 12-13-24-991-020 EFF : 701-749, 12-13-24 Page 314 Config-2 Jan 01/02 R SROS
Subtask 12-13-24-612-068 B. Filling of the IDG with Oil CAUTION : USE ONLY APPROVED TYPES/BRANDS OF LUBRICANTS. _______ DO NOT MIX TYPES/BRANDS OF LUBRICANTS. NOTE : In rain, fog or wet conditions, be careful to prevent water ____ contamination of the IDG oil during the filling procedure. (1) Remove the dust cap (4) from the pressure fill valve (8). (2) Connect the pressure fill hose (7) of the TANK - ENGINE OIL FILLING UP (DH13PM) to the pressure fill valve (8). (3) Fill the IDG with filtered OILS (Material No. 03-002) at a maximum pressure of 35 psi (2.41 bar). NOTE : The AMM 20-34-00 gives a list of oil brand names approved for ____ the IDG. (4) Stop the filling procedure when the quantity of oil collected from the overflow drain hose (5) of the TANK - ENGINE OIL FILLING UP (DH13PM) is 0.95 l (0.25 USgal) minimum. Subtask 12-13-24-020-062 C. Removal of the Hoses (1) Disconnect the pressure fill hose (7) of the TANK - ENGINE OIL FILLING UP (DH13PM) from the pressure fill valve (8). (2) Install the dust cap (4) on the pressure fill valve (8). (3) When only drops of oil come out of the overflow drain hose (5) of the TANK - ENGINE OIL FILLING UP (DH13PM), remove the hose (5). (4) Install the dust cap (3) on the overflow drain valve (2). Subtask 12-13-24-720-057 D. If you replaced a part of the oil system (filter, external system component, drain plug), do dry motoring for leak check before inspection (Ref. TASK 71-00-00-720-828). Subtask 12-13-24-210-053 E. Inspection of the Oil Level R R R
NOTE : After an IDG oil servicing, you must do a reset of the oil level ____ sensor. To do this, release then push the related GEN pushbutton switch.
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NOTE : Before you do a check of the oil level, we recommend that you do ____ dry motoring for two minutes (Ref. TASK 71-00-00-720-828). Alternatively, you can do the check after an engine run at minimum idle (Ref. TASK 71-00-00-860-810). This is to make sure that you get maximum filling of the external oil system. (1) Inspection of the oil level with or without dry motoring. CAUTION : IF YOU DRY-MOTOR THE ENGINE, MAKE SURE THAT THE OIL LEVEL _______ IS STABLE BEFORE YOU DO THE INSPECTION. IN AMBIENT AIR TEMPERATURES OF LESS THAN 20⁰C, THE OIL LEVEL WILL BECOME STABLE ONLY AFTER 30 MINUTES. THUS THE LEVEL INDICATIONS ON THE SIGHTGLASS WILL NOT BE CORRECT BEFORE THE END OF THIS PERIOD. IF YOU ADD OIL WHEN IT IS NOT NECESSARY, THERE IS A RISK THAT YOU WILL CAUSE FAILURE OF THE IDG. (a) Let the oil in the IDG become stable. (b) Look at the oil level sight-glass of the IDG: - if the oil level is at or near the top of the green band, oil servicing is not necessary, - if the oil level is below the green band or above the green band , do the steps 4.A. thru 4.D. again. (2) Inspection of the oil level after an engine run (alternative procedure). (a) Let the oil in the IDG become stable for 5 minutes. (b) Look at the oil level sight-glass of the IDG: - if the oil level is in the green or yellow band, oil servicing is not necessary, - if the oil level is below the green band or above the yellow band, do the steps 4.A. thru 4.D. again. 5. Close-up ________ Subtask 12-13-24-440-060 A. Make the thrust reverser serviceable after maintenance (Ref. TASK 78-3100-440-805).
EFF : 701-749, 12-13-24 Page 316 Config-2 Jul 01/05 R SROS
Subtask 12-13-24-865-071 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1, 1XT1, 4XU1 - FOR 4030EM2 12KS2, 13KS2, 1XT2, 4XU2 R R R
Subtask 12-13-24-860-053 C. Do a reset of the oil level sensor To do this, release then push the related GEN pushbutton switch. Subtask 12-13-24-410-063
R
D. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Close the access door 811. (4) Remove the access platform(s). (5) Close the fan cowl doors (Ref. TASK 71-13-00-410-805): - FOR 4030EM1 415AL, 416AR, - FOR 4030EM2 425AL, 426AR. Subtask 12-13-24-862-060
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E. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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TASK 12-13-24-612-809 R
Drain IDG Oil System, Discard Filter Element and Replenish WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE COMPONENTS IMMEDIATELY AFTER _______ THE ENGINE IS SHUTDOWN. THE ENGINE COMPONENTS CAN STAY HOT FOR UP TO ONE HOUR. WARNING : WEAR GOGGLES, INSULATED GLOVES AND OTHER PROTECTIVE CLOTHES. _______ HOT OIL CAN BURN YOUR EYES AND SKIN. IF OIL TOUCHES YOUR EYES OR SKIN, GET MEDICAL AID. CAUTION : USE ONLY NEW CANS OF OIL WHEN YOU FILL THE IDG WITH OIL OR ADD OIL TO _______ THE IDG. THE CONTAMINATION IN OIL THAT STAYS IN OPEN CANS CAN CAUSE FAST DETERIORATION OF THE OIL AND WILL DECREASE THE LIFE OF THE IDG. CAUTION : DO NOT USE SOLVENTS THAT CONTAIN CHLORINE TO CLEAN THE EQUIPMENT _______ (PUMP, HOSES, TANK AND FUNNEL) USED TO FILL THE IDG WITH OIL. CHLORINE CONTAMINATION OF THE OIL CAN CAUSE FAST DETERIORATION OF THE OIL AND WILL DECREASE THE LIFE OF THE IDG. CAUTION : DO NOT OPERATE THE IDG: _______ - IF IT CONTAINS TOO MUCH OIL - IF IT DOES NOT CONTAIN ENOUGH OIL IF YOU DO, YOU CAN CAUSE DAMAGE TO THE IDG. CAUTION : DO NOT DO THE SERVICING OF A DISCONNECTED IDG. CONTINUED OPERATION OF _______ A DEFECTIVE IDG CAN CAUSE DAMAGE. 1. __________________ Reason for the Job Refer to the MPD TASK: 242100-18 To drain the IDG, replace the IDG oil filter element and fill the IDG with oil.
EFF : 701-749, 12-13-24 Page 318 Config-2 Apr 01/04 SROS
2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No
specific specific specific specific specific
blanking plug circuit breaker(s) safety clip(s) container 5.7 l (1.5 USgal) access platform 2.5 m (8 ft. 2 in.) Torque Wrench : range 2.00 to 26.00 lbf.ft (0.20 to 3.60 m.daN) Torque Wrench : range 36.00 to 220.00 lbf.in (0.40 to 2.60 m.daN) 1 TANK - ENGINE OIL FILLING UP
No specific DH13PM
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
OMAT 1011
Material No.
OMAT 238
Material No. 03-002
* engine lubricating oil (Ref. 70-30-00) * lockwire 0.028 to 0.031 in.(0.71 to 0.79 mm) dia. (Ref. 70-30-00) GB DEF-STAN 91-101 LUBRICATING OIL TURBINE ENGINE SYNT BASE (Ref. 20-31-00)
R
EFF : 701-749, 12-13-24 Page 319 Config-2 Jan 01/06 SROS
R
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-13-24-612-808 12-32-24-281-804 24-21-00-210-810 24-21-00-612-814 24-42-00-861-801 24-42-00-862-801 71-00-00-720-828 71-00-00-860-810 71-13-00-010-805 71-13-00-410-805 78-31-00-040-805 78-31-00-440-805 12-13-24-991-014 12-13-24-991-023
IDG Servicing - Filling of the IDG with Addition of Oil after Level Check Sampling of the IDG Oil for Analysis Inspection of the Filter Element Servicing of the IDG after Oil Chemical Energize the Ground Service Network De-energize the Ground Service Network Dry Motoring Engine Engine Automatic Start Open the Fan Cowl Doors Close the Fan Cowl Doors Deactivation of the Thrust Reverser for Activation of the Thrust Reverser after Fig. 304 Fig. 305
Oil or
Contamination
Maintenance Maintenance
3. __________ Job Set-up Subtask 12-13-24-861-061 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-24-941-064 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure. Subtask 12-13-24-010-075 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU.
EFF : 701-749, 12-13-24 Page 320 Config-2 Jan 01/06 SROS
Subtask 12-13-24-865-072 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU GCU 1 4XU1 Q10 722VU FADEC B ENG 1 13KS1 D44 742VU IDG 1 DISC 1XT1 A76 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 721VU GCU 2 4XU2 N06 722VU FADEC B ENG 2 13KS2 K49 742VU IDG 2 DISC 1XT2 D69 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-13-24-010-076 E. Get Access (1) Open the fan cowl doors (Ref. TASK 71-13-00-010-805): - FOR 4030EM1 415AL, 416AR, - FOR 4030EM2 425AL, 426AR. Subtask 12-13-24-040-054 F. Deactivation of the Thrust Reverser WARNING : YOU MUST DEACTIVATE THE THRUST REVERSER BEFORE YOU DO WORK ON _______ OR AROUND IT. IF YOU DO NOT, THE THRUST REVERSER CAN OPERATE ACCIDENTALLY AND CAUSE INJURY AND/OR DAMAGE. (1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 7831-00-040-805).
EFF : 701-749, 12-13-24 Page 321 Config-2 Jan 01/02 R SROS
4. Procedure _________ (Ref. Fig. 304/TASK 12-13-24-991-014, 305/TASK 12-13-24-991-023) Subtask 12-13-24-864-064 A. Depressurization of the IDG Case (Ref. Fig. 304/TASK 12-13-24-991-014) WARNING : POINT THE OVERFLOW DRAIN HOSE INTO A CONTAINER WHEN YOU CONNECT _______ THE HOSE TO THE OVERFLOW DRAIN VALVE. THIS WILL PREVENT BURNS FROM THE HOT OIL SPRAY. HOT OIL CAN CAUSE BURNS TO EYES AND SKIN. CAUTION : DO NOT USE DEVICES OTHER THAN THE APPROVED OVERFLOW DRAIN-HOSE _______ FITTING. HARD METAL OBJECTS SUCH AS SCREWDRIVERS CAN CAUSE DAMAGE TO THE OVERFLOW DRAIN-VALVE SEAT. (1) Put a container 5.7 l (1.5 USgal) below the IDG (10). (2) Remove the dust cap (4) from the overflow drain valve (3). (3) Put the end of the overflow drain hose (6) of the TANK - ENGINE OIL FILLING UP (DH13PM) in the container (7). (4) Do this step to depressurize the IDG case: (a) Connect the overflow drain hose (6) of the TANK - ENGINE OIL FILLING UP (DH13PM) to the overflow drain valve (3). NOTE : Some oil can come out of the overflow drain hose (6) of ____ the TANK - ENGINE OIL FILLING UP (DH13PM) when you connect it. Subtask 12-13-24-680-062 B. Draining of the Oil (Ref. Fig. 304/TASK 12-13-24-991-014) WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. _______ CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU. (1) Cut and remove the lockwire from the case drain plug (2). R R
NOTE : Approximately 3.8 l (1 USgal) of oil will flow into the ____ container.
EFF : 701-749, 12-13-24 Page 322 Config-2 Jan 01/02 SROS
Draining and Filling of the IDG Figure 304/TASK 12-13-24-991-014 EFF : 701-749, 12-13-24 Page 323 Config-2 Jan 01/02 R SROS
IDG Oil Filter Figure 305/TASK 12-13-24-991-023 EFF : 701-749, 12-13-24 Page 324 Config-2 Jan 01/02 R SROS
(2) Remove the case drain plug (2). (3) Remove the seal-ring (1) and discard it. (4) Drain the oil. NOTE : If the drained oil has a fuel odor, do the servicing of the ____ IDG after oil chemical contamination (Ref. TASK 24-21-00-612814). If you think that the condition of the drained oil is not correct, do a sampling of the IDG oil for analysis (Ref. TASK 12-32-24-281-804). Subtask 12-13-24-020-068 C. Removal of the IDG Oil Filter (Ref. Fig. 305/TASK 12-13-24-991-023) WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. _______ CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU. (1) Cut and remove the lockwire from the filter cover (1). NOTE : Put a container 5.7 l (1.5 USgal) below the filter cavity. ____ R
(2) Remove the filter cover (1). (3) Remove and discard the O-ring (2) from the filter cover (1). (4) Remove the filter element (3). (5) Remove and discard the O-ring (4) from the filter element (3).
R
(6) Install a blanking plug on the filter cavity port. Subtask 12-13-24-210-065 D. Inspection of the IDG Oil Filter (1) Do the inspection of the filter element (Ref. TASK 24-21-00-210-810). NOTE : We recommend you do a visual inspection of the IDG oil filter ____ for possible contamination, debris.
EFF : 701-749, 12-13-24 Page 325 Config-2 Jan 01/02 SROS
Subtask 12-13-24-640-059 E. Lubrication of the Expendable Parts (1) Lubricate the new seal-ring (1) with engine lubricating oil (Material No. OMAT 1011). R
(2) Lubricate the new O-ring (4) with OILS (Material No. 03-002).
R
(3) Lubricate the new O-ring (2) with OILS (Material No. 03-002). Subtask 12-13-24-420-077 F. Installation of the Case Drain Plug (Ref. Fig. 304/TASK 12-13-24-991-014)
R R R
WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. _______ CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU. (1) Install the new seal-ring (1) on the case drain plug (2). (2) Install the case drain plug (2). (3) TORQUE the case drain plug (2) to between 55 and 75 lbf.in (0.62 and 0.84 m.daN). (4) Safety the case drain plug (2) with lockwire 0.028 to 0.031 in.(0.71 to 0.79 mm) dia. (Material No. OMAT 238). Subtask 12-13-24-420-082 G. Installation of the IDG Oil Filter (Ref. Fig. 305/TASK 12-13-24-991-023)
R R R
WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. _______ CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU. CAUTION : MAKE SURE THE COMPONENTS ARE SEATED IN THE IDG SCAVENGE FILTER _______ CAVITY BEFORE YOU INSTALL THE FILTER COVER. DO NOT TIGHTEN THE FILTER COVER SCREWS TO FORCE THE FILTER COMPONENTS INTO THE HOUSING. (1) Install the new O-ring (4) on the filter element (3). (2) Install the new O-ring (2) on the filter cover (1).
EFF : 701-749, 12-13-24 Page 326 Config-2 Jan 01/02 SROS
(3) Put the filter element (3) in the filter cavity. (4) Install the filter cover (1). (5) TORQUE the filter cover (1) to between 13 and 15 lbf.ft (1.76 and 2.03 m.daN). (6) Safety the filter cover (1) with the lockwire 0.028 to 0.031 in.(0.71 to 0.79 mm) dia. (Material No. OMAT 238). Subtask 12-13-24-612-071 H. Filling of the IDG with Oil (Ref. Fig. 304/TASK 12-13-24-991-014) CAUTION : USE ONLY APPROVED TYPES/BRANDS OF LUBRICANTS. _______ DO NOT MIX TYPES/BRANDS OF LUBRICANTS. NOTE : In rain, fog or wet conditions, be careful to prevent water ____ contamination of the IDG oil during the filling procedure. (1) Remove the dust cap (5) from the pressure fill valve (9). (2) Connect the pressure fill hose (8) of the TANK - ENGINE OIL FILLING UP (DH13PM) to the pressure fill valve (9). (3) Fill the IDG with the filtered OILS (Material No. 03-002) at a maximum pressure of 35 psi (2.41 bar). NOTE : The AMM 20-34-00 gives a list of oil brand names approved for ____ the IDG. (4) Stop this operation when the quantity of oil collected from the overflow drain hose (6) of the TANK - ENGINE OIL FILLING UP (DH13PM) is 0.95 l (0.25 USgal) minimum. Subtask 12-13-24-020-064 J. Removal of the Hoses (Ref. Fig. 304/TASK 12-13-24-991-014) (1) Disconnect the pressure fill hose (8) of the TANK - ENGINE OIL FILLING UP (DH13PM) from the pressure fill valve (9). (2) Install the dust cap (5) on the pressure fill valve (9). (3) When only drops of oil come out of the overflow drain hose (6) of the TANK - ENGINE OIL FILLING UP (DH13PM), disconnect the hose (6). (4) Install the dust cap (4) on the overflow drain valve (3).
EFF : 701-749, 12-13-24 Page 327 Config-2 Apr 01/03 R SROS
Subtask 12-13-24-720-050 K. If you replaced a part of the oil system (filter, external system component, drain plug), do a dry motoring for leak check before inspection (Ref. TASK 71-00-00-720-828). Subtask 12-13-24-210-055 L. Inspection of the Oil Level (Ref. Fig. 304/TASK 12-13-24-991-014) NOTE : Before you do a check of the oil level, we recommend that you do ____ dry motoring for two minutes (Ref. TASK 71-00-00-720-828). Alternatively, you can do the check after an engine start at minimum idle (Ref. TASK 71-00-00-860-810). This is to make sure you get maximum filling of the external oil system.
R R
(1) Inspection of the oil level after dry motoring. R R R R R R R
CAUTION : IF YOU DRY-MOTOR THE ENGINE, MAKE SURE THAT THE OIL LEVEL _______ IS STABLE BEFORE YOU DO THE INSPECTION. IN AMBIENT AIR TEMPERATURES OF LESS THAN 20⁰C, THE OIL LEVEL WILL BECOME STABLE ONLY AFTER 30 MINUTES. THUS THE LEVEL INDICATIONS ON THE SIGHTGLASS WILL NOT BE CORRECT BEFORE THE END OF THIS PERIOD. IF YOU ADD OIL WHEN IT IS NOT NECESSARY, THERE IS A RISK THAT YOU WILL CAUSE FAILURE OF THE IDG.
R
(a) Let the oil in the IDG become stable. (b) Look at the oil level sight-glass of the IDG: - if the oil level is at or near the top of the green band, oil servicing is not necessary, - if the oil level is below the green band or above the green band, do the filling of the IDG with oil or addition of oil after level check (Ref. TASK 12-13-24-612-808). (2) Inspection of the oil level after an engine start (alternative procedure). (a) Let the oil in the IDG become stable for 5 minutes. (b) Look at the oil level sight-glass of the IDG: - if the oil level is in the green or yellow band, oil servicing is not necessary, - if the oil level is below the green band or above the yellow band, do the filling of the IDG with oil or addition of oil after level check (Ref. TASK 12-13-24-612-808).
EFF : 701-749, 12-13-24 Page 328 Config-2 Apr 01/03 SROS
5. Close-up ________ Subtask 12-13-24-440-054 A. Make the thrust reverser serviceable after maintenance (Ref. TASK 78-3100-440-805). Subtask 12-13-24-865-073 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1, 1XT1, 4XU1 - FOR 4030EM2 12KS2, 13KS2, 1XT2, 4XU2 Subtask 12-13-24-410-064 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Close the access door 811. (4) Remove the access platform(s). (5) Close the fan cowl doors (Ref. TASK 71-13-00-410-805): - FOR 4030EM1 415AL, 416AR, - FOR 4030EM2 425AL, 426AR. Subtask 12-13-24-862-061 D. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : 701-749, 12-13-24 Page 329 Config-2 Jan 01/02 SROS
FLIGHT CONTROLS - SERVICING ___________________________ TASK 12-13-27-612-801 Oil Replenishing of the THS Actuator (1CS) WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific No specific 0U190363 0U190364
circuit breaker(s) safety clip(s) 1 ACCESS PLATFORM 5M (16 FT) 1 TOOL - OIL FILLING, THS ACTUATOR 1 TOOL - OIL DRAINING, THS ACTUATOR
EFF : ALL 12-13-27 SROS
Page 301 Jan 01/05
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 03-003 Material No. 19-003
USA MIL-PRF-7808 LUBRICATING OIL TURBINE SYNTHETIC BASE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------4
packing
27-44-51 02 -100
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 27-40-00-866-801 29-00-00-864-804 R 12-13-27-991-001
Energize the Ground Service Network De-energize the Ground Service Network Operation of the THS Actuator Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Fig. 301
3. __________ Job Set-up Subtask 12-13-27-860-052 A. Aircraft Maintenance Configuration (1) Move the THS actuator five times fully up and down and then in the 0⁰ position (Ref. TASK 27-40-00-866-801). (2) Energize the ground service network (Ref. TASK 24-42-00-861-801). (3) Make sure that the hydraulic systems are depressurized (Ref. TASK 29-00-00-864-804).
EFF : ALL 12-13-27 SROS
Page 302 Jul 01/02
Subtask 12-13-27-865-050 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU FCPC3 STBY COM 7CE6 R20 721VU FCPC3 STBY MON 7CE5 R19 722VU FCPC 3 7CE3 V42 722VU FCPC 2 NORM 7CE2 V41 722VU FCPC 3 7CE4 V38 742VU FCPC 1 NORM 7CE1 C69 742VU FCPC 1 STBY 11CE K69 Subtask 12-13-27-010-050 C. Put the ACCESS PLATFORM 5M (16 FT) in position below the access door 312AR and open the access door 312AR. 4. Procedure _________ (Ref. Fig. 301/TASK 12-13-27-991-001) NOTE : Wait one hour after movement of the THS Actuator before you do the ____ check of the oil level. Subtask 12-13-27-612-050 A. Oil Replenishing of the THS Actuator WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Remove the manual cranking plug (3) between the two hydraulic motors and remove and discard the packing (4). (2) Remove the cap (1) from the oil fill plug (2) and install the TOOL OIL FILLING, THS ACTUATOR on the oil fill plug (2). R R
(3) Monitor the oil level indicator (5) and fill the THS actuator with OILS (Material No. 03-003), until the quantity is correct. The correct quantity is when the oil level is in the middle position between the MINI and the MAXI marks.
EFF : ALL 12-13-27 SROS
Page 303 Apr 01/02
R
THS Actuator Figure 301/TASK 12-13-27-991-001
EFF : ALL 12-13-27 SROS
Page 304 Apr 01/02
NOTE : The volume between MINI and MAXI indication on the oil level ____ indicator is 0.2 l (0.0528 USgal). (4) If the gearbox oil level is too much, drain the oil which is too much from the gearbox. (a) Remove the drain plug (6) from the gearbox and install the TOOL OIL DRAINING, THS ACTUATOR (0U190364) in the gearbox and let the oil drain until the oil level is correct. (b) Remove the TOOL - OIL DRAINING, THS ACTUATOR (0U190364) from the gearbox and install the drain plug (6). (5) Remove the TOOL - OIL FILLING, THS ACTUATOR and clean the cap (1) with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003). (6) Install the new packing (4) on the manual cranking plug (3) and install the cap (1) and the manual cranking plug (3). 5. Close-up ________ Subtask 12-13-27-865-051 A. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 7CE1, 7CE2, 7CE3, 7CE4, 7CE5, 7CE6, 11CE. Subtask 12-13-27-410-050 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. R
(2) Close the access door 312AR and remove the access platform. (3) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-13-27-860-053 C. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-13-27 SROS
Page 305 Jul 01/06
TASK 12-13-27-612-802 Oil Replenishing of the Flap Power Control Unit (PCU) Gearbox (5000CV) WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No No No No
specific specific specific specific
circuit breaker(s) safety clip(s) 1 CONTAINER 1 L (1/4 USGAL) 1 WARNING NOTICE Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft)
EFF : ALL 12-13-27 SROS
Page 306 Jan 01/05
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 03-003 Material No. 19-003 R
USA MIL-PRF-7808 LUBRICATING OIL TURBINE SYNTHETIC BASE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Expendable Parts
R R R
------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
R
2
R
preformed packing
27-54-51 01 -110
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 27-50-00-866-801 27-50-00-866-802 32-12-00-010-801 32-12-00-410-801 27-54-51-000-801 27-54-51-400-801 12-13-27-991-002
Energize the Ground Service Network De-energize the Ground Service Network Extension of the Flaps on the Ground Retraction of the Flaps on the Ground Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Removal of the Flaps Power Control-Unit (PCU) (5000CV) (for corrective action) Installation of the Flaps Power Control-Unit (PCU) (5000CV) (for corrective action) Fig. 302
3. __________ Job Set-up Subtask 12-13-27-860-054 A. Energize the ground service network (Ref. TASK 24-42-00-861-801).
EFF : ALL 12-13-27 SROS
Page 307 Jan 01/06
INTENTIONALLY BLANK
R 12-13-27 SROS
Page 308 Jul 01/02
Subtask 12-13-27-865-052 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM 10CV X14 722VU SFCC 2 FLAP 2CV T43 742VU SFCC 1 FLAP 1CV L61 Subtask 12-13-27-010-051 C. Get Access (1) Open the right MLG door (Ref. TASK 32-12-00-010-801). (2) Put the CONTAINER 1 L (1/4 USGAL) in position below the flap PCU. (3) Put the WARNING NOTICE in position to tell persons not to operate the flap/slat system. 4. Procedure _________ (Ref. Fig. 302/TASK 12-13-27-991-002) Subtask 12-13-27-612-051 A. Oil Replenishing of the Flap Power Control Unit (PCU) Gearbox WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. R R R
NOTE : After installation of a new PCU (5000CV), extend and retract the ____ flaps before you do the oil replenishing (Ref. TASK 27-50-00-866801) and (Ref. TASK 27-50-00-866-802). (1) Remove the oil-fill plug (1) and remove and discard the preformed packing (2).
EFF : ALL 12-13-27 SROS
Page 309 Oct 01/01
Flap PCU Figure 302/TASK 12-13-27-991-002 EFF : ALL 12-13-27 R SROS
Page 310 Apr 01/01
(2) Slowly add the OILS (Material No. 03-003) to the flap PCU gearbox until it comes out of the oil-fill hole. NOTE : If the added oil quantity is between 50 cm3 (3.05 in.3) and 70 ____ cm3 (4.27 in.3) and there is no leak visible, check the oil level at the next A-Check and top-up as necessary: - if you add up to 50 cm3 (3.05 in.3) replace the PCU, but not later than the next A-Check (Ref. TASK 27-54-51-000-801) and (Ref. TASK 27-54-51-400-801). - if you add more than 50 cm3 (3.05 in.3) replace the PCU before the next 20 flights (Ref. TASK 27-54-51-000-801) and (Ref. TASK 27-54-51-400-801). R R
(3) Clean the oil-fill plug (1) with a clean lint-free cloth, MISCELLANEOUS (Material No. 19-003).
R R R
(4) Apply the OILS (Material No. 03-003) to the new preformed packing (2).
R R R
(5) Install the preformed packing (2) on the oil-fill plug (1) and install the oil-fill plug (1)
R
(6) TORQUE the oil-fill plug (1) to between 2.0 and 2.5 m.daN (14.74 and 18.43 lbf.ft).
R R
(7) Remove the unwanted oil from the area of the oil-fill plug (1) with a lint-free cloth, MISCELLANEOUS (Material No. 19-003).
R R
(8) Make sure that there is no oil leakage at the preformed packing (2). 5. Close-up ________ Subtask 12-13-27-865-053 A. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1CV, 2CV, 10CV.
EFF : ALL 12-13-27 SROS
Page 311 Jan 01/06
Subtask 12-13-27-410-051 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the right MLG door (Ref. TASK 32-12-00-410-801). (3) Remove the access platform(s). (4) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-13-27-860-055 C. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-13-27 R SROS
Page 312 Jan 01/06
TASK 12-13-27-612-803 Oil Replenishing of the Slat Power Control-Unit (PCU) Gearbox (5000CW) WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No No No No No
specific specific specific specific specific
circuit breaker(s) safety clip(s) 1 ACCESS PLATFORM 2M (6 FT) 1 CONTAINER 1 L (1/4 USGAL) 1 WARNING NOTICE Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft)
EFF : ALL 12-13-27 SROS
Page 313 Jan 01/05
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 03-003 Material No. 19-003
USA MIL-PRF-7808 LUBRICATING OIL TURBINE SYNTHETIC BASE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------2
preformed packing
27-84-03 01 -320
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R R
24-42-00-861-801 24-42-00-862-801 53-35-13-000-802 53-35-13-400-802 27-84-51-000-801 27-84-51-400-801 12-13-27-991-003
Energize the Ground Service Network De-energize the Ground Service Network Removal of the Belly Fairing Access Panels Installation of the Belly Fairing Access Panels Removal of the Slat Power Control-Unit (PCU) (5000CW) (for corrective action) Installation of the Slat Power Control-Unit (PCU) (5000CW) (for corrective action) Fig. 303
3. __________ Job Set-up Subtask 12-13-27-860-056 A. Energize the ground service network (Ref. TASK 24-42-00-861-801).
EFF : ALL 12-13-27 SROS
Page 314 Jul 01/02
Subtask 12-13-27-865-054 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM AVAIL 10CW X13 722VU SFCC 2 SLAT 2CW V40 742VU SFCC 1 SLAT 1CW L62 Subtask 12-13-27-010-052 C. Get Access (1) Put the WARNING NOTICE in position to tell persons not to operate the flap/slat system. (2) Put the ACCESS PLATFORM 2M (6 FT) in position below the access panel 195CB and remove the access panel 195CB (Ref. TASK 53-35-13-000-802). (3) Put the CONTAINER 1 L (1/4 USGAL) in position below the slat PCU. 4. Procedure _________ (Ref. Fig. 303/TASK 12-13-27-991-003) Subtask 12-13-27-612-052 R
A. Oil Replenishing of Slat Power Control Unit (PCU) Gearbox WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Remove the oil-fill plug (1) and remove and discard the preformed packing (2). (2) Slowly add the OILS (Material No. 03-003) to the slat PCU gearbox until it comes out of the oil-fill hole. NOTE : If the added oil quantity is between 50 cm3 (3.05 in.3) and 70 ____ cm3 (4.27 in.3) and there is no leak visible, check the oil level at the next A-Check and top-up as necessary: - if you add up to 50 cm3 (3.05 in.3) replace the PCU, but not later than the next A-Check (Ref. TASK 27-84-51-000-801) and (Ref. TASK 27-84-51-400-801), - if you add more than 50 cm3 (3.05 in.3) replace the PCU before the next 20 flights (Ref. TASK 27-84-51-000-801) and (Ref. TASK 27-84-51-400-801).
EFF : ALL 12-13-27 SROS
Page 315 Jul 01/06
Slat PCU Figure 303/TASK 12-13-27-991-003 EFF : ALL 12-13-27 R SROS
Page 316 Jul 01/01
(3) Clean the oil-fill plug (1) with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003) and apply the OILS (Material No. 03-003) to the new preformed packing (2). (4) Install the preformed packing (2) on the oil-fill plug (1) and install the oil-fill plug (1) (5) TORQUE the oil-fill plug (1) to between 2.0 and 2.5 m.daN (14.74 and 18.43 lbf.ft) and remove the unwanted oil from near the oil-fill plug (1) with a lint-free cloth MISCELLANEOUS (Material No. 19-003). (6) Examine the preformed packing (2) for signs of oil leakage. NOTE : Leaks are not permitted. ____ 5. Close-up ________ Subtask 12-13-27-865-055 A. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1CW, 2CW, 10CW. Subtask 12-13-27-410-052 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panel 195CB (Ref. TASK 53-35-13-400-802). (3) Remove the access platform(s). (4) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-13-27-860-057 C. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-13-27 R SROS
Page 317 Apr 01/02
TASK 12-13-27-612-804 Drain and Refill the Rotary Actuators WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Refer to the MPD TASK: 275400-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R R
No No No No No No No No
specific specific specific specific specific specific specific specific
1 2 1 1 1
No specific 1X56176802
1
circuit breaker(s) safety clip(s) TRANSPARENT TUBE WITH A MALE 3/8 in. FITTING ACCESS PLATFORM 3M (10 FT) CONTAINER 3 L(3/4 USGAL) GUN - GREASE, DIA 3/8 IN FEMALE ADAPTER HOSE - HIGH PRESSURE, DIA 3/8 MALE FITTINGS WARNING NOTICE Torque Wrench : range 0.00 to 1.20 m.daN (0.00 to 9.00 lbf.ft) Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft) FILLER
EFF : ALL 12-13-27 SROS
Page 318 Apr 01/05
------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------98D27803000000 FOR FIN 5122CV 98F29208217000
1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER 1 SAFETY PIN - RAT
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 04-022
USA MIL-PRF-81322 SYNTHE.HYDROCARBON GREASE HIGH PRESSURE (Ref. 20-31-00)
Material No. 04-025 Material No. 19-003
LUBRICANT, SEMIFLUID (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------R
2 2
packing packing
27-54-59 04 -040 27-54-59 04 -040A
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 57-56-11-000-807 57-56-11-400-807 27-50-00-866-801 27-50-00-866-802
Energize the Ground Service Network De-energize the Ground Service Network Removal of the Movable Flap Track Fairings Nos. 2 thru 5 for Access Installation of the Movable Flap Track Fairings Nos. 2 thru 5 after Access Extension of the Flaps on the Ground (for corrective action) Retraction of the Flaps on the Ground (for corrective action)
EFF : ALL 12-13-27 SROS
Page 319 Jul 01/06
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------27-54-59-000-801 27-54-59-000-802 27-54-59-400-801 27-54-59-400-802
Removal of the Rotary Actuator (5009CV, 5087CV) (for corrective action) Removal of the Rotary Actuator (5024CV, 5034CV, 5044CV, 5055CV, 5102CV, 5112CV, 5122CV, 5133CV) (for corrective action) Installation of the Rotary Actuator (5009CV, 5087CV) (for corrective action) Installation of the Rotary Actuator (5024CV, 5034CV, 5044CV, 5055CV, 5102CV, 5112CV, 5122CV, 5133CV) (for corrective action) Fig. 304 Fig. 305
12-13-27-991-004 12-13-27-991-007 FOR FIN 5009CV, 5087CV 27-50-00-866-801 Extension of the Flaps on the Ground 27-50-00-866-802 Retraction of the Flaps on the Ground 32-12-00-010-801 Open the MLG Doors for Maintenance 32-12-00-410-801 Close the MLG Doors after Maintenance FOR FIN 5122CV 29-24-00-081-801 Removal of the RAT Safety Pin 29-24-00-481-801 Installation of the RAT Safety Pin FOR FIN 5024CV, 5034CV, 5044CV, 5055CV, 5102CV, 5112CV, 5122CV, 5133CV 27-50-00-866-802 Retraction of the Flaps on the Ground 3. __________ Job Set-up Subtask 12-13-27-860-050 A. Aircraft Maintenance Configuration (1) If the ambient temperature is aircraft is on the ground for least 15 time to increase the more than 20 times (Ref. TASK 00-866-802).
below 15 DEG.C (59.00 DEG.F) or the less than 10 hours, cycle the flaps at temperature. But do not cycle the flaps 27-50-00-866-801) and (Ref. TASK 27-50-
(2) Energize the ground service network (Ref. TASK 24-42-00-861-801).
EFF : ALL 12-13-27 R SROS
Page 320 Apr 01/02
Subtask 12-13-27-010-053 B. Get Access (1) FOR 5009CV, 5087CV open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Put the ACCESS PLATFORM 3M (10 FT) in position below the applicable access panel. (3) FOR 5122CV - install the SAFETY PIN - RAT (Ref. TASK 29-24-00-481-801). (4) Remove the applicable movable 000-807): - FOR 5024CV, 5102CV remove the No. 2 flap track - FOR 5034CV, 5112CV remove the No. 3 flap track - FOR 5044CV, 5122CV remove the No. 4 flap track - FOR 5055CV, 5133CV remove the No. 5 flap track
flap track fairing (Ref. TASK 57-56-11fairing, fairing, fairing, fairing.
(5) Put a CONTAINER 3 L(3/4 USGAL) in position below the applicable rotary actuator. Subtask 12-13-27-860-062 C. Aircraft Maintenance Configuration
R
(1) Put the flaps in position: - FOR 5024CV, 5034CV, 5044CV, 5055CV, 5102CV, 5112CV, 5122CV, 513 make sure that the flaps are retracted (Ref. TASK 27-50-00-866-802) - FOR 5009CV, 5087CV extend the flaps to the position 2 (Ref. TASK 27-50-00-866-801).
R R
NOTE : The two different flap positions are necessary for the correct ____ access to the applicable actuator.
R R
(2) Attach the LOCKING TOOL - FLAP/SLAT CONTROL LEVER to the flap/slat control lever on the panel 114VU.
R R
(3) Put the WARNING NOTICE in position on the panel 114VU to tell persons not to operate the flap/slat controls.
EFF : ALL 12-13-27 SROS
Page 321 Jan 01/06
Subtask 12-13-27-865-056 D. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM 10CV X14 722VU SFCC 2 FLAP 2CV T43 742VU SFCC 1 FLAP 1CV L61 4. Procedure _________ (Ref. Fig. 304/TASK 12-13-27-991-004, 305/TASK 12-13-27-991-007) NOTE : The SEMIFLUID must have a temperature of at least 15 DEG.C (59 DEG.F) ____ but not more than 40 DEG.C (104 DEG.F). If the temperature is too high the SEMIFLUID becomes too thin and will not coat the actuator gears correctly. R
NOTE : Before you use the SEMIFLUID, you must stir it fully. This make sure ____ that the SEMIFLUID has its original viscosity. NOTE : To drain and fill the 10 actuators, you need approximately 25 l (6.6 ____ USgal) SEMIFLUID. Subtask 12-13-27-612-053 A. Drain and refill the Rotary Actuator to confirm the SEMIFLUID Level WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Clean all the rotary actuator (3). (2) Draining (a) Remove the top plugs (1) and the bottom plug (6). Some SEMIFLUID may flow through the bottom hole. (b) Examine the packing (2) and replace them if necessary packing (2). (c) When the flow of SEMIFLUID stops, install the bottom plug (6) but do not tighten at this time.
EFF : ALL 12-13-27 SROS
Page 322 Jul 01/06
Flap Rotary Actuator Figure 304/TASK 12-13-27-991-004 EFF : ALL 12-13-27 R SROS
Page 323 Jul 01/01
R
Rotary Actuator Filling Set-up Figure 305/TASK 12-13-27-991-007
EFF : ALL 12-13-27 SROS
Page 324 Jul 01/01
(3) Refill (a) Install a TRANSPARENT TUBE WITH A MALE 3/8 in. FITTING on the upper hole and put a CONTAINER 3 L(3/4 USGAL) in position below the tube for the used fluid. (b) Remove the plug (5) with the lubrication plate and install the FILLER (1X56176802) (4) in the actuator (3). Only apply hand force for the installation of the FILLER (4). NOTE : It is recommended to use a HOSE - HIGH PRESSURE, DIA 3/8 ____ MALE FITTINGS with between the grease gun and the FILLER. (c) Make sure that the SEMIFLUID has a temperature of at least 15 DEG.C (59 DEG.F) but not more than 40 DEG.C (104 DEG.F). If the temperature is too high the SEMIFLUID becomes too thin and will not coat the actuator gears correctly. R
(d) Attach a GUN - GREASE, DIA 3/8 IN FEMALE ADAPTER with the flexible HP tube on the FILLER (4) and fill the rotary actuator with SEMIFLUID GREASE COMMON GREASE (Material No. 04-025) until: - for the flap drive station 1, 4 and 5, approx. 500ml, - for the flap drive station 2 and 3, approx. 1000ml, of the SEMIFLUID flows through the top hole and the transparent tube into the container. During the filling of the rotary actuator, examine the rotary actuator for leaks. (e) Disconnect the grease gun and the HP tube from the FILLER (4) and remove the FILLER (1X56176802) (4) from the actuator (3). (f) Disconnect the transparent tube from the upper hole. (g) Apply COMMON GREASE (Material No. 04-022) to the threads of the plug (5) and install the plug (5) with the lubrication plate on the actuator (3). (h) TORQUE the plug (5) to between 0.68 and 0.92 m.daN (60.17 and 81.41 lbf.in). (i) Remove the bottom plug (6) and monitor the fluid that comes out. (j) Apply COMMON GREASE (Material No. 04-022) to the thread of the plugs (1) and (6).
EFF : ALL 12-13-27 SROS
Page 325 Apr 01/05
(k) When the flow of fluid decreases and only drops come out, install the bottom plug (6). NOTE : The remaining SEMIFLUID is sufficient to lubricate the ____ actuator. (l) Install the top plug (1). (m) TORQUE the top and the bottom plugs (1) and (6) to between 1.45 and 1.95 m.daN (10.69 and 14.38 lbf.ft). (n) Remove the unwanted fluid from the actuator (3) with a cloth MISCELLANEOUS (Material No. 19-003). (4) Examine the actuator (3) for leakage. NOTE : If leakage is detected, do the subsequent steps: ____ - make sure that all three plugs are tight, - clean the actuator, - examine the actuator for leakage again. If there is no significant leakage, no further maintenance action is necessary. If there is still a leakage more than 1 drop thin liquid fluid per 1 hour or any else than thin liquid fluid (i.e. semifluid), replace the rotary actuator with the next C check (Ref. TASK 27-54-59-000-801) and (Ref. TASK 2754-59-400-801) or (Ref. TASK 27-54-59-000-802) and (Ref. TASK 27-54-59-400-802). 5. Close-up ________ Subtask 12-13-27-865-057 A. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1CV, 2CV, 10CV. Subtask 12-13-27-410-053 B. Close Access (1) FOR 5009CV, 5087CV close the MLG doors (Ref. TASK 32-12-00-410-801). (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 12-13-27 R SROS
Page 326 Oct 01/01
(3) Install the applicable movable 11-400-807): - FOR 5024CV, 5102CV install the No. 2 flap track - FOR 5034CV, 5112CV install the No. 3 flap track - FOR 5044CV, 5122CV install the No. 4 flap track - FOR 5055CV, 5133CV install the No. 5 flap track
flap track fairing (Ref. TASK 57-56fairing, fairing, fairing, fairing.
(4) FOR 5122CV - remove the SAFETY PIN - RAT (Ref. TASK 29-24-00-081-801). (5) Remove the access platform(s). (6) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-13-27-860-051 C. Aircraft Maintenance Configuration (1) Remove the warning notice(s). (2) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever on panel 114VU. (3) FOR 5009CV, 5087CV retract the flaps (Ref. TASK 27-50-00-866-802). (4) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-13-27 R SROS
Page 327 Oct 01/01
TASK 12-13-27-612-805 Oil Replenishing of the Flap System Torque Limiter (5003CV, 5081CV) WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No No No No
specific specific specific specific
98D27803000000
circuit breaker(s) safety clip(s) 1 CAN - OIL 1 CONTAINER 1 L (1/4 USGAL) Torque Wrench : range 1.00 to 10.00 m.daN (8.00 to 75.00 lbf.ft) 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
EFF : ALL 12-13-27 SROS
Page 328 Jan 01/05
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R
Material No. 02-001 Material No. 02-001A Material No. 19-003
USA MIL-H-5606 OIL, HYDRAULICPETROLEUM FLUID (Ref. 20-31-00) USA MIL-H-6083D OIL, HYDRAULICPETROLEUM FLUID (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------2
packing
27-54-42 01 -020
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 27-50-00-866-802 32-12-00-010-801 32-12-00-410-801 27-54-42-000-801 27-54-42-400-801 12-13-27-991-005
Energize the Ground Service Network De-energize the Ground Service Network Retraction of the Flaps on the Ground Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Removal of the System Torque Limiter (5003CV, 5081CV) (for corrective action) Installation of the System Torque Limiter (5003CV, 5081CV) (for corrective action) Fig. 306
EFF : ALL 12-13-27 SROS
Page 329 Jan 01/02
3. __________ Job Set-up Subtask 12-13-27-860-058 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). (2) Make sure that the flaps are retracted (Ref. TASK 27-50-00-866-802). (3) Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER on the slat/flap control lever. Subtask 12-13-27-865-058 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM 10CV X14 722VU SFCC 2 FLAP 2CV T43 742VU SFCC 1 FLAP 1CV L61 Subtask 12-13-27-010-059 C. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Put the CONTAINER 1 L (1/4 USGAL) in position below the system torque limiter. 4. Procedure _________ (Ref. Fig. 306/TASK 12-13-27-991-005) Subtask 12-13-27-612-054 R
A. Oil Replenishing of the Flap System Torque-Limiter WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES.
EFF : ALL 12-13-27 SROS
Page 330 Jul 01/06
Flap System Torque Limiter Figure 306/TASK 12-13-27-991-005 EFF : ALL 12-13-27 R SROS
Page 331 Jul 01/01
(1) Remove the oil-fill plug (1) and remove and discard the packing (2). (2) Use a CAN - OIL and slowly add the HYDRAULIC FLUIDS (Material No. 02001A) to the flap system torque limiter until it comes out of the oil-fill hole. NOTE : HYDRAULIC FLUIDS (Material No. 02-001A) is preferable, but ____ HYDRAULIC FLUIDS (Material No. 02-001) can also be used. R R R R R R R R R
NOTE : If the added oil quantity is between 50 cm3 (3.05 in.3) and 70 ____ cm3 (4.27 in.3) and there is no leak visible, check the oil level at the next A-Check and top-up as necessary: - if you add up to 50 cm3 (3.05 in.3) replace the STL, but not later than the next A-Check (Ref. TASK 27-54-42-000-801) and (Ref. TASK 27-54-42-400-801), - if you add more than 50 cm3 (3.05 in.3) replace the STL before the next 20 flights (Ref. TASK 27-54-42-000-801) and (Ref. TASK 27-54-42-400-801). (3) Clean the oil-fill plug (1) with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003). (4) Apply the HYDRAULIC FLUIDS (Material No. 02-001A) to the new packing (2) and install the packing (2) on the oil-fill plug (1). (5) Install the oil-fill plug (1) in the system torque limiter.
R R
(6) TORQUE the oil-fill plug (1) to between 3.05 and 3.73 m.daN (22.49 and 27.50 lbf.ft). (7) Remove the unwanted oil from near the oil-fill plug (1) with a clean cloth MISCELLANEOUS (Material No. 19-003). (8) Examine the oil fill plug (1) for signs of oil leakage. NOTE : Leaks are not permitted. ____ 5. Close-up ________ Subtask 12-13-27-865-059 A. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1CV, 2CV, 10CV.
EFF : ALL 12-13-27 SROS
Page 332 Jul 01/02
Subtask 12-13-27-410-054 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the MLG doors (Ref. TASK 32-12-00-410-801). (3) Remove the access platform(s). (4) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-13-27-860-059 C. Put the Aircraft back to its Initial Configuration (1) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever. (2) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-13-27 R SROS
Page 333 Oct 01/01
TASK 12-13-27-612-806 R
Oil Replenishing of the Slat System Torque Limiter (5009CW, 5069CW) WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No
specific specific specific specific specific
98D27803000000
circuit breaker(s) safety clip(s) 1 ACCESS PLATFORM 2M (6 FT) 1 CAN - OIL 1 CONTAINER 1 L (1/4 USGAL) Torque Wrench : range 1.00 to 10.00 m.daN (8.00 to 75.00 lbf.ft) 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
EFF : ALL 12-13-27 SROS
Page 334 Jul 01/06
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R
Material No. 02-001 Material No. 02-001A Material No. 19-003
USA MIL-H-5606 OIL, HYDRAULICPETROLEUM FLUID (Ref. 20-31-00) USA MIL-H-6083D OIL, HYDRAULICPETROLEUM FLUID (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------2
packing
27-84-42 01 -020
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801
Energize the Ground Service Network De-energize the Ground Service Network
53-35-13-000-802 53-35-13-400-802 27-80-00-866-802
Removal of the Belly Fairing Access Panels Installation of the Belly Fairing Access Panels Retraction of the Slats on the Ground (for corrective action) Removal of the System Torque Limiter (5009CW, 5069CW) (for corrective action) Installation of the System Torque Limiter (5009CW, 5069CW) (for corrective action) Fig. 307
R R R
27-84-42-000-801 27-84-42-400-801 R
12-13-27-991-006-A
EFF : ALL 12-13-27 SROS
Page 335 Jan 01/02
3. __________ Job Set-up Subtask 12-13-27-860-060 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). R
(2) Make sure that the slats are retracted (Ref. TASK 27-80-00-866-802). (3) Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER on the slat/flap control lever. Subtask 12-13-27-865-060 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM AVAIL 10CW X13 722VU SFCC 2 SLAT 2CW V40 742VU SFCC 1 SLAT 1CW L62 Subtask 12-13-27-010-061 C. Get Access (1) Put the ACCESS PLATFORM 2M (6 FT) in position below the access panel 193FB. (2) Remove the access panel 193FB (Ref. TASK 53-35-13-000-802). (3) Put the CONTAINER 1 L (1/4 USGAL) in position below the system torque limiter.
EFF : ALL 12-13-27 SROS
Page 336 Jan 01/02
4. Procedure _________ (Ref. Fig. 307/TASK 12-13-27-991-006-A) Subtask 12-13-27-612-055 R
A. Oil Replenishing of the Slat System Torque-Limiter WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Remove the oil-fill plug (1) and remove and discard the packing (2). (2) Use a CAN - OIL Slowly add the HYDRAULIC FLUIDS (Material No. 02001A) to the slat system torque limiter until it comes out of the oil-fill hole. NOTE : HYDRAULIC FLUIDS (Material No. 02-001A) is preferable, but ____ HYDRAULIC FLUIDS (Material No. 02-001) can also be used. NOTE : If the added oil quantity is between 50 cm3 (3.05 in.3) and 70 ____ cm3 (4.27 in.3) and there is no leak visible, check the oil level at the next A-Check and top-up as necessary: - if you add up to 50 cm3 (3.05 in.3) replace the STL, but not later than the next A-Check (Ref. TASK 27-84-42-000-801) and (Ref. TASK 27-84-42-400-801), - if you add more than 50 cm3 (3.05 in.3) replace the STL before the next 20 flights (Ref. TASK 27-84-42-000-801) and (Ref. TASK 27-84-42-400-801). (3) Clean the oil-fill plug (1) with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003). (4) Apply the HYDRAULIC FLUIDS (Material No. 02-001A) to the new packing (2) and install the packing (2) on the oil-fill plug (1) (5) Install the oil-fill plug (1) in the system torque limiter. (6) TORQUE the oil-fill plug (1) to between 3.05 and 3.73 m.daN (22.49 and 27.50 lbf.ft). (7) Remove the unwanted oil from near the oil-fill plug (1) with a clean cloth.
EFF : ALL 12-13-27 SROS
Page 337 Jul 01/06
R R
Slat System Torque Limiter Figure 307/TASK 12-13-27-991-006-A
EFF : ALL 12-13-27 SROS
Page 338 Jan 01/02
(8) Examine the oil fill plug (1) for signs of oil leakage. NOTE : Leaks are not permitted. ____ 5. Close-up ________ Subtask 12-13-27-865-061 A. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1CW, 2CW, 10CW. Subtask 12-13-27-410-055 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panel 193FB (Ref. TASK 53-35-13-400-802) and remove the access platform. (3) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-13-27-860-061 C. Put the Aircraft back to its Initial Configuration (1) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever. (2) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-13-27 R SROS
Page 339 Jan 01/02
**ON A/C 002-049, 202-249, 252-252, 255-299, 301-399, 451-499, 701-749, TASK 12-13-27-612-807 R
Semi-Fluid Sampling and Replenishing of the Input Gearbox (5007CV, 5022CV, 5032CV, 5042CV, 5053CV, 5085CV, 5100CV, 5110CV, 5120CV, 5131CV) WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Self Explanatory
EFF : 002-049, 202-249, 252-252, 255-299, 12-13-27 301-399, 451-499, 701-749, SROS
Page 340 Jan 01/06
2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No No
specific specific specific specific specific specific specific specific specific
1 1 1
circuit breaker(s) safety clip(s) container commercial 50 ml GREASE GUN THREAD ADAPTER (0.500-20UNF) TRANSPARENT TUBE WITH A MALE 3/8 in. FITTING ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE CONTAINER 1 L (1/4 USGAL) WARNING NOTICE Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft) LOCKING TOOL - FLAP/SLAT CONTROL LEVER
98D27803000000 FOR FIN 5120CV 98F29208217000
1
1 SAFETY PIN - RAT
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 04-025 Material No. 19-003
LUBRICANT, SEMIFLUID (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------2
packing
27-54-57 01 -020
R EFF : 002-049, 202-249, 252-252, 255-299, 12-13-27 301-399, 451-499, 701-749, SROS
Page 341 Jul 01/05
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 27-50-00-866-801 32-12-00-010-801 32-12-00-410-801 57-56-11-000-807 57-56-11-400-807 27-50-00-866-801 27-50-00-866-802 12-13-27-991-008 FOR FIN 5120CV 29-24-00-081-801 29-24-00-481-801 FOR FIN 5009CV, 5087CV 27-50-00-866-802
Energize the Ground Service Network De-energize the Ground Service Network Extension of the Flaps on the Ground Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Removal of the Movable Flap Track Fairings Nos. 2 thru 5 for Access Installation of the Movable Flap Track Fairings Nos. 2 thru 5 after Access Extension of the Flaps on the Ground (for corrective action) Retraction of the Flaps on the Ground (for corrective action) Fig. 308 Removal of the RAT Safety Pin Installation of the RAT Safety Pin Retraction of the Flaps on the Ground
3. __________ Job Set-up Subtask 12-13-27-860-070 A. Aircraft Maintenance Configuration (1) If the ambient temperature is aircraft is on the ground for least 15 time to increase the more than 20 times (Ref. TASK 00-866-802).
below 15 DEG.C (59.00 DEG.F) or the less than 10 hours, cycle the flaps at temperature. But do not cycle the flaps 27-50-00-866-801) and (Ref. TASK 27-50-
(2) Fully extend the flaps (Ref. TASK 27-50-00-866-801) and install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000). (3) Energize the ground service network (Ref. TASK 24-42-00-861-801). (4) Put WARNING NOTICE in position to tell persons not to operate the slat/flap system.
R EFF : 002-049, 202-249, 252-252, 255-299, 12-13-27 301-399, 451-499, 701-749, SROS
Page 342 Jul 01/05
Subtask 12-13-27-865-069 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM 10CV X14 722VU SFCC 2 FLAP 2CV T43 742VU SFCC 1 FLAP 1CV L61 Subtask 12-13-27-010-068 C. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801): - FOR 5007CV open 734, - FOR 5085CV open 744. (2) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position. R
(3) FOR 5120CV - install the SAFETY PIN - RAT (Ref. TASK 29-24-00-481-801). (4) Remove the access panels: - FOR 5022CV remove 573BB, 573FB, 531EL, - FOR 5032CV remove 574BB, 574CB, 532EL, - FOR 5042CV remove 574EB, 574FB, 533EL, - FOR 5053CV remove 574KB, 574LB, 534EL, - FOR 5100CV remove 673BB, 673FB, 631ER, - FOR 5110CV remove 674BB, 674CB, 632ER, - FOR 5120CV remove 674EB, 674FB, 633ER, - FOR 5131CV remove 674MB, 674LB, 634ER. (5) Remove the related flap track fairing (Ref. TASK 57-56-11-000-807).
R EFF : 002-049, 202-249, 252-252, 255-299, 12-13-27 301-399, 451-499, 701-749, SROS
Page 343 Jul 01/05
4. Procedure _________ (Ref. Fig. 308/TASK 12-13-27-991-008) Subtask 12-13-27-612-058 R
A. Semi-Fluid Sampling and Replenishing of the Input Gearbox WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Clean the input gearbox. (2) Put the CONTAINER 1 L (1/4 USGAL) in position below the input gearbox (3). (3) Remove the top plug (1) and the bottom plug (1) and let at least 20 cm3 (1.22 in.3) of the first SEMIFLUID into a container commercial 50 ml. NOTE : If the SEMIFLUID does not drain, apply a pressure up to 7 psi ____ (0.4826 bar) to the top plug. (4) Let the remaining SEMIFLUID drain into the container. (5) When the flow of SEMIFLUID stops, install the THREAD ADAPTER (0.50020UNF) (4) in the lower hole of the actuator (3). Only apply hand force for the installation of the THREAD ADAPTER (4). (6) Sampling (a) Put a label with the subsequent information on the sample container: - P/N and Serial No. of the affected input gearbox, - sample date, - date of installation of the input gearbox, - wing position (station) of the input gearbox, - number of cycles/flight hours of the input gearbox. (b) Send the sample to any Laboratory for analysis for water content. NOTE : The analysis is in accordance with Karl Fischer-Direct ____ Method; ASTM D1744.If the water content in the SEMIFLUID is more than 12%, the input gearbox must be replaced within the next 100 flights latest.
EFF : 002-049, 202-249, 252-252, 255-299, 12-13-27 301-399, 451-499, 701-749, SROS
Page 344 Jul 01/06
R
Flap Input Gearbox Figure 308/TASK 12-13-27-991-008
EFF : 002-049, 202-249, 252-252, 255-299, 12-13-27 301-399, 451-499, 701-749, SROS
Page 345 Jul 01/06
(7) Examine the packings (2) and replace them if necessary packing (2). (8) Install a TRANSPARENT TUBE WITH A MALE 3/8 in. FITTING on the upper hole and put a CONTAINER 1 L (1/4 USGAL) in position below the tube for the used fluid. (9) Make sure that the SEMIFLUID has a temperature of at least 15 DEG.C (59 DEG.F) but not more than 40 DEG.C (104 DEG.F). If the temperature is too high the SEMIFLUID becomes too thin and will not coat the gearbox gears correctly. R R
(10) Attach a GREASE GUN on the THREAD ADAPTER (4) and fill the input gearbox with SEMIFLUID GREASE COMMON GREASE (Material No. 04-025) until the SEMIFLUID flows through the top hole and the transparent tube into the container. During the filling of the input gearbox, examine the input gearbox for leaks. (11) Disconnect the grease gun and the THREAD ADAPTER (4) from the input gearbox (3) and let approx. 0.175 l (0.0462 USgal) SEMIFLUID drain into the container. (12) Install the lower plug (1) with the O-ring (2). (13) Disconnect the transparent tube from the upper hole and install the top plug (1) with the O-ring (2). (14) TORQUE the plugs (1) to 1.69 m.daN (12.46 lbf.ft). (a) Remove the unwanted fluid from the actuator (3) with a cloth MISCELLANEOUS (Material No. 19-003). (15) Examine the actuator (3) for leakage. NOTE : If leakage is detected, do the subsequent steps: ____ - make sure that all plugs are tight, - clean the actuator, - examine the actuator for leakage again. (16) Remove the container.
EFF : 002-049, 202-249, 252-252, 255-299, 12-13-27 301-399, 451-499, 701-749, SROS
Page 346 Jul 01/06
5. Close-up ________ Subtask 12-13-27-010-069 A. Close Access (1) Install the flap track fairing (Ref. TASK 57-56-11-400-807). (2) Close the MLG doors (Ref. TASK 32-12-00-410-801). - FOR 5007CV close 734, - FOR 5085CV close 744. (3) Install the access panels: - FOR 5022CV install 573BB, 573FB, 531EL, - FOR 5032CV install 574BB, 574CB, 532EL, - FOR 5042CV install 574EB, 574FB, 533EL, - FOR 5053CV install 574KB, 574LB, 534EL, - FOR 5100CV install 673BB, 673FB, 631ER, - FOR 5110CV install 674BB, 674CB, 632ER, - FOR 5120CV install 674EB, 674FB, 633ER, - FOR 5131CV install 674MB, 674LB, 634ER. R
(4) FOR 5120CV - remove the SAFETY PIN - RAT (Ref. TASK 29-24-00-081-801). (5) Remove the access platform(s). (6) De-energize the ground service network (Ref. TASK 24-42-00-862-801). Subtask 12-13-27-865-070 B. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1CV, 2CV, 10CV.
R EFF : 002-049, 202-249, 252-252, 255-299, 12-13-27 301-399, 451-499, 701-749, SROS
Page 347 Jul 01/05
Subtask 12-13-27-860-071 C. Put the Aircraft back to its Initial Configuration (1) Remove the warning notice(s). (2) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever on panel 114VU. R
(3) FOR 5009CV, 5087CV retract the flaps (Ref. TASK 27-50-00-866-802). (4) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
R EFF : 002-049, 202-249, 252-252, 255-299, 12-13-27 301-399, 451-499, 701-749, SROS
Page 348 Jul 01/05
**ON A/C ALL TASK 12-13-27-680-801 Oil Draining of the Flap/Slat PCU (5000CV, 5000CW) WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific No specific No specific FOR FIN 5000CW No specific No specific
circuit breaker(s) safety clip(s) 1 CONTAINER 1 L (1/4 USGAL) 1 WARNING NOTICE 1 ACCESS PLATFORM 2M (6 FT) Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft)
EFF : ALL 12-13-27 SROS
Page 349 Jan 01/05
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------FOR FIN 5000CW Material No. 19-010
R
USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
C. Expendable Parts
R R R
------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
R R R R
FOR FIN 5000CV 4 preformed packing FOR FIN 5000CW 4 preformed packing
R
D. Referenced Information
27-54-51 01 -110 27-84-51 03 -020
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 12-13-27-991-002 12-13-27-991-003 FOR FIN 5000CV 12-13-27-612-802 32-12-00-010-801 32-12-00-410-801 FOR FIN 5000CW 12-13-27-612-803 53-35-13-000-802 53-35-13-400-802
Energize the Ground Service Network De-energize the Ground Service Network Fig. 302 Fig. 303 Oil Replenishing of the Flap Power Control Unit (PCU) Gearbox (5000CV) Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Oil Replenishing of the Slat Power Control-Unit (PCU) Gearbox (5000CW) Removal of the Belly Fairing Access Panels Installation of the Belly Fairing Access Panels
EFF : ALL 12-13-27 SROS
Page 350 Jan 01/06
3. __________ Job Set-up Subtask 12-13-27-860-063 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-27-865-063 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 5000CV 721VU SFCC 1 NORM 10CV X14 722VU SFCC 2 FLAP 2CV T43 742VU SFCC 1 FLAP 1CV L61 FOR 5000CW 721VU SFCC 1 NORM AVAIL 10CW X13 722VU SFCC 2 SLAT 2CW V40 742VU SFCC 1 SLAT 1CW L62 Subtask 12-13-27-010-063 C. Get Access (1) Put the WARNING NOTICE in position to tell persons not to operate the flap/slat system. (2) FOR 5000CV (a) Open the right MLG door (Ref. TASK 32-12-00-010-801). (3) FOR 5000CW (a) Put the ACCESS PLATFORM 2M (6 FT) in position below the access panel 195CB. (b) Remove the access panel 195CB (Ref. TASK 53-35-13-000-802). (4) Put the CONTAINER 1 L (1/4 USGAL) in position below the related PCU.
EFF : ALL 12-13-27 R SROS
Page 351 Jan 01/06
4. Procedure _________ (Ref. Fig. 302/TASK 12-13-27-991-002, 303/TASK 12-13-27-991-003) Subtask 12-13-27-680-050 A. Oil Drainage of the Flap/Slat PCU. WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Remove the oil-fill plug (1) and remove and discard the preformed packing (2). (2) Remove and discard the lockwire from the oil-drain plug (3). (3) Remove the oil-drain plug (3) and remove and discard the preformed packing (4) and let the oil drain into an empty container. R R
(4) FOR 5000CV
R R R
(a) When the oil is fully drained, install the new preformed packing (4) and the oil-drain plug (3) in the flap PCU.
R R
(b) Measure the quantity of the oil.
R
1 _
Make sure that the drained oil quantity is not less than 100 cm3 (6.10 in.3). NOTE : If the oil quantity is less than 100 cm3 (6.10 in.3), ____ replace the PCU within the next 20 flights.
R R
(5) FOR 5000CW
R R
(a) When the oil is fully drained, install the new preformed packing (4) and the oil-drain plug (3) in the slat PCU.
R
(6) TORQUE the oil-drain plug (3) to between 2 and 2.5 m.daN (14.74 and 18.43 lbf.ft).
R
(7) Safety the oil-drain plug (3) with the lockwire, MISCELLANEOUS (Material No. 19-010).
EFF : ALL 12-13-27 SROS
Page 352 Jan 01/06
Subtask 12-13-27-612-056 R
B. Do the oil replenishing of the PCU: - FOR 5000CV (Ref. TASK 12-13-27-612-802), - FOR 5000CW (Ref. TASK 12-13-27-612-803). 5. Close-up ________ Subtask 12-13-27-865-064 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 5000CV 1CV, 2CV, 10CV, FOR 5000CW 1CW, 2CW, 10CW. Subtask 12-13-27-410-056 B. Close Access (1) Remove the container. (2) Remove the warning notice(s). (3) Make sure that the work area is clean and clear of tools and other items. (4) FOR 5000CV (a) Close the right MLG door (Ref. TASK 32-12-00-410-801). (5) FOR 5000CW (a) Install the access panel 195CB (Ref. TASK 53-35-13-400-802). (6) Remove the access platform(s). (7) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-13-27-860-064 C. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-13-27 SROS
Page 353 Jul 01/06
TASK 12-13-27-680-802 Oil Draining of the Flap/Slat System Torque Limiter (5003CV, 5081CV, 5009CW, 5069CW) WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. 1. __________________ Reason for the Job Self Explanatory
EFF : ALL 12-13-27 R SROS
Page 354 Jan 01/03
2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific 98D27803000000 FOR FIN 5000CW No specific
circuit breaker(s) safety clip(s) 1 ACCESS PLATFORM 2M (6 FT) 1 CONTAINER 1 L (1/4 USGAL) 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------FOR FIN 5000CW Material No. 19-010
USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------R R R
FOR FIN 5000CV 4 plug preformed packing
27-54-42 01 -020
FOR FIN 5000CW 4 plug preformed packing
27-84-42 01 -020
EFF : ALL 12-13-27 SROS
Page 355 Jul 01/06
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 27-50-00-866-802 27-80-00-866-802 12-13-27-991-005 12-13-27-991-006-A FOR FIN 5003CV, 5081CV 12-13-27-612-805
R
32-12-00-010-801 32-12-00-410-801 FOR FIN 5009CW, 5069CW 12-13-27-612-806 53-35-13-000-802 53-35-13-400-802
Energize the Ground Service Network De-energize the Ground Service Network Retraction of the Flaps on the Ground Retraction of the Slats on the Ground Fig. 306 Fig. 307 Oil Replenishing of the Flap System Torque Limiter (5003CV, 5081CV) Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Oil Replenishing of the Slat System Torque Limiter (5009CW, 5069CW) Removal of the Belly Fairing Access Panels Installation of the Belly Fairing Access Panels
3. __________ Job Set-up Subtask 12-13-27-860-065 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). (2) Make sure that the flaps and slats are retracted (Ref. TASK 27-50-00866-802) and (Ref. TASK 27-80-00-866-802). (3) Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER on the slat/flap control lever.
EFF : ALL 12-13-27 SROS
Page 356 Jul 01/06
Subtask 12-13-27-865-065 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 5003CV, 5081CV 721VU SFCC 1 NORM 10CV X14 722VU SFCC 2 FLAP 2CV T43 742VU SFCC 1 FLAP 1CV L61 FOR 5009CW, 5069CW 721VU SFCC 1 NORM AVAIL 10CW X13 722VU SFCC 2 SLAT 2CW V40 742VU SFCC 1 SLAT 1CW L62 Subtask 12-13-27-010-065 C. Get Access (1) Put the ACCESS PLATFORM 2M (6 FT) in position below the access panel 193BB. (2) FOR 5003CV, 5081CV open the MLG doors (Ref. TASK 32-12-00-010-801). (3) FOR 5009CW, 5069CW remove the access panel 193FB (Ref. TASK 53-35-13-000-802). (4) Put the CONTAINER 1 L (1/4 USGAL) in position below the system torque limiter. 4. Procedure _________ (Ref. Fig. 306/TASK 12-13-27-991-005, 307/TASK 12-13-27-991-006-A) Subtask 12-13-27-680-051 A. Oil Drainage of the Flap/Slat System Torque Limiter (1) Remove the oil-fill plug (1) and remove and discard the preformed packing (2). (2) Remove and discard the lockwire from the oil-drain plug (3).
EFF : ALL 12-13-27 R SROS
Page 357 Jan 01/03
(3) Remove the oil-drain plug (3) and remove and discard the preformed packing (4) and let the oil drain into the container. (4) Measure the quantity of the oil. R R R
(5) FOR 5000CV after the oil has completely drained, install the new plug preformed packing (4) and the oil-drain (3) into the flap system torque limiter.
R R R
(6) FOR 5000CW after the oil has completely drained, install the new plug preformed packing (4) and the oil-drain (3) into the slat system torque limiter. (7) TORQUE the oil drain plug to between 1.23 and 1.5 m.daN (108.84 and 132.74 lbf.in). (8) Safety the oil-drain plug with MISCELLANEOUS (Material No. 19-010). Subtask 12-13-27-612-057
R
B. Do the oil replenishing of the system torque limiter: - FOR 5003CV, 5081CV (Ref. TASK 12-13-27-612-805), - FOR 5009CW, 5069CW (Ref. TASK 12-13-27-612-806). 5. Close-up ________ Subtask 12-13-27-865-066 A. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 5003CV, 5081CV 1CV, 2CV, 10CV, FOR 5009CW, 5069CW 1CV, 2CV, 10CV. Subtask 12-13-27-410-057 B. Close Access (1) Remove the container. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 12-13-27 SROS
Page 358 Jul 01/06
(3) FOR 5003CV, 5081CV close the MLG doors (Ref. TASK 32-12-00-410-801). (4) FOR 5009CW, 5069CW install the access panel 193FB (Ref. TASK 53-35-13-400-802). (5) Remove the access platform(s). (6) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-13-27-860-066 C. Put the Aircraft back to its Initial Configuration (1) Remove the warning notice(s). (2) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever. (3) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-13-27 R SROS
Page 359 Jan 01/03
TASK 12-13-27-281-801 Sampling of the SEMIFLUID from the Flap Rotary Actuator WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. 1. __________________ Reason for the Job R R
To analyze the SEMIFLUID for water content, if the flap actuator is suspected for water ingress
EFF : ALL 12-13-27 SROS
Page 360 Jul 01/06
2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific No specific No specific No specific 98D27803000000 FOR FIN 5122CV 98F29208217000
circuit breaker(s) safety clip(s) container commercial 50 ml 1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE 1 WARNING NOTICE 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER 1 SAFETY PIN - RAT
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-13-27-612-804 24-42-00-861-801 24-42-00-862-801 57-56-11-000-807 57-56-11-400-807 27-50-00-866-801 27-50-00-866-802
Drain and Refill the Rotary Actuators Energize the Ground Service Network De-energize the Ground Service Network Removal of the Movable Flap Track Fairings Nos. 2 thru 5 for Access Installation of the Movable Flap Track Fairings Nos. 2 thru 5 after Access Extension of the Flaps on the Ground (for corrective action) Retraction of the Flaps on the Ground (for corrective action) Fig. 304
12-13-27-991-004 FOR FIN 5009CV, 5087CV 27-50-00-866-801 Extension of the Flaps on the Ground 27-50-00-866-802 Retraction of the Flaps on the Ground 32-12-00-010-801 Open the MLG Doors for Maintenance 32-12-00-410-801 Close the MLG Doors after Maintenance FOR FIN 5122CV 29-24-00-081-801 Removal of the RAT Safety Pin 29-24-00-481-801 Installation of the RAT Safety Pin FOR FIN 5024CV, 5034CV, 5044CV, 5055CV, 5102CV, 5112CV, 5122CV, 5133CV 27-50-00-866-802 Retraction of the Flaps on the Ground
EFF : ALL 12-13-27 SROS
Page 361 Jan 01/05
3. __________ Job Set-up Subtask 12-13-27-860-067 A. Aircraft Maintenance Configuration (1) If the ambient temperature is aircraft is on the ground for least 15 time to increase the more than 20 times (Ref. TASK 00-866-802).
below 15 DEG.C (59.00 DEG.F) or the less than 10 hours, cycle the flaps at temperature. But do not cycle the flaps 27-50-00-866-801) and (Ref. TASK 27-50-
(2) Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-27-010-066 B. Get Access (1) FOR 5009CV, 5087CV open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position below the applicable access panel. (3) FOR 5122CV - install the SAFETY PIN - RAT (Ref. TASK 29-24-00-481-801). (4) Remove the applicable movable 000-807): - FOR 5024CV, 5102CV remove the No. 2 flap track - FOR 5034CV, 5112CV remove the No. 3 flap track - FOR 5044CV, 5122CV remove the No. 4 flap track - FOR 5055CV, 5133CV remove the No. 5 flap track
flap track fairing (Ref. TASK 57-56-11fairing, fairing, fairing, fairing.
EFF : ALL 12-13-27 R SROS
Page 362 Jan 01/03
Subtask 12-13-27-860-068 C. Aircraft Maintenance Configuration (1) Put the flaps in position: - FOR 5024CV, 5034CV, 5044CV, 5055CV, 5102CV, 5112CV, 5122CV, 513 make sure that the flaps are retracted (Ref. TASK 27-50-00-866802), - FOR 5009CV, 5087CV extend the flaps to the position 2 (Ref. TASK 27-50-00-866-801). (2) Attach the LOCKING TOOL - FLAP/SLAT CONTROL LEVER to the flap/slat control lever on panel 114VU. (3) Put the WARNING NOTICE in position on panel 114VU to tell persons not to operate the flap/slat controls. Subtask 12-13-27-865-067 D. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM 10CV X14 722VU SFCC 2 FLAP 2CV T43 742VU SFCC 1 FLAP 1CV L61 4. Procedure _________ Subtask 12-13-27-281-050 A. Sampling of the SEMIFLUID of the Flap Rotary Actuator (Ref. Fig. 304/TASK 12-13-27-991-004) (1) Clean all the rotary actuator (3). (2) Remove the bottom plug (6) and if necessary the top plug (1). (3) Let at least 20 ml of SEMIFLUID flow into a container commercial 50 ml. (4) Examine the O-rings (2) and replace them if necessary. (5) Install the bottom plug (6) but do not tighten at this time.
EFF : ALL 12-13-27 R SROS
Page 363 Jan 01/03
(6) Put a label with the subsequent information on the sample container: - P/N and Serial No. of the affected actuator, - sample date, - date of installation of the actuator, - wing position (station) of the actuator, - number of cycles/flight hours of the actuator. (7) Send the sample to any Laboratory for analysis for water content. NOTE : The analysis is in accordance with Karl Fischer-Direct Method; ____ ASTM D1744. The rotary actuator must be replaced if the water content in the SEMIFLUID is more than 12%. (8) Do the drain and refill procedure (Ref. TASK 12-13-27-612-804). NOTE : After correct draining and filling of the actuator, a faulty ____ actuator will operate at least 500 flight cycles without any low-temperature performance problems. 5. Close-up ________ Subtask 12-13-27-865-068 A. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1CV, 2CV, 10CV. Subtask 12-13-27-410-058 B. Close Access (1) FOR 5009CV, 5087CV close the MLG doors (Ref. TASK 32-12-00-410-801). (2) Make sure that the work area is clean and clear of tools and other items. (3) Install the applicable movable 11-400-807): - FOR 5024CV, 5102CV install the No. 2 flap track - FOR 5034CV, 5112CV install the No. 3 flap track - FOR 5044CV, 5122CV install the No. 4 flap track - FOR 5055CV, 5133CV
flap track fairing (Ref. TASK 57-56fairing, fairing, fairing,
EFF : ALL 12-13-27 R SROS
Page 364 Jan 01/03
install the No. 5 flap track fairing. (4) FOR 5122CV - remove the SAFETY PIN - RAT (Ref. TASK 29-24-00-081-801). (5) Remove the access platform(s). (6) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-13-27-860-069 C. Aircraft Maintenance Configuration (1) Remove the warning notice(s). (2) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever on panel 114VU. (3) FOR 5009CV, 5087CV retract the flaps (Ref. TASK 27-50-00-866-802). (4) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-13-27 SROS
Page 365 Jan 01/03
HYDRAULIC POWER - SERVICING ___________________________ TASK 12-13-29-612-801 Oil Replenishment of the Ram Air Turbine (RAT) (11JR) WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No
specific specific specific specific specific specific
circuit breaker(s) safety clip(s) safety barriers 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 CAN - OIL 1 WARNING NOTICE Torque Wrench : range 2.00 to 26.00 lbf.ft (0.20 to 3.60 m.daN)
EFF : ALL 12-13-29 R SROS
Page 301 Jan 01/06
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 03-003 Material No. 19-003 Material No. 19-010
USA MIL-PRF-7808 LUBRICATING OIL TURBINE SYNTHETIC BASE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00) USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------R R
2 2 2 3 3 3
packing packing packing packing packing packing
29-24-54 29-24-54 29-24-54 29-24-54 29-24-54 29-24-54
02 -020 02A-020 02B-020 03 -020 03A-020 03B-020
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-24-00-869-801 29-24-00-869-802 12-13-29-991-001
Extension of the Ram Air Turbine (RAT) on the Ground Retraction of the Ram Air Turbine (RAT) on the Ground Fig. 301
EFF : ALL 12-13-29 SROS
Page 302 Jan 01/06
3. __________ Job Set-up Subtask 12-13-29-010-050 A. Get Access (1) Put the safety barriers in position. (2) Put the WARNING NOTICE in position to tell persons not to operate the RAT. (3) Extend the RAT (Ref. TASK 29-24-00-869-801). (4) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the RAT. (5) Remove the access panel 633HB. Subtask 12-13-29-865-050 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------742VU RAT STOW CTL 1JR D77
EFF : ALL 12-13-29 R SROS
Page 303 Jan 01/06
4. Procedure _________ (Ref. Fig. 301/TASK 12-13-29-991-001) **ON A/C 001-001, 201-207, 251-252, 255-299, 401-449, Subtask 12-13-29-612-050 A. Oil Replenishment of the Upper and/or Lower RAT Gearbox WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK _______ AREA WHEN YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. (1) Remove and discard the lockwire from the oil fill plug (1). (2) Remove the oil fill plug (1) and the packing (2) and/or (3). (3) Discard the packing (2) and/or (3). R R
(4) Fill the RAT gearbox with the OILS (Material No. 03-003) with a CAN OIL , until it comes out of the fill port. (5) Clean the oil fill plug (1) with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003).
R R R R R
(6) Install the oil fill plug: - for the upper RAT gearbox, install the new packing (2) and the oil fill plug (1) - for the lower RAT gearbox,install the new packing (3) and the oil fill plug (1). (7) TORQUE the fill plug (1) to between 9.2 and 12.5 lbf.ft (1.24 and 1.69 m.daN).
EFF : ALL 12-13-29 SROS
Page 304 Jan 01/06
RAT Oil Fill Ports - Location Figure 301/TASK 12-13-29-991-001 R EFF : ALL 12-13-29 SROS
Page 305 Jan 01/06
R
(8) Safety the oil fill plug (1) with the lockwire, MISCELLANEOUS (Material No. 19-010) **ON A/C 002-049, 208-249, 301-399, 451-499, 701-749, Subtask 12-13-29-612-050-A A. Oil Replenishment of the Upper and/or Lower RAT Gearbox (1) Remove and discard the lockwire from the oil fill plug (1). (2) Remove the oil fill plug (1) and the packing (2) and/or (3). (3) Discard the packing (2) and/or (3). (4) Fill the RAT gearbox WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE _______ THIS/THESE MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. - Fill the RAT gearbox with OILS (Material No. 03-003) with a CAN OIL, until it spills from the fill port. (5) Clean the oil fill plug (1) with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003). (6) Install for: - the upper RAT gearbox, the new packing (2) and the oil fill plug (1), - for the lower RAT gearbox, the new packing (3) and the oil fill plug (1). (7) TORQUE the fill plug CAUTION : YOU MUST NOT TIGHTEN MORE THAN THE MAXIMUM TORQUE VALUE. _______ IF YOU DO YOU CAN CAUSE DAMAGE. - TORQUE the fill plug (1) to between 9.2 and 12.5 lbf.ft (1.24 and 1.69 m.daN). (8) Safety the oil fill plug (1) with lockwire MISCELLANEOUS (Material No. 19-010)
R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-29 301-399, 401-449, 451-499, 701-749, SROS
Page 306 Jan 01/06
**ON A/C ALL 5. Close-up ________ Subtask 12-13-29-865-051 A. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1JR. Subtask 12-13-29-410-050 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panel 633HB. (3) Retract the RAT (Ref. TASK 29-24-00-869-802). (4) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 12-13-29 SROS
Page 307 Jan 01/06
APU - SERVICING _______________ TASK 12-13-49-612-801 Gravity Servicing of the APU Oil Reservoir WARNING : DO NOT TOUCH THE APU UNTIL IT IS SUFFICIENTLY COOL TO PREVENT BURNS _______ WHEN YOU DO THE MAINTENANCE TASK(S). WARNING : USE THE CORRECT PERSONAL PROTECTION. OIL CAN HAVE AN ADDITIVE CALLED _______ TRICRESYL PHOSPHATE IN IT. THIS CHEMICAL IS AN ASPHYXIANT, IT IS POISONOUS AND CAN BE ABSORBED THROUGH THE SKIN. USE CARE WHEN ENGINE OIL IS DRAINED. HOT OIL CAN POSSIBLY CAUSE BAD BURNS. CAUTION : OIL CONSUMPTION IS THE TERM USED FOR THE INTERNAL LOSS OF OIL FROM _______ BEARING SEALS AND AIR/OIL SEPARATOR DURING APU OPERATION. EXTERNAL LEAKS ARE NOT PERMITTED. YOU MUST CORRECT EXTERNAL LEAKS AND CLEAN THE APU, APU COMPARTMENT AND APU AIR INTAKE IMMEDIATELY IF CONTAMINATED. IF THE OIL CONSUMPTION IS HIGHER THAN THE GRAPH A LIMIT, OR THERE IS A SUDDEN INCREASE IN OIL CONSUMPTION, YOU MUST DO THE OIL CONSUMPTION MONITORING VERY CAREFULLY TO PREVENT BAD APU DAMAGE. 1. __________________ Reason for the Job Add oil to the APU oil reservoir, which is integral with the accessory drive gearbox (referred to as the gear box), - if the oil level check shows that you must add oil, - if the APU oil reservoir was drained, - if you prepare a replacement APU for installation. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No No No No
specific specific specific specific
circuit breaker(s) safety clip(s) warning notice container 3 l (0.7925 USgal) access platform 7.2 m (23 ft. 7 in.)
EFF : ALL 12-13-49 SROS
Page 301 Jan 01/05
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------No specific
lint-free cloth
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 29-00-00-864-804 R 49-91-00-600-801 12-13-49-991-001 12-13-49-991-002
Energize the Ground Service Network De-energize the Ground Service Network Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Oil Change Fig. 301 Fig. 302
3. __________ Job Set-up Subtask 12-13-49-860-050 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). (2) Make sure that the hydraulic systems are depressurized (Ref. TASK 29-00-00-864-804). (3) Put the warning notice in position on the panel 215VU to tell persons not to start the APU. NOTE : To get an accurate oil level indication, do not wait longer ____ than 5 to 15 minutes after APU shutdown before you do the APU oil level check.
EFF : ALL 12-13-49 SROS
Page 302 Jul 01/02
Subtask 12-13-49-865-050 R R
B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU APU FIRE SQUIB B 2WF P09 721VU APU FIRE VLV CTL 4WF P07 742VU APU START CTL 1KA C72 742VU APU FIRE SQUIB A 1WF J72 742VU APU FIRE VLV CTL 3WF J71 Subtask 12-13-49-010-050
R
C. Get Access (1) Put the access platform in position below the APU compartment. (2) Open the APU access doors 315AL and 316AR and safety them in the open position. (3) Set the LIGHT switch 3LJ to the on position. 4. Procedure _________ Subtask 12-13-49-612-050 A. Add Oil to the APU Oil Reservoir (Ref. Fig. 301/TASK 12-13-49-991-001, 302/TASK 12-13-49-991-002) WARNING : USE THE CORRECT PERSONAL PROTECTION. OIL CAN HAVE AN ADDITIVE _______ CALLED TRICRESYL PHOSPHATE IN IT. THIS CHEMICAL IS AN ASPHYXIANT, IT IS POISONOUS AND CAN BE ABSORBED THROUGH THE SKIN. USE CARE WHEN ENGINE OIL IS DRAINED. HOT OIL CAN POSSIBLY CAUSE BAD BURNS. WARNING : DO NOT REMOVE OIL FILLER CAP WHEN OIL IS HOT AND OIL LEVEL IS _______ ABOVE ADD RANGE ON SIGHT GLASS. HOT OIL CAN CAUSE SEVERE BURNS. (1) Do an oil level check on the oil sight glass. NOTE : To get an accurate oil level indication, do not wait longer ____ than 5 to 15 minutes after APU shutdown before you do the APU oil level check.
EFF : ALL 12-13-49 SROS
Page 303 Apr 01/02
APU Oil-Servicing Ports Figure 301/TASK 12-13-49-991-001 EFF : ALL 12-13-49 SROS
Page 304 Apr 01/98
Guideline for Oil Consumption of GTCP 331-350 APUs In Service Figure 302/TASK 12-13-49-991-002 EFF : ALL 12-13-49 SROS
Page 305 Apr 01/98
If the oil level is at the FULL mark on the oil sight glass, do not add oil to the APU oil reservoir. (2) Put the container in position below the gearbox to collect oil leakage. (3) Make sure that the oil scupper and the oil filler cap are clean. Make them clean with a lint-free cloth, if they are dirty. (4) Open the oil filler cap. WARNING : DO NOT REMOVE OIL FILLER CAP WHEN OIL IS HOT AND OIL LEVEL _______ IS ABOVE ADD RANGE ON SIGHT GLASS. HOT OIL CAN CAUSE SEVERE BURNS. (a) Open the lock and slowly loosen the oil filler cap to release remaining pressure from the oil reservoir. (b) Remove the oil filler cap and make it dry with a lint-free cloth.
EFF : ALL 12-13-49 R SROS
Page 306 Apr 01/02
(5) Add the oil. WARNING : PUT THE OIL INTO THE GRAVITY-FILL PORT SLOWLY. THIS WILL _______ PREVENT A BLOW-BACK OF HOT OIL WHICH CAN BURN YOU. CAUTION : WHEN YOU DO THE SERVICING OF THE APU OIL RESERVOIR, MAKE _______ SURE YOU USE AN APPROVED ENGINE OIL OF THE SAME TYPE AND BRAND. IF YOU MIX DIFFERENT OILS YOU CAN DAMAGE THE APU. CAUTION : MAKE SURE OIL SERVICING STOPS WHEN GRAVITY-FILL CAP OPENING _______ STARTS TO OVERFLOW OR WHEN OIL FLOWS FROM PRESSURE SYSTEM OVERFILL FITTINGS. OVER-SERVICING CAN CAUSE FOAMING OF OIL WHICH CAN CAUSE LOP SHUTDOWN OF ENGINE. (a) Make sure that the oil-can(s) is(are) clean and the oil does not contain unwanted materials. (b) Use the following oil brands and types
R
-------------------------------------------------------------------------BRAND NAME OIL TYPE -------------------------------------------------------------------------AeroShell Turbine Oil 390 1 Castrol 325 1 Castrol 399 1 BP Exxon Turbo Oil 2389 1 -------------------------------------------------------------------------AeroShell Turbinen Oil 500 2 AeroShell 555 2 AeroShell Turbine Oil 560 2 Castrol Aero 5000 2 Castrol Aero 5050 2 Exxon/Esso Turbo Oil 25 2 Exxon/Esso Turbo Oil 2380 2 BP/Exxon Turbine Oil 2197 2 Hatco 3211 2 Hatco 3611 2 Mobil Jet Oil II 2 Mobil 254 2 Royco Turbine Oil 500 2 Royco 555 2 Royco Turbine Oil 560 2 Royco 899 2
EFF : ALL 12-13-49 SROS
Page 307 Jul 01/02
(c) Carefully add the oil until the oil level in the oil reservoir is at the FULL mark on the oil sight glass. NOTE : If the oil which is available for the oil servicing is of ____ a different type or brand than the oil which is in the APU oil reservoir, you can change the oil in the reservoir (Ref. TASK 49-91-00-600-801), or you apply the replenishment method approved by the OEM. Add the new approved oil to the reservoir as necessary, at each routine oil servicing interval, to complete the oil change.
R R R R R R R
(6) Install and lock the oil filler cap. NOTE : Make sure that the oil filler cap is tight and locked ____ correctly. (7) Remove the oil from the oil scupper and make it dry with a lint-free cloth. (8) Remove the container. (9) If oil fell on the APU, the air intake duct and/or the adjacent area, remove it and make the area dry with a lint-free cloth. (10) Make an entry in the applicable logbook(s). (Ref. Fig. 302/TASK 12-13-49-991-002) CAUTION : OIL CONSUMPTION IS THE TERM USED FOR THE INTERNAL LOSS OF _______ OIL FROM BEARING SEALS AND AIR/OIL SEPARATOR DURING APU OPERATION. EXTERNAL LEAKS ARE NOT PERMITTED. YOU MUST CORRECT EXTERNAL LEAKS AND CLEAN THE APU, APU COMPARTMENT AND APU AIR INTAKE IMMEDIATELY IF CONTAMINATED. IF THE OIL CONSUMPTION IS HIGHER THAN THE GRAPH A LIMIT, OR THERE IS A SUDDEN INCREASE IN OIL CONSUMPTION, YOU MUST DO THE OIL CONSUMPTION MONITORING VERY CAREFULLY TO PREVENT BAD APU DAMAGE. (a) Make an entry in the applicable logbook(s) to tell people the quantity of the oil which you have added to the APU oil reservoir.
EFF : ALL 12-13-49 SROS
Page 308 Apr 01/02
5. Close-up ________ Subtask 12-13-49-410-050 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Set the LIGHT switch 3LJ to the off position. (3) Close the APU access doors 315AL and 316AR. (4) Remove the access platform(s). Subtask 12-13-49-865-051 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1KA, 1WF, 2WF, 3WF, 4WF Subtask 12-13-49-860-053 C. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801) (2) Remove the warning notice(s). (3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL 12-13-49 R SROS
Page 309 Jan 01/05
TASK 12-13-49-612-801- 01 Pressure Servicing of the APU Oil Reservoir WARNING : DO NOT TOUCH THE APU UNTIL IT IS SUFFICIENTLY COOL TO PREVENT BURNS _______ WHEN YOU DO THE MAINTENANCE TASK(S). WARNING : USE THE CORRECT PERSONAL PROTECTION. OIL CAN HAVE AN ADDITIVE CALLED _______ TRICRESYL PHOSPHATE IN IT. THIS CHEMICAL IS AN ASPHYXIANT, IT IS POISONOUS AND CAN BE ABSORBED THROUGH THE SKIN. USE CARE WHEN ENGINE OIL IS DRAINED. HOT OIL CAN POSSIBLY CAUSE BAD BURNS. CAUTION : OIL CONSUMPTION IS THE TERM USED FOR THE INTERNAL LOSS OF OIL FROM _______ BEARING SEALS AND AIR/OIL SEPARATOR DURING APU OPERATION. EXTERNAL LEAKS ARE NOT PERMITTED. YOU MUST CORRECT EXTERNAL LEAKS AND CLEAN THE APU, APU COMPARTMENT AND APU AIR INTAKE IMMEDIATELY IF CONTAMINATED. IF THE OIL CONSUMPTION IS HIGHER THAN THE GRAPH A LIMIT, OR THERE IS A SUDDEN INCREASE IN OIL CONSUMPTION, YOU MUST DO THE OIL CONSUMPTION MONITORING VERY CAREFULLY TO PREVENT BAD APU DAMAGE. 1. __________________ Reason for the Job Add oil to the APU oil reservoir, which is integral with the accessory drive gearbox (referred to as the gear box), - if the oil level check shows that you must add oil, - if the oil reservoir was drained, - if you prepare a replacement APU for installation. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific No specific No specific No specific DH13PM
circuit breaker(s) safety clip(s) warning notice container 10.0 l (2.6416 USgal) access platform 7.2 m (23 ft. 7 in.) 1 TANK - ENGINE OIL FILLING UP
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B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------No specific
lint-free cloth
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 29-00-00-864-804 R 49-91-00-600-801 12-13-49-991-001 12-13-49-991-002
Energize the Ground Service Network De-energize the Ground Service Network Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Oil Change Fig. 301 Fig. 302
3. __________ Job Set-up Subtask 12-13-49-860-054 A. Aircraft Maintenance Configuration (1) Put the warning notice in position on the panel 215VU to tell persons not to start the APU. (2) Energize the ground service network (Ref. TASK 24-42-00-861-801). (3) Make sure that the hydraulic systems are depressurized (Ref. TASK 29-00-00-864-804).
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Subtask 12-13-49-865-054 R R
B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU APU FIRE SQUIB B 2WF P09 721VU APU FIRE VLV CTL 4WF P07 742VU APU START CTL 1KA C72 742VU APU FIRE SQUIB A 1WF J72 742VU APU FIRE VLV CTL 3WF J71 Subtask 12-13-49-010-055
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C. Get Access (1) Put the access platform in position below the APU compartment. (2) Open the APU access doors 315AL and 316AR and safety them in the open position. (3) Set the LIGHT switch 3LJ to the on position. 4. Procedure _________ Subtask 12-13-49-612-052 A. Add Oil to the APU Oil Reservoir (Ref. Fig. 301/TASK 12-13-49-991-001, 302/TASK 12-13-49-991-002) WARNING : USE THE CORRECT PERSONAL PROTECTION. OIL CAN HAVE AN ADDITIVE _______ CALLED TRICRESYL PHOSPHATE IN IT. THIS CHEMICAL IS AN ASPHYXIANT, IT IS POISONOUS AND CAN BE ABSORBED THROUGH THE SKIN. USE CARE WHEN ENGINE OIL IS DRAINED. HOT OIL CAN POSSIBLY CAUSE BAD BURNS. WARNING : DO NOT REMOVE OIL FILLER CAP WHEN OIL IS HOT AND OIL LEVEL IS _______ ABOVE ADD RANGE ON SIGHT GLASS. HOT OIL CAN CAUSE SEVERE BURNS. (1) Do an oil level check on the oil sight glass. NOTE : To get an accurate oil level indication, do not wait longer ____ than 5 to 15 minutes after APU shutdown before you do the APU oil level check.
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If the oil level is at the FULL mark on the oil sight glass, do not add oil to the APU oil reservoir. (2) Put the container in position below the gearbox to collect oil leakage. (3) Put the TANK - ENGINE OIL FILLING UP in position below the APU gearbox. R CAUTION : WHEN YOU DO THE SERVICING OF THE APU OIL RESERVOIR, MAKE _______ SURE YOU USE AN APPROVED ENGINE OIL OF THE SAME TYPE AND BRAND. IF YOU MIX DIFFERENT OILS YOU CAN DAMAGE THE APU. (a) Make sure that the TANK - ENGINE OIL FILLING UP is filled with clean and approved oil which is of the same type and brand than the oil which is in the APU oil reservoir. NOTE : If the oil which is in the TANK - ENGINE OIL FILLING UP is ____ of a different type or brand than the oil which is in the APU oil reservoir, you can change the oil in the TANK ENGINE OIL FILLING UP or in the APU oil reservoir (Ref. TASK 49-91-00-600-801) or you can apply the replenishment methode approved by the OEM. Add the new approved oil to the reservoir as necessary at each routine oil servicing interval to complete the oil change.
R R R R R R R
Use the following oil brands and types
R
-------------------------------------------------------------------------BRAND NAME OIL TYPE -------------------------------------------------------------------------AeroShell 390 1 Brayco 880 1
R R R
Castrol 325 Castrol 399
1 1
BP Exxon Turbo Oil 2389
1
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R R R R R R R R R R
-------------------------------------------------------------------------BRAND NAME OIL TYPE -------------------------------------------------------------------------AeroShell Turbine Oil 500 2 AeroShell Turbine Oil 555 2 AeroShell Turbine Oil 560 2 Castrol Aero 5000 2 Castrol Aero 5050 2 BP Exxon Turbo Oil 25 2 BP Exxon Turbo Oil 2380 2 Hatco Hatco Mobil Mobil Royco Royco Royco Royco
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3211 3611 Jet Oil Jet Oil Turbine 555 Turbine 899
2 2 2 2 2 2 2 2
II 254 Oil 500 Oil 560
(4) Connect the overflow hose and the pressure fill hose. CAUTION : POINT THE OVERFLOW DRAIN HOSE IN A CORRECT CONTAINER WHEN _______ YOU CONNECT IT. (a) Clean the caps on the overflow port and the pressure fill port with a lint-free cloth and then remove them from the ports.
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(5) Clean the connectors of the overflow hose and the pressure fill hose with a lint-free cloth and make sure that they are serviceable. (a) Put the outlet of the overflow hose into the container. (b) Connect the overflow hose to the overflow port. (c) Connect the pressure fill hose to the pressure fill port.
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(6) Add oil. CAUTION : MAKE SURE OIL SERVICING STOPS WHEN GRAVITY-FILL CAP OPENING _______ STARTS TO OVERFLOW OR WHEN OIL FLOWS FROM PRESSURE SYSTEM OVERFILL FITTINGS. OVER-SERVICING CAN CAUSE FOAMING OF OIL WHICH CAN CAUSE LOP SHUTDOWN OF ENGINE. CAUTION : DO NOT OVERFILL APU RESERVOIR. TO REMOVE OVERFILL HOSE _______ BEFORE OIL HAS BECOME STABLE, OR PRESSURE-FILL WITHOUT OVERFILL HOSE VENTING, CAN CAUSE ENGINE DAMAGE.
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(a) Operate the TANK - ENGINE OIL FILLING UP (DH13PM) and slowly add oil until it flows from the overfill hose into the container. NOTE : Make sure that the outlet end of the overflow hose is ____ above the fluid level in the container and not blocked. Keep the overflow hose connected for approximately 2 minutes, after you have stopped to add the oil. This makes sure that the oil level in the APU oil reservoir becomes stable and the oil which was added too much is drained. R
(7) Disconnect the overflow hose and the pressure fill hose. (a) Remove the pressure fill hose from the pressure fill port. (b) Remove the overflow hose from the overflow port. (c) Clean the ports with a lint-free cloth. (d) Make sure that the caps are clean and in the correct condition and install them onto the ports. NOTE : Make sure that the caps on the pressure fill port and the ____ overflow port are installed correctly and tight.
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(8) Remove the TANK - ENGINE OIL FILLING UP.
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(9) Remove the container.
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(10) If oil fell on the APU, the air intake duct and/or the adjacent area during the oil servicing, remove it and make the area dry with a lint-free cloth.
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(11) Make an entry in the applicable logbook(s). (Ref. Fig. 302/TASK 12-13-49-991-002) CAUTION : OIL CONSUMPTION IS THE TERM USED FOR THE INTERNAL LOSS OF _______ OIL FROM BEARING SEALS AND AIR/OIL SEPARATOR DURING APU OPERATION. EXTERNAL LEAKS ARE NOT PERMITTED. YOU MUST CORRECT EXTERNAL LEAKS AND CLEAN THE APU, APU COMPARTMENT AND APU AIR INTAKE IMMEDIATELY IF CONTAMINATED. IF THE OIL CONSUMPTION IS HIGHER THAN THE GRAPH A LIMIT, OR THERE IS A SUDDEN INCREASE IN OIL CONSUMPTION, YOU MUST DO THE OIL CONSUMPTION MONITORING VERY CAREFULLY TO PREVENT BAD APU DAMAGE.
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(a) Make an entry in the applicable logbook(s) to tell people the quantity of the oil which you have added to the APU oil reservoir. 5. Close-up ________ Subtask 12-13-49-410-054 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Set the LIGHT switch 3LJ to the off position. (3) Close the APU access doors 315AL and 316AR. (4) Remove the access platform(s). Subtask 12-13-49-865-055 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1KA, 1WF, 2WF, 3WF, 4WF Subtask 12-13-49-410-055 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access door 811. (3) Remove the access platform(s). Subtask 12-13-49-860-055 D. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801) (2) Remove the warning notice(s). (3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
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ENGINE OIL - SERVICING ______________________ TASK 12-13-79-610-806 Servicing of the Engine Oil System WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE AFTER THE ENGINE IS SHUTDOWN. _______ THE ENGINE CAN STAY HOT FOR A LONG TIME AFTER THE ENGINE IS SHUTDOWN. WARNING : USE PROTECTIVE CLOTHING WHEN YOU USE ENGINE OIL. OIL CAN CAUSE SKIN _______ IRRITATION. CAUTION : YOU MUST EXAMINE THE OIL LEVEL BETWEEN 15 MINUTES AND 2 HOURS AFTER _______ SHUTDOWN. IF YOU DO NOT, THE OIL LEVEL SIGHTGLASS INDICATION WILL NOT BE ACCURATE. CAUTION : DO NOT OPERATE THE ENGINE WITHOUT SUFFICIENT OIL. THIS WILL CAUSE A _______ POSSIBLE INFLIGHT SHUTDOWN AND POSSIBLE DAMAGE TO THE ENGINE. CAUTION : YOU MUST DO THIS SERVICING PROCEDURE TO PREVENT TOO MUCH OIL IN THE _______ OIL SYSTEM. DO NOT OPERATE THE ENGINE WITH TOO MUCH OIL. THIS WILL CAUSE A POSSIBLE IN FLIGHT SHUTDOWN AND POSSIBLE DAMAGE TO THE ENGINE. CAUTION : DO NOT LET ENGINE FUEL OR OIL FALL ON THE ENGINE. YOU MUST _______ IMMEDIATELY REMOVE UNWANTED FUEL OR OIL WITH A CLOTH. THE FUEL OR OIL CAN CAUSE DAMAGE TO SOME ENGINE PARTS. CAUTION : OPERATORS MUST MAKE SURE THE OIL TANK _______ GOOD WORKING ORDER PRIOR TO OPERATING FLAPPER VALVE. IF YOU DO NOT DO THIS, INFLIGHT SHUTDOWN AND POSSIBLE DAMAGE
CAP IS SECURELY LATCHED AND IN WITH A DAMAGED OR BROKEN IT WILL CAUSE A POSSIBLE TO THE ENGINE.
1. __________________ Reason for the Job To make a check of the engine oil level. To fill the engine oil system to get the correct oil level. NOTE : Do not use this servicing task for filling the engine oil system ____ after the replacement of an oil system component. To fill the engine oil system after the replacement of an oil system component (Ref. TASK 12-13-79-610-80700). NOTE : Do not use this servicing task for changing the engine oil. To change ____ the engine oil (Ref. TASK 12-13-79-610-80800).
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NOTE : If you see black oil in the oil system, refer to Inspection for ____ Black Oil (Ref. TASK 79-00-00-280-80400). Black oil may be an indication of a serious problem or it can be a condition that requires no maintenance action. If you notice a damaged or broken oil tank flapper valve during servicing the following conditions apply. NOTE : It is permitted to fly with a damaged valve if: ____ - The flapper valve is replaced at the next visit to a maintenance facility, not to exceed 5 cycles. - The damaged or broken flapper valve does not pose a risk of contamination of the oil system. - The engine is not experiencing oil loss due to oil leakage from the oil tank cap or flapper valve. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No
specific specific specific specific specific specific specific specific
circuit breaker(s) safety clip(s) drain hose dust cover flashlight pressure fill service unit fluid drain collector/container 10 USgal (37.8544 l) access platform 2.5 m (8 ft. 2 in.) adjustable access platform 3.7 m (12 ft. 2 in.)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
P03-001
Material No.
P05-005
Material No.
P05-421
Material No.
P05-422
* oil, lubricating, turbine engine (Ref. 70-30-00) * cloth, cotton, lint free (Ref. 70-30-00) * Nylon Pads and Rolls, Abrasive impregnated (Ref. 70-30-00) *
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Scrub Pad (Ref. 70-30-00) C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 70-57-00-910-802 71-00-00-720-816 12-13-79-991-006
Energize the Ground Service Network De-energize the Ground Service Network Degreasing of Parts by Solvent Wipe (SPOP 208) Test No. 2 - Engine Motor Leak Test (Dry Method) Thrust Reverser Cowl Doors Open Fig. 301
3. __________ Job Set-up Subtask 12-13-79-861-055 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-79-941-055 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure. Subtask 12-13-79-010-062 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU.
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Subtask 12-13-79-865-060 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-13-79-010-063 E. Get Access (1) Open the upper left thrust reverser access door: - FOR 4030EM1 417DL - FOR 4030EM2 427DL (2) Put the adjustable access platform in position. 4. Procedure _________ (Ref. Fig. 301/TASK 12-13-79-991-006) Subtask 12-13-79-210-052 A. Make a Check of the Engine Oil Level WARNING : IT IS NOT NECESSARY TO REMOVE THE OIL TANK CAP TO EXAMINE THE _______ OIL LEVEL. IF YOU DO NEED TO REMOVE THE OIL TANK CAP, YOU MUST WAIT A MINIMUM OF 5 MINUTES AFTER SHUTDOWN TO LET THE OIL PRESSURE BLEED OFF. THE HOT OIL CAN BURN YOUR EYES AND SKIN. CAUTION : YOU MUST EXAMINE THE OIL LEVEL BETWEEN 15 MINUTES AND 2 HOURS _______ AFTER SHUTDOWN. IF YOU DO NOT, THE OIL LEVEL SIGHTGLASS INDICATION WILL NOT BE ACCURATE.
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Engine Oil System Level Servicing Figure 301/TASK 12-13-79-991-006 R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-79 Page 305 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
(1) Examine the oil level between 15 minutes and 2 hours of shutdown. If the engine shutdown was more than two hours ago, you must dry motor the engine so that the engine oil pressure is stable (Ref. TASK 7100-00-720-816). This is necessary so that the oil in the system returns to the oil tank and so that the level indication is accurate. (2) Use a flashlight and find the engine oil level sightglass on the oil tank. (3) If necessary, clean the sightglass with one of the methods as follows: (a) Use a cloth, cotton, lint free (Material No. P05-005) and wipe the sightglass so that it is clean. (b) Or Use SPOP 208 (Ref. TASK 70-57-00-910-802) with Nylon Pads and Rolls, Abrasive impregnated (Material No. P05-421) a or Scrub Pad (Material No. P05-422) to clean the sightglass so that it is clean. (4) Examine the oil level in the sightglass as follows: CAUTION : YOU MUST EXAMINE THE OIL LEVEL BETWEEN 15 MINUTES AND 2 _______ HOURS AFTER SHUTDOWN. IF YOU DO NOT, THE OIL LEVEL SIGHTGLASS INDICATION WILL NOT BE ACCURATE. (a) If the oil level is in the green area, do not add oil and close the access door: - FOR 4030EM1 417DL FOR 4030EM2 427DL (b) If the oil level is below the green area, service the engine oil system as follows. NOTE : The oil can expand from heat during engine operation. This ____ can cause the oil level indication to be above the full mark. This is acceptable. NOTE : If the aircraft is not parked level, the oil level ____ indication in the sightglass is affected and may be above the full mark. This is acceptable.
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Subtask 12-13-79-610-054 B. Service the Engine Oil System (Without Pressure Fill Equipment) WARNING : BEFORE YOU REMOVE THE OIL TANK CAP, YOU MUST WAIT A MINIMUM OF _______ 5 MINUTES AFTER SHUTDOWN TO LET THE OIL PRESSURE BLEED OFF. THE HOT OIL CAN BURN YOUR EYES AND SKIN. WARNING : DO NOT OPEN THE OIL TANK CAP IF THE SIGHTGLASS OIL INDICATION _______ IS ABOVE THE FULL MARK. IF YOU DO OPEN THE CAP WHEN THE OIL IS ABOVE FULL, THE HOT OIL WILL SPILL FROM THE FILLER OPENING. THE HOT OIL CAN BURN YOUR EYES AND SKIN. (1) Wait a minimum of five minutes after shutdown before you open the oil tank cap. (2) Loosen and remove the oil tank cap only if the oil level in the sightglass is below the green area. (3) Add the oil: CAUTION : WE RECOMMEND THAT YOU DO NOT MIX DIFFERENT BRANDS OF OIL. _______ IF YOU DO, ENGINE DAMAGE CAN BE THE RESULT. (a) Add the correct oil, lubricating, turbine engine (Material No. P03-001) into the filler neck until no more oil can be added without overflow into the scupper drain. NOTE : It is permitted to mix different brands of oil when you ____ service the engine oil system as specified in Service Bulletin N⁰. 238. NOTE : The stable oil level in the sightglass will now be in the ____ green area. NOTE : If the aircraft is not parked level, the oil level ____ indication in the sightglass is affected and may be above the full mark. This is acceptable. The oil system is serviced correctly if no more oil can be added without overflow into the scupper drain. (4) Install the oil tank cap as follows: (a) With the handle at open, align and install the cap to the filler neck. (b) Push down on the cap and turn the handle clockwise to close.
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(c) Push the handle into the cap to lock the cap. (d) Make sure that the cap is installed equally and completely. (5) Close the upper thrust reverser access door: - FOR 4030EM1 417DL - FOR 4030EM2 427DL. (6) Write the amount of oil that you added. Subtask 12-13-79-610-055 C. Service the Engine Oil System (With Pressure Fill Equipement): WARNING : DO NOT OPEN THE OIL TANK CAP IF THE SIGHTGLASS OIL INDICATION _______ IS ABOVE THE FULL MARK. IF YOU DO OPEN THE CAP WHEN THE OIL IS ABOVE FULL, THE HOT OIL WILL SPILL FROM THE FILLER OPENING. THE HOT OIL CAN BURN YOUR EYES AND SKIN. (1) Do not open the oil tank cap for this pressure fill procedure. (2) Lift the lever and remove the dust cover from the oil pressure fill valve. (3) Drain the hose: WARNING : YOU MUST CONNECT THE DRAIN HOSE TO THE OVERFLOW DRAIN _______ CONNECTOR AND PUT THE DRAIN HOSE INTO A COLLECTOR/CONTAINER BEFORE YOU CONNECT THE PRESSURE FILL HOSE TO THE ENGINE OIL FILL CONNECTOR. MAKE THE DRAIN HOSE HANG STRAIGHT DOWN. MAKE SURE THAT THE HOSE IS ABOVE AND NOT INTO THE FLUID IN THE COLLECTOR/CONTAINER. WHEN YOU CONNECT THE PRESSURE FILL HOSE, THE DRAIN CONNECTOR (LINE) OPENS AUTOMATICALLY AND RELEASES THE PRESSURE IN THE OIL SYSTEM. WHEN YOU RELEASE THE PRESSURE, OIL AND AIR CAN SPRAY FROM THE OVERFLOW CONNECTOR. (a) Put the drain hose into the fluid drain collector/container and make sure that the end of the hose is not in the fluid. (4) Connect the drain hose to the (larger) overflow connector before you connect the pressure fill hose. NOTE : Some oil can come out of the overflow connector if you connect ____ the pressure fill hose first.
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(5) Connect the pressure fill hose from the pressure fill service unit to the (smaller) pressure fill connector. (6) Add the oil: CAUTION : DO NOT MIX TYPES OF OIL WHEN YOU ADD OR REPLACE THE ENGINE _______ OIL. (a) Use the pressure fill service unit and add the correct oil, lubricating, turbine engine (Material No. P03-001) at a maximum pressure of 100 psi (6.8947 bar). (7) Fill the oil tank until oil comes out the drain hose. NOTE : If the aircraft is not parked level, the oil level indication ____ in the sightglass is affected and may be above the full mark. This is acceptable. The oil system is serviced correctly if no more oil can be added without overflow from the drain hose. NOTE : The oil fill pressure connector has a restrictor so that the ____ rate of oil pressure fill is less then the rate of the gravity drain. This prevents you from putting too much oil in the system. (8) Remove the pressure hose from the pressure fill valve. (9) After the oil drains, remove the drain hose. (10) Install the dust cover to the pressure fill valve assembly and turn the handle to lock the cover. (11) Close the upper thrust reverser access door: - FOR 4030EM1 417DL - FOR 4030EM2 427DL. (12) Write the amount of oil that you added.
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5. Close-up ________ Subtask 12-13-79-865-061 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2 Subtask 12-13-79-410-058 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Close the access door 811. (4) Remove the access platform(s). Subtask 12-13-79-862-065 C. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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TASK 12-13-79-610-807 Filling the Engine Oil System after the Replacement of an Oil System Component WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE AFTER THE ENGINE IS SHUTDOWN. _______ THE ENGINE CAN STAY HOT FOR A LONG TIME AFTER THE ENGINE IS SHUTDOWN. WARNING : USE PROTECTIVE CLOTHING WHEN YOU USE ENGINE OIL. OIL CAN CAUSE SKIN _______ IRRITATION. CAUTION : DO NOT OPERATE THE ENGINE WITHOUT SUFFICIENT OIL. THIS WILL CAUSE A _______ POSSIBLE INFLIGHT SHUTDOWN AND POSSIBLE DAMAGE TO THE ENGINE. CAUTION : YOU MUST DO THIS SERVICING PROCEDURE TO PREVENT TOO MUCH OIL IN THE _______ OIL SYSTEM. DO NOT OPERATE THE ENGINE WITH TOO MUCH OIL. THIS WILL CAUSE A POSSIBLE IN FLIGHT SHUTDOWN AND POSSIBLE DAMAGE TO THE ENGINE. CAUTION : DO NOT LET ENGINE FUEL OR OIL FALL ON THE ENGINE. YOU MUST _______ IMMEDIATELY REMOVE UNWANTED FUEL OR OIL WITH A CLOTH. THE FUEL OR OIL CAN CAUSE DAMAGE TO SOME ENGINE PARTS. CAUTION : DO NOT MOTOR THE ENGINE WITHOUT OIL IN THE OIL TANK. IF THE OIL WAS _______ DRAINED DURING MAINTENANCE, YOU WILL FILL THE TANK BEFORE YOU MOTOR THE ENGINE. IF YOU DO NOT DO THIS, DAMAGE TO THE ENGINE CAN OCCUR. 1. __________________ Reason for the Job To fill the engine oil system after the replacement of an oil system component. NOTE : Do not use this filling task for normal servicing of the engine oil. ____ To service the engine oil system for normal maintenance (Ref. TASK 12-13-79-610-80600). NOTE : Do not use this filling task for changing the engine oil. To change ____ the engine oil (Ref. TASK 12-13-79-610-80800). NOTE : If the engine oil tank was not drained, begin this task in step 4. C. ____ NOTE : If you see black oil in the oil system, refer to Inspection for ____ Black Oil (Ref. TASK 79-00-00-280-80400). Black oil may be an indication of a serious problem or it can be a condition that requires no maintenance action.
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2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No
specific specific specific specific specific specific
circuit breaker(s) safety clip(s) drain hose pressure fill service unit adjustable access platform 1.22 m (4 ft.) fluid drain container 10 USgal (37.8544 l) access platform 2.5 m (8 ft. 2 in.)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
P03-001
* oil, lubricating, turbine engine (Ref. 70-30-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-13-79-610-806 24-42-00-861-801 24-42-00-862-801 71-00-00-720-816 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801 78-30-00-040-804 78-30-00-410-801 78-30-00-440-804 12-13-79-991-007
Servicing of the Engine Oil System Energize the Ground Service Network De-energize the Ground Service Network Test No. 2 - Engine Motor Leak Test (Dry Method) Thrust Reverser Cowl Doors Open Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Deactivation of the Thrust Reverser for Maintenance Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Reactivation of the Thrust Reverser after Maintenance Fig. 302
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3. __________ Job Set-up Subtask 12-13-79-860-050 A. Aircraft Maintenance Configuration (1) Make sure that the ground service network is energized (Ref. TASK 24-42-00-861-801). (2) Make sure that the engine 1, (2) shut-down occurred not less than 5 minutes before you do this procedure. Subtask 12-13-79-010-088 B. Get Access (1) Make sure that the access platform is in position at the access door 811. (2) Make sure that the access door 811 is open. (3) Make sure that the protective door of the AC/DC emergency power center 740VU is open. (4) Make sure that the left and right aft fan cowl doors is open: (Ref. TASK 71-13-00-010-802) - FOR 4030EM1 415BL, 416BR - FOR 4030EM2 425BL, 426BR (5) Make sure that the left thrust reverser is open: (Ref. TASK 78-30-00010-801) - FOR 4030EM1 417AL - FOR 4030EM2 427AL (6) Make sure that the adjustable access platform is in position. Subtask 12-13-79-040-056 C. Make sure that the thrust reverser is unserviceable (Ref. TASK 78-30-00040-804)
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Subtask 12-13-79-865-063 D. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 4. Procedure _________ (Ref. Fig. 302/TASK 12-13-79-991-007) Subtask 12-13-79-610-067 A. If the oil tank was drained during maintenance, fill the oil tank (without pressure fill equipment) as follows: NOTE : If you use the pressure fill equipment go to step B. ____ (1) Loosen and remove the oil tank cap. (2) Add the engine oil: CAUTION : WE RECOMMEND THAT YOU DO NOT MIX DIFFERENT BRANDS OF OIL. _______ IF YOU DO, ENGINE DAMAGE CAN BE THE RESULT. (a) Add the correct oil, lubricating, turbine engine (Material No. P03-001) into the filler neck until no more oil can be added without overflow into the scupper drain. NOTE : It is permitted to mix different brands of oil when you ____ service the engine oil system as specified in Service Bulletin No. 238. NOTE : The stable oil level in the sightglass will now be in the ____ green area.
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Engine Oil Filling after Replacement of an Oil System Component Figure 302/TASK 12-13-79-991-007 R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-79 Page 315 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
NOTE : If the aircraft is not parked level, the oil level ____ indication in the sightglass is affected. The oil engine system is serviced correctly if no more oil can be added without overflow into the scupper drain. (3) Install the oil tank cap as follows: (a) With the handle at open, align and install the cap to the filler neck (b) Push down on the cap and turn the handle clockwise to close (c) Push the handle into the cap to lock the cap (d) Make sure that the cap is installed equally and completely. (4) Write the amount of oil that you added. Subtask 12-13-79-610-068 B. If the oil tank was drained during maintenance, fill the oil tank (with pressure fill equipment) as follows: (1) If removed, install the oil tank cap for this pressure fill procedure as follows: (a) With the handle at open, align and install the cap to the filler neck (b) Push down on the cap and turn the handle clockwise to close (c) Push the handle into the cap to lock the cap (d) Make sure that the cap is installed equally and completely. (2) Lift the lever and remove the dust cover from the oil pressure fill valve.
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(3) Install and connect the drain hose: WARNING : YOU MUST CONNECT THE DRAIN HOSE TO THE OVERFLOW DRAIN _______ CONNECTOR AND PUT THE DRAIN HOSE INTO A COLLECTOR/CONTAINER BEFORE YOU CONNECT THE PRESSURE FILL HOSE TO THE ENGINE OIL FILL CONNECTOR. MAKE THE DRAIN HOSE HANG STRAIGHT DOWN. MAKE SURE THAT THE HOSE IS ABOVE AND NOT INTO THE FLUID IN THE COLLECTOR/CONTAINER. WHEN YOU CONNECT THE PRESSURE FILL HOSE, THE DRAIN CONNECTOR (LINE) OPENS AUTOMATICALLY AND RELEASES THE PRESSURE IN THE OIL SYSTEM. WHEN YOU RELEASE THE PRESSURE, OIL AND AIR CAN SPRAY FROM THE OVERFLOW CONNECTOR. (a) Put the drain hose into the fluid drain container and make sure that the end of the hose is not in the fluid. (4) Connect the drain hose to the (larger) overflow connector before you connect the pressure fill hose. NOTE : Some oil can come out of the overflow connector if you connect ____ the pressure fill hose first. (5) Connect the pressure fill hose from the pressure fill service unit to the (smaller) pressure fill connector. (6) Add the engine oil: CAUTION : WE RECOMMEND THAT YOU DO NOT MIX DIFFERENT BRANDS OF OIL. _______ IF YOU DO, ENGINE DAMAGE CAN BE THE RESULT. (a) Use the pressure fill service unit and add the correct oil, lubricating, turbine engine (Material No. P03-001) at a maximum pressure of 100 psi (6.90 bar). (7) Fill the oil tank until oil comes out the drain hose. NOTE : It is permitted to mix different brands of oil when you ____ service the engine oil system as specified in Service Bulletin No. 238. NOTE : The oil fill pressure connector has a restrictor so that the ____ rate of oil pressure fill is less than the rate of the gravity drain. This prevents you from putting too much oil in the system. NOTE : If the aircraft is not parked level, the oil level indication ____ in the sightglass is affected. The engine oil system is
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serviced correctly if no more oil can be added without overflow from the drain hose. (8) Remove the pressure hose from the pressure fill valve. (9) After the oil drains, remove the drain hose. (10) Install the dust cover to the pressure fill valve assembly and turn the handle to lock the cover. (11) Write the amount of oil that you added. Subtask 12-13-79-410-075 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the left thrust reverser: (Ref. TASK 78-30-00-410-801) - FOR 4030EM1 417AL - FOR 4030EM2 427AL Subtask 12-13-79-865-062 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2 Subtask 12-13-79-700-050 E. Turn the engine: CAUTION : DO NOT OPERATE THE ENGINE. YOU CAN ONLY TURN THE ENGINE WITH _______ THE STARTER LONG ENOUGH TO: - PUMP THE OIL INTO THE OIL TANK - REMOVE ANY UNWANTED AIR FROM THE OIL SYSTEM. (1) Turn (dry motor) the power plant so that the engine oil pressure is stable (Ref. TASK 71-00-00-720-816). NOTE : Do not exceed 5 minutes of starter operation. ____
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Subtask 12-13-79-865-086 F. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-13-79-010-089 G. Get Access (1) Open the left thrust reverser: (Ref. TASK 78-30-00-010-801) - FOR 4030EM1 417AL - FOR 4030EM2 427AL Subtask 12-13-79-610-056 H. Fill the Engine Oil System (Without Pressure Fill Equipment) NOTE : If you use pressure fill equipment go to step J. ____ (1) Loosen and remove the oil tank cap. (2) Add the engine oil: CAUTION : DO NOT MIX TYPES OF OIL WHEN YOU ADD OR REPLACE THE ENGINE _______ OIL. (a) Add the correct oil, lubricating, turbine engine (Material No. P03-001) into the filler neck until no more oil can be added without overflow into the scupper drain. NOTE : The stable oil level in the sightglass will now be in the ____ green area. NOTE : If the aircraft is not parked level, the oil level ____ indication in the sightglass is affected. The oil engine
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system is serviced correctly if no more oil can be added without overflow into the scupper drain. (3) Install the oil tank cap as follows: (a) With the handle at open, align and install the cap to the filler neck (b) Push down on the cap and turn the handle clockwise to close (c) Push the handle into the cap to lock the cap (d) Make sure that the cap is installed equally and completely. (4) Write the amount of oil that you added. Subtask 12-13-79-610-057 J. Fill the Engine Oil System (With Pressure Fill Equipment) (1) If removed, install the oil tank cap for this pressure fill procedure as follows: (a) With the handle at open, align and install the cap to the filler neck (b) Push down on the cap and turn the handle clockwise to close (c) Push the handle into the cap to lock the cap (d) Make sure that the cap is installed equally and completely. (2) Lift the lever and remove the dust cover from the oil pressure fill valve. (3) Install and connect the drain hose: WARNING : YOU MUST CONNECT THE DRAIN HOSE TO THE OVERFLOW DRAIN _______ CONNECTOR AND PUT THE DRAIN HOSE INTO A COLLECTOR/CONTAINER BEFORE YOU CONNECT THE PRESSURE FILL HOSE TO THE ENGINE OIL FILL CONNECTOR. MAKE THE DRAIN HOSE HANG STRAIGHT DOWN. MAKE SURE THAT THE HOSE IS ABOVE AND NOT INTO THE FLUID IN THE COLLECTOR/CONTAINER. WHEN YOU CONNECT THE PRESSURE FILL HOSE, THE DRAIN CONNECTOR (LINE) OPENS AUTOMATICALLY AND RELEASES THE PRESSURE IN THE OIL SYSTEM. WHEN YOU RELEASE THE PRESSURE, OIL AND AIR CAN SPRAY FROM THE OVERFLOW CONNECTOR.
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(a) Put the drain hose into the fluid drain container and make sure that the end of the hose is not in the fluid. (4) Connect the drain hose to the (larger) overflow connector before you connect the pressure fill hose. NOTE : Some oil can come out of the overflow connector if you connect ____ the pressure fill hose first. (5) Connect the pressure fill hose from the pressure fill service unit to the (smaller) pressure fill connector. (6) Add the engine oil: CAUTION : WE RECOMMEND THAT YOU DO NOT MIX DIFFERENT BRANDS OF OIL. _______ IF YOU DO, ENGINE DAMAGE CAN BE THE RESULT. (a) Use the pressure fill service unit and add the correct oil, lubricating, turbine engine (Material No. P03-001) at a maximum pressure of 100 psi (6.90 bar). (7) Fill the oil tank until oil comes out the drain hose. NOTE : It is permitted to mix different brands of oil when you ____ service the engine oil system as specified in Service Bulletin No. 238. NOTE : The oil fill pressure connector has a restrictor so that the ____ rate of oil pressure fill is less than the rate of the gravity drain. This prevents you from putting too much oil in the system. NOTE : If the aircraft is not parked level, the oil level indication ____ in the sightglass is affected. The engine oil system is serviced correctly if no more oil can be added without overflow from the drain hose. (8) Remove the pressure hose from the pressure fill valve. (9) After the oil drains, remove the drain hose. (10) Install the dust cover to the pressure fill valve assembly and turn the handle to lock the cover. (11) Write the amount of oil that you added.
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Subtask 12-13-79-410-076 K. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the left thrust reverser: (Ref. TASK 78-30-00-410-801) - FOR 4030EM1 417AL - FOR 4030EM2 427AL Subtask 12-13-79-865-064 L. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2 Subtask 12-13-79-700-051 M. Turn (dry motor) the power plant so that the engine oil pressure is stable (Ref. TASK 71-00-00-720-816). NOTE : Do not exceed 5 minutes of starter operation. ____ Subtask 12-13-79-610-058 N. Service the engine oil system again. See servicing of the engine oil system (Ref. TASK 12-13-79-610-806). 5. Close-up ________ Subtask 12-13-79-440-056 A. Make the thrust reverser serviceable (Ref. TASK 78-30-00-440-804)
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Subtask 12-13-79-410-077 B. Close Access (1) Close the left and right aft fan cowl doors: (Ref. TASK 71-13-00-410802) - FOR 4030EM1 415BL, 416BR - FOR 4030EM2 425BL, 426BR (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Close the access door 811. (4) Remove the access platform(s). Subtask 12-13-79-862-064 C. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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TASK 12-13-79-610-808 Changing the Oil in the Engine Oil System WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE AFTER THE ENGINE IS SHUTDOWN. _______ THE ENGINE CAN STAY HOT FOR A LONG TIME AFTER THE ENGINE IS SHUTDOWN. WARNING : USE PROTECTIVE CLOTHING WHEN YOU USE ENGINE OIL. OIL CAN CAUSE SKIN _______ IRRITATION. CAUTION : DO NOT OPERATE THE ENGINE WITHOUT SUFFICIENT OIL. THIS WILL CAUSE A _______ POSSIBLE INFLIGHT SHUTDOWN AND POSSIBLE DAMAGE TO THE ENGINE. CAUTION : YOU MUST DO THIS SERVICING PROCEDURE TO PREVENT TOO MUCH OIL IN THE _______ OIL SYSTEM. DO NOT OPERATE THE ENGINE WITH TOO MUCH OIL. THIS WILL CAUSE A POSSIBLE IN FLIGHT SHUTDOWN AND POSSIBLE DAMAGE TO THE ENGINE. CAUTION : DO NOT LET ENGINE FUEL OR OIL FALL ON THE ENGINE. YOU MUST _______ IMMEDIATELY REMOVE UNWANTED FUEL OR OIL WITH A CLOTH. THE FUEL OR OIL CAN CAUSE DAMAGE TO SOME ENGINE PARTS. 1. __________________ Reason for the Job To change the engine oil. NOTE : Do not use this oil changing task for normal servicing of the engine ____ oil. To service the engine oil system for normal maintenance (Ref. TASK 12-13-79-610- 80600). NOTE : Do not use this oil changing task for filling the engine with oil ____ after replacement on an oil system component. To fill the oil the engine oil system after the replacement of an oil system component (Ref. TASK 12-13-79-610-80700). NOTE : If you see black oil in the oil system, refer to Inspection for ____ Black Oil (Ref. TASK 79-00-00-280-80400). Black oil may be an indication of a serious problem or it can a condition that requires no maintenance action.
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2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No
specific specific specific specific specific specific specific
circuit breaker(s) safety clip(s) drain hose pressure fill service unit adjustable access platform 1.22 m (4 ft.) fluid drain container 10 USgal (37.8544 l) access platform 2.5 m (8 ft. 2 in.) Torque Wrench : range 36.00 to 220.00 lbf.in (0.40 to 2.60 m.daN)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
P03-001
Material No.
P11-027
* oil, lubricating, turbine engine (Ref. 70-30-00) * solvent, petroleum (Ref. 70-30-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------3
packing
72-62-11 43 -060
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D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-13-79-610-806 24-42-00-861-801 24-42-00-862-801 71-00-00-720-816 71-13-00-010-802 71-13-00-410-802 72-34-13-000-801 72-34-13-400-801 78-30-00-010-801 78-30-00-040-804 78-30-00-410-801 78-30-00-440-804 79-21-22-000-801 79-21-22-400-801 79-22-11-000-801 79-22-11-400-801 12-13-79-991-008 12-13-79-991-009
Servicing of the Engine Oil System Energize the Ground Service Network De-energize the Ground Service Network Test No. 2 - Engine Motor Leak Test (Dry Method) Thrust Reverser Cowl Doors Open Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Removal of the Fan Exit Liner (Inner) Segments Installation of the Fan Exit Liner (Inner) Segments Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Deactivation of the Thrust Reverser for Maintenance Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Reactivation of the Thrust Reverser after Maintenance Removal of the Main Oil Filter Element (5010EN) Installation of the Main Oil Filter Element (5010EN) Removal of the Magnetic Chip Detectors (5006EN) Installation of the Magnetic Chip Detectors (5006EN) Fig. 303 Fig. 304
3. __________ Job Set-up Subtask 12-13-79-861-064 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-79-941-064 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure.
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Subtask 12-13-79-010-085 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU. Subtask 12-13-79-865-065 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-13-79-010-086 E. Get Access (1) Open the left and right aft fan cowl doors: (Ref. TASK 71-13-00-010802) - FOR 4030EM1 415BL, 416BR - FOR 4030EM2 425BL, 426BR Subtask 12-13-79-040-055 F. Make the thrust reverser unserviceable (Ref. TASK 78-30-00-040-804)
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Subtask 12-13-79-010-087 G. Get Access (1) Open the left and right thrust reverser: (Ref. TASK 78-30-00-010-801) - FOR 4030EM1 417AL, 418AR - FOR 4030EM2 427AL, 428AR (2) Put the adjustable access platform in position. 4. Procedure _________ (Ref. Fig. 303/TASK 12-13-79-991-008, 304/TASK 12-13-79-991-009) Subtask 12-13-79-680-052 A. Drain the oil from the engine oil system WARNING : BEFORE YOU REMOVE THE OIL TANK CAP, YOU MUST WAIT A MINIMUM OF _______ 5 MINUTES AFTER SHUTDOWN TO LET THE OIL PRESSURE BLEED OFF. THE HOT OIL CAN BURN YOUR EYES AND SKIN. WARNING : DO NOT OPEN THE OIL TANK CAP IF THE SIGHTGLASS OIL INDICATION _______ IS ABOVE THE FULL MARK. IF YOU DO OPEN THE CAP WHEN THE OIL IS ABOVE FULL, THE HOT OIL WILL SPILL FROM THE FILLER OPENING. THE HOT OIL CAN BURN YOUR EYES AND SKIN. CAUTION : INSTALL PROTECTION COVERS OVER ALL OPENINGS AS SOON AS POSSIBLE _______ TO PREVENT ENGINE DAMAGE. CAUTION : DO NOT MOTOR THE ENGINE WHEN THE ENGINE OIL IS DRAINED. IF IT _______ IS MOTORED WITHOUT ANY OIL, DAMAGE TO THE ENGINE CAN OCCUR. (1) Wait a minimum of five minutes after shutdown before you open the oil tank cap. (2) Loosen and remove the oil tank cap. NOTE : Some hot oil can drain out of the filler neck if the oil level ____ is above the full mark on the oil level sightglass. (3) Drain the oil tank as follows: (a) Remove the magnetic chip detector from the oil tank and let the oil drain (Ref. TASK 79-22-11-000-801).
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Engine Oil Changing Figure 303/TASK 12-13-79-991-008 R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-79 Page 329 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
Engine Oil Changing Figure 304/TASK 12-13-79-991-009 R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-79 Page 330 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
(4) Install oil tank cap loosely as follows: (a) Put the oil tank cap over the fill opening (b) Do not push and engage the cap to the filler neck (c) Do not turn and lock the cap in position. NOTE : This prevents dirt and dust in the oil tank. ____ (5) Remove the magnetic chip detector from the front of the main gearbox and let the oil drain (Ref. TASK 79-22-11-000-801). NOTE : You must remove the detail probe and the valve from the main ____ gearbox. (6) Drain the angle gearbox as follows: (a) Remove the fan exit liner segment (inner) at 6 oclock position (Ref. TASK 72-34-13-000-801). (b) Put the fluid drain container under the angle gearbox (c) Remove the two bolts (1), washers (2) and the plug (4) from the right side of the angle gearbox. (d) Discard the packing (3) from the plug. (e) Let all the oil drain from the angle gearbox. (7) Remove the main oil filter element and let the oil drain (Ref. TASK 79-21-22-000-801). (8) Remove the four magnetic chip detectors from the lubrication and scavenge oil pump and let the oil drain (Ref. TASK 79-22-11-000-801). NOTE : You must remove the detail probes and the valves from the oil ____ pump. (9) Clean all the magnetic chip detectors with solvent, petroleum (Material No. P11-027), then dry them with a clean cloth. (10) Let the engine oil drain for a minimum of 30 minutes. NOTE : This will let the engine oil completely drain from all the ____ components.
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Subtask 12-13-79-420-050 B. Install the Engine Parts after Draining CAUTION : REMOVE THE PROTECTION COVERS FROM THE OPENINGS AS NECESSARY TO _______ PREVENT ENGINE DAMAGE. (1) Install the magnetic chip detectors (Ref. TASK 79-22-11-400-801). (2) Install the main oil filter element (Ref. TASK 79-21-22-400-801). (3) Install the plug (4) to the angle gearbox as follows: (a) Apply oil, lubricating, turbine engine (Material No. P03-001) to the two bolts (1) and the new packing (3) (b) Install the new packing (3) to the plug (4) (c) Install the plug (4) with the two washers (2) and bolts (1) to the right side of the angle gearbox. (d) TORQUE the bolts (1) to between 85 and 95 lbf.in (0.96 and 1.07 m.daN). (e) Install the fan exit liner segment (inner) at 6 oclock position (Ref. TASK 72-34-13-400-801). Subtask 12-13-79-610-059 C. Fill the Engine Oil System (Without Pressure Fill Equipment). (1) Loosen and remove the oil tank cap. (2) Add the engine oil: CAUTION : WE RECOMMEND THAT YOU DO NOT MIX DIFFERENT BRANDS OF OIL. _______ IF YOU DO, ENGINE DAMAGE CAN BE THE RESULT. (a) Add the correct oil, lubricating, turbine engine (Material No. P03-001) into the filler neck until no more oil can be added without overflow into the scupper drain. NOTE : It is permitted to mix different brands of oil when you ____ service the engine oil system as specified in Service Bulletin No. 238.
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NOTE : The stable oil level in the sightglass will now be in the ____ green area. NOTE : If the aircraft is not parked level, the oil level ____ indication in the sightglass is affected. The engine oil system is serviced correctly if no more oil can be added without overflow into the scupper drain. (3) Install the oil tank cap as follows: (a) With the handle at open, align and install the cap to the filler neck (b) Push down on the cap and turn the handle clockwise to close (c) Push the handle into the cap to lock the cap (d) Make sure that the cap is installed equally and completely. (4) Write the amount of oil that you added. Subtask 12-13-79-610-060 D. Fill the Engine Oil System (With Pressure Fill Equipment). (1) Install the oil tank cap for this pressure fill procedure as follows: (a) With the handle at open, align and install the cap to the filler neck. (b) Push down on the cap and turn the handle clockwise to close. (c) Push the handle into the cap to lock the cap. (d) Make sure that the cap is installed equally and completely. (2) Lift the lever and remove the dust cover from the oil pressure fill valve.
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(3) Install and connect the drain hose: WARNING : YOU MUST CONNECT THE DRAIN HOSE TO THE OVERFLOW DRAIN _______ CONNECTOR AND PUT THE DRAIN HOSE INTO A COLLECTOR/CONTAINER BEFORE YOU CONNECT THE PRESSURE FILL HOSE TO THE ENGINE OIL FILL CONNECTOR. MAKE THE DRAIN HOSE HANG STRAIGHT DOWN. MAKE SURE THAT THE HOSE IS ABOVE AND NOT INTO THE FLUID IN THE COLLECTOR/CONTAINER. WHEN YOU CONNECT THE PRESSURE FILL HOSE, THE DRAIN CONNECTOR (LINE) OPENS AUTOMATICALLY AND RELEASES THE PRESSURE IN THE OIL SYSTEM. WHEN YOU RELEASE THE PRESSURE, OIL AND AIR CAN SPRAY FROM THE OVERFLOW CONNECTOR. (a) Put the drain hose into the fluid drain container and make sure that the end of the hose is not in the fluid. (4) Connect the drain hose to the (larger) overflow connector before you connect the pressure fill hose. NOTE : Some oil can come out of the overflow connector if you connect ____ the pressure fill hose first. (5) Connect the pressure fill hose from the pressure fill service unit to the (smaller) pressure fill connector. (6) Add the engine oil: CAUTION : DO NOT MIX TYPES OF OIL WHEN YOU ADD OR REPLACE THE ENGINE _______ OIL. (a) Use the pressure fill service unit and add the correct oil, lubricating, turbine engine (Material No. P03-001) at a maximum pressure of 100 psi (6.90 bar). (7) Fill the oil tank until oil comes out the drain hose. NOTE : The oil fill pressure connector has a restrictor so that the ____ rate of oil pressure fill is less then the rate of the gravity drain. This prevents you from putting too much oil in the system. NOTE : If the aircraft is not parked level, the oil level indication ____ in the sightglass is affected. The engine oil system is serviced correctly if no more oil can be added without overflow from the drain hose. (8) Remove the pressure hose from the pressure fill valve.
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(9) After the oil drains, remove the drain hose. (10) Install the dust cover to the oil pressure fill valve assembly and turn the handle to lock the cover. (11) Write the amount of oil that you added. Subtask 12-13-79-410-073 E. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the left and right thrust reverser: (Ref. TASK 78-30-00-410801) - FOR 4030EM1 417AL, 418AR - FOR 4030EM2 427AL, 428AR Subtask 12-13-79-440-055 F. Make the thrust reverser serviceable (Ref. TASK 78-30-00-440-804) Subtask 12-13-79-865-066 G. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2 Subtask 12-13-79-700-052 H. Turn (dry motor) the power plant so that the engine oil pressure is stable (Ref. TASK 71-00-00-720-816). NOTE : Do not exceed 5 minutes of starter operation. ____ Subtask 12-13-79-610-061 J. Service the engine oil system again. See servicing of the engine oil system (Ref. TASK 12-13-79-610-806).
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5. Close-up ________ Subtask 12-13-79-410-074 A. Close Access (1) Close the left and right aft fan cowl doors: (Ref. TASK 71-13-00-410802) - FOR 4030EM1 415BL, 416BR - FOR 4030EM2 425BL, 426BR (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Close the access door 811. (4) Remove the access platform(s). Subtask 12-13-79-862-063 B. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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TASK 12-13-79-170-802 Flushing the Oil in the Engine Oil System. WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE AFTER THE ENGINE IS SHUTDOWN. _______ THE ENGINE CAN STAY HOT FOR A LONG TIME AFTER THE ENGINE IS SHUTDOWN. WARNING : USE PROTECTIVE CLOTHING WHEN YOU USE ENGINE OIL. OIL CAN CAUSE SKIN _______ IRRITATION. CAUTION : DO NOT OPERATE THE ENGINE WITHOUT SUFFICIENT OIL. THIS WILL CAUSE A _______ POSSIBLE INFLIGHT SHUTDOWN AND POSSIBLE DAMAGE TO THE ENGINE. CAUTION : YOU MUST DO THIS SERVICING PROCEDURE TO PREVENT TOO MUCH OIL IN THE _______ OIL SYSTEM. DO NOT OPERATE THE ENGINE WITH TOO MUCH OIL. THIS WILL CAUSE A POSSIBLE IN FLIGHT SHUTDOWN AND POSSIBLE DAMAGE TO THE ENGINE. CAUTION : DO NOT LET ENGINE FUEL OR OIL FALL ON THE ENGINE. YOU MUST _______ IMMEDIATELY REMOVE UNWANTED FUEL OR OIL WITH A CLOTH. THE FUEL OR OIL CAN CAUSE DAMAGE TO SOME ENGINE PARTS. 1. __________________ Reason for the Job To flush the engine oil. NOTE : It is only necessary to flush the engine oil system for these ____ reasons: A different type or brand of oil is to be used. The engine has oil system contamination. Preservation for 60 days or less (Method I). 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
circuit breaker(s) safety clip(s) adjustable access platform 1.22 m (4 ft.) access platform 2.5 m (8 ft. 2 in.)
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B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-13-79-610-808 24-42-00-861-801 24-42-00-862-801 71-00-00-720-824 71-00-00-860-818 71-00-00-860-820 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801 78-30-00-040-804 78-30-00-410-801 78-30-00-440-804
Changing the Oil in the Engine Oil System Energize the Ground Service Network De-energize the Ground Service Network Test No. 3A - Idle Power Test (Reverser Open) Normal Engine Automatic Start Procedure Engine Shutdown Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Deactivation of the Thrust Reverser for Maintenance Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Reactivation of the Thrust Reverser after Maintenance
3. __________ Job Set-up Subtask 12-13-79-861-063 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-79-941-063 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure. Subtask 12-13-79-010-082 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU.
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Subtask 12-13-79-865-083 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-13-79-010-083 E. Get Access (1) Open the left and right aft fan cowl doors: (Ref. TASK 71-13-00-010802) - FOR 4030EM1 415BL, 416BR - FOR 4030EM2 425BL, 426BR Subtask 12-13-79-040-054 F. Make the thrust reverser unserviceable (Ref. TASK 78-30-00-040-804) Subtask 12-13-79-010-084 G. Get Access (1) Open the left and right thrust reverser: (Ref. TASK 78-30-00-010-801) - FOR 4030EM1 417AL, 418AR - FOR 4030EM2 427AL, 428AR (2) Put the adjustable access platform in position. Subtask 12-13-79-610-065 H. Change the oil in the engine oil system (Ref. TASK 12-13-79-610-808). NOTE : When you change the oil, you drain the system, install a new oil ____ filter element, and fill the system.
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4. Procedure _________ Subtask 12-13-79-710-051 A. Operate the Engine (1) Start and operate the engine at idle power for 2 - 5 minutes (Ref. TASK 71-00-00-860-818) and (Ref. TASK 71-00-00-720-824). (2) Shut down the engine by shutdown procedures (Ref. TASK 71-00-00-860820). Subtask 12-13-79-610-066 B. Change the oil in the engine oil system again (Ref. TASK 12-13-79-610808). NOTE : When you change the oil, you drain the system, install a new oil ____ filter element, and fill the system. 5. Close-up ________ Subtask 12-13-79-410-071 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the left and right thrust reverser: (Ref. TASK 78-30-00-410801) - FOR 4030EM1 417AL, 418AR - FOR 4030EM2 427AL, 428AR Subtask 12-13-79-440-054 B. Make the thrust reverser serviceable (Ref. TASK 78-30-00-440-804)
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Subtask 12-13-79-865-084 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2 Subtask 12-13-79-410-072 D. Close Access (1) Close the left and right aft fan cowl doors: (Ref. TASK 71-13-00-410802) - FOR 4030EM1 415BL, 416BR - FOR 4030EM2 425BL, 426BR (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Close the access door 811. (4) Remove the access platform(s). Subtask 12-13-79-862-062 E. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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ENGINE OIL - SERVICING ______________________ TASK 12-13-79-610-809 To Service the Engine Oil System WARNING : YOU MUST BE CAREFUL WHEN YOU DO WORK ON THE ENGINE PARTS AFTER THE _______ ENGINE IS SHUTDOWN. THE ENGINE PARTS CAN STAY HOT FOR ALMOST 1 HOUR. R R R
WARNING : YOU MUST NOT LET ENGINE OIL STAY ON YOUR SKIN. FLUSH THE OIL FROM _______ YOUR SKIN WITH WATER. THE OIL IS POISONOUS AND CAN BE ABSORBED INTO THE BODY.
R R R R
CAUTION : YOU MUST NOT LET ENGINE FUEL OR OIL FALL ON THE ENGINE. UNWANTED FUEL _______ OR OIL MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT-FREE CLOTH. THE FUEL OR OIL CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job The procedure that follows tells you how to fill the engine oil system with approved oil. This can be done by the gravity fill procedure or the pressure fill procedure. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R R
No specific No specific No specific No specific No specific No specific UT954 U999092 3409536
circuit breaker(s) safety clip(s) drain hose pressure fill service unit clean container 0.5 USgal (1.8927 l) adjustable access platform 1.22 m (4 ft.) access platform 2.5 m (8 ft. 2 in.) 1 ADAPTER - OIL TANK 1 HOSE - OIL TANK 1 GUN - OIL TANK
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B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
OMAT 1011
Material No.
OMAT 238
* engine lubricating, oil (synthetic) (Ref. 70-30-00) * lockwire 0.028 to 0.031 in. (0.71 to 0.79 m) dia (Ref. 70-30-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R
24-42-00-861-801 24-42-00-862-801 71-00-00-860-810 71-00-00-860-814 72-61-00-000-801 79-00-00-280-805 12-13-79-991-011 12-13-79-991-019
Energize the Ground Service Network De-energize the Ground Service Network Engine Automatic Start Engine Shutdown Removal of the External Gearbox Module Do a Check for Fuel Contamination of the Engine Oil Fig. 301 Fig. 302
3. __________ Job Set-up Subtask 12-13-79-861-058 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-79-941-058 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure. Subtask 12-13-79-010-068 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811.
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(3) Open the protective door of the AC/DC emergency power-center 740VU. Subtask 12-13-79-865-073 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-13-79-010-069 E. Get Access (1) Put the adjustable access platform in the correct position at the right side of the engine position. (2) Open the access panel on the right fan cowl door: - FOR 4030EM1 416CR - FOR 4030EM2 426CR Subtask 12-13-79-612-055 F. Do a Check of the Engine Oil Level in the Oil Tank Sight Glass NOTE : You must wait a minimum of 10 minutes after the engine has stopped ____ before you do a check of the oil level. This will let the oil level become stable. (1) If the engine has been stopped for less than 6 hours and the oil level is low, fill the engine oil tank. (2) If the engine has been stopped for more than 6 hours and the oil level is low, but above the 5 US QUARTS (4.73 l) REQUIRED level: (a) Do not fill the engine oil system. (b) Start the engine (Ref. TASK 71-00-00-860-810).
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(c) Run the engine at idle for 2 minutes. R R
(d) Shut down the engine (Ref. TASK 71-00-00-860-814).
R
(e) Do a check of the engine oil level again. If the oil level is low, fill the engine oil tank. NOTE : You must wait a minimum of 10 minutes after the engine has ____ stopped before you do a check of the oil level. This will let the oil level become stable.
R
(3) If the engine has been stopped for more than 6 hours and the oil level is below the 5 US QUARTS (4.73 l) REQUIRED level: (a) Drain the external gearbox (Ref. TASK 72-61-00-000-801). (b) Fill the engine oil tank. (c) Start the engine (Ref. TASK 71-00-00-860-810). (d) Run the engine at idle for 2 minutes.
R R
(e) Shut down the engine (Ref. TASK 71-00-00-860-814).
R
(f) Do a check of the engine oil level again. If the oil level is low, fill the engine oil tank. NOTE : You must wait a minimum of 10 minutes after the engine has ____ stopped before you do a check of the oil level. This will let the oil level become stable.
R R
(4) If the oil level is low after you do a dry or wet motor procedure, do the steps that follow:
R R R R
CAUTION : YOU MUST NOT ADD OIL TO THE ENGINE AFTER YOU DO A DRY OR _______ WET MOTOR PROCEDURE. THE OIL WILL NOT GO BACK TO THE OIL TANK FULLY AND WILL SHOW AN INCORRECT OIL LEVEL. TOO MUCH OIL IN THE ENGINE CAN CAUSE DAMAGE TO THE ENGINE.
R
(a) Do not fill the oil system.
R
(b) Start the engine (Ref. TASK 71-00-00-860-810).
R
(c) Run the engine at idle for 2 minutes.
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R
(d) Shut down the engine (Ref. TASK 71-00-00-860-814).
R R
(e) Do a check of the engine oil level after a minimum of 10 minutes. If the oil level is low, fill the engine oil tank. 4. Procedure _________ (Ref. Fig. 301/TASK 12-13-79-991-011, 302/TASK 12-13-79-991-019) Subtask 12-13-79-612-056 A. Fill the Engine Oil Tank (Gravity Fill Procedure) CAUTION : IF YOU CHANGE TO A DIFFERENT APPROVED OIL TYPE, YOU MUST ADD _______ THE REPLACEMENT OIL TO THE TANK DURING THE REGULAR SERVICING OF THE ENGINE. IT IS VERY IMPORTANT THAT YOU DO NOT DRAIN THE OIL SYSTEM AND FILL IT WITH THE REPLACEMENT OIL IN ONE OPERATION. IF YOU DO NOT OBEY THIS INSTRUCTION, YOU CAN CAUSE DAMAGE TO THE ENGINE. NOTE : It is recommended that you use the same oil type, when you fill ____ the engine oil system. If there is no oil of the same type available, use one of the other oils from the approved list. (1) Remove the oil filler cap (1) from the oil tank. (2) If you can smell fuel in the oil tank when you remove the oil filler cap, do a check for fuel contamination of the engine oil (Ref. TASK 79-00-00-280-805). (3) Add engine lubricating, oil (synthetic) (Material No. OMAT 1011) to the engine oil tank. (a) Add clean, approved engine lubricating, oil (synthetic) (Material No. OMAT 1011) to the engine oil tank. Make sure the correct level can be seen in the oil tank sight indicator. (b) Install the oil filler cap (1) to the engine oil tank. NOTE : Make sure the seal ring (2) is fully engaged in the groove ____ of the oil filler cap (1). If it is loose, replace the seal ring. This will make sure of the correct installation of the filler cap and prevent oil tank leaks.
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Engine Oil Tank-Oil Fill Location Figure 301/TASK 12-13-79-991-011 EFF : 701-749, 12-13-79 Page 306 Config-2 Apr 01/05 R SROS
Engine Oil Tank-Oil Fill Location (SB79-C455) Figure 302/TASK 12-13-79-991-019 EFF : 701-749, 12-13-79 Page 307 Config-2 Apr 01/05 R SROS
Subtask 12-13-79-612-057 B. Fill the Engine Oil Tank (Pressure Fill Procedure) CAUTION : IF YOU CHANGE TO A DIFFERENT APPROVED OIL TYPE, YOU MUST ADD _______ THE REPLACEMENT OIL TO THE TANK DURING THE REGULAR SERVICING OF THE ENGINE. IT IS VERY IMPORTANT THAT YOU DO NOT DRAIN THE OIL SYSTEM AND FILL IT WITH THE REPLACEMENT OIL IN ONE OPERATION. IF YOU DO NOT OBEY THIS INSTRUCTION, YOU CAN CAUSE DAMAGE TO THE ENGINE. NOTE : It is recommended that you use the same oil type, when you fill ____ the engine oil system. If there is no oil of the same type available, use one of the other oils from the approved list. PRE SB79-C455 (1) Remove the lockwire from the pressure fill (3) and overflow (2) couplings. (2) Remove the dust caps from the pressure fill (3) and overflow (2) couplings. (3) Install the drain hose to the overflow coupling (2). (4) If you can smell fuel when you install the drain hose, do para 4.C. (5) Add engine lubricating, oil (synthetic) (Material No. OMAT 1011) to the engine oil tank. (a) Get the pressure fill service unit or the GUN - OIL TANK (3409536), HOSE - OIL TANK (U999092), and the ADAPTER - OIL TANK (UT954). (b) Put the open end of the overflow drain hose in to the clean container. (c) If a pressure fill service unit is to be used, do the steps that follow: 1 _
Connect the pressure fill service unit to the pressure fill coupling (3) on the oil tank.
2 _
Add approved, clean engine lubricating, oil (synthetic) (Material No. OMAT 1011) to the tank until the correct level is seen in the oil tank sight indicator.
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NOTE : A small quantity of oil will drain from the overflow ____ drain hose when the oil is at the correct level. 3 _
Disconnect the pressure fill service unit from the pressure fill coupling (3).
4 _
Disconnect the overflow drain hose from the overflow coupling (2).
5 _
Install the dust caps on the pressure fill (3) and overflow (2) couplings.
6 _
Safety the dust caps together with lockwire 0.028 to 0.031 in. (0.71 to 0.79 m) dia (Material No. OMAT 238).
(d) If the GUN - OIL TANK (3409536) is to be used, do the steps that follow: 1 _
Install the ADAPTER - OIL TANK (UT954) to the pressure fill coupling (3).
2 _
Connect the HOSE - OIL TANK (U999092) to the ADAPTER - OIL TANK (UT954), on the pressure fill coupling (3).
3 _
Connect the GUN - OIL TANK (3409536), to the HOSE - OIL TANK (U999092).
4 _
Use the GUN - OIL TANK (3409536) to add clean engine lubricating, oil (synthetic) (Material No. OMAT 1011) to the tank until the correct level is seen in the oil tank sight indicator. NOTE : A small quantity of oil will drain from the overflow ____ drain hose when the oil is at the correct level.
5 _
Disconnect the GUN - OIL TANK (3409536) from the HOSE - OIL TANK (U999092) and disconnect the HOSE - OIL TANK (U999092) from the ADAPTER - OIL TANK (UT954).
6 _
Disconnect the ADAPTER - OIL TANK (UT954) from the pressure fill coupling (3).
7 _
Disconnect the overflow drain hose from the overflow coupling (2).
8 _
Install the dust caps on the pressure fill (3) and overflow (2) couplings.
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9 _
Safety the dust caps together, with lockwire 0.028 to 0.031 in. (0.71 to 0.79 m) dia (Material No. OMAT 238).
5. Close-up ________ Subtask 12-13-79-865-074 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2 Subtask 12-13-79-410-062 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Close the access door 811. (4) Close the access panel on the right fan cowl door: - FOR 4030EM1 416CR - FOR 4030EM2 426CR (5) Remove the access platform(s). Subtask 12-13-79-862-057 C. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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TASK 12-13-79-680-801 Drain the Engine Oil System WARNING : YOU MUST BE CAREFUL WHEN YOU DO WORK ON THE ENGINE PARTS AFTER THE _______ ENGINE IS SHUTDOWN. THE ENGINE PARTS CAN STAY HOT FOR ALMOST 1 HOUR. WARNING : YOU MUST NOT TOUCH HOT PARTS WITHOUT APPLICABLE GLOVES. HOT PARTS CAN _______ CAUSE AN INJURY. IF YOU GET AN INJURY PUT IT IN COLD WATER FOR 10 MINUTES AND GET MEDICAL AID. WARNING : YOU MUST NOT LET ENGINE OIL STAY ON YOUR SKIN. FLUSH THE OIL FROM _______ YOUR SKIN WITH WATER. THE OIL IS POISONOUS AND CAN BE ABSORBED INTO THE BODY. CAUTION : YOU MUST NOT MOTOR THE ENGINE AFTER THE OIL TANK IS DRAINED. IF YOU _______ MOTOR THE ENGINE THE OIL TANK IS DRAINED, DAMAGE TO THE ENGINE CAN OCCUR. CAUTION : YOU MUST NOT PUT OIL THAT HAS BEEN DRAINED FROM THE ENGINE BACK INTO _______ THE OIL SYSTEM. CONTAMINATION IN THE OIL CAN CAUSE DAMAGE TO SOME PARTS OR FAILURE OF THE OIL. CAUTION : YOU MUST NOT LET ENGINE FUEL OR OIL FALL ON THE ENGINE. UNWANTED FUEL _______ OR OIL MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT-FREE CLOTH. THE FUEL OR OIL CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No
specific specific specific specific
circuit breaker(s) safety clip(s) container 10 USgal (40 liter) access platform 2.5 m (8 ft. 2 in.) Torque Wrench : range 36.00 to 220.00 lbf.in (0.40 to 2.60 m.daN)
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B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
OMat 2-142
Material No.
OMat 238
Material No.
OMat2-142
* Safety Cable (Ref. 70-30-00) * lockwire 0.028 to 0.031 in. (0.71 to 0.79 mm) (Ref. 70-30-00) * Safety Cable (Ref. 70-30-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
R
1 1 1 1 1 2 2 2 2 2
seal ring seal ring seal ring seal ring seal ring seal ring washer washer washer washer
79-21-41 79-22-46 79-22-46 79-22-46 79-22-46 72-61-00 79-22-51 79-22-51 79-22-51 79-22-51
60 -150 61 -030 61A-030 61B-030 61C-030 61 -020 61 -020 61 -020A 61 -020B 61 -070
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 70-02-01-910-801 70-12-04-910-804 70-12-04-910-806 71-13-00-010-805 71-13-00-410-805 79-22-43-100-801 79-22-45-920-801 12-13-79-991-013
Energize the Ground Service Network De-energize the Ground Service Network Identification, Lubrication and Fitting of Flexible Seal Rings Locking Techniques - Wire locking Locking Techniques - Safety Cable Open the Fan Cowl Doors Close the Fan Cowl Doors Cleaning of the Pressure Oil Filter Element (5004EN) Remove, Discard and Replace Oil Scavenge Filter Fig. 303
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-13-79-991-014 12-13-79-991-015 12-13-79-991-016 12-13-79-991-017 12-13-79-991-018
Fig. Fig. Fig. Fig. Fig.
304 305 306 307 308
3. __________ Job Set-up Subtask 12-13-79-861-065 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-79-941-065 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure. Subtask 12-13-79-010-090 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU. Subtask 12-13-79-865-087 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74
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Subtask 12-13-79-010-091 E. Get Access (1) Open the fan cowl doors (Ref. TASK 71-13-00-010-805): - FOR 4030EM1 415AL, 416AR - FOR 4030EM2 425AL, 426AR 4. Procedure _________ Subtask 12-13-79-680-054 A. Drain the Engine Oil System (1) Drain the oil tank (Ref. Fig. 303/TASK 12-13-79-991-013) (a) Put the clean container 10 USgal (40 liter) in position to catch the oil. R R
(b) Remove the drain plug (1) from the oil tank and let all the oil drain into the container.
R
(c) Remove and discard the washer (2).
R
(d) Install a new washer (2) on the drain plug (1) (Ref. TASK 70-0201-910-801).
R
(e) Install the drain plug (1) in the oil tank.
R R
(f) TORQUE the drain plug (1) to 205 lbf.in (2.31 m.daN). (2) Drain the Air/Oil Heat Exchanger (AOHE). (Ref. Fig. 304/TASK 12-13-79-991-014) (a) Put the container 10 USgal (40 liter) in position to catch the oil.
R R
(b) Remove and discard the safety cable/lockwire from the drain plug (1) on the AOHE. (c) Remove the drain plug (1) from the AOHE and let all the oil drain into the container.
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Drain Plug on the Oil Tank Figure 303/TASK 12-13-79-991-013 EFF : 701-749, 12-13-79 Page 315 Config-2 Apr 01/02 R SROS
Drain Plug on the Air/Oil Heat Exchanger Figure 304/TASK 12-13-79-991-014 EFF : 701-749, 12-13-79 Page 316 Config-2 Oct 01/00 SROS
(d) Remove and discard the washer (2). (e) Install a new washer (2) on the drain plug (1) (Ref. TASK 70-0201-910-801). (f) Install the drain plug (1) in the AOHE. (g) TORQUE the drain plug (1) to between 40 and 50 lbf.in (0.45 and 0.56 m.daN). (h) Safety the drain plug (1) with safety cable 0.032 in.(0.81 mm) Safety Cable (Material No. OMat 2-142), (Ref. TASK 70-12-04-910806), or with the lockwire 0.028 to 0.031 in. (0.71 to 0.79 mm) (Material No. OMat 238), (Ref. TASK 70-12-04-910-804). (3) Drain the external gearbox module (Ref. Fig. 305/TASK 12-13-79-991-015) (a) Put the container 10 USgal (40 liter) in position to catch the oil. (b) Remove and discard the safety cable/lockwire from the drain plug (1) on the gearbox module. (c) Remove the drain plug (1) from the gearbox module and let all the oil drain into the container. (d) Remove and discard the seal ring (2). R
(e) Install a new seal ring (2) on the drain plug (1) (Ref. TASK 7002-01-910-801). (f) Install the drain plug (1) in the gearbox module. (g) TORQUE the drain plug (1) to between 202 and 220 lbf.in (2.28 and 2.48 m.daN). (h) Safety the drain plug (1) with safety cable 0.032 in.(0.81 mm) Safety Cable (Material No. OMat2-142), (Ref. TASK 70-12-04-910806), or with the lockwire 0.028 to 0.031 in. (0.71 to 0.79 mm) (Material No. OMat 238), (Ref. TASK 70-12-04-910-804). (4) Drain the bevel gears housing (Ref. Fig. 306/TASK 12-13-79-991-016) (a) Put the container 10 USgal (40 liter) in position to catch the oil.
EFF : 701-749, 12-13-79 Page 317 Config-2 Jul 01/04 SROS
Drain Plug on the External Gearbox Module Figure 305/TASK 12-13-79-991-015 EFF : 701-749, 12-13-79 Page 318 Config-2 Oct 01/00 SROS
Drain Plug on the Bevel Gears Housing Figure 306/TASK 12-13-79-991-016 EFF : 701-749, 12-13-79 Page 319 Config-2 Oct 01/00 SROS
R R
(b) Remove and discard the safety cable/lockwire from the drain plug (1) on the housing. (c) Remove the drain plug (1) from the housing and let all the oil drain into the container. (d) Remove and discard the seal ring (2). (e) Install a new seal ring (2) on the drain plug (1) (Ref. TASK 7002-01-910-801). (f) Install the drain plug (1) in the housing. (g) TORQUE the drain plug (1) to between 202 and 220 lbf.in (2.28 and 2.48 m.daN).
R R R R
(h) Safety the drain plug (1) with safety cable 0.032 in.(0.81 mm) Safety Cable (Material No. OMat 2-142), (Ref. TASK 70-12-04-910806), or with the lockwire 0.028 to 0.031 in. (0.71 to 0.79 mm) (Material No. OMat 238), (Ref. TASK 70-12-04-910-804). (5) Clean the pressure filter element (Ref. TASK 79-22-43-100-801). (6) Replace the scavenge filter element (Ref. TASK 79-22-45-920-801). (7) Drain the oil from the Fuel Oil Heat Exchanger (FOHE) (Ref. Fig. 307/TASK 12-13-79-991-017) (a) Put the container 10 USgal (40 liter) in position to catch the oil.
R R
(b) Remove and discard the safety cable/lockwire from the drain plug (2). (c) Remove the drain plug (2) from the FOHE and let all the oil drain into the container. (d) Remove and discard the seal ring (1). (e) Install a new seal ring (1) and the drain plug (2) (Ref. TASK 7002-01-910-801). (f) Install the drain plug (2) in the FOHE. (g) TORQUE the drain plug (2) to between 110 and 120 lbf.in (1.24 and 1.35 m.daN).
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Drain Plug on Fuel/Oil Heat Exchanger Figure 307/TASK 12-13-79-991-017 EFF : 701-749, 12-13-79 Page 321 Config-2 Oct 01/00 SROS
R R R R
(h) Safety the drain plug (2) with safety cable 0.032 in.(0.81 mm) Safety Cable (Material No. OMat 2-142), (Ref. TASK 70-12-04-910806), or with the lockwire 0.028 to 0.031 in. (0.71 to 0.79 mm) (Material No. OMat 238), (Ref. TASK 70-12-04-910-804). (8) Drain the oil from the oil pump assembly (Ref. Fig. 308/TASK 12-13-79-991-018) (a) Put the container 10 USgal (40 liter) in position to catch the oil. (b) Remove the bolts (4) and the washers (3) from each of the Magnetic Chip Detector (MCD) housing blanks (2). (c) Remove the MCD housing blanks (2) and let all the oil drain into the container. (d) Remove and discard the seal rings (1) from the housing blanks (2). (e) Install a new seal ring (1) on each housing blank (2) (Ref. TASK 70-02-01-910-801). (f) Put the housing blanks (2) in position and install the bolts (4) and the washers (3). (g) TORQUE the bolts (4) to 100 lbf.in (1.13 m.daN). Subtask 12-13-79-865-088 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2 5. Close-up ________ Subtask 12-13-79-410-078 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the protective door of the AC/DC emergency power center 740VU.
EFF : 701-749, 12-13-79 Page 322 Config-2 Jul 01/03 SROS
Magnetic Chip Detector - Housing Blank Figure 308/TASK 12-13-79-991-018 EFF : 701-749, 12-13-79 Page 323 Config-2 Jul 01/03 R SROS
(3) Close the access door 811. (4) Close the fan cowl doors (Ref. TASK 71-13-00-410-805): - FOR 4030EM1 415AL, 416AR - FOR 4030EM2 425AL, 426AR (5) Remove the access platform(s). Subtask 12-13-79-862-066 B. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : 701-749, 12-13-79 Page 324 Config-2 Jul 01/03 R SROS
ENGINE STARTING - SERVICING ___________________________ TASK 12-13-80-612-802 Servicing of the Starter (Pressure and Gravity Fill - with Thrust Reverser Cowl Doors Open) WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE AFTER THE ENGINE IS SHUTDOWN. _______ THE ENGINE CAN STAY HOT FOR A LONG TIME AFTER THE ENGINE IS SHUTDOWN. WARNING : USE PROTECTIVE CLOTHING WHEN YOU USE ENGINE OIL. OIL CAN CAUSE SKIN _______ IRRITATION. CAUTION : DO NOT OPERATE THE STARTER WITHOUT SUFFICIENT OIL. THIS WILL CAUSE _______ DAMAGE TO THE STARTER. CAUTION : DO NOT OPERATE THE STARTER WITH TOO MUCH OIL. THIS WILL CAUSE DAMAGE _______ TO THE STARTER. CAUTION : DO NOT LET ENGINE FUEL OR OIL FALL ON THE ENGINE. YOU MUST _______ IMMEDIATELY REMOVE UNWANTED FUEL OR OIL WITH A CLOTH. THE FUEL OR OIL CAN CAUSE DAMAGE TO SOME ENGINE PARTS. 1. __________________ Reason for the Job Replenish starter oil with the thrust reverser open. NOTE : Do not use this servicing task for draining and filling the starter. ____ To drain and fill the starter oil (Ref. TASK 12-13-80-610-803). 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No
specific specific specific specific specific specific specific specific
circuit breaker(s) safety clip(s) drain hose flashlight fluid drain container 5 USgal (19 l) pressure fill service unit squeeze bottle adjustable access platform 1.22 m (4 ft.) access platform 2.5 m (8 ft. 2 in.)
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------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
Torque Wrench : range 5.00 to 35.00 lbf.in (0.05 to 0.40 m.daN)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
P03-001
Material No.
P05-287
* oil, lubricating, turbine engine (Ref. 70-30-00) * lockwire 0.020 in. (0.50 mm) dia. (Ref. 70-30-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------16 16
packing packing
80-11-11 40 -190 80-11-11 40A-190
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801 78-30-00-040-804 78-30-00-410-801 78-30-00-440-804 12-13-80-991-002
Energize the Ground Service Network De-energize the Ground Service Network Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Deactivation of the Thrust Reverser for Maintenance Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Reactivation of the Thrust Reverser after Maintenance Fig. 301
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3. __________ Job Set-up Subtask 12-13-80-861-054 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-80-941-055 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure. Subtask 12-13-80-010-062 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU. Subtask 12-13-80-865-058 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-13-80-010-063 E. Get Access (1) Open the left and right aft fan cowl doors (Ref. TASK 71-13-00-010802): - FOR 4030EM1 415BL, 416BR - FOR 4030EM2
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425BL, 426BR Subtask 12-13-80-040-053 F. Deactivation of the Thrust Reverser. WARNING : YOU MUST DEACTIVATE THE THRUST REVERSER DIRECTIONAL CONTROL _______ VALVE (DCV) BEFORE YOU WORK ON OR AROUND THE TRANSLATING COWL. IF YOU DO NOT DEACTIVATE THE DCV, YOU CAN CAUSE ACCIDENTAL THRUST REVERSER OPERATION AND INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT. (1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 7830-00-040-804). Subtask 12-13-80-010-064 G. Get Access (1) Open the left and right thrust reverser cowl doors (Ref. TASK 78-3000-010-801): - FOR 4030EM1 417AL, 418AR - FOR 4030EM2 427AL, 428AR (2) Put the adjustable access platform in position. 4. Procedure _________ (Ref. Fig. 301/TASK 12-13-80-991-002) Subtask 12-13-80-210-052 A. Make a Check of the Starter Oil Level (1) Use a flashlight and find the oil level sightglass on the right side of the starter attached to the rear of the main gearbox. (2) If necessary, wipe the sightglass to make it clean. (3) Examine the oil level in the starter as follows: (a) If the oil level in the sightglass is between three quarters and seven eighths, do not fill the starter.
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(b) If the oil level in the sightglass is at approximately three quarters or below, you must service the starter as follows. (c) If the oil level in the sightglass is above the sightglass, the oil level in the starter is more than necessary and you must service the starter as follows. NOTE : The starter is full when the oil level shows approximately ____ seven eighths full on the sightglass. Subtask 12-13-80-612-053 B. Service the Starter (without Pressure Fill Equipment) CAUTION : INSTALL PROTECTION COVERS OVER ALL OPENINGS AS SOON AS POSSIBLE _______ TO PREVENT ENGINE DAMAGE. (1) Put the fluid drain container 5 USgal (19 l) under the starter. (2) Remove the lockwire and fill plug (15). (3) Discard the packing (16) from the plug (15). (4) If the oil in the starter is more than necessary, let the oil drain from the fill port until it only drips. NOTE : The oil level in the sightglass will now show at approximately ____ seven eighths. The starter is full when the oil level shows approximately seven eighths full on the sightglass. (5) If the oil in the starter is less than necessary, fill the starter to an acceptable level as follows: (a) Fill a standard squeeze bottle with clean oil, lubricating, turbine engine (Material No. P03-001). (b) Attach a piece of flex hose approximately 6 in. (152.40 mm) long to the squeeze bottle. (c) Put the flex hose into the fill port of the starter and squeeze the oil into the starter until oil drips from the fill port. NOTE : The oil level in the sightglass will now show at ____ approximately seven eighths. The starter is full when the oil level shows approximately seven eighths full on the sightglass.
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Starter Oil Level Servicing - Thrust Reverser Cowl Doors Open Figure 301/TASK 12-13-80-991-002- 12 (SHEET 1) R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-80 Page 306 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
Starter Oil Level Servicing - Thrust Reverser Cowl Doors Open Figure 301/TASK 12-13-80-991-002- 22 (SHEET 2) R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-80 Page 307 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
(6) Install the fill plug (15) as follows: CAUTION : REMOVE THE PROTECTION COVERS FROM THE OPENINGS AS NECESSARY _______ TO PREVENT ENGINE DAMAGE. (a) Apply oil, lubricating, turbine engine (Material No. P03-001) to the new packing (16) and the threads of the plug (15). (b) Install the new packing (16) to the plug (15). (c) Install the plug (15) to the fill port. (d) TORQUE the plug (15) to between 20 and 30 lbf.in (0.22 and 0.33 m.daN). (e) Safety the plug (15) with lockwire 0.020 in. (0.50 mm) dia. (Material No. P05-287). Subtask 12-13-80-612-054 C. Service the Starter (with Pressure Fill Equipment) (1) Remove the coupling covers from the overflow drain quick disconnect coupling and the pressure fill quick disconnect coupling on the air starter duct bracket. (2) Put the end of the drain hose in the fluid drain container 5 USgal (19 l). (3) Connect the drain hose fitting to the overflow drain quick disconnect (larger) coupling on the air starter duct bracket. NOTE : Some oil can come out of the drain hose when you connect the ____ drain hose. (4) Connect the pressure fill hose from the pressure fill service unit to the pressure fill quick disconnect (smaller) coupling on the air starter duct bracket. (5) Fill the starter as follows: CAUTION : MAKE SURE THAT YOU ATTACH THE DRAIN HOSE TO THE OVERFLOW _______ DRAIN QUICK DISCONNECT COUPLING BEFORE YOU TRY AND FILL THE STARTER. IF YOU DO NOT CONNECT THE DRAIN HOSE FIRST, YOU CAN PUT TOO MUCH PRESSURE INSIDE THE STARTER AND DAMAGE CAN OCCUR.
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(a) Use the pressure fill service unit and add the correct oil, lubricating, turbine engine (Material No. P03-001) until the oil comes out of the drain hose. (6) Remove the pressure hose from the coupling at the air starter duct bracket. (7) Install the coupling cover to the pressure fill quick disconnect coupling. (8) When the oil from the drain hose decreases to a drip, disconnect the drain hose from the overflow drain quick disconnect coupling on the air starter duct bracket. (9) Install the coupling cover to the overflow drain quick disconnect coupling. NOTE : The oil level in the sightglass will now show at approximately ____ seven eighths. The starter is full when the oil level shows approximately seven eighths full on the sightglass. 5. Close-up ________ Subtask 12-13-80-410-062 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the left and right thrust reverser cowl doors (Ref. TASK 78-3000-410-801): - FOR 4030EM1 417AL, 418AR - FOR 4030EM2 427AL, 428AR Subtask 12-13-80-440-053 B. Make the thrust reverser serviceable (Ref. TASK 78-30-00-440-804).
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Subtask 12-13-80-865-059 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2 Subtask 12-13-80-410-064 D. Close Access (1) Close the left and right aft fan cowl doors (Ref. TASK 71-13-00-410802): - FOR 4030EM1 415BL, 416BR - FOR 4030EM2 425BL, 426BR (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Close the access door 811. (4) Remove the access platform(s). Subtask 12-13-80-862-057 E. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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TASK 12-13-80-610-803 R R
Change Starter Oil (with the Threaded Type Starter Magnetic Chip Detector (Vickers/Tedeco)) WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE AFTER THE ENGINE IS SHUTDOWN. _______ THE ENGINE CAN STAY HOT FOR A LONG TIME AFTER THE ENGINE IS SHUTDOWN. WARNING : USE PROTECTIVE CLOTHING WHEN YOU USE ENGINE OIL. OIL CAN CAUSE SKIN _______ IRRITATION. CAUTION : DO NOT OPERATE THE STARTER WITHOUT SUFFICIENT OIL. THIS WILL CAUSE _______ DAMAGE TO THE STARTER. CAUTION : DO NOT OPERATE THE STARTER WITH TOO MUCH OIL. THIS WILL CAUSE DAMAGE _______ TO THE STARTER. CAUTION : DO NOT LET ENGINE FUEL OR OIL FALL ON THE ENGINE. YOU MUST _______ IMMEDIATELY REMOVE UNWANTED FUEL OR OIL WITH A CLOTH. THE FUEL OR OIL CAN CAUSE DAMAGE TO SOME ENGINE PARTS. CAUTION : WHEN YOU REPLACE THE STARTER DUE TO FAILURE OR OIL CONTAMINATION, YOU _______ MUST REPLACE ALL OIL SERVICING HARDWARE INCLUDING THE OIL SERVICE LINES, PLUGS, AND FITTINGS. IF YOU DO NOT DO THIS, YOU CAN TRANSFER THE OIL CONTAMINATION INTO THE NEW STARTER. 1. __________________ Reason for the Job Refer to the MPD TASK: 800000-P2 To change (drain and fill) the starter oil. To drain and fill the starter oil for replacement of the starter. To drain and fill the starter oil after fluid contamination.
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2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No
specific specific specific specific specific specific specific specific
circuit breaker(s) safety clip(s) drain hose fluid drain container 5 USgal (19 l) pressure fill service unit squeeze bottle adjustable access platform 1.22 m (4 ft.) access platform 2.5 m (8 ft. 2 in.) Torque Wrench : range 5.00 to 35.00 lbf.in (0.05 to 0.40 m.daN)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
P03-001
Material No.
P05-287
* oil, lubricating, turbine engine (Ref. 70-30-00) * lockwire 0.020 in. (0.50 mm) dia. (Ref. 70-30-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------39 39 39 41 41 46 46
packing packing packing packing packing packing packing
80-11-18 80-11-18 80-11-18 80-11-18 80-11-18 80-11-11 80-11-11
40 -030 40 -030A 40A-030 40 -010 40A-010 40 -190 40A-190
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D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-13-80-612-802 24-42-00-861-801 24-42-00-862-801 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801 78-30-00-040-804 78-30-00-410-801 78-30-00-440-804 80-11-11-000-801 80-11-11-400-801 12-13-80-991-003
Servicing of the Starter (Pressure and Gravity Fill with Thrust Reverser Cowl Doors Open) Energize the Ground Service Network De-energize the Ground Service Network Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Deactivation of the Thrust Reverser for Maintenance Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Reactivation of the Thrust Reverser after Maintenance Removal of the Starter (5000ES) Installation of the Starter (5000ES) Fig. 302
3. __________ Job Set-up Subtask 12-13-80-861-052 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-80-941-053 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure. Subtask 12-13-80-010-056 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU.
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Subtask 12-13-80-865-054 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-13-80-010-057 E. Get Access (1) Open the left and right aft fan cowl doors (Ref. TASK 71-13-00-010802): - FOR 4030EM1 415BL, 416BR - FOR 4030EM2 425BL, 426BR Subtask 12-13-80-040-051 F. deactivation of the Thrust Reverser. WARNING : YOU MUST DEACTIVATE THE THRUST REVERSER DIRECTIONAL CONTROL _______ VALVE (DCV) BEFORE YOU WORK ON OR AROUND THE TRANSLATING COWL. IF YOU DO NOT DEACTIVATE THE DCV, YOU CAN CAUSE ACCIDENTAL THRUST REVERSER OPERATION AND INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT. (1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 7830-00-040-804). Subtask 12-13-80-010-058 G. Get Access (1) Open the right thrust reverser cowl door (Ref. TASK 78-30-00-010801): - FOR 4030EM1 418AR - FOR 4030EM2
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428AR (2) Open the lower left thrust reverser access door: - FOR 4030EM1 417EL - FOR 4030EM2 427EL (3) Put the adjustable access platform in position. 4. Procedure _________ (Ref. Fig. 302/TASK 12-13-80-991-003) Subtask 12-13-80-680-051 A. Drain the Oil from the Starter WARNING : BE CAREFUL WHEN YOU DRAIN OIL FROM A HOT ENGINE. HOT OIL IS _______ DANGEROUS. IF IT TOUCHES YOUR BODY OR EYES IT WILL BURN BADLY. CAUTION : WHEN YOU REPLACE THE STARTER DUE TO FAILURE OR OIL _______ CONTAMINATION, YOU MUST REPLACE ALL OIL SERVICING HARDWARE INCLUDING THE OIL SERVICE LINES, PLUGS, AND FITTINGS. IF YOU DO NOT DO THIS, YOU CAN TRANSFER THE OIL CONTAMINATION INTO THE NEW STARTER. CAUTION : INSTALL PROTECTION COVERS OVER ALL OPENINGS AS SOON AS POSSIBLE _______ TO PREVENT ENGINE DAMAGE. NOTE : Do not use this draining and filling task for normal oil ____ servicing. To make a check of the starter oil level (Ref. TASK 1213-80-612-802). (1) Remove the chip detector (Threaded Type - Vickers/Tedeco) from the starter as follows: (a) Put the fluid drain container 5 USgal (19 l) under the starter. CAUTION : DO NOT PUT CONTAMINATED OIL DRAINED FROM THE STARTER _______ BACK INTO THE OIL CART. IF YOU DO NOT DO THIS, YOU CAN TRANSFER THE OIL CONTAMINATION INTO THE OIL CART. (b) Remove the lockwire from the magnetic chip detector probe (38). (c) Remove the magnetic chip detector probe (38) from the valve (40).
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Starter Oil Draining and Filling Figure 302/TASK 12-13-80-991-003- 12 (SHEET 1)
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Starter Oil Draining and Filling Figure 302/TASK 12-13-80-991-003- 22 (SHEET 2)
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(d) Discard the packing (39) from the probe (38). (2) Examine the magnetic chip detector probe (38) as follows: (a) If you find metallic chips larger than 0.100 in. (2.54 mm) you must remove the starter (Ref. TASK 80-11-11-000-801). (b) If you find metallic chips smaller than 0.100 in. (2.54 mm), remove the chips from the probe (38) and proceed with step (3). (c) If you find no chips, proceed with step (3). (3) Remove the valve from the starter as follows: (a) Remove the lockwire from the valve (40). (b) Discard the packing (41) from the valve (40). (c) Let the oil drain from the starter. (d) Write down the quantity of the drained oil: If the quantity of the drained oil is less than 7 OZF (207.0 ml), replace the starter (Ref. TASK 80-11-11-000-801), (Ref. TASK 8011-11-400-801). (4) Install the starter magnetic chip detector (Threaded Type Vickers/Tedeco) as follows: CAUTION : REMOVE THE PROTECTION COVERS FROM THE OPENINGS AS NECESSARY _______ TO PREVENT ENGINE DAMAGE. (a) Apply oil, lubricating, turbine engine (Material No. P03-001) to the new packing (39) and to the new packing (41). (b) Install the new packings (39) and (41) to the chip detector probe (38) and the valve (40). (c) Install the valve (40) to the starter. (d) Torque the valve as follows: CAUTION : DO NOT TORQUE THE VALVE TOO MUCH. _______ IF YOU DO, YOU WILL BREAK OFF THE END OF THE VALVE. 1 _
TORQUE the valve (40) to between 10 and 25 lbf.in (0.11 and 0.28 m.daN).
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(e) Safety the valve (40) with lockwire 0.020 in. (0.50 mm) dia. (Material No. P05-287). (f) Install the chip detector probe (38) into the valve (40). (g) Torque the probe as follows: CAUTION : DO NOT TORQUE THE PROBE TOO MUCH. _______ IF YOU DO, YOU WILL BREAK OFF THE END OF THE PROBE. 1 _
TORQUE the chip detector probe (38) to between 5 and 15 lbf.in (0.05 and 0.16 m.daN).
(h) Safety the chip detector probe (38) with lockwire 0.020 in. (0.50 mm) dia. (Material No. P05-287). Subtask 12-13-80-612-062 B. Fill the Starter (without Pressure Fill Equipment) CAUTION : WHEN YOU REPLACE THE STARTER DUE TO FAILURE OR OIL _______ CONTAMINATION, YOU MUST REPLACE ALL OIL SERVICING HARDWARE INCLUDING THE OIL SERVICE LINES, PLUGS, AND FITTINGS. IF YOU DO NOT DO THIS, YOU CAN TRANSFER THE OIL CONTAMINATION INTO THE NEW STARTER. CAUTION : INSTALL PROTECTION COVERS OVER ALL OPENINGS AS SOON AS POSSIBLE _______ TO PREVENT ENGINE DAMAGE. (1) Remove the lockwire and fill plug (47). (2) Discard the packing (46) from the fill plug (47). (3) Fill the starter to an acceptable level as follows: (a) Fill a standard squeeze bottle with clean oil, lubricating, turbine engine (Material No. P03-001). (b) Attach a piece of flex hose approximately 6 in. (152.4 mm) long to the squeeze bottle. (c) Put the flex hose into the fill port of the starter and squeeze the oil into the starter until oil drips from the fill port. NOTE : The oil level in the sightglass will now show at ____ approximately seven eighths. The starter is full when the
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oil level shows approximately seven eighths full on the sightglass. (4) Install the fill plug (47) as follows: CAUTION : REMOVE THE PROTECTION COVERS FROM THE OPENINGS AS NECESSARY _______ TO PREVENT ENGINE DAMAGE. (a) Apply oil, lubricating, turbine engine (Material No. P03-001) to the new packing (46) and the threads of the plug (47). (b) Install the new packing (46) to the plug (47). (c) Install the plug (47) to the fill port. (d) TORQUE the plug (47) to between 20 and 30 lbf.in (0.22 and 0.33 m.daN). (e) Safety the plug with lockwire 0.020 in. (0.50 mm) dia. (Material No. P05-287). Subtask 12-13-80-612-063 C. Fill the Starter (with Pressure Fill Equipment) CAUTION : WHEN YOU REPLACE THE STARTER DUE TO FAILURE OR OIL _______ CONTAMINATION, YOU MUST REPLACE ALL OIL SERVICING HARDWARE INCLUDING THE OIL SERVICE LINES, PLUGS, AND FITTINGS. IF YOU DO NOT DO THIS, YOU CAN TRANSFER THE OIL CONTAMINATION INTO THE NEW STARTER. (1) Remove the coupling covers from the overflow drain quick disconnect couplind and the pressure fill quick disconnect coupling on the air starter duct bracket. (2) Put the end of the drain hose in the fluid drain container 5 USgal (19 l). (3) Connect the drain hose to the overflow drain quick disconnect (larger) coupling on the air starter duct bracket. NOTE : Some oil can come out of the drain hose when you connect the ____ drain hose. (4) Connect the pressure fill hose from the pressure fill service unit to the pressure fill quick disconnect (smaller) coupling on the air starter duct bracket.
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(5) Fill the starter as follows: CAUTION : MAKE SURE THAT YOU ATTACH THE DRAIN HOSE TO THE OVERFLOW _______ DRAIN QUICK DISCONNECT COUPLING BEFORE YOU TRY AND FILL THE STARTER. IF YOU DO NOT CONNECT THE DRAIN HOSE FIRST, YOU CAN PUT TOO MUCH PRESSURE INSIDE THE STARTER AND DAMAGE CAN OCCUR. (a) Use the pressure fill service unit and add the correct oil, lubricating, turbine engine (Material No. P03-001) until the oil comes out of the drain hose. (6) Remove the pressure hose from the coupling on the air starter duct bracket. (7) Install the coupling cover to the pressure fill quick disconnect coupling. (8) When the oil from the drain hose decreases to a drip, disconnect the drain hose from the overflow drain quick disconnect coupling on the air starter duct bracket. (9) Install the coupling cover to the overflow drain quick disconnect coupling. NOTE : The oil level in the sightglass will now show at approximately ____ seven eighths. The starter is full when the oil level shows approximately seven eighths full on the sightglass. 5. Close-up ________ Subtask 12-13-80-410-057 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Remove the fluid drain container. (3) Close the lower left thrust reverser access door: - FOR 4030EM1 417EL - FOR 4030EM2 427EL
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(4) Close the right thrust reverser cowl door (Ref. TASK 78-30-00-410801): - FOR 4030EM1 418AR - FOR 4030EM2 428AR Subtask 12-13-80-440-051 B. Make the thrust reverser serviceable (Ref. TASK 78-30-00-440-804). Subtask 12-13-80-865-055 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2 Subtask 12-13-80-410-059 D. Close Access (1) Close the left and right aft fan cowl doors (Ref. TASK 71-13-00-410802): - FOR 4030EM1 415BL, 416BR - FOR 4030EM2 425BL, 426BR (2) Close the protective door of the AC/DC emergency power-center 740VU. (3) Close the access door 811. (4) Remove the access platform(s). Subtask 12-13-80-862-058 E. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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TASK 12-13-80-610-803- 01 R R
Change Starter Oil (with the Bayonet Type Starter Magnetic Chip Detector (Lisle)) WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE AFTER THE ENGINE IS SHUTDOWN. _______ THE ENGINE CAN STAY HOT FOR A LONG TIME AFTER THE ENGINE IS SHUTDOWN. WARNING : USE PROTECTIVE CLOTHING WHEN YOU USE ENGINE OIL. OIL CAN CAUSE SKIN _______ IRRITATION. CAUTION : DO NOT OPERATE THE STARTER WITHOUT SUFFICIENT OIL. THIS WILL CAUSE _______ DAMAGE TO THE STARTER. CAUTION : DO NOT OPERATE THE STARTER WITH TOO MUCH OIL. THIS WILL CAUSE DAMAGE _______ TO THE STARTER. CAUTION : DO NOT LET ENGINE FUEL OR OIL FALL ON THE ENGINE. YOU MUST _______ IMMEDIATELY REMOVE UNWANTED FUEL OR OIL WITH A CLOTH. THE FUEL OR OIL CAN CAUSE DAMAGE TO SOME ENGINE PARTS. CAUTION : WHEN YOU REPLACE THE STARTER DUE TO FAILURE OR OIL CONTAMINATION, YOU _______ MUST REPLACE ALL OIL SERVICING HARDWARE INCLUDING THE OIL SERVICE LINES, PLUGS, AND FITTINGS. IF YOU DO NOT DO THIS, YOU CAN TRANSFER THE OIL CONTAMINATION INTO THE NEW STARTER. 1. __________________ Reason for the Job Refer to the MPD TASK: 800000-P2 To change (drain and fill) the starter oil. To drain and fill the starter oil for replacement of the starter. To drain and fill the starter oil after fluid contamination.
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2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No
specific specific specific specific specific specific specific specific
circuit breaker(s) safety clip(s) drain hose fluid drain container 5 USgal (19 l) pressure fill service unit squeeze bottle adjustable access platform 1.22 m (4 ft.) access platform 2.5 m (8 ft. 2 in.) Torque Wrench : range 5.00 to 35.00 lbf.in (0.05 to 0.40 m.daN)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
P03-001
Material No.
P05-287
* oil, lubricating, turbine engine (Ref. 70-30-00) * lockwire 0.020 in. (0.50 mm) dia. (Ref. 70-30-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------41 41 43 44 44 44 46 46
packing packing packing packing packing packing packing packing
80-11-18 80-11-18 80-11-18 80-11-18 80-11-18 80-11-18 80-11-11 80-11-11
40 -010 40A-010 40A-040 40 -030 40 -030A 40A-030 40 -190 40A-190
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D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-13-80-612-802 24-42-00-861-801 24-42-00-862-801 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801 78-30-00-040-804 78-30-00-410-801 78-30-00-440-804 80-11-11-000-801 80-11-11-400-801 12-13-80-991-008
Servicing of the Starter (Pressure and Gravity Fill with Thrust Reverser Cowl Doors Open) Energize the Ground Service Network De-energize the Ground Service Network Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Deactivation of the Thrust Reverser for Maintenance Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Reactivation of the Thrust Reverser after Maintenance Removal of the Starter (5000ES) Installation of the Starter (5000ES) Fig. 303
3. __________ Job Set-up Subtask 12-13-80-861-059 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-80-941-060 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure. Subtask 12-13-80-010-076 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU.
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Subtask 12-13-80-865-068 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-13-80-010-077 E. Get Access (1) Open the left and right aft fan cowl doors (Ref. TASK 71-13-00-010802): - FOR 4030EM1 415BL, 416BR - FOR 4030EM2 425BL, 426BR Subtask 12-13-80-040-057 F. Deactivation of the Thrust Reverser. WARNING : YOU MUST DEACTIVATE THE THRUST REVERSER DIRECTIONAL CONTROL _______ VALVE (DCV) BEFORE YOU WORK ON OR AROUND THE TRANSLATING COWL. IF YOU DO NOT DEACTIVATE THE DCV, YOU CAN CAUSE ACCIDENTAL THRUST REVERSER OPERATION AND INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT. (1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 7830-00-040-804). Subtask 12-13-80-010-078 G. Get Access (1) Open the right thrust reverser cowl door (Ref. TASK 78-30-00-010801): - FOR 4030EM1 418AR - FOR 4030EM2
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428AR (2) Open the lower left thrust reverser access door: - FOR 4030EM1 417EL - FOR 4030EM2 427EL (3) Put the adjustable access platform in position. 4. Procedure _________ (Ref. Fig. 303/TASK 12-13-80-991-008) Subtask 12-13-80-680-052 A. Drain the Oil from the Starter WARNING : BE CAREFUL WHEN YOU DRAIN OIL FROM A HOT ENGINE. HOT OIL IS _______ DANGEROUS. IF IT TOUCHES YOUR BODY OR EYES IT WILL BURN BADLY. CAUTION : DO NOT REMOVE OR INSTALL THE CHIP DETECTOR AS AN ASSEMBLY. YOU _______ MUST REMOVE THE MAGNETIC PROBE FROM THE VALVE. IF YOU DO NOT DO THIS, YOU CAN DAMAGE THE ASSEMBLY. CAUTION : DO NOT USE TOOLS TO REMOVE OR INSTALL THE CHIP DETECTOR PROBE. _______ IF YOU DO, YOU CAN DAMAGE THE PROBE. CAUTION : WHEN YOU REPLACE THE STARTER DUE TO FAILURE OR OIL _______ CONTAMINATION, YOU MUST REPLACE ALL OIL SERVICING HARDWARE INCLUDING THE OIL SERVICE LINES, PLUGS, AND FITTINGS. IF YOU DO NOT DO THIS, YOU CAN TRANSFER THE OIL CONTAMINATION INTO THE NEW STARTER. CAUTION : INSTALL PROTECTION COVERS OVER ALL OPENINGS AS SOON AS POSSIBLE _______ TO PREVENT ENGINE DAMAGE. NOTE : Do not use this draining and filling task for normal oil ____ servicing. To make a check of the starter oil level (Ref. TASK 1213-80-612-802).
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Starter Oil Draining and Filling Figure 303/TASK 12-13-80-991-008- 12 (SHEET 1) R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-80 Page 328 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
Starter Oil Draining and Filling Figure 303/TASK 12-13-80-991-008- 22 (SHEET 2) R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-80 Page 329 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
(1) Remove the chip detector (Bayonnet Type - Lisle) from the starter as follows: (a) Put the fluid drain container 5 USgal (19 l) under the starter. CAUTION : DO NOT PUT CONTAMINATED OIL DRAINED FROM THE STARTER _______ BACK INTO THE OIL CART. IF YOU DO NOT DO THIS, YOU CAN TRANSFER THE OIL CONTAMINATION INTO THE OIL CART. (b) Hold the magnetic probe (42) by the grip. (c) Push the probe (42) in and turn it counterclockwise. (d) Pull the probe (42) out. (2) Examine the magnetic chip detector probe (42) as follows: (a) If you find metallic chips larger than 0.100 in. (2.54 mm) you must remove the starter (Ref. TASK 80-11-11-000-801). (b) If you find metallic chips smaller than 0.100 in. (2.54 mm), remove the chips from the probe (42) and proceed with step (3). (c) If you find no chips, proceed with step (3). (3) Remove the valve (45) from the starter as follows: (a) Remove the lockwire from the magnetic chip detector valve (45). (b) Remove the valve (45) from the starter. (c) Discard the packing (43) from the probe (42). R
(d) Discard the packing (41) from the valve (45). (e) Let the oil drain from the starter. (f) Write down the quantity of the drained oil: If the quantity of the drained oil is less than 7 OZF (207.0 ml), replace the starter (Ref. TASK 80-11-11-000-801), (Ref. TASK 8011-11-400-801) (4) Install the starter magnetic chip detector (Bayonnet Type-Lisle) as follows: CAUTION : REMOVE THE PROTECTION COVERS FROM THE OPENINGS AS NECESSARY _______ TO PREVENT ENGINE DAMAGE.
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CAUTION : DO NOT REMOVE OR INSTALL THE CHIP DETECTOR AS AN ASSEMBLY. _______ YOU MUST REMOVE THE MAGNETIC PROBE FROM THE VALVE. IF YOU DO NOT DO THIS, YOU CAN DAMAGE THE ASSEMBLY. CAUTION : DO NOT USE TOOLS TO REMOVE OR INSTALL THE CHIP DETECTOR _______ PROBE. IF YOU DO, YOU CAN DAMAGE THE PROBE. (a) Apply oil, lubricating, turbine engine (Material No. P03-001) to the new packing (41). (b) Install the new packing (41) to the washer face of the valve (45). (c) Apply oil, lubricating, turbine engine (Material No. P03-001) to the new packing (44). R R
(d) Install the valve (45) to the starter.
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(e) Torque the valve as follows: CAUTION : DO NOT TORQUE THE VALVE TOO MUCH. _______ IF YOU DO, YOU WILL BREAK OFF THE END OF THE VALVE. 1 _
TORQUE the valve (45) to between 10 and 25 lbf.in (0.11 and 0.28 m.daN).
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(f) Safety the valve (45) with lockwire 0.020 in. (0.50 mm) dia. (Material No. P05-287).
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(g) Apply oil, lubricating, turbine engine (Material No. P03-001) to the new packing (43).
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(h) Install the new packing (43) to the magnetic probe (42).
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(i) Install the magnetic probe (42) into the valve (45).
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(j) Push the magnetic probe (42) in and turn it clockwise until it locks.
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(k) Pull the magnetic probe (42) to make sure it is locked. NOTE : The magnetic probe is correctly installed when you align ____ the red marks on the probe with the red marks on the valve.
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Subtask 12-13-80-612-064 B. Fill the Starter (without Pressure Fill Equipment) CAUTION : WHEN YOU REPLACE THE STARTER DUE TO FAILURE OR OIL _______ CONTAMINATION, YOU MUST REPLACE ALL OIL SERVICING HARDWARE INCLUDING THE OIL SERVICE LINES, PLUGS, AND FITTINGS. IF YOU DO NOT DO THIS, YOU CAN TRANSFER THE OIL CONTAMINATION INTO THE NEW STARTER. CAUTION : INSTALL PROTECTION COVERS OVER ALL OPENINGS AS SOON AS POSSIBLE _______ TO PREVENT ENGINE DAMAGE. (1) Remove the lockwire and fill plug (47). (2) Discard the packing (46) from the fill plug (47). (3) Fill the starter to an acceptable level as follows: (a) Fill a standard squeeze bottle with clean oil, lubricating, turbine engine (Material No. P03-001). (b) Attach a piece of flex hose approximately 6 in. (152.4 mm) long to the squeeze bottle. (c) Put the flex hose into the fill port of the starter and squeeze the oil into the starter until oil drips from the fill port. NOTE : The oil level in the sightglass will now show at ____ approximately seven eighths. The starter is full when the oil level shows approximately seven eighths full on the sightglass. (4) Install the fill plug (47) as follows: CAUTION : REMOVE THE PROTECTION COVERS FROM THE OPENINGS AS NECESSARY _______ TO PREVENT ENGINE DAMAGE. (a) Apply oil, lubricating, turbine engine (Material No. P03-001) to the new packing (46) and the threads of the plug (47). (b) Install the new packing (46) to the plug (47). (c) Install the plug (47) to the fill port. (d) TORQUE the plug (47) to between 20 and 30 lbf.in (0.22 and 0.33 m.daN).
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(e) Safety the plug with lockwire 0.020 in. (0.50 mm) dia. (Material No. P05-287). Subtask 12-13-80-612-065 C. Fill the Starter (with Pressure Fill Equipment) CAUTION : WHEN YOU REPLACE THE STARTER DUE TO FAILURE OR OIL _______ CONTAMINATION, YOU MUST REPLACE ALL OIL SERVICING HARDWARE INCLUDING THE OIL SERVICE LINES, PLUGS, AND FITTINGS. IF YOU DO NOT DO THIS, YOU CAN TRANSFER THE OIL CONTAMINATION INTO THE NEW STARTER. (1) Remove the coupling covers from the overflow drain quick disconnect coupling and the pressure fill quick disconnect coupling on the air starter duct bracket. (2) Put the end of the drain hose in the fluid drain container 5 USgal (19 l). (3) Connect the drain hose to the overflow drain quick disconnect (larger) coupling on the air starter duct bracket. NOTE : Some oil can come out of the drain hose when you connect the ____ drain hose. (4) Connect the pressure fill hose from the pressure fill service unit to the pressure fill quick disconnect (smaller) coupling on the air starter duct bracket. (5) Fill the starter as follows: CAUTION : MAKE SURE THAT YOU ATTACH THE DRAIN HOSE TO THE OVERFLOW _______ DRAIN QUICK DISCONNECT COUPLING BEFORE YOU TRY AND FILL THE STARTER. IF YOU DO NOT CONNECT THE DRAIN HOSE FIRST, YOU CAN PUT TOO MUCH PRESSURE INSIDE THE STARTER AND DAMAGE CAN OCCUR. (a) Use the pressure fill service unit and add the correct oil, lubricating, turbine engine (Material No. P03-001) until the oil comes out of the drain hose. (6) Remove the pressure hose from the coupling on the air starter duct bracket. (7) Install the coupling cover to the pressure fill quick disconnect coupling.
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(8) When the oil from the drain hose decreases to a drip, disconnect the drain hose from the overflow drain quick disconnect coupling on the air starter duct bracket. (9) Install the coupling cover to the overflow drain quick disconnect coupling. NOTE : The oil level in the sightglass will now show at approximately ____ seven eighths. The starter is full when the oil level shows approximately seven eighths full on the sightglass. 5. Close-up ________ Subtask 12-13-80-410-073 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Remove the fluid drain container. (3) Close the lower left thrust reverser access door: - FOR 4030EM1 417EL - FOR 4030EM2 427EL (4) Close the right thrust reverser cowl door (Ref. TASK 78-30-00-410801): - FOR 4030EM1 418AR - FOR 4030EM2 428AR Subtask 12-13-80-440-057 B. Make the thrust reverser serviceable (Ref. TASK 78-30-00-440-804). Subtask 12-13-80-865-069 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2
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Subtask 12-13-80-410-074 D. Close Access (1) Close the left and right aft fan cowl doors (Ref. TASK 71-13-00-410802): - FOR 4030EM1 415BL, 416BR - FOR 4030EM2 425BL, 426BR (2) Close the protective door of the AC/DC emergency power-center 740VU. (3) Close the access door 811. (4) Remove the access platform(s). Subtask 12-13-80-862-059 E. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-80 Page 335 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
TASK 12-13-80-612-803 Check and Replenish Starter Oil by Remote Fill - Through Access Door WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE AFTER THE ENGINE IS SHUTDOWN. _______ THE ENGINE CAN STAY HOT FOR A LONG TIME AFTER THE ENGINE IS SHUTDOWN. WARNING : USE PROTECTIVE CLOTHING WHEN YOU USE ENGINE OIL. OIL CAN CAUSE SKIN _______ IRRITATION. CAUTION : DO NOT OPERATE THE STARTER WITHOUT SUFFICIENT OIL. THIS WILL CAUSE _______ DAMAGE TO THE STARTER. CAUTION : DO NOT OPERATE THE STARTER WITH TOO MUCH OIL. THIS WILL CAUSE DAMAGE _______ TO THE STARTER. CAUTION : DO NOT LET ENGINE FUEL OR OIL FALL ON THE ENGINE. YOU MUST _______ IMMEDIATELY REMOVE UNWANTED FUEL OR OIL WITH A CLOTH. THE FUEL OR OIL CAN CAUSE DAMAGE TO SOME ENGINE PARTS. 1. __________________ Reason for the Job R NOTE : Do not use this servicing task for draining and filling the starter. ____ To drain and fill the starter oil (Ref. TASK 12-13-80-610-803). 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No
specific specific specific specific specific specific
circuit breaker(s) safety clip(s) drain hose fluid drain container 5 USgal (19 l) pressure fill service unit adjustable access platform 1.22 m (4 ft.) access platform 2.5 m (8 ft. 2 in.)
EFF : 001-049, 201-249, 251-252, 255-299, 12-13-80 Page 336 301-399, 401-449, 451-499, Config-1 Jan 01/06 SROS
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
P03-001
* oil, lubricating, turbine engine (Ref. 70-30-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 71-13-00-010-802 71-13-00-410-802 78-30-00-040-804 78-30-00-440-804 12-13-80-991-006
Energize the Ground Service Network De-energize the Ground Service Network Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Deactivation of the Thrust Reverser for Maintenance Reactivation of the Thrust Reverser after Maintenance Fig. 304
3. __________ Job Set-up Subtask 12-13-80-861-058 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-80-941-059 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure. Subtask 12-13-80-010-073 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-80 Page 337 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
(3) Open the protective door of the AC/DC emergency power-center 740VU. Subtask 12-13-80-865-066 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-13-80-010-075 E. Get Access (1) Open the right aft fan cowl door (Ref. TASK 71-13-00-010-802): - FOR 4030EM1 416BR - FOR 4030EM2 426BR Subtask 12-13-80-040-056 F. Deactivation of the Thrust Reverser. WARNING : YOU MUST DEACTIVATE THE THRUST REVERSER DIRECTIONAL CONTROL _______ VALVE (DCV) BEFORE YOU WORK ON OR AROUND THE TRANSLATING COWL. IF YOU DO NOT DEACTIVATE THE DCV, YOU CAN CAUSE ACCIDENTAL THRUST REVERSER OPERATION AND INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT. (1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 7830-00-040-804).
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Subtask 12-13-80-010-074 G. Get Access (1) Put the adjustable access platform in position. (2) Open the thrust reverser lower left access door. - FOR 4030EM1 417EL - FOR 4030EM2 427EL 4. Procedure _________ (Ref. Fig. 304/TASK 12-13-80-991-006) Subtask 12-13-80-612-058 A. Do a Check and Service the Starter (with Pressure Fill Equipment) (1) Find the starter oil fill couplings attached to the bottom of the starter air duct towards the right side of the engine. NOTE : Make sure you do not use the Integrated Drive Generator (IDG) ____ oil fill connectors on the rear of the IDG. (2) Remove the coupling covers from the overflow drain quick disconnect coupling and the pressure fill quick disconnect coupling on the air starter duct bracket. (3) Put the end of the drain hose in the fluid drain container 5 USgal (19 l). (4) Connect the drain hose fitting to the overflow drain quick disconnect (larger) coupling on the air starter duct bracket. NOTE : Some oil can come out of the drain hose when you connect the ____ drain hose. (5) Connect the pressure fill hose from the pressure fill service unit to the pressure fill quick disconnect (smaller) coupling on the air starter duct bracket.
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Starter Oil Level Servicing - Pressure Fill Through Access Door Figure 304/TASK 12-13-80-991-006 R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-80 Page 340 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
(6) Add oil as follows: CAUTION : MAKE SURE THAT YOU ATTACH THE DRAIN HOSE TO THE OVERFLOW _______ DRAIN QUICK DISCONNECT COUPLING BEFORE YOU TRY AND FILL THE STARTER. IF YOU DO NOT CONNECT THE DRAIN HOSE FIRST, YOU CAN PUT TOO MUCH PRESSURE INSIDE THE STARTER AND DAMAGE CAN OCCUR. (a) Use the pressure fill service unit and add the correct oil, lubricating, turbine engine (Material No. P03-001) until the oil comes out of the drain hose. (7) Remove the pressure hose from the coupling on the air starter bracket. (8) Install the coupling cover to the pressure fill quick disconnect coupling. (9) When the oil from the drain hose decreases to a drip, disconnect the drain hose from the overflow drain quick disconnect coupling on the air starter duct bracket. (10) Install the coupling cover to the overflow drain quick disconnect coupling. 5. Close-up ________ Subtask 12-13-80-410-072 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the lower left thrust reverser access door. - FOR 4030EM1 417EL - FOR 4030EM2 427EL Subtask 12-13-80-440-056 B. Make the thrust reverser serviceable (Ref. TASK 78-30-00-440-804).
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Subtask 12-13-80-865-067 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2 Subtask 12-13-80-410-071 D. Close Access (1) Close the right aft fan cowl door (Ref. TASK 71-13-00-410-802): - FOR 4030EM1 416BR - FOR 4030EM2 426BR (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Close the access door 811. (4) Remove the access platform(s). Subtask 12-13-80-862-056 E. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-80 Page 342 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
ENGINE STARTING - SERVICING ___________________________ TASK 12-13-80-610-804 To Service the Pneumatic Starter Oil System WARNING : YOU MUST BE CAREFUL WHEN YOU DO WORK ON THE ENGINE PARTS AFTER THE _______ ENGINE IS SHUTDOWN. THE ENGINE PARTS CAN STAY HOT FOR ALMOST 1 HOUR. 1. __________________ Reason for the Job This procedure is applicable to engines with an Allied Signal or Hamilton Standard pneumatic starter. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R
No No No No
specific specific specific specific
circuit breaker(s) safety clip(s) adjustable access platform 1.22 m (4 ft.) access platform 2.5 m (8 ft. 2 in.) Torque Wrench : range 5.00 to 35.00 lbf.in (0.05 to 0.40 m.daN) Torque Wrench : range 36.00 to 220.00 lbf.in (0.40 to 2.60 m.daN)
No specific B. Consumable Materials
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
OMat 1011
Material No.
OMat 238
* engine oil (Ref. 70-30-00) * lockwire 0.028 to 0.031 in. (0.71 to 0.79 mm) dia (Ref. 70-30-00)
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C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------2 3
seal ring seal ring
80-11-41 60 -070 80-11-41 60 -070
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 70-02-01-910-801 70-12-04-910-804 70-51-00-910-802 71-13-00-010-805 71-13-00-410-805 80-11-41-000-803 80-11-41-400-803 12-13-80-991-005
Energize the Ground Service Network De-energize the Ground Service Network Identification, Lubrication and Fitting of Flexible Seal Rings Locking Techniques - Wire locking Torque Tightening Techniques Open the Fan Cowl Doors Close the Fan Cowl Doors Removal of the Pneumatic Starter (5000ES) Installation of the Pneumatic Starter (5000ES) Fig. 301
3. __________ Job Set-up Subtask 12-13-80-861-056 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-80-941-057 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure.
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Subtask 12-13-80-010-068 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU. Subtask 12-13-80-865-062 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-13-80-010-069 E. Get Access (1) Open the fan cowl doors: (Ref. TASK 71-13-00-010-805) - FOR 4030EM1 415AL, 416AR - FOR 4030EM2 425AL, 426AR (2) Put the adjustable access platform in position. Subtask 12-13-80-020-050 F. Get Access to the Pneumatic Starter (1) Remove the oil fill plug (1) and the oil level overflow plug (4) from the pneumatic starter. (Ref. Fig. 301/TASK 12-13-80-991-005) (2) Remove the lockwire from the oil fill plug (1) and the oil level overflow plug (4).
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Pneumatic Starter (Allied Signal) - Oil Fill Location Figure 301/TASK 12-13-80-991-005 EFF : 701-749, 12-13-80 Page 304 Config-2 Oct 01/00 SROS
(3) Remove the oil fill plug (1) and the oil level overflow plug (4). (4) Discard the seal rings (2) and (3). 4. Procedure _________ (Ref. Fig. 301/TASK 12-13-80-991-005) Subtask 12-13-80-612-056 A. Fill the Allied Signal Pneumatic Starter with clean engine oil: (Ref. Fig. 301/TASK 12-13-80-991-005) WARNING : YOU MUST NOT LET ENGINE OIL STAY ON YOUR SKIN. FLUSH THE OIL _______ FROM YOUR SKIN WITH WATER. THE OIL IS POISONOUS AND CAN BE ABSORBED INTO THE BODY. CAUTION : YOU MUST NOT LET ENGINE FUEL OR OIL FALL ON THE ENGINE. _______ UNWANTED FUEL OR OIL MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT-FREE CLOTH. THE FUEL OR OIL CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. CAUTION : YOU MUST USE THE SAME TYPE OF APPROVED OIL EACH TIME YOU FILL _______ THE PNEUNATIC STARTER WITH OIL. YOU MUST ONLY MIX APPROVED OILS IF IT BECOMES OPERATIONALLY NECESSARY. (1) Add clean engine oil (Material No. OMat 1011) to the pneumatic starter. (a) Continue to put oil in the pneumatic starter until oil starts to drip from the oil level overflow. (b) Wait until oil does not drip form the oil level overflow. (c) Use a clean cloth to remove oil from the external surface of the starter. (2) Install a new seal ring (3) on the oil level overflow plug (4) (Ref. TASK 70-02-01-910-801). (a) Lubricate the seal ring (3) with clean engine oil (Material No. OMat 1011). (3) Install the oil level overflow plug (4) to the pneumatic starter. (a) TORQUE the oil level overflow plug (4) to between 120 and 130 lbf.in (1.35 and 1.46 m.daN) (Ref. TASK 70-51-00-910-802)
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(4) Safety the oil level overflow plug (4) with lockwire 0.028 to 0.031 in. (0.71 to 0.79 mm) dia (Material No. OMat 238) (Ref. TASK 70-1204-910-804). (5) Install a new seal ring (2) to the oil fill plug (1) (Ref. TASK 7002-01-910-801). (a) Lubricate the seal ring (2) with clean engine oil (Material No. OMat 1011). (6) Install the oil fill plug (1) to the pneumatic starter. Subtask 12-13-80-612-059 B. Torque the oil fill plug. (1) TORQUE the oil fill plug (1) to between 20 and 35 lbf.in (0.22 and 0.39 m.daN) (Ref. TASK 70-51-00-910-802) Subtask 12-13-80-612-060 C. Safety the oil fill plug. (1) Safety the oil fill plug (1) with lockwire 0.028 to 0.031 in. (0.71 to 0.79 mm) dia (Material No. OMat 238). (Ref. TASK 70-12-04-910-804) (2) Look at the oil level sight glass; the oil level must be above the ADD mark. (3) If the oil level is not above the ADD mark on the oil level sight glass, replace the pneumatic starter (Ref. TASK 80-11-41-000-803) and (Ref. TASK 80-11-41-400-803). 5. Close-up ________ Subtask 12-13-80-865-063 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2
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Subtask 12-13-80-410-067 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Close the access door 811. (4) Close the fan cowl doors: (Ref. TASK 71-13-00-410-805) - FOR 4030EM1 415AL, 416AR - FOR 4030EM2 425AL, 426AR (5) Remove the access platform(s). Subtask 12-13-80-862-053 C. De-energize the ground service network (Ref. TASK 24-42-00-862-801)
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TASK 12-13-80-610-805 To Change the Oil in the Pneumatic Starter WARNING : YOU MUST BE CAREFUL WHEN YOU DO WORK ON THE ENGINE PARTS AFTER THE _______ ENGINE IS SHUTDOWN. THE ENGINE PARTS CAN STAY HOT FOR ALMOST 1 HOUR. 1. __________________ Reason for the Job This procedure is applicable to engines with Allied Signal Pneumatic Starter 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No
specific specific specific specific specific specific
circuit breaker(s) safety clip(s) lint-free cloth adjustable access platform 1.22 m (4 ft.) access platform 2.5 m (8 ft. 2 in.) container 5 l (1.3208 USgal) Torque Wrench : range 36.00 to 220.00 lbf.in (0.40 to 2.60 m.daN)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
OMat 1011
Material No.
OMat 238
* engine lubricating oil (synthetic) (Ref. 70-30-00) * lockwire 0.028 to 0.031 in. (0.71 to 0.79 mm) dia. (Ref. 70-30-00)
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C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------R R R
2 3 6
seal ring seal ring seal ring
80-11-41 60 -070 80-11-41 60 -070 80-11-41 60 -100
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 70-02-01-910-801 70-12-04-910-804 70-51-00-910-802 71-13-00-010-805 71-13-00-410-805 80-11-41-000-803 80-11-41-400-803 12-13-80-991-005
Energize the Ground Service Network De-energize the Ground Service Network Identification, Lubrication and Fitting of Flexible Seal Rings Locking Techniques - Wire locking Torque Tightening Techniques Open the Fan Cowl Doors Close the Fan Cowl Doors Removal of the Pneumatic Starter (5000ES) Installation of the Pneumatic Starter (5000ES) Fig. 301
3. __________ Job Set-up Subtask 12-13-80-861-060 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-80-941-061 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure.
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Subtask 12-13-80-010-079 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power center 740VU. Subtask 12-13-80-865-070 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-13-80-010-080 E. Get Access to the Pneumatic Starter (1) Open the fan cowl doors (Ref. TASK 71-13-00-010-805): - FOR 4030EM1 415AL, 416AR - FOR 4030EM2 425AL, 426AR (2) Put the adjustable access platform in position. 4. Procedure _________ (Ref. Fig. 301/TASK 12-13-80-991-005) Subtask 12-13-80-610-061 A. Change the Oil in the Allied Signal Pneumatic Starter WARNING : YOU MUST NOT LET ENGINE OIL STAY ON YOUR SKIN. FLUSH THE OIL _______ FROM YOUR SKIN WITH WATER. THE OIL IS POISONOUS AND CAN BE ABSORBED INTO THE BODY.
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CAUTION : YOU MUST NOT LET ENGINE FUEL OR OIL FALL ON THE ENGINE. _______ UNWANTED FUEL OR OIL MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT-FREE CLOTH. THE FUEL OR OIL CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. (1) Put a container in position to catch the oil that will come out of the starter. (2) Remove the lockwire that safeties the oil drain plug (5). (3) Remove the oil drain plug (5) and let unwanted oil drain into the container. (4) Remove and discard the seal ring (6). R
(5) Install a new seal ring (6) on the oil drain plug (5) (Ref. TASK 7002-01-910-801). (6) Install the oil drain plug (5) on the starter. TORQUE the plug to between 110 and 120 lbf.in (1.24 and 1.35 m.daN). (7) Safety the oil drain plug (5) with lockwire 0.028 to 0.031 in. (0.71 to 0.79 mm) dia. (Material No. OMat 238) (Ref. TASK 70-12-04-910804). (8) Remove the lockwire from the oil fill plug (1) and the oil level overflow plug (4). (9) Remove the oil fill plug (1) and the oil level overflow plug (4) from the starter. (10) Remove and discard the seal rings (2) and (3). (11) Put engine lubricating oil (synthetic) (Material No. OMat 1011) into the oil fill port of the starter: (a) Continue to put oil into the starter until the oil comes out from the overflow port. (b) Wait until the overflow stops. (c) Remove unwanted oil from the outside of the starter with a clean lint-free cloth.
R
(12) Install a new seal ring (3) on the oil level overflow plug (4) (Ref. TASK 70-02-01-910-801).
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(13) Install the oil level overflow plug (4) on the starter. TORQUE the plug to between 120 and 130 lbf.in (1.35 and 1.46 m.daN) (Ref. TASK 70-51-00-910-802). (14) Safety the oil level overflow plug (4) with lockwire 0.028 to 0.031 in. (0.71 to 0.79 mm) dia. (Material No. OMat 238) (Ref. TASK 70-1204-910-804). R
(15) Install a new seal ring (2) on the oil fill plug (1) (Ref. TASK 7002-01-910-801). (16) Install the oil fill plug (1) on the starter. TORQUE the plug to between 120 and 130 lbf.in (1.35 and 1.46 m.daN) (Ref. TASK 70-51-00910-802). (17) Safety the oil fill plug (1) with lockwire 0.028 to 0.031 in. (0.71 to 0.79 mm) dia. (Material No. OMat 238) (Ref. TASK 70-12-04-910804). Subtask 12-13-80-210-055 B. Do a Check of the Sight Glass (1) Look at the oil level sight glass on the starter. The oil level must be above the ADD mark on the right side of the sight glass. (2) If the oil level is not above the ADD mark, replace the pneumatic starter (Ref. TASK 80-11-41-000-803) and (Ref. TASK 80-11-41-400803). 5. Close-up ________ Subtask 12-13-80-865-071 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2
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Subtask 12-13-80-410-075 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Close the access door 811. (4) Close the fan cowl doors (Ref. TASK 71-13-00-410-805): - FOR 4030EM1 415AL, 416AR - FOR 4030EM2 425AL, 426AR (5) Remove the container. (6) Remove the access platform(s). Subtask 12-13-80-862-060 C. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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GAS - DESCRIPTION AND OPERATION _______________________________ 1. _______ General This section gives the instructions to charge the hydraulic power and components related to the landing gear. It includes the topics below: 12-14-29, P. Block 301 HYDRAULIC POWER 12-14-32, P. Block 301 LANDING GEAR
EFF : ALL 12-14-00 SROS
Page 1 Apr 01/98
HYDRAULIC POWER - SERVICING ___________________________ TASK 12-14-29-614-801 Fill the Green Power Accumulator (5151JM1) with Nitrogen 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific R
98F29103500000
access platform 2.5 m (8 ft. 2 in.) Torque Wrench : range 2.00 to 20.00 m.daN (15.00 to 150.00 lbf.ft) 1
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-801 29-10-00-200-801 12-14-29-991-001
Depressurize the Green Hydraulic System (Pressurized with the Hydraulic Ground Supply) Leak Check of Pressure on Hydraulic Power Accumulators (5151JM1,5151JM2,5151JM3) Fig. 301
3. __________ Job Set-up Subtask 12-14-29-864-050 A. Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801).
EFF : ALL 12-14-29 SROS
Page 301 Jan 01/07
Subtask 12-14-29-010-050 B. Get Access (1) Put the access platform in position at the access door 197CB. (2) Open the Green ground service panel access door 197CB. 4. Procedure _________ (Ref. Fig. 301/TASK 12-14-29-991-001) Subtask 12-14-29-220-050 A. If the decrease in nitrogen pressure is more than 30 bar (435.1131 psi) (with respect to nominal pressure of accumulators) you must make sure that there are no leaks (Ref. TASK 29-10-00-200-801). Subtask 12-14-29-614-050 B. Fill the applicable accumulator with nitrogen. (1) Remove the blanking cap (2) from the charging valve (1). R
(2) Connect to the charging valve (1) the (98F29103500000) or a nitrogen bench capable of maxi pressure 150 bar (2175.5655 psi). (3) Loosen the charging valve nut (3). (4) Open the charging valve nut (3) slowly (turn to the OPEN direction) and fill the hydraulic power accumulator to the correct pressure for the ambient temperature.
R R R
NOTE : If you do this check immediately after aircraft landing, let ____ the pressure become stable for one hour to get a more accurate measurement (temperature compensation of the accumulator). NITROGEN PRESSURE
EFF : ALL 12-14-29 SROS
Page 302 Jan 01/07
Filling of the Green Power Accumulator Figure 301/TASK 12-14-29-991-001 EFF : ALL 12-14-29 SROS
Page 303 Apr 01/98
------------------------------------------------------------------------------| Temperature | Charging Pressure | |---------------------------|-------------------------------------------------| | deg.C | deg.F | bar | PSI | |-----------------------------------------------------------------------------| | -30 | -22 | 108 | 1566 | | -20 | - 4 | 112 | 1624 | | -10 | 14 | 116.5 | 1689 | | 0 | 32 | 121 | 1754 | | 10 | 50 | 125.5 | 1820 | | 20 | 68 | 130 | 1885 | | 30 | 86 | 134.5 | 1950 | | 40 | 104 | 139 | 2015 | | 50 | 112 | 143.5 | 2081 | | 60 | 140 | 148 | 2146 | ------------------------------------------------------------------------------(5) When the pressure is stable and correct, tighten the charging valve nut (3) (CLOSE position). (6) Make sure that the pressure shown on the pressure gage is correct. (7) Stop the supply and remove the nitrogen filling system from the charging valve (1). R R
(8) TORQUE the charging valve nut (3) to between 10.7 and 11.8 m.daN (78.90 and 87.02 lbf.ft).
R
(9) Install the blanking cap (2) on the charging valve. 5. Close-up ________ Subtask 12-14-29-410-050 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the Green ground service panel 197CB. (3) Remove the access platform(s).
EFF : ALL 12-14-29 SROS
Page 304 Jul 01/06
TASK 12-14-29-614-802 Fill the Blue Power Accumulator (5151JM2) with Nitrogen 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific R
98F29103500000
access platform 2.5 m (8 ft. 2 in.) Torque Wrench : range 2.00 to 20.00 m.daN (15.00 to 150.00 lbf.ft) 1
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-802 29-10-00-200-801 12-14-29-991-002
Depressurize the Blue Hydraulic System (Pressurized with the Hydraulic Ground Supply) Leak Check of Pressure on Hydraulic Power Accumulators (5151JM1,5151JM2,5151JM3) Fig. 302
3. __________ Job Set-up Subtask 12-14-29-864-051 A. Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802). Subtask 12-14-29-010-051 B. Get Access (1) Put the access platform in position at the access door 195BB. (2) Open the Blue ground service panel access door 195BB.
EFF : ALL 12-14-29 SROS
Page 305 Jan 01/07
4. Procedure _________ (Ref. Fig. 302/TASK 12-14-29-991-002) Subtask 12-14-29-220-051 A. If the decrease in nitrogen pressure is more than 30 bar (435.1131 psi) (with respect to nominal pressure of accumulators) you must make sure that there are no leaks (Ref. TASK 29-10-00-200-801). Subtask 12-14-29-614-051 B. Fill the applicable accumulator with nitrogen. (1) Remove the blanking cap (2) from the charging valve (1). R
(2) Connect to the charging valve (1) the (98F29103500000) or a nitrogen bench capable of maxi pressure 150 bar (2175.5655 psi). (3) Loosen the charging valve nut (3). (4) Open the charging valve nut (3) slowly (turn to the OPEN direction) and fill the hydraulic power accumulator to the correct pressure for the ambient temperature.
R R R
NOTE : If you do this check immediately after aircraft landing, let ____ the pressure become stable for one hour to get a more accurate measurement (temperature compensation of the accumulator). NITROGEN PRESSURE ------------------------------------------------------------------------------| Temperature | Charging Pressure | |---------------------------|-------------------------------------------------| | deg.C | deg.F | bar | PSI | |-----------------------------------------------------------------------------| | -30 | -22 | 108 | 1566 | | -20 | - 4 | 112 | 1624 | | -10 | 14 | 116.5 | 1689 | | 0 | 32 | 121 | 1754 | | 10 | 50 | 125.5 | 1820 | | 20 | 68 | 130 | 1885 | | 30 | 86 | 134.5 | 1950 | | 40 | 104 | 139 | 2015 | | 50 | 112 | 143.5 | 2081 | | 60 | 140 | 148 | 2146 | ------------------------------------------------------------------------------(5) When the pressure is stable and correct, tighten the charging valve nut (3) (CLOSE position).
EFF : ALL 12-14-29 SROS
Page 306 Jan 01/07
Filling of the Blue Power Accumulator Figure 302/TASK 12-14-29-991-002 EFF : ALL 12-14-29 SROS
Page 307 Apr 01/98
(6) Make sure that the pressure shown on the pressure gage is correct. (7) Stop the supply and remove the nitrogen filling system from the charging valve (1). R R
(8) TORQUE the charging valve nut (3) to between 10.7 and 11.8 m.daN (78.90 and 87.02 lbf.ft).
R
(9) Install the blanking cap (2) on the charging valve. 5. Close-up ________ Subtask 12-14-29-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the Blue ground service panel 195BB. (3) Remove the access platform(s).
EFF : ALL 12-14-29 SROS
Page 308 Jul 01/06
TASK 12-14-29-614-803 Fill the Yellow Power Accumulator (5151JM3) with Nitrogen 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific R
98F29103500000
access platform 2.5 m (8 ft. 2 in.) Torque Wrench : range 2.00 to 20.00 m.daN (15.00 to 150.00 lbf.ft) 1
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-803 29-10-00-200-801 12-14-29-991-003
Depressurize the Yellow Hydraulic System (Pressurized with the Hydraulic Ground Supply) Leak Check of Pressure on Hydraulic Power Accumulators (5151JM1,5151JM2,5151JM3) Fig. 303
3. __________ Job Set-up Subtask 12-14-29-864-052 A. Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803). Subtask 12-14-29-010-052 B. Get Access (1) Put the access platform in position at the access door 196BB. (2) Open the Yellow ground service panel access door 196BB.
EFF : ALL 12-14-29 SROS
Page 309 Jan 01/07
4. Procedure _________ (Ref. Fig. 303/TASK 12-14-29-991-003) Subtask 12-14-29-220-052 A. If the decrease in nitrogen pressure is more than 30 bar (435.1131 psi) (with respect to nominal pressure of accumulators) you must make sure that there are no leaks (Ref. TASK 29-10-00-200-801). Subtask 12-14-29-614-052 B. Fill the applicable accumulator with nitrogen. (1) Remove the blanking cap (2) from the charging valve (1). R
(2) Connect to the charging valve (1) the (98F29103500000) or a nitrogen bench capable of maxi pressure 150 bar (2175.5655 psi). (3) Loosen the charging valve nut (3). (4) Open the charging valve nut (3) slowly (turn to the OPEN direction) and fill the hydraulic power accumulator to the correct pressure for the ambient temperature.
R R R
NOTE : If you do this check immediately after aircraft landing, let ____ the pressure become stable for one hour to get a more accurate measurement (temperature compensation of the accumulator). NITROGEN PRESSURE ------------------------------------------------------------------------------| Temperature | Charging Pressure | |---------------------------|-------------------------------------------------| | deg.C | deg.F | bar | PSI | |-----------------------------------------------------------------------------| | -30 | -22 | 108 | 1566 | | -20 | - 4 | 112 | 1624 | | -10 | 14 | 116.5 | 1689 | | 0 | 32 | 121 | 1754 | | 10 | 50 | 125.5 | 1820 | | 20 | 68 | 130 | 1885 | | 30 | 86 | 134.5 | 1950 | | 40 | 104 | 139 | 2015 | | 50 | 112 | 143.5 | 2081 | | 60 | 140 | 148 | 2146 | ------------------------------------------------------------------------------(5) When the pressure is stable and correct, tighten the charging valve nut (3) (CLOSE position).
EFF : ALL 12-14-29 SROS
Page 310 Jan 01/07
Filling of the Yellow Power Accumulator Figure 303/TASK 12-14-29-991-003 EFF : ALL 12-14-29 SROS
Page 311 Apr 01/98
(6) Make sure that the pressure shown on the pressure gage is correct. (7) Stop the supply and remove the nitrogen filling system from the charging valve (1). R R
(8) TORQUE the charging valve nut (3) to between 10.7 and 11.8 m.daN (78.90 and 87.02 lbf.ft).
R
(9) Install the blanking cap (2) on the charging valve. 5. Close-up ________ Subtask 12-14-29-410-052 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the Yellow ground service panel 196BB. (3) Remove the access platform(s).
EFF : ALL 12-14-29 SROS
Page 312 Jul 01/06
LANDING GEAR - SERVICING ________________________ TASK 12-14-32-614-801 Replenishment of the Tires WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED ON THE _______ LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. WARNING : LET THE BRAKES AND THE WHEELS BECOME COOL BEFORE YOU GO NEAR THE _______ LANDING GEAR. DO NOT APPLY A LIQUID OR GAS FIRE EXTINGUISHER DIRECTLY ON A HOT WHEEL OR BRAKE UNIT. THIS COULD CAUSE AN EXPLOSION. WARNING : USE ONLY DRY NITROGEN OR OTHER GASES TO INFLATE THE TIRES ON THE MAIN _______ GEAR WHEELS. THE OXYGEN IN THE GAS USED TO INFLATE THESE TIRES MUST NOT BE MORE THAN 5% (VOLUME). IF THE AIRCRAFT IS FAR FROM ITS BASE AND NO DRY NITROGEN IS AVAILABLE, YOU CAN USE AIR FOR THE SERVICING OF THE TIRES IF: - THE OXYGEN IN THE TIRES IS NOT MORE THAN 5% (VOLUME) OR - MAINTENANCE PERSONNEL REMOVE THE AIR FROM THE TIRES AND INFLATE THEM WITH DRY NITROGEN BEFORE 15 HOURS TIME SERVICE. A CHEMICAL REACTION BETWEEN THE OXYGEN IN THE TIRES AND GASES FROM THE INNER LINER CAN CAUSE A TIRE EXPLOSION. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R R R
No specific No specific No specific
1 ADAPTER - TIRE INFLATION/DEFLATION 1 CART - INFLATION, TIRE, NITROGEN 1 GAGE - PRESSURE, TIRE
EFF : ALL 12-14-32 SROS
Page 301 Jan 01/07
3. __________ Job Set-up Subtask 12-14-32-941-055 A. Preparation for Replenishment R
(1) Put the CART - INFLATION, TIRE, NITROGEN near the tire to be inflated. (2) Remove the tire-inflation valve cap.
R R
(3) Use a GAGE - PRESSURE, TIRE and a ADAPTER - TIRE INFLATION/DEFLATION to connect the inflation cart to the tire inflation valve. 4. Procedure _________ WARNING : DO NOT PUT COMPRESSED GAS IN CONTACT WITH YOUR SKIN. THE GAS CAN _______ GO THROUGH THE SKIN AND MAKE BUBBLES IN THE BLOOD. THIS CONDITION CAN KILL YOU. NOTE : AIRBUS recommends that when you inflate the tires, you use the ____ maximum normal pressure (given in the table). This is necessary to keep tire inflation to a minimum. NOTE : In the tables that follow the term loaded means with the aircraft ____ weight on the wheels. The term unloaded is when the applicable wheel is off the ground (jacked). Subtask 12-14-32-614-058-A A. Replenishment of the NLG Tires (1) Refer to the table to find the correct tire pressure. Inflate the tire with nitrogen. (2) If there is a large temperature decrease between the departure and the destination airports, the tire pressures given must be adjusted. If the temperature difference is more than 24 deg C lower, do this procedure: (a) Increase the given tire pressures 3.7% for each 10 deg C of temperature difference.
EFF : ALL 12-14-32 SROS
Page 302 Jan 01/07
EXAMPLE
Temperature at departure airport = 20 deg C Temperature at arrival airport = -10 deg C Temperature difference = 30 deg C Increase the tire pressure: 30/10 x 3.7% = 11.1% If the loaded tire pressure is 13.0 bar, increase the tire pressure: 13.0 bar +(13.0 bar x 11.1%) = 14.4 bar -------------------------------------------------------| TIRE DIMENSION | INFLATION PRESSURE | | AND TYPE |---------------------------------------| | | UNLOADED | LOADED | | | BAR (PSI) | BAR (PSI) | |----------------|-------------------|-------------------| | 1050 X 395R16 | 12.2 (177) normal | 12.7 (184) normal | | RADIAL | 12.8 (186) max | 13.3 (193) max | --------------------------------------------------------
Subtask 12-14-32-614-059 B. Replenishment of the MLG Tires (1) Refer to the table to find the correct tire pressure. Inflate the tire with nitrogen. (2) If there is a large temperature decrease between the departure and the destination airports, the tire pressures given must be adjusted. If the temperature difference is more than 24 deg C lower, do this procedure:
R R
(a) Increase the given tire pressures 3.7% for each 10 deg C of temperature difference. EXAMPLE
Temperature at departure airport = 20 deg C Temperature at arrival airport = -10 deg C Temperature difference = 30 deg C Increase the tire pressure: 30/10 x 3.7% = 11.1% If the loaded tire pressure is 13.0 bar, increase the tire pressure: 13.0 bar +(13.0 bar x 11.1%) = 14.4 bar
EFF : ALL 12-14-32 SROS
Page 303 Jan 01/03
-------------------------------------------------------| TIRE DIMENSION | INFLATION PRESSURE | | AND TYPE |---------------------------------------| | | UNLOADED | LOADED | | | BAR (PSI) | BAR (PSI) | |----------------|-------------------|-------------------| | 1400 X 530R23 | 13.6 (198) normal | 14.2 (206) normal | | RADIAL | | | | 54 X 21-23 | 14.3 (208) max | 14.9 (216) max | | BIAS | | | -------------------------------------------------------5. Close-up ________ Subtask 12-14-32-942-055 A. Removal of the Ground Support Equipment (1) Remove the inflation cart, pressure gage and adapter from the applicable tire. R R
(2) Remove the CART - INFLATION, TIRE, NITROGEN, GAGE - PRESSURE, TIRE and ADAPTER - TIRE INFLATION/DEFLATION from the applicable tire.
R
(3) Install the tire-inflation valve cap.
R
(4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL 12-14-32 SROS
Page 304 Jan 01/07
TASK 12-14-32-614-802 Gas Replenishment of the MLG Shock Absorber WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED ON THE _______ LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. 1. __________________ Reason for the Job NOTE : You can complete this procedure with the aircraft on the ground or on ____ jacks. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No
specific specific specific specific specific specific specific specific
460007156
nitrogen source pressure gage 0 - 200 bar pressure gage 0 - 60 bar standard charging equipment thermometer warning notice access platform 3 m (9 ft. 10 in.) Torque Wrench : range 0.00 to 1.20 m.daN (0.00 to 9.00 lbf.ft) 1 ADAPTER, CHARGING - MLG
R
EFF : ALL 12-14-32 SROS
Page 305 Jul 01/06
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 05-004B Material No. 19-010
USA MIL-L-25567 TYPE I OXYGEN LEAK DETECTOR (Ref. 20-31-00) USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-804 32-00-00-481-801
R R
32-12-00-010-801 32-12-00-410-801 12-14-32-991-001 12-14-32-991-031 12-14-32-991-002-A
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Installation of the Safety Devices on the Landing Gears Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Fig. 301 Fig. 302 Fig. 303
3. __________ Job Set-up Subtask 12-14-32-941-050 A. Safety Precautions (1) Put the warning notice in the cockpit to tell persons not to operate the landing gear controls. Subtask 12-14-32-860-050 B. Aircraft Maintenance Configuration (1) Make sure that the Green hydraulic system is depressurized (Ref. TASK 29-00-00-864-804). (2) Make sure that the safety devices are installed on the L/G (Ref. TASK 32-00-00-481-801).
EFF : ALL 12-14-32 SROS
Page 306 Apr 01/04
Subtask 12-14-32-010-054 C. Get Access (Ref. Fig. 301/TASK 12-14-32-991-001) (1) Open the applicable MLG door (Ref. TASK 32-12-00-010-801). (2) Put an access platform adjacent to the applicable MLG: - for the LH MLG at zone 731 - for the RH MLG at zone 741. (3) Remove and discard the lockwire from the bolts (5). (4) Remove the bolts (5), the washers (4), the bracket (3) and the panel (2). 4. Procedure _________ (Ref. Fig. 302/TASK 12-14-32-991-031, 303/TASK 12-14-32-991-002-A) Subtask 12-14-32-614-050 R
A. Gas Replenishment of the MLG Shock Absorber (Aircraft on the Ground) CAUTION : DO NOT INFLATE THE MLG SHOCK ABSORBER AT THE LOWER VALVE. IF _______ YOU USE THE LOWER VALVE HYDRAULIC FLUID WILL COME OUT. (1) Measure and write down the shock absorber extension (dimension H).
R
(2) Connect the nitrogen source to the standard charging equipment.
R
(3) Install the ADAPTER, CHARGING - MLG to the standard charging equipment. (4) Install the ADAPTER, CHARGING - MLG on the bleed/inflation valve (1). (5) Open the bleed/inflation valve (1). (6) Read and write down the pressure shown on the pressure gage 0 - 200 bar. (7) Close the bleed/inflation valve (1).
EFF : ALL 12-14-32 SROS
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MLG Bleed/Inflation Valve Figure 301/TASK 12-14-32-991-001 EFF : ALL 12-14-32 SROS
Page 308 Apr 01/98
R R
Shock Absorber Dimension H Figure 302/TASK 12-14-32-991-031
R EFF : ALL 12-14-32 SROS
Page 309 Apr 01/04
R
MLG Shock Absorber Inflation Chart Figure 303/TASK 12-14-32-991-002-A12 (SHEET 1)
EFF : ALL 12-14-32 SROS
Page 310 Jul 01/04
R
MLG Shock Absorber Inflation Chart Figure 303/TASK 12-14-32-991-002-A22 (SHEET 2)
EFF : ALL 12-14-32 SROS
Page 311 Jul 01/04
(8) Do these steps: (a) Use a thermometer to measure and write down the surface temperature of the aluminium piston adjacent to the bleed inflation valve (1). (b) Use the inflation chart to find the correct pressure from the temperature and dimension H measurements you recorded. (9) If the pressure measured at step (6) is lower than the pressure got from the inflation chart, do this procedure: WARNING : DO NOT PUT COMPRESSED GAS IN CONTACT WITH YOUR SKIN. THE _______ GAS CAN GO THROUGH THE SKIN AND MAKE BUBBLES IN THE BLOOD. THIS CONDITION CAN KILL YOU. (a) Adjust the nitrogen source to give the necessary pressure. (b) Slowly open the bleed/inflation valve (1). (c) Inflate the shock absorber to the correct pressure shown on the inflation chart. (d) When the pressure is correct, close the bleed/inflation valve (1). If dimension H changes (before the correct pressure has been reached), measure dimension H again and do the steps from (8)(b) again with the new dimension H. (e) Close the charge valve on the nitrogen source and leave for a minimum of 10 minutes (to let the shock absorber stabilize). (f) Measure the pressure and dimension H again. (g) If the pressure has changed, do the steps (c) and (d) again. If the dimension H has changed, do the steps from (8)(b) again with the new dimension H. (h) Close the bleed/inflation valve (1). R R
(i) Stop the supply from the nitrogen source. Release the pressure and remove the nitrogen source from the standard charging equipment.
R
(j) Remove the standard charging equipment from the ADAPTER, CHARGING - MLG.
R EFF : ALL 12-14-32 SROS
Page 312 Jul 01/06
(k) TORQUE the bleed/inflation valve (1) to between 0.60 and 0.8 m.daN (50 and 70 lbf.in). (l) Remove the ADAPTER, CHARGING - MLG from the bleed/inflation valve (1). CAUTION : DO NOT INSTALL A DUST CAP ON THE BLEED/INFLATION VALVE _______ OF THE MLG SHOCK ABSORBER. IF YOU DO, THERE IS A RISK THAT IT WILL FALL INTO THE SHOCK ABSORBER. 1 _
Do not install a dust cap on the bleed/inflation valve.
(m) Use SPECIAL MATERIALS (Material No. 05-004B) to do a leak test of the bleed/inflation valve (1). Leakage must not occur. (10) If the pressure measured at step (6) is higher than the pressure got from the inflation chart, do this procedure: (a) Slowly open the bleed/inflation valve (1). (b) Deflate the shock absorber to the correct pressure you got at step (8)(b) from the inflation chart. If the dimension H changes (before the correct pressure has been reached), measure the dimension H again. Do the steps from (8)(b) again with the new dimension H. (c) Close the charge valve on the nitrogen source and leave for a minimum of 10 minutes (to let the shock absorber stabilize). (d) Measure the pressure and the dimension H again. (e) If the pressure has changed, do the steps (b) and (c) again. If the dimension H has changed, do the steps from (8)(b) again. Use the new dimension H. (f) Close the bleed/inflation valve (1). R
(g) Remove the nitrogen source from the standard charging equipment.
R
(h) Remove the standard charging equipment from the ADAPTER, CHARGING - MLG. (i) TORQUE the bleed/inflation valve (1) to between 0.60 and 0.8 m.daN (50 and 70 lbf.in).
EFF : ALL 12-14-32 SROS
Page 313 Jul 01/06
INTENTIONALLY BLANK
R 12-14-32 SROS
Page 314 Jul 01/06
(j) Remove the ADAPTER, CHARGING - MLG. CAUTION : DO NOT INSTALL A DUST CAP ON THE BLEED/INFLATION VALVE _______ OF THE MLG SHOCK ABSORBER. IF YOU DO, THERE IS A RISK THAT IT WILL FALL INTO THE SHOCK ABSORBER. 1 _
Do not install a dust cap on the bleed/inflation valve.
(k) Use the SPECIAL MATERIALS (Material No. 05-004B) to do a leak test of the bleed/inflation valve (1). Leakage must not occur. Subtask 12-14-32-614-051 B. Gas Replenishment of the MLG Shock Absorber (Aircraft on Jacks). WARNING : DO NOT PUT COMPRESSED GAS IN CONTACT WITH YOUR SKIN. THE GAS _______ CAN GO THROUGH THE SKIN AND MAKE BUBBLES IN THE BLOOD. THIS CONDITION CAN KILL YOU. CAUTION : DO NOT INFLATE THE MLG SHOCK ABSORBER AT THE LOWER VALVE. IF _______ YOU USE THE LOWER VALVE HYDRAULIC FLUID WILL COME OUT. (1) Make sure that the shock absorber is extended fully and the dimension H is between 773.5 mm (30.4527 in.) and 782.5 mm (30.8071 in.). (2) Do these steps: (a) Use a thermometer to measure and then write down the surface temperature of the aluminium piston adjacent to the bleed/inflation valve (1). (b) Look at the inflation chart and find the nearest fully extended inflation pressure (for the temperature you measured at step (a)). (3) Install the ADAPTER, CHARGING - MLG on the bleed/inflation valve (1). R
(4) Install the GEAR FILLING KIT-SHOCK ABSORBER or the standard charging equipment on the ADAPTER, CHARGING - MLG. (5) Set the nitrogen charge pressure to the inflation pressure you found at step (2)(b). Make sure the pressure control valve or the shut-off valve is closed. (6) Open the bleed/inflation valve (1) and read the pressure gage 0 - 60 bar.
EFF : ALL 12-14-32 SROS
Page 315 Apr 01/03
(7) To get the correct shock absorber pressure you calculated at step (2)(b): - open the pressure control valve to inflate the shock absorber OR - open the bleed control valve to deflate the shock absorber. (8) Inflate or deflate the shock absorber to get the correct pressure you calculated at step (2). (9) Close the nitrogen charge valve. (10) After a period of 10 minutes (to let the shock absorber become stable), measure the pressure again. (11) If the pressure has changed, do the steps (6) thru (8) again. (12) Close the bleed/inflation valve (1). (13) Stop the nitrogen supply and remove the nitrogen source from the GEAR FILLING KIT-SHOCK ABSORBER or the standard charging equipment. (14) Remove the GEAR FILLING KIT-SHOCK ABSORBER or the standard charging equipment from the ADAPTER, CHARGING - MLG. (15) TORQUE the bleed/inflation valve (1) to between 0.60 and 0.8 m.daN (50 and 70 lbf.in). (16) Remove the ADAPTER, CHARGING - MLG. CAUTION : DO NOT INSTALL A DUST CAP ON THE BLEED/INFLATION VALVE OF _______ THE MLG SHOCK ABSORBER. IF YOU DO, THERE IS A RISK THAT IT WILL FALL INTO THE SHOCK ABSORBER. (a) Do not install a dust cap on the bleed/inflation valve. (17) Use the SPECIAL MATERIALS (Material No. 05-004B) to do a leak test of the Bleed/inflation valve (1). Leakage must not occur. 5. Close-up ________ Subtask 12-14-32-410-050 A. Close Access (1) Install the access panel (2) with the bracket (3), the washers (4) and the bolts (5). (a) TORQUE tighten the bolts (5) to 0.34 m.daN (30.08 lbf.in).
EFF : ALL 12-14-32 R SROS
Page 316 Apr 01/03
(b) Safety the bolts (5) with MISCELLANEOUS (Material No. 19-010). (2) Remove the access platform(s). (3) Close the applicable MLG door (Ref. TASK 32-12-00-410-801). Subtask 12-14-32-942-050 B. Removal of Equipment (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 12-14-32 R SROS
Page 317 Apr 01/03
TASK 12-14-32-614-804 Gas Replenishment of the NLG Shock Absorber WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED ON THE _______ LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. 1. __________________ Reason for the Job This task gives the procedure for gas replenishment when the aircraft is on the ground and when the aircraft is on jacks. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No No R
specific specific specific specific specific specific specific specific specific
U21891000
nitrogen source pressure gage 130 bar pressure gage 20 bar pressure gage 80 bar safety barriers standard charging equipment warning notices access platform 2.5 m (8 ft. 2 in.) Torque Wrench : range 0.00 to 1.20 m.daN (0.00 to 9.00 lbf.ft) 2 ADAPTOR - INFLATION
EFF : ALL 12-14-32 SROS
Page 318 Jan 01/07
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 05-004B
USA MIL-L-25567 TYPE I OXYGEN LEAK DETECTOR (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-804 32-00-00-481-801 32-00-00-860-805 32-00-00-860-806 32-22-00-010-801 32-22-00-410-801 32-51-00-040-801 12-14-32-991-006 12-14-32-991-005 12-14-32-991-027 12-14-32-991-026 12-14-32-991-029
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Installation of the Safety Devices on the Landing Gears Ground Configuration after Flight Configuration Put the Aircraft in a Ground Configuration when it is Raised on Jacks Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance Deactivation of the Nose Wheel Steering Fig. 304 Fig. 305 Fig. 306 Fig. 307 Fig. 308
3. __________ Job Set-up Subtask 12-14-32-941-054 A. Safety Precautions (1) Put the warning notices in the cockpit to tell persons not to: - operate the landing gear controls - operate the nose wheel steering controls.
R
(2) Put the safety barriers in position.
EFF : ALL 12-14-32 SROS
Page 319 Jul 01/06
Subtask 12-14-32-860-054 B. Aircraft Maintenance Configuration NOTE : Do not install chocks to the NLG or the CLG during this procedure. ____ (1) Put the aircraft in: (a) Ground configuration after flight configuration, (Ref. TASK 3200-00-860-805). R R
(b) Aircraft in ground configuration when it is raised on jacks, (Ref. TASK 32-00-00-860-806). (2) Put the nose wheels in a central position. (3) Make sure that the green hydraulic system is depressurized, (Ref. TASK 29-00-00-864-804). (4) Deactivate the nose wheel steering NW/S, (Ref. TASK 32-51-00-040801). (5) Install the safety devices on the landing gear, (Ref. TASK 32-00-00481-801). Subtask 12-14-32-010-050 C. Get Access (1) Open the NLG doors (Ref. TASK 32-22-00-010-801). (2) Put the access platform adjacent to the NLG. 4. Procedure _________ (Ref. Fig. 304/TASK 12-14-32-991-006) Subtask 12-14-32-614-056
R
A. Gas Replenishment of the NLG Shock Absorber (Aircraft on the Ground) (Ref. Fig. 305/TASK 12-14-32-991-005) WARNING : DO NOT PUT COMPRESSED GAS IN CONTACT WITH YOUR SKIN. THE GAS _______ CAN GO THROUGH THE SKIN AND MAKE BUBBLES IN THE BLOOD. THIS CONDITION CAN KILL YOU.
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NLG - Pressure/Extension Graph 1 Figure 304/TASK 12-14-32-991-006
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Page 321 Apr 01/04
NLG Shock Absorber - Inflation Valves Figure 305/TASK 12-14-32-991-005
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Page 322 Apr 01/04
(1) Remove the blanking caps (1) and (3) from the inflation valves (2) and (4). (2) Install the nitrogen source to the standard charging equipment. R R
(3) Install the standard charging equipment to supply each ADAPTOR INFLATION. Connect a pressure gage 130 bar to each of the charging valves (2) and (4).
R
(4) Install a ADAPTOR - INFLATION on the inflation valves (2) and (4). (5) Open the inflation valves (2) and (4). (6) Measure and write down the ambient temperature (temperature T1). (7) Read and write down the pressure at the inflation valve (2) (pressure P1) and at the inflation valve (4) (pressure P2).
R R
(8) If the pressure at P2 is less than the pressure at P1 plus 6.9 bar (100 psi): (a) Open the shut off valves X and Z. (b) Slowly pressurize the inflation valve (4) until the pressure at P2 is 6.9 bar (100 psi) more than the pressure at P1. NOTE : This makes sure that the floating piston goes against its ____ stop in the fully up position. (9) Measure and write down the shock absorber extension (dimension H). (10) Close the shut off valve Z and open the shut off valve Y. (a) Slowly add or remove nitrogen at the inflation valve (2) until the dimension H plus or minus 1 mm (0.04 in) agrees with the pressure P1 shown on the graph at ambient temperature T1. (Ref. Fig. 306/TASK 12-14-32-991-027) (11) Compare the pressure P1 and the pressure P2. If the pressure P2 is more than the pressure at P1, do paragraphs (13) thru (23). NOTE : If the pressure P2 is more than the pressure P1, this shows ____ that the floating piston has stayed against the stop in the fully up position. (12) If the pressure P2 is equal to or less than the pressure at P1, do paragraphs (5) thru (11) again.
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R
NLG - Pressure/Extension Graph ( C) Figure 306/TASK 12-14-32-991-027
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Page 324 Jan 01/07
(13) Use the pressure P1 and T1 and find the position of P1 in relation to the Nominal pressure line on the graph. (Ref. Fig. 307/TASK 12-14-32-991-026) (14) If the measured pressure P1 is above the Nominal line shown on the graph, do this step: (a) Close the shut off valve Y and open the shut off valve Z. (b) Slowly remove nitrogen at the inflation valve (4) until the dimension H plus or minus 1 mm (0.04 in) agrees with the graph at pressure P1 and temperature T1. (Ref. Fig. 304/TASK 12-14-32-991-006) NOTE : The floating piston moves away from the stop. ____ (c) Compare the pressure P1 and P2. If the pressure P2 is the same as pressure P1, do paragraphs (16) to (23). (15) If the measured pressure P1 is equal to or below the Nominal line shown on the graph, do this step: (a) Slowly decrease the pressure at the inflation valve (4) until the pressure P2 agrees with the graph. (Ref. Fig. 307/TASK 12-14-32-991-026) NOTE : The floating piston stays against the stop. ____ (b) Compare the pressures P1 and P2. If the pressure P2 is more than the pressure P1 do the paragraphs (16) thru (23). (16) Close the inflation valves (2) and (4). (17) Stop the supply from the nitrogen source. Release the pressure and remove the nitrogen source from the standard charging equipment. R
(18) Remove the standard charging equipment from each ADAPTOR - INFLATION.
R
(19) Remove each ADAPTOR - INFLATION from the inflation valves (2) and (4). (20) TORQUE the inflation valves (2) and (4) to between 0.5 and 0.8 m.daN (44.24 and 70.79 lbf.in). (21) Use the SPECIAL MATERIALS (Material No. 05-004B) to do a leak test of the inflation valves (2) and (4). Leakage must not occur.
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NLG Shock Absorber - Pressure/Temperature Graph Figure 307/TASK 12-14-32-991-026
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Page 326 Apr 01/04
(22) Install the blanking caps (1) and (3) on the inflation valves (2) and (4). (23) Close the NLG doors (Ref. TASK 32-22-00-410-801). Subtask 12-14-32-614-057 B. Gas Replenishment of the NLG Shock Absorber (Aircraft on Jacks) (Ref. Fig. 305/TASK 12-14-32-991-005, 308/TASK 12-14-32-991-029) (1) Make sure that the shock absorber is extended fully and the dimension H is between 408 and 416 mm (16.07 and 16.37 in). (2) Remove the blanking caps (1) and (3) from the inflation valves (2) and (4). R
(3) Install a ADAPTOR - INFLATION on each of the inflation valves (2) and (4).
R
(4) Install the GEAR FILLING KIT-SHOCK ABSORBER or the standard charging equipment to supply each ADAPTOR - INFLATION. Make sure that the pressure gage 20 bar connects to the charging valve (2) and the pressure gage 80 bar connects to the charging valve (4) (5) Measure and write down the ambient temperature. (6) Make sure that the shut-off valve Z is closed and open the inflation valve (4) with the ADAPTOR - INFLATION.
R
(7) Read and write down the pressure shown on the pressure gage for the inflation valve (4)(Pressure P2). (8) Compare the values with the values shown on the graph. (Ref. Fig. 307/TASK 12-14-32-991-026) (9) If the nitrogen pressure is not correct for the ambient temperature on the graph, do this procedure: WARNING : DO NOT PUT COMPRESSED GAS IN CONTACT WITH YOUR SKIN. THE _______ GAS CAN GO THROUGH THE SKIN AND MAKE BUBBLES IN THE BLOOD. THIS CONDITION CAN KILL YOU. (a) Open the shut-off valve X and Z and adjust the nitrogen-source supply pressure to the correct figure shown on the graph. (b) Close the shut-off valves X and Z and stop the supply from the nitrogen source.
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Pressure/Temperature Graph 2 Figure 308/TASK 12-14-32-991-029
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Page 328 Apr 01/04
(10) Close the inflation valve (4). (11) Make sure that the shut-off valve Y is closed and open the inflation valve (2) with the ADAPTOR - INFLATION.
R
(12) Read and write down the pressure shown on the pressure gage for the inflation valve (2)(Pressure P1). (13) Compare the values with the values shown on the graph. (Ref. Fig. 308/TASK 12-14-32-991-029) (14) If the nitrogen pressure is not correct for the ambient temperature on the graph, do this procedure: WARNING : DO NOT PUT COMPRESSED GAS IN CONTACT WITH YOUR SKIN. THE _______ GAS CAN GO THROUGH THE SKIN AND MAKE BUBBLES IN THE BLOOD. THIS CONDITION CAN KILL YOU. (a) Open the shut-off valve X and Y and adjust the nitrogen-source supply pressure to the correct figure shown on the graph. (b) Close the shut-off valves X and Y and stop the supply from the nitrogen source. (15) Close the inflation valve (2). (16) Repeat steps (5) thru (15) and make sure that the pressures P1 and P2 are correct. R
(17) Remove the GEAR FILLING KIT-SHOCK ABSORBER or the standard charging equipment from each ADAPTOR - INFLATION.
R
(18) Remove the ADAPTOR - INFLATION from each inflation valve. (19) TORQUE the inflation valve (2) and (4) to between 0.5 and 0.8 m.daN (44.24 and 70.79 lbf.in). (20) Install the blanking caps (1) and (3) to the inflation valves (2) and (4). (21) Use the SPECIAL MATERIALS (Material No. 05-004B) to do a leak test of the inflation valves (2) and (4). Leakage must not occur. 5. Close-up ________ Subtask 12-14-32-942-054 A. Removal of the Ground Support Equipment (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
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INTENTIONALLY BLANK
R 12-14-32 SROS
Page 330 Jan 01/07
TASK 12-14-32-614-807 Pressurization of the Brake Accumulator (5258GG, 5259GG, 5490GG, 5491GG, 5426GG, 5427GG) WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED ON THE _______ LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. WARNING : MAKE SURE THAT THE WHEEL CHOCKS ARE IN POSITION. MOVEMENTS OF THE _______ AIRCRAFT COULD BE DANGEROUS. 1. __________________ Reason for the Job NOTE : The Alternate Brake Return Accumulator is part of the Manifold ____ 5490GG(5491GG). 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R R
No No No No No
specific specific specific specific specific
accumulator filling system circuit breaker(s) safety clip(s) warning notice access platform 2.1 m (6 ft. 11 in.) Torque Wrench : range 0.00 to 1.20 m.daN (0.00 to 9.00 lbf.ft)
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B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-804 32-45-00-864-801 R R R R
12-14-32-991-007 12-14-32-991-012 12-14-32-991-014 12-14-32-991-020
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Release the Pressure from the Parking Brake System after Depressurization Fig. 309 Fig. 310 Fig. 311 Fig. 312
3. __________ Job Set-up Subtask 12-14-32-941-056 A. Safety Precautions WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. (1) Put the warning notice in the cockpit to tell persons not to pressurize the Blue or Green hydraulic systems. Subtask 12-14-32-860-055 B. Aircraft Maintenance Configuration (1) Put the wheel chocks in position. (2) On the panel 117VU, set the PARK BRK to the OFF position. (3) Make sure that the hydraulic systems are depressurized (Ref. TASK 2900-00-864-804). (4) Release the pressure from the Parking Brake system after depressurization (Ref. TASK 32-45-00-864-801).
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Subtask 12-14-32-010-052 C. Get Access (1) Put the access platform in the applicable position: FOR 5426GG, 5427GG at the zone 195 FOR 5258GG, 5259GG, 5490GG, 5491GG at the zone 731(741). Subtask 12-14-32-865-059 D. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU HYD PUMP G CTL 9JV U09 721VU HYD PUMP B CTL 9JC X12 722VU BSCU SYS 2 2GG U37 742VU BSCU SYS 1 1GG G62 4. Procedure _________ (Ref. Fig. 309/TASK 12-14-32-991-007) Subtask 12-14-32-614-061 R
A. Pressurize the Brake Return Accumulator (5258GG, 5259GG, 5490GG, 5491GG) (1) Remove the cap (1). (2) Install the accumulator filling system on the applicable charge valve. (3) Set the nitrogen supply pressure on the gage to 1 bar (14.5037 psi) more than the correct pressure for the related ambient temperature.
R R
CAUTION : MAKE SURE THAT YOU USE THE CORRECT PRESSURE CHART. THIS _______ PREVENTS DAMAGE TO THE HYDRAULIC SYSTEM COMPONENTS. (Ref. Fig. 310/TASK 12-14-32-991-012)
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Brake Accumulators - Location and Detail Figure 309/TASK 12-14-32-991-007
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Page 334 Apr 01/04
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Brake Return Accumulators - Pressure Graph Figure 310/TASK 12-14-32-991-012
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Page 335 Jan 01/07
(4) Slowly open the control nut (2) on the charge valve. NOTE : When the charge valve is opened initially, the pressure will ____ decrease to approximately 1 bar (14.5 psi) less than the correct pressure. It will then slowly increase. (5) Close the control nut (2) when the needle on the accumulator pressure gage goes through the correct pressure. (6) TORQUE the control nut (2) to between 0.5 and 0.85 m.daN (44.24 and 75.22 lbf.in). (7) Stop the nitrogen supply. (8) Let the accumulator stay for approximately 10 minutes for its temperature to become stable. (9) Make sure that the accumulator gage needle is in the green sector. (10) Remove the accumulator filling system and check for leakage. (11) Install the cap (1). (12) TORQUE the cap (1) to between 0.1 and 0.12 m.daN (8.84 and 10.61 lbf.in). Subtask 12-14-32-614-067 R
B. Pressurize the Alternate Brake 6L Accumulators (5426GG, 5427GG) (1) Remove the cap (1). (2) Install the accumulator filling system on the applicable charge valve. (3) Set the supply pressure to the correct pressure for the related ambient temperature.
R R
CAUTION : MAKE SURE THAT YOU USE THE CORRECT PRESSURE CHART. THIS _______ PREVENTS DAMAGE TO THE HYDRAULIC SYSTEM COMPONENTS. (Ref. Fig. 311/TASK 12-14-32-991-014) (4) Open the control nut (2) and slowly pressurize the accumulator to the correct pressure for the related ambient temperature.
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R
Alternate Brake 6L Accumulators - Pressure Graph Figure 311/TASK 12-14-32-991-014
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Page 337 Jul 01/06
(5) Let the filling system and accumulator pressure become equal and close the control nut (2). (Ref. Fig. 312/TASK 12-14-32-991-020) NOTE : The other accumulator will show a pressure increase. ____ This is an incorrect indication. (6) TORQUE the control nut (2) to between 0.5 and 0.85 m.daN (44.24 and 75.22 lbf.in). (7) Release the pressure from the Parking Brake System (Ref. TASK 32-4500-864-801). (8) Do the steps 1 thru 7 again for the other accumulator. NOTE : It is possible that you will need to do the steps 1 thru 7 ____ more than once for each accumulator, until a correct stable pressure shows. (9) Let the accumulator stay for approximately 10 minutes for its temperature to become stable. (10) Make sure that the accumulator gage shows the correct pressure. (11) Remove the accumulator filling system and check for leakage. (12) Install the cap (1). (13) TORQUE the cap (1) to between 0.1 and 0.12 m.daN (8.84 and 10.61 lbf.in). 5. Close-up ________ Subtask 12-14-32-865-060 A. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GG, 2GG, 9JC, 9JV. Subtask 12-14-32-942-056 B. Removal of Equipment (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
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Alternate Park Brake Accumulators - Location and Detail Figure 312/TASK 12-14-32-991-020 EFF : ALL 12-14-32 R SROS
Page 339 Jul 01/06
TASK 12-14-32-614-811 Depressurization of the Brake Accumulator (5258GG, 5259GG, 5490GG, 5491GG, 5426GG and 5427GG) WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED ON THE _______ LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. WARNING : MAKE SURE THAT THE WHEEL CHOCKS ARE IN POSITION. MOVEMENTS OF THE _______ AIRCRAFT COULD BE DANGEROUS. 1. __________________ Reason for the Job NOTE : The Alternate Brake Return Accumulator is part of the Manifold ____ 5490GG(5491GG). 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific No specific No specific
circuit breaker(s) safety clip(s) warning notice access platform 2.1 m (6 ft. 11 in.)
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B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-804 32-12-14-400-801 32-42-41-000-801 32-42-41-400-801 32-43-00-870-801 32-43-24-000-801 32-43-24-400-801 32-45-00-864-801 R R R
12-14-32-991-009 12-14-32-991-010 12-14-32-991-011 FOR FIN 5490GG, 5491GG 32-12-14-000-801
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Installation of the MLG Fixed Fairing Assembly Removal of the MLG Normal Brake Return Accumulator 5258GG(5259GG) Installation of the MLG Normal Brake Return Accumulator 5258GG(5259GG) Bleeding the Alternate Braking System at the Wheel Brakes Removal of the MLG Alternate Brake Return Accumulator Installation of the MLG Alternate Brake Return Accumulator Release the Pressure from the Parking Brake System after Depressurization Fig. 313 Fig. 314 Fig. 315 Removal of the MLG Fixed Fairing Assembly
3. __________ Job Set-up Subtask 12-14-32-941-057 A. Safety Precautions WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. (1) Put the warning notice in the cockpit to tell persons not to pressurize the hydraulic systems. Subtask 12-14-32-860-056 B. Aircraft Maintenance Configuration (1) Put the wheel chocks in position. (2) On the panel 117VU, set the PARK BRK to the OFF position.
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Page 341 Apr 01/04
(3) Make sure that the hydraulic systems are depressurized (Ref. TASK 2900-00-864-804) (4) Make sure that the Park Brake accumulators are depressurized (Ref. TASK 32-45-00-864-801). Subtask 12-14-32-010-053 C. Get Access (1) Put the access platform in the applicable position: FOR 5426GG, 5427GG at the zone 195 FOR 5258GG, 5259GG, 5490GG, 5491GG at the zone 731(741). (2) FOR 5490GG, 5491GG remove the fixed fairing assembly (Ref. TASK 32-12-14-000-801). Subtask 12-14-32-865-061 D. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU HYD PUMP G CTL 9JV U09 721VU HYD PUMP B CTL 9JC X12 722VU BSCU SYS 2 2GG U37 742VU BSCU SYS 1 1GG G62 4. Procedure _________ Subtask 12-14-32-614-062 R
A. Depressurization of the Brake Accumulator (5258GG and 5259GG) (Ref. Fig. 313/TASK 12-14-32-991-009) (1) Remove the applicable return Brake accumulator (Ref. TASK 32-42-41000-801), but do not disconnect the hydraulic connectors. (2) Put the accumulator in the vertical position with the pressure gage (2) at the top.
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Brake Accumulators - Location and Detail Figure 313/TASK 12-14-32-991-009
R
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(3) Remove the cap (3). (4) Carefully loosen the control nut (1) and let the pressure decrease to zero on the pressure gage (2). (5) Close the control nut (1). (6) Install the cap (3). (7) Install the accumulator (Ref. TASK 32-42-41-400-801). Subtask 12-14-32-614-063 R
B. Depressurization of the Brake Accumulator (5490GG and 5491GG) (Ref. Fig. 314/TASK 12-14-32-991-010) (1) Remove the accumulator (Ref. TASK 32-43-24-000-801). (2) Hold the accumulator in the vertical position with the pressure gage (2) at the top. (3) Remove the cap (3). (4) Carefully loosen the control nut (1) and let the pressure decrease to zero on the pressure gage (2). NOTE : An amount of hydraulic fluid can come out with the nitrogen. ____ This is normal and further maintenance is not necessary. (5) Close the control nut (1). (6) Install the cap (3). (7) Install the accumulator (Ref. TASK 32-43-24-400-801). (8) Bleed the Blue hydraulic system (Ref. TASK 32-43-00-870-801). (9) Install the fixed fairing assembly (Ref. TASK 32-12-14-400-801). Subtask 12-14-32-614-064
R
C. Depressurization of the Park Brake Accumulator (5426GG, 5427GG) (Ref. Fig. 315/TASK 12-14-32-991-011) (1) Remove the cap (2). (2) Carefully loosen the control nut (3) and let the pressure decrease to zero on the pressure gage (1). (3) Close the control nut (3).
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Brake Accumulators - Location and Detail Figure 314/TASK 12-14-32-991-010
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Brake Accumulators - Location and Detail Figure 315/TASK 12-14-32-991-011
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(4) Install the cap (2). 5. Close-up ________ Subtask 12-14-32-942-057 A. Removal of Equipment (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
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Page 347 Jul 01/03
TASK 12-14-32-614-814 Depressurization of the Nose Wheel Steering Accumulator 5110GC WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED ON THE _______ LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No No No No No No
specific specific specific specific specific specific
bleed hose circuit breaker(s) safety clip(s) safety barriers warning notices container 2.0 l (0.5283 USgal) access platform 2.0 m (6 ft. 7 in.)
EFF : ALL 12-14-32 SROS
Page 348 Jan 01/05
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-14-32-614-812 29-00-00-864-801 29-14-00-614-801 R 32-51-00-040-801 12-14-32-991-015
Pressurization of the Nose Wheel Steering Accumulator 5110GC Depressurize the Green Hydraulic System (Pressurized with the Electric Pump) Depressurization of the Green Hydraulic Reservoir with Ground Equipment Deactivation of the Nose Wheel Steering Fig. 316
3. __________ Job Set-up Subtask 12-14-32-941-069 A. Safety Precautions (1) Put the safety barriers in position. (2) Put the warning notices in these positions: - on the ground services panel, to tell persons not to pressurize the Green hydraulic system - on the panel 245VU, to tell persons not to pressurize the Green hydraulic system. Subtask 12-14-32-860-062 B. Aircraft Maintenance Configuration (1) Deactivate the Nose Wheel Steering (Ref. TASK 32-51-00-040-801). (2) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (3) Depressurize the reservoir of the Green hydraulic system (Ref. TASK 29-14-00-614-801).
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Page 349 Apr 01/05
Subtask 12-14-32-865-073 C. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------722VU BSCU SYS 2 2GG U37 742VU BSCU SYS 1 1GG G62 4. Procedure _________ Subtask 12-14-32-614-068 A. Depressurization of the Nose Wheel Steering Accumulator WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. R
(Ref. Fig. 316/TASK 12-14-32-991-015) (1) Put the access platform in position adjacent to the NWS hydraulic block. (2) Cut, remove and discard the lockwire from the cover (1). (3) Remove the cover (1) and the dustcap (2). (4) Slowly open the charge valve to release the pressure. (5) Close the charge valve and temporarily install the dustcap (2) and the cover (1). (6) To release the hydraulic pressure remaining in the Nose Wheel Steering System, do these steps: (a) Put a container below the bleed valve. (b) Remove the cap (3). (c) Put a bleed hose on the bleed valve. (d) Slowly loosen the bleed valve to release the hydraulic pressure. (e) When the flow of hydraulic fluid stops, tighten the bleed valve and remove the bleed hose.
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Page 350 Apr 01/04
Nose Wheel Steering Accumulator - Location and Detail Figure 316/TASK 12-14-32-991-015
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Page 351 Apr 01/04
(f) Install the cap (3) on the bleed valve. 5. Close-up ________ Subtask 12-14-32-860-061 A. Aircraft Maintenance Configuration (1) When the related maintenance operation is complete, pressurize the Nose Wheel Steering accumulator (Ref. TASK 12-14-32-614-812).
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Page 352 Jul 01/03
TASK 12-14-32-614-812 Pressurization of the Nose Wheel Steering Accumulator 5110GC WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED ON THE _______ LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No
specific specific specific specific specific specific specific
container pressure gage safety barriers thermometer warning notices Nitrogen Filling System access platform 2.0 m (6 ft. 7 in.)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------No specific
lockwire, corrosion resistant steel 0.8 mm (0.032 in.)
EFF : ALL 12-14-32 R SROS
Page 353 Apr 01/04
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-802 29-00-00-864-801 29-14-00-614-801 R 12-14-32-991-015
Fill the Green Hydraulic Reservoir with a Hand Pump Depressurize the Green Hydraulic System (Pressurized with the Hydraulic Ground Supply) Depressurization of the Green Hydraulic Reservoir with Ground Equipment Fig. 316
3. __________ Job Set-up Subtask 12-14-32-941-058 A. Safety Precautions (1) Put the safety barriers in position. (2) Put the warning notices in the cockpit and on the ground services panel to tell persons: - not to pressurize the Green hydraulic system - not to pressurize the Green hydraulic system reservoir. Subtask 12-14-32-860-059 B. Aircraft Maintenance Configuration (1) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (2) Depressurize the Green hydraulic system reservoir (Ref. TASK 29-1400-614-801). (3) Put the access platform in position at the NLG leg. Subtask 12-14-32-865-071 C. Get access to the avionics compartment. Then make sure that this(these) circuit breaker(s) is (are) open, safetied and tagged: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------722VU BSCU SYS 2 2GG U37 742VU BSCU SYS 1 1GG G62
EFF : ALL 12-14-32 SROS
Page 354 Apr 01/05
4. Procedure _________ Subtask 12-14-32-614-066 R
A. Pressurization of the NWS Accumulator with Nitrogen (Ref. Fig. 316/TASK 12-14-32-991-015) (1) Remove the cap (3) from the hydraulic bleed valve. (2) Put a container in position below the bleed valve. (3) Open the bleed valve. NOTE : The flow of hydraulic fluid from the bleed valve can stop and ____ start again as the accumulator is filled. (4) Remove and discard the lockwire from the cover (1). (5) Remove the cover (1) and the dust cap (2) from the charge valve. (6) Install the Nitrogen Filling System on the charge valve. (7) Slowly open the charge valve to pressurize the NWS accumulator to between 25 bar (362.5942 psi) and 40 bar (580.1508 psi). This will make sure that the piston in the accumulator is at the bottom. NOTE : The flow of hydraulic fluid from the bleed valve can stop and ____ start again as the accumulator is filled. (8) Close the charge valve. (9) Use a thermometer to measure the ambient temperature. (10) On the filling system, set the nitrogen pressure to the correct value for the ambient temperature (as shown in Table 1). Table 1
EFF : ALL 12-14-32 SROS
Page 355 Apr 01/04
------------------------------------------------------------------------------| Temperature | Charging Pressure | |---------------------------|-------------------------------------------------| | deg.C | deg.F | BAR | PSI | |-----------------------------------------------------------------------------| | -40 | -40 | 3.60 | 52.2 | | -30 | -22 | 3.75 | 54.4 | | -20 | - 4 | 3.90 | 56.6 | | -10 | 14 | 4.05 | 58.7 | | 0 | 32 | 4.20 | 60.9 | | 10 | 50 | 4.35 | 63.1 | | 20 | 68 | 4.50 | 65.1 | | 30 | 86 | 4.65 | 67.4 | | 40 | 104 | 4.75 | 68.8 | | 50 | 112 | 5.00 | 72.5 | | 60 | 140 | 5.20 | 75.4 | ------------------------------------------------------------------------------(11) Slowly open the charge valve and let the NWS accumulator pressure decrease to the correct value. (12) Close the charge valve. (13) Let the accumulator temperature become stable (approximately 10 minutes for a full pressurization from zero pressure). (14) Close the hydraulic bleed valve. (15) Remove the Nitrogen Filling System. (16) Use an applicable pressure gage to do a check of the gas pressure. If necessary pressurize the accumulator again. (17) Install the cap (3). (18) Install the dust cap (2) and the cover (1). R R
(19) TORQUE the cover (1) to between 0.15 m.daN (13.27 lbf.in) and 0.17 m.daN (15.04 lbf.in). (20) Safety the cover (1) with lockwire, corrosion resistant steel 0.8 mm (0.032 in.).
EFF : ALL 12-14-32 SROS
Page 356 Jan 01/06
5. Close-up ________ Subtask 12-14-32-611-050 A. Aircraft Maintenance Configuration (1) Make sure that the contents of the Green hydraulic reservoir is correct (Ref. TASK 12-12-29-611-802). R R R R
Subtask 12-14-32-865-072 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GG, 2GG Subtask 12-14-32-942-058
R
C. Removal of Equipment (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 12-14-32 SROS
Page 357 Jul 01/03
OXYGEN - SERVICING __________________ TASK 12-14-35-600-801 Servicing of the Oxygen Replenishing WARNING : KEEP ALL HYDROCARBONS (FUELS, LUBRICANTS, ETC.) AWAY FROM ALL SOURCES _______ OF OXYGEN. OXYGEN BECOMES EXPLOSIVE WHEN IT TOUCHES HYDROCARBONS. R
R R
WARNING : OBEY THESE SPECIAL PRECAUTIONS WHEN YOU DO THIS PROCEDURE: _______ - PREVENT ALL MAINTENANCE PROCEDURES NEARER THAN 5M (16.5 FT) TO THE WORKING AREA OF THE AIRCRAFT: - ALSO STOP ALL REFUELING, ALL REPAIRS ON FUEL AND HYDRAULIC SYSTEMS, ALL PROCEDURES THAT USE FLAMMABLE MATERIALS SUCH AS CLEANING AND DE-ICING MATERIALS. MAKE SURE THAT NO PERSONS CONNECT/DISCONNECT THE GROUND POWER CONNECTOR. - MAKE SURE THAT NO PERSONS SMOKE, AND THAT THERE ARE NO FLAMES, IN A RADIUS OF 15M (49.5 FT) OF THE REPLENISHING EQUIPMENT. USE ONLY TOOLS/GROUND SERVICING EQUIPMENT MADE SPECIALLY FOR OXYGEN SYSTEMS. - MAKE SURE THAT YOUR HANDS AND ALL THE TOOLS/GROUND SERVICING EQUIPMENT ARE CLEAN. THIS WILL PREVENT CONTAMINATION OF THE OXYGEN SYSTEM AND OF THE GROUND SERVICING EQUIPMENT. - CAREFULLY OBEY THE REPLENISHING INSTRUCTIONS ON THE AIRCRAFT PLACARDS. IF YOU DO NOT OBEY THESE INSTRUCTIONS, YOU CAN CAUSE A FIRE OR AN EXPLOSION. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No
specific specific specific specific
bonding cable circuit breaker(s) safety clip(s) warning notice access platform 2.5 m (8 ft. 2 in.)
EFF : ALL 12-14-35 SROS
Page 301 Oct 01/04
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-34-24-860-801 24-41-00-861-801 24-41-00-862-801 31-60-00-860-801 31-60-00-860-802 12-14-35-991-001 12-14-35-991-002
Aircraft Grounding for the Refuel/Defuel and Oxygen Servicing Operations Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A EIS Start Procedure EIS Stop Procedure Fig. 301 Fig. 302
3. __________ Job Set-up Subtask 12-14-35-861-050 R
A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). Subtask 12-14-35-010-050 B. Get Access (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the cover of the oxygen box. Subtask 12-14-35-941-050 C. Safety Precautions (Ref. Fig. 301/TASK 12-14-35-991-001) (1) Make sure that the overboard discharge indicator shows green. (2) Put a warning notice in position in the work area to tell persons that the oxygen filling operation is dangerous. (3) Make sure that the date of the test given on the cylinder is in the permitted time limit.
EFF : ALL 12-14-35 SROS
Page 302 Oct 01/04
Location of the Oxygen Filling Port Figure 301/TASK 12-14-35-991-001 EFF : ALL 12-14-35 R SROS
Page 303 Apr 01/00
(4) Make sure that the oxygen line end-fittings and the electrical connectors are in the correct condition. Subtask 12-14-35-865-050 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------742VU CREW OXY CTL 4HT L73 Subtask 12-14-35-860-050 E. Aircraft Maintenance Configuration (Ref. Fig. 302/TASK 12-14-35-991-002) (1) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00-860-801). (2) Do this step to electrically ground the oxygen ground-filling equipment: (a) Connect a bonding cable between the aircraft and the oxygen ground-filling equipment (Ref. TASK 12-34-24-860-801). 4. Procedure _________ Subtask 12-14-35-614-050 A. Servicing of the Oxygen Replenishing (Ref. Fig. 301/TASK 12-14-35-991-001) (1) Remove the blanking plug from the filling port 5769HT. R R
(2) Connect the filling assembly to the filling port 5769HT. (3) Measure the Outside Air Temperature (OAT) and the cockpit temperature with a thermometer. (4) Find the filling pressure. To do this, refer to the temperatures and the aircraft placards. (Ref. Fig. 302/TASK 12-14-35-991-002) (5) Slowly pressurize the system. Make sure that the filling pressure is correct on the pressure gage on the cylinder.
EFF : ALL 12-14-35 SROS
Page 304 Apr 01/02
Filling Pressure Figure 302/TASK 12-14-35-991-002 EFF : ALL 12-14-35 SROS
Page 305 Apr 01/98
Subtask 12-14-35-210-050 B. Test (1) Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 4HT (2) Make sure that the pressure value shown on the pressure gage is the same as the pressure indication on the DOOR page of the SD. 5. Close-up ________ Subtask 12-14-35-860-051 A. Put the Aircraft back to its Initial Configuration (1) Disconnect the filling assembly. (2) Put the blanking plug on the filling port. (3) Disconnect the bonding cable (Ref. TASK 12-34-24-860-801). (4) Make sure that the work area is clean and clear of tools and other items. (5) Do the EIS stop procedure (Ref. TASK 31-60-00-860-802). Subtask 12-14-35-410-050 B. Close Access R
(1) Close the cover of the oxygen box.
R
(2) Remove the warning notice(s).
R
(3) Close the access door 811.
R
(4) Remove the access platform(s). Subtask 12-14-35-862-050 C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
EFF : ALL 12-14-35 SROS
Page 306 Apr 01/02
WATER - DESCRIPTION AND OPERATION _________________________________ 1. _______ General This topic gives instructions for the servicing of the potable water system.
EFF : ALL 12-15-00 SROS
Page 1 Apr 01/98
POTABLE WATER - SERVICING _________________________ TASK 12-15-38-613-801 Fill the Potable Water System (Aircraft Electrical Power Available) WARNING : DO NOT DO WORK ON THE TOILET WASTE SYSTEM AND THE POTABLE WATER _______ SYSTEM AT THE SAME TIME. THIS WILL PREVENT CONTAMINATION OF THE POTABLE WATER SYSTEM. SUCH CONTAMINATION CAN BE DANGEROUS TO HEALTH. WARNING : BEFORE YOU DO WORK ON THE POTABLE WATER SYSTEM, CLEAN YOUR HANDS WITH _______ SOAP AND WATER. THIS WILL PREVENT INFECTION. (CONTAMINATION FROM TOILET WASTE IS DANGEROUS TO HEALTH). WARNING : MAKE SURE THAT THE EQUIPMENT YOU USE FOR THIS PROCEDURE IS CLEAN AND _______ APPROVED FOR THE POTABLE WATER SYSTEM. IF NOT IT CAN CAUSE CONTAMINATION OF THE POTABLE WATER SYSTEM. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
1 ACCESS PLATFORM 1M (3 FT) 1 CART - SERVICING, WATER, POTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-31-38-660-801 12-33-21-618-801 24-41-00-861-801 24-41-00-862-801 12-15-38-991-001-A
Cold Weather Maintenance Practices for Water/Waste Pre-conditioning through the Low-Pressure Ground Connection Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Fig. 301
EFF : ALL 12-15-38 R SROS
Page 301 Jul 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-15-38-991-003 12-15-38-991-002
Fig. 302 Fig. 303
3. __________ Job Set-up Subtask 12-15-38-861-051 A. Make sure that the Aircraft Electrical Circuits are energized (Ref. TASK 24-41-00-861-801). Subtask 12-15-38-865-053 B. Get access to the applicable 5000VE series panel(s). Then make sure that this(these) circuit breaker(s) is (are) closed.
R
------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------5005VE WATER SYSTEM QUANT IND 1MA E06 5005VE WATER SYSTEM DRAIN 1MP E05 Subtask 12-15-38-618-050 C. Preparation to Fill the Potable Water System (1) Obey the cold weather maintenance procedure (Ref. TASK 12-31-38-660801). (2) If the temperature in the aircraft is below 4 DEG.C (39.20 DEG.F) do the pre-conditioning procedure (Ref. TASK 12-33-21-618-801). Subtask 12-15-38-010-054 D. Get Access (1) Put the ACCESS PLATFORM 1M (3 FT) in position below the Potable-Water Service Panel (PWSP) at Zone 164. (2) Put the ACCESS PLATFORM 1M (3 FT) in position below the aft potable-water drain-panel at Zone 154.
EFF : ALL 12-15-38 SROS
Page 302 Jul 01/06
4. Procedure _________ Subtask 12-15-38-613-055 A. Fill the Potable Water System WARNING : MAKE SURE THAT THE EQUIPMENT YOU USE FOR THIS PROCEDURE IS _______ CLEAN AND APPROVED FOR THE POTABLE WATER SYSTEM. IF NOT IT CAN CAUSE CONTAMINATION OF THE POTABLE WATER SYSTEM. (1) Make sure that the PWSP access door 164AR is closed. (Ref. Fig. 301/TASK 12-15-38-991-001-A) NOTE : You can set the water quantity only at the FAP 120RH when the ____ PWSP access door 164AR is closed. (2) On the FAP 120RH set the necessary quantity of water. (Ref. Fig. 302/TASK 12-15-38-991-003) (a) Push the WATER hardkey. (b) Make sure that the amber NO WATER PRESELECT AVAIL message is not shown. (c) Push the necessary + and/or - softkeys to set the necessary quantity of water. NOTE : You can set 25%, 50%, 75% and 100%. The keys are only ____ activated, if the PWSP access door 164AR is closed. (3) Connect the potable-water service-vehicle. (Ref. Fig. 301/TASK 12-15-38-991-001-A) (a) Open the PWSP access door 164AR. NOTE : You must not do the filling procedure if the ATTENTION ____ STOP FILLING 38MA light is ON. (b) On the PWSP remove the cap 5252MB from the fill/drain nipple 26DV. (c) Connect the CART - SERVICING, WATER, POTABLE hose to the fill/drain nipple 26DV. (d) On the PWSP turn the control handle 5254MB from the NORMAL to the PULL TO FILL position. Then pull it out to the mechanical stop.
EFF : ALL 12-15-38 R SROS
Page 303 Jul 01/05
R
Potable-Water Service Panel Figure 301/TASK 12-15-38-991-001-A
EFF : ALL 12-15-38 SROS
Page 304 Jul 01/03
FAP Display Figure 302/TASK 12-15-38-991-003 EFF : ALL 12-15-38 R SROS
Page 305 Jul 01/98
(e) Make sure that the control light 3MP comes ON and the control light 38MA is OFF. (4) Fill the Potable Water Tanks CAUTION : DO NOT LET THE WATER PRESSURE BE MORE THAN THE SPECIFIED _______ VALUE. IF THE WATER PRESSURE IS TOO HIGH IT WILL CAUSE DAMAGE TO THE POTABLE WATER SYSTEM. NOTE : Stop immediately the fill procedure of the potable water tanks ____ if the control light ATTENTION STOP FILLING 38MA comes ON at the PWSP. (a) Operate the CART - SERVICING, WATER, POTABLE at a pressure of max. 125 psi (8.6184 bar) and fill the potable water tanks. NOTE : When the set value is reached, the control lights 5MA for ____ the FWD tank system and 15MA for the AFT tank system come ON. When the control light 5MA comes ON, the valve 22MA closes and the control light 3MP goes OFF. When the control light 15MA comes ON at first, the valve 37MA closes and the control light 38MA is not activated. In this case the valve 37MA opens again after the FWD tanks system has reached the set level. After the FWD and AFT tank systems have reached the set value, the valve 9MA closes and the control handle 5254MB turns automatically back to the NORMAL position. NOTE : To stop the fill procedure before the set quantity is ____ reached, you must turn the control handle 5254MB to the NORMAL position. (b) Stop the water flow at the CART - SERVICING, WATER, POTABLE. (5) Make sure that the actual quantity indication on the FAP and at PWSP is the same as the set quantity indication. (Ref. Fig. 301/TASK 12-15-38-991-001-A, 302/TASK 12-15-38-991-003) (6) Disconnect the potable-water service-vehicle. (Ref. Fig. 301/TASK 12-15-38-991-001-A) (a) Disconnect the CART - SERVICING, WATER, POTABLE hose from the fill/drain nipple 26DV at the PWSP. (b) Clean and dry the PWSP and the adjacent area.
EFF : ALL 12-15-38 R SROS
Page 306 Jul 01/05
(c) Visually examine the connections for leaks. NOTE : Leaks are not permitted. ____ (d) Install the cap 5252MB on the fill/drain nipple 26DV. (7) Clean and dry the aft potable-water drain-panel. (Ref. Fig. 303/TASK 12-15-38-991-002) (a) Open the aft potable-water drain-panel access door 154AR. (b) Clean and dry the aft potable-water drain-panel and the adjacent area. (c) Visually examine the connections for leaks. NOTE : Leaks are not permitted. ____ (d) Close the aft potable-water drain-panel access door 154AR. **ON A/C 001-049, Subtask 12-15-38-870-052 B. Bleed the Components (1) Galley Water-Heater NOTE : This procedure is the same for all the faucets of the galley ____ water-heaters. (a) Open the faucet of the galley water-heater. NOTE : This is only possible when the potable-water system is ____ pressurized and the shutoff valve of the galley is open. (b) Put an applicable container below the faucet to collect the water. NOTE : If you use the washbasin make sure that hoses are ____ connected to the drain masts (c) Close the faucet of the galley water-heater.
EFF : ALL 12-15-38 R SROS
Page 307 Jul 01/05
Aft Potable-Water Drain-Panel Figure 303/TASK 12-15-38-991-002 EFF : ALL 12-15-38 R SROS
Page 308 Jul 01/03
**ON A/C ALL 5. Close-up ________ Subtask 12-15-38-410-052 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access door 164AR and make sure that the access door 154AR is closed. (3) Make sure that the latches are correctly locked and that the doors make a continuous surface with the skin of the aircraft. (4) Remove the access platform(s). (5) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-15-38-862-051 B. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
EFF : ALL 12-15-38 R SROS
Page 309 Jul 01/05
TASK 12-15-38-613-802 Fill the Potable Water System (Aircraft Electrical Power not Available) 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No
specific specific specific specific
1 1 1 1
ACCESS PLATFORM 1M (3 FT) CART - SERVICING, WATER, POTABLE CONTAINER 10 L(2 1/2 USGAL) HOSE - DRAIN
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-31-38-660-801 12-33-21-618-801 12-15-38-991-001-A 12-15-38-991-002
Cold Weather Maintenance Practices for Water/Waste Pre-conditioning through the Low-Pressure Ground Connection Fig. 301 Fig. 303
3. __________ Job Set-up Subtask 12-15-38-865-054 A. Make sure that the electrical-power supply system is de-energized: Get access to the applicable 5000VE series panel(s). Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------5005VE WATER SYSTEM QUANT IND 1MA 17 C 5005VE WATER SYSTEM DRAIN 1MP 16 C
EFF : ALL 12-15-38 R SROS
Page 310 Jul 01/05
Subtask 12-15-38-618-051 B. Preparation to Fill the Potable Water System (1) Obey the cold weather maintenance procedure (Ref. TASK 12-31-38-660801). (2) If the temperature in the aircraft is below 4 DEG.C (39.20 DEG.F) do the pre-conditioning procedure (Ref. TASK 12-33-21-618-801). Subtask 12-15-38-010-055 C. Get Access (1) Put the ACCESS PLATFORM 1M (3 FT) in position below the Potable-Water Service Panel (PWSP) at Zone 164. (2) Put the ACCESS PLATFORM 1M (3 FT) in position below the Aft Potable-Water Drain Panel (APWDP) at Zone 154. 4. Procedure _________ Subtask 12-15-38-613-056 A. Fill the Potable Water Tanks WARNING : MAKE SURE THAT THE EQUIPMENT YOU USE FOR THIS PROCEDURE IS _______ CLEAN AND APPROVED FOR THE POTABLE WATER SYSTEM. IF NOT IT CAN CAUSE CONTAMINATION OF THE POTABLE WATER SYSTEM. (1) On the APWDP: (Ref. Fig. 303/TASK 12-15-38-991-002) (a) Open the access door 154AR. (b) Connect a HOSE - DRAIN to the drain (overflow) nipple 5255MB connection on the APWDP. (c) Put a CONTAINER 10 L(2 1/2 USGAL) under the drain hose. (2) On the PWSP: (Ref. Fig. 301/TASK 12-15-38-991-001-A) (a) Open the access door 164AR. (b) Remove the cap assy 5252MB from the fill/drain nipple 26DV .
EFF : ALL 12-15-38 R SROS
Page 311 Jul 01/05
(c) Connect the CART - SERVICING, WATER, POTABLE hose to the fill/drain nipple 26DV. (d) Connect a hose to the overflow nipple 28DV. (3) On the APWDP turn the FILL/DRAIN VALVE control handle to the OPEN position. (4) On the PWSP turn the control handle 5254MB to the PULL TO FILL position. Then pull it out to the mechanical stop. (5) Fill the potable water tanks. CAUTION : DO NOT LET THE WATER PRESSURE BE MORE THAN THE SPECIFIED _______ VALUE. IF THE WATER PRESSURE IS TOO HIGH IT WILL CAUSE DAMAGE TO THE POTABLE WATER SYSTEM. (a) Operate the potable-water service-vehicle at a pressure of 125 psi (8.6184 bar) and fill the potable water tanks. NOTE : When the tanks are full, water will flow from the overflow ____ nipple 28DV at the PWSP and drain (overflow) nipple 5255MB at the APWDP. (6) When water flows from: - the APWDP, turn the FILL/DRAIN VALVE control handle to the SHUT position, - the PWSP, push in the control handle 5254MB and turn it to the NORMAL position. (7) Stop the water flow at the potable-water service-vehicle. (8) On the PWSP: (a) Disconnect the hose from the fill/drain nipple 26DV. (b) Disconnect the overflow nipple 28DV. (c) Turn the control handle 5254MB to the PULL TO DRAIN position. Then pull it out to the mechanical stop. NOTE : Water will flow from the fill/drain nipple 26DV on the ____ PWSP. (d) After approximately 15 seconds, push in the control handle 5254MB and then turn to the NORMAL position.
EFF : ALL 12-15-38 R SROS
Page 312 Jul 01/05
(e) Install the cap assy 5252MB on the fill/drain nipple 26DV. (f) Clean and dry the PWSP and the adjacent area. (g) Visually examine the connections for leaks. NOTE : Leaks are not permitted. ____ (h) Make sure that the work area is clean and clear of tools and other items. (i) Close the PWSP access door 164AR. (9) On the APWDP (a) Disconnect the drain hose. (b) Remove the container. (c) Clean and dry the APWDP and the adjacent area. (d) Visually examine the connections for leaks. NOTE : Leaks are not permitted. ____ (e) Make sure that the work area is clean and clear of tools and other items. (f) Close the APWDP access door 154AR. **ON A/C 001-049, Subtask 12-15-38-870-053 B. Bleed the Components (1) Galley Water-Heater NOTE : This procedure is the same for all the faucets of the galley ____ water heaters. (a) Open the faucet of the galley water-heater. NOTE : This is only possible when the potable-water system is ____ pressurized and the shutoff valve of the galley is open.
EFF : ALL 12-15-38 R SROS
Page 313 Jul 01/05
(b) Put an applicable container below the faucet to collect the water. NOTE : If you use the washbasin make sure that hoses are ____ connected to the drain masts (c) Close the faucet of the galley water-heater. **ON A/C ALL 5. Close-up ________ Subtask 12-15-38-865-055 A. Make sure that the system is energized: Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1MA, 1MP Subtask 12-15-38-410-053 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access doors 164AR and 154AR. (3) Make sure that the latches are correctly locked and that the access doors make a continuous surface with the skin of the aircraft. (4) Remove the access platform(s). (5) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL 12-15-38 R SROS
Page 314 Jul 01/05
TOILET SANITARY FLUID - DESCRIPTION AND OPERATION _________________________________________________ 1. _______ General This topic gives instructions for the servicing of the waste water system.
EFF : ALL 12-16-00 SROS
Page 1 Apr 01/98
LAVATORY ARTICLE - SERVICING ____________________________ TASK 12-16-25-613-801 Servicing of the Liquid Soap Dispenser 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
No specific
weak liquid soap
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 R
Energize the Ground Service Network De-energize the Ground Service Network
**ON A/C 001-049, 201-208, 251-252, 255-299, 401-449, 451-499, 12-16-25-991-001
Fig. 301
**ON A/C 209-249, 301-399, 701-749, 12-16-25-991-001-A
Fig. 301A
EFF : ALL 12-16-25 SROS
Page 301 Jul 01/05
**ON A/C ALL 3. __________ Job Set-up Subtask 12-16-25-861-050 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). 4. Procedure _________ Subtask 12-16-25-613-050 R
A. Servicing of the Soap Dispenser.
R R R R R
CAUTION : DO NOT USE INDUSTRIAL HAND CLEANERS, NATURAL SOAPS AND CLEANING _______ AGENTS THAT CONTAIN ABRASIVES, SOLVENTS OR A LARGE PROPORTION OF DISINFECTANT. THESE MATERIALS CAN CAUSE THE PUMP MECHANISM TO WEAR MORE QUICKLY.
R R R R
NOTE : The dispenser is applicable for normal liquid hand-cleaning ____ agents, soap creams and dish-washing agents for household use. We recommend that you use weak, biodegradable, fully synthetic agents.
R R R R
(1) Fill the Soap Dispenser **ON A/C 001-049, 201-208, 251-252, 255-299, 401-449, 451-499, (Ref. Fig. 301/TASK 12-16-25-991-001) **ON A/C 209-249, 301-399, 701-749, (Ref. Fig. 301A/TASK 12-16-25-991-001-A)
R
EFF : ALL 12-16-25 SROS
Page 302 Jul 01/05
Liquid Soap Dispenser Figure 301/TASK 12-16-25-991-001 R EFF : 001-049, 201-208, 251-252, 255-299, 12-16-25 401-449, 451-499, SROS
Page 303 Jul 01/05
Liquid Soap Dispenser Figure 301A/TASK 12-16-25-991-001-A R EFF : 209-249, 301-399, 701-749, 12-16-25 SROS
Page 304 Oct 01/00
**ON A/C ALL R R R
(a) Turn the cover (2) counterclockwise to release it from the shank (3) (refer to Step 1).
R R R
(b) Carefully lift and remove the cover (2) together with the spout (1) and the tube (4) from the shank (3) (refer to Step 2).
R R R
(c) Fill the soap dispenser with weak liquid soap through the shank (3) (refer to Step 3).
R R R
(d) Carefully put the cover (2) together with the spout (1) and the tube (4) on the shank (3).
R R R
(e) Turn the cover (2) clockwise until it is locked in position on the shank (3).
R
(f) Make sure that the work area is clean and clear of tools and other items. 5. Close-up ________ Subtask 12-16-25-862-050 A. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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TOILET SANITARY FLUID - SERVICING _________________________________ TASK 12-16-38-613-801 Servicing of the Toilet System WARNING : ALWAYS USE RUBBER GLOVES WHEN YOU DO WORK: _______ - ON THE TOILET WASTE SYSTEM, OR - ON PARTS THAT HAVE CONTAMINATION FROM THE WASTE SYSTEM. WHEN YOU COMPLETE THE WORK PROCEDURE, CLEAN YOUR HANDS WITH SOAP AND WATER. THIS WILL PREVENT INFECTION (TOILET WASTE IS DANGEROUS FOR HEALTH). WARNING : DO NOT DO WORK ON THE TOILET WASTE SYSTEM AND THE POTABLE WATER _______ SYSTEM AT THE SAME TIME. THIS WILL PREVENT CONTAMINATION OF THE POTABLE WATER SYSTEM. SUCH CONTAMINATION CAN BE DANGEROUS TO HEALTH. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific No specific
1 ACCESS PLATFORM 2M (6 FT) 4 CART - SERVICING, TOILET
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 14-001A Material No. 19-003
DEODORANT AIRCRAFT TOILET NON FORMALDE- HYDE BASE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
EFF : ALL 12-16-38 SROS
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C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-31-38-660-801 12-33-21-618-801 24-41-00-861-801 24-41-00-862-801 38-31-00-680-801 R
Cold Weather Maintenance Practices for Water/Waste Pre-conditioning through the Low-Pressure Ground Connection Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Draining of the Waste Holding Tanks
**ON A/C 001-049, 201-249, 251-252, 255-299, 12-16-38-991-001
Fig. 301
**ON A/C ALL R
Post SB
38-3040 For A/C 001-049,201-249,251-252,255-299,
12-16-38-991-001-B
Fig. 301A
**ON A/C ALL 3. __________ Job Set-up Subtask 12-16-38-861-050 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). Subtask 12-16-38-680-050 B. If the outside air temperature is as shown in the table drain the waste holding tanks (Ref. TASK 38-31-00-680-801). CAUTION : MAKE SURE THAT THE WATER TEMPERATURE IS NOT HIGHER THAN 60 _______ DEG.C (140.00 DEG.F), IF IT IS HIGHER, IT CAN CAUSE DAMAGE TO THE COMPONENT. Table 1 - Waste-Holding Tank Drain Configuration
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Page 302 Jul 01/05
R R
----------------------------------------------------------------------------I Configuration I I I I---------------------------------------------------I Exposure I Waste tank I I Air I Cabin I Outside air I time I drain I IconditioningItemperatureI temperature I I I I------------I-----------I--------------------------I------------I------------I I I I Between 0 and -15 DEG.C I I Not I I ON I Above I 32 and 5 DEG.F I Any I required I I I 10DEG.C I--------------------------I------------I------------I I I I Below -15 DEG.C I I I I I 50DEG.F I 5 DEG.F I 1 h 15 min I I I------------I-----------I--------------------------I------------I I I I I Between 0 and -7 DEG.C I I I I I I 38 and 19.4 DEG.F I 1 h 30 min I Required I I I I--------------------------I------------I I I OFF I I Between -7 and -15 DEG.C I I I I I I 19.4 and 5 DEG.F I 0 h 45 min I I I I I--------------------------I------------I I I I I Below -15 DEG.C I I I I I I 5 DEG.F I any I I I-----------------------------------------------------------------------------I I If you have drained the waste holding tanks you must put 18l (4.755 USgal) I I of warm disinfectant at 30 DEG.C (86 DEG.F) in each waste holding tank I I 30 minutes before you start the engines. I ----------------------------------------------------------------------------Subtask 12-16-38-010-050 C. Get Access (1) Put an ACCESS PLATFORM 2M (6 FT) in position below the waste service panel. (2) Put the CART - SERVICING, TOILET in position. (3) Open the waste service panel door 171AL. 4. Procedure _________ **ON A/C 001-049, 201-249, 251-252, 255-299, (Ref. Fig. 301/TASK 12-16-38-991-001)
EFF : ALL 12-16-38 SROS
Page 303 Jan 01/07
Waste Service Panel Figure 301/TASK 12-16-38-991-001 R EFF : 001-049, 201-249, 251-252, 255-299, 12-16-38 SROS
Page 304 Jul 01/05
**ON A/C ALL R
Post SB
38-3040 For A/C 001-049,201-249,251-252,255-299,
(Ref. Fig. 301A/TASK 12-16-38-991-001-B) **ON A/C ALL WARNING : YOU MUST ALWAYS WEAR RUBBER GLOVES WHEN YOU DO THIS PROCEDURE TO _______ PREVENT INFECTION. Subtask 12-16-38-680-051 A. Draining of the System (1) Open the cap of the waste drain-line valve and the tank flush connections. (2) Connect the hose adapter and the 4-inch diameter drain hose of the CART - SERVICING, TOILET to the waste-tank drain connection. (3) Push the PUSH TO OPEN lever on the waste drain-line valve to the OPEN position. (4) Put the drain-valve control-lever to the OPEN position and let the waste drain. (5) Touch the drain hose and make sure that the waste has drained completely. Subtask 12-16-38-170-050 B. Flushing of the Waste Holding Tanks CAUTION : MAKE SURE THAT THE WATER TEMPERATURE IS NOT HIGHER THAN 60 _______ DEG.C (140.00 DEG.F), IF IT IS HIGHER, IT CAN CAUSE DAMAGE TO THE COMPONENT. (1) Connect the flush/fill hose (1-inch diameter) of the CART SERVICING, TOILET to a flush connection. (2) Operate the CART - SERVICING, TOILET. (a) Make sure that the water pressure is stable at 2.4 bar (35 psi) and the water flow rate is stable at 38.0 l (10.0 USgal) per minute.
EFF : ALL 12-16-38 SROS
Page 305 Jul 01/05
Waste Service Panel Figure 301A/TASK 12-16-38-991-001-B
R
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Page 306 Oct 01/03
(b) Flush the waste holding tank with 100 l (26.5 USgal) of water. (3) Do this procedure for each waste holding tank. (4) Put the drain-valve control-lever to the CLOSED position. (5) Disconnect the drain hose and the hose adapter. Subtask 12-16-38-618-050 C. Preparation to fill the Waste Holding Tanks with disinfectant (1) Obey the cold weather maintenance procedure (Ref. TASK 12-31-38-660801). (2) If the temperature in the aircraft is below 4 DEG.C (39.20 DEG.F) do the pre-conditioning procedure (Ref. TASK 12-33-21-618-801). Subtask 12-16-38-613-051 D. Disinfection of the Tanks R R R
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL _______ MATERIAL. THIS MATERIAL IS DANGEROUS. CAUTION : MAKE SURE THAT THE WATER TEMPERATURE IS NOT HIGHER THAN 60 _______ DEG.C (140.00 DEG.F), IF IT IS HIGHER, IT CAN CAUSE DAMAGE TO THE COMPONENT.
R (1) Use the CART - SERVICING, TOILET to fill each waste holding tank with 18 l (4.8 USgal) of disinfectant solution. NOTE : The disinfection solution is a 0.25% solution of DISINFECTANTS ____ (Material No. 14-001A) You must obey the instructions of the manufacturer fully for the correct solution, when other disinfection materials are used. NOTE : Some disinfectant will drain from the flush connections when ____ you disconnect the fill hose.
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Page 307 Apr 01/05
(2) Make sure that there are no leaks from the toilet drain connections or the fill/rinse connections. NOTE : Leaks are not permitted. ____ (3) Close the cap of the waste drain-line valve. (4) Turn off the CART - SERVICING, TOILET and disconnect the flush/fill hose. (5) Close the caps of the tank flush connections. (6) Clean and dry the service panel area with a clean cloth MISCELLANEOUS (Material No. 19-003). 5. Close-up ________ Subtask 12-16-38-410-051 A. Close the Access door WARNING : AFTER YOU DO WORK ON THE TOILET WASTE SYSTEM, DO NOT DO _______ SERVICING OF THE POTABLE WATER SYSTEM. THIS WILL PREVENT CONTAMINATION OF THE POTABLE WATER SYSTEM. SUCH CONTAMINATION CAN BE DANGEROUS TO HEALTH. (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access door 171AL. NOTE : Make sure that the latches are correctly locked and that the ____ door makes a continuous surface with the skin of the aircraft. Subtask 12-16-38-862-050 B. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862801). Subtask 12-16-38-942-050 C. Removal of the Ground Support Equipment (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 12-16-38 R SROS
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RAIN REPELLENT - DESCRIPTION AND OPERATION __________________________________________ 1. General _______ This section gives the instructions related to fill the rain repellent can. It includes the topic below: 12-17-30/ P. Block 301 ICE AND RAIN PROTECTION
EFF : ALL 12-17-00 SROS
Page 1 Apr 01/98
ICE AND RAIN PROTECTION - SERVICING ___________________________________ TASK 12-17-30-200-801 Do a Check of Rain Repellent Fluid Can Assy For Correct Fluid Level and Pressure NOTE : If there is leakage of FORALKYL 2211, you can smell a pine odor. ____ 1. __________________ Reason for the Job R R
Self Explanatory 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------30-45-00-600-801 12-17-30-991-001-A
Servicing of the Rain-Repellent Fluid Can (5101DG) Fig. 301
3. __________ Job Set-up **ON A/C 002-049, 203-249, 301-399, 403-449, 451-499, 701-749, Subtask 12-17-30-869-050 A. Not applicable.
EFF : ALL 12-17-30 SROS
Page 301 Jul 01/06
**ON A/C ALL 4. Procedure _________ (Ref. Fig. 301/TASK 12-17-30-991-001-A) R
**ON A/C 001-001, 201-202, 251-252, 255-299, 401-402, Subtask 12-17-30-210-050 A. Inspection/Check of the Pressure Gage and Fluid Level (1) Pressure gage (a) Make sure that the pointer points to the green area (green band). (b) If the pointer points to the yellow area, replace the can (Ref. TASK 30-45-00-600-801). (2) Fluid level indication (a) Make sure that the fluid level indicator does not show the REFILL indication. (b) If you see the REFILL float, replace the can (Ref. TASK 30-45-00600-801). **ON A/C 002-049, 203-249, 301-399, 403-449, 451-499, 701-749, Subtask 12-17-30-210-050-A A. Inspection/Check of the Pressure Gage and Fluid Level (1) Pressure gage (a) Make sure that the pointer points to the green area (green band). (b) If the pointer points to the yellow area, replace the can (Ref. TASK 30-45-00-600-801). (2) Fluid level indication (a) Make sure that there is sufficient rain repellent fluid in the gage assy.
EFF : ALL 12-17-30 SROS
Page 302 Jul 01/05
Rain Repellent Fluid Gage Assy Figure 301/TASK 12-17-30-991-001-A EFF : ALL 12-17-30 R SROS
Page 303 Jan 01/03
(b) If you see the surface of the fluid, replace the can (Ref. TASK 30-45-00-600-801). R
**ON A/C ALL 5. Close-up ________
R
**ON A/C 002-049, 203-249, 301-399, 403-449, 451-499, 701-749, Subtask 12-17-30-869-051 A. Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 12-17-30 SROS
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SCHEDULED SERVICING - DESCRIPTION AND OPERATION _______________________________________________ 1. General _______ This section gives the instructions related to the servicing operations, for which a frequency is specified. It includes 12-21-00/P. 12-22-00/P. 12-24-00/P. 12-28-00/P.
the topics below: Block 301 CLEANING Block 301 LUBRICATION Block 301 DRAINAGE Block 301 USE OF MANUAL (MAGNETIC) FUEL QUANTITY INDICATORS
EFF : ALL 12-20-00 SROS
Page 1 Apr 01/98
CLEANING - DESCRIPTION AND OPERATION ____________________________________ 1. General _______ This section gives the instructions related to the aircraft external and internal cleaning. It includes the topics below: 12-21-11/P. Block 301 EXTERNAL CLEANING 12-21-12/P. Block 301 INTERNAL CLEANING
EFF : ALL 12-21-00 SROS
Page 1 Apr 01/98
EXTERNAL CLEANING - SERVICING _____________________________ TASK 12-21-11-615-802 External Cleaning WARNING : BE VERY CAREFUL IF YOU GO ON WET AIRCRAFT SURFACES. IF YOU SLIP, _______ THERE IS A RISK THAT YOU WILL FALL. WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A _______ FALL CAN KILL OR INJURE YOU. CAUTION : DO NOT USE HIGH-PRESSURE JETS OR VAPOR TO DO THE CLEANING PROCEDURE. _______ THIS TYPE OF EQUIPMENT CAN PUT WATER AND MOISTURE IN PARTS, AND CAN CAUSE DAMAGE TO EQUIPMENT, SPECIALLY TO: - ELECTRICAL EQUIPMENT SUCH AS HARNESSES, PROXIMITY SENSORS AND CONNECTORS (WITH SHORT CIRCUITS OR INCORRECT INDICATIONS AS A RESULT) - EQUIPMENT SUCH AS GEAR BOX SEALS, STEADY BEARINGS, ROTARY ACTUATORS AND UNIVERSAL JOINTS. R R
CAUTION : DURING THE ANTI-ICING/DE-ICING AND WASHING PROCEDURES, MAKE SURE THAT _______ THE HOT WATER OR HOT WATER/FLUID MIXTURES DO NOT CAUSE THE TEMPERATURE OF THE AIRCRAFT SKIN TO INCREASE TO MORE THAN +70⁰C. CAUTION : DO NOT USE A COMPRESSED AIR SUPPLY OF MORE THAN 10 PSI (0.70 BAR) _______ PRESSURE: - IF YOU USE A SPRAY GUN OR - WHEN YOU USE COMPRESSED AIR TO DRY THE CLEANED PARTS. AN IMPACT PRESSURE OF MORE THAN 10 PSI (0.70 BAR) WILL CAUSE DAMAGE TO THE PARTS.
R R R R R R R R R R R R R
WARNING : THERE IS A POSSIBLE HEALTH RISK TO PERSONNEL WHO DO MAINTENANCE TASKS _______ AFTER A BIRD STRIKE. THE SAFETY MEASURES THAT FOLLOW ARE RECOMMENDED: - USE DISPOSABLE GLOVES. - USE A DISPOSABLE COVERALL IF THERE IS A RISK OF BODY CONTACT WITH THE BIRD REMAINS. - DO NOT USE PRESSURIZED AIR OR WATER TO CLEAN THE PARTS WHICH WERE IN CONTACT WITH THE BIRD. - REMOVE THE BIRD REMAINS AND PUT THEM IN A PLASTIC BAG. - DO NOT TOUCH YOUR FACE, EYES, NOSE, ETC. WITH YOUR GLOVES. - REMOVE THE GLOVES AND THE DISPOSABLE COVERALL AND PUT THEM IN THE SAME PLASTIC BAG AS THE REMAINS. SEAL THE BAG. - DISCARD THE BAG AS YOU DO FOR USUAL GARBAGE. - CAREFULLY WASH YOUR HANDS WITH SOAP AND WATER.
EFF : ALL 12-21-11 SROS
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1. __________________ Reason for the Job R
NOTE : This task can contribute to fuel savings. ____
R
This task gives the procedure for: - external cleaning of the A/C, - cleaning of the windows, - cleaning of the landing gears and landing gear bays. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No No No No No
specific specific specific specific specific specific specific specific specific specific specific specific
1 1 6 1 2 1 1 1 1 1 1 1
BOOT - RUBBER BRUSH - BRISTLED, SOFT CHOCK - WHEEL CLEANING EQUIPMENT HEIGHT 17M (55FT) - MOBILE FILM - POLYETHYLENE GLOVES - RUBBER GOGGLES - PROTECTIVE OVERALL WITH HOOD - WATERPROOF SCRAPER - PLASTIC SPRAYING EQUIPMENT - LOW PRESSURE TAPE - ADHESIVE SPONGE
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 05-005
USA MIL-C-16173 GRADE II CORROSION PREVENTIVE (Ref. 20-31-00)
Material No. 05-027 Material No. 10-001 Material No. 11-001
RUST INHIBITOR(FOR CORROSION USE 15-004) (Ref. 20-31-00) USA AMS 1424 DE-ICING FLUID AEA/ISO TYPE I ISO 11075 (Ref. 20-31-00) USA MIL-D-16791 TYPE I DETERGENT (Ref. 20-31-00)
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 11-002 Material No. 11-026 Material No. 19-003
USA MIL-PRF-680 DRY CLEANING SOLVENT (VARSOL/WHITE SPIRIT) (Ref. 20-31-00) GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------09-10-00-584-802 09-10-00-584-808 10-11-00-555-814 12-22-32-600-817 12-22-32-600-819 12-31-12-660-801 12-34-24-860-802 24-41-00-861-801 24-41-00-861-801 24-41-00-862-801 32-11-00-100-801 32-12-00-010-801 32-12-00-410-801
Towing with the Nose Landing Gear from the Front Towing with Towbarless Tractor Aircraft Protection Equipment Lubrication of Main Landing Gear and Doors Lubrication of Nose Gear and Doors De-icing of the Aircraft Parked in an Open Area (Engines Stopped) Aircraft Grounding for the Maintenance Operations Energize the Aircraft Electrical Circuits from the External Power A Energize the Aircraft Electrical Circuits from the APU (APU Started with APU BAT) De-energize the Aircraft Electrical Circuits from the External Power A Cleaning of the Main Landing Gear Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance
R 32-21-00-100-801 32-22-00-010-801 32-22-00-410-801 56-10-00-100-801 56-10-00-100-802 56-21-15-100-801
Cleaning of the Nose Landing Gear Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance Cleaning of the Windshield (3DG1,3DG2). Cleaning of the Sliding (8DG1,8DG2) and the Fixed Windows (7DG1,7DG2). Cleaning of the Outer Surfaces of the Window Panes
EFF : ALL 12-21-11 SROS
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3. __________ Job Set-up Subtask 12-21-11-941-052 A. General (1) Quality of water for aircraft external cleaning (a) We recommend that you use potable water that has these qualities: - pH between 5 to 8.5 - Chloride level less than 100ppm. NOTE : Water that contains a high level of chloride and/or is ____ acidic-alkaline can cause corrosion. Treated water from city drainage can cause a risk of bacteriological contamination. Refer to the local regulations. (2) The persons that do the cleaning must put on BOOT - RUBBER, GLOVES RUBBER, GOGGLES - PROTECTIVE and OVERALL WITH HOOD - WATERPROOF. Subtask 12-21-11-860-052 B. Aircraft Maintenance Configuration (1) Tow the aircraft to the cleaning area (Ref. TASK 09-10-00-584-802) or (Ref. TASK 09-10-00-584-808). (2) Electrically ground the aircraft (Ref. TASK 12-34-24-860-802). (3) Put the CHOCK - WHEEL in position: (a) For the nose landing gear: - in front of and behind the wheels. (b) For the main landing gear: - in front of the FWD wheels and behind the AFT wheels. (4) Make sure that the slats, flaps, spoilers, ailerons and thrust reversers are retracted. (5) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801).
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(6) On the panel 225VU, push the DITCHING pushbutton switch to close: - the outflow valves 313HL and 315HL, - the underfloor extract valve 12HQ, - the overboard extract valve 13HQ. (7) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). (8) Electrically ground the aircraft (Ref. TASK 12-34-24-860-802). (9) Make sure that all landing gear doors, passenger/crew doors, cargo compartment doors, emergency exits, service panels and sliding windows are closed and that the engines are cold. (10) Install aircraft protection equipment (Ref. TASK 10-11-00-555-814). R R R R R R R R R R
WARNING : USE ONLY THE SPECIFIED TOOLS FOR THE PROTECTION OF THE _______ AIRCRAFT. DO NOT APPLY ADHESIVE TAPE ON THE PROBES, DUCTS, SENSORS (STATIC, PITOT, TAT, AOA). THE SPECIFIED TOOLS : - GIVE THE CORRECT PROTECTION TO THE AIRCRAFT EQUIPMENT, - ARE EASY TO SEE FROM THE GROUND. MAKE AN ENTRY IN THE AIRCRAFT LOG BOOK OR ATTACH A TAG ON THE CAPTAIN SIDE STICK TO TELL THE CREW THAT PROTECTION COVERS/DEVICES ARE INSTALLED. (11) Install a FILM - POLYETHYLENE or equivalent, on each landing gear wheel/brake. (12) Put TAPE - ADHESIVE on all remaining joints and openings where the cleaning products could fall and cause damage. Record the locations where you put the TAPE - ADHESIVE. Subtask 12-21-11-941-053 C. Job Set-up WARNING : CLEANING AGENT IS A HAZARDOUS MATERIAL WHICH CAN CAUSE INJURY _______ OR ILLNESS IF IT IS NOT CORRECTLY USED. REFER TO MANUFACTURERS SPECIFIC SAFETY AND HEALTH RECOMMENDATIONS BEFORE YOU USE THIS PRODUCT. CAREFULLY READ THE APPLICABLE MATERIAL SAFETY DATA SHEET AND OBEY ALL SAFETY AND HEALTH PRECAUTIONS. (1) Put CLEANING EQUIPMENT HEIGHT 17M (55FT) - MOBILE in position.
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(2) Prepare the cleaning equipment and the cleaning solution with CLEANING AGENTS (Material No. 11-001). Obey the manufacturer instructions. In very dirty areas, increase the concentration but obey the manufacturer instructions for use. If the temperature is less than or equal to 0 deg.C (32.00 deg.F) , use hot water between 38 deg.C (100.40 deg.F) and 43 deg.C (109.40 deg.F) with ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-001). Obey the manufacturer instructions. 4. Procedure _________ Subtask 12-21-11-615-053 A. Aircraft External Cleaning CAUTION : DO NOT USE A COMPRESSED AIR SUPPLY OF MORE THAN 10 PSI (0.70 _______ BAR) PRESSURE: - IF YOU USE A SPRAY GUN OR - WHEN YOU USE COMPRESSED AIR TO DRY THE CLEANED PARTS. AN IMPACT PRESSURE OF MORE THAN 10 PSI (0.70 BAR) WILL CAUSE DAMAGE TO THE PARTS. CAUTION : DO NOT USE STEAM AT MORE THAN THE SPECIFIED PRESSURE. BE _______ CAREFUL TO HOLD THE SPRAY GUN AT THE SPECIFIED DISTANCE AND ANGLE FROM THE SURFACE. IF YOU DO NOT OBEY THESE PRECAUTIONS, YOU CAN CAUSE DAMAGE TO THE SURFACE. (1) If the temperature is less than or equal to 0 deg.C (32.00 deg.F) do the de-icing of the aircraft (Ref. TASK 12-31-12-660-801). (2) Adjust the SPRAYING EQUIPMENT - LOW PRESSURE: - Adjust water, steam, cleaning solution and the temperature controls to the required settings. - Set the steam pressure to less than 10 psi (0.6894 bar), the steam pressure must not cause damage to materials. - Set the temperature so that the cleaning solution is not more than 50 deg.C (122.00 deg.F). (3) Hold the spray gun approximately 1 m (3.28 ft.) from the surface and inclined at approximately 45 degrees to the surface, never at 90 degrees. Move the spray head over the surface and be careful not to stay at one spot for more than 5 seconds. NOTE : If the weather temperature is hot, clean small areas so that ____ the cleaning solution does not become dry on the external skin.
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(4) Apply the cleaning solution from the bottom to the top of the aircraft (this prevents scratches and runs) in the sequence below: - lower forward fuselage from the leading edge of the wing to the nose of the aircraft. - lower aft fuselage from the wings to the leading edge of the horizontal stabilizer. - upper wing surface between the fuselage and the outboard engine pylon. - upper fuselage from the nose to the horizontal stabilizer. - lower center fuselage, engine nacelles and wing bottom skin. - tail cone, rudder, bottom and top skins of the horizontal stabilizer. NOTE : In the THS apron ____ the front to the If you point the anti-icing fluid compartment.
area, it is important to point the spray from rear. spray in the other direction (rear to front), can go into the rear fuselage non-pressurized
- wing top skin between the outboard engine pylon and the wing tips. (a) If there are signs of asphalt, remove them with a SPONGE lightly soaked with CLEANING AGENTS (Material No. 11-026) or CLEANING AGENTS (Material No. 11-002). (b) To remove mud or other unwanted material (insects,...), make it soft with water, and scrape it off with a SCRAPER - PLASTIC and a SPONGE soaked in water. Be very careful not to scratch the surface. If there are stains on the painted area, do not try to remove them. (5) Flushing of the aircraft CAUTION : MAKE SURE YOU FLUSH THE SURFACE SUFFICIENTLY TO REMOVE ALL _______ THE CLEANING SOLUTION. CLEANING SOLUTION THAT STAYS ON THE AIRCRAFT SURFACE CAN CAUSE CORROSION. (a) Let the cleaning solution have an effect, and after approximately 10 minutes, flush before it becomes dry. (b) Flush with hot water at 65 deg.C (149.00 deg.F) maximum to remove signs of cleaning solution. Do not use steam. (c) When you flush the wing and the horizontal stabilizer, always complete this step with the bottom skin.
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(d) If there is ice after the flushing operation, do the de-icing of the aircraft (Ref. TASK 12-31-12-660-801). (e) In the zones where access is not easy, use clean, dry compressed air that does not contain oil, to remove the remaining moisture. Subtask 12-21-11-615-054 B. Cleaning of the Windows (1) Clean the windshield (Ref. TASK 56-10-00-100-801). (2) Clean the sliding and the fixed windows (Ref. TASK 56-10-00-100-802). (3) Clean the outer surfaces of the window panes (Ref. TASK 56-21-15-100801). R R
Subtask 12-21-11-615-055-B C. Cleaning of the Landing Gear Bays and Landing Gears
R R R
CAUTION : MAKE SURE YOU FLUSH THE SURFACE SUFFICIENTLY TO REMOVE ALL THE _______ CLEANING SOLUTION. CLEANING SOLUTION THAT STAYS ON THE AIRCRAFT SURFACE CAN CAUSE CORROSION.
R R R
(1) Opening of the landing-gear doors: - open the nose landing-gear doors (Ref. TASK 32-22-00-010-801), - open the main landing-gear doors (Ref. TASK 32-12-00-010-801).
R R
(2) Make sure that the opening in the landing-gear bays are correctly closed.
R
(3) Cleaning of the landing-gear bays
R R R
NOTE : As there are many components in the landing-gear bays that can ____ be easily damaged. We recommend that you clean the landing-gear bays only when you do maintenance procedures.
R
(a) Make sure that each landing-gear wheel/brake has protection.
R R R
(b) Apply CLEANING AGENTS (Material No. 11-001) with a SPONGE only on the applicable parts of the landing-gear bays, and in the internal surfaces of the landing-gear doors.
R R R
(c) In the zones where access is not easy, apply CLEANING AGENTS (Material No. 11-001) with a BRUSH - BRISTLED, SOFT, to remove all signs of grease and oil.
EFF : ALL 12-21-11 SROS
Page 308 Jan 01/07
R R
(d) Flush the applicable parts of the landing-gear bays to remove all signs of cleaning solution.
R R
(e) In the zones where access is not easy, use clean, dry compressed air that does not contain oil, to remove the remaining moisture.
R
(4) Cleaning of the landing-gears
R
(a) Cleaning of the Nose Landing-Gear (Ref. TASK 32-21-00-100-801).
R
(b) Cleaning of the Main Landing-Gear (Ref. TASK 32-11-00-100-801). Subtask 12-21-11-916-050 D. Corrosion Prevention (1) Remove SPECIAL MATERIALS (Material No. 05-005): - to all threads of studs on the bridge brackets, the washers and the nuts of the landing-gears. (2) Apply SPECIAL MATERIALS (Material No. 05-027): (a) On the painted surfaces of the landing-gears and the landing-gear bays. NOTE : The painted surfaces must be in the correct condition (no ____ damage, marks, scratches and/or signs of corrosion) before you apply the material. (3) Apply SPECIAL MATERIALS (Material No. 05-005): - to all threads of studs on the bridge brackets, the washers and the nuts of the landing-gears. Subtask 12-21-11-640-051 E. Lubrication (1) Lubricate the main landing gear and doors (Ref. TASK 12-22-32-600817). (2) Lubricate the nose gear and doors (Ref. TASK 12-22-32-600-819).
EFF : ALL 12-21-11 SROS
Page 309 Jan 01/07
Subtask 12-21-11-210-053 F. Visual Inspection (1) Make sure that the paint on the components is in the correct condition and that there are no signs of corrosion. (2) Make sure that the bond is correct and that none of the rubber sealant is missing. (3) Make sure that there is no unwanted material in the holes and threads. (4) Make sure that there is no hydraulic fluid on the hydraulic pipes. 5. Close-up ________ Subtask 12-21-11-860-053 A. Aircraft Maintenance Configuration (1) Remove the aircraft protective equipment (Ref. TASK 10-11-00-555814). (2) Remove all FILM - POLYETHYLENE. (3) Remove all signs of TAPE - ADHESIVE with a MISCELLANEOUS (Material No. 19-003) soaked in CLEANING AGENTS (Material No. 11-002). (4) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (5) On the panel 225 VU, release the DITCHING pushbutton switch to open: - the outflow valves 313HL and 315HL, - the underfloor extract valve 12HQ, - the overboard extract valve 13HQ. (a) Visually make sure that: - the outflow valves 313HL and 315HL are in the open position before you apply air on the aircraft and you start the air conditioning packs, - the avionics compartment ventilation operates correctly.
EFF : ALL 12-21-11 R SROS
Page 310 Jan 01/07
Subtask 12-21-11-410-051 B. Put the aircraft back to its initial configuration (1) Remove the tag from the Captain side stick or write in the log book that the protection covers/devices are not installed. (2) Close the main landing-gear doors (Ref. TASK 32-12-00-410-801). (3) Close the nose landing-gear doors (Ref. TASK 32-22-00-410-801). (4) Remove the ground support and the maintenance equipment, the special and standard tools and all other items. (5) De-energize the aircraft electrical circuit (Ref. TASK 24-41-00-862801).
EFF : ALL 12-21-11 SROS
Page 311 Jan 01/07
INTERNAL CLEANING - SERVICING _____________________________ R
TASK 12-21-12-100-801
R
Cleaning of the Cockpit Display-Units
R
1. __________________ Reason for the Job
R
Self Explanatory
R R
2. ______________________ Job Set-up Information A. Referenced Information
R R R
------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R R R R R
22-82-12-100-801
R
3. __________ Job Set-up
R
Subtask 12-21-12-861-050
R R
24-42-00-861-801 24-42-00-862-801 31-63-22-100-801 12-21-12-991-008
A. Energize the ground service network (Ref. TASK 24-42-00-861-801)
R
4. Procedure _________
R
Subtask 12-21-12-160-050
R R
Cleaning of the Screen of the Multipurpose Control Display Unit (MCDU) (2CA1,2CA2,2CA3) Energize the Ground Service Network De-energize the Ground Service Network Cleaning of the Display Unit (DU) (1WK1,1WK2,2WK1,2WK2,3WK1,3WK2) Fig. 301
A. Cleaning of the Cockpit Display-Units (Ref. Fig. 301/TASK 12-21-12-991-008)
R R
(1) Clean the instrument panel display-units (DU) (Ref. TASK 31-63-22100-801).
R R
(2) Clean the multipurpose control display-unit(s) (MCDU) (Ref. TASK 2282-12-100-801).
EFF : ALL 12-21-12 SROS
Page 301 Apr 01/05
R R
Cockpit Display Units Figure 301/TASK 12-21-12-991-008
EFF : ALL 12-21-12 SROS
Page 302 Apr 01/05
R R
(3) Make sure that the work area is clean and clear of tools and other items.
R
5. Close-up ________
R
Subtask 12-21-12-862-050
R R
A. De-energize the ground service network (Ref. TASK 24-42-00-862-801)
EFF : ALL 12-21-12 SROS
Page 303 Apr 01/05
TASK 12-21-12-100-802 R
Cleaning of the Cockpit Equipment/Furnishings 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R R R
No No No No
specific specific specific specific
vacuum cleaner 1 BRUSH - BRISTLED, FIBER, SOFT 1 BRUSH - BRISTLED, STIFF 1 CAP - PROTECTION
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------No specific Material No. 11-017 R R
Material No. 19-003
warm clean water USA AMS 1550 INTERIOR GENERAL PLASTIC CLEANER (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
EFF : ALL 12-21-12 SROS
Page 304 Apr 01/05
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R
24-42-00-861-801 24-42-00-862-801 25-13-00-100-801 56-10-00-100-801 56-10-00-100-802
Energize the Ground Service Network De-energize the Ground Service Network Cleaning of Foam Plastic (Polyurethane) Parts Cleaning of the Windshield (3DG1,3DG2). Cleaning of the Sliding (8DG1,8DG2) and the Fixed Windows (7DG1,7DG2).
R R
CMM 25-11-XX 12-21-12-991-005
Fig. 302
3. __________ Job Set-up Subtask 12-21-12-861-057 A. Energize the ground service network (Ref. TASK 24-42-00-861-801) 4. Procedure _________ Subtask 12-21-12-160-054 R
A. Cleaning of the Cockpit Equipment/Furnishings (Ref. Fig. 302/TASK 12-21-12-991-005) WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL _______ MATERIALS ONLY WITH A GOOD FLOW OF AIR THROUGH THE WORK AREA. THESE MATERIALS ARE POISONOUS AND FLAMMABLE AND SKIN IRRITANTS. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
R R R R
(1) Clean the inner surface of the cockpit windows: (Ref. TASK 56-10-00-100-801) and (Ref. TASK 56-10-00-100-802).
R R
(2) Clean the foam plastic (polyurethane) parts (Ref. TASK 25-13-00-100801).
EFF : ALL 12-21-12 SROS
Page 305 Apr 01/05
Linings and furnishing - Cockpit Figure 302/TASK 12-21-12-991-005
R
EFF : ALL 12-21-12 SROS
Page 306 Apr 01/05
R R
(3) Clean the overhead panel, the glare shield, the main instrument panel, the lateral consoles and the center pedestal. (a) Put a CAP - PROTECTION on each electrical outlet. (b) Remove the loose dirt from the surfaces with a BRUSH - BRISTLED, FIBER, SOFT and a vacuum cleaner. CAUTION : USE ONLY THE SPECIFIED MATERIALS AND OBEY THE _______ INSTRUCTIONS FROM THE MANUFACTURERS. OTHER MATERIALS CAN CAUSE DAMAGE TO THE SURFACE PROTECTION OF THE COMPONENTS AND THE RELATED AREA. (c) Moisten a clean, lint-free cotton cloth MISCELLANEOUS (Material No. 19-003) with CLEANING AGENTS (Material No. 11-017) and apply it to the surface you will clean.
R R
NOTE : To prevent contamination of the cleaning agent, do not put ____ the cloth into the cleaning agent. (d) Moisten a clean, lint-free cotton cloth MISCELLANEOUS (Material No. 19-003) with warm clean water and lightly rub the surface you will clean. NOTE : Always make the cloth moist, not the part you will clean. ____ (e) Dry the surface with a clean, lint-free cotton cloth MISCELLANEOUS (Material No. 19-003). (4) Clean the Seats (a) Clean the seats as given in the (Ref. CMM 25-11-XX) of the seat manufacturer. (5) Clean the floor (a) Remove the loose dirt with a vacuum cleaner. NOTE : The following work steps are only applicable if ____ non-textile floor covering (NTF) is installed. (b) Apply CLEANING AGENTS (Material No. 11-017) to the surface with a BRUSH - BRISTLED, STIFF.
R R
NOTE : To prevent contamination of the cleaning agent, do not put ____ the brush into the cleaning agent.
EFF : ALL 12-21-12 SROS
Page 307 Jul 01/05
(c) Clean the surface with a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003) and warm clean water. (d) Dry the surface with a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003). (6) Remove the protection caps from the electrical outlets. (7) Make sure that the work area is clean and clear of tools and other items. 5. Close-up ________ Subtask 12-21-12-862-057 A. De-energize the ground service network (Ref. TASK 24-42-00-862-801)
EFF : ALL 12-21-12 R SROS
Page 308 Jul 01/05
TASK 12-21-12-100-803 Cleaning of the Carpets and Non-Textile Floor (NTF) Covering 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No
specific specific specific specific specific
cloth medium fiber brush paper towels stiff fiber brush vacuum cleaner
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------No specific No specific Material No. 11-017 Material No. 11-018
warm clean water warm water USA AMS 1550 INTERIOR GENERAL PLASTIC CLEANER (Ref. 20-31-00) USA AMS 1630 CARPET AND FABRIC CLEANER (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801
Energize the Ground Service Network De-energize the Ground Service Network
EFF : ALL 12-21-12 R SROS
Page 309 Apr 01/05
3. __________ Job Set-up Subtask 12-21-12-861-058 A. Energize the ground service network (Ref. TASK 24-42-00-861-801) 4. Procedure _________ Subtask 12-21-12-160-055 A. Cleaning of the Carpets and NTF Floor Covering WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL _______ MATERIALS ONLY WITH A GOOD FLOW OF AIR THROUGH THE WORK AREA. THESE MATERIALS ARE POISONOUS AND FLAMMABLE AND SKIN IRRITANTS. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. CAUTION : USE ONLY THE SPECIFIED MATERIALS AND OBEY THE INSTRUCTIONS FROM _______ THE MANUFACTURERS. OTHER MATERIALS CAN CAUSE DAMAGE TO THE SURFACE PROTECTION OF THE COMPONENTS AND THE RELATED AREA. (1) Clean the carpets. (a) Stain removal. 1 _
Soak the area of the stain with warm clean water.
2 _
Dry the area of the stain with paper towels.
3 _
Carefully apply CLEANING AGENTS (Material No. 11-018) to the area of the stain with a medium fiber brush.
4 _
Dry the area with paper towels.
5 _
Use a medium fiber brush to lift the carpet pile.
(b) Dirt removal. 1 _
Clean the area with a vacuum cleaner.
2 _
Use a medium fiber brush to lift the carpet pile.
EFF : ALL 12-21-12 R SROS
Page 310 Apr 01/05
(2) Clean the NTF floor covering. (a) Remove the loose dirt from surface with a vacuum cleaner. (b) Apply CLEANING AGENTS (Material No. 11-017) to the surface with a stiff fiber brush. (c) Clean the surface with a cloth and a warm water. (d) Dry the surface with a cloth. 5. Close-up ________ Subtask 12-21-12-862-058 A. De-energize the ground service network (Ref. TASK 24-42-00-862-801)
R EFF : ALL 12-21-12 SROS
Page 311 Apr 01/05
TASK 12-21-12-100-804 Cleaning of the Plastic Surfaces and Mirrors 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R R R
No specific No specific No specific
1 BRUSH - BRISTLED, FIBER, SOFT 1 CAP - PROTECTION 1 CHAMOIS LEATHER
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
No specific No specific Material No. 05-010 Material No. 11-017 Material No. 11-019
R R
Material No. 19-003
sponge warm clean water PLASTIC CLEANER (Ref. 20-31-00) USA AMS 1550 INTERIOR GENERAL PLASTIC CLEANER (Ref. 20-31-00) USA AMS 1535 CABIN WINDOW CLEANER (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
EFF : ALL 12-21-12 SROS
Page 312 Jul 01/06
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R
24-42-00-861-801 24-42-00-862-801 12-21-12-991-003
R
**ON A/C 301-399,
R
12-21-12-991-007
Energize the Ground Service Network De-energize the Ground Service Network Fig. 303
Fig. 304
**ON A/C ALL 3. __________ Job Set-up Subtask 12-21-12-861-059 A. Energize the ground service network (Ref. TASK 24-42-00-861-801) 4. Procedure _________ Subtask 12-21-12-160-056 A. Clean the Plastic Surfaces and Mirrors R R R
(Ref. Fig. 303/TASK 12-21-12-991-003) **ON A/C 301-399,
R
(Ref. Fig. 304/TASK 12-21-12-991-007)
EFF : ALL 12-21-12 SROS
Page 313 Apr 01/05
Component Location/Surface Finish Identification Figure 303/TASK 12-21-12-991-003- 12 (SHEET 1)
R
R EFF : ALL 12-21-12 SROS
Page 314 Apr 01/05
Component Location/Surface Finish Identification Figure 303/TASK 12-21-12-991-003- 22 (SHEET 2)
R
EFF : ALL 12-21-12 SROS
Page 315 Apr 01/05
Linings and furnishing - Lower Deck Cabin Figure 304/TASK 12-21-12-991-007
R
R EFF : 301-399, 12-21-12 SROS
Page 316 Apr 01/05
**ON A/C ALL WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL _______ MATERIALS ONLY WITH A GOOD FLOW OF AIR THROUGH THE WORK AREA. THESE MATERIALS ARE POISONOUS AND FLAMMABLE AND SKIN IRRITANTS. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. CAUTION : USE ONLY THE SPECIFIED MATERIALS AND OBEY THE INSTRUCTIONS FROM _______ THE MANUFACTURERS. OTHER MATERIALS CAN CAUSE DAMAGE TO THE SURFACE PROTECTION OF THE COMPONENTS AND THE RELATED AREA. NOTE : The water and equipment that you use for these procedures must be ____ clean and contain no particles that could damage the surfaces. (1) Cleaning of the plastic surfaces. R
(a) Put CAP - PROTECTION on the electrical outlets so that they do not get wet. (b) Remove the loose dirt from the surface with a BRUSH - BRISTLED, FIBER, SOFT.
R R R
(c) Apply CLEANING AGENTS (Material No. 11-017) to the dirty surface with a lint-free cotton cloth MISCELLANEOUS (Material No. 19003).
R
(d) Clean the surface with a sponge and warm clean water.
R R
(e) Dry the surface with a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003).
R
(f) Remove the protection caps from the electrical outlets. (2) Cleaning of the transparent plastic surfaces.
R
(a) Put CAP - PROTECTION on the electrical outlets so that they do not get wet.
R R R
(b) Clean the surface with a clean lint-free cotton cloth MISCELLANEOUS (Material No. 19-003) and warm clean water.
EFF : ALL 12-21-12 SROS
Page 317 Jul 01/06
R R
(c) Apply CLEANING AGENTS (Material No. 11-017) to the surface with a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003) .
R R
(d) Clean the surface with warm clean water and dry it with a CHAMOIS LEATHER . (e) If there is a stain:
R R R R R R R
- Apply SPECIAL MATERIALS (Material No. 05-010) to the surface with a lint-free cotton cloth MISCELLANEOUS (Material No. 19003). - Clean the surface with warm water and dry it with a chamois leather.
R
(f) Remove the protection caps from the electrical outlets. (3) Cleaning of the mirrors.
R
(a) Clean the surface with a sponge and warm clean water.
R R
(b) Apply CLEANING AGENTS (Material No. 11-019) to the surface with a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003).
R R
(c) Clean the surface with warm clean water and dry it with a CHAMOIS LEATHER. 5. Close-up ________ Subtask 12-21-12-862-059 A. De-energize the ground service network (Ref. TASK 24-42-00-862-801)
EFF : ALL 12-21-12 SROS
Page 318 Jul 01/06
TASK 12-21-12-100-805 Cleaning of the Curtains 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
paper towels
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 11-002 Material No. 11-018
USA MIL-PRF-680 DRY CLEANING SOLVENT (VARSOL/WHITE SPIRIT) (Ref. 20-31-00) USA AMS 1630 CARPET AND FABRIC CLEANER (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801
Energize the Ground Service Network De-energize the Ground Service Network
3. __________ Job Set-up Subtask 12-21-12-861-060 A. Energize the ground service network (Ref. TASK 24-42-00-861-801)
EFF : ALL 12-21-12 R SROS
Page 319 Jan 01/06
4. Procedure _________ Subtask 12-21-12-110-050 A. Cleaning of the Curtains WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL _______ MATERIALS ONLY WITH A GOOD FLOW OF AIR THROUGH THE WORK AREA. THESE MATERIALS ARE POISONOUS AND FLAMMABLE AND SKIN IRRITANTS. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. CAUTION : USE ONLY THE SPECIFIED MATERIALS AND OBEY THE INSTRUCTIONS FROM _______ THE MANUFACTURERS. OTHER MATERIALS CAN CAUSE DAMAGE TO THE SURFACE PROTECTION OF THE COMPONENTS AND THE RELATED AREA. (1) Stain removal. (a) Soak the area of the stain with CLEANING AGENTS (Material No. 11018). 1 _
Dry the wet area with paper towels.
(b) Dry clean. 1 _
Dry clean the area of the stain with a solution of CLEANING AGENTS (Material No. 11-018) and CLEANING AGENTS (Material No. 11-002).
5. Close-up ________ Subtask 12-21-12-862-060 A. De-energize the ground service network (Ref. TASK 24-42-00-862-801)
EFF : ALL 12-21-12 R SROS
Page 320 Jan 01/06
TASK 12-21-12-100-806 Cleaning of Light Alloy and Steel Components 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
cloth masking paper
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------No specific Material No. 11-016
warm clean water USA BOEING BAC 5000 BAC 5504 CLEANING SOLVENT (Ref. 20-31-00)
BAC 5750
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801
Energize the Ground Service Network De-energize the Ground Service Network
3. __________ Job Set-up Subtask 12-21-12-861-061 A. Energize the ground service network (Ref. TASK 24-42-00-861-801)
EFF : ALL 12-21-12 R SROS
Page 321 Jan 01/06
4. Procedure _________ Subtask 12-21-12-160-057 A. Cleaning of Light Alloy and Stainless Steel Components (1) Put masking paper on the electrical outlets so that they do not get wet. (a) Apply CLEANING AGENTS (Material No. 11-016) to the surface with a cloth. (b) Clean the surface with a cloth and warm clean water. (c) Dry the surface with a cloth. (d) Remove the masking paper from the electrical outlets. 5. Close-up ________ Subtask 12-21-12-862-061 A. De-energize the ground service network (Ref. TASK 24-42-00-862-801)
EFF : ALL 12-21-12 R SROS
Page 322 Jan 01/06
TASK 12-21-12-100-807 Cleaning of the Cargo Compartments 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
R
No No No No No No
specific specific specific specific specific specific
blanking caps BRUSH - NON METALLIC CONTAINER 100 L(25 USGAL) HOT AIR BLOWER OPERATING 40 DEG C (100 DEG F) SCRAPER - NON METALLIC VACUUM CLEANER
2 2 2 2 2
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R
No specific No specific Material No. 09-005 Material No. 11-001 Material No. 19-003
clean water Clean water USA MIL-S-81733 CLASS C CORROSION INHIBITIVE INTERFAY SEALANT (Ref. 20-31-00) USA MIL-D-16791 TYPE I DETERGENT (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
EFF : ALL 12-21-12 SROS
Page 323 Jan 01/07
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801
Energize the Ground Service Network De-energize the Ground Service Network
25-51-26-000-801 25-51-26-400-801 25-51-58-000-801
Removal of the Power Drive Units Installation of the Power Drive Units Removal of the Drain System in the FWD Cargo Compartment Removal of the Drain System in the AFT Cargo Compartment Installation of the Drain System in the FWD Cargo Compartment Installation of the Drain System in the AFT Cargo Compartment Visual Check of Drain Outlets for Evidence of Drainage System Obstruction and Clean as Necessary. Visual Check of Drain Outlets for Evidence of Drainage System Obstruction and Clean as Necessary. Aircraft Cleaning after a Fish Shipment Opening of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Removal of the Safety Support Equipment Closing of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Installation of the Safety Support Equipment
R
25-51-58-000-802 25-51-58-400-801 25-51-58-400-802 R R R R
25-52-00-210-802 25-53-00-210-804 51-78-00-615-803 52-30-00-010-801 52-30-00-080-801 52-30-00-410-801 52-30-00-480-801 3. __________ Job Set-up Subtask 12-21-12-861-063
A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-21-12-010-054 B. Get Access (1) If necessary, open the FWD and/or AFT cargo-compartment door (Ref. TASK 52-30-00-010-801). (2) Safety the cargo compartment door(s) (Ref. TASK 52-30-00-480-801).
EFF : ALL 12-21-12 SROS
Page 324 Jan 01/07
Subtask 12-21-12-865-057 C. Get access to the applicable 5000VE series panel(s). Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 14MY 5002VE FWD CARGO LOADING POWER RH1 5MY A13 5002VE FWD CARGO LOADING POWER LH1 3MY A10 5002VE FWD CARGO LOADING POWER RH2 4MY B13 5002VE FWD CARGO LOADING POWER LH2 2MY B10 5002VE FWD CARGO LOADING CTL 1MY C13 FOR 114MY **ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, 701-749, 5006VE 5006VE 5006VE 5006VE
AFT AFT AFT AFT
CLS / RH1-PWR CLS/LH1-POWER CLS / RH2-PWR CLS/LH2-POWER
105MY 103MY 104MY 102MY
A13 A10 B13 B10
101MY
C13
105MY 103MY 104MY 102MY
A13 A10 B13 B10
**ON A/C ALL 5006VE AFT CARGO LOADING CTL **ON A/C 301-399, 5006VE 5006VE 5006VE 5006VE
AFT AFT AFT AFT
CARGO CARGO CARGO CARGO
LOADING LOADING LOADING LOADING
POWER POWER POWER POWER
RH1 LH1 RH2 LH2
EFF : ALL 12-21-12 R SROS
Page 325 Jan 01/06
**ON A/C ALL 4. Procedure _________ Subtask 12-21-12-160-059 A. Dry Cleaning of the Cargo Compartment(s) WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL _______ MATERIALS ONLY WITH A GOOD FLOW OF AIR THROUGH THE WORK AREA. THESE MATERIALS ARE POISONOUS AND FLAMMABLE AND SKIN IRRITANTS. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. R
(1) Remove loose materials with a SCRAPER - NON METALLIC or a BRUSH - NON METALLIC and a VACUUM CLEANER.
R R
(2) Clean the area with CLEANING AGENTS (Material No. 11-001) and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003).
R
(3) Additional Special Cleaning after Seafood/Wet Cargo Shipment: NOTE : This procedure is only applicable if leakage from a shipping ____ container has been reported.
R R
(a) Make a cleaning solution of 0.5 % CLEANING AGENTS (Material No. 11-001) and Clean water: - Mix 5.0 g (0.17 oz) of CLEANING AGENTS (Material No. 11-001) with every 1 l (0.2641 USgal) of water. (b) Clean the area with the cleaning solution and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003). (c) Dry the area with a HOT AIR BLOWER OPERATING 40 DEG C (100 DEG F) .
R R
(4) If necessary clean the bilge area (Ref. TASK 51-78-00-615-803).
EFF : ALL 12-21-12 SROS
Page 326 Jan 01/07
Subtask 12-21-12-160-065 B. Wet Cleaning of the Cargo Compartment(s) WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL _______ MATERIALS ONLY WITH A GOOD FLOW OF AIR THROUGH THE WORK AREA. THESE MATERIALS ARE POISONOUS AND FLAMMABLE AND SKIN IRRITANTS. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. (1) Remove loose materials with a SCRAPER - NON METALLIC or a BRUSH - NON METALLIC and a VACUUM CLEANER.
R
(2) Remove the Power Drive Units (PDUs) (Ref. TASK 25-51-26-000-801). (3) Put blanking caps on the disconnected electrical connectors. (4) Apply SEALANT SEALANTS (Material No. 09-005) on all the mounting holes of the PDUs bonding points. R R R R R
(5) Do a check and clean as necessary the drain filters of the cargo loading system (CLS): - Forward cargo compartment (Ref. TASK 25-52-00-210-802), - Aft cargo compartment (Ref. TASK 25-53-00-210-804).
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(6) Put a CONTAINER 100 L(25 USGAL) below the drain mast(s). (7) Clean the cargo compartment(s) as follows: CAUTION : MAKE SURE THAT YOU DO NOT PUT WATER DIRECTLY ON THE BALL _______ MATS AND THE FLOOR PANEL AREAS THAT HAVE POWER DRIVE UNITS. WATER ON THESE AREAS CAN CAUSE CORROSION AND ELECTRICAL MALFUNCTIONS IN THE CLS.
R R R R R R R R
(a) Flush hot max 60.0 deg.C (140.00 deg.F) clean water (or a cleaning solution of 0.5 % CLEANING AGENTS (Material No. 11-001) and water) with a maximum flow rate of 5 l/min: - On the floor panel area at the aft end of the forward compartment, - On the ball mat area of the aft compartment, - On the rigid corner sheets and the lower sidewall panels.
EFF : ALL 12-21-12 SROS
Page 327 Jan 01/07
R (b) Brush the floor panels to apply water flow to the roller track outer flanges. (c) Make sure that water flows freely through the drain masts. (8) Replace Drain System filters (Ref. TASK 25-51-58-000-801), (Ref. TASK 25-51-58-400-801), (Ref. TASK 25-51-58-000-802) and (Ref. TASK 25-5158-400-802), as necessary. R R
(9) Dry the compartment floor and the CLS with a HOT AIR BLOWER OPERATING 40 DEG C (100 DEG F) . (10) Install the PDUs (Ref. TASK 25-51-26-400-801). 5. Close-up ________ Subtask 12-21-12-865-058 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 14MY 1MY, 2MY, 3MY, 4MY, 5MY. FOR 114MY 101MY, 102MY, 103MY, 104MY, 105MY. Subtask 12-21-12-410-054 B. Close Access (1) Remove the safety support equipment from the cargo compartment doors (Ref. TASK 52-30-00-080-801). (2) Remove the access platform(s). (3) Close the cargo compartment door(s) (Ref. TASK 52-30-00-410-801). Subtask 12-21-12-862-063 C. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-21-12 SROS
Page 328 Jan 01/07
TASK 12-21-12-100-808 Cleaning of the Monitors and Display Screens in the Cabin 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
absorbent surgical cotton wadding sterile gauze pad
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 11-020 VISUAL DISPLAY UNIT ANTI-STATIC CLEANER (Ref. 20-31-00) C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801
Energize the Ground Service Network De-energize the Ground Service Network
3. __________ Job Set-up Subtask 12-21-12-861-062 A. Energize the ground service network (Ref. TASK 24-42-00-861-801).
EFF : ALL 12-21-12 R SROS
Page 329 Jan 01/06
4. Procedure _________ Subtask 12-21-12-160-058 A. Cleaning of the Monitors and Display Screens CAUTION : USE ONLY THE SPECIFIED MATERIALS AND OBEY THE INSTRUCTIONS FROM _______ THE MANUFACTURERS. OTHER MATERIALS CAN CAUSE DAMAGE TO THE SURFACE PROTECTION OF THE COMPONENTS AND THE RELATED AREA. (1) Get a absorbent surgical cotton wadding or a sterile gauze pad moist with CLEANING AGENTS (Material No. 11-020). Lightly rub one time the surface. (2) Get a new piece of wadding or gauze soaked with the anti-static cleaner. Rub the surface of the screen again and remove all the marks. NOTE : Use a new piece of wadding (or gauze) each time, because dust ____ on the wadding (or gauze) can cause scratches on the screen. Dry the screen with a clean wadding (or gauze). Rub the screen one time only with each new piece of wadding (or gauze). NOTE : Always make the pad moist, not the screen. ____ Rub the screen lightly. We recommend you mist the surface of the screen before you rub it with the wadding (or gauze). This prevents scratches. The more frequently you replace the wadding (or gauze) the faster and better is the cleaning. 5. Close-up ________ Subtask 12-21-12-862-062 A. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-21-12 R SROS
Page 330 Jan 01/06
TASK 12-21-12-100-809 Cleaning of the Plastic Wash Basin in the Lavatories 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 BRUSH - BRISTLED, FIBER, SOFT
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific No specific Material No. 05-008 Material No. 05-009 Material No. 19-003
abrasive general household cleaning agent mild soap solution sponge warm, clean water PLASTIC POLISHING COMPOUND (COARSE GRADE) (Ref. 20-31-00) USA PP-560 TYPE 1 PLASTIC POLISHING COMPOUND (FINE GRADE) (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 25-00-00-340-808 12-21-12-991-004
Energize the Ground Service Network De-energize the Ground Service Network Repair of the Lavatory Plastic Wash-Basin Fig. 305
EFF : ALL 12-21-12 R SROS
Page 331 Jan 01/06
3. __________ Job Set-up Subtask 12-21-12-861-064 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). 4. Procedure _________ Subtask 12-21-12-160-060 A. General Cleaning (Ref. Fig. 305/TASK 12-21-12-991-004) NOTE : The water and equipment that you use for these procedures must be ____ clean and contain no particles that could damage the surfaces. (1) Remove the loose dirt from the surface with a BRUSH - BRISTLED, FIBER, SOFT. (2) Apply a mild soap solution to the dirty surface with a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003). NOTE : If necessary, use more soap for a stronger solution. ____ (3) Rinse the surface with a sponge and warm, clean water. (4) Wipe the surface dry with a soft lint-free cotton cloth MISCELLANEOUS (Material No. 19-003) NOTE : Make sure that there is no abrasive material on the surface. ____ Abrasive materials can damage the surface. (5) If necessary, do Para. B. steps (1) thru (3). Subtask 12-21-12-160-061 B. Special Cleaning CAUTION : USE ONLY THE SPECIFIED MATERIALS AND OBEY THE INSTRUCTIONS FROM _______ THE MANUFACTURERS. OTHER MATERIALS CAN CAUSE DAMAGE TO THE SURFACE PROTECTION OF THE COMPONENTS AND THE RELATED AREA. NOTE : Removal of the Stain(s) made with: ____ - cigarette burns, - a felt pen, - a lipstick,
EFF : ALL 12-21-12 R SROS
Page 332 Jan 01/06
Linings and furnishing - Lavatory Figure 305/TASK 12-21-12-991-004 EFF : ALL 12-21-12 R SROS
Page 333 Jan 01/06
-
hair dye, hairspray, mascara, nail varnish, shoe polish.
(1) Apply an abrasive general household cleaning agent to the area of the stain(s) and wipe it with a moist cloth. NOTE : Do step (2) again, if necessary. ____ (2) Rinse the surface with a sponge and warm, clean water. (3) Wipe the surface dry with a soft lint-free cotton cloth MISCELLANEOUS (Material No. 19-003). NOTE : Make sure that there is no abrasive material on the surface. ____ Abrasive materials can damage the surface. (a) If necessary, do Para. C. steps (1) thru (3). Subtask 12-21-12-160-062 C. Intensive Cleaning (Polishing) CAUTION : USE ONLY THE SPECIFIED MATERIALS AND OBEY THE INSTRUCTIONS FROM _______ THE MANUFACTURERS. OTHER MATERIALS CAN CAUSE DAMAGE TO THE SURFACE PROTECTION OF THE COMPONENTS AND THE RELATED AREA. NOTE : Removal of the Stain(s) made with: ____ - cigarette burns, - a felt pen, - a lipstick, - hair dye, - hairspray, - mascara, - nail varnish, - shoe polish. (1) Apply SPECIAL MATERIALS (Material No. 05-008) to the area of the stain(s) and wipe it with a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003). (2) Apply SPECIAL MATERIALS (Material No. 05-009) to the area of the stain(s) and wipe it with a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003).
EFF : ALL 12-21-12 R SROS
Page 334 Jan 01/06
(3) Polish the surface with a soft lint-free cotton cloth MISCELLANEOUS (Material No. 19-003). NOTE : Make sure that there is no abrasive material on the surface. ____ Abrasive materials can damage the surface. Subtask 12-21-12-160-063 D. Removal of Scratches (1) Repair the surfaces that have scratches (Ref. TASK 25-00-00-340-808). 5. Close-up ________ Subtask 12-21-12-862-064 A. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-21-12 R SROS
Page 335 Jan 01/06
TASK 12-21-12-100-810 Cleaning of the Seat Covers 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
paper towel vacuum cleaner
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 11-002 Material No. 11-018
USA MIL-PRF-680 DRY CLEANING SOLVENT (VARSOL/WHITE SPIRIT) (Ref. 20-31-00) USA AMS 1630 CARPET AND FABRIC CLEANER (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 24-41-00-862-801
Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A
EFF : ALL 12-21-12 R SROS
Page 336 Apr 01/05
3. __________ Job Set-up Subtask 12-21-12-861-065 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). 4. Procedure _________ Subtask 12-21-12-110-051 A. Cleaning (1) Remove the loose dirt from the seats with a vacuum cleaner. (2) Removal of the Stains WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL _______ MATERIALS ONLY WITH A GOOD FLOW OF AIR THROUGH THE WORK AREA. THESE MATERIALS ARE POISONOUS AND FLAMMABLE AND SKIN IRRITANTS. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. WARNING : DO NOT GET THE COMPOUND ON YOUR SKIN. _______ IF YOU DO: - REMOVE IT IMMEDIATELY WITH A CLEAN CLOTH - WASH YOUR SKIN WITH SOAP AND RINSE WITH CLEAN WATER. CAUTION : USE ONLY THE SPECIFIED MATERIALS AND OBEY THE INSTRUCTIONS _______ FROM THE MANUFACTURERS. OTHER MATERIALS CAN CAUSE DAMAGE TO THE SURFACE PROTECTION OF THE COMPONENTS AND THE RELATED AREA. (a) Soak the area of the stain with CLEANING AGENTS (Material No. 11018). (b) Dry the wet area with a paper towel.
EFF : ALL 12-21-12 R SROS
Page 337 Apr 01/05
(3) Dry Clean (a) Dry clean the area of the stain with CLEANING AGENTS (Material No. 11-018) and CLEANING AGENTS (Material No. 11-002). (b) Dry the wet area with a paper towel. (4) Refer to the vendor documentation if necessary. 5. Close-up ________ Subtask 12-21-12-862-065 A. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
EFF : ALL 12-21-12 R SROS
Page 338 Apr 01/05
TASK 12-21-12-100-811 Cleaning of the Air Inlet Grids of Galleys and Lavatories 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------No specific No specific Material No. 11-017 Material No. 19-003
clean warm water sponge USA AMS 1550 INTERIOR GENERAL PLASTIC CLEANER (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------21-23-00-600-801 24-42-00-861-801 24-42-00-862-801 25-30-00-920-802 25-35-19-000-801 25-35-19-400-801
Replacement of the Lavatory Air-Extraction Filter Energize the Ground Service Network De-energize the Ground Service Network Discard the Galley Air-Extraction Filter-Element Removal of the Oven Installation of the Oven
3. __________ Job Set-up Subtask 12-21-12-861-067 A. Energize the ground service network (Ref. TASK 24-42-00-861-801)
EFF : ALL 12-21-12 R SROS
Page 339 Apr 01/05
4. Procedure _________ WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL MATERIALS _______ ONLY WITH A GOOD FLOW OF AIR THROUGH THE WORK AREA. THESE MATERIALS ARE POISONOUS AND FLAMMABLE AND SKIN IRRITANTS. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. CAUTION : USE ONLY THE SPECIFIED MATERIALS AND OBEY THE INSTRUCTIONS FROM _______ THE MANUFACTURERS. OTHER MATERIALS CAN CAUSE DAMAGE TO THE SURFACE PROTECTION OF THE COMPONENTS AND THE RELATED AREA. Subtask 12-21-12-160-066 A. Cleaning of the Ventilation Grids in the Galleys that have Ovens Installed. (1) Remove the oven(s) if necessary (Ref. TASK 25-35-19-000-801). (2) Apply CLEANING AGENTS (Material No. 11-017) to the grids. (3) Clean the grids with a sponge and clean warm water and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003). (4) Do a visual inspection of the component interface and/or the adjacent area. (5) If necessary replace the air filter pads (Ref. TASK 25-30-00-920802). (6) Install the oven(s) if removed (Ref. TASK 25-35-19-400-801). Subtask 12-21-12-160-067 B. Cleaning of the Ventilation Grids in the Lavatories (1) Apply CLEANING AGENTS (Material No. 11-017) to the grids. (2) Clean the grids with a sponge and clean warm water and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003). (3) Do a visual inspection of the component interface and/or the adjacent area.
EFF : ALL 12-21-12 R SROS
Page 340 Apr 01/05
(4) If necessary replace the air filter pads (Ref. TASK 21-23-00-600801). 5. Close-up ________ Subtask 12-21-12-862-067 A. De-energize the ground service network (Ref. TASK 24-42-00-862-801)
EFF : ALL 12-21-12 R SROS
Page 341 Apr 01/05
TASK 12-21-12-670-801 Disinfection of the Aircraft Equipment and Furnishing WARNING : ONLY PERSONS NECESSARY FOR THIS PROCEDURE ARE PERMITTED IN THE _______ AIRCRAFT DURING THE TASK. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific No specific
1 GUN - SPRAY 1 WARNING NOTICE
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------No specific Material No. 14-006B Material No. 19-003
clean water USA AMS 1452 DISINFECTANT LIQUID AIRCRAFT GENERAL PURPOSE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 52-30-00-010-801 52-30-00-410-801
Energize the Ground Service Network De-energize the Ground Service Network Opening of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Closing of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump
EFF : ALL 12-21-12 SROS
Page 342 Jan 01/06
3. __________ Job Set-up Subtask 12-21-12-861-051 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-21-12-010-051 B. Get Access (1) Get access to the cabin. (2) Open the FWD and AFT cargo-compartment doors (Ref. TASK 52-30-00-010801). (3) In the cockpit: - Open the floor panel (access hatch) 211FF. (4) Put the WARNING NOTICE in position to tell your personnel about the aircraft disinfection. **ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, Subtask 12-21-12-865-051 C. Get access to the avionics compartment and to the applicable 5000VE-series panel(s). Then open, safety and tag this (these) circuit breaker(s) : ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------715VU GALLEY AFT 12MC A54 715VU GALLEY FWD MID 23MC P56 **ON A/C 210-249, 715VU GALLEY FWD MID AFT 715VU GALLEY FWD MID AFT
112MC 223MC
C55 P57
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EFF : ALL 12-21-12 SROS
Page 343 Jul 01/06
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------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------**ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, 717VU GALLEY FWD MID
11MC
B51
717VU GALLEY FWD MID
111MC
C51
24MC
B60
223MC
P57
1MC 2MC
T10 S39 F06 F05 F04 F03 F02 F01 C07 C06 D16 D15
R R 718VU GALLEY AFT **ON A/C 001-049, 201-209, 251-252, 255-299, 401-449, 451-499, 718VU GALLEY FWD MID AFT **ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, 721VU GALLEY SYS 1 722VU GALLEY SYS 2 R R R R R R R R
5001VE 5001VE 5001VE 5001VE 5001VE 5001VE
RAZOR SOCKET RAZOR SOCKET VACUUM CLEANER VACUUM CLEANER VACUUM CLEANER VACUUM CLEANER
Z241 Z222 Z242 Z221
3MT 1MT 3ME 2ME 4ME 1ME
5005VE 5005VE 5005VE 5005VE
RAZOR SOCKET RAZOR SOCKET VACUUM CLEANER SOCKET Z272 VACUUM CLEANER SOCKET Z271
7MT 5MT 6ME 5ME
SOCKET SOCKET SOCKET SOCKET
EFF : 001-049, 201-249, 251-252, 255-299, 12-21-12 401-449, 451-499, SROS
Page 344 Jul 01/06
**ON A/C ALL 4. Procedure _________ WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL MATERIALS _______ ONLY WITH A GOOD FLOW OF AIR THROUGH THE WORK AREA. THESE MATERIALS ARE POISONOUS AND FLAMMABLE AND SKIN IRRITANTS. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL _______ MATERIAL. THIS MATERIAL IS DANGEROUS. R R
WARNING : DO NOT LET DISINFECTANTS GO ONTO FOODSTUFFS. DISINFECTANTS ARE _______ POISONOUS. DO NOT APPLY THEM AS A SPRAY DIRECTLY TO CARPETS OR COCKPIT INSTRUMENT PANELS. DISINFECTANTS CAN CAUSE DAMAGE TO FURNISHINGS AND EQUIPMENT. Subtask 12-21-12-615-050 A. Disinfection of the Aircraft Equipment and Furnishings (1) Cockpit Equipment and Furnishings: NOTE : Do NOT spray the disinfectant directly on cockpit panels. ____ (a) Carefully apply DISINFECTANTS (Material No. 14-006B) to all surfaces of the cockpit equipment and furnishings with a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003). (b) Clean and dry the cockpit equipment and furnishings with and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003). (2) Galleys: (a) Apply DISINFECTANTS (Material No. 14-006B) to the galleys and galley equipment with a GUN - SPRAY. (b) Clean and dry the galleys and the galley equipment with clean water and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003).
EFF : ALL 12-21-12 SROS
Page 345 Jan 01/07
(3) Lavatories: (a) Apply DISINFECTANTS (Material No. 14-006B) to all toilet seats and the lavatory equipment with a GUN - SPRAY. (b) Clean and dry the toilet seats and the lavatory equipment with clean water and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003). (4) Passenger Seating and Crew Rest Areas: (a) Apply DISINFECTANTS (Material No. 14-006B) to the cabin seats and the cabin equipment with a GUN - SPRAY. (b) Clean and dry the cabin equipment with clean water and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003). (5) Cargo Compartments: (a) Apply DISINFECTANTS (Material No. 14-006B) to the cargo compartments with a GUN - SPRAY. (b) Clean and dry the cargo compartments with clean water and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003). 5. Close-up ________ **ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, Subtask 12-21-12-865-052 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1MT, 3MT, 5MT, 7MT, 1ME, 2ME, 3ME, 4ME, 5ME, 6ME, 1MC, 11MC, 111MC, 2MC, 12MC, 112MC, 23MC, 223MC, 24MC
EFF : ALL 12-21-12 R SROS
Page 346 Jul 01/06
R
**ON A/C ALL Subtask 12-21-12-410-051 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the FWD and AFT cargo-compartment doors (Ref. TASK 52-30-00410-801). (3) Close the access hatch 211FF. (4) Remove the warning notice(s).
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(5) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-21-12-862-051 C. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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EFF : ALL 12-21-12 SROS
Page 347 Jan 01/06
TASK 12-21-12-670-802 Fumigation of the Aircraft Equipment and Furnishing WARNING : ONLY PERSONS NECESSARY FOR THIS PROCEDURE ARE PERMITTED IN THE _______ AIRCRAFT DURING THE TASK. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific
1 WARNING NOTICE
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 14-004 Material No. 19-003
INSECTICIDE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
12-21-12-100-801 12-21-12-100-802 12-21-12-100-804 12-21-12-100-806 12-21-12-100-808 12-33-21-618-801 24-42-00-861-801
Cleaning of the Cockpit Display-Units Cleaning of the Cockpit Equipment/Furnishings Cleaning of the Plastic Surfaces and Mirrors Cleaning of Light Alloy and Steel Components Cleaning of the Monitors and Display Screens in the Cabin Pre-conditioning through the Low-Pressure Ground Connection Energize the Ground Service Network
EFF : ALL 12-21-12 SROS
Page 348 Jan 01/06
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-862-801 52-10-00-010-801 52-10-00-410-801 52-30-00-010-801 52-30-00-410-801
De-energize the Ground Service Network Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door Opening of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Closing of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump
3. __________ Job Set-up Subtask 12-21-12-861-052 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). R R
Subtask 12-21-12-010-052-A B. Get Access
R
(1) Get access to the cabin through one of the passenger/crew doors.
R
NOTE : All other passenger/crew doors must be closed. ____
R R
(2) Open the forward and aft cargo-compartment doors (Ref. TASK 52-30-00010-801).
R R
(3) In the cockpit: - Open the floor panel (access hatch) 211FF.
R R
(4) If necessary remove the cushions and backrests of the cabin seats, the cockpit seats and the cabin attendants seats.
R R R
NOTE : We recommend that you remove all of the cushions and ____ backrests. The insecticide soaks into these materials and extends the ventilation time after fumigation.
R
(5) Open all of the stowages, the lavatory doors and the cockpit door.
R
(6) Remove the contents of the compartments of the galleys.
R
(7) Remove the galley equipment.
EFF : ALL 12-21-12 SROS
Page 349 Jan 01/06
R R
(8) Put the WARNING NOTICE in position to tell your personnel about the aircraft fumigation.
R R R R R R R R R R R R R R R R R R R
NOTE : Fumigation is required for these compartment volumes: ____ -----------------------------------------------------------------------------| | Aircraft Model | | Compartment |-----------------------------------------------------------| | A330/A340-200 | A330/A340-300| A340-500 | A340-600 | -----------------------------------------------------------------------------| Cockpit | 12 m3 | 12 m3 | 12 m3 | 12 m3 | | | (424 ft.3) | (424 ft.3) | (424 ft.3) | (424 ft.3) | -----------------------------------------------------------------------------| Cabin | 317 m3 | 346 m3 | 370 m3 | 420 m3 | | (SEE NOTE) | (11195 ft.3) | (12219 ft.3) | (13066 ft.3) | (14832 ft.3)| -----------------------------------------------------------------------------| Forward Cargo | 92 m3 | 107 m3 | 110.7 m3 | 144 m3 | | | (3249 ft.3) | (3779 ft.3) | (3909 ft.3) | (5085 ft.3) | -----------------------------------------------------------------------------| Aft and Bulk | 94 m3 | 108,4 m3 | 124 m3 | 129 m3 | | Cargo (basic, | (3320 ft.3) | (3828 ft.3) | (3850 ft.3 ) | (4414 ft.3) | | no options) | | | | | ------------------------------------------------------------------------------
R R R
NOTE : Cabin volumes are calculated with the compartment furnishings ____ installed. 109 m3 (3849.299 ft.3)
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, Subtask 12-21-12-865-053
R R R
C. Get access to the avionics compartment and to the applicable 5000VE-series panel(s). Then open, safety and tag this (these) circuit breaker(s) : ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION -------------------------------------------------------------------------------
R 715VU GALLEY AFT 715VU GALLEY FWD MID R
12MC 23MC
A54 P56
112MC
C55
**ON A/C 210-249, 715VU GALLEY FWD MID AFT
EFF : ALL 12-21-12 SROS
Page 350 Jan 01/06
------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------715VU GALLEY FWD MID AFT 223MC P57 R R
**ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, 717VU GALLEY FWD MID
11MC
B51
717VU GALLEY FWD MID
111MC
C51
24MC
B60
223MC
P57
1MC 2MC
T10 S39 F06 F05 F04 F03 F02 F01 C07 C06 D16 D15
R R 718VU GALLEY AFT **ON A/C 001-049, 201-209, 251-252, 255-299, 401-449, 451-499, 718VU GALLEY FWD MID AFT **ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, 721VU GALLEY SYS 1 722VU GALLEY SYS 2 R R R R R R R R
5001VE 5001VE 5001VE 5001VE 5001VE 5001VE
RAZOR SOCKET RAZOR SOCKET VACUUM CLEANER VACUUM CLEANER VACUUM CLEANER VACUUM CLEANER
Z241 Z222 Z242 Z221
3MT 1MT 3ME 2ME 4ME 1ME
5005VE 5005VE 5005VE 5005VE
RAZOR SOCKET RAZOR SOCKET VACUUM CLEANER SOCKET Z272 VACUUM CLEANER SOCKET Z271
7MT 5MT 6ME 5ME
SOCKET SOCKET SOCKET SOCKET
EFF : 001-049, 201-249, 251-252, 255-299, 12-21-12 401-449, 451-499, SROS
Page 351 Jul 01/06
**ON A/C 301-399, 701-749, Subtask 12-21-12-865-062 D. Get access to the avionics compartment and to the applicable 5000VE-series panel(s). Then open, safety and tag this (these) circuit breaker(s) : ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------R 710VU GALLEY FWD MID AFT
223MC
P57
715VU GALLEY FWD MID AFT
112MC
C55
12MC 11MC 111MC 23MC 24MC 1MC 2MC 3ME 2ME 4ME 1LQ 1ME 6ME 5ME
A54 B51 C51 P56 B60 T10 S39 F04 F03 F02 F01 F01 D16 D15
11LQ
D08
11LQ
D08
R R
R R R R R R R
717VU 717VU 717VU 717VU 718VU 721VU 722VU 5001VE 5001VE 5001VE 5001VE 5001VE 5005VE 5005VE
GALLEY AFT GALLEY FWD MID GALLEY FWD MID GALLEY FWD MID GALLEY AFT GALLEY SYS 1 GALLEY SYS 2 VACUUM CLEANER SOCKET Z241 VACUUM CLEANER SOCKET Z222 VACUUM CLEANER SOCKET Z242 LAV FWD&MID DOOR 2 LIGHT VACUUM CLEANER SOCKET Z221 VACUUM CLEANER SOCKET Z272 VACUUM CLEANER SOCKET Z271
R
**ON A/C 301-399,
R
5005VE LIGHT LAV AFT & LOWER
R
**ON A/C 701-749,
R
5005VE LIGHT LAV AFT & MID
R EFF : 301-399, 701-749, 12-21-12 SROS
Page 352 Jul 01/06
**ON A/C ALL 4. Procedure _________ Subtask 12-21-12-615-051 A. Fumigation of the Aircraft WARNING : ONLY PERSONS NECESSARY FOR THIS PROCEDURE ARE PERMITTED IN THE _______ AIRCRAFT DURING THE TASK. WARNING : USE THE CORRECT BREATHING EQUIPMENT. THE GAS IS POISONOUS. _______ WARNING : ALWAYS PUT ON RUBBER GLOVES, GOGGLES AND PROTECTIVE CLOTHES TO _______ PREVENT INFECTION WHEN YOU DO THIS WORK. WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL _______ MATERIAL. THIS MATERIAL IS DANGEROUS. R R
WARNING : DO NOT LET DISINFECTANTS GO ONTO FOODSTUFFS. DISINFECTANTS ARE _______ POISONOUS. DO NOT APPLY THEM AS A SPRAY DIRECTLY TO CARPETS OR COCKPIT INSTRUMENT PANELS. DISINFECTANTS CAN CAUSE DAMAGE TO FURNISHINGS AND EQUIPMENT. (1) Fumigate the Cockpit and the Cabin Area (a) Apply DISINFECTANTS (Material No. 14-004) or equivalent to the: - Floor area of the cockpit - Floor of the galleys and the lavatories - Floor adjacent to the galleys and lavatories - Cabin area. (b) Dry all wet surfaces and covers immediately with a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003). (c) Close the forward passenger/crew door (Ref. TASK 52-10-00-410801). (2) Fumigate the Cargo Compartments (a) Apply DISINFECTANTS (Material No. 14-004) or equivalent to the cargo compartments. (b) Close the forward and aft cargo-compartment doors (Ref. TASK 5230-00-410-801).
EFF : ALL 12-21-12 SROS
Page 353 Jan 01/07
(c) Keep the aircraft doors closed for 45 minutes. (3) Do the ground air pre-conditioning for 1 hour to remove the insecticide from the cabin and cockpit (Ref. TASK 12-33-21-618-801). (4) Open all of the passenger/crew doors (Ref. TASK 52-10-00-010-801) and the forward and aft cargo-compartment doors (Ref. TASK 52-30-00-010801). (5) Let all doors stay open for 5 hours before you go into the aircraft. (6) Clean all the surfaces of the cockpit and the cabin: - The cockpit display units (Ref. TASK 12-21-12-100-801) - The cockpit equipment and furnishings (Ref. TASK 12-21-12-100-802) - The plastic surfaces and mirrors (Ref. TASK 12-21-12-100-804) - The light alloy and steel components (Ref. TASK 12-21-12-100-806) - The monitors and display screens in the cabin (Ref. TASK 12-21-12-100-808). 5. Close-up ________ Subtask 12-21-12-865-054 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1MT, 3MT, 5MT, 7MT, 1ME, 2ME, 3ME, 4ME, 5ME, 6ME, 1MC, 11MC, 111MC, 2MC, 12MC, 112MC, 23MC, 223MC, 24MC **ON A/C 301-399, 701-749, Subtask 12-21-12-865-063 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1LQ, 11LQ, 1ME, 2ME, 3ME, 4ME, 5ME, 6ME, 1MC, 11MC, 111MC, 2MC, 12MC, 112MC, 23MC, 223MC, 24MC
EFF : ALL 12-21-12 R SROS
Page 354 Jul 01/06
**ON A/C ALL Subtask 12-21-12-410-052 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the forward and aft cargo-compartment doors (Ref. TASK 52-3000-410-801). (3) Close the access hatch 211FF. (4) Remove the warning notice(s). (5) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-21-12-862-052 D. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-21-12 R SROS
Page 355 Jul 01/06
TASK 12-21-12-670-804 R
Fumigation of the Fuselage Pressurized Areas with Carbon-Dioxide (CO2 Gas) 1. __________________ Reason for the Job Refer to the SIL 12-007 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific No specific No specific No specific No specific No specific No specific FOR FIN 8DG2 No specific FOR FIN 315HL No specific
1 3 1 2 1 1 2
CHARGING EQUIPMENT - GAS, STANDARD DETECTOR ACT8800 - GRAS HOSE - RUBBER LOCALLY MANUFACTURED - ADAPTER SAFETY BARRIER SUPPLY LINE - GAS, PRESSURIZED WARNING NOTICE
1 ACCESS PLATFORM 5M (16 FT) 1 ACCESS PLATFORM 2M (6 FT)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------No specific Material No. 08-074
cable ties MASKING TAPE (Ref. 20-31-00)
Material No. 14-009 C02 GAS (Ref. 20-31-00)
EFF : ALL 12-21-12 SROS
Page 356 Jan 01/06
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------08-21-00-200-801 12-33-21-618-801
R
21-31-00-710-802 24-42-00-861-801 24-42-00-862-801 25-25-11-000-801 25-25-11-400-801 52-10-00-010-801 52-10-00-410-801 52-30-00-010-801 52-30-00-010-803 52-30-00-410-801
R R
52-30-00-410-803 53-00-00-991-013 AMM AMM
Quick Leveling Procedures Pre-conditioning through the Low-Pressure Ground Connection Operational Test of the Manual Mode Energize the Ground Service Network De-energize the Ground Service Network Removal of a Filler Panel Installation of a Filler Panel Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door Opening of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Opening of the BULK Cargo-Compartment Door Closing of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Closing of the BULK Cargo-Compartment Door Piston Drain Valves of the Lower Fuselage and Bilge Area
30-71-00 52-41-00
R AMM 56-12-00 SIL 12-007 12-21-12-991-009 12-21-12-991-001
Fig. 306 Fig. 307
R 3. __________ Job Set-up Subtask 12-21-12-941-050 A. Safety Precautions WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL _______ MATERIAL. THIS MATERIAL IS DANGEROUS. (1) Make sure that there is sufficient airflow around the aircraft. (2) Do this task on the apron.
EFF : ALL 12-21-12 SROS
Page 357 Jan 01/06
(3) If you do the task in the hangar: (a) Open the doors of the hangar. R
(b) Put SAFETY BARRIER in position to keep all persons out of the work area. (c) Put the WARNING NOTICE in position to tell your personnel about the aircraft fumigation.
R R
(d) If you do the task in a hangar which has under-floor areas, make sure that they are sealed.
R
NOTE : This carbon-dioxide gas (CO2 gas) is heavier than air. ____ Subtask 12-21-12-010-055 B. Get Access
R R
(1) Put the access platforms in position. (a) FOR 8DG2 - Put the ACCESS PLATFORM 5M (16 FT) in position at the sliding window 8DG2.
R R
(b) FOR 315HL - Put the ACCESS PLATFORM 2M (6 FT) in position at the outflow valve 315HL.
R
(2) In the cockpit: (a) Open the sliding window 8DG2 (Ref. AMM 56-12-00).
R
(3) In the forward utility area of the cabin: (a) Remove the filler-panels of the center service-channel as necessary to get access to the area above the ceiling (Ref. TASK 25-25-11-000-801).
EFF : ALL 12-21-12 SROS
Page 358 Jan 01/06
Subtask 12-21-12-480-050 C. Installation of the Equipment (Ref. SIL 12-007) (1) Install the sliding window adapter. (Ref. Fig. 306/TASK 12-21-12-991-009) (a) Put the LOCALLY MANUFACTURED - ADAPTER (1) in position in the cockpit window frame and attach it with the screws and the wing nuts. R R
(b) Put the HOSE - RUBBER, min. dia. 150 mm (6.0 in.), (2) through the opening in the center service channel.
R R
(c) Put the upper end of the hose (2) in the highest position in the fuselage and attach it with cable ties. (d) Connect the lower end of the hose (2) to the window adapter. (2) Install the air-outflow valve-adapter. (Ref. Fig. 307/TASK 12-21-12-991-001)
R R
(a) Put the LOCALLY MANUFACTURED - ADAPTER (1) in position on the outflow valve 315HL and attach it with the hooks and the wing nuts. (b) Connect the SUPPLY LINE - GAS, PRESSURIZED of the DISINFECTANTS (Material No. 14-009) CHARGING EQUIPMENT - GAS, STANDARD to the adapter (1). Subtask 12-21-12-869-050 D. Aircraft Maintenance Configuration (1) Close the air outflow valve 313HL (Ref. TASK 21-31-00-710-802). (2) Make sure that the attitude of the aircraft is level or nose-up (Ref. TASK 08-21-00-200-801). (3) Close the passenger/crew door(s) (Ref. TASK 52-10-00-410-801).
R
(4) Close the forward and aft cargo-compartment doors (Ref. TASK 52-3000-410-801). (5) Make sure that the avionics compartment access door Z811 is closed (Ref. AMM 52-41-00).
EFF : ALL 12-21-12 SROS
Page 359 Jan 01/06
Adapter Cockpit Sliding-Window Figure 306/TASK 12-21-12-991-009 EFF : ALL 12-21-12 R SROS
Page 360 Jan 01/06
R
Adapter Aft Air-Outflow Valve Figure 307/TASK 12-21-12-991-001
EFF : ALL 12-21-12 SROS
Page 361 Jan 01/06
(6) Make sure that the BULK cargo compartment door is closed (Ref. TASK 52-30-00-410-803). (7) Close the outlet of all: - Fuselage drain valves (Ref. TASK 53-00-00-991-013) and - Waste-water drain masts (Ref. AMM 30-71-00)
R R
with BONDING AND ADHESIVE COMPOUNDS (Material No. 08-074). 4. Procedure _________ Subtask 12-21-12-614-050 A. Fumigation of the Aircraft (Ref. SIL 12-007) WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL _______ MATERIAL. THIS MATERIAL IS DANGEROUS. WARNING : DO NOT BREATHE THE GAS. CARBON DIOXIDE IS POISONOUS AND CAN _______ KILL YOU. R
WARNING : USE THE CORRECT BREATHING EQUIPMENT. THE GAS IS POISONOUS. _______ WARNING : BEFORE YOU START THE FUMIGATION PROCEDURE, MAKE SURE THAT NO _______ PERSONS ARE IN THE AIRCRAFT. THE FUMIGATION GAS CAN CAUSE DEATH. WARNING : DO NOT OPEN THE DOORS DURING THE PROCEDURE. POISONOUS GAS IS _______ INSIDE THE AIRCRAFT. (1) Put a WARNING NOTICE in position at all doors to tell your personnel not to open them. (2) Operate the gas charging equipment to fill the pressurized area of the fuselage with DISINFECTANTS (Material No. 14-009) (carbon-dioxide). (a) Refer to the following table for the required quantity of CO2 gas.
EFF : ALL 12-21-12 SROS
Page 362 Jan 01/06
-----------------------------------------------------------------------------| | Aircraft Model | -----------------------------------------------------------------------------| | A330/A340-200 | A330/A340-300 | A340-500 | A340-600 | -----------------------------------------------------------------------------| Quantity of | | | | | | CO2 gas | 2300kg | 2500kg | 2700kg | 3000kg | | (carbon-dioxide) | | | | | | | | | | | -----------------------------------------------------------------------------(3) Stop the gas charging equipment when the DETECTOR ACT8800 - GRAS shows that CO2 (carbon-dioxide) flows out of the outlet hose (2). (Ref. Fig. 306/TASK 12-21-12-991-009)
R
(4) Keep all doors closed for 12 hours. Subtask 12-21-12-010-056 B. Opening of all Pressure Sealed Doors WARNING : STOP THE OPENING PROCEDURE IF THE RED WARNING LIGHT FLASHES. _______ RESIDUAL PRESSURE COULD CAUSE THE DOOR TO OPEN WITH A SUDDEN FORCE AND INJURE PERSONS AND/OR DAMAGE THE AIRCRAFT. WARNING : DO NOT BREATHE THE GAS. CARBON DIOXIDE IS POISONOUS AND CAN _______ KILL YOU. R
WARNING : USE THE CORRECT BREATHING EQUIPMENT. THE GAS IS POISONOUS. _______ (1) Make sure that there is sufficient airflow around the aircraft.
R
(2) Open the forward and aft cargo compartment doors (Ref. TASK 52-30-00010-801). (3) Open the avionics compartment access door Z811 (Ref. AMM 52-41-00). (4) Open the BULK cargo-compartment door (Ref. TASK 52-30-00-010-803). (5) Open all the passenger/crew doors (Ref. TASK 52-10-00-010-801). (6) Open the air-outflow valve 313HL (Ref. TASK 21-31-00-710-802).
EFF : ALL 12-21-12 SROS
Page 363 Jan 01/06
Subtask 12-21-12-080-050 C. Removal of the Equipment (Ref. Fig. 306/TASK 12-21-12-991-009, 307/TASK 12-21-12-991-001) (1) Disconnect the gas charging equipment from the air-outflow valve adapter (1). (2) Remove the outlet tube (2) and the adapters (1). R R R R R
(3) Remove the masking tape (Mat. No. 08-074) from the outlet of the: - waste-water drain masts (Ref. AMM 30-71-00) and - all fuselage drain valves (Ref. TASK 53-00-00-991-013). Subtask 12-21-12-861-066 D. Energize the ground service network (Ref. TASK 24-42-00-861-801) Subtask 12-21-12-618-050 E. Removal of the Remaining CO2 (Carbon-Dioxide) WARNING : DO NOT BREATHE THE GAS. CARBON DIOXIDE IS POISONOUS AND CAN _______ KILL YOU.
R
WARNING : USE THE CORRECT BREATHING EQUIPMENT. THE GAS IS POISONOUS. _______ (1) Do the ground air pre-conditioning for a minimum of 30 min to remove the remaining CO2 from all areas (Ref. TASK 12-33-21-618-801). (2) Do a check of the CO2 concentration. (a) Use a DETECTOR ACT8800 - GRAS and examine the aircraft for remaining CO2. (b) Make sure that there is less than 5% Vol. CO2 concentration 0.2 m (0.65 ft.) above the cabin floor level.
EFF : ALL 12-21-12 SROS
Page 364 Jan 01/06
5. Close-up ________ Subtask 12-21-12-410-055 A. Close Access (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items. (2) Remove the warning notice(s). (3) Install the filler-panels of the center service channel in the forward cabin utility area (Ref. TASK 25-25-11-400-801). (4) Close the cockpit sliding window 8DG2 (Ref. AMM 56-12-00). (5) Close all pressure sealed doors. R R
(a) Close the forward and aft cargo compartment doors (Ref. TASK 5230-00-410-801).
R
(b) Close the avionics compartment access door (Ref. AMM 52-41-00).
R
(c) Close the bulk cargo compartment door (Ref. TASK 52-30-00-410803).
R
(d) Close the passenger/crew door(s) (Ref. TASK 52-10-00-410-801). (6) If you did the task in a hangar with under-floor areas: WARNING : DO NOT BREATHE THE GAS. CARBON DIOXIDE IS POISONOUS AND CAN _______ KILL YOU. WARNING : USE THE CORRECT BREATHING EQUIPMENT. THE GAS IS POISONOUS. _______ (a) Carefully open the sealed areas of the hangar and do a check for remaining CO2 concentration with a DETECTOR ACT8800 - GRAS. (b) Make sure that there is less than 5% Vol. CO2 concentration 0.2 m (0.65 ft.) above the floor of the under floor areas of the hangar. Subtask 12-21-12-862-066 B. De-energize the ground service network (Ref. TASK 24-42-00-862-801)
EFF : ALL 12-21-12 SROS
Page 365 Jan 01/07
INTENTIONALLY BLANK
R 12-21-12 SROS
Page 366 Jan 01/07
TASK 12-21-12-670-805 Special Precautions to Apply Insecticide Agent in Auxiliary Area Compartments and Cargo Compartments, during Turn-Around 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 WARNING NOTICE
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 14-010 INSECTICIDE A/C CABIN (IN FLIGHT) (Ref. 20-31-00) Material No. 14-010A Material No. 14-010B
INSECTICIDE,A/C CABIN (IN FLIGHT) (Ref. 20-31-00) USA AMS 1450 INSECTICIDE,AIRCRAFT (Ref. 20-31-00)
3. __________ Job Set-up Subtask 12-21-12-941-051 A. Preparation (1) Put a WARNING NOTICE in position in the cockpit to tell the flight crew that: - The procedure to apply insecticides in compartments that have smoke detectors is in progress. - Smoke warning(s) caused from the insecticide agent can occur.
R R R
EFF : ALL 12-21-12 SROS
Page 367 Jan 01/06
4. Procedure _________ Subtask 12-21-12-670-050 R R
A. Application of the Insecticide Agent
R
(1) Apply the insecticide agent: - DISINFECTANTS (Material No. 14-010) or - DISINFECTANTS (Material No. 14-010A) or - DISINFECTANTS (Material No. 14-010B) to the auxiliary area compartments and the cargo compartments as necessary. Subtask 12-21-12-210-050 B. Visual Inspection (1) If a smoke warning occurs during the procedure: (a) Do a visual inspection of the related compartment to make sure that there is no smoke. (b) If the insecticide agent caused the warning: - The warning will stop automatically after 3 minutes. Subtask 12-21-12-865-059 C. Put the Aircraft back to its Initial Configuration (1) If a smoke warning has occurred: (a) Start the ventilation controller 280HN again to get the normal ventilation of the affected compartment(s). - In the cockpit on the overhead RESET panel 262VU: pull the C/Bs - VENT CONT LANE 1 and - VENT CONT LANE 2 at the same time for a minimum of 5 seconds but less than 10 seconds.
EFF : ALL 12-21-12 SROS
Page 368 Jan 01/06
NOTE : The CBs must be closed in less than 10 seconds to avoid ____ the automatic shut-down of the IFE system. **ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, Subtask 12-21-12-710-050 D. Test of the Ventilation of the Auxiliary Areas (Crew-Rest) Compartment(s). (1) In the related crew-rest compartment(s): - Make sure that the ventilation and heating system operates correctly. **ON A/C ALL 5. Close-up ________ Subtask 12-21-12-942-055 A. Close Access (1) Remove the warning notice(s).
EFF : ALL 12-21-12 SROS
Page 369 Jan 01/06
DUST REMOVAL - CLEANING/PAINTING ________________________________ TASK 12-21-13-100-801 Dust Removal 1. __________________ Reason for the Job To remove the dust from the avionics compartment and from the center pedestal 100VU in the cockpit. R
NOTE : This task can contribute to fuel savings. ____ 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
soft brush vacuum cleaner access platform 2.5 m (8 ft. 2 in.)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 19-003
USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
EFF : ALL 12-21-13 SROS
Page 701 Jan 01/07
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------21-28-34-000-801 21-28-34-400-801 21-31-34-000-801 21-31-34-400-801
R R R R
21-53-34-000-801 21-53-34-400-801 21-63-34-000-801 21-63-34-400-801 22-82-12-000-801 22-82-12-400-801 22-83-34-000-802 22-83-34-400-802 23-11-33-000-801 23-11-33-400-801 23-12-33-000-801 23-12-33-400-801 23-24-34-000-801 23-24-34-400-801 23-51-12-000-801 23-51-12-400-801 23-51-34-000-801 23-51-34-400-801 23-73-34-000-801 23-73-34-400-801 23-81-13-000-801 23-81-13-400-801 24-41-34-000-801 24-41-34-400-801 24-42-00-861-801 24-42-00-862-801 26-16-34-000-801 26-16-34-400-801
Removal of the Ventilation Controller (280HN) Installation of the Ventilation Controller (280HN) Removal of the Cabin Pressure Controller (311HL,312HL) Installation of the Cabin Pressure Controller (311HL,312HL) Removal of the Pack Controller (531HH, 532HH) Installation of the Pack Controller (531HH, 532HH) Removal of the Zone Controller (630HK) Installation of the Zone Controller (630HK) Removal of the MCDU (2CA1,2CA2,2CA3) Installation of the MCDU (2CA1,2CA2,2CA3) Removal of the FMGEC (1CA1,1CA2) Installation of the FMGEC (1CA1,1CA2) Removal of the HF Transceiver (1RE1) Installation of the HF Transceiver (1RE1) Removal of the VHF Transceiver (1RC1,1RC2,1RC3) Installation of the VHF Transceiver (1RC1,1RC2,1RC3) Removal of the ACARS Management Unit (or ACARS Communications Management Unit (1RB1) Installation of the ACARS Management Unit (or ACARS Communications Management Unit (1RB1) Removal of the Audio Control Panel Installation of the Audio Control Panel Removal of the Audio Management Unit (1RN) Installation of the Audio Management Unit (1RN) Removal of the CIDS Director (101RH,102RH) Installation of the CIDS Director (101RH,102RH) Removal of the Radio Management Panel (1RG1,1RG2,1RG3) Installation of the Radio Management Panel (1RG1,1RG2,1RG3) Removal of the Ground Power Control Unit (GPCU) (1XG) Installation of the Ground Power Control Unit (GPCU) (1XG) Energize the Ground Service Network De-energize the Ground Service Network Removal of the Smoke Detection Control-Unit (SDCU) (20WH) Installation of the Smoke Detection Control-Unit (SDCU) (20WH)
EFF : ALL 12-21-13 SROS
Page 702 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------27-51-34-000-801 27-51-34-400-801 27-92-14-000-801 27-92-14-400-801 27-93-34-000-801 27-93-34-400-801 27-94-34-000-801 27-94-34-400-801 27-95-34-000-801 27-95-34-400-801 28-51-34-000-801 28-51-34-400-801 29-11-34-000-801 29-11-34-400-801 31-33-34-000-801 31-33-34-400-803 31-33-52-000-801 31-33-52-400-801 31-36-34-000-801 31-36-34-400-801 31-36-52-000-801 31-36-52-400-801 31-53-34-000-801 31-53-34-400-801 31-55-34-000-801 31-55-34-400-801 31-62-34-000-801 31-62-34-400-801 32-31-71-000-801 32-31-71-400-801
Removal of the Slat and Flap Control Computer (SFCC) (21CV,22CV) Installation of the Slat and Flap Control Computer (SFCC) (21CV,22CV) Removal of the Speedbrake Control-Lever Assy (20CE) Installation of the Speedbrake Control-Lever Assy (20CE) Removal of the Flight Control Primary Computer (FCPC) (2CE1,2CE2,2CE3) Installation of the Flight Control Primary Computer (FCPC) (2CE1,2CE2,2CE3) Removal of the Flight Control Secondary Computer (FCSC) (3CE1,3CE2) Installation of the Flight Control Secondary Computer (FCSC) (3CE1,3CE2) Removal of the Flight Control Data Concentrator (FCDC) (1CE1,1CE2) Installation of the Flight Control Data Concentrator (FCDC) (1CE1,1CE2) Removal of the Fuel Control and Monitoring Computer (FCMC) (5QM1,5QM2) Installation of the Fuel Control and Monitoring Computer (FCMC) (5QM1,5QM2) Removal of the HSMU (1JG) Installation of the HSMU (1JG) Removal of the FDIU (2TU) Installation of the FDIU (2TU) Removal of the Quick Access Recorder (QAR)(3TU) Installation of the Quick Access Recorder (QAR)(3TU) Removal of the Data Management Unit (DMU)(1TV) Installation of the Data Management Unit (DMU)(1TV) Removal of the Digital ACMS Recorder (DAR)(2TV) Installation of the Digital ACMS Recorder (DAR)(2TV) Removal of the FWC (1WW1,1WW2) Installation of the FWC (1WW1,1WW2) Removal of the SDAC (1WV1,1WV2) Installation of the SDAC (1WV1,1WV2) Removal of the Display Management Computer (DMC)(1WT1, 1WT2, 1WT3) Installation of the Display Management Computer (DMC)(1WT1, 1WT2, 1WT3) Removal of the LGCIU (5GA1,5GA2) Installation of the LGCIU (5GA1,5GA2)
EFF : ALL 12-21-13 R SROS
Page 703 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-42-34-000-801 32-42-34-400-801 32-49-34-000-801 32-49-34-400-801 34-12-34-000-801 34-12-34-400-801 R R R
34-36-31-000-801 34-36-31-000-802 34-36-31-400-801 34-36-31-400-802 34-41-12-000-801 34-41-12-400-801 34-41-33-000-801 34-41-33-400-801 34-43-34-000-801 34-43-34-400-801 34-48-34-000-801 34-48-34-400-801 34-51-33-000-801 34-51-33-400-801 34-52-12-000-801 34-52-12-400-801 34-52-33-000-801 34-52-33-400-801 34-53-31-000-801 34-53-31-400-801 34-55-31-000-801 34-55-31-400-801 36-11-34-000-801 36-11-34-400-801 45-13-34-000-801 45-13-34-400-801
Removal of the BSCU (3GG) Installation of the BSCU (3GG) Removal of the TPIC (2GV) Installation of the TPIC (2GV) Removal of the Air Data/Inertial Reference Unit (ADIRU) (1FP1, 1FP2, 1FP3) Installation of the Air Data/Inertial Reference Unit (ADIRU) (1FP1, 1FP2, 1FP3) Removal of the ILS Receiver (1RT1,1RT2) Removal of the Multi Mode Receiver (40RT1, 40RT2) Installation of the ILS Receiver (1RT1,1RT2) Installation of the Multi Mode Receiver (40RT1, 40RT2) Removal of the Weather Radar Control Unit (3SQ) Installation of the Weather Radar Control Unit (3SQ) Removal of the Weather Radar Transceiver (1SQ1, 1SQ2) Installation of the Weather Radar Transceiver (1SQ1, 1SQ2) Removal of the TCAS Computer (1SG) Installation of the TCAS Computer (1SG) Removal of the Ground Proximity Warning Computer (GPWC) (1WZ) Installation of the Ground Proximity Warning Computer (GPWC) (1WZ) Removal of the DME Interrogator (1SD1, 1SD2) Installation of the DME Interrogator (1SD1, 1SD2) Removal of the ATC/TCAS Control Unit (2SH) Installation of the ATC/TCAS Control Unit (2SH) Removal of the ATC/Mode S Transponder (1SH1, 1SH2) Installation of the ATC/Mode S Transponder (1SH1, 1SH2) Removal of the ADF Receiver (1RP1, 1RP2) Installation of the ADF Receiver (1RP1, 1RP2) Removal of the VOR/MKR Receiver (1RS1, 1RS2) Installation of the VOR/MKR Receiver (1RS1, 1RS2) Removal of the Bleed Monitoring Computer (BMC) (1HA1, 1HA2, 1HA3, 1HA4) Installation of the Bleed Monitoring Computer (BMC) (1HA1, 1HA2, 1HA3, 1HA4) Removal of the Central Maintenance Computer (CMC) (1TM1,1TM2) Installation of the Central Maintenance Computer (CMC) (1TM1,1TM2)
EFF : ALL 12-21-13 SROS
Page 704 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R
45-41-22-000-801 45-41-22-400-801 46-21-34-000-801 46-21-34-400-801 52-71-34-000-801 52-71-34-400-801 73-25-34-000-801
R R R R R R R R
73-25-34-000-802 73-25-34-000-803 73-25-34-000-804 73-25-34-000-805 73-25-34-400-801
R R R R R R
73-25-34-400-802 73-25-34-400-803 73-25-34-400-804 12-21-13-991-001 12-21-13-991-002
Removal of the Printer (2TP) Installation of the Printer (2TP) Removal of the Air Traffic Service Unit (ATSU) (1TX1) Installation of the Air Traffic Service Unit (ATSU) (1TX1) Removal of the Proximity Switch Control Unit (5MJ). Installation of the Proximity Switch Control Unit (5MJ). Removal of the EIVMU (Engine Interface Vibration Monitoring Unit) (1KS1,1KS2,1KS3,1KS4) Removal of the EIVMU (Engine Interface Vibration Monitoring Unit) (1KS1,1KS2) Removal of the EIVMU (Engine Interface Vibration Monitoring Unit) (1KS1,1KS2). Removal of the EIVMU (Engine Interface and Vibration Monitoring Unit) (1KS1, 1KS2) Removal of the EIVMU (Engine Interface and Vibration Monitoring Unit) (1KS1,1KS2,1KS3,1KS4) Installation of the EIVMU (Engine Interface Vibration Monitoring Unit) (1KS1,1KS2,1KS3,1KS4) Installation of the EIVMU (Engine Interface Vibration Monitoring Unit) (1KS1,1KS2) Installation of the EIVMU (Engine Interface Vibration Monitoring Unit). (1KS1,1KS2). Installation of the EIVMU (Engine Interface and Vibration Monitoring Unit) (1KS1, 1KS2) Fig. 701 Fig. 702
3. __________ Job Set-up Subtask 12-21-13-861-050 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-21-13-010-050 B. Get Access (1) Put the access platform in position at the access door 811. (2) Open the access door 811.
EFF : ALL 12-21-13 SROS
Page 705 Jan 01/07
(3) Removal of the units from the cockpit. (Ref. Fig. 701/TASK 12-21-13-991-001) (a) On the center pedestal 100VU: - remove the MCDU (2CA1, 2CA2, 2CA3) (Ref. TASK 22-82-12-000801), - remove the radio management panel (1RG1, 1RG2) (Ref. TASK 2381-13-000-801), - remove the audio control panel (2RN1, 2RN2) (Ref. TASK 23-5112-000-801), - remove the weather radar control unit (3SQ) (Ref. TASK 34-4112-000-801), - remove the ATC/TCAS control unit (2SH) (Ref. TASK 34-52-12-000801), - remove the speedbrake control-lever assy (20CE) (Ref. TASK 2792-14-000-801), - remove the printer (2TP) (Ref. TASK 45-41-22-000-801). - remove the air traffic service unit (1TX1) (Ref. TASK 46-21-34000-801).
R R
(4) Removal of the computers from the avionics compartment. (Ref. Fig. 702/TASK 12-21-13-991-002) (a) On the shelf - remove the - remove the 000-801), - remove the - remove the - remove the 801), - remove the 801), - remove the
811VU: HF transceiver (1RE1) (Ref. TASK 23-11-33-000-801), ATC/Mode S transponder (1SH1) (Ref. TASK 34-52-33-
(b) On the shelf - remove the - remove the 801), - remove the - remove the 801), - remove the 801), - remove the 000-801), - remove the
812VU: ADF receiver (1RP2) (Ref. TASK 34-53-31-000-801), audio management unit (1RN) (Ref. TASK 23-51-34-000-
TCAS computer (1SG) (Ref. TASK 34-43-34-000-801), VHF transceiver (1RC1) (Ref. TASK 23-12-33-000-801), DME interrogator (1SD1) (Ref. TASK 34-51-33-000VOR/MKR receiver (1RS1) (Ref. TASK 34-55-31-000ADF receiver (1RP1) (Ref. TASK 34-53-31-000-801).
VHF transceiver (1RC2) (Ref. TASK 23-12-33-000-801), DME interrogator (1SD2) (Ref. TASK 34-51-33-000VOR/MKR receiver (1RS2) (Ref. TASK 34-55-31-000ATC/Mode S transponder (1SH2) (Ref. TASK 34-52-33HF transceiver (1RE2) (Ref. TASK 23-11-33-000-801).
EFF : ALL 12-21-13 SROS
Page 706 Jan 01/07
Location of Units in the Cockpit (Center Pedestal 100VU) Figure 701/TASK 12-21-13-991-001 EFF : ALL 12-21-13 R SROS
Page 707 Jan 01/07
Location of Shelves and Computers in the Avionics Compartment Figure 702/TASK 12-21-13-991-002 EFF : ALL 12-21-13 R SROS
Page 708 Jan 01/07
(c) On the shelf - remove the - remove the 000-801), - remove the
821VU: VHF transceiver (1RC3) (Ref. TASK 23-12-33-000-801), ACARS management unit (1RB1) (Ref. TASK 23-24-34CIDS director (101RH) (Ref. TASK 23-73-34-000-801).
(d) On the shelf 822VU: - remove the CIDS director (102RH) (Ref. TASK 23-73-34-000-801). (e) On the shelf 831VU: - remove the EIVMU (Engine Interface Vibration Monitoring Unit (1KS1) (Ref. TASK 73-25-34-000-801) , (Ref. TASK 73-25-34-000802), (Ref. TASK 73-25-34-000-803), (Ref. TASK 73-25-34-000804), - remove the Fuel Control and Monitoring Computer (FCMC) (5QM1) (Ref. TASK 28-51-34-000-801), - remove the Display Management Computer (DMC) (1WT1) (Ref. TASK 31-62-34-000-801), - remove the FWC (1WW1) (Ref. TASK 31-53-34-000-801), - remove the SDAC (1WV1) (Ref. TASK 31-55-34-000-801).
R R R R
(f) On the shelf 832VU: - remove the EIVMU (Engine Interface Vibration Monitoring Unit) (1KS2) (Ref. TASK 73-25-34-000-801) , (Ref. TASK 73-25-34-000802), (Ref. TASK 73-25-34-000-803), (Ref. TASK 73-25-34-000804), (Ref. TASK 73-25-34-000-805), - remove the Fuel Control and Monitoring Computer (FCMC) (5QM2) (Ref. TASK 28-51-34-000-801), - remove the Display Management Computer (DMC) (1WT2) (Ref. TASK 31-62-34-000-801), - remove the FWC (1WW2) (Ref. TASK 31-53-34-000-801), - remove the SDAC (1WV2) (Ref. TASK 31-55-34-000-801).
R R R R
(g) On the shelf 841VU: - remove the FMGEC (1CA1) (Ref. TASK 22-83-34-000-802), - remove the Slat and Flap Control Computer (SFCC) (21CV) (Ref. TASK 27-51-34-000-801), - remove the Display Management Computer (DMC) (1WT3) (Ref. TASK 31-62-34-000-801), - remove the HSMU (1JG) (Ref. TASK 29-11-34-000-801), - remove the Flight Control Data Concentrator (FCDC) (1CE1) (Ref. TASK 27-95-34-000-801), - remove the Flight Control Primary Computer (FCPC) (2CE3) (Ref. TASK 27-93-34-000-801).
EFF : ALL 12-21-13 SROS
Page 709 Jan 01/07
(h) On the shelf - remove the - remove the (Ref. TASK - remove the (Ref. TASK - remove the (Ref. TASK - remove the (Ref. TASK
842VU: FMGEC (1CA2) (Ref. TASK 22-83-34-000-802), Slat and Flap Control Computer (SFCC) (22CV) 27-51-34-000-801), Flight Control Data Concentrator (FCDC) (1CE2) 27-95-34-000-801), Flight Control Secondary Computer (FCSC) (3CE2) 27-94-34-000-801), Flight Control Primary Computer (FCPC) (2CE2) 27-93-34-000-801).
(i) On the shelf 851VU: - remove the Ground Proximity Warning Computer (GPWC) (1WZ) (Ref. TASK 34-48-34-000-801), - remove the zone controller (630HK) (Ref. TASK 21-63-34-000801), - remove the cabin pressure controller (311HL) (Ref. TASK 21-3134-000-801), - remove the pack controller (531HH) (Ref. TASK 21-53-34-000801), - remove the Bleed Monitoring Computer (BMC) (1HA1) (Ref. TASK 36-11-34-000-801), - remove the BSCU (3GG) (Ref. TASK 32-42-34-000-801), - remove the LGCIU (5GA1) (Ref. TASK 32-31-71-000-801). (j) On the shelf 852VU: - remove the ventilation controller (280HN) (Ref. TASK 21-28-34000-801), - remove the cabin pressure controller (312HL) (Ref. TASK 21-3134-000-801), - remove the Bleed Monitoring Computer (BMC) (1HA2) (Ref. TASK 36-11-34-000-801), - remove the pack controller (532HH) (Ref. TASK 21-53-34-000801), - remove the Ground Power Control Unit (GPCU) (1XG) (Ref. TASK 24-41-34-000-801), - remove the TPIC (2GV) (Ref. TASK 32-49-34-000-801), - remove the Smoke Detection Control-Unit (SDCU) (20WH) (Ref. TASK 26-16-34-000-801), - remove the LGCIU (5GA2) (Ref. TASK 32-31-71-000-801). (k) On the shelf 861VU: - remove the Central Maintenance Computer (CMC) (1TM1) (Ref. TASK 45-13-34-000-801).
EFF : ALL 12-21-13 R SROS
Page 710 Jan 01/07
(l) On the shelf 862VU: - remove the proximity switch control unit (5MJ) (Ref. TASK 5271-34-000-801), - remove the FDIU (2TU) (Ref. TASK 31-33-34-000-801), - Remove the Quick Access Recorder (QAR) (3TU) (Ref. TASK 31-3352-000-801), - remove the Digital ACMS Recorder (DAR) (2TV) (Ref. TASK 31-3652-000-801), - remove the Data Management Unit (DMU) (1TV) (Ref. TASK 31-3634-000-801), - remove the Central Maintenance Computer (CMC) (1TM2) (Ref. TASK 45-13-34-000-801), (m) On the shelf 872VU: - remove the Air Data/Inertial Reference Unit (ADIRU) (1FP1, 1FP2) (Ref. TASK 34-12-34-000-801). (n) Remove the Air Data/Inertial Reference Unit (ADIRU) (1FP3) (Ref. TASK 34-12-34-000-801). (o) On the mounting tray 5SQ: - remove the weather radar transceiver (1SQ1, 1SQ2) (Ref. TASK 34-41-33-000-801). (p) On the shelf - remove the (Ref. TASK - remove the (Ref. TASK - remove the (Ref. TASK - remove the (Ref. TASK
R R
R R
915VU: ILS receiver (1RT1) (Ref. TASK 34-36-31-000-801), 34-36-31-000-802). Flight Control Secondary Computer (FCSC) (3CE1) 27-94-34-000-801), Flight Control Primary Computer (FCPC) (2CE1) 27-93-34-000-801), ILS receiver (1RT2) (Ref. TASK 34-36-31-000-801), 34-36-31-000-802).
(q) On the shelves 811VU, 812VU, 821VU, 822VU, 831VU, 832VU, 841VU, 842VU, 851VU, 852VU, 861VU, 862VU, 915VU: (Ref. Fig. 702/TASK 12-21-13-991-002) - remove the rack assy.
EFF : ALL 12-21-13 SROS
Page 711 Jan 01/07
4. Procedure _________ (Ref. Fig. 701/TASK 12-21-13-991-001, 702/TASK 12-21-13-991-002) Subtask 12-21-13-160-050 A. Cleaning of the Avionics Compartment and of the Cockpit (1) Use a vacuum cleaner and a soft brush or a MISCELLANEOUS (Material No. 19-003) and clean: (a) the area where the units and computers were installed, (b) the area of the rack assy. (c) all the faces of the removed units and computers, (d) the avionics compartment, (e) the ducts, (f) the shelves. NOTE : Keep the vacuum cleaner out of the avionics compartment to ____ prevent new dust contamination in the avionics compartment. 5. Close-up ________ Subtask 12-21-13-410-050 A. Close Access (1) Installation of the units in the cockpit. (Ref. Fig. 701/TASK 12-21-13-991-001) NOTE : For computers with loadable software, software loading is not ____ necessary if you install the computer removed for access. (a) On the center pedestal 100VU: - install the MCDU (2CA1, 2CA2, 2CA3) (Ref. TASK 22-82-12-400801), - install the radio management panel (1RG1, 1RG2) (Ref. TASK 2381-13-400-801), - install the audio control panel (2RN1, 2RN2) (Ref. TASK 23-5112-400-801),
EFF : ALL 12-21-13 R SROS
Page 712 Jan 01/07
- install the weather radar control unit (3SQ) (Ref. TASK 34-4112-400-801), - install the ATC/TCAS control unit (2SH) (Ref. TASK 34-52-12400-801), - install the speedbrake control lever assy (20CE) (Ref. TASK 2792-14-400-801), - install the printer (2TP) (Ref. TASK 45-41-22-400-801), (Ref. TASK 46-21-34-400-801).
R R
(2) Installation of the computers in the avionics compartment. (Ref. Fig. 702/TASK 12-21-13-991-002) NOTE : For computers with loadable software, software loading is not ____ necessary if you install the computer removed for access. (a) On the shelves 811VU, 812VU, 821VU, 822VU, 831VU, 832VU, 841VU, 842VU, 851VU, 852VU, 861VU, 862VU, 915VU: (Ref. Fig. 702/TASK 12-21-13-991-002) - install the rack assy. (b) On the shelf 811VU: - install the HF transceiver (1RE1) (Ref. TASK 23-11-33-400-801), - install the ATC/Mode S transponder (1SH1) (Ref. TASK 34-52-33400-801), - install the TCAS computer (1SG) (Ref. TASK 34-43-34-400-801), - install the VHF transceiver (1RC1) (Ref. TASK 23-12-33-400801), - install the DME interrogator (1SD1) (Ref. TASK 34-51-33-400801), - install the VOR/MKR receiver (1RS1) (Ref. TASK 34-55-31-400801), - install the ADF receiver (1RP1) (Ref. TASK 34-53-31-400-801). (c) On the shelf 812VU: - install the ADF receiver (1RP2) (Ref. TASK 34-53-31-400-801), - install the audio management unit (1RN) (Ref. TASK 23-51-34400-801), - install the VHF transceiver (1RC2) (Ref. TASK 23-12-33-400801), - install the DME interrogator (1SD2) (Ref. TASK 34-51-33-400801), - install the VOR/MKR receiver (1RS2) (Ref. TASK 34-55-31-400801), - install the ATC/Mode S transponder (1SH2) (Ref. TASK 34-52-33400-801), - install the HF transceiver (1RE2) (Ref. TASK 23-11-33-400-801).
EFF : ALL 12-21-13 SROS
Page 713 Jan 01/07
(d) On the shelf 821VU: - install the VHF transceiver (1RC3) (Ref. TASK 23-12-33-400801), - install the ACARS management unit (1RB1) (Ref. TASK 23-24-34400-801), - install the CIDS director (101RH) (Ref. TASK 23-73-34-400-801). (e) On the shelf 822VU: - install the CIDS director (102RH) (Ref. TASK 23-73-34-400-801). (f) On the shelf 831VU: - install the EIVMU (Engine Interface Vibration Monitoring Unit) (1KS1) (Ref. TASK 73-25-34-400-801) , (Ref. TASK 73-25-34-400802), (Ref. TASK 73-25-34-400-803), (Ref. TASK 73-25-34-400804), - install the Fuel Control and Monitoring Computer (FCMC) (5QM1) (Ref. TASK 28-51-34-400-801), - install the Display Management Computer (DMC) (1WT1) (Ref. TASK 31-62-34-400-801), - install the FWC (1WW1) (Ref. TASK 31-53-34-400-801), - install the SDAC (1WV1) (Ref. TASK 31-55-34-400-801).
R R R R
(g) On the shelf 832VU: - install the EIVMU (Engine Interface Vibration Monitoring Unit) (1KS2) (Ref. TASK 73-25-34-400-801) , (Ref. TASK 73-25-34-400802), (Ref. TASK 73-25-34-400-803), (Ref. TASK 73-25-34-400804), - install the Fuel Control and Monitoring Computer (FCMC) (5QM2) (Ref. TASK 28-51-34-400-801), - install the Display Management Computer (DMC) (1WT2) (Ref. TASK 31-62-34-400-801), - install the FWC (1WW2) (Ref. TASK 31-53-34-400-801), - install the SDAC (1WV2) (Ref. TASK 31-55-34-400-801).
R R R R
(h) On the shelf 841VU: - install the FMGEC (1CA1) (Ref. TASK 22-83-34-400-802), - install the Slat and Flap Control Computer (SFCC) (21CV) (Ref. TASK 27-51-34-400-801), - install the Display Management Computer (DMC) (1WT3) (Ref. TASK 31-62-34-400-801), - install the HSMU (1JG) (Ref. TASK 29-11-34-400-801), - install the Flight Control Data Concentrator (FCDC) (1CE1) (Ref. TASK 27-95-34-400-801), - install the Flight Control Primary Computer (FCPC) (2CE3) (Ref. TASK 27-93-34-400-801).
EFF : ALL 12-21-13 SROS
Page 714 Jan 01/07
(i) On the shelf 842VU: - install the FMGEC (1CA2) (Ref. TASK 22-83-34-400-802), - install the Slat and Flap Control Computer (SFCC) (22CV) (Ref. TASK 27-51-34-400-801), - install the Flight Control Data Concentrator (FCDC) (1CE2) (Ref. TASK 27-95-34-400-801), - install the Flight Control Secondary Computer (FCSC) (3CE2) (Ref. TASK 27-94-34-400-801), - install the Flight Control Primary Computer (FCPC) (2CE2) (Ref. TASK 27-93-34-400-801). (j) On the shelf 851VU: - install the Ground Proximity Warning Computer (GPWC) (1WZ) (Ref. TASK 34-48-34-400-801), - install the zone controller (630HK) (Ref. TASK 21-63-34-400801), - install the cabin pressure controller (311HL) (Ref. TASK 21-3134-400-801), - install the pack controller (531HH) (Ref. TASK 21-53-34-400801), - install the Bleed Monitoring Computer (BMC) (1HA1) (Ref. TASK 36-11-34-400-801), - install the BSCU (3GG) (Ref. TASK 32-42-34-400-801), - install the LGCIU (5GA1) (Ref. TASK 32-31-71-400-801). (k) On the shelf 852VU: - install the ventilation controller (280HN) (Ref. TASK 21-28-34400-801), - install the cabin pressure controller (312HL) (Ref. TASK 21-3134-400-801), - install the Bleed Monitoring Computer (BMC) (1HA2) (Ref. TASK 36-11-34-400-801), - install the pack controller (532HH) (Ref. TASK 21-53-34-400801), - install the Ground Power Control Unit (GPCU) (1XG) (Ref. TASK 24-41-34-400-801), - install the TPIC (2GV) (Ref. TASK 32-49-34-400-801), - install the Smoke Detection Control-Unit (SDCU) (20WH) (Ref. TASK 26-16-34-400-801), - install the LGCIU (5GA2) (Ref. TASK 32-31-71-400-801). (l) On the shelf 861VU: - install the Central Maintenance Computer (CMC) (1TM1) (Ref. TASK 45-13-34-400-801).
EFF : ALL 12-21-13 R SROS
Page 715 Jan 01/07
(m) On the shelf 862VU: - install the proximity switch control unit (5MJ) (Ref. TASK 5271-34-400-801), - install the FDIU (2TU) (Ref. TASK 31-33-34-400-803), - install the Quick Access Recorder (QAR) (3TU) (Ref. TASK 31-3352-400-801), - install the Digital ACMS Recorder (DAR) (2TV) (Ref. TASK 31-3652-400-801), - install the Data Management Unit (DMU) (1TV) (Ref. TASK 31-3634-400-801), - install the Central Maintenance Computer (CMC) (1TM2) (Ref. TASK 45-13-34-400-801), (n) On the shelf 872VU: - install the Air Data/Inertial Reference Unit (ADIRU) (1FP1, 1FP2) (Ref. TASK 34-12-34-400-801). (o) Install the Air Data/Inertial Reference Unit (ADIRU) (1FP3) (Ref. TASK 34-12-34-400-801). (p) On the mounting tray 5SQ: - install the weather radar transceiver (1SQ1, 1SQ2) (Ref. TASK 34-41-33-400-801). (q) On the shelf 915VU: - install the ILS receiver (1RT1) (Ref. TASK 34-36-31-400-801), (Ref. TASK 34-36-31-400-802). - install the Flight Control Secondary Computer (FCSC) (3CE1) (Ref. TASK 27-94-34-400-801), - install the Flight Control Primary Computer (FCPC) (2CE1) (Ref. TASK 27-93-34-400-801), - install the ILS receiver (1RT2) (Ref. TASK 34-36-31-400-801).
R R
(3) Make sure that the work area is clean and clear of tools and other items. (4) Close the access door 811. (5) Remove the access platform(s). Subtask 12-21-13-862-050 B. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-21-13 SROS
Page 716 Jan 01/07
TASK 12-21-13-100-802 Cleaning of Relay Box VU Panel Grids 1. __________________ Reason for the Job Refer to the MPD TASK: 212600-07 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 12-21-13-991-003
Energize the Ground Service Network De-energize the Ground Service Network Fig. 703
3. __________ Job Set-up Subtask 12-21-13-860-050 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). (2) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the access door 811. (3) Open the access door 811.
EFF : ALL 12-21-13 R SROS
Page 717 Jan 01/07
4. Procedure _________ (Ref. Fig. 703/TASK 12-21-13-991-003) Subtask 12-21-13-140-050 A. Cleaning of the Grids of the Relay Boxes NOTE : In the avionics compartment, use a vacuum cleaner and a soft brush ____ to clean the equipments. Keep the vacuum cleaner out of the avionics compartment to prevent dust contamination. (1) Clean the grids of the left relay box 751VU (a) Clean the left and right external grids. (b) Clean the bottom external grid. (c) Open the door of the relay box. (d) Clean the left and right internal grids. (e) Clean the bottom internal grid. (f) Close the door of the relay box. (2) Clean the grids of the right relay box 752VU (a) Clean the left and right external grids. (b) Clean the bottom external grid. (c) Open the door of the relay box. (d) Clean the left and right internal grids. (e) Clean the bottom internal grid. (f) Close the door of the relay box.
EFF : ALL 12-21-13 R SROS
Page 718 Jan 01/07
Location of Relay Boxes in the Avionics Compartment Figure 703/TASK 12-21-13-991-003 EFF : ALL 12-21-13 R SROS
Page 719 Jan 01/07
5. Close-up ________ Subtask 12-21-13-860-051 A. Put the Aircraft back to its Initial Configuration (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access door 811. (3) Remove the access platform(s). (4) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-21-13 SROS
Page 720 Jan 01/07
LUBRICATION - DESCRIPTION AND OPERATION _______________________________________ 1. _______ General This section gives the instructions related to the lubrication of the flight controls, the landing gear, the doors, the fuselage, the rudder and sliding windows. It includes the topics below: 12-22-27/P. Block 301 FLIGHT CONTROLS 12-22-32/P. Block 301 LANDING GEAR 12-22-52/P. Block 301 DOORS 12-22-53/P. Block 301 FUSELAGE 12-22-55/P. Block 301 STABILIZERS 12-22-56/P. Block 301 WINDOWS A. Lubrication Point Symbols: Each type of lubrication point is identified by a symbol. (Ref. Fig. 001)
EFF : ALL 12-22-00 SROS
Page 1 Apr 01/98
Lubrication Point Symbols Figure 001 EFF : ALL 12-22-00 SROS
Page 2 Apr 01/98
FLIGHT CONTROLS - SERVICING ___________________________ TASK 12-22-27-640-801 Lubricate the Trimmable Horizontal Stabilizer (THS) Actuator Ball Screw Nut WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. 1. __________________ Reason for the Job Refer to the MPD TASK: 274400-09 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No No No No No
specific specific specific specific specific
circuit breaker(s) safety clip(s) ACCESS PLATFORM 5M (16 FT) CONTAINER 1 L (1/4 USGAL) GUN - GREASE WARNING NOTICE
1 1 1 1
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 04-004 Material No. 19-003
USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
EFF : ALL 12-22-27 SROS
Page 301 Jan 01/05
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 27-40-00-866-801 29-00-00-863-802 29-00-00-863-803 29-00-00-864-802 29-00-00-864-803 29-00-00-864-804 R
ESPM 20-55-10 ESPM 20-55-20 12-22-27-991-001-A
Energize the Ground Service Network De-energize the Ground Service Network Operation of the THS Actuator Pressurize the Blue Hydraulic System with the Electric Pump Pressurize the Yellow Hydraulic System with the Electric Pump Depressurize the Blue Hydraulic System (Pressurized with the Electric Pump) Depressurize the Yellow Hydraulic System (Pressurized with the Electric Pump) Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Fig. 301
3. __________ Job Set-up Subtask 12-22-27-860-054 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). (2) Make sure that the hydraulic systems are depressurized (Ref. TASK 29-00-00-864-804).
EFF : ALL 12-22-27 SROS
Page 302 Apr 01/05
Subtask 12-22-27-865-050 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU FCPC3 STBY COM 7CE6 R20 721VU FCPC3 STBY MON 7CE5 R19 722VU FCPC 3 7CE3 V42 722VU FCPC 2 NORM 7CE2 V41 722VU FCPC 3 7CE4 V38 742VU FCPC 1 NORM 7CE1 C69 742VU FCPC 1 STBY 11CE K69 Subtask 12-22-27-010-050 C. Get Access (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the THS. (2) Put the ACCESS PLATFORM 5M (16 FT) below the access door 312AR, open the access door 312AR and set the LIGHT switch 4LJ to ON. (3) Make sure that the temperature of the ball screw nut is above 1 DEG.C (33.80 DEG.F). 4. Procedure _________ (Ref. Fig. 301/TASK 12-22-27-991-001-A) Subtask 12-22-27-640-063 A. Lubricate the THS-Actuator Ball Screw-Nut CAUTION : DO NOT MIX LITHIUM-COMPLEX THICKENED GREASE WITH CLAY_______ THICKENED GREASE. IF YOU MIX THESE GREASES, YOU CAN CAUSE DAMAGE TO THE BALL NUT OF THE THS ACTUATOR. R R
(1) Clean the vent hole area, the grease nipple and the THS-actuator ball screw-nut.To do this, use a clean lint-free cloth MISCELLANEOUS (Material No. 19-003). (2) Use a non-metallic device and make sure that the vent hole is clear.
EFF : ALL 12-22-27 SROS
Page 303 Jul 01/06
R
Trimmable Horizontal Stabilizer (THS) Actuator Figure 301/TASK 12-22-27-991-001-A
EFF : ALL 12-22-27 SROS
Page 304 Jan 01/04
(3) Use a GUN - GREASE (MIL-PRF-23827) and apply the new COMMON GREASE (Material No. 04-004) through the grease nipple of the THS-actuator ball screw-nut. Do this until the grease comes out of the nut vent hole. It is usual that some grease comes out of the upper/lower nut seal. (4) Make sure that no grease comes out of the transfer tubes. If grease comes out of the transfer tubes, speak to Airbus.
R
(5) Put a CONTAINER 1 L (1/4 USGAL) in position below the vent hole. (6) Use a GUN - GREASE (MIL-PRF-23827) and again apply the new COMMON GREASE (Material No. 04-004) through the grease nipple of the THS-actuator ball screw-nut. Do this until 150 cm3 (9.15 in.3) of the grease comes out of the nut vent hole. (7) Remove the unwanted grease from the grease nipple and the top and bottom of the nut. To do this, use a clean lint-free cloth MISCELLANEOUS (Material No. 19-003). (8) Pressurize the Blue or the Yellow hydraulic system (Ref. TASK 29-0000-863-802) or (Ref. TASK 29-00-00-863-803). (9) Operate the THS R R R
CAUTION : MAKE SURE THAT YOU REMOVE THE GREASING TOOL BEFORE YOU _______ OPERATE THE THS ACTUATOR. THE GREASING TOOL CAN CAUSE DAMAGE TO THE THS ACTUATOR. (a) Move the THS to the 14⁰UP stop position and then back to the neutral position (Ref. TASK 27-40-00-866-801). (10) Depressurize the Blue or the Yellow hydraulic system (Ref. TASK 2900-00-864-802) or (Ref. TASK 29-00-00-864-803) and make sure that the hydraulic system is depressurized (Ref. TASK 29-00-00-864-804). (11) Clean the THS-actuator ball screw-nut around the transfer tubes with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003). (12) Use a GUN - GREASE (MIL-PRF-23827) and again apply the new COMMON GREASE (Material No. 04-004) through the grease nipple of the THS-actuator ball screw-nut. Do this until the grease comes continuously out of the nut vent hole. (13) Make sure that no grease comes out of the transfer tubes. If grease comes out of the transfer tubes, contact Airbus. (14) Put a CONTAINER 1 L (1/4 USGAL) in position below the vent hole.
EFF : ALL 12-22-27 SROS
Page 305 Jan 01/07
(15) Use a GUN - GREASE and again apply the new COMMON GREASE (Material No. 04-004) through the grease nipple of the THS-actuator ball screw-nut. Do this until 150 cm3 (9.15 in.3) of the grease comes out of the nut vent hole. (16) Clean the vent hole area, the grease nipple and the THS-actuator ball screw-nut. To do this, use a clean lint-free cloth MISCELLANEOUS (Material No. 19-003). (a) If you find contamination of the electrical cables, you must clean them (Ref. ESPM 20-55-10) and (Ref. ESPM 20-55-20). (17) Make sure that the ball in the grease nipple closes correctly the grease nipple. 5. Close-up ________ Subtask 12-22-27-865-051 A. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 7CE1, 7CE2, 7CE3, 7CE4, 7CE5, 7CE6, 11CE. Subtask 12-22-27-410-050 B. Close Access R R R
CAUTION : MAKE SURE THAT YOU REMOVE THE GREASING TOOL BEFORE YOU OPERATE _______ THE THS ACTUATOR. THE GREASING TOOL CAN CAUSE DAMAGE TO THE THS ACTUATOR. (1) Make sure that the work area is clean and clear of tools and other items. (2) Set the LIGHT switch 4LJ to OFF and close the access door 312AR. (3) Remove the access platform(s). (4) Remove the warning notice(s). (5) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-22-27-860-055 C. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-22-27 SROS
Page 306 Jan 01/07
TASK 12-22-27-640-802 Lubricate the Trimmable Horizontal Stabilizer (THS) Mechanical Control Chains R R
WARNING : KEEP ALL HYDROCARBONS (FUELS, LUBRICANTS, ETC.) AWAY FROM ALL SOURCES _______ OF OXYGEN. OXYGEN BECOMES EXPLOSIVE WHEN IT TOUCHES HYDROCARBONS. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Refer to the MPD TASK: 274100-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific No specific 98F27401000000
1 1 1 1
circuit breaker(s) safety clip(s) ACCESS PLATFORM 3M (10 FT) BRUSH - BRISTLED WARNING NOTICE PITCH TRIM CONTROL LOCKING
EFF : ALL 12-22-27 SROS
Page 307 Jul 01/06
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 04-004 Material No. 05-002 Material No. 05-005 Material No. 11-002 R R
Material No. 19-003
USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00) USA MIL-C-16173 GRADE II CORROSION PREVENTIVE (Ref. 20-31-00) USA MIL-PRF-680 DRY CLEANING SOLVENT (VARSOL/WHITE SPIRIT) (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------1
cotter pins
27-41-04 03 -110
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 27-40-00-866-801 29-00-00-864-804 12-22-27-991-002
Energize the Ground Service Network De-energize the Ground Service Network Operation of the THS Actuator Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Fig. 302
R EFF : ALL 12-22-27 SROS
Page 308 Jul 01/06
INTENTIONALLY BLANK
R 12-22-27 SROS
Page 309 Jul 01/06
INTENTIONALLY BLANK
R 12-22-27 SROS
Page 310 Apr 01/03
3. __________ Job Set-up Subtask 12-22-27-860-056 A. Aircraft Maintenance Configuration (1) Make sure that the pitch-trim control wheels on the panel 125VU are in the 0 position (Ref. TASK 27-40-00-866-801). (2) Install the PITCH TRIM CONTROL LOCKING (98F27401000000) on the pitch-trim control wheels. (3) Put the WARNING NOTICE in position on the panel 125VU to tell persons not to operate the pitch-trim controls. (4) Energize the ground service network (Ref. TASK 24-42-00-861-801). (5) Make sure that the hydraulic systems are depressurized (Ref. TASK 29-00-00-864-804). Subtask 12-22-27-865-052 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU FCPC3 STBY COM 7CE6 R20 721VU FCPC3 STBY MON 7CE5 R19 722VU FCPC 3 7CE3 V42 722VU FCPC 2 NORM 7CE2 V41 722VU FCPC 3 7CE4 V38 742VU FCPC 1 NORM 7CE1 C69 742VU FCPC 1 STBY 11CE K69 Subtask 12-22-27-010-051 C. Get Access (Ref. Fig. 302/TASK 12-22-27-991-002) (1) Put the ACCESS PLATFORM 3M (10 FT) below the access door 312AR and open the access door 312AR and set the LIGHT switch 4LJ to ON. (2) Remove the screws (8), the washers (7), release the quick-release fasteners (6) and remove the protective cover (9).
R EFF : ALL 12-22-27 SROS
Page 311 Jul 01/02
Control Chain Figure 302/TASK 12-22-27-991-002- 12 (SHEET 1) EFF : ALL 12-22-27 R SROS
Page 312 Jan 01/02
Control Chain Figure 302/TASK 12-22-27-991-002- 22 (SHEET 2) EFF : ALL 12-22-27 R SROS
Page 313 Jan 01/02
(3) Remove and discard the cotter pins (1), remove the nuts (2), the washers (3), the bolts (4) and the chain cover (5). 4. Procedure _________ (Ref. Fig. 302/TASK 12-22-27-991-002) Subtask 12-22-27-640-051 A. Lubrication of the THS Mechanical Control Chains R R R
WARNING : KEEP ALL HYDROCARBONS (FUELS, LUBRICANTS, ETC.) AWAY FROM ALL _______ SOURCES OF OXYGEN. OXYGEN BECOMES EXPLOSIVE WHEN IT TOUCHES HYDROCARBONS. WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Clean the forward and the aft chain with CLEANING AGENTS (Material No. 11-002) and a BRUSH - BRISTLED.
R R
(2) Use a BRUSH - BRISTLED to apply a thin layer of the COMMON GREASE (Material No. 04-004) to the chains.
R
(3) Do not apply too much grease to the chains.
R R R
(a) If you apply too much grease to the chains: - Use a clean lint-free cloth MISCELLANEOUS (Material No. 19-003) to remove the unwanted grease from the chains.
R R
(4) Make sure that the grease does not fall into the area of the electronic and/or oxygen equipment. 5. Close-up ________ Subtask 12-22-27-410-058 A. Close Access (Ref. Fig. 302/TASK 12-22-27-991-002) (1) Install the chain cover (5). (a) Apply the SPECIAL MATERIALS (Material No. 05-002) to the interface of the chain cover (5), to the bolts (4) and the nuts (2).
EFF : ALL 12-22-27 SROS
Page 314 Jul 01/06
(b) Install the chain cover (5), the bolts (4), the washers (3), the nuts (2) and safety the nuts (2) with the new cotter pins (1). (c) Apply the SPECIAL MATERIALS (Material No. 05-005) to the bolts (4) and the nuts (2). (2) Install the protective cover (9), tighten the quick-release fasteners (6) and install the washers (7) and the screws (8). Subtask 12-22-27-865-053 B. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 7CE1, 7CE2, 7CE3, 7CE4, 7CE5, 7CE6, 11CE. Subtask 12-22-27-410-051 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Set the LIGHT switch 4LJ to OFF and close the access door 312AR. (3) Remove the access platform(s). (4) Remove the warning notice(s). (5) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-22-27-860-057 D. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801). (2) Remove the PITCH TRIM CONTROL LOCKING from the pitch-trim control wheels.
EFF : ALL 12-22-27 R SROS
Page 315 Jul 01/06
TASK 12-22-27-640-803 R
Lubrication of Flap Track/Carriage (1-5) Roller Bearings WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Refer to the MPD TASK: 275400-04 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific 98D27803000000 98F29208217000
circuit breaker(s) safety clip(s) 1 WARNING NOTICE 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER 1 SAFETY PIN - RAT
EFF : ALL 12-22-27 SROS
Page 316 Jan 01/06
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R
Material No. 04-004 Material No. 19-003
USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 27-50-00-866-801 27-50-00-866-802 29-24-00-081-801 29-24-00-481-801 32-12-00-010-801 32-12-00-410-801 12-22-27-991-003
Energize the Ground Service Network De-energize the Ground Service Network Extension of the Flaps on the Ground Retraction of the Flaps on the Ground Removal of the RAT Safety Pin Installation of the RAT Safety Pin Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Fig. 303
3. __________ Job Set-up Subtask 12-22-27-860-050 A. Aircraft Maintenance Configuration (1) Fully extend the flaps (Ref. TASK 27-50-00-866-801). (2) Put the WARNING NOTICE in position on panel 114VU to tell persons not to operate the flap/slat controls. (3) Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER on the flap/slat control lever on panel 114VU. (4) Energize the ground service network (Ref. TASK 24-42-00-861-801).
EFF : ALL 12-22-27 SROS
Page 317 Jul 01/04
Subtask 12-22-27-865-054 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM 10CV X14 722VU SFCC 2 FLAP 2CV T43 742VU SFCC 1 FLAP 1CV L61 Subtask 12-22-27-010-052 C. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Install the SAFETY PIN - RAT (Ref. TASK 29-24-00-481-801). 4. Procedure _________ (Ref. Fig. 303/TASK 12-22-27-991-003) Subtask 12-22-27-640-052 A. Lubrication of the Flap Track/Carriage Roller Bearings WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Clean the grease nipples with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003). R R R
(2) Apply the COMMON GREASE (Material No. 04-004) to the flap-track/carriage roller bearings through the the grease nipples until the new grease comes out from the fittings. (3) Remove the unwanted grease from the greasing points.
EFF : ALL 12-22-27 SROS
Page 318 Jul 01/04
5. Close-up ________ Subtask 12-22-27-865-055 A. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1CV, 2CV, 10CV Subtask 12-22-27-410-052 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the MLG doors (Ref. TASK 32-12-00-410-801). (3) Remove the SAFETY PIN - RAT (Ref. TASK 29-24-00-081-801). (4) Remove the access platform(s). Subtask 12-22-27-860-051 C. Put the Aircraft back to its Initial Configuration (1) Remove the warning notice(s). (2) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever on panel 114VU. (3) Retract the flaps (Ref. TASK 27-50-00-866-802). (4) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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R
Flap Track Rollers Figure 303/TASK 12-22-27-991-003- 12 (SHEET 1)
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Page 320 Jul 01/04
R
Flap Track Rollers Figure 303/TASK 12-22-27-991-003- 22 (SHEET 2)
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Page 321 Jul 01/04
TASK 12-22-27-640-804 R
Lubrication of all Slat Track Roller Bearings, Pinion Bearings, Rack and Pinion Teeth and Slat Track 2 and 3 Lever Bearings WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Refer to the MPD TASK: 278000-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific 98D27803000000
circuit breaker(s) safety clip(s) 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 WARNING NOTICE 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
EFF : ALL 12-22-27 SROS
Page 322 Jan 01/06
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 04-022 Material No. 19-003
USA MIL-PRF-81322 SYNTHE.HYDROCARBON GREASE HIGH PRESSURE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 27-50-00-866-801 27-50-00-866-802 27-80-00-866-801 27-80-00-866-802 57-41-37-000-801 57-41-37-400-801 57-42-37-000-801 57-42-37-400-801 12-22-27-991-004
Energize the Ground Service Network De-energize the Ground Service Network Extension of the Flaps on the Ground Retraction of the Flaps on the Ground Extension of the Slats on the Ground Retraction of the Slats on the Ground Removal of the Access Panels and Covers Installation of the Access Panels and Covers Removal of the Access Panels and Covers Installation of the Access Panels and Covers Fig. 304
3. __________ Job Set-up Subtask 12-22-27-860-052 A. Aircraft Maintenance Configuration (1) Fully extend the flaps (Ref. TASK 27-50-00-866-801). (2) Fully extend the slats (Ref. TASK 27-80-00-866-801). (3) Put the WARNING NOTICE in position on panel 114VU to tell persons not to operate the flap/slat controls. (4) Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER on the flap/slat control lever on panel 114VU. (5) Energize the ground service network (Ref. TASK 24-42-00-861-801).
EFF : ALL 12-22-27 SROS
Page 323 Jan 01/06
Subtask 12-22-27-865-056 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM AVAIL 10CW X13 722VU SFCC 2 SLAT 2CW V40 742VU SFCC 1 SLAT 1CW L62 Subtask 12-22-27-010-064 C. Get Access (1) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position. (2) Remove the access panels (Ref. TASK 57-41-37-000-801) 57-42-37-000-801): - in the Zone 521: 521BB, 521CB, 521GB, 521JB, - in the Zone 522: 522CB, 522TB, 522GB, 522HB, 522JB, 522RB, - in the Zone 523: 523CB, 523EB, 523GB, 523JB, 523LB, - in the Zone 621: 621BB, 621CB, 621GB, 621JB, - in the Zone 622: 622CB, 622TB, 622GB, 622HB, 622JB, 622RB, - in the Zone 623: 623CB, 623EB, 623GB, 623JB, 623LB,
and (Ref. TASK 522LB, 522NB, 523NB, 622LB, 622NB, 623NB.
4. Procedure _________ (Ref. Fig. 304/TASK 12-22-27-991-004) Subtask 12-22-27-640-053 A. Lubrication of all the Slat Track Roller Bearings, the Pinion Bearings, the Rack and Pinion Teeth, including the Slat Track 2 and 3 Lever Bearings WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Clean the grease nipples with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003).
R EFF : ALL 12-22-27 SROS
Page 324 Jul 01/06
R R
Slat Track Rollers and Pinions Figure 304/TASK 12-22-27-991-004
EFF : ALL 12-22-27 SROS
Page 325 Jul 01/06
INTENTIONALLY BLANK
R 12-22-27 SROS
Page 326 Jul 01/06
(2) Apply COMMON GREASE (Material No. 04-022) to: - the slat track roller bearings, - the pinion bearings, - the rack and pinion teeth and - the slat track 2 and track 3 lever bearings through the grease nipples until the new grease comes out. (3) Remove the unwanted grease from the greasing points. 5. Close-up ________ Subtask 12-22-27-410-054 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access 57-42-37-400-801): - in the Zone 521: - in the Zone 522: 522RB, - in the Zone 523: - in the Zone 621: - in the Zone 622: 622RB, - in the Zone 623:
panels (Ref. TASK 57-41-37-400-801) and (Ref. TASK 521BB, 521CB, 521GB, 521JB, 522CB, 522TB, 522GB, 522HB, 522JB, 522LB, 522NB, 523CB, 523EB, 523GB, 523JB, 523LB, 523NB, 621BB, 621CB, 621GB, 621JB, 622CB, 622TB, 622GB, 622HB, 622JB, 622LB, 622NB, 623CB, 623EB, 623GB, 623JB, 623LB, 623NB.
Subtask 12-22-27-865-057 B. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1CW, 2CW, 10CW Subtask 12-22-27-860-053 C. Put the Aircraft back to its Initial Configuration (1) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever on panel 114VU. (2) Retract the slats (Ref. TASK 27-80-00-866-802). R
(3) Retract the flaps (Ref. TASK 27-50-00-866-802).
R
(4) Remove the warning notice(s).
EFF : ALL 12-22-27 SROS
Page 327 Apr 01/04
R
(5) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
R EFF : ALL 12-22-27 SROS
Page 328 Apr 01/04
TASK 12-22-27-640-805 Lubrication of all Spoiler Linkage Bearings fitted with Grease Nipples WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Refer to the MPD TASK: 276400-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific No specific 98D27603002001 98D27803000000
circuit breaker(s) safety clip(s) 1 WARNING NOTICE 1 SPOILER MAINTENANCE KEY 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
EFF : ALL 12-22-27 SROS
Page 329 Jan 01/05
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R
Material No. 04-004 Material No. 19-003
USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 27-50-00-866-801 27-50-00-866-802 27-60-00-866-801 27-60-00-866-802 27-64-00-710-801 29-00-00-864-804 12-22-27-991-005
Energize the Ground Service Network De-energize the Ground Service Network Extension of the Flaps on the Ground Retraction of the Flaps on the Ground Extension of the Spoilers for Maintenance Retraction of the Spoilers after Maintenance Operational Test of the Spoilers Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Fig. 305
3. __________ Job Set-up Subtask 12-22-27-860-058 A. Aircraft Maintenance Configuration (1) Extend the flaps (Ref. TASK 27-50-00-866-801). (2) Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER on the slat/flap control lever on the panel 114VU. (3) Make sure that the aircraft hydraulic systems are depressurized (Ref. TASK 29-00-00-864-804). (4) Energize the ground service network (Ref. TASK 24-42-00-861-801).
EFF : ALL 12-22-27 SROS
Page 330 Jul 01/04
(5) Put the WARNING NOTICE in position in the cockpit to tell persons not to operate the flight controls. Subtask 12-22-27-865-058 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU FCPC3 STBY COM 7CE6 R20 721VU FCPC3 STBY MON 7CE5 R19 722VU FCDC 2 6CE2 T42 722VU FCSC 2 10CE2 T39 722VU FCPC 3 7CE3 V42 722VU FCPC 2 NORM 7CE2 V41 722VU FCPC 3 7CE4 V38 742VU FCSC 1 NORM 10CE1 C70 742VU FCPC 1 NORM 7CE1 C69 742VU FCSC 1 STBY 9CE G77 742VU FCPC 1 STBY 11CE K69 742VU FCDC 1 6CE1 L76 Subtask 12-22-27-860-067 C. Aircraft Maintenance Configuration (1) Extend the spoilers (Ref. TASK 27-60-00-866-801). R
(2) Install the SPOILER MAINTENANCE KEY (98D27603002001). 4. Procedure _________ (Ref. Fig. 305/TASK 12-22-27-991-005) Subtask 12-22-27-640-054 A. Lubrication of all Spoiler Linkage Bearings fitted with Grease Nipples WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Clean the grease nipples with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003).
EFF : ALL 12-22-27 SROS
Page 331 Apr 01/04
R
Spoiler Hinge Bearings Figure 305/TASK 12-22-27-991-005
EFF : ALL 12-22-27 SROS
Page 332 Jul 01/04
R R
(2) Apply the COMMON GREASE (Material No. 04-004) to the spoiler hinge bearings through the grease nipples until the new grease comes out. (3) Remove the unwanted grease from the greasing points. 5. Close-up ________ Subtask 12-22-27-860-059 A. Put the Aircraft back to its Initial Configuration (1) Remove the SPOILER MAINTENANCE KEY (98D27603002001). (2) Retract the spoilers (Ref. TASK 27-60-00-866-802). (3) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the slat/flap control lever on the panel 114VU. (4) Retract the flaps (Ref. TASK 27-50-00-866-802). (5) Remove the warning notice(s). Subtask 12-22-27-865-059 B. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CE1, 6CE2, 7CE1, 7CE2, 7CE3, 7CE4, 7CE5, 7CE6, 9CE, 10CE1, 10CE2, 11CE. Subtask 12-22-27-710-050 C. Do the operational test of the spoilers (Ref. TASK 27-64-00-710-801). Subtask 12-22-27-860-062 D. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-22-27 SROS
Page 333 Jul 01/04
TASK 12-22-27-640-806 Lubrication of Flap Steady Bearings WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Refer to the MPD TASK: 275400-08 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific No specific No specific 98D27803000000
circuit breaker(s) safety clip(s) 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 WARNING NOTICE 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
EFF : ALL 12-22-27 SROS
Page 334 Jan 01/05
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 04-022 Material No. 04-024 Material No. 19-003
USA MIL-PRF-81322 SYNTHE.HYDROCARBON GREASE HIGH PRESSURE (Ref. 20-31-00) AIB AIMS 09-06-001 SYNTHETIC GREASE FOR FLAP & SLAT MECHANISM (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 27-50-00-866-801 27-50-00-866-802 27-80-00-866-801 27-80-00-866-802 12-22-27-991-006-A
Energize the Ground Service Network De-energize the Ground Service Network Extension of the Flaps on the Ground Retraction of the Flaps on the Ground Extension of the Slats on the Ground Retraction of the Slats on the Ground Fig. 306
3. __________ Job Set-up Subtask 12-22-27-860-060 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). (2) Fully extend the flaps (Ref. TASK 27-50-00-866-801). (3) Fully extend the slats (Ref. TASK 27-80-00-866-801). (4) Put the WARNING NOTICE in position on panel 114VU to tell persons not to operate the flap/slat controls. (5) Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER on the flap/slat control lever on panel 114VU.
EFF : ALL 12-22-27 SROS
Page 335 Jan 01/06
Subtask 12-22-27-865-060 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM 10CV X14 722VU SFCC 2 FLAP 2CV T43 742VU SFCC 1 FLAP 1CV L61 Subtask 12-22-27-010-060 C. Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position. 4. Procedure _________ (Ref. Fig. 306/TASK 12-22-27-991-006-A) Subtask 12-22-27-640-055 A. Lubrication of the Flap Steady Bearings WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Clean the grease nipples with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003). (2) Apply COMMON GREASE (Material No. 04-022) or COMMON GREASE (Material No. 04-024) to the steady bearings through the grease nipples until the new grease comes out. (3) Remove the unwanted grease from the greasing points. 5. Close-up ________ Subtask 12-22-27-865-061 A. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1CV, 2CV, 10CV.
EFF : ALL 12-22-27 R SROS
Page 336 Oct 01/03
Flap/Slat Steady Bearings Figure 306/TASK 12-22-27-991-006-A EFF : ALL 12-22-27 R SROS
Page 337 Oct 01/03
Subtask 12-22-27-860-061 B. Put the Aircraft back to its Initial Configuration (1) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever on panel 114VU. R
(2) Retract the slats (Ref. TASK 27-80-00-866-802).
R
(3) Retract the flaps (Ref. TASK 27-50-00-866-802). Subtask 12-22-27-410-055 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Remove the warning notice(s). (3) Remove the access platform(s). (4) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-22-27-860-063 D. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-22-27 SROS
Page 338 Apr 01/04
TASK 12-22-27-640-807 Lubrication of the Aileron Hinge Bearings WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Refer to the MPD TASK: 271400-04 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific No specific No specific 98F27108438000
circuit breaker(s) safety clip(s) 1 ACCESS PLATFORM 5M (16 FT) 1 WARNING NOTICE 4 DISTANCE COLLAR - AILERON
EFF : ALL 12-22-27 SROS
Page 339 Jan 01/05
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 04-022 Material No. 19-003
USA MIL-PRF-81322 SYNTHE.HYDROCARBON GREASE HIGH PRESSURE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 29-00-00-864-804 12-22-27-991-007
Energize the Ground Service Network De-energize the Ground Service Network Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Fig. 307
3. __________ Job Set-up Subtask 12-22-27-860-064 A. Aircraft Maintenance Configuration (1) Make sure that the aircraft hydraulic systems are depressurized (Ref. TASK 29-00-00-864-804). (2) Energize the ground service network (Ref. TASK 24-42-00-861-801). (3) Put the WARNING NOTICE in position in the cockpit to tell persons not to operate the flight controls.
EFF : ALL 12-22-27 SROS
Page 340 Jan 01/06
Subtask 12-22-27-865-062 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------722VU FCDC 2 6CE2 T42 722VU FCSC 2 10CE2 T39 722VU FCPC 3 7CE3 V42 722VU FCPC 2 NORM 7CE2 V41 722VU FCPC 3 7CE4 V38 742VU FCSC 1 NORM 10CE1 C70 742VU FCPC 1 NORM 7CE1 C69 742VU FCSC 1 STBY 9CE G77 742VU FCPC 1 STBY 11CE K69 742VU FCDC 1 6CE1 L76 Subtask 12-22-27-010-063 C. Get Access R R
(1) Put the ACCESS PLATFORM 5M (16 FT) in position below the inboard aileron. (2) Remove the applicable access panels: - For the left inboard aileron, access panels 575AB, 575BB, 591AB, 591BB, 591CB, 591DB, 575AT. - For the right inboard aileron, access panels 675AB, 675BB, 691AB, 691BB, 691CB, 691DB, 675AT. - For the left outboard aileron, access panels 575CB, 575DB, 592AB, 592BB, 592CB, 592DB, 575BT. - For the right outboard aileron, access panels 675CB, 675DB, 692AB, 692BB, 692CB, 692DB, 675BT.
R R R R
(3) Move the trailing edge of the inboard and outboard ailerons up and install the DISTANCE COLLAR - AILERON (98F27108438000) on the aileron servo controls.
R R
EFF : ALL 12-22-27 SROS
Page 341 Oct 01/04
4. Procedure _________ (Ref. Fig. 307/TASK 12-22-27-991-007) Subtask 12-22-27-640-056 A. Lubrication of all Aileron Hinge Bearings WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Clean the grease nipples with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003). (2) Apply COMMON GREASE (Material No. 04-022) to the aileron hinge bearings through the grease nipples until the new grease comes out. (3) Remove the unwanted grease from the greasing points. 5. Close-up ________ Subtask 12-22-27-410-059 A. Close Access R R
(1) Remove the DISTANCE COLLAR - AILERON (98F27108438000) from the aileron servo controls. (2) Install the applicable access panels: - For the left inboard aileron, access panels 575AB, 575BB, 591AB, 591BB, 591CB, 591DB, 575AT. - For the right inboard aileron, access panels 675AB, 675BB, 691AB, 691BB, 691CB, 691DB, 675AT. - For the left outboard aileron, access panels 575CB, 575DB, 592AB, 592BB, 592CB, 592DB, 575BT. - For the right outboard aileron, access panels 675CB, 675DB, 692AB, 692BB, 692CB, 692DB, 675BT.
R R R R
Subtask 12-22-27-865-063 B. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CE1, 6CE2, 7CE1, 7CE2, 7CE3, 7CE4, 9CE, 10CE1, 10CE2, 11CE.
EFF : ALL 12-22-27 SROS
Page 342 Oct 01/04
Aileron Hinge Bearings Figure 307/TASK 12-22-27-991-007 EFF : ALL 12-22-27 R SROS
Page 343 Oct 01/03
Subtask 12-22-27-410-056 C. Close Access (1) Remove the warning notice(s). (2) Remove the access platform(s). (3) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-22-27-860-065 D. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-22-27 R SROS
Page 344 Oct 01/03
TASK 12-22-27-640-808 Lubrication of Slat Rotary Actuator Type A (Track 2-3) WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Refer to the MPD TASK: 278000-05 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific 98D27803000000
circuit breaker(s) safety clip(s) 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 WARNING NOTICE 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
EFF : ALL 12-22-27 R SROS
Page 345 Jan 01/07
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R
Material No. 04-004 Material No. 04-022 Material No. 04-024 Material No. 19-003
USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) USA MIL-PRF-81322 SYNTHE.HYDROCARBON GREASE HIGH PRESSURE (Ref. 20-31-00) AIB AIMS 09-06-001 SYNTHETIC GREASE FOR FLAP & SLAT MECHANISM (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R
24-42-00-861-801 24-42-00-862-801 27-80-00-866-801 27-80-00-866-802 57-41-37-000-801 57-41-37-400-801 57-42-37-000-801 57-42-37-400-801 SIL 12-008
Energize the Ground Service Network De-energize the Ground Service Network Extension of the Slats on the Ground Retraction of the Slats on the Ground Removal of the Access Panels and Covers Installation of the Access Panels and Covers Removal of the Access Panels and Covers Installation of the Access Panels and Covers (for corrective action)
**ON A/C ALL Post SB Post SB
27-3077 For A/C 401-449, 27-3100 For A/C ALL
12-22-27-991-008
Fig. 308
EFF : ALL 12-22-27 SROS
Page 346 Jan 01/07
**ON A/C ALL 3. __________ Job Set-up R
**ON A/C ALL
R
Post SB
27-3100 For A/C ALL
Subtask 12-22-27-860-066 A. Aircraft Maintenance Configuration (1) Fully extend the slats (Ref. TASK 27-80-00-866-801). (2) Put the WARNING NOTICE in position on panel 114VU to tell persons not to operate the flap/slat controls. (3) Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER on the flap/slat control lever on panel 114VU. (4) Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-22-27-865-064 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM AVAIL 10CW X13 722VU SFCC 2 SLAT 2CW V40 742VU SFCC 1 SLAT 1CW L62 R R
Subtask 12-22-27-010-066-A C. Get Access
R
(1) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position.
R R R R
(2) Remove the access panels (Ref. TASK 57-41-37-000-801) and (Ref. TASK 57-42-37-000-801): - in the Zone 521: 521DB, 521GB, - in the Zone 621: 621DB, 621GB,
EFF : ALL 12-22-27 SROS
Page 347 Jan 01/06
**ON A/C ALL 4. Procedure _________ **ON A/C ALL Post SB Post SB
27-3077 For A/C 401-449, 27-3100 For A/C ALL
(Ref. Fig. 308/TASK 12-22-27-991-008) Subtask 12-22-27-640-057-A A. Lubrication of the Slat Rotary Actuators Type A R (1) Lubrication of the Slat Rotary Actuators (Type A) on Slat Track 2 and 3 PN: 954A0000-03, 954A0000-04, 954B0000-02, 954C0000-01 and subsequent versions
R R R R R
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE _______ THIS/THESE MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES.
R R R R R R R R R R R R R R R
CAUTION : WHEN YOU DO A MAINTENANCE TASK THAT USES COMMON GREASE, _______ OBEY THESE PRECAUTIONS: - IF POSSIBLE, USE ONLY GREASES OF THE SAME SPECIFICATION TYPE (IT IS PERMITTED TO USE DIFFERENT BRANDS IF THE SPECIFICATION TYPE IS THE SAME). WE SPECIALLY RECOMMEND THAT YOU DO NOT MIX GREASES THAT HAVE CLAY THICKENERS WITH GREASES THAT HAVE LITHIUM THICKENERS. SUCH A MIXTURE CAN CHANGE THE LUBRICATION PROPERTIES OF THE GREASE. - IF YOU CANNOT OBEY THESE PRECAUTIONS AND YOU USE GREASES OF DIFFERENT TYPES (SPECIALLY THOSE WITH CLAY THICKENERS AND LITHIUM THICKENERS), DECREASE THE SERVICING INTERVALS (BY HALF, FOR EXAMPLE) SPECIFIED IN THE MAINTENANCE PLANNING DOCUMENT. DO THIS FOR APPROXIMATELY THREE OR FOUR SERVICES (REFER TO YOUR IN-SERVICE DATA TO FIND THE NUMBER OF SERVICES BEST ADAPTED TO AIRCRAFT). NOTE : It is not permitted to apply grease again to the slat rotary ____ actuators (Type A) PN: 954A0000-01, 954A0000-02, 954B0000-01. (a) Clean the grease nipple (1) of the rotary actuator with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003).
EFF : ALL 12-22-27 SROS
Page 348 Jan 01/07
R R
Slat Rotary Actuator Type A Figure 308/TASK 12-22-27-991-008
R EFF : ALL 12-22-27 SROS
Page 349 Jan 01/06
R R R R
(b) Apply the COMMON GREASE (Material No. 04-022), or the COMMON GREASE (Material No. 04-024), or the COMMON GREASE (Material No. 04-004) to the grease nipple (1). For the correct type of grease to use, refer to the the SIL (Ref. SIL 12-008). (c) Make sure that the new grease comes out of the actuator vent valve (2). (d) Remove the unwanted grease from the grease nipple (1) and the actuator vent valve (2). **ON A/C ALL 5. Close-up ________ **ON A/C ALL Post SB
27-3100 For A/C ALL
Subtask 12-22-27-410-057-A A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels (Ref. TASK 57-41-37-400-801) and (Ref. TASK 57-42-37-400-801): - in the Zone 521: 521DB, 521GB, - in the Zone 621: 621DB, 621GB, Subtask 12-22-27-865-065 B. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1CW, 2CW, 10CW. Subtask 12-22-27-860-068 C. Put the Aircraft back to its Initial Configuration (1) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever on panel 114VU. (2) Retract the slats (Ref. TASK 27-80-00-866-802).
EFF : ALL 12-22-27 SROS
Page 350 Jan 01/07
(3) Remove the access platform(s). (4) Remove the warning notice(s). (5) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-22-27 R SROS
Page 351 Jan 01/07
**ON A/C ALL TASK 12-22-27-640-815 Lubrication of Slat Rotary Actuator Type B (Track 5-16) WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Refer to the MPD TASK: 278000-07 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No
specific specific specific specific
98D27803000000 98F20008247000
circuit breaker(s) safety clip(s) 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 WARNING NOTICE Torque Wrench : range 0.00 to 1.20 m.daN (0.00 to 9.00 lbf.ft) 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER 1 QUANTITY LIMITER - REGREASING
EFF : ALL 12-22-27 R SROS
Page 352 Jan 01/07
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R
Material No. 04-004 Material No. 04-022 Material No. 04-024
USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) USA MIL-PRF-81322 SYNTHE.HYDROCARBON GREASE HIGH PRESSURE (Ref. 20-31-00) AIB AIMS 09-06-001 SYNTHETIC GREASE FOR FLAP & SLAT MECHANISM (Ref. 20-31-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------3
O-ring
27-84-49 01 -020
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R
24-42-00-861-801 24-42-00-862-801 27-80-00-866-801 27-80-00-866-802 57-41-37-000-801 57-41-37-400-801 57-42-37-000-801 57-42-37-400-801 SIL 12-008
Energize the Ground Service Network De-energize the Ground Service Network Extension of the Slats on the Ground Retraction of the Slats on the Ground Removal of the Access Panels and Covers Installation of the Access Panels and Covers Removal of the Access Panels and Covers Installation of the Access Panels and Covers (for corrective action)
**ON A/C 001-001, 201-205, 251-252, 255-299, 401-449, 12-22-27-991-013-A
Fig. 309
EFF : ALL 12-22-27 SROS
Page 353 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------**ON A/C 002-049, 206-249, 301-399, 401-449, 451-499, 701-749, Post SB
27-3077 For A/C 401-449,
12-22-27-991-013
Fig. 309A
**ON A/C ALL 3. __________ Job Set-up Subtask 12-22-27-860-080 A. Aircraft Maintenance Configuration (1) Fully extend the slats (Ref. TASK 27-80-00-866-801). (2) Put the WARNING NOTICE in position on panel 114VU to tell persons not to operate the flap/slat controls. (3) Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER on the flap/slat control lever on panel 114VU. (4) Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-22-27-865-078 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM AVAIL 10CW X13 722VU SFCC 2 SLAT 2CW V40 742VU SFCC 1 SLAT 1CW L62
EFF : ALL 12-22-27 R SROS
Page 354 Jan 01/07
Subtask 12-22-27-010-075 C. Get Access (1) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position. (2) Remove the access panels (Ref. TASK 57-41-37-000-801) 57-42-37-000-801): - In the Zone 522: 522CB, 522TB, 522JB, 522LB, 522NB, - In the Zone 523: 523CB, 523EB, 523GB, 523JB, 523LB, - In the Zone 622: 622CB, 622TB, 622JB, 622LB, 622NB, - In the Zone 623: 623CB, 623EB, 623GB, 623JB, 623LB,
R R R R
and (Ref. TASK 522RB 523NB 622RB 623NB.
4. Procedure _________ **ON A/C 001-001, 201-205, 251-252, 255-299, 401-449, (Ref. Fig. 309/TASK 12-22-27-991-013-A) **ON A/C 002-049, 206-249, 301-399, 401-449, 451-499, 701-749, Post SB
27-3077 For A/C 401-449,
(Ref. Fig. 309A/TASK 12-22-27-991-013) **ON A/C 001-001, 201-205, 251-252, 255-299, 401-449, Subtask 12-22-27-640-064-A R
A. Lubrication of all Slat Rotary Actuators (Type B) Track 5 thru 16 WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES.
R EFF : ALL 12-22-27 SROS
Page 355 Jan 01/07
Slat Rotary Actuator Type B Figure 309/TASK 12-22-27-991-013-A R EFF : 001-001, 201-205, 251-252, 255-299, 12-22-27 401-449, SROS
Page 356 Jan 01/07
Slat Rotary Actuator Type B Figure 309A/TASK 12-22-27-991-013 R EFF : 002-049, 206-249, 301-399, 401-449, 12-22-27 451-499, 701-749, SROS
Page 357 Jan 01/07
R R R R R R R R R R R R R R R
CAUTION : WHEN YOU DO A MAINTENANCE TASK THAT USES COMMON GREASE, OBEY _______ THESE PRECAUTIONS: - IF POSSIBLE, USE ONLY GREASES OF THE SAME SPECIFICATION TYPE (IT IS PERMITTED TO USE DIFFERENT BRANDS IF THE SPECIFICATION TYPE IS THE SAME). WE SPECIALLY RECOMMEND THAT YOU DO NOT MIX GREASES THAT HAVE CLAY THICKENERS WITH GREASES THAT HAVE LITHIUM THICKENERS. SUCH A MIXTURE CAN CHANGE THE LUBRICATION PROPERTIES OF THE GREASE. - IF YOU CANNOT OBEY THESE PRECAUTIONS AND YOU USE GREASES OF DIFFERENT TYPES (SPECIALLY THOSE WITH CLAY THICKENERS AND LITHIUM THICKENERS), DECREASE THE SERVICING INTERVALS (BY HALF, FOR EXAMPLE) SPECIFIED IN THE MAINTENANCE PLANNING DOCUMENT. DO THIS FOR APPROXIMATELY THREE OR FOUR SERVICES (REFER TO YOUR IN-SERVICE DATA TO FIND THE NUMBER OF SERVICES BEST ADAPTED TO AIRCRAFT).
R R R R
(1) Fill the QUANTITY LIMITER - REGREASING with the COMMON GREASE (Material No. 04-022), or the COMMON GREASE (Material No. 04-024), or the COMMON GREASE (Material No. 04-004). For the correct type of grease to use, refer to the SIL (Ref. SIL 12-008).
R R
NOTE : Step 1 is only applicable when you fill the quantity limiter ____ (5) and the hose (1) for the first time.
R R R
(a) Remove the hose (1) from the quantity limiter (5). Connect the grease gun to the quantity limiter on the same side as the piston. (b) Operate the grease gun until the piston of the quantity limiter (5) is at the opposite end of the chamber.
R R
(c) Make sure that the chamber of the quantity limiter (5) is full with grease.
R R
(d) Remove the grease gun from the quantity limiter (5). Install it on the opposite side and connect the hose (1) to the quantity limiter (5). (e) Operate the grease gun until the piston of the quantity limiter (5) is at the opposite end of the chamber.
R R
(f) Make sure that the chamber of the quantity limiter (5) is full with grease.
R
(g) Make sure that the new grease comes out of the adapter (4). If not, do the steps (a) thru (f) again as necessary.
R EFF : 001-001, 201-205, 251-252, 255-299, 12-22-27 401-449, SROS
Page 358 Jan 01/07
(h) Interchange the grease gun and the hose (1) at the quantity limiter (5). R R
NOTE : The hose (1), the quantity limiter (5) and the adapter (4) ____ are part of the QUANTITY LIMITER - REGREASING (98F20008247000). (2) Lubricate the Slat Rotary Actuator
R R
(a) Remove the plug (2) and the O-ring (3) from the rotary actuator and install the adapter (4) on the rotary actuator. (b) Operate the grease gun until the piston of the quantity limiter (5) is at the opposite end of the chamber. (c) Remove the adapter (4) of the QUANTITY LIMITER - REGREASING from the rotary actuator. (d) Remove the O-ring (3) from the plug (2) and install the new Oring (3) on the plug (2). (e) Install the plug (2) on the rotary actuator. (f) TORQUE the plug (2) to between 0.4 and 0.6 m.daN (35.39 and 53.09 lbf.in). (g) Interchange the grease gun and the hose (1) at the quantity limiter (5).
R R
(h) Make sure that the chamber of the quantity limiter (5) is full with grease.
R
(i) Repeat the steps (a) thru (h) for each rotary actuator. **ON A/C 002-049, 206-249, 301-399, 451-499, 701-749, Subtask 12-22-27-640-064
R
A. Lubrication of all Slat Rotary Actuators (Type B) Track 5 thru 16 WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-22-27 301-399, 401-449, 451-499, 701-749, SROS
Page 359 Jan 01/07
R R R R R R R R R R R R R R R
CAUTION : WHEN YOU DO A MAINTENANCE TASK THAT USES COMMON GREASE, OBEY _______ THESE PRECAUTIONS: - IF POSSIBLE, USE ONLY GREASES OF THE SAME SPECIFICATION TYPE (IT IS PERMITTED TO USE DIFFERENT BRANDS IF THE SPECIFICATION TYPE IS THE SAME). WE SPECIALLY RECOMMEND THAT YOU DO NOT MIX GREASES THAT HAVE CLAY THICKENERS WITH GREASES THAT HAVE LITHIUM THICKENERS. SUCH A MIXTURE CAN CHANGE THE LUBRICATION PROPERTIES OF THE GREASE. - IF YOU CANNOT OBEY THESE PRECAUTIONS AND YOU USE GREASES OF DIFFERENT TYPES (SPECIALLY THOSE WITH CLAY THICKENERS AND LITHIUM THICKENERS), DECREASE THE SERVICING INTERVALS (BY HALF, FOR EXAMPLE) SPECIFIED IN THE MAINTENANCE PLANNING DOCUMENT. DO THIS FOR APPROXIMATELY THREE OR FOUR SERVICES (REFER TO YOUR IN-SERVICE DATA TO FIND THE NUMBER OF SERVICES BEST ADAPTED TO AIRCRAFT).
R R R R
(1) Fill the quantity limiter (3) with the COMMON GREASE (Material No. 04-022), or the COMMON GREASE (Material No. 04-024), or the COMMON GREASE (Material No. 04-004). For the correct type of grease to use, refer to the SIL (Ref. SIL 12-008). NOTE : The step 1 is only applicable when you fill the quantity ____ limiter (3) and the hose (4) for the first time.
R R
NOTE : The hose (4), the quantity limiter (3) and the adapter (2) are ____ part of the QUANTITY LIMITER - REGREASING. (a) Remove the hose (4) from the quantity limiter (3). Connect the grease gun to the quantity limiter (3) on the same side as the piston. (b) Operate the grease gun until the piston of the quantity limiter (3) is at the opposite end of the chamber. (c) Make sure that the chamber of the quantity limiter (3) is full with grease. (d) Remove the grease gun from the quantity limiter (3). (e) Install the grease gun on the opposite side and connect the hose (4) to the quantity limiter (3). (f) Operate the grease gun until the piston of the quantity limiter (3) is at the opposite end of the chamber. (g) Make sure that the chamber of the quantity limiter (3) is full with grease.
R EFF : 002-049, 206-249, 301-399, 451-499, 12-22-27 701-749, SROS
Page 360 Jan 01/07
(h) Make sure that the new grease comes out of the adapter (2). If not, do the steps (a) thru (g) again as necessary.
R
(i) Interchange the grease gun and the hose (4) at the quantity limiter (3). (2) Lubricate the Slat Rotary Actuator (a) Remove the plug (1) from the rotary actuator and install the adapter (2) on the rotary actuator. (b) Operate the grease gun until the piston of the quantity limiter (3) is at the opposite end of the chamber. (c) Remove the adapter (2) from the rotary actuator. (d) Install the plug (1) on the rotary actuator. (e) TORQUE the plug (1) to between 0.4 and 0.6 m.daN (35.39 and 53.09 lbf.in). (f) Interchange the grease gun and the hose (4) at the quantity limiter (3). (g) Make sure that the chamber of the quantity limiter (3) is full with grease. R
(h) Do the steps (a) thru (g) again for each rotary actuator. **ON A/C 001-001, 201-205, 251-252, 255-299, Post SB
27-3100 For A/C 001-001,201-205,251-252,255-299,
Subtask 12-22-27-640-064-C R
A. Lubrication of all Slat Rotary Actuators (Type B) Track 5 thru 16 WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-22-27 301-399, 451-499, 701-749, SROS
Page 361 Jan 01/07
R R R R R R R R R R R R R R R
CAUTION : WHEN YOU DO A MAINTENANCE TASK THAT USES COMMON GREASE, OBEY _______ THESE PRECAUTIONS: - IF POSSIBLE, USE ONLY GREASES OF THE SAME SPECIFICATION TYPE (IT IS PERMITTED TO USE DIFFERENT BRANDS IF THE SPECIFICATION TYPE IS THE SAME). WE SPECIALLY RECOMMEND THAT YOU DO NOT MIX GREASES THAT HAVE CLAY THICKENERS WITH GREASES THAT HAVE LITHIUM THICKENERS. SUCH A MIXTURE CAN CHANGE THE LUBRICATION PROPERTIES OF THE GREASE. - IF YOU CANNOT OBEY THESE PRECAUTIONS AND YOU USE GREASES OF DIFFERENT TYPES (SPECIALLY THOSE WITH CLAY THICKENERS AND LITHIUM THICKENERS), DECREASE THE SERVICING INTERVALS (BY HALF, FOR EXAMPLE) SPECIFIED IN THE MAINTENANCE PLANNING DOCUMENT. DO THIS FOR APPROXIMATELY THREE OR FOUR SERVICES (REFER TO YOUR IN-SERVICE DATA TO FIND THE NUMBER OF SERVICES BEST ADAPTED TO AIRCRAFT).
R R R R
(1) Fill the quantity limiter (5) with the COMMON GREASE (Material No. 04-022) or the COMMON GREASE (Material No. 04-024), or the COMMON GREASE (Material No. 04-004). For the correct type of grease to use, refer to the SIL (Ref. SIL 12-008).
R R
NOTE : Step 1 is only applicable when you fill the quantity limiter ____ (5) and the hose (1) for the first time.
R R
NOTE : The hose (1), the quantity limiter (5) and the adapter (4) are ____ part of the QUANTITY LIMITER - REGREASING. (a) Remove the hose (1) from the quantity limiter (5). Connect the grease gun to the quantity limiter (5) on the same side as the piston. (b) Operate the grease gun until the piston of the quantity limiter (5) is at the opposite end of the chamber. (c) Make sure that the chamber of the quantity limiter (5) is full with grease. (d) Remove the grease gun from the quantity limiter (5). (e) Install the grease gun on the opposite side and connect the hose (1) to the quantity limiter (5). (f) Operate the grease gun until the piston of the quantity limiter (5) is at the opposite end of the chamber. (g) Make sure that the chamber of the quantity limiter (5) is full with grease.
R EFF : 001-001, 201-205, 251-252, 255-299, 12-22-27 SROS
Page 362 Jan 01/07
(h) Make sure that the new grease comes out of the adapter (4). If not, do the steps (a) thru (g) again as necessary.
R
(i) Interchange the grease gun and the hose (1) at the quantity limiter (5). (2) Lubricate the Slat Rotary Actuator R R
(a) Remove the plug (2) and the O-ring (3) from the rotary actuator and install the adapter (4) on the rotary actuator. (b) Operate the grease gun until the piston of the quantity limiter (6) is at the opposite end of the chamber. (c) Remove the adapter (4) of the QUANTITY LIMITER - REGREASING from the rotary actuator. (d) Remove the O-ring (3) from the plug (2) and install the new Oring (3) on the plug (2). (e) Install the plug (2) on the rotary actuator. (f) TORQUE the plug (2) to between 0.4 and 0.6 m.daN (35.39 and 53.09 lbf.in). (g) Interchange the grease gun and the hose (1) at the quantity limiter (5). (h) Make sure that the chamber of the quantity limiter (5) is full with grease.
R
(i) Do the steps (a) thru (h) again for each rotary actuator. **ON A/C 002-049, 206-249, 301-399, 401-449, 451-499, 701-749, Post SB Post SB
27-3077 For A/C 401-449, 27-3100 For A/C 002-049,206-249,301-399,401-449,451-499,701-749,
Subtask 12-22-27-640-064-B R
A. Lubrication of all Slat Rotary Actuators (Type B) Track 5 thru 16 WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-22-27 301-399, 401-449, 451-499, 701-749, SROS
Page 363 Jan 01/07
R R R R R R R R R R R R R R R
CAUTION : WHEN YOU DO A MAINTENANCE TASK THAT USES COMMON GREASE, OBEY _______ THESE PRECAUTIONS: - IF POSSIBLE, USE ONLY GREASES OF THE SAME SPECIFICATION TYPE (IT IS PERMITTED TO USE DIFFERENT BRANDS IF THE SPECIFICATION TYPE IS THE SAME). WE SPECIALLY RECOMMEND THAT YOU DO NOT MIX GREASES THAT HAVE CLAY THICKENERS WITH GREASES THAT HAVE LITHIUM THICKENERS. SUCH A MIXTURE CAN CHANGE THE LUBRICATION PROPERTIES OF THE GREASE. - IF YOU CANNOT OBEY THESE PRECAUTIONS AND YOU USE GREASES OF DIFFERENT TYPES (SPECIALLY THOSE WITH CLAY THICKENERS AND LITHIUM THICKENERS), DECREASE THE SERVICING INTERVALS (BY HALF, FOR EXAMPLE) SPECIFIED IN THE MAINTENANCE PLANNING DOCUMENT. DO THIS FOR APPROXIMATELY THREE OR FOUR SERVICES (REFER TO YOUR IN-SERVICE DATA TO FIND THE NUMBER OF SERVICES BEST ADAPTED TO AIRCRAFT).
R R R R
(1) Fill the quantity limiter (3) with the COMMON GREASE (Material No. 04-022), or the COMMON GREASE (Material No. 04-024), or the COMMON GREASE (Material No. 04-004). For the correct type of grease to use, refer to the SIL (Ref. SIL 12-008).
R R
NOTE : Step 1 is only applicable when you fill the quantity limiter ____ (3) and the hose (4) for the first time.
R R
NOTE : The hose (4), the quantity limiter (3) and the adapter (2) are ____ part of the QUANTITY LIMITER - REGREASING. (a) Remove the hose (4) from the quantity limiter (3). Connect the grease gun to the quantity limiter (3) on the same side as the piston. (b) Operate the grease gun until the piston of the quantity limiter (3) is at the opposite end of the chamber. (c) Make sure that the chamber of the quantity limiter (3) is full with grease. (d) Remove the grease gun from the quantity limiter (3). (e) Install the grease gun on the opposite side and connect the hose (4) to the quantity limiter (3). (f) Operate the grease gun until the piston of the quantity limiter (3) is at the opposite end of the chamber. (g) Make sure that the chamber of the quantity limiter (3) is full with grease.
R EFF : 002-049, 206-249, 301-399, 401-449, 12-22-27 451-499, 701-749, SROS
Page 364 Jan 01/07
(h) Make sure that the new grease comes out of the adapter (2). If not, do the steps (a) thru (g) again as necessary.
R
(i) Interchange the grease gun and the hose (4) at the quantity limiter (3). (2) Lubricate the Slat Rotary Actuator (a) Remove the plug (1) from the rotary actuator and install the adapter (2) on the rotary actuator. (b) Operate the grease gun until the piston of the quantity limiter (3) is at the opposite end of the chamber. (c) Remove the adapter (2) of the QUANTITY LIMITER - REGREASING from the rotary actuator. (d) Install the plug (1) on the rotary actuator. (e) TORQUE the plug (1) to between 0.4 and 0.6 m.daN (35.39 and 53.09 lbf.in). (f) Interchange the grease gun and the hose (4) at the quantity limiter (3). (g) Make sure that the chamber of the quantity limiter (3) is full with grease. R
(h) Do the steps (a) thru (g) again for each rotary actuator. **ON A/C ALL 5. Close-up ________ Subtask 12-22-27-410-068 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access 57-42-37-400-801): - In the Zone 522: - In the Zone 523: - In the Zone 622:
R R R
panels (Ref. TASK 57-41-37-400-801) and (Ref. TASK 522CB, 522TB, 522JB, 522LB, 522NB, 522RB 523CB, 523EB, 523GB, 523JB, 523LB, 523NB 622CB, 622TB, 622JB, 622LB, 622NB, 622RB
EFF : ALL 12-22-27 SROS
Page 365 Jan 01/07
R
- In the Zone 623: 623CB, 623EB, 623GB, 623JB, 623LB, 623NB. Subtask 12-22-27-865-079 B. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1CW, 2CW, 10CW. Subtask 12-22-27-860-081 C. Put the Aircraft back to its Initial Configuration (1) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever on panel 114VU. (2) Retract the slats (Ref. TASK 27-80-00-866-802). (3) Remove the access platform(s). (4) Remove the warning notice(s). (5) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-22-27 SROS
Page 366 Jan 01/07
TASK 12-22-27-640-810 Lubrication of Rudder Servo-Control Roller-Bearings (Rudder Side) WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Refer to the MPD TASK: 272400-06 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific 98F27207514000
circuit breaker(s) safety clip(s) warning notice(s) 1 ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE 1 PIN - RIGGING
EFF : ALL 12-22-27 R SROS
Page 367 Jan 01/07
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 04-004 Material No. 19-003
USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 27-21-00-840-801 29-00-00-863-801 29-00-00-863-802 29-00-00-863-803 29-00-00-864-801 29-00-00-864-802 29-00-00-864-803 55-33-13-000-801 55-33-13-400-801 12-22-27-991-010
Energize the Aircraft Electrical Circuits from the External Power A Removal/Installation of the Control Rod on the Rudder Mechanical control Pressurize the Green Hydraulic System with the Electric Pump Pressurize the Blue Hydraulic System with the Electric Pump Pressurize the Yellow Hydraulic System with the Electric Pump Depressurize the Green Hydraulic System (Pressurized with the Electric Pump) Depressurize the Blue Hydraulic System (Pressurized with the Electric Pump) Depressurize the Yellow Hydraulic System (Pressurized with the Electric Pump) Removal of the Vertical-Stabilizer Trailing-Edge Access-Panels Installation of the Vertical-Stabilizer Trailing-Edge Access-Panels Fig. 310
EFF : ALL 12-22-27 R SROS
Page 368 Jan 01/07
3. __________ Job Set-up Subtask 12-22-27-869-050 A. To do this task outside the hangar during wind gusts, refer to the removal/installation of the control rod on the rudder mechanical control (Ref. TASK 27-21-00-840-801). Refer again to the above mentioned task to install the control rod at the end of this procedure. Subtask 12-22-27-010-069 B. Get Access (1) Put the ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE in position at the rudder leading-edge. (2) Remove the trailing-edge access-panels 325NL (Ref. TASK 55-33-13-000801). Subtask 12-22-27-860-071 C. Aircraft Maintenance Configuration (Ref. Fig. 310/TASK 12-22-27-991-010) (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) On the FLT CTL section of the overhead panel 241VU, make sure that the PRIM 1 and SEC 1 pushbutton switches are pushed (the OFF and FAULT legends of these pushbutton switches are off). (3) On the FLT CTL section of the overhead panel 212VU, make sure that the PRIM 2, PRIM 3 and SEC 2 pushbutton switches are pushed (the OFF and FAULT legends of these pushbutton switches are off). (4) Pressurize the aircraft hydraulic systems (Ref. TASK 29-00-00-863-801), (Ref. TASK 29-00-00-863-802) and (Ref. TASK 29-00-00-863-803). (5) Put the rudder pedals in the neutral position. (6) Make sure that the RUD TRIM control switch on the panel 115VU is set to the neutral position. (7) Make sure that the RUD TRIM indicator on the panel 115VU shows 0.
EFF : ALL 12-22-27 R SROS
Page 369 Jan 01/07
Rudder Servo Control Figure 310/TASK 12-22-27-991-010 EFF : ALL 12-22-27 R SROS
Page 370 Jan 01/07
(8) Install the PIN - RIGGING (98F27207514000) A in the bellcrank assembly of the servo control actuator 5002CY3. (9) Depressurize the aircraft hydraulic systems (Ref. TASK 29-00-00-864-801), (Ref. TASK 29-00-00-864-802) and (Ref. TASK 29-00-00-864-803). (10) Put the warning notice(s) in position in the cockpit to tell persons: - not to operate the flight controls, - not to pressurize the aircraft hydraulic systems. Subtask 12-22-27-865-076 D. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU FCPC3 STBY COM 7CE6 R20 721VU FCPC3 STBY MON 7CE5 R19 722VU FCDC 2 6CE2 T42 722VU FCSC 2 10CE2 T39 722VU FCPC 3 7CE3 V42 722VU FCPC 2 NORM 7CE2 V41 722VU FCPC 3 7CE4 V38 742VU FCSC 1 NORM 10CE1 C70 742VU FCPC 1 NORM 7CE1 C69 742VU FCSC 1 STBY 9CE G77 742VU FCPC 1 STBY 11CE K69 742VU FCDC 1 6CE1 L76 4. Procedure _________ (Ref. Fig. 310/TASK 12-22-27-991-010) Subtask 12-22-27-640-059 A. Lubrication of the Rudder Servo-Control Tailstock Roller-Bearings (Rudder Side) WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Clean the grease nipples with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003).
EFF : ALL 12-22-27 R SROS
Page 371 Jan 01/07
(2) Apply COMMON GREASE (Material No. 04-004) to the roller bearings through the grease nipples until the new grease comes out. (3) Remove the unwanted grease from the greasing points. 5. Close-up ________ Subtask 12-22-27-865-077 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CE1, 6CE2, 7CE1, 7CE2, 7CE3, 7CE4, 7CE5, 7CE6, 9CE, 10CE1, 10CE2, 11CE. Subtask 12-22-27-860-072 B. Put the Aircraft back to its Initial Configuration (1) Pressurize the Green hydraulic system (Ref. TASK 29-00-00-863-801). (2) On the FLT CTL section of the overhead panel 241VU, make sure that the PRIM 1 and SEC 1 pushbutton switches are pushed (the OFF and FAULT legends of these pushbutton switches are off). (3) Remove the PIN - RIGGING (98F27207514000) A from the bellcrank assembly of the servo control actuator 5002CY3. (4) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (5) Make sure that the work area is clean and clear of tools and other items. Subtask 12-22-27-410-063 C. Close Access (1) Install the trailing-edge access-panel 325NL (Ref. TASK 55-33-13-400801). (2) Remove the access platform(s). (3) Remove the warning notice(s).
EFF : ALL 12-22-27 R SROS
Page 372 Jan 01/07
TASK 12-22-27-640-811 Lubrication of the Aileron Actuator Roller Bearings WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Refer to the MPD TASK: 271400-05 NOTE : This Task is applicable only for aileron actuators which have ____ installed grease nipples at the actuator eye-end. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific 98D27903500000
circuit breaker(s) safety clip(s) 1 ACCESS PLATFORM 5M (16 FT) 1 WARNING NOTICE 2 PIN-SIDE STICK LOCKING
EFF : ALL 12-22-27 R SROS
Page 373 Jan 01/07
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 04-004 Material No. 19-003
USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-804 12-22-27-991-011
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Fig. 311
3. __________ Job Set-up Subtask 12-22-27-860-073 A. Aircraft Maintenance Configuration (1) Make sure that the aircraft hydraulic systems are depressurized (Ref. TASK 29-00-00-864-804). (2) Put the WARNING NOTICE in position to tell persons: - not to pressurize the hydraulic systems, - not to pressurize the hydraulic reservoirs. (3) Install the PIN-SIDE STICK LOCKING in the capt and F/O side stick. (4) Put a warning notice in the cockpit to tell persons not to operate the flight controls.
EFF : ALL 12-22-27 R SROS
Page 374 Jan 01/07
Subtask 12-22-27-865-070 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU FCPC3 STBY COM 7CE6 R20 721VU FCPC3 STBY MON 7CE5 R19 722VU FCDC 2 6CE2 T42 722VU FCSC 2 10CE2 T39 722VU FCPC 3 7CE3 V42 722VU FCPC 2 NORM 7CE2 V41 722VU FCPC 3 7CE4 V38 742VU FCSC 1 NORM 10CE1 C70 742VU FCPC 1 NORM 7CE1 C69 742VU FCSC 1 STBY 9CE G77 742VU FCPC 1 STBY 11CE K69 742VU FCDC 1 6CE1 L76 Subtask 12-22-27-010-071 C. Get Access (1) Put the ACCESS PLATFORM 5M (16 FT) in position below the applicable aileron. (2) Remove the applicable access panels: - FOR 7CS1, 8CS1 remove 575AB, - FOR 7CS2, 8CS2 remove 675AB, - FOR 9CS1, 10CS1 remove 575CB, - FOR 9CS2, 10CS2 remove 675CB.
EFF : ALL 12-22-27 R SROS
Page 375 Jan 01/07
4. Procedure _________ (Ref. Fig. 311/TASK 12-22-27-991-011) Subtask 12-22-27-640-060 A. Lubrication of the Aileron Servo-Control Roller-Bearings WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Clean the grease nipples with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003). (2) Apply COMMON GREASE (Material No. 04-004) with maximum 10 Lbs/min. to the roller bearings through the grease nipples until the new grease comes out. (3) Remove the unwanted grease from the greasing points. 5. Close-up ________ Subtask 12-22-27-410-064 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the applicable access panels: - FOR 7CS1, 8CS1 install 575AB, - FOR 7CS2, 8CS2 install 675AB, - FOR 9CS1, 10CS1 install 575CB, - FOR 9CS2, 10CS2 install 675CB. (3) Remove the access platform(s). Subtask 12-22-27-865-071 B. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CE1, 6CE2, 7CE1, 7CE2, 7CE3, 7CE4, 7CE5, 7CE6, 9CE, 10CE1, 10CE2, 11CE.
EFF : ALL 12-22-27 R SROS
Page 376 Jan 01/07
ASC Roller Bearings Figure 311/TASK 12-22-27-991-011 EFF : ALL 12-22-27 R SROS
Page 377 Jan 01/07
Subtask 12-22-27-860-074 C. Remove the PIN-SIDE STICK LOCKING from the capt and F/O side stick.
EFF : ALL 12-22-27 R SROS
Page 378 Jan 01/07
TASK 12-22-27-640-813 Lubrication of Slat Steady Bearings WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Refer to the MPD TASK: 278000-06 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific 98D27803000000
circuit breaker(s) safety clip(s) 1 ACCESS PLATFORM 2M (6 FT) 1 WARNING NOTICE 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
EFF : ALL 12-22-27 R SROS
Page 379 Jan 01/07
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 04-022 Material No. 04-024 Material No. 19-003
USA MIL-PRF-81322 SYNTHE.HYDROCARBON GREASE HIGH PRESSURE (Ref. 20-31-00) AIB AIMS 09-06-001 SYNTHETIC GREASE FOR FLAP & SLAT MECHANISM (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 27-80-00-866-801 27-80-00-866-802 53-35-13-000-802 53-35-13-400-802 57-41-37-000-801 57-41-37-400-801 57-42-37-000-801 57-42-37-400-801 12-22-27-991-006-A
Energize the Ground Service Network De-energize the Ground Service Network Extension of the Slats on the Ground Retraction of the Slats on the Ground Removal of the Belly Fairing Access Panels Installation of the Belly Fairing Access Panels Removal of the Access Panels and Covers Installation of the Access Panels and Covers Removal of the Access Panels and Covers Installation of the Access Panels and Covers Fig. 306
3. __________ Job Set-up Subtask 12-22-27-860-075 A. Aircraft Maintenance Configuration (1) Fully extend the slats (Ref. TASK 27-80-00-866-801). (2) Put the WARNING NOTICE in position on panel 114VU to tell persons not to operate the flap/slat controls. (3) Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER on the flap/slat control lever on panel 114VU.
EFF : ALL 12-22-27 R SROS
Page 380 Jan 01/07
(4) Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-22-27-865-072 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM AVAIL 10CW X13 722VU SFCC 2 SLAT 2CW V40 742VU SFCC 1 SLAT 1CW L62 Subtask 12-22-27-010-073-A C. Get Access (1) Put the ACCESS PLATFORM 2M (6 FT) in position. (2) Remove the applicable access panels (Ref. TASK 53-35-13-000-802), (Ref. TASK 57-41-37-000-801) or (Ref. TASK 57-42-37-000-801): - FOR 5003CW, 5005CW remove 193DB, - FOR 5017CW remove 521BB, - FOR 5023CW remove 522AB, - FOR 5025CW remove 522BB, - FOR 5031CW remove 522HB, - FOR 5066CW remove 523CB, - FOR 5077CW remove 621BB, - FOR 5083CW remove 622AB, - FOR 5085CW remove 622BB, - FOR 5091CW remove 622HB, - FOR 5126CW remove 623CB.
EFF : ALL 12-22-27 R SROS
Page 381 Jan 01/07
4. Procedure _________ (Ref. Fig. 306/TASK 12-22-27-991-006-A) Subtask 12-22-27-640-061 A. Lubrication of the Slat Steady Bearings WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Clean the grease nipples with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003). (2) Apply COMMON GREASE (Material No. 04-022) or COMMON GREASE (Material No. 04-024) to the steady bearings through the grease nipples until the new grease comes out. (3) Remove the unwanted grease from the greasing points. 5. Close-up ________ Subtask 12-22-27-865-073 A. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1CW, 2CW, 10CW. Subtask 12-22-27-860-076 B. Put the Aircraft back to its Initial Configuration (1) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever on panel 114VU. (2) Retract the slats (Ref. TASK 27-80-00-866-802). (3) Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER on the flap/slat control lever on panel 114VU.
EFF : ALL 12-22-27 R SROS
Page 382 Jan 01/07
Subtask 12-22-27-410-066-A C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panel (Ref. TASK 53-35-13-400-802), (Ref. TASK 5741-37-400-801) or (Ref. TASK 57-42-37-400-801): - FOR 5003CW, 5005CW install 193DB, - FOR 5017CW install 521BB, - FOR 5023CW install 522AB, - FOR 5025CW install 522BB, - FOR 5031CW install 522HB, - FOR 5066CW install 523CB, - FOR 5077CW install 621BB, - FOR 5083CW install 622AB, - FOR 5085CW install 622BB, - FOR 5091CW install 622HB, - FOR 5126CW install 623CB. (3) Remove the warning notice(s). (4) Remove the access platform(s). (5) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL 12-22-27 R SROS
Page 383 Jan 01/07
Subtask 12-22-27-860-077 D. Put the Aircraft back to its Initial Configuration (1) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever on panel 114VU. (2) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-22-27 R SROS
Page 384 Jan 01/07
TASK 12-22-27-640-814 Lubrication of the Elevator Actuator Roller Bearings WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Refer to the MPD TASK: 273400-06 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific 98D27903500000
circuit breaker(s) safety clip(s) 1 ACCESS PLATFORM 6M (20 FT) 1 WARNING NOTICE 2 PIN-SIDE STICK LOCKING
EFF : ALL 12-22-27 R SROS
Page 385 Jan 01/07
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 04-004 Material No. 19-003
USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-804 55-13-11-000-801 55-13-11-400-801
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Removal of the Trailing-Edge Access Panels Installation of the Trailing-Edge Access Panels
**ON A/C ALL Post SB
27-3076 For A/C 001-049,201-210,251-252,255-299,301-399,401-449, 451-499,701-749,
12-22-27-991-012
Fig. 312
EFF : ALL 12-22-27 R SROS
Page 386 Jan 01/07
**ON A/C ALL 3. __________ Job Set-up **ON A/C ALL Post SB
27-3076 For A/C 001-049,201-210,251-252,255-299,301-399,401-449, 451-499,701-749,
Subtask 12-22-27-860-078 A. Aircraft Maintenance Configuration (1) Make sure that the aircraft hydraulic systems are depressurized (Ref. TASK 29-00-00-864-804). (2) Put the WARNING NOTICE in position to tell persons: - not to pressurize the hydraulic systems, - not to pressurize the hydraulic reservoirs. (3) Install the PIN-SIDE STICK LOCKING in the capt and F/O side stick. (4) Put a warning notice in the cockpit to tell persons not to operate the flight controls. Subtask 12-22-27-865-074 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU FCPC3 STBY COM 7CE6 R20 721VU FCPC3 STBY MON 7CE5 R19 722VU FCDC 2 6CE2 T42 722VU FCSC 2 10CE2 T39 722VU FCPC 3 7CE3 V42 722VU FCPC 2 NORM 7CE2 V41 722VU FCPC 3 7CE4 V38 742VU FCSC 1 NORM 10CE1 C70 742VU FCPC 1 NORM 7CE1 C69 742VU FCSC 1 STBY 9CE G77 742VU FCPC 1 STBY 11CE K69 742VU FCDC 1 6CE1 L76
EFF : ALL 12-22-27 R SROS
Page 387 Jan 01/07
Subtask 12-22-27-010-074 C. Get Access (1) Put the ACCESS PLATFORM 6M (20 FT) in position and open the trailing-edge access panels 334CB, 344CB (Ref. TASK 55-13-11-000801). **ON A/C ALL 4. Procedure _________ **ON A/C ALL Post SB
27-3076 For A/C 001-049,201-210,251-252,255-299,301-399,401-449, 451-499,701-749,
(Ref. Fig. 312/TASK 12-22-27-991-012) Subtask 12-22-27-640-062 A. Lubrication of the Elevator Servo-Control Roller-Bearings WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Clean the grease nipples with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003). (2) Apply COMMON GREASE (Material No. 04-004) with maximum 10 Lbs/min. to the roller bearings through the grease nipples until the new grease comes out. (3) Remove the unwanted grease from the greasing points.
EFF : ALL 12-22-27 SROS
Page 388 Jan 01/07
Elevator Actuator Roller-Bearings Figure 312/TASK 12-22-27-991-012 EFF : ALL 12-22-27 SROS
Page 389 Jan 01/07
**ON A/C ALL 5. Close-up ________ **ON A/C ALL Post SB
27-3076 For A/C 001-049,201-210,251-252,255-299,301-399,401-449, 451-499,701-749,
Subtask 12-22-27-410-067 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the trailing-edge access panel 334CB, 344CB (Ref. TASK 55-1311-400-801). (3) Remove the PIN-SIDE STICK LOCKING from the capt and F/O side stick. (4) Remove all the fixtures, tools, test and support equipment used during this procedure. Subtask 12-22-27-865-075 B. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CE1, 6CE2, 7CE1, 7CE2, 7CE3, 7CE4, 7CE5, 7CE6, 9CE, 10CE1, 10CE2, 11CE.
EFF : ALL 12-22-27 SROS
Page 390 Jan 01/07
LANDING GEAR - SERVICING ________________________ TASK 12-22-32-600-817 Lubrication of Main Landing Gear and Doors WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED ON THE _______ LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. R R R R R R R R R
WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL MATERIALS _______ ONLY WITH A GOOD FLOW OF AIR THROUGH THE WORK AREA. THESE MATERIALS ARE POISONOUS AND FLAMMABLE AND SKIN IRRITANTS. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. 1. __________________ Reason for the Job
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Refer to the MPD TASK: 321000-03 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No
specific specific specific specific
circuit breaker(s) safety clip(s) 1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE 1 LUBRICATING EQUIPMENT 1 WARNING NOTICE
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B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 04-022 Material No. 05-047
USA MIL-PRF-81322 SYNTHE.HYDROCARBON GREASE HIGH PRESSURE (Ref. 20-31-00) C Z-11.904 ANTI COR. COMPOUND(HIGH TEMP.SILICONE SEALANT) (Ref. 20-31-00)
Material No. 11-024 Material No. 11-026 Material No. 19-003 Material No. 19-010
CLEANING AGENT, ALKALINE-WATERBASED. (Ref. 20-31-00) GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00) USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------1 1
O-ring O-ring
32-11-11 73 -070 32-11-11 73 -070A
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-801 R R R
32-00-00-860-804 32-00-00-860-805 32-12-00-010-801 32-12-00-410-801 12-22-32-991-037
Depressurize the Green Hydraulic System (Pressurized with the Electric Pump) Flight Configuration Precautions Ground Configuration after Flight Configuration Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Fig. 301
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
**ON A/C 001-049, 201-210, 251-252, 255-299, 301-399, 401-449, 451-499,
R
12-22-32-991-005
R
**ON A/C ALL
R R R
Post SB
R
12-22-32-991-005-B
R
**ON A/C ALL
R R R
12-22-32-991-038 12-22-32-991-041 12-22-32-991-042
R
**ON A/C ALL
R
Post SB
R
12-22-32-991-042-A
R
**ON A/C ALL
R R
12-22-32-991-043 12-22-32-991-013
Post SB
Fig. 302
32-3125 For A/C 001-049,201-210,251-252,255-299,301-399,401-449, 451-499, 32-3141 For A/C ALL Fig. 302A
Fig. 303 Fig. 304 Fig. 305
32-3138 For A/C ALL Fig. 305A
Fig. 306 Fig. 307
3. __________ Job Set-up Subtask 12-22-32-941-067 A. Safety Precautions R (1) In the cockpit, on the panel 312VU: - make sure that the landing gear lever (6GA) is in the DOWN position - put a WARNING NOTICE in the cockpit to tell persons not to operate the landing gear lever.
EFF : ALL 12-22-32 SROS
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Subtask 12-22-32-860-078 B. Aircraft Maintenance Configuration (1) Make sure that the Green hydraulic system is depressurized (Ref. TASK 29-00-00-864-801). R R
(2) Do the flight configuration precautions (Ref. TASK 32-00-00-860-804). Subtask 12-22-32-865-068
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C. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU HYD PUMP G CTL 9JV U09 722VU LGCIU 2 2GA U38 742VU LGCIU 1 1GA L63
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Subtask 12-22-32-010-071 D. Get Access (Ref. Fig. 301/TASK 12-22-32-991-037)
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(1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position adjacent to the applicable MLG leg.
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(2) Open the MLG doors (Ref. TASK 32-12-00-010-801).
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(3) Remove and discard the lockwire from the bolts (5).
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(4) Remove the bolts (5) and the washers (4).
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(5) Remove the bracket (3) and the cover (2).
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(6) Remove and discard the O-ring (1).
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(7) Cut, remove and discard the lockwire from the bolts (6).
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(8) Remove the bolts (6) and the cover (7).
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MLG-Greasing Point Access Figure 301/TASK 12-22-32-991-037
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Page 305 Jul 01/06
Subtask 12-22-32-110-054 E. Preparation of Equipment (1) Make sure that the LUBRICATING EQUIPMENT is in the correct condition before you use it. (2) Operate the LUBRICATING EQUIPMENT to make sure that the lines and adaptors are full of new lubricant. R R R
(3) Clean the greasers with the clean cloth MISCELLANEOUS (Material No. 19-003) and CLEANING AGENTS (Material No. 11-026). 4. Procedure _________
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**ON A/C 001-049, 201-210, 251-252, 255-299, 301-399, 401-449, 451-499, (Ref. Fig. 302/TASK 12-22-32-991-005)
R
**ON A/C ALL
R R R
Post SB
R R R
Post SB
32-3125 For A/C 001-049,201-210,251-252,255-299,301-399,401-449, 451-499, 32-3141 For A/C ALL
(Ref. Fig. 302A/TASK 12-22-32-991-005-B) **ON A/C ALL (Ref. Fig. 303/TASK 12-22-32-991-038, 304/TASK 12-22-32-991-041, 305/TASK 12-22-32-991-042)
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**ON A/C ALL
R
Post SB
R R R
32-3138 For A/C ALL
(Ref. Fig. 305A/TASK 12-22-32-991-042-A) **ON A/C ALL (Ref. Fig. 306/TASK 12-22-32-991-043, 307/TASK 12-22-32-991-013)
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Page 306 Jul 01/06
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Shortening Mechanism - Lubrication Points Figure 302/TASK 12-22-32-991-005
EFF : 001-049, 201-210, 251-252, 255-299, 12-22-32 301-399, 401-449, 451-499, SROS
Page 307 Jul 01/06
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Shortening Mechanism - Lubrication Points Figure 302A/TASK 12-22-32-991-005-B
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INTENTIONALLY BLANK
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MLG - Shortening Mechanism - Lubrication Points Figure 303/TASK 12-22-32-991-038- 12 (SHEET 1)
EFF : ALL 12-22-32 SROS
Page 310 Jul 01/06
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MLG - Shortening Mechanism - Lubrication Points Figure 303/TASK 12-22-32-991-038- 22 (SHEET 2)
EFF : ALL 12-22-32 SROS
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MLG Lubrication Points Location Figure 304/TASK 12-22-32-991-041- 16 (SHEET 1)
EFF : ALL 12-22-32 SROS
Page 312 Jan 01/07
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MLG Lubrication Points Location Figure 304/TASK 12-22-32-991-041- 26 (SHEET 2)
EFF : ALL 12-22-32 SROS
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MLG Lubrication Points Location Figure 304/TASK 12-22-32-991-041- 36 (SHEET 3)
EFF : ALL 12-22-32 SROS
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MLG Lubrication Points Location Figure 304/TASK 12-22-32-991-041- 46 (SHEET 4)
EFF : ALL 12-22-32 SROS
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MLG Lubrication Points Location Figure 304/TASK 12-22-32-991-041- 56 (SHEET 5)
EFF : ALL 12-22-32 SROS
Page 316 Jan 01/07
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MLG Lubrication Points Location Figure 304/TASK 12-22-32-991-041- 66 (SHEET 6)
EFF : ALL 12-22-32 SROS
Page 317 Jan 01/07
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MLG Greaser location Figure 305/TASK 12-22-32-991-042
EFF : ALL 12-22-32 SROS
Page 318 Jul 01/06
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MLG Greaser location Figure 305A/TASK 12-22-32-991-042-A
EFF : ALL 12-22-32 SROS
Page 319 Jul 01/06
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MLG Lubrication Points Location Figure 306/TASK 12-22-32-991-043
EFF : ALL 12-22-32 SROS
Page 320 Jul 01/06
INTENTIONALLY BLANK
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Page 321 Jul 01/06
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MLG Uplock, Door Uplock Units and Pins - Lubrication Points Figure 307/TASK 12-22-32-991-013- 12 (SHEET 1)
EFF : ALL 12-22-32 SROS
Page 322 Jan 01/07
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MLG Uplock, Door Uplock Units and Pins - Lubrication Points Figure 307/TASK 12-22-32-991-013- 22 (SHEET 2)
EFF : ALL 12-22-32 SROS
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**ON A/C 001-049, 201-210, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 12-22-32-640-084 A. Lubrication of the MLG Shortening Mechanism -------------------------------------------------------------------| SHORTENING MECHANISM | |--------------------------------------------------------------------| | No.| Component/Location |Total| Position of Greasers | |----|--------------------|-----|------------------------------------| | 1 | Pintle Pin | 3 | 3 on the pin. | | | Connection | | | | | View A | | | |----|--------------------|-----|------------------------------------| | 2 | Adjustable Link | 3 | 2 on the body of the link | | | View B | | (Lubricate only one). | | | | | 1 on the adjustable links | | | | | spherical bearing eye-end and | | | | | bellcrank interface. | |----|--------------------|-----|------------------------------------| | 3 | Bellcrank | 3 | 2 on the bellcrank lever. | | | View C | | 1 on the bellcrank link bearing/ | | | | | bellcrank bearing joint. | |----|--------------------|-----|------------------------------------| | 4 | Bellcrank | 1 | 1 on the pivot pin. | |----|--------------------|-----|------------------------------------| | 5 | Link Sub-Assy | 2 | 2 on the link body. | | | View D | | | |----|--------------------|-----|------------------------------------| | 6 | Upper Link Pin | 4 | 2 on each end of the pivot pin | | | View E | | (Lubricate only one greaser on | | | | | each end of the pin). | |----|--------------------|-----|------------------------------------| | 7 | Upper Link | 4 | 4 on the link body | | | View E | | (Access through change over | | | | | valve access hole) | |----|--------------------|-----|------------------------------------| | 8 | Lower Link | 4 | 4 on the link body. | | | View E | | (Access through change over | | | | | valve access hole) | |----|--------------------|-----|------------------------------------| | 9 | Shock Absorber | 6 | 2 on each lug on the top surface | | | View F | | (Lubricate only one greaser on | | | | | each lug). | | | | | (Access through change over |
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R R R R R R R R R R R R R R R R R R R R
R EFF : 001-049, 201-210, 251-252, 255-299, 12-22-32 301-399, 401-449, 451-499, SROS
Page 324 Jul 01/06
-------------------------------------------------------------------| SHORTENING MECHANISM | |--------------------------------------------------------------------| | No.| Component/Location |Total| Position of Greasers | |----|--------------------|-----|------------------------------------| | | | | valve access hole). | --------------------------------------------------------------------
R
(1) Lubricate the greasers with COMMON GREASE (Material No. 04-022) until the new grease comes out. Use the table above, to find the greasers. NOTE : The grease gun pressure must be less than 3000 psi (200 bar). ____ (2) Remove the unwanted grease. R R
(3) Clean the greasers with a clean cloth MISCELLANEOUS (Material No. 19003) and CLEANING AGENTS (Material No. 11-026). **ON A/C ALL Post SB
32-3125 For A/C 001-049,201-210,251-252,255-299,301-399,401-449, 451-499,
Subtask 12-22-32-640-084-A A. Lubrication of the MLG Shortening Mechanism -------------------------------------------------------------------| SHORTENING MECHANISM | |--------------------------------------------------------------------| | No.| Component/Location |Total| Position of Greasers | |----|--------------------|-----|------------------------------------| | 1 | Pintle Pin | 3 | 3 on the pin. | | | Connection | | | | | View A | | | |----|--------------------|-----|------------------------------------| | 2 | Adjustable Link | 3 | 2 on the body of the link | | | View B | | (Lubricate only one). | | | | | 1 on the adjustable links | | | | | spherical bearing eye-end and | | | | | bellcrank interface. | |----|--------------------|-----|------------------------------------| | 3 | Bellcrank | 4 | 2 on the bellcrank lever. | | | View C | | 1 on the bellcrank link bearing/ | | | | | bellcrank bearing joint. | | | | | 1 on the inboard bush in the main | | | | | fitting for the bellcrank. |
R R R
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EFF : ALL 12-22-32 SROS
Page 325 Jul 01/06
-------------------------------------------------------------------| SHORTENING MECHANISM | |--------------------------------------------------------------------| | No.| Component/Location |Total| Position of Greasers | |----|--------------------|-----|------------------------------------| |----|--------------------|-----|------------------------------------| | 4 | Bellcrank | 1 | 1 on the pivot pin. | |----|--------------------|-----|------------------------------------| | 5 | Link Sub-Assy | 2 | 2 on the link body. | | | View D | | | |----|--------------------|-----|------------------------------------| | 6 | Upper Link Pin | 4 | 2 on each end of the pivot pin | | | | | (Lubricate only one greaser on | | | | | each end of the pin). | |----|--------------------|-----|------------------------------------| | 7 | Upper Link | 4 | 4 on the link body. | | | View E | | (Access through change over | | | | | valve access hole). | | | | | | |----|--------------------|-----|------------------------------------| | 8 | Lower Link | 4 | 4 on the link body. | | | View E | | (Access through change over | | | | | valve access hole). | |----|--------------------|-----|------------------------------------| | 9 | Shock Absorber | 6 | 2 on each lug on the top surface | | | View F | | (Lubricate only one greaser on| | | | | | each lug). | | | | | (Access through change over | | | | | valve access hole). | --------------------------------------------------------------------
R R R R R R R R R R R R R R R R R R R
(1) Lubricate the greasers with COMMON GREASE (Material No. 04-022) until the new grease comes out. Use the table above, to find the greasers. NOTE : The grease gun pressure must be less than 3000 psi (200 bar). ____ (2) Remove the unwanted grease. R R
(3) Clean the greasers with a clean cloth MISCELLANEOUS (Material No. 19003) and CLEANING AGENTS (Material No. 11-026).
EFF : ALL 12-22-32 SROS
Page 326 Jul 01/06
R
**ON A/C ALL
R R R
Post SB
R
Subtask 12-22-32-640-084-B
R
Post SB
32-3125 For A/C 001-049,201-210,251-252,255-299,301-399,401-449, 451-499, 32-3141 For A/C ALL
A. Lubrication of the MLG Shortening Mechanism
R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R
-------------------------------------------------------------------| SHORTENING MECHANISM | |--------------------------------------------------------------------| | No.| Component/Location |Total| Position of Greasers | |----|--------------------|-----|------------------------------------| | 1 | Pintle Pin | 3 | 3 on the pin. | | | Connection | | | | | View A | | | |----|--------------------|-----|------------------------------------| | 2 | Adjustable Link | 3 | 2 on the body of the link | | | View B | | (Lubricate only one). | | | | | 1 on the adjustable links | | | | | spherical bearing eye-end and | | | | | bellcrank interface. | |----|--------------------|-----|------------------------------------| | 3 | Bellcrank | 4 | 2 on the bellcrank body. | | | View C | | 1 on the bellcrank link bearing/ | | | | | bellcrank bearing joint. | | | | | 1 on the inboard bush in the main | | | | | fitting for the bellcrank. | |----|--------------------|-----|------------------------------------| | 4 | Bellcrank | 1 | 1 on the pivot pin. | |----|--------------------|-----|------------------------------------| | 5 | Link Sub-Assy | 2 | 2 on the link body. | | | View D | | | |----|--------------------|-----|------------------------------------| | 6 | Upper Link Pin | 4 | 2 on each end of the pivot pin | | | | | (Lubricate only one greaser on | | | | | each end of the pin). | |----|--------------------|-----|------------------------------------| | 7 | Upper Link | 4 | 4 on the link body | | | View E | | (Access through change over | | | | | valve access hole). | |----|--------------------|-----|------------------------------------| | 8 | Lower Link | 4 | 4 on the link body | | | View E | | (Access through change over. | | | | | valve access hole). |
EFF : ALL 12-22-32 SROS
Page 327 Jul 01/06
-------------------------------------------------------------------| SHORTENING MECHANISM | |--------------------------------------------------------------------| | No.| Component/Location |Total| Position of Greasers | |----|--------------------|-----|------------------------------------| |----|--------------------|-----|------------------------------------| | 9 | Shock Absorber | 6 | 2 on each lug on the top surface | | | View F | | (Lubricate only one greaser on | | | | | each lug) | | | | | (Access through change over. | | | | | valve access hole). | --------------------------------------------------------------------(1) Lubricate the greasers with COMMON GREASE (Material No. 04-022) until the new grease comes out. Use the table above, to find the greasers. NOTE : The grease gun pressure must be less than 3000 psi (200 bar). ____ (2) Remove the unwanted grease. (3) Clean the greasers with a clean cloth MISCELLANEOUS (Material No. 19003) and CLEANING AGENTS (Material No. 11-026). **ON A/C ALL Subtask 12-22-32-640-085-B R
B. Lubrication of Main Gear -------------------------------------------------------------------| No.| Component/Location|Total| Position of Greasers | |----|-------------------|-----|-------------------------------------| | 10 | Rear Pintle | 10 | | |10A | View A | | 3 on the pintle pin greaser insert. | |10B | View A | | 2 on the eccentric pin. | |10C | View A | | 3 on the turnbuckle link upper pin. | |10D | View A | | 2 on the main fitting bearing. | |----|-------------------|-----|-------------------------------------| | 11 | Forward Pintle | 8 | | |11A | View B | | 4 on the fwd bearing (only the 2 | | | | | inboard greasers need to be | | | | | lubricated). | |11B | View B | | 3 on the pin greaser insert. | |11C | View B | | 1 on the strut/actuator bracket. | |----|-------------------|-----|-------------------------------------| | 12 | Intermediate Link | 9 | |
EFF : ALL 12-22-32 SROS
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-------------------------------------------------------------------| No.| Component/Location|Total| Position of Greasers | |----|-------------------|-----|-------------------------------------| |12A | View C | | 1 on the retraction link. | |12B | View C | | 3 on the retraction link/retraction | | | | | bracket attachment pin. | |12C | View C,M | | 3 on the attachment pin at the rear | | | | | spar/retraction link. | |12D | View C | | 2 on the retraction link fitting | | | | | bearing. | |----|-------------------|-----|-------------------------------------| | 13 | Retraction | 7 | | | | Actuator | | | |13A | View D | | 2 on the actuator ram eye end/ | | | | | retraction link attachment pin. | |13B | View D | | 1 on the actuator ram eye end. | |13C | View D | | 1 on the actuator cylinder eye end. | |13D | View D | | 3 on the actuator cylinder/main leg | | | | | attachment pin. | |----|-------------------|-----|-------------------------------------| | 14 | Lock Stay/Actuator| 28 | | |14A | View E | | 2 on the upper attachment pin. | |14B | View E | | 3 on the upper lock stay connector | | | | | link. | |14C | View E | | 1 on the upper lock stay eye end. | |14D | View E | | 1 on the upper lock stay eye end. | |14E | View E,N | | 8 on the lower lock stay. | |14F | View E | | 4 on the link pivot. | |14G | View E | | 2 on the connecting link. | |14H | View E | | 1 on the actuator ram eye end. | |14I | View E | | 4 on the actuator cylinder eye end. | |14J | View W | | 2 on the link pivot bracket. | |----|-------------------|-----|-------------------------------------| | 15 | Side Stay Assembly| 27 | | |15A | View F,V | | 4 on the bearings of the side stay | | | | | fitting on the rear spar. | |15B | View F | | 2 on the lower cardan lubrication | | | | | spool. | |15C | View F | | 2 on the upper side stay at the | | | | | lock stay attachment pin. | |15D | View F,R | | 8 1 at each end of the springs. | |15E | View F,R | | 1 on the actuator attachment bracket| |15F | View F,P | | 8 4 on the upper and lower cardan | | | | | attachment pins. | |15G | View F,Q | | 2 on the upper and lower lock stay | | | | | connection pin. | |----|-------------------|-----|-------------------------------------|
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EFF : ALL 12-22-32 SROS
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-------------------------------------------------------------------| No.| Component/Location|Total| Position of Greasers | |----|-------------------|-----|-------------------------------------| | 16 | Articulation Link | 22 | | | | Pitch Trimmer | | | |16A | View G | | 3 on the pitch trimmer/pivot link | | | | | attachment pin. | |16B | View G,S | | 1 on the pitch trimmer eye end. | |16C | View G | | 3 on the pivot pin/lower. | | | | | articulation link attachment pin. | |16D | View G | | 2 on the lower articulation link. | |16E | View G | | 3 on the lower articulation link/ | | | | | bogie attachment pin. | |16F | View G | | 4 2 on each end of the pitch trimmer| | | | | /main leg attachment pin. | |16G | View G | | 6 3 on each upper articulation link/| | | | | main leg attachment pin. | |----|-------------------|-----|-------------------------------------| | 17 | Shock Strut/ | 36 | | | | Bogie Beam | | | |17A | View H,U | | 2 on the shock strut/bogie beam | | | | | attachment. | |17A | View H,U | | 2 on the shock strut/brake rod | | | | | attachment. | |17B | View H | | 8 2 on each brake unit. | |17C | View H | | 2 on the bogie beam at the shock | | | | | strut /bogie beam attachment. | |17D | View H | | 2 on the lower torque link. | |17D | View H | | 2 on the lower torque link sleeve. | |17E | View H | | 2 on the torque link apex pin. | |17F | View H | | 2 on the upper torque link. | |17F | View H | | 2 on the upper torque link/main leg | | | | | attachment lugs. | |17G | View H,T | |12 3 on each brake rod. | R -------------------------------------------------------------------(1) Lubricate the greasers with COMMON GREASE (Material No. 04-022) until the new grease comes out. Use the table above, to find the greasers. NOTE : The grease pressure must be less than 3000 psi (207 bar). ____ (2) Remove the unwanted grease. (3) Clean the greasers with a clean cloth MISCELLANEOUS (Material No. 19003) and CLEANING AGENTS (Material No. 11-026).
EFF : ALL 12-22-32 SROS
Page 330 Jan 01/07
**ON A/C ALL Post SB
32-3138 For A/C ALL
Subtask 12-22-32-640-085-C R
B. Lubrication of Main Gear -------------------------------------------------------------------| No.| Component/Location|Total| Position of Greasers | |----|-------------------|-----|-------------------------------------| | 10 | Rear Pintle | 10 | | |10A | View A | | 3 on the pintle pin greaser insert. | |10B | View A | | 2 on the eccentric pin. | |10C | View A | | 3 on the turnbuckle link upper pin. | |10D | View A | | 2 on the main fitting bearing. | |----|-------------------|-----|-------------------------------------| | 11 | Forward Pintle | 8 | | |11A | View B | | 4 on the fwd bearing (only the 2 | | | | | inboard greasers need to be | | | | | lubricated). | |11B | View B | | 3 on the pin greaser insert. | |11C | View B | | 1 on the strut/actuator bracket. | |----|-------------------|-----|-------------------------------------| | 12 | Intermediate Link | 9 | | |12A | View C | | 1 on the retraction link. | |12B | View C | | 3 on the retraction link/retraction | | | | | bracket attachment pin. | |12C | View C,M | | 3 on the attachment pin at the rear | | | | | spar/retraction link. | |12D | View C | | 2 on the retraction link fitting | | | | | bearing. | |----|-------------------|-----|-------------------------------------| | 13 | Retraction | 7 | | | | Actuator | | | |13A | View D | | 2 on the actuator ram eye end/ | | | | | retraction link attachment pin. | |13B | View D | | 1 on the actuator ram eye end. | |13C | View D | | 1 on the actuator cylinder eye end. | |13D | View D | | 3 on the actuator cylinder/main leg | | | | | attachment pin. | |----|-------------------|-----|-------------------------------------| | 14 | Lock Stay/Actuator| 28 | | |14A | View E | | 2 on the upper attachment pin. | |14B | View E | | 3 on the upper lock stay connector | | | | | link. | |14C | View E | | 1 on the upper lock stay eye end. |
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Page 331 Jan 01/07
-------------------------------------------------------------------| No.| Component/Location|Total| Position of Greasers | |----|-------------------|-----|-------------------------------------| |14D | View E | | 1 on the upper lock stay eye end. | |14E | View E,N | | 8 on the lower lock stay. | |14F | View E | | 4 on the link pivot. | |14G | View E | | 2 on the connecting link. | |14H | View E | | 1 on the actuator ram eye end. | |14I | View E | | 4 on the actuator cylinder eye end. | |14J | View W | | 2 on the link pivot bracket. | |----|-------------------|-----|-------------------------------------| | 15 | Side Stay Assembly| 27 | | |15A | View F,V | | 4 on the bearings of the side stay | | | | | fitting on the rear spar. | |15B | View F | | 2 on the lower cardan lubrication | | | | | spool. | |15C | View F | | 2 on the upper side stay at the | | | | | lock stay attachment pin. | |15D | View F,R | | 8 1 at each end of the springs. | |15E | View F,R | | 1 on the actuator attachment bracket| |15F | View F,P | | 8 4 on the upper and lower cardan | | | | | attachment pins. | |15G | View F,Q | | 2 on the upper and lower lock stay | | | | | connection pin. | |----|-------------------|-----|-------------------------------------| | 16 | Articulation Link | 22 | | | | Pitch Trimmer | | | |16A | View G | | 3 on the pitch trimmer/pivot link | | | | | attachment pin. | |16B | View G,S | | 1 on the pitch trimmer eye end. | |16C | View G | | 3 on the pivot pin/lower | | | | | articulation link attachment pin. | |16D | View G | | 2 on the lower articulation link. | |16E | View G | | 3 on the lower articulation link/ | | | | | bogie attachment pin. | |16F | View G | | 4 2 on each end of the pitch trimmer| | | | | /main leg attachment pin. | |16G | View G | | 6 3 on each upper articulation link/| | | | | main leg attachment pin. | |----|-------------------|-----|-------------------------------------| | 17 | Shock Strut/ | 44 | | | | Bogie Beam | | | |17B | View H,U | | 2 on the shock strut/bogie beam | | | | | attachment. | |17A | View H,U | | 2 on the shock strut/brake rod | | | | | attachment. | |17B | View H | |16 4 on each brake unit. |
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-------------------------------------------------------------------| No.| Component/Location|Total| Position of Greasers | |----|-------------------|-----|-------------------------------------| |17C | View H | | 2 on the bogie beam at the shock | | | | | strut /bogie beam attachment. | |17D | View H | | 2 on the lower torque link. | |17D | View H | | 2 on the lower torque link sleeve. | |17E | View H | | 2 on the torque link apex pin. | |17F | View H | | 2 on the upper torque link. | |17F | View H | | 2 on the upper torque link/main leg | | | | | attachment lugs. | |17G | View H,T | |12 3 on each brake rod. | R -------------------------------------------------------------------(1) Lubricate the greasers with COMMON GREASE (Material No. 04-022) until the new grease comes out. Use the table above, to find the greasers. NOTE : The grease pressure must be less than 3000 psi (207 bar). ____ (2) Remove the unwanted grease. (3) Clean the greasers with a clean cloth MISCELLANEOUS (Material No. 19003) and CLEANING AGENTS (Material No. 11-026). **ON A/C ALL Subtask 12-22-32-640-086 R R
C. Lubrication of the MLG Uplock, the Door Uplock Unit, the Door Hinges and Actuator -------------------------------------------------------------------| No.| Component/Location|Total| Position of Greasers | |----|-------------------|-----|-------------------------------------| | 18 | Main Door | 5 | | |18A | Actuator | | 2 1 on the upper and lower eye end. | | | | | NOTE: Do not apply grease to the | | | | | attachment bolt greasers. | |18B | Hinges | | 3 1 on each door hinge bolt. | |----|-------------------|-----|-------------------------------------| | 19 | MLG Uplock | 4 | | |19A | View A | | 2 on each side of the casing. | |----|-------------------|-----|-------------------------------------| | 20 | MLG Door Uplock | 4 | | |20A | View B | | 2 on each side of the casing. |
R R R R R R R R R R R R R
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-------------------------------------------------------------------| No.| Component/Location|Total| Position of Greasers | |----|-------------------|-----|-------------------------------------| |----|-------------------|-----|-------------------------------------| | 21 | Door Uplock Roller| 1 | | |21A | View D | | 1 on the roller attachment pin. | --------------------------------------------------------------------
R R R
(1) Lubricate the greasers with COMMON GREASE (Material No. 04-022) until the new grease comes out of the vent holes. Use the table above to find the greasers (which are identified by a red washer): NOTE : The grease pressure must be less than 3000 psi (200 bar). ____ (2) Remove the unwanted grease. (3) Clean the greasers with a clean cloth MISCELLANEOUS (Material No. 19003) and CLEANING AGENTS (Material No. 11-026). (4) Apply a layer of COMMON GREASE (Material No. 04-022) by hand to the surface of the: - gear uplock roller (22) - door uplock roller (23). (5) Remove the unwanted grease. 5. Close-up ________ Subtask 12-22-32-410-068 A. Close Access (1) Install the new O-ring (1) on the cover (2). (2) Hold the cover (2) and the bracket (3) in position. (3) Install the washers (4) and the bolts (5). (4) Safety the bolts (5) with MISCELLANEOUS (Material No. 19-010). (5) Install the cover (7). (6) Install the bolts (6). (7) Safety the bolts (6) with MISCELLANEOUS (Material No. 19-010).
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(8) Use a clean cloth MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-024) to clean the interface of the cover (7) and the heads of the bolts (6). (9) Apply a continuous bead of SPECIAL MATERIALS (Material No. 05-047) on the interface of the cover (7) and a layer on the heads of the bolts (6). (10) Remove the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE. (11) Close the MLG doors (Ref. TASK 32-12-00-410-801). Subtask 12-22-32-865-069 B. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GA, 2GA, 9JV. Subtask 12-22-32-860-089 C. Aircraft Maintenance Configuration (1) Put the aircraft back to the correct (ground) condition (Ref. TASK 32-00-00-860-805). (2) Put the Aircraft back to its Initial Configuration Subtask 12-22-32-942-067 D. Removal of Equipment (1) Remove the access platform(s). (2) Remove the warning notice(s). (3) Remove all the fixtures, tools, test and support equipment used during this procedure.
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TASK 12-22-32-600-819 Lubrication of Nose Gear and Doors WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THE GROUND SAFETY LOCKS ARE CORRECTLY INSTALLED ON THE _______ NOSE GEAR AND DOORS. THIS PREVENTS UNWANTED MOVEMENT OF THE NLG AND NLG DOORS. WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL MATERIALS _______ ONLY WITH A GOOD FLOW OF AIR THROUGH THE WORK AREA. THESE MATERIALS ARE POISONOUS AND FLAMMABLE AND SKIN IRRITANTS. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. 1. __________________ Reason for the Job Refer to the MPD TASK: 322000-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific D23304000
circuit breaker(s) safety clip(s) 1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE 4 WARNING NOTICE 1 GROUNDLOCK PIN - NLG
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B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 04-022
USA MIL-PRF-81322 SYNTHE.HYDROCARBON GREASE HIGH PRESSURE (Ref. 20-31-00)
Material No. 11-026
GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
R Material No. 19-003
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-801 32-00-00-481-801 32-22-00-010-801 32-22-00-410-801 32-51-00-040-801 32-51-00-440-801 32-51-00-720-801 32-51-00-720-801 R R R
12-22-32-991-002 12-22-32-991-014 12-22-32-991-010
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**ON A/C ALL
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Post SB
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12-22-32-991-010-A
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**ON A/C ALL
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12-22-32-991-036
Depressurize the Green Hydraulic System (Pressurized with the Electric Pump) Installation of the Safety Devices on the Landing Gears Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance Deactivation of the Nose Wheel Steering Reactivation of the Nose Wheel Steering Functional Test of the Nose Wheel Steering (NWS) with the Handwheel(s) Functional Test of the Nose Wheel Steering (NWS) with the Handwheel(s) (CMS Procedure) Fig. 308 Fig. 309 Fig. 310
32-3192 For A/C ALL Fig. 310A
Fig. 311
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3. __________ Job Set-up Subtask 12-22-32-941-066 A. Safety Precautions (1) Put the WARNING NOTICE on the steering handwheels and the rudder pedals to tell persons not to operate the nose wheel steering (NWS). (2) Install the GROUNDLOCK PIN - NLG (D23304000) in the NLG Lock Stay (Ref. TASK 32-00-00-481-801). (3) On the panel 312VU: - make sure that the landing gear lever (6GA) is in the DOWN position - put the WARNING NOTICE to tell persons not to operate the landing gear. Subtask 12-22-32-860-076 B. Aircraft Maintenance Configuration (1) Deactivate the (NWS) (Ref. TASK 32-51-00-040-801). (2) Make sure that the Green hydraulic system is depressurized (Ref. TASK 29-00-00-864-801). Subtask 12-22-32-865-066 C. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------722VU BSCU SYS 2 2GG U37 742VU BSCU SYS 1 1GG G62 Subtask 12-22-32-010-069 D. Get Access (1) Open the NLG doors (Ref. TASK 32-22-00-010-801). (2) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE adjacent to the NLG leg.
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Subtask 12-22-32-840-051 E. Preparation of the Lubrication Equipment (1) Make sure that the lubrication equipment is serviceable before you fill it. (2) Operate the lubrication equipment to make sure that the lines and the adaptors are full of new lubricant. (3) Clean the greasers with a cloth MISCELLANEOUS (Material No. 19-003) and CLEANING AGENTS (Material No. 11-026). 4. Procedure _________ Subtask 12-22-32-640-078 R
A. Lubrication of the Nose Gear (Ref. Fig. 308/TASK 12-22-32-991-002) -------------------------------------------------------------------| NOSE LANDING GEAR | |--------------------------------------------------------------------| | No.| Component/Location |Total| Position of Greasers | |----|--------------------|-----|------------------------------------| | 1 | Attachment Points | 7 | 2 on the structure at the trunnion | | | to A/C Structure | | bearings (1 each side). | | | | | 5 on the dragstay trunnion pin | | | | | (3 on one side, 2 on the other). | |----|--------------------|-----|------------------------------------| | 2 | Retraction | 7 | 1 on the actuator cylinder eye end.| | | Actuator | | 1 on the attachment pin to the leg.| | | | | 3 on the structure pin. | | | | | 2 on the actuator rod eye-end | |----|--------------------|-----|------------------------------------| | 3 | Upper Leg | 6 | 4 on the top of the trunnion pin | | | | | housing (2 each side). | | | | | 2 on the end of the trunnion pins | | | | | (1 each side). | |----|--------------------|-----|------------------------------------| | 4 | Downlock Actuator | 3 | 2 on the actuator lugs on the leg. | | | Attachment | | 1 on the actuator/locklink | | | | | attachment pin. | |----|--------------------|-----|------------------------------------| | 5 | Torque Links and | 13 | 2 on the lugs at the connection of |
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NLG - Lubrication Points Figure 308/TASK 12-22-32-991-002- 18 (SHEET 1)
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NLG - Lubrication Points Figure 308/TASK 12-22-32-991-002- 28 (SHEET 2)
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NLG - Lubrication Points Figure 308/TASK 12-22-32-991-002- 38 (SHEET 3)
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NLG - Lubrication Points Figure 308/TASK 12-22-32-991-002- 48 (SHEET 4)
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NLG - Lubrication Points Figure 308/TASK 12-22-32-991-002- 58 (SHEET 5)
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NLG - Lubrication Points Figure 308/TASK 12-22-32-991-002- 68 (SHEET 6)
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NLG - Lubrication Points Figure 308/TASK 12-22-32-991-002- 78 (SHEET 7)
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NLG - Lubrication Points Figure 308/TASK 12-22-32-991-002- 88 (SHEET 8)
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-------------------------------------------------------------------| NOSE LANDING GEAR | |--------------------------------------------------------------------| | No.| Component/Location |Total| Position of Greasers | |----|--------------------|-----|------------------------------------| | | Shock Absorber | | the upper torque link to the leg.| | | | | 3 on the upper torque link. | | | | | 4 on the lower torque link. | | | | | 2 on the lugs at the connection | | | | | of the lower torque link to the | | | | | shock absorber piston. | | | | | 2 on the lower bearing of the shock| | | | | absorber cylinder. | |----|--------------------|-----|------------------------------------| | 6 | Steering Actuators | 12 | 1 on each rod end of the steering | | | and Leg Flanges | | actuator. | | | | | 2 on the upper flange. | | | | | 4 on the steering actuator | | | | | attachment pins (2 each side). | | | | | 4 on the lower flange. | |----|--------------------|-----|------------------------------------| | 7 | Lock Links | 4 | 2 on the fork end. | | | | | 1 at the central pin. | | | | | 1 at the leg attachment pin. | |----|--------------------|-----|------------------------------------| | 8 | Drag Stay | 14 | 4 on the fork end of the upper | | | | | stay. | | | | | 3 on the leg attachment pin. | | | | | 2 on the dragstay/trunnion | | | | | attachment pin. | | | | | 3 on the lower stay. | | | | | 2 on apex pin. | --------------------------------------------------------------------
R R R
R R R R R
(1) Lubricate the greasers with COMMON GREASE (Material No. 04-022) until the new grease comes out. Use the tables above, to find the greasers: NOTE : The grease pressure must be less than 3000 psi (206 bar). ____ (2) Remove the unwanted grease. R R
(3) Clean the greasers with a clean cloth MISCELLANEOUS (Material No. 19003) and CLEANING AGENTS (Material No. 11-026).
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Page 348 Jul 01/06
Subtask 12-22-32-640-079 B. Lubrication of NLG Doors (Ref. Fig. 309/TASK 12-22-32-991-014) -------------------------------------------------------------------| NLG DOORS | |--------------------------------------------------------------------| | No.| Component/Location |Total| Position of Greasers | |----|--------------------|-----|------------------------------------| | 9 | Bracket | 2 | 1 on each bracket (in bay) | | | | | NOTE : Do not apply grease to the | | | | | attachment bolt greasers. | |----|--------------------|-----|------------------------------------| | 10 | Door Actuator | 2 | 1 on each eye-end (in bay). | |----|--------------------|-----|------------------------------------| | 11 | Door Actuator | 2 | 1 on each eye-end (on door). | |----|--------------------|-----|------------------------------------| | 12 | Forward Door Hinge | 2 | 1 on each bracket (on door). | | | | | - NOTE: Do not apply grease to | | | | | attachment bolt greaser. | |----|--------------------|-----|------------------------------------| | 13 | Forward Door Hinge | 2 | 1 on each door bracket (in bay) | |-------------------------|-----|------------------------------------| | 14 | Rear Door Strut | 4 | 1 on pivot assembly. | | | | | 1 on fitting assembly. | | | | | 2 on strut. | --------------------------------------------------------------------
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(1) lubricate the greasers with COMMON GREASE (Material No. 04-022) until the new grease comes out. Use the tables above to find the greasers. NOTE : The grease pressure must be less than 3000 psi (206 bar). ____ (2) Remove the unwanted grease. (3) Clean the greasers with a clean cloth MISCELLANEOUS (Material No. 19003) and CLEANING AGENTS (Material No. 11-026).
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NLG Doors - Lubrication Points Figure 309/TASK 12-22-32-991-014- 12 (SHEET 1)
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NLG Doors - Lubrication Points Figure 309/TASK 12-22-32-991-014- 22 (SHEET 2)
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Subtask 12-22-32-640-080 R R
C. Lubrication of Nose Landing Gear Rotating Sleeve (Ref. Fig. 310/TASK 12-22-32-991-010) -------------------------------------------------------------------| NWS ROTATING SLEEVE | |--------------------------------------------------------------------| | No.| Component/Location |Total| Position of Greasers | |----|--------------------|-----|------------------------------------| | 15 | NWS Rotating | 2 | 2 on the front face of | | | Sleeve | | the rotating sleeve. | --------------------------------------------------------------------
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R R R
(1) Clean the greasers with a clean cloth MISCELLANEOUS (Material No. 19003) and CLEANING AGENTS (Material No. 11-026).
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(2) Use the table above to find the location of the greasers: NOTE : The grease pressure must be less than 3000 psi (206.8427 bar). ____
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(3) Lubricate the rotating sleeve through the greasers with COMMON GREASE (Material No. 04-022) until new grease comes out. NOTE : A large amount of grease can come out of the lower part of the ____ rotating sleeve before grease comes out of the top witness holes.
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(4) Remove the unwanted grease.
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(5) Do a test of the nose wheel steering to distribute the grease in the rotating sleeve, (Ref. TASK 32-51-00-720-801) or (Ref. TASK 32-51-00720-801).
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NLG - Nose Wheel Steering - Rotating Sleeve - Lubrication Points Figure 310/TASK 12-22-32-991-010
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Page 353 Jul 01/06
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**ON A/C ALL
R
Post SB
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Subtask 12-22-32-640-080-A
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32-3192 For A/C ALL
C. Lubrication of Nose Landing Gear Rotating Sleeve (Ref. Fig. 310A/TASK 12-22-32-991-010-A)
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-------------------------------------------------------------------| NWS ROTATING SLEEVE | |--------------------------------------------------------------------| | No.| Component/Location |Total| Position of Greasers | |----|--------------------|-----|------------------------------------| | 15 | NWS Rotating Sleeve| 4 | 4 on the rotating sleeve. | --------------------------------------------------------------------
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(1) Clean the greasers with a clean cloth MISCELLANEOUS (Material No. 19003) and CLEANING AGENTS (Material No. 11-026).
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(2) Use the table above to find the location of the greasers:
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NOTE : The grease pressure must be less than 3000 psi (206.8427 bar). ____
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(3) Lubricate the rotating sleeve through the greasers with COMMON GREASE (Material No. 04-022) until new grease comes out.
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NOTE : A large amount of grease can come out of the lower part of the ____ rotating sleeve before grease comes out of the top witness holes.
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(4) Remove the unwanted grease.
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(5) Do a test of the nose wheel steering to distribute the grease in the rotating sleeve, (Ref. TASK 32-51-00-720-801) or (Ref. TASK 32-51-00720-801).
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NLG - Nose Wheel Steering - Rotating Sleeve - Lubrication Points Figure 310A/TASK 12-22-32-991-010-A
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**ON A/C ALL Subtask 12-22-32-640-081 D. Lubrication of all Gear Up-Locks, Door Up-Lock Units and Pins (Ref. Fig. 311/TASK 12-22-32-991-036) R
------------------------------------------------------------------| NLG UPLOCK, DOOR UPLOCK | | ------------------------------------------------------------------| | No.| Component/Location |Total| Position of Greasers | |----|--------------------|-----|-----------------------------------| | 16 | NLG Uplock | 4 | 2 on each side of the casing. | |----|--------------------|-----|-----------------------------------| | 19 | NLG Door Uplock | 2 | 1 on each door. | | | Fitting | | | |----|--------------------|-----|-----------------------------------| | 20 | NLG Door Uplock | 4 | 4 on the casing. | -------------------------------------------------------------------
R R R R R R R R R R
(1) Lubricate the greasers with COMMON GREASE (Material No. 04-022) until the new grease comes out of the vent holes. Use the table above to find the greasers (identified by a red washer): NOTE : The grease pressure must be less than 3000 psi (200 bar). ____ NOTE : Look at work step (4) for the parts on which you apply grease ____ with your hand. (2) Remove the unwanted grease. (3) Clean the greasers with a cloth MISCELLANEOUS (Material No. 19-003) and CLEANING AGENTS (Material No. 11-026). (4) Apply (by hand) COMMON GREASE (Material No. 04-022) to the external surface of: - the apex pin of the drag stay (17) - the NLG door uplock fitting (18) on each door. (5) Remove the unwanted grease.
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NLG Uplock, Door Uplock Units and Pins - Lubrication Points Figure 311/TASK 12-22-32-991-036
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Page 357 Jul 01/06
5. Close-up ________ Subtask 12-22-32-865-067 A. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GG, 2GG. Subtask 12-22-32-410-067 B. Close Access (1) Remove the adjustable access platform. (2) Close the NLG doors (Ref. TASK 32-22-00-410-801). Subtask 12-22-32-860-077 C. Reactivate the NWS (Ref. TASK 32-51-00-440-801). Subtask 12-22-32-942-066 D. Removal of Equipment (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
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TASK 12-22-32-640-801
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Lubrication of MLG Bogie Pivot Pin
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WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS.
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1. __________________ Reason for the Job
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Refer to the MPD TASK: 321000-04 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment
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------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
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No specific No specific
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1 LUBRICATING EQUIPMENT 1 WARNING NOTICE
B. Consumable Materials
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------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R R R R R
Material No. 04-022 Material No. 11-026 Material No. 19-003
USA MIL-PRF-81322 SYNTHE.HYDROCARBON GREASE HIGH PRESSURE (Ref. 20-31-00) GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
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C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-801 R
12-22-32-991-040
Depressurize the Green Hydraulic System (Pressurized with the Electric Pump) Fig. 312
3. __________ Job Set-up Subtask 12-22-32-941-072 A. Safety Precautions (1) In the cockpit, on the panel 312VU: - make sure that the landing gear lever (6GA) is in the DOWN position - put a WARNING NOTICE in the cockpit to tell persons not to operate the landing gear lever. (2) Make sure that the Green hydraulic system is depressurized (Ref. TASK 29-00-00-864-801). Subtask 12-22-32-110-056 B. Preparation of Equipment (1) Make sure that the LUBRICATING EQUIPMENT is in the correct condition before you use it. (2) Operate the LUBRICATING EQUIPMENT to make sure that the lines and adaptors are full of new lubricant. (3) Application of the cleaning agents: WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL _______ MATERIALS ONLY WITH A GOOD FLOW OF AIR THROUGH THE WORK AREA. THESE MATERIALS ARE POISONOUS AND FLAMMABLE AND SKIN IRRITANTS. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
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(a) Clean the greasers with a clean MISCELLANEOUS (Material No. 19003) and CLEANING AGENTS (Material No. 11-026). 4. Procedure _________ R
(Ref. Fig. 312/TASK 12-22-32-991-040) Subtask 12-22-32-640-104 A. Lubrication of MLG Bogie Pivot Pin ------------------------------------------------------------------| MLG BOGIE PIVOT PIN | |-------------------------------------------------------------------| | No.| Component/Location |Total| Position of Greasers | |----|--------------------|-----|-----------------------------------| | 1 | Bogie Beam | 2 | 1 each side at pivot point | |----|--------------------|-----|-----------------------------------| | 2 | Pivot Pin | 2 | 1 below each end of pivot pin | ------------------------------------------------------------------(1) Lubricate the greasers with COMMON GREASE (Material No. 04-022) until the new grease comes out. Use the table above to find the greasers. NOTE : The grease gun pressure must be less than 3000 psi (200 bar). ____ (2) Remove the unwanted grease. (3) Application of cleaning agents: WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL _______ MATERIALS ONLY WITH A GOOD FLOW OF AIR THROUGH THE WORK AREA. THESE MATERIALS ARE POISONOUS AND FLAMMABLE AND SKIN IRRITANTS. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. (a) Clean the greasers with the clean MISCELLANEOUS (Material No. 19003) and CLEANING AGENTS (Material No. 11-026). (4) Remove any unwanted grease that has come out from the joints.
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MLG Bogie Pivot Pin - Lubrication Points Figure 312/TASK 12-22-32-991-040
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5. Close-up ________ Subtask 12-22-32-942-072 A. Removal of Equipment (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 12-22-32 R SROS
Page 363 Jan 01/07
R R R
CLG - Gear Uplock and Door Uplock Units and Pins and Door hinges - Lubrication Points Figure 313/TASK 12-22-32-991-008- 12 (SHEET 1) EFF : ALL Page 364 Jan 01/07 SROS
12-22-32
R R R
CLG - Gear Uplock and Door Uplock Units and Pins and Door hinges - Lubrication Points Figure 313/TASK 12-22-32-991-008- 22 (SHEET 2) EFF : ALL Page 365 Jan 01/07 SROS
12-22-32
DOORS - SERVICING _________________ TASK 12-22-52-600-801 Lubrication of the FWD Cargo-Compartment Door Hinge Arm Bearings, Locking Mechanism, Latching Mechanism and Interlock Mechanism 1. __________________ Reason for the Job Refer to the MPD TASK: 523100-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific No specific No specific No specific 98F52308279000
adjustable access platform brush circuit breaker(s) safety clip(s) grease gun lint-free cloth oil can 1 BAR - R/I ACTUATOR
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 03-001 Material No. 04-004
USA MIL-PRF-7870 MINERAL OIL (LOW TEMP) (Ref. 20-31-00) USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00)
EFF : ALL 12-22-52 SROS
Page 301 Jan 01/05
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------52-30-00-010-801 52-30-00-080-801 52-30-00-410-801 52-30-00-480-801 R R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 701-749, 12-22-52-991-001
R
Opening of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Removal of the Safety Support Equipment Closing of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Installation of the Safety Support Equipment
Fig. 301
**ON A/C 001-001, 201-202, 251-252, 401-449, 12-22-52-991-002
Fig. 302
**ON A/C 002-049, 203-249, 255-299, 301-399, 451-499, 701-749, 12-22-52-991-002-A R
Fig. 302A
**ON A/C 001-001, 201-202, 251-252, 401-449, 12-22-52-991-003
Fig. 303
**ON A/C 002-049, 203-249, 255-299, 301-399, 451-499, 701-749, 12-22-52-991-003-A R
Fig. 303A
**ON A/C 001-001, 201-202, 251-252, 401-449, 12-22-52-991-004
Fig. 304
**ON A/C 002-049, 203-249, 255-299, 301-399, 451-499, 701-749, 12-22-52-991-004-A
Fig. 304A
EFF : ALL 12-22-52 SROS
Page 302 Jul 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-22-52-991-010 R
Fig. 305
**ON A/C 001-001, 201-202, 251-252, 401-449, 12-22-52-991-016 12-22-52-991-017 12-22-52-991-018 12-22-52-991-019
Fig. Fig. Fig. Fig.
306 307 308 309
**ON A/C ALL 3. __________ Job Set-up Subtask 12-22-52-010-050 A. Get Access (1) Put the adjustable access platform in position below the closed FWD cargo-compartment door (referred to as cargo door). (2) Remove the access panels 132AR, 132BR, 132CR, 132DR, 132ER, 132FR, 132GR, 132HR, 132JR, 132KR, 132LR from the fuselage above the cargo door to get access to the door hinge arms. (3) Remove the access panels 821AR, 821BR, 821CR, 821DR from the cargo door to get access to the different door mechanism. (4) Open the cargo door to the vertical position (Ref. TASK 52-30-00-010801) and safety it with the BAR - R/I ACTUATOR (98F52308279000) (Ref. TASK 52-30-00-480-801). Subtask 12-22-52-865-050 B. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------5002VE CARGO DOOR CTL 1MJ A02
EFF : ALL 12-22-52 SROS
Page 303 Jul 01/05
4. Procedure _________ R
**ON A/C 001-001, 201-202, 251-252, 401-449, Subtask 12-22-52-640-050 A. Lubrication (Ref. Fig. 301/TASK 12-22-52-991-001, 302/TASK 12-22-52-991-002, 303/TASK 12-22-52-991-003, 304/TASK 12-22-52-991-004) NOTE : This procedure is applicable for door serial No. 1001 to 1252. ____ (1) Lubricate the door hinges (1) with COMMON GREASE (Material No. 04004). Use a grease gun. (2) Lubricate the door eccentric bushes (2) and the eccentric bolts with COMMON GREASE (Material No. 04-004). Use a grease gun and a brush. (3) Lubricate the door handle mechanism (3) and the handle flap mechanism (4) with OILS (Material No. 03-001), COMMON GREASE (Material No. 04004). Use a grease gun, an oil can and a brush. (4) Lubricate the door locking shaft (6), the interlock mechanism and the door latching shaft (5) with OILS (Material No. 03-001). Use an oil can. (5) Lubricate the door hook attachment bolts (7) and (8) with COMMON GREASE (Material No. 04-004). Use a grease gun. (6) Lubricate the universal joints (9) with OILS (Material No. 03-001). Use an oil can. (7) Lubricate the spring unit (10) and the link assembly (11) with OILS (Material No. 03-001). Use an oil can. (8) Remove the unwanted lubricant with a lint-free cloth.
EFF : ALL 12-22-52 SROS
Page 304 Jul 01/05
FWD Cargo-Compartment Door - Lubrication of Door Hinges and Lock Fittings Figure 301/TASK 12-22-52-991-001 R EFF : ALL 12-22-52 SROS
Page 305 Jul 01/99
Cargo-Compartment Doors - Lubrication - Door Serial No. 1001 to 1252 Figure 302/TASK 12-22-52-991-002 R EFF : 001-001, 201-202, 251-252, 401-449, 12-22-52 SROS
Page 306 Jul 01/05
INTENTIONALLY BLANK
R 12-22-52 SROS
Page 307 Jul 01/99
FWD Cargo-Compartment Door - Lubrication of Latching Mechanism Figure 302A/TASK 12-22-52-991-002-A12 (SHEET 1) R EFF : 002-049, 203-249, 255-299, 301-399, 12-22-52 451-499, 701-749, SROS
Page 308 Apr 01/04
FWD Cargo-Compartment Door - Lubrication of Latching Mechanism Figure 302A/TASK 12-22-52-991-002-A22 (SHEET 2) R EFF : 002-049, 203-249, 255-299, 301-399, 12-22-52 451-499, 701-749, SROS
Page 309 Apr 01/04
Cargo Compartment Doors - Lubrication - Door Serial No. 1001 to 1252 Figure 303/TASK 12-22-52-991-003 R EFF : 001-001, 201-202, 251-252, 401-449, 12-22-52 SROS
Page 310 Jul 01/05
INTENTIONALLY BLANK
R 12-22-52 SROS
Page 311 Jul 01/99
FWD Cargo-Compartment Door - Lubrication of Locking Mechanism Figure 303A/TASK 12-22-52-991-003-A12 (SHEET 1) R EFF : 002-049, 203-249, 255-299, 301-399, 12-22-52 451-499, 701-749, SROS
Page 312 Apr 01/04
FWD Cargo-Compartment Door - Lubrication of Locking Mechanism Figure 303A/TASK 12-22-52-991-003-A22 (SHEET 2) R EFF : 002-049, 203-249, 255-299, 301-399, 12-22-52 451-499, 701-749, SROS
Page 313 Apr 01/04
Cargo Compartment Doors - Lubrication - Door Serial No. 1001 to 1252 Figure 304/TASK 12-22-52-991-004 R EFF : 001-001, 201-202, 251-252, 401-449, 12-22-52 SROS
Page 314 Jul 01/05
R
**ON A/C 002-049, 203-249, 255-299, 301-399, 451-499, 701-749, Subtask 12-22-52-640-050-A A. Lubrication of the FWD Cargo Door NOTE : Use a grease gun, an oil can or a brush as required for the ____ lubrication procedure. (1) Lubricate the door hinge arms and the latch fittings as follows: (Ref. Fig. 301/TASK 12-22-52-991-001) (a) Lubricate the hinge bolt (1) with COMMON GREASE (Material No. 04004). (b) Lubricate the eccentric bushes (2) and the eccentric bolts (3) with COMMON GREASE (Material No. 04-004). (2) Lubricate the latching mechanism as follows: (Ref. Fig. 302A/TASK 12-22-52-991-002-A) (a) Lubricate the handle bolt (5), the hook bolt (9) and the bellcrank bolt (10) with COMMON GREASE (Material No. 04-004). (b) Apply COMMON GREASE (Material No. 04-004) to the mating surface of the catch hook (7). (c) Lubricate the push button (4) and the catch hook linkage (6) of the latching handle with OILS (Material No. 03-001). (d) Lubricate the cardan joints (11) of the torque tube assy with OILS (Material No. 03-001). (e) Lubricate the bearings of the latching shaft (8) with OILS (Material No. 03-001). (3) Lubricate the locking mechanism as follows: (Ref. Fig. 303A/TASK 12-22-52-991-003-A) (a) Lubricate the bearings of the locking handle (15) with OILS (Material No. 03-001). (b) Lubricate the bearings of the double lever shaft (12) with OILS (Material No. 03-001).
R EFF : 002-049, 203-249, 255-299, 301-399, 12-22-52 451-499, 701-749, SROS
Page 315 Apr 01/04
(c) Lubricate the bearings of the bellcrank shaft (14) with OILS (Material No. 03-001). (d) Lubricate the bearings of the rear locking shaft (17) and the joint fork assemblies (17) with OILS (Material No. 03-001). (e) Lubricate the universal joint bearings of the locking shafts (18) with OILS (Material No. 03-001). (f) Lubricate the upper and lower pins of the gas spring (13) with OILS (Material No. 03-001). (4) Lubricate the switch mechanism as follows: (Ref. Fig. 304A/TASK 12-22-52-991-004-A) (a) Lubricate the bearings of the support lever shaft (21) with OILS (Material No. 03-001). (b) Lubricate the upper and lower pins of the gas spring (22) with OILS (Material No. 03-001). (c) Lubricate the spring of the target lever (23) with OILS (Material No. 03-001). (5) Lubricate the interlock mechanism as follows: (Ref. Fig. 305/TASK 12-22-52-991-010) (a) Lubricate the mating surface of the integrated stop (27) (part of the fuselage latch fitting) with COMMON GREASE (Material No. 04004). (b) Lubricate the mating surface of the interlock lever (28) with OILS (Material No. 03-001). (c) Lubricate the bearings of the interlock shaft (29) with OILS (Material No. 03-001). (6) Remove the unwanted lubricant with a lint-free cloth.
R EFF : 002-049, 203-249, 255-299, 301-399, 12-22-52 451-499, 701-749, SROS
Page 316 Apr 01/04
FWD Cargo-Compartment Door - Lubrication of Switch Mechanism Figure 304A/TASK 12-22-52-991-004-A R EFF : 002-049, 203-249, 255-299, 301-399, 12-22-52 451-499, 701-749, SROS
Page 317 Apr 01/04
Lubrication of Interlock Mechanism Figure 305/TASK 12-22-52-991-010 R EFF : 002-049, 203-249, 255-299, 301-399, 12-22-52 451-499, 701-749, SROS
Page 318 Apr 01/04
R
**ON A/C 001-001, 201-202, 251-252, 401-449, Subtask 12-22-52-640-058 B. Lubrication of the FWD Cargo Door NOTE : This procedure is applicable for door serial No. 1253 and ____ subsequent. NOTE : Use a grease gun, an oil can or a brush as required for the ____ lubrication procedure. (1) Lubricate the door hinge arms and the latch fittings as follows: (Ref. Fig. 301/TASK 12-22-52-991-001) (a) Lubricate the hinge bolt (1) with COMMON GREASE (Material No. 04004). (b) Lubricate the eccentric bushes (2) and the eccentric bolts (3) with COMMON GREASE (Material No. 04-004). (2) Lubricate the latching mechanism as follows: (Ref. Fig. 306/TASK 12-22-52-991-016) (a) Lubricate the handle bolt (5), the hook bolt (9) and the bellcrank bolt (10) with COMMON GREASE (Material No. 04-004). (b) Apply COMMON GREASE (Material No. 04-004) to the mating surface of the catch hook (7). (c) Lubricate the push button (4) and the catch hook linkage (6) of the latching handle with OILS (Material No. 03-001). (d) Lubricate the cardan joints (11) of the torque tube assy with OILS (Material No. 03-001). (e) Lubricate the bearings of the latching shaft (8) with OILS (Material No. 03-001). (3) Lubricate the locking mechanism as follows: (Ref. Fig. 307/TASK 12-22-52-991-017) (a) Lubricate the bearings of the locking handle (15) with OILS (Material No. 03-001).
R EFF : 001-001, 201-202, 251-252, 401-449, 12-22-52 SROS
Page 319 Jul 01/05
Cargo Compartment Doors - Lubrication - Door Serial No. 1253 and subsequent Figure 306/TASK 12-22-52-991-016- 12 (SHEET 1) R EFF : 001-001, 201-202, 251-252, 401-449, 12-22-52 SROS
Page 320 Jul 01/05
Cargo Compartment Doors - Lubrication - Door Serial No. 1253 and subsequent Figure 306/TASK 12-22-52-991-016- 22 (SHEET 2) R EFF : 001-001, 201-202, 251-252, 401-449, 12-22-52 SROS
Page 321 Jul 01/05
Cargo Compartment Doors - Lubrication - Door Serial No. 1253 and subsequent Figure 307/TASK 12-22-52-991-017- 12 (SHEET 1) R EFF : 001-001, 201-202, 251-252, 401-449, 12-22-52 SROS
Page 322 Jul 01/05
Cargo Compartment Doors - Lubrication - Door Serial No. 1253 and subsequent Figure 307/TASK 12-22-52-991-017- 22 (SHEET 2) R EFF : 001-001, 201-202, 251-252, 401-449, 12-22-52 SROS
Page 323 Jul 01/05
(b) Lubricate the bearings of the double lever shaft (12) with OILS (Material No. 03-001). (c) Lubricate the bearings of the bellcrank shaft (14) with OILS (Material No. 03-001). (d) Lubricate the bearings of the rear locking shaft (17) and the joint fork assemblies (17) with OILS (Material No. 03-001). (e) Lubricate the universal joint bearings of the locking shafts (18) with OILS (Material No. 03-001). (f) Lubricate the upper and lower pins of the gas spring (13) with OILS (Material No. 03-001). (4) Lubricate the switch mechanism as follows: (Ref. Fig. 308/TASK 12-22-52-991-018) (a) Lubricate the bearings of the support lever shaft (21) with OILS (Material No. 03-001). (b) Lubricate the upper and lower pins of the gas spring (22) with OILS (Material No. 03-001). (c) Lubricate the bearings of the target lever (23) with OILS (Material No. 03-001). (5) Lubricate the interlock mechanism as follows: (Ref. Fig. 309/TASK 12-22-52-991-019) (a) Lubricate the mating surface of the integrated stop (27) (part of the fuselage stop fitting) with COMMON GREASE (Material No. 04004). (b) Lubricate the mating surface of the interlock lever (28) with OILS (Material No. 03-001). (c) Lubricate the bearings of the interlock shaft (29) with OILS (Material No. 03-001). (6) Remove the unwanted lubricant with a lint-free cloth.
R EFF : 001-001, 201-202, 251-252, 401-449, 12-22-52 SROS
Page 324 Jul 01/05
Cargo Compartment Doors - Lubrication - Door Serial No. 1253 and subsequent Figure 308/TASK 12-22-52-991-018 R EFF : 001-001, 201-202, 251-252, 401-449, 12-22-52 SROS
Page 325 Jul 01/05
FWD Cargo-Compartment Door Lubrication of Interlock Mechanism - Door Serial No. 1253 and subsequent Figure 309/TASK 12-22-52-991-019 R EFF : 001-001, 201-202, 251-252, 401-449, Page 326 Jul 01/05 SROS
12-22-52
**ON A/C ALL 5. Close-up ________ Subtask 12-22-52-410-050 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels 821AR, 821BR, 821CR, 821DR on the cargo door. (3) Remove the BAR - R/I ACTUATOR (Ref. TASK 52-30-00-080-801) and close the cargo door (Ref. TASK 52-30-00-410-801). (4) Install the access panels 132AR, 132BR, 132CR, 132DR, 132ER, 132FR, 132GR, 132HR, 132JR, 132KR, 132LR on the fuselage above the cargo door. (5) Remove the access platform(s).
EFF : ALL 12-22-52 R SROS
Page 327 Oct 01/99
TASK 12-22-52-600-802 R
Lubrication of the Telescopic Arm and Exterior Control Handle 1. __________________ Reason for the Job Refer to the MPD TASK: 521121-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
brush grease gun lint-free cloth
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 04-004 Material No. 04-017
USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) USA A-A-59173 SILICONE GREASE (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------52-10-00-010-801 52-10-00-410-801 12-22-52-991-005 12-22-52-991-006
Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door Fig. 310 Fig. 311
EFF : ALL 12-22-52 SROS
Page 328 Jul 01/06
3. __________ Job Set-up Subtask 12-22-52-010-051 A. Get Access (1) Open the passenger crew exit doors (Ref. TASK 52-10-00-010-801). 4. Procedure _________ R
(Ref. Fig. 310/TASK 12-22-52-991-005, 311/TASK 12-22-52-991-006) Subtask 12-22-52-640-051 A. Lubricating (1) Lubricate the door damper connection linkage (12) with COMMON GREASE (Material No. 04-004). Use a grease gun. (2) Lubricate the external door operating handle mechanism (13) with COMMON GREASE (Material No. 04-017). Use a brush. (3) Remove the unwanted lubricant with a lint-free cloth. 5. Close-up ________ Subtask 12-22-52-410-051 A. Close Access (1) Close the passenger crew exit doors (Ref. TASK 52-10-00-410-801). Subtask 12-22-52-942-051 B. Close Up (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL 12-22-52 SROS
Page 329 Oct 01/99
Doors - Lubrication Figure 310/TASK 12-22-52-991-005
R
EFF : ALL 12-22-52 SROS
Page 330 Oct 01/99
Doors - Lubrication Figure 311/TASK 12-22-52-991-006
R
EFF : ALL 12-22-52 SROS
Page 331 Oct 01/99
TASK 12-22-52-600-807 R
Lubrication of the Telescopic Arm and Exterior Control Handle 1. __________________ Reason for the Job Refer to the MPD TASK: 522200-03 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
brush grease gun lint-free cloth
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 04-004 Material No. 04-017
USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) USA A-A-59173 SILICONE GREASE (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------52-20-00-010-801 52-20-00-410-801 12-22-52-991-005 12-22-52-991-006
Opening of the Emergency Exit Door Closing of the Emergency Exit Door Fig. 310 Fig. 311
EFF : ALL 12-22-52 SROS
Page 332 Jul 01/06
3. __________ Job Set-up Subtask 12-22-52-010-056 A. Get Access (1) Open the emergency exit doors (Ref. TASK 52-20-00-010-801). 4. Procedure _________ Subtask 12-22-52-640-056 R
A. Lubricating (Ref. Fig. 310/TASK 12-22-52-991-005, 311/TASK 12-22-52-991-006) (1) Lubricate the door damper connection linkage (12) with COMMON GREASE (Material No. 04-004). Use a grease gun. (2) Lubricate the external door operating handle mechanism (13) with COMMON GREASE (Material No. 04-017). Use a brush. (3) Remove unwanted lubricant with a lint-free cloth. 5. Close-up ________ Subtask 12-22-52-410-056 A. Close Access (1) Close the emergency exit doors (Ref. TASK 52-20-00-410-801). Subtask 12-22-52-942-056 B. Close Up (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL 12-22-52 SROS
Page 333 Oct 01/99
TASK 12-22-52-600-803 Lubrication of the BULK Cargo-Compartment Door 1. __________________ Reason for the Job Refer to the MPD TASK: 523300-03 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
lint-free cloth
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 03-001 Material No. 04-004
USA MIL-PRF-7870 MINERAL OIL (LOW TEMP) (Ref. 20-31-00) USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------52-30-00-010-803 52-30-00-410-803 52-33-15-000-801 52-33-15-400-801 12-22-52-991-007
Opening of the BULK Cargo-Compartment Door Closing of the BULK Cargo-Compartment Door Removal of the Protection Lining Installation of the Protection Lining Fig. 312
EFF : ALL 12-22-52 SROS
Page 334 Jan 01/05
R
3. __________ Job Set-up
R
Subtask 12-22-52-010-052
R
A. Get Access
R R R
(1) Open the BULK cargo-compartment door (referred to as BULK door) (Ref. TASK 52-30-00-010-803) sufficiently to get access to the barrel lock assembly.
R R
(2) Safety the not fully opened BULK door with an applicable support device.
R R
(3) Remove the protection lining from the BULK door (Ref. TASK 52-33-15000-801).
R R R R
4. Procedure _________ (Ref. Fig. 312/TASK 12-22-52-991-007) Subtask 12-22-52-640-052 A. Lubrication
R
(1) Lubricate the universal joint (61) with OILS (Material No. 03-001).
R
(2) Lubricate the barrel lock (62) with OILS (Material No. 03-001).
R
(3) Lubricate the latch rod (63) with OILS (Material No. 03-001).
R
(4) Lubricate the catch assembly (64) with OILS (Material No. 03-001).
R
(5) Lubricate the handle rod (65) with OILS (Material No. 03-001).
R
(6) Lubricate the handle shaft (66) as follows:
R R
(a) Push the push button of the outer handle, so that the handle comes free of its recess.
R R
(b) Lubricate the handle shaft (66) with COMMON GREASE (Material No. 04-004).
R R
(c) Move the handle several times in and out to make sure that the shaft is sufficiently lubricated.
R
(7) Remove the unwanted grease and oil with a lint-free cloth.
EFF : ALL 12-22-52 SROS
Page 335 Apr 01/03
R R
BULK Cargo-Compartment Door - Lubrication Figure 312/TASK 12-22-52-991-007
EFF : ALL 12-22-52 SROS
Page 336 Apr 01/03
R
5. Close-up ________
R
Subtask 12-22-52-410-052
R
A. Close Access
R R
(1) Make sure that the work area is clean and clear of tools and other items.
R R
(2) Install the protection lining on the BULK door (Ref. TASK 52-33-15400-801).
R
(3) Make sure that the support device is removed.
R
(4) Close the BULK door (Ref. TASK 52-30-00-410-803).
R R
Subtask 12-22-52-942-052 B. Close-up
R R
(1) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL 12-22-52 SROS
Page 337 Apr 01/03
TASK 12-22-52-600-808 Lubrication of the AFT Cargo-Compartment Door Hinge Arm Bearings, Locking, Latching and Interlock Mechanism 1. __________________ Reason for the Job Refer to the MPD TASK: 523200-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific No specific No specific No specific 98F52308279000
adjustable access platform brush circuit breaker(s) safety clip(s) grease gun lint-free cloth oil can 1 BAR - R/I ACTUATOR
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 03-001 Material No. 04-004
USA MIL-PRF-7870 MINERAL OIL (LOW TEMP) (Ref. 20-31-00) USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00)
EFF : ALL 12-22-52 SROS
Page 338 Jan 01/05
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------52-30-00-010-801 52-30-00-080-801 52-30-00-410-801 52-30-00-480-801 R
**ON A/C 001-001, 201-202, 251-252, 401-449, 12-22-52-991-002 12-22-52-991-003 12-22-52-991-004
R R
Opening of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Removal of the Safety Support Equipment Closing of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Installation of the Safety Support Equipment
Fig. 302 Fig. 303 Fig. 304
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 701-749, 12-22-52-991-011
Fig. 313
**ON A/C 002-049, 203-249, 255-299, 301-399, 451-499, 701-749, 12-22-52-991-012 12-22-52-991-013 12-22-52-991-014 12-22-52-991-015 R
Fig. Fig. Fig. Fig.
314 315 316 317
**ON A/C 001-001, 201-202, 251-252, 401-449, 12-22-52-991-020 12-22-52-991-021 12-22-52-991-022 12-22-52-991-023
Fig. Fig. Fig. Fig.
318 319 320 321
EFF : ALL 12-22-52 SROS
Page 339 Jul 01/05
**ON A/C ALL 3. __________ Job Set-up Subtask 12-22-52-010-057 A. Get Access (1) Put the adjustable access platform in position below the closed AFT cargo-compartment door (referred to as cargo door). (2) Remove the access panels 152AR, 152BR, 152CR, 152DR, 152ER, 152FR, 152GR, 152HR, 152JR, 152KR, 152LR from the fuselage above the cargo door to get access to the door hinge arms. (3) Open the cargo door to the vertical position (Ref. TASK 52-30-00-010801) and safety it with the BAR - R/I ACTUATOR (98F52308279000) (Ref. TASK 52-30-00-480-801). (4) Remove the access panels 822AR, 822BR, 822CR, 822DR from the cargo door to get access to the different door mechanism. Subtask 12-22-52-865-053 B. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------5002VE CARGO DOOR CTL 1MJ A02 4. Procedure _________ R
**ON A/C 001-001, 201-202, 251-252, 401-449, Subtask 12-22-52-640-057 A. Lubrication (Ref. Fig. 302/TASK 12-22-52-991-002, 303/TASK 12-22-52-991-003, 304/TASK 12-22-52-991-004, 313/TASK 12-22-52-991-011) NOTE : This procedure is applicable for door serial No. 1001 to 1252. ____ (1) Lubricate the door hinges (31) with COMMON GREASE (Material No. 04004). Use a grease gun.
EFF : ALL 12-22-52 SROS
Page 340 Jul 01/05
AFT Cargo-Compartment Door Lubrication of Hinge Arms and Lock Fittings Figure 313/TASK 12-22-52-991-011
R
R EFF : ALL 12-22-52 SROS
Page 341 Apr 01/03
(2) Lubricate the door eccentric bushes (32) and the eccentric bolts (33) with COMMON GREASE (Material No. 04-004). Use a grease gun and a brush. (3) Lubricate the door handle mechanism (3) and the handle flap mechanism (4) with OILS (Material No. 03-001), COMMON GREASE (Material No. 04004). Use a grease gun, an oil can and a brush. (4) Lubricate the door locking schaft (6), the interlock mechanism and the door latching schaft (5) with OILS (Material No. 03-001). Use an oil can. (5) Lubricate the door hook attachment bolts (7) and (8) with COMMON GREASE (Material No. 04-004). Use a grease gun. (6) Lubricate the universal joints (9) with OILS (Material No. 03-001). Use an oil can. (7) Lubricate the spring unit (10) and the link assembly (11) with OILS (Material No. 03-001). Use an oil can. (8) Remove the unwanted lubricant with a lint-free cloth. **ON A/C 002-049, 203-249, 255-299, 301-399, 451-499, 701-749, Subtask 12-22-52-640-057-A A. Lubrication of the AFT Cargo Door NOTE : Use a grease gun, an oil can or a brush as required for the ____ lubrication procedure. (1) Lubricate the door hinge arms and the latch fittings as follows: (Ref. Fig. 313/TASK 12-22-52-991-011) (a) Lubricate the hinge bolt (31) with COMMON GREASE (Material No. 04-004). (b) Lubricate the eccentric bushes (32) and the eccentric bolts (33) with COMMON GREASE (Material No. 04-004). (2) Lubricate the latching mechanism as follows: (Ref. Fig. 314/TASK 12-22-52-991-012) (a) Lubricate the handle bolt (35), the hook bolt (39) and the bellcrank bolt (40) with COMMON GREASE (Material No. 04-004).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-22-52 301-399, 401-449, 451-499, 701-749, SROS
Page 342 Jul 01/05
(b) Apply COMMON GREASE (Material No. 04-004) to the mating surface of the catch hook (37). (c) Lubricate the push button (34) and the catch hook linkage (36) of the latching handle with OILS (Material No. 03-001). (d) Lubricate the cardan joints (41) of the torque tube assy with OILS (Material No. 03-001). (e) Lubricate the bearings of the latching shaft (38) with OILS (Material No. 03-001). (3) Lubricate the locking mechanism as follows: (Ref. Fig. 315/TASK 12-22-52-991-013) (a) Lubricate the bearings of the locking handle (45) with OILS (Material No. 03-001). (b) Lubricate the bearings of the double lever shaft (42) with OILS (Material No. 03-001). (c) Lubricate the bearings of the bellcrank shaft (44) with OILS (Material No. 03-001). R R
(d) Lubricate the bearings of the joint fork assemblies (47) with OILS (Material No. 03-001). (e) Lubricate the universal joints bearings of the locking shafts (48) with OILS (Material No. 03-001). (f) Lubricate the upper and lower pins of the gas spring (43) with OILS (Material No. 03-001). (4) Lubricate the switch mechanism as follows: (Ref. Fig. 316/TASK 12-22-52-991-014) (a) Lubricate the bearings of the support lever shaft (51) with OILS (Material No. 03-001). (b) Lubricate the upper and lower pins of the gas spring (53) with OILS (Material No. 03-001). (c) Lubricate the spring of the target lever (52) with OILS (Material No. 03-001).
EFF : 002-049, 203-249, 255-299, 301-399, 12-22-52 451-499, 701-749, SROS
Page 343 Jul 01/06
AFT Cargo-Compartment Door - Lubrication of Latching Mechanism Figure 314/TASK 12-22-52-991-012- 12 (SHEET 1) R EFF : 002-049, 203-249, 255-299, 301-399, 12-22-52 451-499, 701-749, SROS
Page 344 Apr 01/04
AFT Cargo-Compartment Door - Lubrication of Latching Mechanism Figure 314/TASK 12-22-52-991-012- 22 (SHEET 2) R EFF : 002-049, 203-249, 255-299, 301-399, 12-22-52 451-499, 701-749, SROS
Page 345 Apr 01/04
AFT Cargo-Compartment Door - Lubrication of Locking Mechanism Figure 315/TASK 12-22-52-991-013- 12 (SHEET 1) R EFF : 002-049, 203-249, 255-299, 301-399, 12-22-52 451-499, 701-749, SROS
Page 346 Apr 01/04
AFT Cargo-Compartment Door - Lubrication of Locking Mechanism Figure 315/TASK 12-22-52-991-013- 22 (SHEET 2) R EFF : 002-049, 203-249, 255-299, 301-399, 12-22-52 451-499, 701-749, SROS
Page 347 Apr 01/04
AFT Cargo-Compartment Door - Lubrication of Switch Mechanism Figure 316/TASK 12-22-52-991-014 R EFF : 002-049, 203-249, 255-299, 301-399, 12-22-52 451-499, 701-749, SROS
Page 348 Apr 01/04
(5) Lubricate the interlock mechanism as follows: (Ref. Fig. 317/TASK 12-22-52-991-015) (a) Lubricate the mating surface of the integrated stop (57) (part of the fuselage latch fitting ) with COMMON GREASE (Material No. 04004). (b) Lubricate the mating surface of the interlock lever (56) with OILS (Material No. 03-001). (c) Lubricate the bearings of the interlock shaft (58) with OILS (Material No. 03-001). (6) Remove the unwanted lubricant with a lint-free cloth. R
**ON A/C 001-001, 201-202, 251-252, 401-449, Subtask 12-22-52-640-059 B. Lubrication of the AFT Cargo Door NOTE : This procedure is applicable for door serial No. 1253 and ____ subsequent. NOTE : Use a grease gun, an oil can or a brush as required for the ____ lubrication procedure. (1) Lubricate the door hinge arms and the latch fittings as follows: (Ref. Fig. 313/TASK 12-22-52-991-011) (a) Lubricate the hinge bolt (31) with COMMON GREASE (Material No. 04-004). (b) Lubricate the eccentric bushes (32) and the eccentric bolts (33) with COMMON GREASE (Material No. 04-004). (2) Lubricate the latching mechanism as follows: (Ref. Fig. 318/TASK 12-22-52-991-020) (a) Lubricate the handle bolt (35), the hook bolt (39) and the bellcrank bolt (40) with COMMON GREASE (Material No. 04-004). (b) Apply COMMON GREASE (Material No. 04-004) to the mating surface of the catch hook (37).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-22-52 301-399, 401-449, 451-499, 701-749, SROS
Page 349 Jul 01/05
AFT Cargo-Compartment Door - Lubrication of Interlock Mechanism Figure 317/TASK 12-22-52-991-015 R EFF : 002-049, 203-249, 255-299, 301-399, 12-22-52 451-499, 701-749, SROS
Page 350 Apr 01/04
INTENTIONALLY BLANK
R 12-22-52 SROS
Page 351 Apr 01/03
AFT Cargo-Compartment Door - Lubrication Latching Mechanism - Door Serial No. 1253 and subsequent Figure 318/TASK 12-22-52-991-020- 12 (SHEET 1) R EFF : 001-001, 201-202, 251-252, 401-449, Page 352 Jul 01/05 SROS
12-22-52
AFT Cargo-Compartment Door - Lubrication Latching Mechanism - Door Serial No. 1253 and subsequent Figure 318/TASK 12-22-52-991-020- 22 (SHEET 2) R EFF : 001-001, 201-202, 251-252, 401-449, Page 353 Jul 01/05 SROS
12-22-52
(c) Lubricate the push button (34) and the catch hook linkage (36) of the latching handle with OILS (Material No. 03-001). (d) Lubricate the cardan joints (41) of the torque tube assy with OILS (Material No. 03-001). (e) Lubricate the bearings of the latching shaft (38) with OILS (Material No. 03-001). (3) Lubricate the locking mechanism as follows: (Ref. Fig. 319/TASK 12-22-52-991-021) (a) Lubricate the bearings of the locking handle (45) with OILS (Material No. 03-001). (b) Lubricate the bearings of the bellcrank shaft (44) with OILS (Material No. 03-001). (c) Lubricate the bearings of the double lever shaft (42) with OILS (Material No. 03-001). (d) Lubricate the bearings of the joint fork asssemblies (47) with OILS (Material No. 03-001). (e) Lubricate the universal joints bearings of the locking shafts (48) with OILS (Material No. 03-001). (f) Lubricate the upper and lower pins of the gas spring (43) with OILS (Material No. 03-001). (4) Lubricate the switch mechanism as follows: (Ref. Fig. 320/TASK 12-22-52-991-022) (a) Lubricate the bearings of the support lever shaft (51) with OILS (Material No. 03-001). (b) Lubricate the upper and lower pins of the gas spring (53) with OILS (Material No. 03-001). (c) Lubricate the spring of the target lever (52) with OILS (Material No. 03-001). (5) Lubricate the interlock mechanism as follows: (Ref. Fig. 321/TASK 12-22-52-991-023) (a) Lubricate the mating surface of the integrated stop (57) (part of the fuselage latch fitting) with OILS (Material No. 03-001).
R EFF : 001-001, 201-202, 251-252, 401-449, 12-22-52 SROS
Page 354 Jul 01/05
(b) Lubricate the mating surface of the interlock lever (56) with OILS (Material No. 03-001). (c) Lubricate the bearings of the interlock shaft (58) with OILS (Material No. 03-001). (6) Remove the unwanted lubricant with a lint-free cloth. **ON A/C ALL 5. Close-up ________ Subtask 12-22-52-410-057 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels 822AR, 822BR, 822CR, 822DR on the cargo door. (3) Remove the BAR - R/I ACTUATOR (Ref. TASK 52-30-00-080-801) and close the cargo door (Ref. TASK 52-30-00-410-801). (4) Install the access panels 152AR, 152BR, 152CR, 152DR, 152ER, 152FR, 152GR, 152HR, 152JR, 152KR, 152LR on the fuselage above the cargo door. (5) Remove the access platform(s).
R EFF : ALL 12-22-52 SROS
Page 355 Apr 01/03
AFT Cargo-Compartment Door - Lubrication of Locking Mechanism - Door Serial No. 1253 and subsequent Figure 319/TASK 12-22-52-991-021- 12 (SHEET 1) R EFF : 001-001, 201-202, 251-252, 401-449, Page 356 Jul 01/05 SROS
12-22-52
AFT Cargo-Compartment Door - Lubrication of Locking Mechanism - Door Serial No. 1253 and subsequent Figure 319/TASK 12-22-52-991-021- 22 (SHEET 2) R EFF : 001-001, 201-202, 251-252, 401-449, Page 357 Jul 01/05 SROS
12-22-52
AFT Cargo-Compartment Door - Lubrication of Switch Mechanisn - Door Serial No. 1253 and subsequent Figure 320/TASK 12-22-52-991-022 R EFF : 001-001, 201-202, 251-252, 401-449, Page 358 Jul 01/05 SROS
12-22-52
AFT Cargo-Compartment Door - Lubrication of Interlock Mechanism - Door Serial No. 1253 and subsequent Figure 321/TASK 12-22-52-991-023 R EFF : 001-001, 201-202, 251-252, 401-449, Page 359 Jul 01/05 SROS
12-22-52
TASK 12-22-52-600-809 Lubrication of the Slider Mechanism on all Pax/Crew and Emergency Exit Doors 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 04-004 R R
USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00)
Material No. 04-017A Material No. 15-004
SILICONE GREASE (Ref. 20-31-00) USA MIL-C-16173 GRADE 3 CORROSION PREVENTIVE COMPOUND (Ref. 20-31-00)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 25-62-41-000-801 25-62-41-400-801 52-10-00-010-801 52-10-00-860-801 52-10-00-860-802 52-20-00-010-801 52-20-00-860-801 52-20-00-860-802 CMM 521216 12-22-52-991-024
Energize the Ground Service Network De-energize the Ground Service Network Removal of the Escape Facilities Installation of the Escape Facilities Opening of the Passenger/Crew Door Special Precautions before Work on the Passenger/Crew Door Special Precautions after Work on the Passenger/Crew Door Opening of the Emergency Exit Door Special Precautions before Work on the Emergency Exit Door Special Precautions after Work on the Emergency Exit Door (for corrective action) Fig. 322
EFF : ALL 12-22-52 SROS
Page 360 Jul 01/05
3. __________ Job Set-up Subtask 12-22-52-861-050 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-22-52-010-058 B. Get Access WARNING : DO NOT OPEN THE PASSENGER/CREW DOORS WHILE THE RED WARNING _______ LIGHT FLASHES, IF THE RED WARNING LIGHT FLASHES, REMAINING PRESSURE COULD CAUSE DOOR TO OPEN SUDDENLY AND COULD: - KILL OR CAUSE SERIOUS INJURY TO PERSONS - CAUSE DAMAGE TO THE AIRCRAFT. CAUTION : DO NOT APPLY TEMPORARY PROTECTION ON THE OXYGEN SYSTEMS. _______ MAKE SURE THAT THE TEMPORARY PROTECTION DOES NOT GET : - ON COMPOSITE PARTS, CONTROL CABLES, PULLEYS, TEFLON BEARINGS, - ON LUBRICATED SURFACES, - IN DRAIN VALVES OR OTHER ORIFICES. TEMPORARY PROTECTION ON OR IN THESE PARTS CAN CAUSE DAMAGE. CAUTION : DO NOT OPEN THE DOOR IF THE WIND SPEED IS MORE THAN 40 KNOTS TO _______ PREVENT DAMAGE TO THE DOOR OR TO THE AIRCRAFT STRUCTURE. IF THE AIRCRAFT IS PUT INTO THE WIND THE MAXIMUM WIND SPEED CAN BE 50 KNOTS. R R
(1) Open the applicable passenger/crew door (Ref. TASK 52-10-00-010-801) or the emergency exit door (Ref. TASK 52-20-00-010-801).
R R
(2) Do the special precautions before you start work on the applicable door (Ref. TASK 52-10-00-860-801) or (Ref. TASK 52-20-00-860-801).
R R
(3) If necessary, remove the escape facilities (Ref. TASK 25-62-41-000801).
EFF : ALL 12-22-52 SROS
Page 361 Apr 01/05
4. Procedure _________ Subtask 12-22-52-640-060 A. Lubrication of the Slider Mechanism (Ref. Fig. 322/TASK 12-22-52-991-024) WARNING : MAKE SURE THE PERCUSSION LEVER OF THE DOOR DAMPER CYLINDER IS _______ IN THE DISARMED POSITION WITH THE SAFETY PIN INSTALLED. TO MAKE SURE THAT THE DOOR DOES NOT OPEN SUDDENLY. IF THE DOOR OPENS SUDDENLY IT CAN CAUSE INJURY AND OR DAMAGE. R R
(1) Close the applicable door and make sure that slide control handle stays in the DISARMED position. (2) Clean the component interface and/or the adjacent area.
R R
(3) Apply a layer of the COMMON GREASE (Material No. 04-004) to the mating surfaces of the sliders and the girt bar.
R R
NOTE : It is permitted to apply the COMMON GREASE (Material No. 04____ 017A) as an alternative to the COMMON GREASE (Material No. 04004). (4) Make sure that the applicable door is correctly closed and the slide control handle is in the ARMED position.
R
(5) Apply a layer of the STORAGE PRESERVATION (Material No. 15-004) as a spray to the spring guide and the pawl. (6) Operate the pawl to make sure that the slider mechanism operates correctly. (7) If the slider mechanism does not operate correctly, replace or repair the slider. (Ref. CMM 521216). 5. Close-up ________ Subtask 12-22-52-410-058 A. Close Access (1) Do the special precautions after work on the applicable door (Ref. TASK 52-10-00-860-802) or (Ref. TASK 52-20-00-860-802). (2) If necessary, install the escape facilities (Ref. TASK 25-62-41-400801).
EFF : ALL 12-22-52 SROS
Page 362 Jul 01/05
R
Lubrication of Slider Mechanism Figure 322/TASK 12-22-52-991-024
EFF : ALL 12-22-52 SROS
Page 363 Apr 01/05
R R
(3) Remove all the fixtures, tools, test and support equipment used during this procedure. Subtask 12-22-52-862-050 B. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-22-52 SROS
Page 364 Apr 01/05
FUSELAGE - SERVICING ____________________ TASK 12-22-53-600-801 Lubrication of the THS Hinge Line Bearings WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. 1. __________________ Reason for the Job Refer to the MPD TASK: 551600-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No
specific specific specific specific
circuit breaker(s) safety clip(s) warning notices access platform 6.0 m (19 ft. 8 in.) 1 GUN - GREASE
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R
Material No. 04-004 Material No. 19-003
USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
EFF : ALL 12-22-53 SROS
Page 301 Jul 01/04
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-804 R 12-22-53-991-001
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Fig. 301
3. __________ Job Set-up Subtask 12-22-53-864-050 A. Make sure that the Blue, Green and Yellow hydraulic systems are depressurized (Ref. TASK 29-00-00-864-804). Subtask 12-22-53-865-050 B. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------742VU FCPC 1 NORM 7CE1 C69 Subtask 12-22-53-941-050 C. Get Access (1) Put warning notices in position in the cockpit to tell persons: - not to pressurize the hydraulic systems, - not to operate the flight controls. (2) Put the access platform in position at the access door 313AL. (3) Open and safety the access door 313AL.
EFF : ALL 12-22-53 SROS
Page 302 Apr 01/03
4. ___________________ Servicing Procedure (Ref. Fig. 301/TASK 12-22-53-991-001) Subtask 12-22-53-640-050 A. Lubrication of the THS Hinge Line Bearings (1) Clean the grease nipples with a lint-free cotton cloth, MISCELLANEOUS (Material No. 19-003). (2) Do a check of the grease nipples for good condition. R
(3) Lubricate the bearings with the COMMON GREASE (Material No. 04-004) through the grease nipples with a GUN - GREASE. (4) Make sure that the new grease comes out of the bearings. (5) Remove the unwanted grease with a lint-free cotton cloth, MISCELLANEOUS (Material No. 19-003). 5. Close-up ________ Subtask 12-22-53-410-050 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access door 313AL. (3) Remove the access platform(s). (4) Remove the warning notice(s). Subtask 12-22-53-865-051 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 7CE1.
EFF : ALL 12-22-53 SROS
Page 303 Jul 01/04
R
Lubrication Points of the THS Bearings Figure 301/TASK 12-22-53-991-001
EFF : ALL 12-22-53 SROS
Page 304 Jul 01/04
TASK 12-22-53-600-802 Lubrication of the THS Upper and Lower Frame Attachment Bearings WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. 1. __________________ Reason for the Job Refer to the MPD TASK: 551600-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No
specific specific specific specific
circuit breaker(s) safety clip(s) 1 ACCESS PLATFORM 6M (20 FT) 1 GUN - GREASE 1 WARNING NOTICE
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R
Material No. 04-004 Material No. 19-003
USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
EFF : ALL 12-22-53 SROS
Page 305 Jul 01/04
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-804 R
12-22-53-991-002
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Fig. 302
3. __________ Job Set-up Subtask 12-22-53-864-051 A. Make sure that the Blue, Green and Yellow hydraulic systems are depressurized (Ref. TASK 29-00-00-864-804). Subtask 12-22-53-865-052 B. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------742VU FCPC 1 NORM 7CE1 C69 Subtask 12-22-53-941-051 C. Get Access (1) Put a WARNING NOTICE in position in the cockpit to tell persons: - not to pressurize the hydraulic systems, - not to operate the flight controls. (2) Put the ACCESS PLATFORM 6M (20 FT) in position at the access door 313AL. (3) Open and safety the access door 313AL.
EFF : ALL 12-22-53 SROS
Page 306 Jan 01/04
4. Procedure _________ (Ref. Fig. 302/TASK 12-22-53-991-002) Subtask 12-22-53-640-051 A. Lubrication of the THS Upper and Lower Frame Attachment Bearings R
(1) Clean the grease nipples with a clean cloth MISCELLANEOUS (Material No. 19-003). (2) Do a check of the grease nipples for good condition.
R R R
(3) Lubricate the bearings with the COMMON GREASE (Material No. 04-004) through the grease nipples with a GUN - GREASE.
R
(4) Make sure that the new grease comes out of the bearings.
R
(5) Remove the unwanted grease with a clean cloth MISCELLANEOUS (Material No. 19-003). 5. Close-up ________ Subtask 12-22-53-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access door 313AL. (3) Remove the access platform(s). (4) Remove the warning notice(s). Subtask 12-22-53-865-053 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 7CE1.
EFF : ALL 12-22-53 SROS
Page 307 Jul 01/04
R
Lubrication Points of the THS Bearings Figure 302/TASK 12-22-53-991-002
EFF : ALL 12-22-53 SROS
Page 308 Jul 01/04
STABILIZERS - SERVICING _______________________ TASK 12-22-55-600-802 Lubrication of the Rudder Bearing No. 6 1. __________________ Reason for the Job Refer to the MPD TASK: 272400-07 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
circuit breaker(s) safety clip(s)
R R
No specific No specific No specific
warning notices access platform 17.5 m (57 ft. 5 in.) 1 GUN - GREASE
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R R R
Material No. 04-004 Material No. 19-003
USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-804 55-33-13-000-801 55-33-13-400-801 12-22-55-991-002
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Removal of the Vertical-Stabilizer Trailing-Edge Access-Panels Installation of the Vertical-Stabilizer Trailing-Edge Access-Panels Fig. 301
EFF : ALL 12-22-55 SROS
Page 301 Jul 01/04
3. __________ Job Set-up Subtask 12-22-55-864-051 A. Make sure that the Blue, Green and Yellow hydraulic systems are depressurized (Ref. TASK 29-00-00-864-804). Subtask 12-22-55-865-052 B. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------742VU FCPC 1 NORM 7CE1 C69 Subtask 12-22-55-941-051 C. Get Access (1) Put warning notices in position in the cockpit to tell persons: - not to pressurize the hydraulic systems, - not to operate the flight controls. (2) Put the access platform in position at the vertical stabilizer. (3) Open and safety the access panel (Ref. TASK 55-33-13-000-801) 325PL. 4. Procedure _________ (Ref. Fig. 301/TASK 12-22-55-991-002) Subtask 12-22-55-640-051 A. Lubrication of the Rudder Hinge Bearing No. 6 R R
(1) Clean the grease nipple with a lint-free cotton cloth, MISCELLANEOUS (Material No. 19-003).
R R R
(2) Lubricate with the COMMON GREASE (Material No. 04-004) through the grease nipple with a GUN - GREASE.
R
(3) Make sure that the new grease comes out of the bearing.
R R
(4) Remove the unwanted grease with a lint-free cotton cloth, MISCELLANEOUS (Material No. 19-003).
EFF : ALL 12-22-55 SROS
Page 302 Jul 01/04
R R
Rudder Hinge Bearing No. 6 Figure 301/TASK 12-22-55-991-002
EFF : ALL 12-22-55 SROS
Page 303 Jul 01/00
5. Close-up ________ Subtask 12-22-55-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access panel 325PL (Ref. TASK 55-33-13-400-801). (3) Remove the ground support and maintenance equipment, the special and standard tools and all other items. (4) Remove the access platform(s). (5) Remove the warning notice(s). Subtask 12-22-55-865-053 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 7CE1.
EFF : ALL 12-22-55 R SROS
Page 304 Jul 01/00
WINDOWS - SERVICING ___________________ TASK 12-22-56-600-801 Servicing of the Sliding Windows 1. __________________ Reason for the Job This subject gives the procedure to clean and lubricate the mechanism of the sliding windows. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
brush clean and dry cloth
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 05-001 R
Material No. 11-003
USA SAE-AS8660 INSULATING AND SEALING GREASE SILICONE (Ref. 20-31-00) USA ASTM D 740 METHYL-ETHYL-KETONE (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-22-56-991-001
Fig. 301
EFF : ALL 12-22-56 SROS
Page 301 Oct 01/04
3. __________ Job Set-up Subtask 12-22-56-941-050 A. Get Access (1) Open the right and left sliding window. 4. Procedure _________ (Ref. Fig. 301/TASK 12-22-56-991-001) Subtask 12-22-56-615-050 A. Cleaning of the Rail and of the Locking System (1) Clean the rail and the locking system with a brush soaked in CLEANING AGENTS (Material No. 11-003). (2) Make dry with a clean and dry cloth. Subtask 12-22-56-640-050 B. Lubrication of the Rail and of the Locking System (Ref. Fig. 301/TASK 12-22-56-991-001) (1) Apply SPECIAL MATERIALS (Material No. 05-001) internally to the rails and to all the locking system. (2) Remove all the unwanted material from the rails. 5. Close-up ________ Subtask 12-22-56-942-050 A. Get Access (1) Close the right and the left sliding window. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 12-22-56 SROS
Page 302 Apr 01/98
Lubrication of the Sliding Windows Figure 301/TASK 12-22-56-991-001 EFF : ALL 12-22-56 SROS
Page 303 Apr 01/98
DRAINAGE - DESCRIPTION AND OPERATION ____________________________________ 1. _______ General This section gives the instructions to drain the air data system. It includes the topics below: 12-24-34, P. Block 301 AIR DATA
EFF : ALL 12-24-00 SROS
Page 1 Apr 01/98
HYDRAULIC POWER - SERVICING ___________________________ TASK 12-24-29-600-801 Servicing of the Leakage Recovery Tank (5230JM001, 5230JM002, 5230JM003) 1. __________________ Reason for the Job Refer to the MPD TASK: 291700-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
access platform 1.98 m (6 ft. 6 in.) container 5 l (1.3208 USgal)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-14-00-614-801 R 29-14-00-614-802 R 29-14-00-614-803 R 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 12-24-29-991-001
Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Depressurization of the Green Hydraulic Reservoir with Ground Equipment Depressurization of the Blue Hydraulic Reservoir with Ground Equipment Depressurization of the Yellow Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Fig. 301
EFF : ALL 12-24-29 SROS
Page 301 Jul 01/06
3. __________ Job Set-up Subtask 12-24-29-860-050 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801)
R
(2) Make sure that the hydraulic systems are depressurized and put them in the maintenance configuration. (Ref. TASK 29-00-00-864-804). (3) Depressurize the related hydraulic reservoir Depressurize the reservoir of the Green hydraulic system (Ref. TASK 29-14-00-614-801) Depressurize the reservoir of the Blue hydraulic system (Ref. TASK 29-14-00-614-802) Depressurize the reservoir of the Yellow hydraulic system (Ref. TASK 29-14-00-614-803) Subtask 12-24-29-010-050 B. Get Access (Ref. TASK 32-12-00-010-801) FOR 5230JM001 Open the right MLG door. FOR 5230JM002, 5230JM003 Open the left MLG door. (1) Put a access platform in position below the applicable tank. FOR 5230JM001 In zone 148. FOR 5230JM002 In zone 147. FOR 5230JM003 In zone 195
EFF : ALL 12-24-29 SROS
Page 302 Apr 01/04
4. Procedure _________ (Ref. Fig. 301/TASK 12-24-29-991-001) Subtask 12-24-29-020-050 A. Removal of the Leakage Recovery Tank (1) Disconnect the pipe (1). R
(2) Remove the tank (3) from its support (4). Subtask 12-24-29-680-050 B. Drain all the fluid from the tank. Put the hydraulic fluid into a container. 5. Close-up ________ Subtask 12-24-29-420-050 A. Installation of the Leakage Recovery tank. (1) Clean the component interface and/or the adjacent area. (2) Do a visual inspection of the component interface and/or the adjacent area. (3) Install the tank (3) on its support (4). (4) Hold the tank (3) and tighten the clamp (2). (5) Connect the pipe (1) to the tank. Subtask 12-24-29-860-051 B. Put the Aircraft back to its Initial Configuration (1) Pressurize the reservoirs of the Green, Blue and Yellow hydraulic system (Ref. TASK 29-14-00-614-804) (2) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
EFF : ALL 12-24-29 SROS
Page 303 Apr 01/04
R
Leakage Recovery Tank Figure 301/TASK 12-24-29-991-001
EFF : ALL 12-24-29 SROS
Page 304 Oct 01/01
Subtask 12-24-29-410-050 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Remove the access platform(s). R
(3) Close the applicable MLG door (Ref. TASK 32-12-00-410-801). FOR 5230JM001 Close the right MLG door. FOR 5230JM002, 5230JM003 Close the left MLG door.
R
EFF : ALL 12-24-29 SROS
Page 305 Jul 01/06
AIR DATA SYSTEM - SERVICING ___________________________ TASK 12-24-34-600-801 Draining of the Standby Static Pressure-Lines 1. __________________ Reason for the Job Remove water from the standby static pressure-lines. 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-24-34-991-001
Fig. 301
3. __________ Job Set-up Subtask 12-24-34-010-050 A. Find the static drain 133AL. 4. Procedure _________ (Ref. Fig. 301/TASK 12-24-34-991-001) Subtask 12-24-34-680-050 A. On the static drain 133AL push the drain valve (1) until the water in the standby static pressure-lines is eliminated. 5. Close-up ________ Subtask 12-24-34-410-050 A. Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 12-24-34 SROS
Page 301 Apr 01/98
Draining of the Standby Static Pressure-Lines Figure 301/TASK 12-24-34-991-001 EFF : ALL 12-24-34 SROS
Page 302 Apr 01/98
POTABLE WATER SYSTEM - MAINTENANCE PRACTICES ____________________________________________ TASK 12-24-38-680-801 Draining of the Potable Water System (with Electrical Power) WARNING : DO NOT DO WORK ON THE TOILET WASTE SYSTEM AND THE POTABLE WATER _______ SYSTEM AT THE SAME TIME. THIS WILL PREVENT CONTAMINATION OF THE POTABLE WATER SYSTEM. SUCH CONTAMINATION CAN BE DANGEROUS TO HEALTH. WARNING : BEFORE YOU DO WORK ON THE POTABLE WATER SYSTEM, CLEAN YOUR HANDS WITH _______ SOAP AND WATER. THIS WILL PREVENT INFECTION. (CONTAMINATION FROM TOILET WASTE IS DANGEROUS TO HEALTH). WARNING : MAKE SURE THAT THE EQUIPMENT YOU USE FOR THIS PROCEDURE IS CLEAN AND _______ APPROVED FOR THE POTABLE WATER SYSTEM. IF NOT IT CAN CAUSE CONTAMINATION OF THE POTABLE WATER SYSTEM. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R R R R R
No No No No
specific specific specific specific
1 1 1 1
ACCESS PLATFORM 1M (3 FT) ACCESS PLATFORM 2M (6 FT) CONTAINER 10 L(2 1/2 USGAL) HOSE - DRAIN
B. Consumable Materials
R R R
------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R
Material No. 19-003
USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
EFF : ALL 12-24-38 SROS
Page 201 Oct 01/01
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801
Energize the Ground Service Network De-energize the Ground Service Network
**ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, 701-749, 12-24-38-991-001-A
Fig. 201
**ON A/C 301-399, 12-24-38-991-001-B
Fig. 201A
**ON A/C ALL 3. __________ Job Set-up Subtask 12-24-38-861-050 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-24-38-865-050 B. Get access to the applicable 5000VE series panel(s). Then make sure that this(these) circuit breaker(s) is (are) closed.
R
------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------5005VE WATER SYSTEM QUANT IND 1MA E06 5005VE WATER SYSTEM DRAIN 1MP E05
EFF : ALL 12-24-38 SROS
Page 202 Jul 01/06
**ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, 701-749, Subtask 12-24-38-941-050 C. Put an ACCESS PLATFORM 1M (3 FT) in position at Zone 133, an ACCESS PLATFORM 1M (3 FT) in position at Zone 154 and an ACCESS PLATFORM 1M (3 FT) in position at Zone 164. Subtask 12-24-38-860-050 D. Aircraft Maintenance Configuration (1) Make sure that the potable water shutoff-valves in all lavatories are open. (2) Make sure that the potable water shutoff-valves in all wet galleys are open. Subtask 12-24-38-010-051 E. Get Access (1) Open the access doors 133BL, 154AR, 164AR. **ON A/C 301-399, Subtask 12-24-38-941-050-A C. Put an ACCESS PLATFORM 1M (3 FT) in position at Zone 133, an ACCESS PLATFORM 1M (3 FT) in position at Zone 153, an ACCESS PLATFORM 1M (3 FT) in position at Zone 154 and an ACCESS PLATFORM 2M (6 FT) in position at Zone 164. Subtask 12-24-38-860-050-A D. Aircraft Maintenance Configuration (1) Make sure that the potable water shutoff-valves in all lavatories are open. (2) Make sure that the potable water shutoff-valves in all wet galleys are open. (3) Make sure that the potable water shutoff-valve 5005MB is open.
EFF : 001-049, 201-249, 251-252, 255-299, 12-24-38 301-399, 401-449, 451-499, 701-749, R SROS
Page 203 Jan 01/06
Subtask 12-24-38-010-051-A E. Get Access (1) Open the access doors 133BL, 154AR, 164AR, 197JB. **ON A/C ALL 4. Procedure _________ **ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, 701-749, Subtask 12-24-38-680-050-A A. Drain the System (Ref. Fig. 201/TASK 12-24-38-991-001-A) (1) Connect the HOSE - DRAIN to: - the fill/drain nipple 26DV on the potable water service-panel, - the nipple assy 140DW on the FWD potable-water drain-panel, - the nipple assemblies 5255MB and 1400DW on the AFT potable-water drain-panel.
R R
(2) Turn the fill/drain control handle 5254MB on the potable-water service-panel to the DRAIN position. Then pull it out to the mechanical stop. NOTE : The drain-valve control lights 3MP and 6MP come on. ____ NOTE : Water drains from: ____ - the fill/drain nipple 26DV on the potable-water service-panel, - the nipple assy 140DW on the FWD potable-water drain-panel. NOTE : Operate all water faucets in the galleys and in the ____ lavatories, the coffee makers and the water heaters to drain them. NOTE : When the water level in the FWD potable water-tank is 5%: ____ - the control light 10MP comes on, - water will drain from the nipple assy 5255MB on the AFT potable-water drain-panel.
EFF : ALL 12-24-38 SROS
Page 204 Jul 01/06
(3) Close the drain valves. CAUTION : MAKE SURE THAT THE DRAIN VALVES STAY OPEN AFTER YOU DRAIN _______ THE SYSTEM. THIS PREVENTS DAMAGE TO THE SYSTEM IN FREEZING CONDITIONS. (a) If the outside temperature is less than 0 deg.C (32.00 deg.F) do not close the drain valves. (4) When the system is drained, push in the fill/drain control handle 5254MB on the potable water service-panel and turn it to the NORMAL position. NOTE : The drain-valve control lights 3MP, 6MP and 10MP go off. ____ (5) Disconnect the drain hoses from the drain ports. (6) Clean and dry the panels with a clean cloth MISCELLANEOUS (Material No. 19-003). (7) Install the cap on the fill/drain nipple 26DV of the potable water service-panel. **ON A/C 301-399, Subtask 12-24-38-680-050-B A. Drain the System (Ref. Fig. 201A/TASK 12-24-38-991-001-B) (1) Connect the HOSE - DRAIN to: - The fill/drain nipple 26DV on the potable-water service-panel, - The nipple assemblies 5255MB and 1400DW on the AFT potable-water drain-panel, - The nipple assy 141DW on the LD LAV potable-water drain-panel, - The nipple assy 140DW on the FWD potable-water drain-panel.
R R
(2) Turn the fill/drain control handle 5254MB on the potable-water service-panel to the DRAIN position. Then pull it out to the mechanical stop. NOTE : The drain-valve control lights 3MP, 14MP and 6MP come on. ____ NOTE : Water drains from: ____ - The fill/drain nipple 26DV on the potable-water service-panel,
EFF : 001-049, 201-249, 251-252, 255-299, 12-24-38 301-399, 401-449, 451-499, 701-749, SROS
Page 205 Jul 01/06
Potable Water Service Panels Figure 201/TASK 12-24-38-991-001-A13 (SHEET 1) R EFF : 001-049, 201-249, 251-252, 255-299, 12-24-38 401-449, 451-499, 701-749, SROS
Page 206 Jan 01/06
Potable Water Service Panels Figure 201/TASK 12-24-38-991-001-A23 (SHEET 2) R EFF : 001-049, 201-249, 251-252, 255-299, 12-24-38 401-449, 451-499, 701-749, SROS
Page 207 Jan 01/06
Potable Water Service Panels Figure 201/TASK 12-24-38-991-001-A33 (SHEET 3) R EFF : 001-049, 201-249, 251-252, 255-299, 12-24-38 401-449, 451-499, 701-749, SROS
Page 208 Jan 01/06
INTENTIONALLY BLANK
R 12-24-38 SROS
Page 209 Jan 01/06
Potable Water Service Panel Figure 201A/TASK 12-24-38-991-001-B14 (SHEET 1) R EFF : 301-399, 12-24-38 SROS
Page 210 Jan 01/06
Potable Water Service Panel Figure 201A/TASK 12-24-38-991-001-B24 (SHEET 2) R EFF : 301-399, 12-24-38 SROS
Page 211 Jan 01/06
Potable Water Service Panel Figure 201A/TASK 12-24-38-991-001-B34 (SHEET 3) R EFF : 301-399, 12-24-38 SROS
Page 212 Jan 01/06
Potable Water Service Panel Figure 201A/TASK 12-24-38-991-001-B44 (SHEET 4) R EFF : 301-399, 12-24-38 SROS
Page 213 Jan 01/06
- The nipple assy 141DW on the LD LAV potable water system, - The nipple assy 5250MB on the FWD potable-water drain-panel. NOTE : Operate all water faucets in the galleys and in the ____ lavatories, the coffee makers and the water heaters to drain them. NOTE : When the water level in the FWD potable water-tank is 5%: ____ - the control light 10MP comes on, - water will drain from the nipple assy 5255MB on the AFT potable-water drain-panel. (3) Close the drain valves. CAUTION : MAKE SURE THAT THE DRAIN VALVES STAY OPEN AFTER YOU DRAIN _______ THE SYSTEM. THIS PREVENTS DAMAGE TO THE SYSTEM IN FREEZING CONDITIONS. (a) If the outside temperature is less than 0 deg.C (32.00 deg.F) do not close the drain valves. (4) When the system is drained, push in the fill/drain control handle 5254MB on the potable water service-panel and turn it to the NORMAL position. NOTE : The drain-valve control lights 3MP, 6MP, 14MP and 10MP go off. ____ (5) Disconnect the drain hoses from the drain ports. (6) Clean and dry the panels with a clean cloth MISCELLANEOUS (Material No. 19-003). (7) Install the cap on the fill/drain nipple 26DV of the potable-water service-panel. **ON A/C 001-049, Subtask 12-24-38-680-052 B. Drain the Components WARNING : MAKE SURE THAT THE POTABLE WATER SYSTEM IS DEPRESSURIZED. A _______ PRESSURIZED SYSTEM CAN CAUSE INJURY TO PERSONS WHEN THEY DO WORK ON IT.
R EFF : 001-049, 301-399, 12-24-38 SROS
Page 214 Jan 01/06
(1) Galley Water-Heater NOTE : This procedure is the same for all the faucets of the galley ____ water heaters. (a) On the galley water-heater set the ON/OFF switch (2) to the OFF position. (b) Make sure that the water is not hot. (c) Put an applicable CONTAINER 10 L(2 1/2 USGAL) below the OPEN TO DRAIN connection (1) to collect the water. (d) On the galley water-heater open the OPEN TO DRAIN connection (1). (e) Let the water drain into the applicable container. (f) Close the OPEN TO DRAIN connection (1). NOTE : The connection has to be tight. Leaks are not permitted. ____ **ON A/C ALL 5. Close-up ________ **ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, 701-749, Subtask 12-24-38-410-050 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access doors 133BL, 154AR, 164AR. NOTE : Make sure that the latches are correctly locked and that the ____ door makes a continuous surface with the skin of the aircraft. NOTE : In freezing conditions, when the drain valves are opened ____ manually, you cannot close the access panels. (3) Remove the access platform(s).
R EFF : ALL 12-24-38 SROS
Page 215 Jan 01/06
**ON A/C 301-399, Subtask 12-24-38-410-050-A A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access doors 133BL, 154AR, 164AR, 197JB. NOTE : Make sure that the latches are correctly locked and that the ____ door makes a continuous surface with the skin of the aircraft. NOTE : In freezing conditions, when the drain valves are opened ____ manually, you cannot close the access panels. (3) Remove the access platform(s). **ON A/C ALL Subtask 12-24-38-862-050 B. De-energize the ground service network (Ref. TASK 24-42-00-862-801). Subtask 12-24-38-942-050 C. Remove the ground support and maintenance equipment, the special and standard tools and all other items.
R EFF : ALL 12-24-38 SROS
Page 216 Jan 01/06
TASK 12-24-38-680-802 Draining of the Potable Water System (without Electrical Power) 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
1 ACCESS PLATFORM 1M (3 FT) 1 CONTAINER 10 L(2 1/2 USGAL) 5 HOSE - DRAIN
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 19-003
USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
3. __________ Job Set-up **ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, 701-749, Subtask 12-24-38-941-051 A. Put an ACCESS PLATFORM 1M (3 FT) in position at Zone 133, an ACCESS PLATFORM 1M (3 FT) in position at Zone 154 and an ACCESS PLATFORM 1M (3 FT) in position at Zone 164.
R EFF : ALL 12-24-38 SROS
Page 217 Jan 01/06
Subtask 12-24-38-860-051 B. Aircraft Maintenance Configuration (1) Make sure that the potable water shut-off valves in all lavatories are open. (2) Make sure that the potable water shut-off valves in all wet galleys are open. Subtask 12-24-38-010-052 C. Get Access (1) Open the access doors 133BL, 154AR, 164AR. **ON A/C 301-399, Subtask 12-24-38-941-051-A A. Put an ACCESS PLATFORM 1M (3 FT) in position at Zone 133, an ACCESS PLATFORM 1M (3 FT) in position at Zone 153, an ACCESS PLATFORM 1M (3 FT) in position at Zone 154 and an ACCESS PLATFORM 1M (3 FT) in position at Zone 164. Subtask 12-24-38-860-051-A B. Aircraft Maintenance Configuration (1) Make sure that the potable water shut-off valves in all lavatories are open. (2) Make sure that the potable water shut-off valves in all wet galleys are open. (3) Make sure that the potable water shut-off valve 5005MB is open. Subtask 12-24-38-010-052-A C. Get Access (1) Open the access doors 133BL, 154AR, 164AR, 197JB.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-24-38 301-399, 401-449, 451-499, 701-749, SROS
Page 218 Jan 01/06
**ON A/C ALL 4. Procedure _________ **ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, 701-749, Subtask 12-24-38-680-051 A. Drain the System (1) Connect the HOSE - DRAIN to: - the fill/drain port on the potable water service-panel, - the drain ports on the aft potable-water drain-panel, - the drain port on the forward potable-water drain-panel. (2) Turn the fill/drain control handle 5254MB on the potable water service-panel to the DRAIN position. Then pull it out to the mechanical stop. (3) Turn the fill/drain control handle 5258MB on the aft potable-water drain-panel to the OPEN position. (4) Turn the filling line drain-handle 5259MB on the aft potable-water drain-panel to the OPEN position. (5) Turn the drain control handle on the forward potable-water drain-panel to the OPEN position. NOTE : Water will drain from: ____ - the fill/drain port on the potable water service-panel, - the filling-line drain port on the aft potable-water drain-panel, - the drain port on the forward potable-water drain-panel. (6) When the system is drained: CAUTION : MAKE SURE THAT THE DRAIN VALVES STAY OPEN AFTER YOU DRAIN _______ THE SYSTEM. THIS PREVENTS DAMAGE TO THE SYSTEM IN FREEZING CONDITIONS. - turn the control handles on the aft and forward potable-water drain-panels to the SHUT position, - push the control handle 5254MB on the potable water service-panel in and turn it to the NORMAL position.
R EFF : ALL 12-24-38 SROS
Page 219 Jan 01/06
(7) Disconnect the drain hoses from the drain ports. (8) Clean and dry the panels with a clean cloth MISCELLANEOUS (Material No. 19-003). (9) Install the cap on the fill/drain port of the service panel. **ON A/C 301-399, Subtask 12-24-38-680-051-A A. Drain the System (1) Connect the HOSE - DRAIN to: - The fill/drain port on the potable-water service-panel, - The drain ports on the AFT potable-water drain-panel, - The drain ports on the LD LAV potable-water drain-panel, - The drain port on the FWD potable-water drain-panel. (2) Turn the fill/drain control handle 5254MB on the potable-water service-panel to the DRAIN position. Then pull it out to the mechanical stop. (3) Turn the fill/drain control handle 5258MB on the AFT potable-water drain-panel to the OPEN position. (4) Turn the filling line drain-handle 5259MB on the AFT potable-water drain-panel to the OPEN position. (5) Turn the drain control handle on the LD LAV potable-water drain-panel to the OPEN position. (6) Turn the drain control handle on the FWD potable-water drain-panel to the OPEN position. NOTE : Water will drain from: ____ - The fill/drain port on the potable-water service-panel, - The filling-line drain port on the AFT potable-water drain-panel, - The drain port on the LD LAV potable-water drain-panel. - The drain port on the FWD potable-water drain-panel.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-24-38 301-399, 401-449, 451-499, 701-749, SROS
Page 220 Jan 01/06
(7) When the system is drained: CAUTION : MAKE SURE THAT THE DRAIN VALVES STAY OPEN AFTER YOU DRAIN _______ THE SYSTEM. THIS PREVENTS DAMAGE TO THE SYSTEM IN FREEZING CONDITIONS. - Turn the control handles on the AFT, LD LAV and FWD potable-water drain-panels to the SHUT position, - Push the control handle 5254MB on the potable water service-panel in and turn it to the NORMAL position. (8) Disconnect the drain hoses from the drain ports. (9) Clean and dry the panels with a clean cloth MISCELLANEOUS (Material No. 19-003). (10) Install the cap on the fill/drain port of the service panel. **ON A/C 001-049, Subtask 12-24-38-680-053 B. Drain the Components WARNING : MAKE SURE THAT THE POTABLE WATER SYSTEM IS DEPRESSURIZED. A _______ PRESSURIZED SYSTEM CAN CAUSE INJURY TO PERSONS WHEN THEY DO WORK ON IT. (1) Galley Water-Heater NOTE : This procedure is the same for all the faucets of the galley ____ water-heaters. (a) Make sure that the water is not hot. (b) Put an applicable container below the OPEN TO DRAIN connection (1) to collect the water. (c) On the galley water-heater open the OPEN TO DRAIN connection (1). (d) Let the water drain into the CONTAINER 10 L(2 1/2 USGAL). (e) Close the OPEN TO DRAIN connection (1). NOTE : The connection has to be tight. Leaks are not permitted. ____
R EFF : 001-049, 301-399, 12-24-38 SROS
Page 221 Jan 01/06
**ON A/C ALL 5. Close-up ________ **ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, 701-749, Subtask 12-24-38-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access doors 133BL, 154AR, 164AR. NOTE : Make sure that the latches are correctly locked and that the ____ door makes a continuous surface with the skin of the aircraft. NOTE : In freezing conditions, when the drain valves are opened ____ manually, you cannot close the access panels. (3) Remove the access platform(s). (4) Remove the ground support and maintenance equipment, the special and standard tools and all other items. **ON A/C 301-399, Subtask 12-24-38-410-051-A A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access doors 133BL, 154AR, 164AR, 197JB. NOTE : Make sure that the latches are correctly locked and that the ____ door makes a continuous surface with the skin of the aircraft. NOTE : In freezing conditions, when the drain valves are opened ____ manually, you cannot close the access panels. (3) Remove the access platform(s).
R EFF : ALL 12-24-38 SROS
Page 222 Jan 01/06
(4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : 301-399, 12-24-38 R SROS
Page 223 Jan 01/06
USE OF MANUAL MAGNETIC FUEL QUANTITY INDICATORS - DESCRIPTION AND OPERATION ___________________________________________________________________________ 1. General _______ The Manual Magnetic Indicators (MMIs) can be used to find the quantity of fuel in the tanks when the aircraft is on the ground. There are no MMIs in the trim tank. Thus this procedure cannot be used to calculate the quantity of fuel in the trim tank. Electrical power is not required to operate the MMIs. Before the MMIs are used it is necessary to read the indication on the aircraft attitude monitor (5000QT). Then, to find the quantity of fuel in the tanks it is necessary to use conversion tables and this data: - the MMI indications - the aircraft attitude-monitor indication - the specific gravity of the fuel. For the description and operation of the MMIs refer to 28-43-00. For the use of the MMIs refer to 12-11-28. R
**ON A/C 251-252, 701-749,
R
Post SB
28-3078 For A/C 251-252,701-749,
1. General _______ The Manual Magnetic Indicators (MMIs) can be used to find the quantity of fuel in the tanks when the aircraft is on the ground. There are no MMIs in the trim tank. Thus this procedure cannot be used to calculate the quantity of fuel in the trim tank. Electrical power is not required to operate the MMIs. To find the quantity of fuel in the tanks it is necessary to use conversion tables and this data: - the MMI indications - the specific gravity of the fuel. For the description and operation of the MMIs refer to 28-43-00. For the use of the MMIs refer to 12-11-28.
EFF : ALL 12-28-00 SROS
Page 1 Jul 01/06
UNSCHEDULED SERVICING - DESCRIPTION AND OPERATION _________________________________________________ 1. General _______ This section gives the instructions related to the servicing operations for which no frequency is specified. It includes 12-31-00/P. 12-32-00/P. 12-33-00/P. 12-36-00/P.
the topics below: Block 001 AIRCRAFT PROTECTION Block 001 SAMPLING FOR ANALYSIS Block 001 PRE-CONDITIONING Block 001 SYSTEM LINE FLUSHING
EFF : ALL 12-30-00 SROS
Page 1 Apr 01/98
COLD WEATHER MAINTENANCE - AIRCRAFT PROTECTION - DESCRIPTION AND OPERATION __________________________________________________________________________ 1. General _______ A. Safe operation of aircraft in cold weather conditions raises specific problems. Aircraft downtime and delays in flight schedules caused by cold weather problems can be minimized by a program of preventive cold weather servicing. R R
R R R R
B. Procedures for cold weather servicing during cold weather must be developed by the operator. This servicing must meet their specific requirements based on: - their cold weather experience - the available equipment and materials - the climatic conditions existing at their bases C. This topic contains information to assist the operator in defining, developing, and implementing cold weather preventive maintenance procedures that will minimize aircraft downtime and improve the safe operating level of the aircraft in adverse climatic conditions. These procedures are: - 12-31-11,P. Block 201 ANTI-ICING PROTECTION - 12-31-12,P. Block 201 ICE AND SNOW REMOVAL. - 12-31-21,P. Block 201 AIR CONDITIONING. - 12-31-24,P. Block 201 ELECTRICAL POWER. - 12-31-25,P. Block 201 EQUIPMENT/FURNISHINGS. - 12-31-27,P. Block 201 FLIGHT CONTROLS. - 12-31-28,P. Block 201 FUEL. - 12-31-31,P. Block 201 INDICATING/RECORDING SYSTEMS AND NAVIGATION. - 12-31-32,P. Block 201 LANDING GEAR. - 12-31-35,P. Block 201 DEICING/ANTI-ICING OXYGEN SYSTEM. - 12-31-38,P. Block 201 WATER/WASTE. - 12-31-49,P. Block 201 AUXILIARY POWER UNIT. - 12-31-51,P. Block 201 STRUCTURE. - 12-31-52,P. Block 201 DOORS. - 12-31-71,P. Block 201 POWER PLANT. D. Cold Soak Definition The aircraft is in cold soak configuration when : - it is parked in cold weather (Outside Air Temperature (OAT) lower than 0 deg.C (32.00 deg.F)) and - there is no supply of power to the aircraft (no air conditioning).
EFF : ALL 12-31-00 SROS
Page 1 Oct 01/04
2. __________________________________ De-icing and Anti-icing Guidelines A. De-Icing and Anti-Icing Glossary (1) De-icing is a procedure to remove frost, ice, snow and slush from the aircraft surfaces. R R R R R R
(2) De-icing fluids are normally applied heated. Typical de-icing fluids are: - Heated water, - Newtonian fluids (ISO or SAE or AEA Type I), - Mixtures of water and Type I fluid, - Non-Newtonian fluid (ISO or SAE or AEA Type II or Type IV), - Mixtures of water and Type II or Type IV fluid.
R R R R R R R R R R R R R R R R R
(3) Follow manufacturers guidelines to increase the temperature of de-icing and anti-icing fluids. De-icing and anti-icing fluids are not heated in tanks too many times or for long periods because: - the quantity of water in the fluids will decrease and - there will be a possible degradation of the fluid performance. For Type I fluids, water loss can cause unwanted aerodynamic effects. For Type II and Type IV fluids, thermal exposure and/or water loss can decrease fluid viscosity which causes lower holdover times. One or more of the conditions that follow can decrease fluid performance: - not much fluid used - trucks that do not operate with heating system on for extended periods of time, - high temperatures in fluid tanks, - high temperatures in water tanks which directly touch the fluid tanks (no insulation between tanks).
R R R R
(4) Anti-icing is a precautionary procedure which provides protection against the formation of frost or ice and snow accumulations on the treated surfaces of the aircraft for a limited period of time, the holdover time.
R R R R R
(5) Anti-icing fluids are normally applied cold directly onto clean aircraft surfaces. Typical anti-icing fluids are: - Newtonian fluids (ISO or SAE or AEA type I), - Mixtures of water and Type I fluid, - Non-Newtonian fluids (ISO or SAE or AEA Type II or Type IV), - Mixtures of water and Type II or Type IV fluid.
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(6) Non-Newtonian Fluids (Type II or Type IV) have a viscosity that reduces with increased air flow over the fluid.
EFF : ALL 12-31-00 SROS
Page 2 Oct 01/04
(7) Newtonian Fluids (Type I) have a low viscosity that only changes with temperature. (8) Holdover time is the estimated time during which anti-icing fluids will prevent the formation of frost or ice and snow accumulations on the protected surfaces of the aircraft. The holdover time starts at the beginning of the anti-icing treatment. (9) De-/Anti-icing is a combination of the de-icing and the anti-icing procedures and is performed in one or two steps. (10) One step De-/Anti-icing is carried out with an anti-icing fluid, normally heated. The aircraft is de-iced and the fluid that remains on the aircraft gives limited anti-ice protection. (11) Two step De-icing/Anti-Icing, as inferred, comprises two completely separate steps : The first step is to de-ice the aircraft (remove frost, ice, slush and snow accumulations), then to immediately follow this with an anti-icing procedure. B. An aircraft performance certification is based upon that aircraft having an uncontaminated or clean structure. (1) Ice, snow and frost or combinations of them will disturb the airflow, affecting lift and drag. It also increases the aircraft weight. (2) The aircraft, and especially its surfaces that provide lift and stability, must be aerodynamically clean. If they are not, safe operation is not possible. (3) If the fuel temperature is below freezing point and the aircraft is subject to precipitation, clear ice may form on the wings (wing tank area), even if the outside temperature is as high as 15 deg.C (59.00 deg.F). (4) An aircraft that is ready for flight must not have ice, snow, slush or frost adhering to its critical flight surfaces (Wings, vertical and horizontal stabilizers and rudder). Thin hoarfrost is permitted on the upper surface of the fuselage. NOTE : Thin hoarfrost is usually a white crystalline deposit which ____ usually develops equally on external surfaces on cold nights without clouds; it is sufficiently thin that surface features (lines or markings) can be seen below it. NOTE : A frost layer less than 3 mm (1/8 in.) on the underside of the ____ wing, in the area of fuel tanks, is permitted without effect on take off performance if it is caused by cold fuel (low fuel temperature, OAT above freezing and high humidity). This note is not applicable in THS underside.
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EFF : ALL 12-31-00 SROS
Page 3 Jan 01/07
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(5) A contamination check of the aircraft must include all parts of the aircraft. You must do this visual inspection from a position which gives a clear view of all surfaces. Because collected clear ice is not always easily seen, we recommend that you inspect critical surfaces (wings, vertical and horizontal stabilizers and rudder) with your hands. (6) Weather conditions determine when the aircraft de-/anti-icing must be carried out. (7) During checks on the ground, electrical or mechanical ice-detectors must not replace physical checks. (8) If the aircraft arrives at the gate with the flaps/slats in a position other than fully retracted, you must inspect these flaps/slats, and if necessary de-ice before retraction.
R R
C. De-icing and/or Anti-icing Equipment and Materials (1) Type I Fluids Type I fluids are normally used for aircraft de-icing and have only a limited effect when used for anti-icing purposes. Type I fluids are normally used for aircraft de-icing. These fluids contain at least 80 % by volume of either : - Monoethylene-glycol - Diethylene-glycol - Monopropylene-glycol - or a mixture of these glycols. The other 20% comprise inhibitors to restrict corrosion and increase the flash-point together with water and wetting agents. These fluids show a low viscosity which only changes with temperatures. The freezing point of a water/glycol mixture will vary with the amount of water contained in the fluid. It must be noted that the lowest freezing point of concentrated TYPE I fluid will be approximately -10 deg.C (+14.00 deg.F) whereas the lowest temperature protection will be found with a mixture of 60%/40% TYPE I fluid to water mixture whose freezing point will be below -50 deg.C (-58.00 deg.F) Also due to the lower viscosity, it flows off the wing more easily. Therefore a 50/50 mixture of TYPE I fluids to water is normally used. R
(2) Type II or Type IV fluids contain at least 50% by volume of either : - Monoethylene-glycol - Diethylene-glycol - Monopropylene-glycol - or a mixture of these glycols. The other 50% comprise :
EFF : ALL 12-31-00 SROS
Page 4 Oct 01/04
- inhibitors to restrict corrosion and increase the flash-point - water and wetting agents to allow the fluid to form a uniform film over the aircraft surfaces - thickening agents to enable the fluid to adhere to the aircraft surfaces for longer periods. Type II or Type IV fluids have a longer holdover time than type I fluid. (3) Fluid dilution Type I, Type II and Type IV fluids can be diluted with water. This may be done if due to weather conditions there are no requirements for a long conservation time or the higher freezing points are sufficient for the climatic conditions present.
R R R
(4) Holdover times Holdover times are the estimated times that the applied anti-icing fluid will prevent the formation of frost, ice and the accumulation of snow on the protected surfaces of an aircraft. When applying the first step de/anti-icing process, the holdover time is from the start of the de/anti-icing application and when applying the second step de/anti-icing process, the holdover time is from the start of the anti-icing application. The holdover times given are for general information only. The indicated time of protection may be shortened: - in severe weather - in high winds and jet blasts - by the age and condition of the fluid - by the method of application
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(5) The anti-icing code It is important that the flight crew get clear and precise information from persons who have carried out any de-/anti-icing procedures. In order to improve the quality of communication between the de-/anti-icing team and the flight crew, it is recommended that an anti-icing code be used. This will enable the flight crew to assess the Holdover Time. This code must contain the following information : - Type of Fluid - Percentage of fluid to water (for type II and Type IV fluids only) - Time de-/anti-icing application began (preferably local time) - Complete name of the anti-icing fluid (so called brand-name) for Type II and Type IV fluids only (optional).
R R
NOTE : The time referred to in the anti-icing codes must be the ____ starting time of the anti-icing procedure. Two examples of anti-icing codes are given below :
EFF : ALL 12-31-00 SROS
Page 5 Oct 01/04
R R R R R R R R
AEA Type II/ 75/ 16.43 local XXXXX ----------- --- ----------- ----| | | | | | | | | | | | | | | |__ Complete name of fluid | | | | | |__________ Local Time of start of the application | | | |____________________ % of fluid/water by vol: 75% fluid/25% water | Type of fluid used ISO Type I/ 06.30 UTC ---------- --------| | | | | - Universal coordinated Time of start of the application | ------ Type of fluid used (6) Equipment (a) Mobile equipment Truck mounted de-icing/anti-icing equipment must ideally be compatible for the application of Type I, Type II and Type IV fluids. Therefore the pump must be of the cavity or diaphragm type. Older types of centrifugal pumps cause degradation of fluids and their viscosity is reduced. (b) Static facilities Purpose-built de-icing/anti-icing facilities, available at some airports, consist of spray nozzles mounted on a gantry. The gantry moves at a predetermined speed over the aircraft or the aircraft moves under the gantry. The rate of fluid application can be computer-controlled, giving consistent and fast fluid application.
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(c) Protective clothing The usual precautions generally taken with chemicals must be applied when using de-icing/anti-icing fluids. This includes wearing protective clothing, protective glasses and the application of suitable skin ointment on exposed skin.
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EFF : ALL 12-31-00 SROS
Page 6 Oct 01/04
ANTI-ICING PROTECTION - MAINTENANCE PRACTICES _____________________________________________ TASK 12-31-11-660-801 Anti-Icing Protection R
CAUTION : DO NOT APPLY ANTI-ICING/DE-ICING FLUID IN: _______ - THE AIR INTAKES AND EXHAUST OF THE ENGINES OR APU - THE AIR OUTLET OF THE OUTFLOW VALVES - ALL OTHER AIR INTAKES OR OUTLETS.
R R R
CAUTION : BEFORE YOU DO THE ANTI-ICING/DE-ICING PROCEDURE, ALWAYS PUT _______ PROTECTION (SHEET MATERIAL) ON THE BRAKE UNITS. ANTI-ICING/DE-ICING FLUID CAN CAUSE CORROSION. CAUTION : DO NOT POINT HIGH-PRESSURE JETS: _______ - AT EQUIPMENT SUCH AS GEAR BOX SEALS, STEADY BEARINGS, ROTARY ACTUATORS AND UNIVERSAL JOINTS, - AT ELECTRICAL COMPONENTS SUCH AS HARNESSES, PROXIMITY SENSORS AND CONNECTORS. THE IMPACT PRESSURE OF THE JETS MUST NOT BE MORE THAN 5 PSI (0.35 BAR). FOR FAIRINGS, THE IMPACT PRESSURE OF THE JETS MUST NOT BE MORE THAN 1.5 PSI (0.1 BAR). HIGH PRESSURE JETS CAN PUSH LIQUIDS INTO BEARINGS, JOINTS, BRAKES, ELECTRICAL CONNECTORS AND OTHER SEALED COMPONENTS. LIQUIDS THAT GET INTO THESE AREAS CAN CAUSE CORROSION, FREEZE DURING AIRCRAFT FLIGHT, REMOVE NECESSARY LUBRICANTS OR START INCORRECT ELECTRICAL FUNCTIONS. CAUTION : DO NOT USE JET EXHAUST TO REMOVE SNOW OR ICE FROM THE AIRFRAME. _______ THE HIGH PRESSURE AND HIGH TEMPERATURE OF JET EXHAUST CAN CAUSE DAMAGE TO THE AIRCRAFT.
R R
CAUTION : DURING THE ANTI-ICING/DE-ICING AND WASHING PROCEDURES, MAKE SURE THAT _______ THE HOT WATER OR HOT WATER/FLUID MIXTURES DO NOT CAUSE THE TEMPERATURE OF THE AIRCRAFT SKIN TO INCREASE TO MORE THAN +70⁰C. 1. __________________ Reason for the Job NOTE : These guidelines were prepared with the Association of European ____ Airlines (AEA) recommendations: Recommendations for anti-icing of aircraft on ground. NOTE : The operators must use the procedures applicable to their individual ____ operating procedures and requirements. NOTE : The data given in the tables in this procedure are guidelines only. ____
EFF : ALL 12-31-11 SROS
Page 201 Jan 01/07
The user can use these guidelines and his experience and knowledge of the local weather conditions to help him make the decision. The user must make the decision about the applicable protection procedures. The time of protection will be shorter in very bad weather conditions. High wind speeds and jet blast can cause damage to the protective film. If these conditions occur, the time of protection will be much shorter. The time of protection can also be much shorter if the wind temperature is lower than the OAT. Because conditions are not always the same, a pre-take-off inspection is necessary when you use the times given in the tables.
R R
The procedures prevent the formation of ice in some areas (wings, vertical and horizontal stabilizers, rudder) and make the removal of snow from the aircraft easier. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R R
No specific No specific
warning notice 1 DE-ICING/ANTI-ICING EQUIPMENT - 17 M (55 FT) SPRAYING HEIGHT
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 10-001 Material No. 10-003 Material No. 10-004
USA AMS 1424 DE-ICING FLUID AEA/ISO TYPE I ISO 11075 (Ref. 20-31-00) USA AMS 1428 ANTI/DE-ICING FLUID AEA/ISO TYPE II ISO 11078 (Ref. 20-31-00) USA AMS 1428 ANTI ICE/DE ICINGFLUID TYPE IV (Ref. 20-31-00)
EFF : ALL 12-31-11 SROS
Page 202 Jan 01/07
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
10-11-00-555-814 24-41-00-861-801 24-41-00-862-801 12-31-11-991-002 12-31-11-991-003
Aircraft Protection Equipment Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Fig. 201 Fig. 202
3. __________ Job Set-up Subtask 12-31-11-660-051 A. Recommendations (1) An aircraft that is prepared for flight must not have ice, snow, slush or frost on its critical flight surfaces (wings, vertical and horizontal stabilizers, rudder). (2) A contamination check of the aircraft must include all parts of the aircraft. You must do this visual inspection from a position which gives a clear view of all surfaces. Because you cannot always easily see collected transparent ice, we recommend that you do an inspection of critical surfaces (wings, vertical and horizontal stabilizers, rudder) with your hands. R R
(3) Do the aircraft anti-icing/de-icing if weather conditions make it necessary. (4) When you do a check on the ground, electrical or mechanical ice-detectors must not replace manual checks. (5) If the aircraft comes to the gate with the flaps/slats in a position other than fully retracted: - you must do an inspection of these flaps/slats, - you must de-ice before retraction, if necessary.
R R R
(6) Application limits: Do not apply a new layer of anti-icing fluid directly on a layer applied before. If you must apply new anti-icing protection before the subsequent flight, you must:
EFF : ALL 12-31-11 SROS
Page 203 Jan 01/07
- first, do the de-icing of the aircraft with a hot fluid solution, - then, apply the anti-icing protection on the clean aircraft. Subtask 12-31-11-660-052 B. Different Types of Anti-Icing Fluids (Ref. Fig. 201/TASK 12-31-11-991-002, 202/TASK 12-31-11-991-003) R R R R
CAUTION : DO NOT MAKE THE ANTI-ICING/DE-ICING FLUID IN TANKS HOT TOO MANY _______ TIMES OR FOR LONG PERIODS. IF YOU DO, THE QUANTITY OF WATER IN THE FLUID WILL DECREASE AND THERE WILL BE A POSSIBLE DEGRADATION OF THE FLUID PERFORMANCE.
R R R
You usually apply anti-icing/de-icing fluid cold directly on clean aircraft surfaces. Typical anti-icing/de-icing fluids are: - Newtonian fluids (ISO or SAE or AEA Type I). - Mixtures of water and Type I fluid. - Non-Newtonian fluids (ISO or SAE or AEA Type II or Type IV). - Mixtures of water and Type II or Type IV fluid. Obey manufacturers guidelines to increase the temperature of anti-icing/de-icing fluid. For Type I fluids, water loss may cause unwanted aerodynamic effects. For Type II and Type IV fluids, thermal exposure and/or water loss may decrease fluid viscosity which causes lower holdover times. One or more of the conditions that follow can decrease fluid performance: - not much fluid used, - trucks that do not operate with heating system on for extended periods of time, - high temperatures in fluid tanks, - high temperatures in water tanks which directly touch the fluid tanks (no insulation between tanks).
R R
(1) Type I fluid (a) The primary function of this fluid is to prevent refreezing when no precipitation conditions occur. (b) Newtonian fluids (Type I) have a low viscosity that only changes with temperature. (2) Type II or Type IV fluid (a) The primary function of these fluids is to prevent refreezing when precipitation occurs.
EFF : ALL 12-31-11 SROS
Page 204 Jan 01/07
R
Guidelines for the Application of Fluid/Water Mixtures (Minimum Concentrations) as a Function of OAT Figure 201/TASK 12-31-11-991-002 EFF : ALL Page 205 Oct 01/04 SROS
12-31-11
R R R
Guidelines for Holdover Times Possible for Fluid Mixtures as a Function of Weather Conditions and OAT Figure 202/TASK 12-31-11-991-003- 12 (SHEET 1) EFF : ALL Page 206 Oct 01/04 SROS
12-31-11
R R R
Guidelines for Holdover Times Possible for Fluid Mixtures as a Function of Weather Conditions and OAT Figure 202/TASK 12-31-11-991-003- 22 (SHEET 2) EFF : ALL Page 207 Oct 01/04 SROS
12-31-11
(b) Non-newtonian fluids (Type II or Type IV) have a viscosity that decreases with increased airflow over the fluids. Subtask 12-31-11-555-050 C. Aircraft Maintenance Configuration R R
(1) Install the aircraft protection equipment (Ref. TASK 10-11-00-555814).
R
(2) Make sure that the APU bleed and the aircraft engine bleeds are stopped.
R
(3) Energize the ground service network (Ref. TASK 24-41-00-861-801).
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(4) Make sure that the flaps, the slats, the spoilers, the speed brakes and the thrust reversers are retracted.
R R R R
(5) On the center pedestal, set the pitch-trim control wheel to two degrees NOSE DN. This will drain and prevent accumulation of fluid in the THS.
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(6) On the panel 212VU: - Make sure that the EXTRACT pushbutton switch is pushed (FAULT and OVRD legend off).
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(7) On the panel 225VU: - Release the APU BLEED pushbutton switch (the ON legend goes off). - Release the ENG BLEED 1, ENG BLEED 2, ENG BLEED 3 and ENG BLEED 4 pushbutton switches (the OFF legends come on). - Lift the guard of the DITCHING pushbutton switch and push the pushbutton switch.
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(8) Put a warning notice to tell persons to remove snow from their shoes and clothes before they go into the aircraft. This is very important in the cargo compartments. If there is ice or snow on the latches, this can cause defective operation of the cargo loading system. Subtask 12-31-11-210-050 D. Visual Inspection (1) Make sure that the two sliding windows are closed.
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Page 208 Jan 01/07
4. Procedure _________ Subtask 12-31-11-941-050 R
A. Put the DE-ICING/ANTI-ICING EQUIPMENT - 17 M (55 FT) SPRAYING HEIGHT in position. NOTE : To use the mobile equipment on the ramp, it has a storage tank for ____ the anti-icing/de-icing fluid. Do not mix other fluids with the anti-icing/de-icing fluid. Use the fluid at the recommended concentration for the temperature to get a correct protection.
R R R
Subtask 12-31-11-660-050 R
B. Aircraft Anti-Icing
R
CAUTION : DO NOT APPLY ANTI-ICING/DE-ICING FLUID (MATERIAL NO. 10-001), _______ (MATERIAL NO. 10-003) OR (MATERIAL NO. 10-004) ON THE COCKPIT OR CABIN WINDOWS. IT CAN CAUSE CRACKS ON THE WINDOW. THE FLUID CAN ALSO GO INTO THE WINDOW SEAL. YOU MUST CLOSE ALL DOORS AND WINDOWS TO PREVENT: - CONTAMINATION OF GALLEY FLOOR AREAS WITH FLUID, - CONTAMINATION OF UPHOLSTERY. (1) Apply ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-001) or ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-003) or ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-004) on all aircraft surfaces. Do not apply fluid directly on: - the APU air intake, - the engine air intake and the exhaust, - the underfloor extract and the overboard extract valves, - the air intakes and the outlets, - the landing gear doors, - the pitot probes, - the static probes, - the AOA sensors.
R R R
(2) Do not put too much anti-icing/de-icing fluid in the rudder, elevator and aileron servo-control areas. Use sufficient fluid to remove the ice and the snow.
R R R
NOTE : In the THS apron area, it is important to point the spray from ____ the front to the rear. If you point the spray in the other direction (rear to front), anti-icing/de-icing fluid can go into the rear fuselage non-pressurized compartment.
EFF : ALL 12-31-11 SROS
Page 209 Jan 01/07
R (3) To prevent the flow of fluid on the cockpit windows, remove the remaining ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-001), ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-003) or ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-004) from the forward areas. You can clean the surface with clear water and a soft cloth. (4) If you find ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-001), ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-003) or ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-004) on the cockpit or cabin windows, clean the window with clear water and a soft cloth. NOTE : Do not use the wipers to clean the fluid on the windows. ____ NOTE : If you use ANTI-ICING AND DE-ICING MATERIALS (Material No. 10____ 003), make sure that there is no remaining fluid on the cockpit windows. Be specially careful of windows with wipers. 5. Close-up ________ Subtask 12-31-11-554-050 A. Removal of the Protections (1) Remove the protections and clean them with water to remove the remaining anti-icing/de-icing fluid.
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Subtask 12-31-11-942-050 B. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-41-00-862-801). R
(2) Remove the mobile equipment. (3) Make sure that the work area is clean and clear of tools and other items.
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ICE AND SNOW REMOVAL - MAINTENANCE PRACTICES ____________________________________________ TASK 12-31-12-660-801 De-icing of the Aircraft Parked in an Open Area (Engines Stopped) R
CAUTION : DO NOT APPLY ANTI-ICING/DE-ICING FLUID IN: _______ - THE AIR INTAKES AND EXHAUST OF THE ENGINES OR APU - THE AIR OUTLET OF THE OUTFLOW VALVES - ALL OTHER AIR INTAKES OR OUTLETS.
R R R
CAUTION : BEFORE YOU DO THE ANTI-ICING/DE-ICING PROCEDURE, ALWAYS PUT _______ PROTECTION (SHEET MATERIAL) ON THE BRAKE UNITS. ANTI-ICING/DE-ICING FLUID CAN CAUSE CORROSION. CAUTION : DO NOT POINT HIGH-PRESSURE JETS: _______ - AT EQUIPMENT SUCH AS GEAR BOX SEALS, STEADY BEARINGS, ROTARY ACTUATORS AND UNIVERSAL JOINTS, - AT ELECTRICAL COMPONENTS SUCH AS HARNESSES, PROXIMITY SENSORS AND CONNECTORS. THE IMPACT PRESSURE OF THE JETS MUST NOT BE MORE THAN 5 PSI (0.35 BAR). FOR FAIRINGS, THE IMPACT PRESSURE OF THE JETS MUST NOT BE MORE THAN 1.5 PSI (0.1 BAR). HIGH PRESSURE JETS CAN PUSH LIQUIDS INTO BEARINGS, JOINTS, BRAKES, ELECTRICAL CONNECTORS AND OTHER SEALED COMPONENTS. LIQUIDS THAT GET INTO THESE AREAS CAN CAUSE CORROSION, FREEZE DURING AIRCRAFT FLIGHT, REMOVE NECESSARY LUBRICANTS OR START INCORRECT ELECTRICAL FUNCTIONS.
R R
CAUTION : DURING THE ANTI-ICING/DE-ICING AND WASHING PROCEDURES, MAKE SURE THAT _______ THE HOT WATER OR HOT WATER/FLUID MIXTURES DO NOT CAUSE THE TEMPERATURE OF THE AIRCRAFT SKIN TO INCREASE TO MORE THAN +70⁰C. CAUTION : DO NOT USE JET EXHAUST TO REMOVE SNOW OR ICE FROM THE AIRFRAME. _______ THE HIGH PRESSURE AND HIGH TEMPERATURE OF JET EXHAUST CAN CAUSE DAMAGE TO THE AIRCRAFT. 1. __________________ Reason for the Job NOTE : These guidelines have been prepared using the Association of European ____ Airlines (AEA) anti-icing code: Recommendations for the de-icing of aircraft on ground. NOTE : The operators must use the procedures applicable to their individual ____ operating methods and requirements. NOTE : The data given in the tables in this procedure are guidelines only. ____
EFF : ALL 12-31-12 SROS
Page 201 Jan 01/07
The user can use these guidelines and his experience and knowledge of the local weather conditions to help him make the decision. It is the responsibility of the user to make the decision about the applicable methods of protection. The time of protection will be shorter in very bad weather conditions. High wind speeds and jet blast can cause damage to the protective film. If these conditions occur, the time of protection will be much shorter. The time of protection can also be much shorter if the wing temperature is lower than the OAT. Because conditions are not always the same, the pre-take-off inspection is necessary when you use the times given in the tables. The procedures show how to remove ice and snow from some areas of the aircraft when the engines are stopped. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R
No No No No
specific specific specific specific
broom soft brush warning notice 1 DE-ICING/ANTI-ICING EQUIPMENT - 17 M (55 FT) SPRAYING HEIGHT
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 03-001 Material No. 10-001 Material No. 10-003 Material No. 10-004
USA MIL-PRF-7870 MINERAL OIL (LOW TEMP) (Ref. 20-31-00) USA AMS 1424 DE-ICING FLUID AEA/ISO TYPE I ISO 11075 (Ref. 20-31-00) USA AMS 1428 ANTI/DE-ICING FLUID AEA/ISO TYPE II ISO 11078 (Ref. 20-31-00) USA AMS 1428 ANTI ICE/DE ICINGFLUID TYPE IV (Ref. 20-31-00)
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C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 24-41-00-862-801 12-31-12-991-002 12-31-12-991-003
Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Fig. 201 Fig. 202
3. __________ Job Set-up Subtask 12-31-12-660-055 A. Different Types of Anti-Icing Fluids. (Ref. Fig. 201/TASK 12-31-12-991-002, 202/TASK 12-31-12-991-003) R R R R
CAUTION : DO NOT MAKE THE ANTI-ICING/DE-ICING FLUID IN TANKS HOT TOO MANY _______ TIMES OR FOR LONG PERIODS. IF YOU DO, THE QUANTITY OF WATER IN THE FLUID WILL DECREASE AND THERE WILL BE A POSSIBLE DEGRADATION OF THE FLUID PERFORMANCE. You usually apply anti-icing fluids cold directly onto clean aircraft surfaces. Typical anti-icing fluids are: - Newtonian fluids (ISO or SAE or AEA Type I), - Mixtures of water and Type I fluid, - Non-Newtonian fluids (ISO or SAE or AEA Type II or Type IV), - Mixtures of water and Type II or Type IV fluid. Follow manufacturers guidelines to increase the temperature of de-icing and anti-icing fluids. For Type I fluids, water loss may cause unwanted aerodynamic effects. For Type II or Type IV fluids, thermal exposure and/or water loss may decrease fluid viscosity which causes lower holdover times. One or more of the conditions that follow can decrease fluid performance: - not much fluid used, - trucks that do not operate with heating system on for extended periods of time, - high temperatures in fluid tanks, - high temperatures in water tanks which directly touch the fluid tanks (no insulation between tanks).
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R
Guidelines for the Application of Fluid/Water Mixtures (Minimum Concentrations) as a Function of OAT Figure 201/TASK 12-31-12-991-002 EFF : ALL Page 204 Oct 01/04 SROS
12-31-12
INTENTIONALLY BLANK
R 12-31-12 SROS
Page 205 Oct 01/04
R R R
Guideline for Possible Holdover Times for Fluid Mixtures as a Function of Weather Conditions and OAT Figure 202/TASK 12-31-12-991-003- 12 (SHEET 1) EFF : ALL Page 206 Oct 01/04 SROS
12-31-12
R R R
Guideline for Possible Holdover Times for Fluid Mixtures as a Function of Weather Conditions and OAT Figure 202/TASK 12-31-12-991-003- 22 (SHEET 2) EFF : ALL Page 207 Oct 01/04 SROS
12-31-12
(1) Type I fluid (a) The primary function of this fluid is to prevent refreezing when no precipitation conditions occur. (b) Newtonian fluids (Type I) have a low viscosity that only changes with temperature. (2) Type II or Type IV fluid (a) The primary function of these fluids is to prevent refreezing even when precipitation occurs. (b) Non-newtonian fluids (Type II or Type IV) have a viscosity that decreases with increased airflow over the fluids. Subtask 12-31-12-941-050 B. Safety Precautions (1) Put a warning notice in position to tell persons to remove the snow from their shoes before they go into the aircraft. This is very important specially in the cargo compartment, because the snow can damage the cargo loading system. R Subtask 12-31-12-869-050-A C. Aircraft Maintenance Configuration CAUTION : BEFORE YOU PUSH THE DITCHING PUSHBUTTON SWITCH, MAKE SURE THAT _______ THERE IS NO SUPPLY OF AIR TO THE AIRCRAFT THROUGH THE LOW PRESSURE CONNECTION. IF THERE IS A SUPPLY OF AIR, YOU CAN CAUSE UNWANTED PRESSURIZATION OF THE AIRCRAFT. (1) Energize the ground service network (Ref. TASK 24-41-00-861-801). (2) Make sure that the APU bleed and aircraft engine are stopped. R R R
(3) On the center pedestal, set the pitch-trim control wheel to two degrees NOSE DN. This will drain and prevent accumulation of fluid in the THS.
R
(4) On the panel 212VU: - Make sure that the EXTRACT pushbutton switch is pushed (FAULT and OVRD legend off).
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Page 208 Jul 01/06
(5) On the panel 225VU: - Release the APU BLEED pushbutton switch (the ON legend goes off). - release the ENG BLEED 1, ENG BLEED 2 pushbutton switches (the OFF legend comes on). - Lift the guard of the DITCHING pushbutton switch and push the pushbutton switch (the ON legend comes on). 4. Procedure _________ Subtask 12-31-12-660-050 A. Remove the snow. (1) If the layer of snow is too thick, remove most of the snow with a broom. Use a broom with soft bristles so that you do not damage the aircraft skin. R
(2) Put the DE-ICING/ANTI-ICING EQUIPMENT - 17 M (55 FT) SPRAYING HEIGHT in position.
R R
NOTE : To use the mobile equipment on the ramp, it has a storage tank ____ for the anti-icing fluid. Do not mix other fluids with the anti-icing fluid. Use it at the ambient temperature. (3) Prepare the de-icing compound. For this, obey the instructions of the supplier. Do not mix the de-icing compound with other fluids and use it at ambient temperature. (4) Apply the ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-001) or ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-003) or ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-004) on the aircraft skin with the spray gun of the deicing equipment. Do not apply fluid directly on: - the APU air intake and the exhaust nozzles, - the air-conditioning pack inlets, - the engine cowls, air intake and exhaust nozzle, - the forward outflow valve 313HL, - the aft outflow valve 315HL, - the avionics-ventilation underfloor extract valve 12HQ, - the avionics-ventilation overboard extract valve 13HQ, - the landing gear doors and fairings, - the brake system and wheels of the landing gear, - the battery venturi, - the pitot probes, - the temperature sensors,
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Page 209 Jan 01/07
- the ice detection probes, - the static probes, - the AOA sensors. (5) Do not put too much de-icing fluid in the rudder, elevator and aileron servo-control areas. Use sufficient fluid to remove the ice and the snow. NOTE : In the THS apron area, it is important to point the spray from ____ the front to the rear. If you point the spray in the other direction (rear to front), de-icing fluid can go into the rear fuselage non-pressurized compartment. (6) Remove the snow with a soft brush from: - the engine air intake and exhaust nozzle, - the APU exhaust nozzle, - the landing gear, - the outlets of the outflow and extract valves, - the landing-gear braking system, - the inlets and outlets of the air-conditioning system. (7) Make sure that there is no ice, frost or snow in the engine air intake, all the air inlets and outlets, and the engine fan blades. This includes the rear side of the engine fan blades. R
(8) Landing gear
R R R
CAUTION : REMOVE ICE AND SNOW TO PREVENT INGRESS OF CONTAMINANTS INTO _______ BRAKES AND WHEELS. PUT COVERS ON TO PREVENT FURTHER INGRESS OF CONTAMINANTS.
R R
Remove collected ice or snow on the landing gear with a reg or a soft brush. Subtask 12-31-12-640-050 B. Lubrication (1) If the control handle of the cargo compartment doors stays blocked, lubricate the handle and the latch with OILS (Material No. 03-001)
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5. Close-up ________ Subtask 12-31-12-942-050 A. Put the Aircraft back to its Initial Configuration (1) On the panel 25 VU, release the DITCHING pushbutton switch (the ON legend is off). (2) Visually make sure that the outflow valves 313HL and 315HL are in the OPEN position before: - you supply air to the aircraft, - you start the air conditioning packs. (3) De-energize the ground service network (Ref. TASK 24-41-00-862-801). (4) Remove the access platform(s). (5) Remove the warning notice(s). (6) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
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Page 211 Jan 01/07
TASK 12-31-12-660-802 De-icing of the Aircraft Parked in an Open Area (Engines Running) WARNING : WEAR A SAFETY HARNESS WHEN YOU DE-ICE THE FORWARD FUSELAGE WITH THE _______ ENGINES AT IDLE. THE SUCTION AND EXHAUST OF THE ENGINES CAN BE DANGEROUS. R
CAUTION : DO NOT APPLY ANTI-ICING/DE-ICING FLUID IN: _______ - THE AIR INTAKES AND EXHAUST OF THE ENGINES OR APU - THE AIR OUTLET OF THE OUTFLOW VALVES - ALL OTHER AIR INTAKES OR OUTLETS.
R R R
CAUTION : BEFORE YOU DO THE ANTI-ICING/DE-ICING PROCEDURE, ALWAYS PUT _______ PROTECTION (SHEET MATERIAL) ON THE BRAKE UNITS. ANTI-ICING/DE-ICING FLUID CAN CAUSE CORROSION. CAUTION : DO NOT POINT HIGH-PRESSURE JETS: _______ - AT EQUIPMENT SUCH AS GEAR BOX SEALS, STEADY BEARINGS, ROTARY ACTUATORS AND UNIVERSAL JOINTS, - AT ELECTRICAL COMPONENTS SUCH AS HARNESSES, PROXIMITY SENSORS AND CONNECTORS. THE IMPACT PRESSURE OF THE JETS MUST NOT BE MORE THAN 5 PSI (0.35 BAR). FOR FAIRINGS, THE IMPACT PRESSURE OF THE JETS MUST NOT BE MORE THAN 1.5 PSI (0.1 BAR). HIGH PRESSURE JETS CAN PUSH LIQUIDS INTO BEARINGS, JOINTS, BRAKES, ELECTRICAL CONNECTORS AND OTHER SEALED COMPONENTS. LIQUIDS THAT GET INTO THESE AREAS CAN CAUSE CORROSION, FREEZE DURING AIRCRAFT FLIGHT, REMOVE NECESSARY LUBRICANTS OR START INCORRECT ELECTRICAL FUNCTIONS. CAUTION : DO NOT USE JET EXHAUST TO REMOVE SNOW OR ICE FROM THE AIRFRAME. _______ THE HIGH PRESSURE AND HIGH TEMPERATURE OF JET EXHAUST CAN CAUSE DAMAGE TO THE AIRCRAFT.
R R
CAUTION : DURING THE ANTI-ICING/DE-ICING AND WASHING PROCEDURES, MAKE SURE THAT _______ THE HOT WATER OR HOT WATER/FLUID MIXTURES DO NOT CAUSE THE TEMPERATURE OF THE AIRCRAFT SKIN TO INCREASE TO MORE THAN +70⁰C. 1. __________________ Reason for the Job To de-ice the aircraft before passengers go into it. The flight crew is in the aircraft .
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2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
warning notice
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 10-001 Material No. 10-003 Material No. 10-004
USA AMS 1424 DE-ICING FLUID AEA/ISO TYPE I ISO 11075 (Ref. 20-31-00) USA AMS 1428 ANTI/DE-ICING FLUID AEA/ISO TYPE II ISO 11078 (Ref. 20-31-00) USA AMS 1428 ANTI ICE/DE ICINGFLUID TYPE IV (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-31-12-991-002 12-31-12-991-003
Fig. 201 Fig. 202
3. __________ Job Set-up Subtask 12-31-12-660-056 A. Different Types of Anti-Icing Fluids. (Ref. Fig. 201/TASK 12-31-12-991-002, 202/TASK 12-31-12-991-003) R R R R
CAUTION : DO NOT MAKE THE ANTI-ICING/DE-ICING FLUID IN TANKS HOT TOO MANY _______ TIMES OR FOR LONG PERIODS. IF YOU DO, THE QUANTITY OF WATER IN THE FLUID WILL DECREASE AND THERE WILL BE A POSSIBLE DEGRADATION OF THE FLUID PERFORMANCE.
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Page 213 Jan 01/07
R R R R R R R R R R R R R R R R R R R
You usually apply anti-icing fluids cold directly onto clean aircraft surfaces. Typical anti-icing fluids are: - Newtonian fluids (ISO or SAE or AEA Type I), - Mixtures of water and Type I fluid, - Non-Newtonian fluids (ISO or SAE or AEA Type II or Type IV), - Mixtures of water and Type II or Type IV fluid. Follow manufacturers guidelines to increase the temperature of de-icing and anti-icing fluids. For Type I fluids, water loss may cause unwanted aerodynamic effects. For Type II or Type IV fluids, thermal exposure and/or water loss may decrease fluid viscosity which causes lower holdover times. One or more of the conditions that follow can decrease fluid performance: - not much fluid used, - trucks that do not operate with heating system on for extended periods of time, - high temperatures in fluid tanks, - high temperatures in water tanks which directly touch the fluid tanks (no insulation between tanks).
R
(1) Type I fluid
R R
(a) The primary function of this fluid is to prevent refreezing when no precipitation conditions occur.
R R
(b) Newtonian fluids (Type I) have a low viscosity that only changes with temperature.
R
(2) Type II or Type IV fluid
R R
(a) The primary function of these fluids is to prevent refreezing even when precipitation occurs.
R R
(b) Non-newtonian fluids (Type II or Type IV) have a viscosity that decreases with increased airflow over the fluids.
R
Subtask 12-31-12-941-051
R
B. Safety Precautions
R R R R
(1) Put a warning notice in position to tell persons to remove the snow from their shoes before they go into the aircraft. This is very important specially in the cargo compartment, because the snow can damage the cargo loading system.
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Page 214 Jul 01/06
Subtask 12-31-12-860-051 R
C. Aircraft Maintenance Configuration (1) Make sure that the engine throttle control-levers are at IDLE position.
R R R
(2) On the center pedestal, set the pitch-trim control wheel to two degrees NOSE DN. This will drain and prevent accumulation of fluid in the THS.
R
(3) On the panel 117VU. - Make sure that the PARKING BRAKE selector switch is set to ON.
R
(4) On the panel 212VU: - Make sure that the EXTRACT pushbutton switch is pushed (FAULT and OVRD legends OFF).
R
(5) On the panel 225VU: - release the APU BLEED pushbutton switch (the ON legend goes off) - release the ENG BLEED 1 and ENG BLEED 2 pushbutton switches (the OFF legends come on) - release the PACK 1 and PACK 2 pushbutton switches (the OFF legends come on). - lift the guard of the DITCHING pushbutton switch and push the pushbutton switch (the ON legend comes on).
R
(6) Make sure that the landing gear doors, the passenger/crew doors, the cargo compartment doors and the sliding windows are closed.
R
(7) Make sure that the ground support and maintenance equipment are removed. 4. Procedure _________ Subtask 12-31-12-660-051 A. De-icing of the Aircraft
R R R
(1) Prepare the de-icing compound. For this, obey the instructions of the supplier. Do not mix the de-icing compound with the other fluids and use it at the ambient temperature.
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Page 215 Jul 01/06
R R R R R R R R R R R R R R R R R R R R
(2) Apply the ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-001) or ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-003) or ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-004) on the aircraft skin with the spray gun of the de-icing equipment. Do not apply fluid directly on: - the APU air intake and the exhaust nozzles, - the air-conditioning pack inlets, - the engine cowls, air intake and exhaust nozzles, - the forward outflow valve 313HL, - the aft outflow valve 315HL, - the avionics-ventilation underfloor extract valve 12HQ, - the avionics-ventilation overboard extract valve 13HQ, - the landing gear doors and fairings, - the brake system and the wheels of the landing gear, - the battery venturi, - the pitot probes, - the temperature sensors, - the ice detection probes, - the static probes, - the AOA sensors.
R R R R R
NOTE : In the THS apron area, it is important to point the spray from ____ the front to the rear. If you point the spray in the other direction (rear to front), de-icing fluid can go into the rear fuselage non-pressurized compartment.
R Subtask 12-31-12-210-050 B. Visual Inspection (1) Make sure that after you complete the de-icing procedure, there is no more snow or ice in these areas: - the engine air intakes and exhaust nozzles, - the engine fan blades (this includes the rear side of the engine fan blades), - the APU air intake and exhaust nozzle, - the flight control surfaces: slats, flaps, ailerons, spoilers, elevator, rudder, - the forward outflow valve 313HL, - the aft outflow valve 315HL, - the avionics-ventilation underfloor extract-valve 12HQ, - the avionics-ventilation overboard extract-valve 13HQ, - the pitot probes, - the static ports,
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Page 216 Jul 01/06
- the battery venturi, - the temperature sensors. 5. Close-up ________ Subtask 12-31-12-860-052 A. Aircraft Maintenance Configuration (1) On the panel 225VU: - release the DITCHING pushbutton switch (the ON legend is off). NOTE : Visually make sure that the outflow valves 313HL and 315HL are ____ in the OPEN position before you supply air to the aircraft. - push the PACK 1 and PACK 2 pushbutton switches (the OFF legends go off). - push the ENG BLEED 1 and ENG BLEED 2 pushbutton switches (the OFF legends go off) Subtask 12-31-12-942-051 B. Put the Aircraft back to its Initial Configuration (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
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Page 217 Jul 01/06
TASK 12-31-12-660-803 De-icing of the Aircraft after Landing with Snow on the Runways 1. __________________ Reason for the Job NOTE : The guidelines have been prepared using the Association of European ____ Airlines (AEA) recommendations : Recommendations for the de-icing of aircraft on ground. NOTE : The operators should use the procedures applicable to their ____ individual operating methods and requirements. To remove the snow and ice from some areas of the aircraft. 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R
10-11-00-555-807 32-00-00-481-801
Parking Procedure in Flight-ready Condition (Parking of not more than 15 Days) Installation of the Safety Devices on the Landing Gears
3. __________ Job Set-up Subtask 12-31-12-491-050 A. Safety Precautions (1) Install the safety devices on the landing gear (Ref. TASK 32-00-00481-801).
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4. Procedure _________ Subtask 12-31-12-660-054 A. Removal of the Snow and Ice from the Aircraft (1) Remove all signs of snow and ice from: - the wing leading edges, - the flap and slat mechanisms, - the flap and slat tracks, - the landing gear (wheels and brake system), - the engine air intakes, - the engine fan blades (this includes the rear side of the engine fan blades).
R R
Subtask 12-31-12-860-053 B. If you think that snow will fall, put the aircraft in this configuration. R R
(1) Put the aircraft in the parking configuration (Ref. TASK 10-11-00555-807). (2) Make sure that you close all: - access doors and panels, - landing gear doors, - passenger doors and exits, - cargo compartment doors, - sliding windows. (3) Make sure that: - the flaps, slats, spoilers, airbrakes and thrust reverser doors are retracted - the trimmable horizontal stabilizer is in the neutral position. 5. Close-up ________ Subtask 12-31-12-942-052 A. Put the Aircraft back to its Initial Configuration (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
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COLD WEATHER MAINTENANCE - AIR CONDITIONING - MAINTENANCE PRACTICES ___________________________________________________________________ TASK 12-31-21-660-801 Cold Weather Maintenance Practices for the Air Conditioning 1. __________________ Reason for the Job This procedure gives the cold weather maintenance practices for the air conditioning. 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-31-31-660-801 12-31-38-660-801 12-31-49-660-801 R R R R R
12-33-21-618-801 12-33-21-618-801 12-33-21-618-801
Cold Weather Maintenance Practices for Indicating/Recording and Navigation Systems Cold Weather Maintenance Practices for Water/Waste Cold Weather Maintenance Practices for the Auxiliary Power Unit Pre-conditioning through the Low-Pressure Ground Connection Pre-conditioning through the High-Pressure Ground Connection Pre-conditioning with the APU
3. __________ Job Set-up Subtask 12-31-21-660-050 A. General (1) To know if ground conditioning is necessary, refer to tables 1 and 2 in the cold weather practices for the water/waste system (Ref. TASK 12-31-38-660-801).
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Page 201 Oct 01/01
(2) Avionics Bay Temperature CAUTION : DO NOT ENERGIZE THE AIRCRAFT ELECTRICAL NETWORK IF: _______ - THE TEMPERATURE IN THE AVIONICS COMPARTMENT IS EQUAL TO OR LESS THAN -40⁰C (-40.00⁰F), AND - THE CIRCUIT BREAKERS FOR THE COMPUTERS IN THE AVIONICS COMPARTMENT ARE CLOSED. BEFORE YOU ENERGIZE THE ELECTRICAL CIRCUITS IN THESE TEMPERATURES, YOU MUST OPEN THE CIRCUIT BREAKERS. IF THE CIRCUIT BREAKERS STAY CLOSED, PERMANENT DAMAGE CAN OCCUR TO THE COMPUTERS. NOTE : The temperature factor for operation of those computers ____ located in the aircraft avionics bay is the avionics bay temperature. You must measure the temperature in the avionics bay with a suitable temperature measuring device. (3) If the temperature in the aircraft avionics bay is between -40 deg.C (-40.00 deg.F) and -15 deg.C (+5.00 deg.F): - do not energize the aircraft electrical circuits before the related computer systems circuit breakers are opened. 4. Procedure _________ Subtask 12-31-21-660-051 A. Pre-conditioning Recommendations (1) If the avionics bay temperature is equal to or less than -40 deg.C (40.00 deg.F) you must do the pre-conditioning through the LP ground connector (Ref. TASK 12-33-21-618-801). (2) If the avionics bay temperature is between -15 deg.C (+5.00 deg.F) and -40 deg.C (-40.00 deg.F) you must do the pre-conditioning through: (a) The LP ground connector (Ref. TASK 12-33-21-618-801) or, (b) The HP ground connector (Ref. TASK 12-33-21-618-801). NOTE : When you do the pre-conditioning through the HP ground ____ connector: - it is possible to operate the avionics bay computers in this temperature range but incorrect operation of the computers can occur (Ref. TASK 12-31-31-660-801). - this may cause the pre-conditioning to stop.
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Page 202 Oct 01/01
- this can be because of the temperature conditions and not necessarily through a technical malfunction. (3) If the avionics bay temperature is above -15 deg.C (+5.00 deg.F) you must do the pre-conditioning: (a) Through the LP ground connector (Ref. TASK 12-33-21-618-801) or, (b) Through the HP ground connector (Ref. TASK 12-33-21-618-801) or (c) With the APU (Ref. TASK 12-33-21-618-801) and (Ref. TASK 12-3149-660-801). 5. Close-up ________ Subtask 12-31-21-941-050 A. Not applicable.
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Page 203 Apr 01/98
COLD WEATHER MAINTENANCE - ELECTRICAL POWER - MAINTENANCE PRACTICES ___________________________________________________________________ TASK 12-31-24-660-801 Cold Weather Maintenances for Electrical Power 1. __________________ Reason for the Job R R
This procedure gives the cold weather maintenances practices for the batteries when the aircraft is in cold soak configuration. 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-38-51-000-801 24-38-52-000-801
Removal of the Battery (2PB1, 2PB2) Removal of the Battery 3 (2PB3)
3. __________ Job Set-up Subtask 12-31-24-941-050 R
A. Not applicable. 4. Procedure _________ Subtask 12-31-24-660-050 A. General In very low temperatures, the chemical reaction of the electrolyte is slower and the performance of the batteries decreases : - the quantity of high current the batteries can supply decreases, - the time necessary to charge the batteries increases. This procedure gives you instructions that keep the batteries serviceable. NOTE : The values specified in this procedure are only applicable if the ____ aircraft doors stay closed during the cold soak.
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Page 201 Jan 01/07
Subtask 12-31-24-660-051 B. Battery Cold Weather Maintenance Practices (1) The batteries can stay on the aircraft during the cold soak if : - the OAT stays higher than -15 deg.C (+5.00 deg.F), - the OAT is approximately -15 deg.C (+5.00 deg.F) for not more than 12 hours, - the OAT is between -15 deg.C (+5.00 deg.F) and -30 deg.C (-22.00 deg.F) for not more than 6 hours. However, you must remove the battery if the temperature has been below -15 deg.C (+5.00 deg.F) for more than 12 hours. (2) You must remove the batteries (2PB1, 2PB2 and 2PB3) if the OAT is lower than -30 deg.C (-22.00 deg.F) during the cold soak (Ref. TASK 24-38-51-000-801) (Ref. TASK 24-38-52-000-801). NOTE : We recommend that you use a ground power unit to start the APU ____ if the OAT was lower than -15 deg.C (+5.00 deg.F) during the cold soak.
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Page 202 Apr 01/98
COLD WEATHER MAINTENANCE - EQUIPMENT/FURNISHINGS - MAINTENANCE PRACTICES ________________________________________________________________________ TASK 12-31-25-660-801 Cold Weather Maintenance Practices for Equipment/Furnishings WARNING : DO NOT OPEN OR GO NEAR PRESSURE-SEALED DOORS WHEN THE AIRCRAFT IS _______ PRESSURIZED. A PRESSURE-SEALED DOOR THAT OPENS WHEN THE AIRCRAFT IS PRESSURIZED: - WILL CAUSE EXPLOSIVE DECOMPRESSION. - CAN KILL OR CAUSE INJURY TO PERSONS AND/OR CAUSE DAMAGE TO THE AIRCRAFT/EQUIPMENT. CAUTION : BEFORE YOU SUPPLY AIR FROM AN EXTERNAL SOURCE OF THE APU, MAKE _______ CERTAIN THAT : -AT LEAST ONE COCKPIT WINDOW OR CABIN DOOR IS OPEN AND THAT IT REMAINS OPEN DURING SERVICING. -IF THE AIRCRAFT IS PARKED OUTSIDE AND IS NOT PROTECTED FROM THE RAIN ONE MAINTENANCE DOOR OR AVIONICS COMPARTMENT ACCESS DOOR IS OPEN AND THAT IT REMAINS OPEN DURING SERVICING. 1. __________________ Reason for the Job R
These procedures give the cold weather maintenance practices for the equipment/furnishings. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
2 WARNING NOTICE
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R Material No. 15-005A
AIB TN 10138 TYPE I GRADE 2 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
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C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R R R R R R
12-31-38-660-801 53-00-00-000-802 53-00-00-000-803 53-00-00-400-802 53-00-00-400-803
Cold Weather Maintenance Practices for Water/Waste Removal of the Floor Panels in the FWD Cargo-Compartment Removal of the Floor Panels in the AFT Cargo-Compartment Installation of the Floor Panels in the FWD Cargo-Compartment Installation of the Floor Panels in the AFT Cargo-Compartment
3. __________ Job Set-up Subtask 12-31-25-941-050 A. Not applicable. 4. Procedure _________ Subtask 12-31-25-660-050 A. Cargo Compartment - Door Sill Latch (1) Remove floor covering (Ref. TASK 53-00-00-000-802) (Ref. TASK 53-0000-000-803). (2) Make sure that area is clean and clear. (3) Apply a STORAGE PRESERVATION (Material No. 15-005A) to latch mechanisms. (4) Install floor covering (Ref. TASK 53-00-00-400-802) (Ref. TASK 53-0000-400-803).
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Page 202 Jan 01/01
Subtask 12-31-25-660-051 B. Cabin Escape Facilities (1) Girt Bar (a) If the aircraft is parked and not heated: - Make sure that all snow and/or slush is removed from the door exit area, before you close the doors of the aircraft. (b) Clean dirt from the floor fittings and the sliders. Do a check every 350 flight hours or more frequently as necessary. R R
(2) Do not apply grease to the cleaned area. Subtask 12-31-25-660-052 C. Escape slides (1) If the aircraft is exposed to temperature changes (from cold to warm), the pressure gages of the escape slides can give NO GO indication for a short time because the green temperature compensator cursor in the gage reacts to temperature changes faster than the gas expansion in the bottle. (2) NO GO indications may occur for short periods under the following circumstances : - if the cabin door is open in cold condition when the aircraft in being prepared or while passengers are embarking. - when the aircraft is heated for flight preparation after. (3) After closing of the doors and when the aircraft temperature becomes stable, the NO GO indication is no longer present. Subtask 12-31-25-660-053 D. Galley Equipment (1) You must drain all the galley equipment which contains water, such as coffee makers and water boilers. (2) You must operate the taps several times to make sure that the supply lines are empty (Ref. TASK 12-31-38-660-801). (3) If the conditions to drain all the galley equipment cannot be carried out, the heating recommendations should be used as follows :
EFF : ALL 12-31-25 SROS
Page 203 Apr 01/05
---------------------------------------------------------------------------| OUTSIDE AIR |EXTERNAL HEAT | APU | SUPERVISOR | DRAINING OF | | TEMPERATURE | SOURCE | | | WATER SYSTEM | |--------------|--------------|--------------|--------------|--------------| | 0 deg.C | 1 HOUR | | | | | (32 deg.F) | | | | | | to | EVERY | NO | NO | NO | | -5 deg.C | | | | | | (23 deg.F) | 4 HOURS | | | | |--------------|--------------|--------------|--------------|--------------| | -5 deg.C | 2 HOURS | | | | | (23 deg.F) | | | | | | to | EVERY | NO | NO | NO | | -10 deg.C | | | | | | (14 deg.F) | 4 HOURS | | | | |--------------|--------------|--------------|--------------|--------------| | -10 deg.C | | | | | | (14 deg.F) | | | | | | to | CONTINUOUS | NO | NO | NO | | -15 deg.C | | | | | | (5 deg.F) | | | | | |--------------|--------------|--------------|--------------|--------------| | BELOW | | AS | | | | -15 deg.C | CONTINUOUS | REQUIRED | YES | YES | | (5 deg.F) | | | | | ---------------------------------------------------------------------------Subtask 12-31-25-620-050 E. First Aid Kits (1) Remove the first aid kits from the aircraft if the cabin temperature is below -10 deg.C (+14.00 deg.F). R R
(2) To avoid damage to the kit equipment keep the kits in a place with a temperature between min. 1 deg.C (33.80 deg.F) and 40 deg.C (104.00 deg.F) max.
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(3) Put a WARNING NOTICE in position to tell personnel that the first aid kits are removed.
EFF : ALL 12-31-25 SROS
Page 204 Apr 01/05
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**ON A/C 001-049, 201-202, 251-252, 255-299, 401-449, 451-499, 701-749, Subtask 12-31-25-620-051 F. Doctors Kit (7610MX) (1) Remove the doctors kits from the aircraft if the cabin temperature is less than 1 deg.C (33.80 deg.F). NOTE : To avoid damage to the kit equipment keep the kits in a place ____ with a temperature between min. 1 deg.C (33.80 deg.F) and 40 deg.C (104.00 deg.F) max. (2) Put a WARNING NOTICE in position to tell personnel that the doctors kits are removed.
R EFF : 001-049, 201-202, 251-252, 255-299, 12-31-25 401-449, 451-499, 701-749, SROS
Page 205 Jul 01/05
COLD WEATHER MAINTENANCE - FLIGHT CONTROLS - MAINTENANCE PRACTICES __________________________________________________________________ TASK 12-31-27-660-801 Cold Weather Maintenance Procedures for Flight Controls WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. 1. __________________ Reason for the Job This procedure gives the instructions to lubricate the flight controls in cold weather conditions. 2. ______________________ Job Set-up Information A. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 10-001 Material No. 10-003 Material No. 10-004
USA AMS 1424 DE-ICING FLUID AEA/ISO TYPE I ISO 11075 (Ref. 20-31-00) USA AMS 1428 ANTI/DE-ICING FLUID AEA/ISO TYPE II ISO 11078 (Ref. 20-31-00) USA AMS 1428 ANTI ICE/DE ICINGFLUID TYPE IV (Ref. 20-31-00)
EFF : ALL 12-31-27 R SROS
Page 201 Jan 01/07
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-22-27-640-803 12-22-27-640-804 12-22-27-640-806 12-31-11-660-801
Lubrication of Flap Track/Carriage (1-5) Roller Bearings Lubrication of all Slat Track Roller Bearings, Pinion Bearings, Rack and Pinion Teeth and Slat Track 2 and 3 Lever Bearings Lubrication of Flap Steady Bearings Anti-Icing Protection
3. __________ Job Set-up Subtask 12-31-27-941-050 A. Not applicable. 4. Procedure _________ Subtask 12-31-27-660-050 A. Check of the Flight Controls (1) Make sure that ice and/or snow is not forced into the areas between the flight control surfaces during the deicing procedures. (2) Remove any ice from : - the wing leading edge - the slats - the flaps - the spoilers - the ailerons (3) You must retract the wing flaps and slats during periods of snowfall and icing conditions. If it is necessary to operate these controls, make sure that they are clear of accumulation before retraction. R R R R
(4) If an aircraft arrives with the slats and flaps in a position other than fully retracted during a period of ice or snow conditions, those slats and flaps which are extended must be inspected for ice and snow accumulation before retracting.
EFF : ALL 12-31-27 SROS
Page 202 Jan 01/07
(5) All control surfaces must have no ice, snow or frost. After the deicing operation, do a check of the associated hinges, tracks, actuators and servo controls for trapped moisture that can freeze. Apply anti-icing fluid for protection ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-001), ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-003) or ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-004) (Ref. TASK 12-31-11-660-801) (6) Do a check of the leading edge area of the spoilers, the flaps for ice, snow and frost. (7) Final checks after aircraft deicing on flap/slat areas : the applicable areas must have no snow and ice as well as water accumulation. During snowfall, freezing rain and drifting snow it is possible that snow and melting ice go into slots, drainage openings, hinges and operating linkage and will freeze again. You must do the check of these areas with special attention when an aircraft has been parked outside for a long period under the above conditions. Subtask 12-31-27-660-051 B. Lubrication of the Flaps and Slats (1) Do the applicable flap/slat lubrication tasks (Ref. TASK 12-22-27640-803) (Ref. TASK 12-22-27-640-804) (Ref. TASK 12-22-27-640-806) (2) The winter preparation program should include the flap and slat lubrication. NOTE : In climates where the atmosphere is both particularly cold and ____ humid (mist/fog) use your experience to reduce the lubrication task intervals during winter operations. NOTE : In extreme climates and low ambient temperatures it may be ____ difficult to lubricate the flap and slat systems correctly. If hangar space is not available then it is recommended to do the lubrication tasks at a station where the appropriate facilities are available or where the ambient temperature is above 0 deg.C (32.00 deg.F).
R R R
(3) Increases in grease stiffness may occur if water present within a lubricant forms discrete lumps of ice, the associated increases in system friction may then result in torque limiter operation. (4) When you do the lubrication tasks take care to ensure that all the old grease is removed in order to reduce the risk of an increase in grease stiffness.
EFF : ALL 12-31-27 SROS
Page 203 Jan 01/07
COLD WEATHER MAINTENANCE - FUEL - MAINTENANCE PRACTICES _______________________________________________________ TASK 12-31-28-660-801 Cold Weather Maintenance Practices for the Fuel System WARNING : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND DAMAGE. _______ WARNING : MAKE SURE THE AREA AROUND THE AIRCRAFT IS SAFE BEFORE YOU START A _______ REFUEL/DEFUEL PROCEDURE. IN THIS SAFE AREA, DO NOT LET PERSONS: - SMOKE - MAKE SPARKS OR FIRE - USE ANY EQUIPMENT WHICH IS NOT APPROVED FOR THE TASK. AIRCRAFT FUEL IS FLAMMABLE. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
hot air blower safety barriers surface contact thermometer
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-32-28-281-803 R R
12-32-28-281-810 28-00-00-610-801
Operate Water Drain Valves to Drain Accumulated Water from Trim Tank and Trim Vent Surge Tank Operate Water Drain Valves to Drain Accumulated Water from Center, Inner, Outer and Wing Vent Surge Tanks Fuel Safety Procedures
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Page 201 Apr 01/05
3. __________ Job Set-up Subtask 12-31-28-869-050 A. General Information This procedure gives the cold weather maintenance practices for the fuel system when an aircraft is operated or stored in conditions with ground temperatures of between 0 deg.C (32 deg.F) and -54 deg.C (-67 deg.F). The fuel storage and handling conditions can have an important effect on the amount of water in solution with the fuel. In unsatisfactory conditions, each 3785 liters (1000 USgal) of fuel can contain up to 0.76 l (0.2 USgal) of water. Water can get into the tanks in different ways: - the fuel supplied to the aircraft contains water - the air in the tank contains moisture (water) - during descent large quantities of moist air can enter the tank - fuel which is open to dampness or wet atmospheric conditions will contain larger quantities of water than fuel stored in sealed containers. In cold conditions, much of this water can come out of solution and fall to the bottom of the tank. It then collects at the lowest parts of the tank and can form ice. The formation of ice (and the presence of water) in the fuel tanks can have an effect on the accuracy and/or performance of the quantity indication system. It can also cause engine or corrosion related problems. Approved anti-ice additive can be added, in the correct proportions, to the fuel which is supplied to the aircraft. This can prevent water in the fuel from freezing and let it be drained from a tank with a fuel temperature below 0 deg.C (32 deg.F). The ice in the fuel tank can be melted through these procedures: - ambient air heat in a hangar - a refuel with warm fuel - warm air heat from a blower, until the temperature of the whole of the bottom skin is 1 deg.C (34 deg.F). This procedure is usually done in a hangar, but can be used outside if a hangar is not available - a combination of these methods. NOTE : Ice can form on the inside of the fuel tank close to ____ drain valve. When you drain fuel from the tank for a analysis check, fuel flows over the ice and collects can cause incorrect analysis results. The procedure that follows should remove most of the from the fuel tank.
the water water water. This water/ice
EFF : ALL 12-31-28 SROS
Page 202 Apr 01/98
You must do the water drain procedure regularly to make sure that all the water is drained from the tank low points. Subtask 12-31-28-941-050 B. Safety Precautions WARNING : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND _______ DAMAGE. (1) You must obey the safety procedures when you do work on the fuel system (Ref. TASK 28-00-00-610-801). (2) Put the safety barriers in position. 4. Procedure _________ R R
Subtask 12-31-28-660-050-A A. Water Draining of the Tanks
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CAUTION : DO NOT USE FORCE TO OPEN THE WATER DRAIN VALVES. THIS PREVENTS _______ DAMAGE TO THE VALVES.
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(1) If a water drain does not open with the usual pressure, find the cause. The valve could be frozen because of the low temperature.
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(2) Water draining of the tanks (aircraft in a hangar)
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(a) If possible, refuel the aircraft with warm fuel.
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(b) Use a surface contact thermometer to measure the temperature of the bottom skin of the tank to be drained.
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(c) If necessary, use an approved hot air blower to warm the bottom skin of the tank to be drained. Make sure the temperature of the bottom skin does not increase to more than 50 deg.C (122 deg.F).
R R R
NOTE : The temperature of all the bottom skin should be 1 deg.C ____ (34 deg.F) or more measured one minute after the removal of the hot air blower.
R R R
(d) Drain accumulated water (Ref. TASK 12-32-28-281-810) 30 minutes after the aircraft has been refuelled (and before the bottom skin temperature decreases below 0 deg.C (32 deg.F)).
EFF : ALL 12-31-28 SROS
Page 203 Apr 01/05
R R R R
NOTE : When you do the water drain procedure, it can be necessary ____ to drain large quantities of fuel to get a satisfactory HYDROKIT test result (Ref. TASK 12-32-28-281-810) and (Ref. TASK 12-32-28-281-803).
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(3) Water draining of the tanks (aircraft outside)
R R R R
CAUTION : MAKE SURE THAT THE TEMPERATURE OF THE AIR FROM THE HOT AIR _______ BLOWER IS NOT MORE THAN 50 DEG.C (122 DEG.F). IF THE TEMPERATURE IS MORE THAN 50 DEG.C (122 DEG.F) YOU CAN CAUSE DAMAGE TO THE AIRCRAFT.
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(a) If possible, refuel the aircraft with warm fuel.
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(b) Use a surface contact thermometer to measure the temperature of the bottom skin of the tank to be drained.
R R R R
NOTE : To do the procedure the temperature near to the drain ____ valves should be 1 deg.C (34 deg.F) or more. It is possible that not all of the ice will be melted, thus the drain procedure will not be fully successful.
R R R
(c) Use an approved hot air blower to warm the bottom skin of the tank to be drained. Make sure the temperature of the bottom skin does not increase to more than 50 deg.C (122 deg.F).
R R R
NOTE : The temperature of the bottom skin near to the drain valve ____ should be 1 deg.C (34 deg.F) or more measured one minute after the removal of the hot air blower.
R R R R
(d) Drain the accumulated water (Ref. TASK 12-32-28-281-810) 30 minutes after the aircraft has been refuelled (and before the bottom skin temperature near to the drain valves decreases below 0 deg.C (32 deg.F)).
R R R R
NOTE : When you do the water drain procedure, it can be necessary ____ to drain large quantities of fuel to get a satisfactory HYDROKIT test result (Ref. TASK 12-32-28-281-810) and (Ref. TASK 12-32-28-281-803).
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Subtask 12-31-28-660-051 R
B. Anti-Icing Additives (1) If you think that the fuel temperature will be less than 0 deg.C (32 deg.F) (and if it is not possible to warm the aircraft in a hangar) you can put anti-icing additives in the fuel. This makes sure that the water in the fuel does not freeze. When you add anti-icing additives to the fuel, the concentration must not be more than 0.15% by volume. You must also make sure that the additive is fully mixed with the fuel.
R R R R R
NOTE : Refer to the engine manufacturer data for approved fuel ____ additives. 5. Close-up ________ Subtask 12-31-28-942-050 A. Removal of Equipment (1) Remove the safety barriers. (2) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL 12-31-28 SROS
Page 205 Oct 01/99
______________________________________________________________________ COLD WEATHER MAINTENANCE - INDICATING/RECORDING SYSTEMS AND NAVIGATION MAINTENANCE PRACTICES _____________________ TASK 12-31-31-660-801 Cold Weather Maintenance Practices for Indicating/Recording and Navigation Systems 1. __________________ Reason for the Job This procedure gives the cold weather maintenance practices for indicating/recording and navigation systems. 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-31-21-660-801
Cold Weather Maintenance Practices for the Air Conditioning
3. __________ Job Set-up Subtask 12-31-31-941-050 A. Not applicable. 4. Procedure _________ Subtask 12-31-31-660-050 A. General (1) When the Outside Air Temperature (OAT) is very low, cold (temperature lower than -15 deg.C (+5.00 deg.F)) in the avionics compartment can cause incorrect operation of the computers. NOTE : This is only due to the cold weather conditions and not to a ____ technical malfunction.
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Subtask 12-31-31-660-051 B. Recommendations (1) Make sure that the computers are at a temperature equal to or higher than -15 deg.C (+5.00 deg.F) for correct operation. NOTE : If you energize the computers at very low temperatures the ____ following can occur. If the temperature is : - equal to or lower than -40 deg.C (-40.00 deg.F), you can cause permanent damage to the computers. - between -40 deg.C (-40.00 deg.F) and -15 deg.C (+5.00 deg.F), the computers can operate but normal operation can stop momentarily. - equal to or higher than -15 deg.C (+5.00 deg.F), the computers operate normally. (a) Preconditioning It is recommended to use the pre-conditioning procedure to increase the temperature in the avionics compartment (Ref. TASK 12-31-21-660-801). (b) Energization of the computers If the temperature is higher than -40 deg.C (-40.00 deg.F), you can energize the computers to increase the temperature to -15 deg.C (+5.00 deg.F). The time necessary to increase the temperature will change with the OAT, the humidity and the time since the avionics compartment ventilation stopped.
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COLD WEATHER MAINTENANCE - LANDING GEAR - MAINTENANCE PRACTICES _______________________________________________________________ TASK 12-31-32-660-801 Cold Weather Maintenance Practices for the Landing Gear 1. __________________ Reason for the Job This procedure gives the cold weather maintenance practices for the tires and precautions for towing. 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-41-00-220-801
Check Tire Pressures
3. __________ Job Set-up Subtask 12-31-32-941-050 A. Not applicable. 4. Procedure _________ Subtask 12-31-32-660-050 A. General (1) When there is a decrease in the ambient temperature, the tire pressures also decrease. A 3 deg.C (5.4 deg.F) change in temperature causes a 1 percent change in tire pressure. R R
NOTE : The tires wear faster if the pressure in the tires are low. ____ Low tire pressure can increase the risk of tire failure.
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Page 201 Jul 01/02
Subtask 12-31-32-660-051 B. Recommendations (1) Tire pressure check (a) When the aircraft is parked in cold weather conditions (cold soak) for more than one hour, do a check of the tire pressure (Ref. TASK 32-41-00-220-801). R R R
(b) You must use dry nitrogen to correct the tire pressure. Moisture in air can change to ice in the valve, which causes a permanent leak. However, if dry nitrogen is not available at outstations, air can be used with the limitations that follow: - the total content of oxygen is less than 5% volume - the tire inflation valve does not leak after inflation - the air does not stay in the tire for more than 15 hours. You must service the tire with dry nitrogen at the end of this time.
R R
(c) If a tire is inflated with air, you must record this in the maintenance log. (2) Towing precautions Be careful during aircraft towing operations in cold weather conditions. Do not make small-radius turns which can cause too much load on the sidewalls of the tires.
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TASK 12-31-32-916-801
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Cold Weather Protection for the Landing Gear Axles
R R R R R R R
WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS.
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WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED ON THE _______ LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR.
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1. __________________ Reason for the Job
R R R R
To give more corrosion protection to the landing gear axles when de-icing fluids are used during cold weather. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment
R R R
------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R R
No specific No specific No specific
R
Aerospec Protect 1 SPATULA - NON METALLIC AR WARNING NOTICE
B. Consumable Materials
R R R
------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R R R R R
Material No. 08-074 Material No. 11-002 Material No. 19-003
MASKING TAPE (Ref. 20-31-00) USA MIL-PRF-680 DRY CLEANING SOLVENT (VARSOL/WHITE SPIRIT) (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
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C. Referenced Information
R R R
------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R R R R R R R
32-00-00-481-801
R
3. __________ Job Set-up
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Subtask 12-31-32-941-051
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A. Safety Precautions
32-41-14-000-801 32-41-14-400-801 12-31-32-991-001
Installation of the Safety Devices on the Landing Gears Removal of the MLG Axle Sleeve (6560GG,6561GG,6562GG,6563GG,6564GG,6565GG, 6566GG,6567GG) Installation of the MLG Axle Sleeve (6560GG,6561GG,6562GG,6563GG,6564GG, 6565GG,6566GG,6567GG) Fig. 201
R R
(1) Make sure that the safety devices are installed on the landing gear (Ref. TASK 32-00-00-481-801).
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(2) On the panel 312VU make sure the landing gear is in the down position.
R R R R
(3) Put a WARNING NOTICE: - on the applicable MLG ground-opening handle to tell persons not to operate the handle - on the panel 312VU to tell persons not to operate the landing gear.
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Subtask 12-31-32-010-050 B. Get Access
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(1) Remove the applicable MLG axle sleeve(s) (Ref. TASK 32-41-14-000801).
EFF : ALL 12-31-32 SROS
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R R R R
4. Procedure _________ (Ref. Fig. 201/TASK 12-31-32-991-001) Subtask 12-31-32-916-050 A. Application of Corrosion Protection on the Landing Gear Axles
R R R R R R R R R
WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL _______ MATERIALS ONLY WITH A GOOD FLOW OF AIR THROUGH THE WORK AREA. THESE MATERIALS ARE POISONOUS AND FLAMMABLE AND SKIN IRRITANTS. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
R R R R R
CAUTION : MAKE SURE THAT THE CLEANING AGENTS OR SOLVENTS DO NOT GET IN OR _______ ON : - COMPONENT PARTS - PROTECTIVE COVERS - ELECTRICAL WIRING AND CONNECTORS.
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(1) Use a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-002) to clean the landing gear axle to remove the used Aerospec Protect.
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(2) Do a visual inspection to make sure that the axle is serviceable and there is no corrosion.
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NOTE : If you find corrosion refer to AIRBUS for the repair ____ procedure.
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(3) Apply BONDING AND ADHESIVE COMPOUNDS (Material No. 08-074) to the area of the axle that is not applicable.
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(4) Refer to the manufacturers instructions to apply a thin, smooth layer of Aerospec Protect on the axle.
R R R R
NOTE : During application of the Aerospec Protect you must: ____ - keep the aerosol container vertical. - make sure you have applied the aerosol spray over the full applicable area.
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Cold Weather Protection for the Landing Gear Axles - Location and Details Figure 201/TASK 12-31-32-991-001
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(5) Wait for a minimum of 1 minute drying time, do steps (4) to (5) until you get a satisfactory layer of Aerospec Protect.
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NOTE : Refer to the manufactures instructions for drying times. These ____ can change with local conditions.
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(6) Remove the BONDING AND ADHESIVE COMPOUNDS (Material No. 08-074) from the axle.
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(7) Use a SPATULA - NON METALLIC to make the edges of the Aerospec Protect smooth.
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(8) Use a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-002) to remove unwanted Aerospec Protect.
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Subtask 12-31-32-410-050 B. Close Access
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NOTE : Make sure you do not damage the corrosion protection you have ____ applied to the axle.
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(1) Install the applicable axle sleeve(s) (Ref. TASK 32-41-14-400-801).
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5. Close-up ________
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Subtask 12-31-32-942-050
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A. Removal of Equipment
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(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
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COLD WEATHER MAINTENANCE - OXYGEN - MAINTENANCE PRACTICES _________________________________________________________ TASK 12-31-35-660-801 Cold Weather Maintenance - Oxygen System 1. __________________ Reason for the Job This procedure gives the cold weather maintenance practices for the oxygen system. 2. ______________________ Job Set-up Information A. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 05-004
USA MIL-PRF-25567 TYPE I OXYGEN LEAK DETECTOR (Ref. 20-31-00)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R
12-14-35-600-801 12-33-21-618-801 35-11-41-000-801 35-11-41-400-801
Servicing of the Oxygen Replenishing Pre-conditioning through the Low-Pressure Ground Connection Removal of the Oxygen Cylinder/Valve Assy Installation of the Oxygen Cylinder/Valve Assy
3. __________ Job Set-up Subtask 12-31-35-941-050 A. Not applicable.
EFF : ALL 12-31-35 SROS
Page 201 Jul 01/06
4. Procedure _________ Subtask 12-31-35-660-050 A. Installation of Oxygen Cylinder(s). (Ref. TASK 35-11-41-000-801) (Ref. TASK 35-11-41-400-801) NOTE : When you replace oxygen cylinder(s), you must mandatorily obey the ____ Removal/Installation procedure for oxygen cylinder(s). (1) If you replace the oxygen cylinder(s) of the crew oxygen system when the ambient temperature is -20 deg.C (-4.00 deg.F) or less : - make sure that the temperature in the oxygen cylinder compartment is more than -20 deg.C (-4.00 deg.F). If this temperature is -20 deg.C (-4.00 deg.F) or less, the SPECIAL MATERIALS (Material No. 05-004) used to do the leak test will freeze. (2) It is recommended to replace the cylinder after a flight but before the compartment temperature is -20 deg.C (-4.00 deg.F). Or you can do this task while you pre-condition the aircraft on the ground. (Ref. TASK 12-33-21-618-801) Subtask 12-31-35-660-051 B. Replenishment of Oxygen Cylinder(s). (Ref. TASK 12-14-35-600-801) NOTE : When you fill oxygen cylinder(s), you must mandatorily obey the ____ replenishment procedure for oxygen cylinder(s). (1) The maximum charging pressure of the cylinder changes with the ambient temperature. Be careful that the pressure at which you pressurize the cylinder is not more than the maximum charging pressure.
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(2) It is recommended to fill the cylinder before the temperature in the oxygen cylinder compartment is -20 deg.C (-4.00 deg.F) but only after : - the aircraft network is de-energized, - the aircraft and equipment are bonded to ground.
EFF : ALL 12-31-35 SROS
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COLD WEATHER MAINTENANCE - WATER/ WASTE - MAINTENANCE PRACTICES _______________________________________________________________ TASK 12-31-38-660-801 Cold Weather Maintenance Practices for Water/Waste CAUTION : MAKE SURE THAT THE TEMPERATURE OF THE AIR FROM THE HOT AIR BLOWER IS _______ NOT MORE THAN 50 DEG.C (122 DEG.F). IF THE TEMPERATURE IS MORE THAN 50 DEG.C (122 DEG.F) YOU CAN CAUSE DAMAGE TO THE AIRCRAFT. CAUTION : BEFORE YOU SUPPLY AIR FROM AN EXTERNAL SOURCE OF THE APU, MAKE _______ CERTAIN THAT : -AT LEAST ONE COCKPIT WINDOW OR CABIN DOOR IS OPEN AND THAT IT REMAINS OPEN DURING SERVICING. -IF THE AIRCRAFT IS PARKED OUTSIDE AND IS NOT PROTECTED FROM THE RAIN ONE MAINTENANCE DOOR OR AVIONICS COMPARTMENT ACCESS DOOR IS OPEN AND THAT IT REMAINS OPEN DURING SERVICING. R R R R
CAUTION : IN FREEZING CONDITIONS, MAKE SURE THAT SERVICE PANELS OR CAPS ARE NOT _______ FROZEN BEFORE YOU TRY TO OPEN THEM. IF THE SERVICE PANELS OR CAPS ARE FROZEN, YOU MUST APPLY HOT AIR TO DE-ICE THEM FIRST. IF YOU TRY TO OPEN THEM WHEN THEY ARE FROZEN, YOU CAN CAUSE DAMAGE TO THEM. 1. __________________ Reason for the Job To prevent damage to the water/waste system by ice when the aircraft is not supplied with power or other sources of hot air. NOTE : Although an aircraft is resistant to very low ambient temperatures, ____ the cabin air conditioning (and WIPU system) keep the pipes (and water systems sufficiently warm to prevent them) from freezing. However, when the aircraft is not energized or stays on the ground at sub-zero temperatures, you must do additional procedures to prevent damage to the systems by ice.
R 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 CART - SERVICING, TOILET
EFF : ALL 12-31-38 SROS
Page 201 Jan 01/07
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 14-001A DEODORANT AIRCRAFT TOILET NON FORMALDE- HYDE BASE (Ref. 20-31-00) C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-15-38-613-801 12-24-38-680-801 12-33-21-618-801 38-10-00-614-801 38-10-00-614-803 38-31-00-680-801
Fill the Potable Water System (Aircraft Electrical Power Available) Draining of the Potable Water System (with Electrical Power) Pre-conditioning through the Low-Pressure Ground Connection Pressurization of the Potable Water System Release of the Pressure from the Potable Water System Draining of the Waste Holding Tanks
3. __________ Job Set-up Subtask 12-31-38-941-050 A. There is no special job set-up for this task. 4. Procedure _________ Subtask 12-31-38-660-050 A. Pre-Flight (First Flight of the Day) (1) After draining of the water/waste system due to low ambient temperatures you must obey the steps that follow. (2) Make sure that all drain valves are closed.
EFF : ALL 12-31-38 R SROS
Page 202 Jul 01/06
(3) Potable Water System (a) Fill the potable water system (Ref. TASK 12-15-38-613-801) with warm potable water of 30 deg.C (86.00 deg.F) not earlier than 30 minutes before the engine start. (b) Pressurize the potable water system (Ref. TASK 38-10-00-614-801) and examine the fill/drain valve for leaks. (c) Remove excessive water from around the service panel before you close it. (4) Waste System (a) Pre-charge the waste holding tanks not earlier than 30 minutes before the engine start: - Use a CART - SERVICING, TOILET to fill each waste holding tank with 18 l (4.8 USgal) of DISINFECTANTS (Material No. 14-001A). (b) Remove excessive liquid from around the service panel before you close it. R
**ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, 701-749, Subtask 12-31-38-660-051 B. Post Flight (Last Flight of the Day but not Transit Stops) (Ref. TASK 3831-00-680-801) (Ref. TASK 12-24-38-680-801) (1) General (a) Do the servicing of the potable water system and waste water tanks as soon as possible after a flight. (b) Read tables 1 and 2 (draining of the water and waste system) to find if it is necessary to drain the water and waste from the system. (c) After draining of the system and parking of the aircraft at temperatures below 0 deg.C (32.00 deg.F): - Let the drain valves and the service panels stay open to let remaining fluid to flow out. - Do not install the caps on the drain and the fill/drain nipples.
EFF : ALL 12-31-38 SROS
Page 203 Jul 01/05
NOTE : If you install the caps, the remaining fluid can freeze ____ immediately behind the drain and fill/drain caps and will cause: - Damage to the piping system - The system to become unserviceable - Delay at the next servicing. ------------------------------------------------------------------------------| TABLE 1 | |-----------------------------------------------------------------------------| | CONFIGURATION | | WATER | -------------------------------------------------|COLD SOAK TIME| AND | | AIR | CABIN | OUTSIDE AIR | (HOURS:MIN) | WASTE | | CONDITIONING | TEMPERATURE | TEMPERATURE | | TANKS DRAIN | |--------------|-------------|-------------------|--------------|-------------| | | | BETWEEN | | NOT | | | | 0 AND -15 deg.C | ANY | REQUIRED | | | ABOVE | (32 AND 5 deg.F) | | | | ON | 10 deg.C |-------------------|--------------|-------------| | | (50 deg.F) | BELOW | | | | | | -15 deg.C | 1:15 | | | | | (5 deg.F) | | | |--------------|-------------|-------------------|--------------| | | | | BETWEEN | | | | | | 0 AND -7 deg.C | 1:30 | | | | |(32 AND 19.4 deg.F)| | | | | |-------------------|--------------| | | OFF | | BETWEEN | | REQUIRED | | | | -7 AND -15 deg.C | 0:30 | | | | | (19.4 AND 5 deg.F)| | | | | |-------------------|--------------| | | | | BELOW | | | | | | -15 deg.C | ANY | | | | | (5 deg.F) | | | ------------------------------------------------------------------------------(2) Potable water system CAUTION : DO NOT OPEN THE ELECTRICAL DRAIN VALVES FOR LONGER THAN _______ NECESSARY IF YOU USE THE APU OR ENGINE(S) TO PRESSURIZE THE SYSTEM. IF THE VALVES STAY OPEN TOO LONG, THE HOT BLEED AIR CAN CAUSE DAMAGE TO THE TANK QUANTITY TRANSMITTER. (a) If you park the aircraft at very low temperature: - Drain the water from the potable water system, - Remove the remaining water from the potable water system, as stated below:
R EFF : 001-049, 201-249, 251-252, 255-299, 12-31-38 401-449, 451-499, 701-749, SROS
Page 204 Jul 01/05
1 _
Drain the potable water system (Ref. TASK 12-24-38-680-801).
2 _
Close all the lavatory and galley manual shutoff valves.
3 _
Close all the potable-water drain and fill drain valves.
4 _
Pressurize the potable water system (Ref. TASK 38-10-00-614801).
5 _
To remove the remaining water from the potable water system do the procedure as follows: NOTE : This procedure is the same for all lavatories and ____ galleys which have potable water supplied equipment (as there are water heater, coffeemaker and water faucet). a _
Open one related manual shutoff valve of one lavatory or galley.
b _
Operate the faucet (HOT and COLD).
c _
Make sure that air but no water comes out of the faucet.
d _
Flush the toilet as often as necessary until you are sure that air but no water comes out of the toilet rinse valve.
e _
Close the related manual shutoff valve.
f _
Do the whole procedure for all lavatories and galleys which have potable-water supplied equipment.
6 _
Open all drain valves of the potable water system and release the pressure from the potable water system (Ref. TASK 38-1000-614-803).
7 _
Open the manual shutoff valves in all lavatories or galleys.
(b) If you cannot drain the potable water system: - Do the pre-conditioning of the aircraft (Ref. TASK 12-33-21618-801) as follows:
R EFF : 001-049, 201-249, 251-252, 255-299, 12-31-38 401-449, 451-499, 701-749, SROS
Page 205 Jul 01/05
---------------------------------------------------------------------------| TABLE 2 | |--------------------------------------------------------------------------| | OUTSIDE AIR |EXTERNAL HEAT | APU | SUPERVISOR | DRAINING OF | | TEMPERATURE | SOURCE | | | WATER SYSTEM | |--------------|--------------|--------------|--------------|--------------| | 0 deg.C | 1 HOUR | | | | | (32 deg.F) | | | | | | to | EVERY | NO | NO | NO | | -5 deg.C | | | | | | (23 deg.F) | 4 HOURS | | | | |--------------|--------------|--------------|--------------|--------------| | -5 deg.C | 2 HOURS | | | | | (23 deg.F) | | | | | | to | EVERY | NO | NO | NO | | -10 deg.C | | | | | | (14 deg.F) | 4 HOURS | | | | |--------------|--------------|--------------|--------------|--------------| | -10 deg.C | | | | | | (14 deg.F) | | | | | | to | CONTINUOUS | NO | NO | NO | | -15 deg.C | | | | | | (5 deg.F) | | | | | |--------------|--------------|--------------|--------------|--------------| | BELOW | | AS | | | | -15 deg.C | CONTINUOUS | REQUIRED | YES | YES | | (5 deg.F) | | | | | ---------------------------------------------------------------------------**ON A/C 301-399, Subtask 12-31-38-660-051-A B. Post Flight (Last Flight of the Day but not Transit Stops) (Ref. TASK 3831-00-680-801) (Ref. TASK 12-24-38-680-801) (1) General (a) Push the auto-flush pushbutton on the 5001VE panel. (This starts two flush cycles in the LD-LAVs to prevent waste deposit build up or freezing in the waste pipes). (b) Do the servicing of the potable water system and waste water tanks as soon as possible after a flight.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-31-38 301-399, 401-449, 451-499, 701-749, SROS
Page 206 Jul 01/05
(c) Read tables 1 and 2 (draining of the water and waste system) to find if it is necessary to drain the water and waste from the system. R R R R R R
(d) After draining of the system and parking of the aircraft at temperatures below 0 deg.C (32.00 deg.F): - Let the drain valves and the service panels stay open to let remaining fluid to flow out. - Do not install the caps on the drain and the fill/drain nipples.
R R R R R R R
NOTE : If you install the caps, the remaining fluid can freeze ____ immediately behind the drain and fill/drain caps and will cause: - Damage to the piping system - The system to become unserviceable - Delay at the next servicing. ------------------------------------------------------------------------------| TABLE 1 | |-----------------------------------------------------------------------------| | CONFIGURATION | | WATER | -------------------------------------------------|COLD SOAK TIME| AND | | AIR | CABIN | OUTSIDE AIR | (HOURS:MIN) | WASTE | | CONDITIONING | TEMPERATURE | TEMPERATURE | | TANKS DRAIN | |--------------|-------------|-------------------|--------------|-------------| | | | BETWEEN | | NOT | | | | 0 AND -15 deg.C | ANY | REQUIRED | | | ABOVE | (32 AND 5 deg.F) | | | | ON | 10 deg.C |-------------------|--------------|-------------| | | (50 deg.F) | BELOW | | | | | | -15 deg.C | 1:15 | | | | | (5 deg.F) | | | |--------------|-------------|-------------------|--------------| | | | | BETWEEN | | | | | | 0 AND -7 deg.C | 1:30 | | | | |(32 AND 19.4 deg.F)| | | | | |-------------------|--------------| | | OFF | | BETWEEN | | REQUIRED | | | | -7 AND -15 deg.C | 0:30 | | | | | (19.4 AND 5 deg.F)| | | | | |-------------------|--------------| | | | | BELOW | | | | | | -15 deg.C | ANY | | | | | (5 deg.F) | | | -------------------------------------------------------------------------------
EFF : 301-399, 12-31-38 SROS
Page 207 Jul 01/04
(2) Potable water system CAUTION : DO NOT OPEN THE ELECTRICAL DRAIN VALVES FOR LONGER THAN _______ NECESSARY IF YOU USE THE APU OR ENGINE(S) TO PRESSURIZE THE SYSTEM. IF THE VALVES STAY OPEN TOO LONG, THE HOT BLEED AIR CAN CAUSE DAMAGE TO THE TANK QUANTITY TRANSMITTER. (a) If you park the aircraft at very low temperature: - Drain the water from the potable water system, - Remove the remaining water from the potable water system, as stated below: 1 _
Drain the potable water system (Ref. TASK 12-24-38-680-801).
2 _
Close all the lavatory and galley manual shutoff valves.
3 _
Close all the potable-water drain and fill drain valves.
4 _
Pressurize the potable water system (Ref. TASK 38-10-00-614801).
5 _
To remove the remaining water from the potable water system do the procedure as follows: NOTE : This procedure is the same for all lavatories and ____ galleys which have potable water supplied equipment (as there are water heater, coffeemaker and water faucet). a _
Open one related manual shutoff valve of one lavatory or galley.
b _
Operate the faucet (HOT and COLD).
c _
Make sure that air but no water comes out of the faucet.
d _
Flush the toilet as often as necessary until you are sure that air but no water comes out of the toilet rinse valve.
e _
Close the related manual shutoff valve.
f _
Do the whole procedure for all lavatories and galleys which have potable-water supplied equipment.
EFF : 301-399, 12-31-38 R SROS
Page 208 Jul 01/04
R R R
6 _
Open all drain valves of the potable water system and release the pressure from the potable water system (Ref. TASK 38-1000-614-803).
R
7 _
Open the manual shutoff valves in all galleys and lavatories.
(b) If you cannot drain the potable water system: - Do the pre-conditioning of the aircraft (Ref. TASK 12-33-21618-801) as follows: ---------------------------------------------------------------------------| TABLE 2 | |--------------------------------------------------------------------------| | OUTSIDE AIR |EXTERNAL HEAT | APU | SUPERVISOR | DRAINING OF | | TEMPERATURE | SOURCE | | | WATER SYSTEM | |--------------|--------------|--------------|--------------|--------------| | 0 deg.C | 1 HOUR | | | | | (32 deg.F) | | | | | | to | EVERY | NO | NO | NO | | -5 deg.C | | | | | | (23 deg.F) | 4 HOURS | | | | |--------------|--------------|--------------|--------------|--------------| | -5 deg.C | 2 HOURS | | | | | (23 deg.F) | | | | | | to | EVERY | NO | NO | NO | | -10 deg.C | | | | | | (14 deg.F) | 4 HOURS | | | | |--------------|--------------|--------------|--------------|--------------| | -10 deg.C | | | | | | (14 deg.F) | | | | | | to | CONTINUOUS | NO | NO | NO | | -15 deg.C | | | | | | (5 deg.F) | | | | | |--------------|--------------|--------------|--------------|--------------| | BELOW | | AS | | | | -15 deg.C | CONTINUOUS | REQUIRED | YES | YES | | (5 deg.F) | | | | | ----------------------------------------------------------------------------
EFF : 301-399, 12-31-38 SROS
Page 209 Jul 01/03
COLD WEATHER MAINTENANCE - AIRBORNE AUXILIARY POWER - MAINTENANCE PRACTICES ___________________________________________________________________________ TASK 12-31-49-660-801 Cold Weather Maintenance Practices for the Auxiliary Power Unit 1. __________________ Reason for the Job This procedure gives the cold weather maintenance practices for the Auxiliary Power Unit (APU) when the aircraft is in a cold soak condition. 2. ______________________ Job Set-up Information A. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 03-003
USA MIL-PRF-7808 LUBRICATING OIL TURBINE SYNTHETIC BASE (Ref. 20-31-00)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-31-24-660-801 12-33-21-618-801 12-33-21-618-801 12-33-21-618-801 24-41-00-861-801 49-00-00-860-801 49-00-00-860-801 49-00-00-860-802 49-61-34-000-801 49-61-34-400-801 49-91-00-600-801
Cold Weather Maintenances for Electrical Power Ground Air Pre-conditioning through the Low-Pressure Ground Connection Ground Air Pre-conditioning through the High-Pressure Ground Connection Ground Air Pre-conditioning with the APU Energize the Aircraft Electrical Circuits from the External Power A Start of the APU with Power Supply from the APU Battery Start of the APU with External Power Supply Shutdown of the APU with Power Supply from the APU Battery Removal of the ECB (59KD) Installation of the ECB (59KD) Oil Change
EFF : ALL 12-31-49 SROS
Page 201 Apr 01/99
3. __________ Job Set-up Subtask 12-31-49-941-050 A. Not applicable. 4. Procedure _________ Subtask 12-31-49-660-050 A. Electronic Control Box 59KD (ECB 59KD) (1) If the Outside Air Temperature (OAT) is/will be lower than -40 deg.C (-40.00 deg.F) and the aircraft is not pre-conditioned (heated) alternatively: - through the LP ground connection (Ref. TASK 12-33-21-618-801), - the HP ground connection (Ref. TASK 12-33-21-618-801), or - with the APU (Ref. TASK 12-33-21-618-801). (a) Remove the ECB 59KD from the aircraft (Ref. TASK 49-61-34-000801). (b) Keep the ECB 59KD in a dry storage at a temperature of between 15 deg.C (59.00 deg.F) and 35 deg.C (95.00 deg.F). Subtask 12-31-49-660-051 B. Auxiliary Power Unit (APU) NOTE : DO NOT MIX OILS OF DIFFERENT BRANDS OR TYPES| ____ NOTE : It is recommended to use type 1 oils OILS (Material No. 03-003) ____ for APU operation in cold weather conditions. (1) Oil type. (a) If necessary, do an oil change to type 1 OILS (Material No. 03003) (Ref. TASK 49-91-00-600-801). (2) Electrical power (Ref. TASK 12-31-24-660-801). (a) If external power is available. 1 _
Energize the aircraft electrical circuits from the external power (Ref. TASK 24-41-00-861-801).
EFF : ALL 12-31-49 SROS
Page 202 Apr 01/98
2 _
On the APU section on the overhead panel 215VU, make sure that the APU MASTER SW pushbutton switch is set to OFF (the ON legend is off). NOTE : The APU oil heater increases the temperature of the oil ____ in the APU gearbox oil reservoir during cold soak condition.
(b) If no external power is available. 1 _
It is recommended to start the APU every three hours and operate it for one hour (Ref. TASK 49-00-00-860-801) (Ref. TASK 49-00-00-860-802) if the Outside Air Temperature (OAT) is lower than -30 deg.C (-22.00 deg.F). NOTE : These values are only applicable if all the access ____ doors are closed.
Subtask 12-31-49-660-052 C. APU Starting after a Cold Soak Condition (1) ECB 59KD. NOTE : Do not operate the ECB 59KD for more than 30 minutes at -40 ____ deg.C (-40.00 deg.F) or lower. (a) If the ECB was on the aircraft during the cold soak, make sure that the temperature of the ECB is higher than -40 deg.C (-40.00 deg.F). If the temperature of the ECB is lower than -40 deg.C (-40.00 deg.F), use a pre-conditioning procedure to increase the temperature of the ECB to a minimum of -40 deg.C (-40.00 deg.F) (Ref. TASK 12-33-21-618-801) or (Ref. TASK 12-33-21-618-801). (b) If the ECB was removed from the aircraft and kept at a temperature of between 15 deg.C (59.00 deg.F) and 35 deg.C (95.00 deg.F), install the ECB (Ref. TASK 49-61-34-400-801). (2) Electrical Power. (a) For the cold weather maintenance - electrical power (Ref. TASK 12-31-24-660-801). (b) Start and operate the APU (Ref. TASK 49-00-00-860-801).
EFF : ALL 12-31-49 SROS
Page 203 Apr 01/98
Subtask 12-31-49-660-053 D. Turn-Around Time For turn-around in cold weather conditions, when it is not pratical to remove equipment, it is recommended to keep the APU in operation. In this configuration : - the temperature in the cabin will not decrease, - no specific cold weather maintenance practices are necessary for the APU system.
EFF : ALL 12-31-49 SROS
Page 204 Apr 01/98
COLD WEATHER MAINTENANCE - STRUCTURE - MAINTENANCE PRACTICES ____________________________________________________________ TASK 12-31-51-660-801 Cold Weather Maintenance Practices for the Structure. 1. __________________ Reason for the Job This procedure gives the cold weather maintenance practices for the structure. 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------53-00-00-000-803 53-00-00-200-803 53-00-00-400-803
Removal of the Floor Panels in the AFT Cargo Compartment Visual Check of the Piston Drain Valves in the Lower Fuselage Shell (from Outside) and in the FWD and AFT Cargo Compartment Doors Installation of the Floor Panels in the AFT Cargo Compartment
3. __________ Job Set-up Subtask 12-31-51-941-050 A. Not applicable. 4. Procedure _________ Subtask 12-31-51-660-050 A. General (1) At the start of each winter, make sure that the drain valves in the lower fuselage are clean and operate correctly. (Ref. TASK 53-00-00200-803)
EFF : ALL 12-31-51 SROS
Page 201 Apr 01/98
(2) Ice can collect in the lower fuselage areas especially when the aircraft flies from warm, humid climates to cold climates. In some conditions, the ice can collect during more than one flight. NOTE : Water/ice in the lower fuselage can cause failure of the radio ____ altimeter. (3) When you do a check for ice in the lower fuselage, look for ice in the aft area before you look in the forward area. Ice usually collects more easily in the aft area than in the forward area. Water evaporation is faster in the forward area because of the warnm air from the avionics compartment. Subtask 12-31-51-660-051 B. Check for Ice (1) Remove a floor panel from the forward end of the aft cargo compartment. (Ref. TASK 53-00-00-000-803) (2) Look for ice in the lower fuselage. (3) If you find ice below the aft cargo compartment, look for ice below the forward cargo compartment. (4) Install the floor panel (Ref. TASK 53-00-00-400-803). (5) Frequency of check You must adapt the frequency of the check to the climatic conditions in whichthe aircraft operates. In the worst condition one check per week should be sufficient initially. Subtask 12-31-51-660-052 C. Removal of Ice (1) Warm hangar The recommended procedure is to put the aircraft in a warm hangar with cargo bay doors open. This will cause all the ice in the aircraft to melt and the water will flow out through the drain valves.
EFF : ALL 12-31-51 SROS
Page 202 Apr 01/98
(2) Hot air blower CAUTION : MAKE SURE THAT THE TEMPERATURE OF THE AIR FROM THE HOT AIR _______ BLOWER IS NOT MORE THAN 50 DEG.C (122 DEG.F). IF THE TEMPERATURE IS MORE THAN 50 DEG.C (122 DEG.F) YOU CAN CAUSE DAMAGE TO THE AIRCRAFT. You can use a hot air blower if the aircraft is parked in an open area. (3) Frequency of ice removal You must adapt the frequency of ice removal to the climatic conditions in which the aircraft operates. In the worst conditions, one overnight stop a week is usually sufficient for ice removal. (4) The procedure used to remove ice from the lower fuselage must be monitored to make sure that all water drains are working and that all the ice is removed.
EFF : ALL 12-31-51 SROS
Page 203 Apr 01/98
COLD WEATHER MAINTENANCE - DOORS - MAINTENANCE PRACTICES ________________________________________________________ TASK 12-31-52-660-801 Cold Weather Maintenance Procedures for the Doors System 1. __________________ Reason for the Job This procedure gives the cold weather maintenance practices for the doors system. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 HOT AIR BLOWER OPERATING 40 DEG C (100 DEG F)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 04-011 R
Material No. 04-017 Material No. 05-001 Material No. 11-004 Material No. 15-005A Material No. 19-003
USA MIL-G-4343 SILICONE GREASE PNEUMATIC SYST AND SEALS (Ref. 20-31-00) USA A-A-59173 SILICONE GREASE (Ref. 20-31-00) USA SAE-AS8660 INSULATING AND SEALING GREASE SILICONE (Ref. 20-31-00) USA MIL-T-81533 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (Ref. 20-31-00) AIB TN 10138 TYPE I GRADE 2 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
EFF : ALL 12-31-52 SROS
Page 201 Oct 01/04
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R
12-22-52-600-809 52-10-00-860-801 52-10-00-860-802 52-20-00-860-801 52-20-00-860-802 52-30-00-010-801 52-30-00-010-803 52-30-00-410-801 52-30-00-410-803 52-30-00-480-801 52-31-15-000-801 52-31-15-400-801 52-32-15-000-801 52-32-15-400-801 52-33-15-000-801 52-33-15-400-801
Lubrication of the Slider Mechanism on all Pax/Crew and Emergency Exit Doors Special Precautions before Work on the Passenger/Crew Door Special Precautions after Work on the Passenger/Crew Door Special Precautions before Work on the Emergency Exit Door Special Precautions after Work on the Emergency Exit Door Opening of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Opening of the BULK Cargo-Compartment Door Closing of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Closing of the BULK Cargo-Compartment Door Installation of the Safety Support Equipment Removal of the Protection Linings Installation of the Protection Linings Removal of the Protection Linings Installation of the Protection Linings Removal of the Protection Lining Installation of the Protection Lining
3. __________ Job Set-up Subtask 12-31-52-941-050 A. Get Access (1) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the applicable passenger/crew door, emergency exit door, cargo door, fuselage service panel or fuselage access door. (2) Do the related special precautions, then open the applicable passenger/crew door (Ref. TASK 52-10-00-860-801). (3) Do the related special precautions, then open the applicable emergency exit door (Ref. TASK 52-20-00-860-801).
EFF : ALL 12-31-52 SROS
Page 202 Jan 01/06
(4) Open the FWD and/or AFT cargo-compartment door (Ref. TASK 52-30-00010-801) and install the related actuator safety lock(s) (Ref. TASK 52-30-00-480-801). (5) Remove the protection linings from the FWD and/or AFT cargo-compartment door (Ref. TASK 52-31-15-000-801) and (Ref. TASK 52-32-15-000-801). (6) Open the BULK cargo-compartment door (Ref. TASK 52-30-00-010-803). (7) Remove the protection linings from the BULK cargo-compartment door (Ref. TASK 52-33-15-000-801). (8) Remove/open the applicable fuselage service panel(s) and/or access door(s). 4. Procedure _________ Subtask 12-31-52-660-055 A. Winter Preparation (1) Winter preparation of the passenger crew doors and the emergency exits. (a) Make sure that the pressure seal drains and the drain holes of the passenger/crew doors and the emergency exits are clear and not blocked. R R
(b) Make sure that the slider mechanism is correctly lubricated (Ref. TASK 12-22-52-600-809).
R R R
(c) Use a lint-free cotton cloth, MISCELLANEOUS (Material No. 19003), and the CLEANING AGENTS (Material No. 11-004) to clean these components of the passenger/crew doors and the emergency exits: - the door guide rollers, the roller fittings and the upper and lower door guide fittings - the pressure seals and their contact areas on the fuselage.
R R
(d) Apply the silicone grease, COMMON GREASE (Material No. 04-017), to the door guide rollers, the roller fittings and the upper and lower guide fittings.
R R
(e) Apply the silicone grease, SPECIAL MATERIALS (Material No. 05001), to the pressure seals and to their contact areas on the fuselage.
EFF : ALL 12-31-52 SROS
Page 203 Jan 01/06
R R
(f) Apply the temporary protective compound, STORAGE PRESERVATION (Material No. 15-005A), to these areas of the passenger/crew doors and the emergency exits: - the inner surfaces and the structure - the exterior control handle assemblies. (2) Winter preparation of the FWD, AFT and BULK cargo-compartment doors. (a) Make sure that the pressure seal drains of the cargo-compartment doors are clear and not blocked.
R R R
(b) Use a lint-free cotton cloth, MISCELLANEOUS (Material No. 19003), and the CLEANING AGENTS (Material No. 11-004) to clean these components of the applicable cargo-compartment doors: - the pressure seals and their contact areas on the fuselage - the external operating handles - the door hinges and the guide fittings - the internal mechanisms of the lock shafts, the operating handles and the latch assemblies.
R R R
(c) Apply the silicone grease, SPECIAL MATERIALS (Material No. 05001), and the silicone grease, COMMON GREASE (Material No. 04011) to the pressure seals.
R R
(d) Apply the temporary protective compound, STORAGE PRESERVATION (Material No. 15-005A), to the external control handles and the shafts.
R R
(e) Lubricate the door hinges and guide fittings. Apply the temporary protective compound, STORAGE PRESERVATION (Material No. 15-005A), to the latch assemblies and the latch spools. (f) Lubricate the internal operating mechanisms of the doors (lock shafts, operating handles and latch assemblies).
R R R
(g) Apply the temporary protective compound, STORAGE PRESERVATION (Material No. 15-005A), as a spray, to the lower internal bays of the doors. Subtask 12-31-52-660-050 B. Passenger/Crew Doors and Emergency Exit Doors (Before Flight) (1) Remove all the snow and slush from the subsequent areas before you close a passenger/crew door or an emergency exit door: - the door pressure seal - the seal contact area on the fuselage.
EFF : ALL 12-31-52 SROS
Page 204 Jan 01/06
Subtask 12-31-52-660-051 C. FWD, AFT and BULK Cargo-Compartment Doors (Before Flight) CAUTION : MAKE SURE THAT THE TEMPERATURE OF THE AIR FROM THE HOT AIR _______ BLOWER IS NOT MORE THAN 50 DEG.C (122 DEG.F). IF THE TEMPERATURE IS MORE THAN 50 DEG.C (122 DEG.F) YOU CAN CAUSE DAMAGE TO THE AIRCRAFT. (1) Remove as much snow and/or water as possible from the cargo pallets before you install them in the aircraft. NOTE : Large quantities of melting snow and water can cause the ____ cargo-compartment doors to freeze in their closed positions. (2) Do not open the cargo-compartment doors until immediately before you install the cargo pallets. (3) Close the cargo-compartment doors immediately after the installation of the cargo pallets is complete. (4) If the aircraft is parked in a hangar, open the cargo-compartment doors to their vertical positions. NOTE : This procedure will help to remove the moisture from the inner ____ surfaces of the doors. R
(5) Use a HOT AIR BLOWER OPERATING 40 DEG C (100 DEG F) to remove the ice from doors or panels that are frozen in their closed positions. Do not use hard or sharp tools to remove the ice. Subtask 12-31-52-660-052 D. Passenger/Crew Doors and Emergency Exits (After Flight) (1) Aircraft not parked in a hangar (a) Remove the snow and/or slush from the subsequent areas before you close the passenger/crew doors and/or the emergency exits: - the door pressure seals - the door contact areas on the fuselage. (b) Use a lint-free cotton cloth, MISCELLANEOUS (Material No. 19-003) and the CLEANING AGENTS (Material No. 11-004) to clean the pressure seals of the passenger/crew doors and the emergency exits.
EFF : ALL 12-31-52 SROS
Page 205 Apr 01/04
(c) Apply the silicone grease, SPECIAL MATERIALS (Material No. 05001) to the pressure seals of the passenger/crew doors and the emergency exits. (d) Make sure that the pressure seal drains and the drain holes of the passenger/crew doors and the emergency exits are clear and not blocked. (2) Aircraft parked in a hangar (a) Open the passenger/crew doors and the emergency exits. NOTE : This procedure will help to remove the moisture from the ____ inner surfaces of the doors. Subtask 12-31-52-660-053 E. FWD, AFT and BULK Cargo-Compartment Doors (After Flight) (1) Remove the snow and/or slush from the subsequent areas before you close the cargo-compartment doors: - the door pressure seals - the door contact areas on the fuselage. (2) If the aircraft flies from an airport where the ambient temperature is more than 0 deg.C (32.00 deg.F) to an airport where the ambient temperature is less than 0 deg.C (32.00 deg.F), you must: (a) Apply the temporary protective compound, STORAGE PRESERVATION (Material No. 15-005A) as a spray, to the subsequent areas of the cargo-compartment doors: - the operating mechanisms - the inner surfaces of the lower areas of the cargo doors. NOTE : This procedure will keep the effects of freezing ____ condensation to a minimum at cold airports. (3) Maintenance NOTE : The frequency of the subsequent procedure may be increased as ____ required by the operating environment. (a) Make sure that the pressure seal drains of the cargo-compartment doors are clear and not blocked.
EFF : ALL 12-31-52 R SROS
Page 206 Oct 01/02
(b) Use a lint-free cotton cloth, MISCELLANEOUS (Material No. 19-003) and the CLEANING AGENTS (Material No. 11-004) to clean these components of the applicable cargo-compartment doors: - the pressure seals and their contact areas on the fuselage R - the external operating handles - the door hinges and the guide fittings.
R
(c) Apply the silicone grease, SPECIAL MATERIALS (Material No. 05001) and the silicone grease, COMMON GREASE (Material No. 04-011) to the pressure seals. R R R R
(d) Apply the temporary protective compound, STORAGE PRESERVATION (Material No. 15-005A) to the external control handles and the shafts.
R
(e) Lubricate the door hinges and the guide fittings. Apply the temporary protective compound, STORAGE PRESERVATION (Material No. 15-005A) to the latch assemblies and the latch spools. Subtask 12-31-52-660-054 F. Service Panels (1) Apply the temporary protective compound, STORAGE PRESERVATION (Material No. 15-005A) as a spray, to the hinges and latch mechanisms of the fuselage service panels and doors. 5. Close-up ________ Subtask 12-31-52-942-050 A. Put the aircraft back to its operational configuration. (1) Make sure that the work area is clean and clear of tools and other items. (2) Do the related special precautions, then close the applicable passenger/crew doors (Ref. TASK 52-10-00-860-802). (3) Do the related special precautions, then close the applicable emergency exit doors (Ref. TASK 52-20-00-860-802). (4) Install the protection linings on the FWD and/or AFT cargo-compartment door (Ref. TASK 52-31-15-400-801) and (Ref. TASK 52-32-15-400-801).
EFF : ALL 12-31-52 SROS
Page 207 Oct 01/02
(5) Remove the actuator safety lock(s) and close the FWD and/or AFT cargo-compartment door (Ref. TASK 52-30-00-410-801). (6) Install the protection linings on the BULK cargo-compartment door (Ref. TASK 52-33-15-400-801). (7) Close the BULK cargo-compartment door (Ref. TASK 52-30-00-410-803). (8) Close/Install the applicable fuselage service panel(s) and/or access door(s). (9) Remove the access platform(s).
EFF : ALL 12-31-52 R SROS
Page 208 Oct 01/02
COLD WEATHER MAINTENANCE - POWER PLANT - MAINTENANCE PRACTICES ______________________________________________________________ TASK 12-31-71-660-801 Cold Weather Maintenance Practices of Engines 1. __________________ Reason for the Job This procedure gives the cold weather maintenance practices for the engines. 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------71-00-00-660-801 71-00-00-660-802 71-00-00-860-844
Prepare the Engine After Shutdown in Cold Weather. Prepare the Engine Before Starting in Cold Weather Power Plant Operation During Cold Weather
3. __________ Job Set-up Subtask 12-31-71-941-050 A. Not applicable. 4. Procedure _________ R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 12-31-71-660-050-A A. General (1) Prepare the engine in cold weather conditions (Ref. TASK 71-00-00660-802) and (Ref. TASK 71-00-00-660-801).
EFF : ALL 12-31-71 SROS
Page 201 Jul 01/05
R
**ON A/C 701-749,
R
Subtask 12-31-71-660-050-B
R
A. General
R R
(1) Do the power plant operation during cold weather (Ref. TASK 71-00-00860-844).
EFF : 701-749, 12-31-71 SROS
Page 202 Oct 01/03
SAMPLING FOR ANALYSIS - DESCRIPTION AND OPERATION _________________________________________________ R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 1. General _______ This section gives the instructions related to the different fluid samplings which may be done for an analysis. It includes the topics below: 12-23-24/P. Block 301 INTEGRATED DRIVE GENERATOR OIL 12-32-28/P. Block 301 FUEL 12-32-29/P. Block 301 HYDRAULIC FLUID 12-32-49/P Block 301 APU 12-32-79/P. Block 301 ENGINE OIL **ON A/C 701-749, 1. General _______ This section gives the instructions related to the different fluid samplings which may be done for an analysis. It includes the topics below: 12-23-24/P. Block 301 INTEGRATED DRIVE GENERATOR OIL 12-32-28/P. Block 301 FUEL 12-32-29/P. Block 301 HYDRAULIC FLUID 12-32-49/P Block 301 APU
EFF : ALL 12-32-00 SROS
Page 1 Jul 01/05
INTEGRATED DRIVE GENERATOR OIL - SERVICING __________________________________________ TASK 12-32-24-281-803 Sampling of the IDG Oil for Analysis WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE COMPONENTS IMMEDIATELY AFTER _______ THE ENGINE IS SHUTDOWN. THE ENGINE COMPONENTS CAN STAY HOT FOR UP TO ONE HOUR. WARNING : WEAR GOGGLES, INSULATED GLOVES AND OTHER PROTECTIVE CLOTHES. _______ HOT OIL CAN BURN YOUR EYES AND SKIN. IF OIL TOUCHES YOUR EYES OR SKIN, GET MEDICAL AID. 1. __________________ Reason for the Job To find the cause of the oil contamination (skydrol, fuel, water, chlorine, oil, degradation and other causes). NOTE : The best location and time to get an oil sample is at the case drain ____ after operation of the engine, when the IDG oil is at the operating temperature (80 deg. C (176 deg. F)). 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No
specific specific specific specific specific
DH13PM
circuit breaker(s) safety clip(s) container 5.7 l (1.5 USgal) transparent bottle 1 l (0.26 USgal) access platform 2.5 m (8 ft. 2 in.) Torque Wrench : range 36.00 to 220.00 lbf.in (0.40 to 2.60 m.daN) 1 TANK - ENGINE OIL FILLING UP
R EFF : 001-049, 201-249, 251-252, 255-299, 12-32-24 Page 301 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
P05-289
Material No. 03-002
* lockwire 0.032 in. (0.80 mm) dia. (Ref. 70-30-00) GB DEF-STAN 91-101 LUBRICATING OIL TURBINE ENGINE SYNT BASE (Ref. 20-31-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------2
O-ring
24-21-51 42A-060
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-13-24-610-801 24-42-00-861-801 24-42-00-862-801 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801 78-30-00-040-804 78-30-00-410-801 78-30-00-440-804 12-32-24-991-004
IDG Servicing - Filling of the IDG with Oil or Addition of Oil after a Level Check Energize the Ground Service Network De-energize the Ground Service Network Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Deactivation of the Thrust Reverser for Maintenance Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Reactivation of the Thrust Reverser after Maintenance Fig. 301
R EFF : 001-049, 201-249, 251-252, 255-299, 12-32-24 Page 302 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
3. __________ Job Set-up Subtask 12-32-24-861-052 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-32-24-941-052 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure. Subtask 12-32-24-010-054 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU. Subtask 12-32-24-865-054 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-32-24-010-055 E. Get Access (1) Open the aft fan cowl doors (Ref. TASK 71-13-00-010-802): - FOR 4030EM1 415BL, 416BR, - FOR 4030EM2 425BL, 426BR.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-32-24 Page 303 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
Subtask 12-32-24-040-050 F. Deactivation of the Thrust Reverser WARNING : YOU MUST DEACTIVATE THE THRUST REVERSER DIRECTIONAL CONTROL _______ VALVE (DCV) BEFORE YOU WORK ON OR AROUND THE TRANSLATING COWL. IF YOU DO NOT DEACTIVATE THE DCV, YOU CAN CAUSE ACCIDENTAL THRUST REVERSER OPERATION AND INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT. (1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 7830-00-040-804). Subtask 12-32-24-010-058 G. Get Access (1) Open the thrust reverser cowl doors (Ref. TASK 78-30-00-010-801): FOR 4030EM1 417AL, 418AR, FOR 4030EM2 427AL, 428AR. 4. Procedure _________ (Ref. Fig. 301/TASK 12-32-24-991-004) Subtask 12-32-24-864-052 A. Depressurization of the IDG Case WARNING : POINT THE OVERFLOW DRAIN HOSE INTO A CONTAINER WHEN YOU CONNECT _______ THE HOSE TO THE OVERFLOW DRAIN VALVE. THIS WILL PREVENT BURNS FROM THE HOT OIL SPRAY. HOT OIL CAN CAUSE BURNS TO EYES AND SKIN. CAUTION : DO NOT USE DEVICES OTHER THAN THE APPROVED OVERFLOW DRAIN-HOSE _______ FITTING. HARD METAL OBJECTS SUCH AS SCREWDRIVERS CAN CAUSE DAMAGE TO THE OVERFLOW DRAIN-VALVE SEAT. (1) Put a container 5.7 l (1.5 USgal) below the IDG. (2) Remove the dust cap (4) from the overflow drain valve (8). (3) Put the end of the overflow drain hose (7) of the TANK - ENGINE OIL FILLING UP (DH13PM) in the container (6).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-32-24 Page 304 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
IDG Oil Sampling for Analysis Figure 301/TASK 12-32-24-991-004 R EFF : 001-049, 201-249, 251-252, 255-299, 12-32-24 Page 305 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
(4) Do this step to depressurize the IDG case: (a) Connect the overflow drain hose (7) of the TANK - ENGINE OIL FILLING UP (DH13PM) to the overflow drain valve (8). NOTE : Some oil can come out of the overflow drain hose (7) of ____ the TANK - ENGINE OIL FILLING UP (DH13PM) when you connect it. Subtask 12-32-24-281-054 B. Oil Sampling WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. _______ CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU. NOTE : Make sure that the oil is not too hot. ____ (1) Cut and remove the lockwire from the case drain plug (1). (2) Loosen the case drain plug (1). (3) Put a transparent bottle 1 l (0.26 USgal) below the case drain port (3). NOTE : The transparent bottle (5) must be clean and sterilized. ____ (4) Slowly remove the case drain plug (1) until oil flows out of the case drain port (3). (5) Fill the transparent bottle (5) with approximately 20 ml (0.0053 USgal) of oil. (6) Seal the case drain port (3). (7) Remove the O-ring (2) from the case drain plug (1) and discard it. Subtask 12-32-24-640-052 C. Lubricate the new O-ring (2) with OILS (Material No. 03-002).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-32-24 Page 306 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
Subtask 12-32-24-420-052 D. Installation of the Case Drain Plug (1) Install the new O-ring (2) on the case drain plug (1). (2) Install the case drain plug (1) in the case drain port (3). (3) TORQUE the case drain plug (1) to between 55 and 75 lbf.in (0.62 and 0.84 m.daN). (4) Safety the case drain plug (1) with lockwire 0.032 in. (0.80 mm) dia. (Material No. P05-289). Subtask 12-32-24-281-055 E. Oil Sample Bottle (1) Send the oil sample bottle to laboratory immediately with these data: (a) Oil sampling date. (b) Type and brand of oil used. (c) Operating time since last oil sampling. (d) IDG total operating time. (e) Identification of the IDG (Serial Number). NOTE : If you do not do the analysis immediately, seal the ____ bottle. Subtask 12-32-24-020-052 F. Removal of the Overflow Drain Hose (1) Disconnect the overflow drain hose (7) of the TANK - ENGINE OIL FILLING UP (DH13PM) from the overflow drain valve (8). (2) Install the dust cap (4) on the overflow drain valve (8). Subtask 12-32-24-612-052 G. Fill the IDG with oil or add oil to the IDG after a level check (Ref. TASK 12-13-24-610-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-32-24 Page 307 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
5. Close-up ________ Subtask 12-32-24-410-054 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the thrust reverser cowl doors (Ref. TASK 78-30-00-410-801): - FOR 4030EM1 417AL, 418AR, - FOR 4030EM2 427AL, 428AR. Subtask 12-32-24-440-050 B. Make the thrust reverser serviceable after maintenance (Ref. TASK 78-3000-440-804). Subtask 12-32-24-865-055 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2 Subtask 12-32-24-410-052 D. Close Access (1) Close the protective door of the AC/DC emergency power center 740VU. (2) Close the access door 811. (3) Remove the access platform(s). (4) Close the aft fan cowl doors (Ref. TASK 71-13-00-410-802): - FOR 4030EM1 415BL, 416BR, - FOR 4030EM2 425BL, 426BR.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-32-24 Page 308 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
Subtask 12-32-24-862-052 E. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : 001-049, 201-249, 251-252, 255-299, 12-32-24 Page 309 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
INTEGRATED DRIVE GENERATOR OIL - SERVICING __________________________________________ TASK 12-32-24-281-804 Sampling of the IDG Oil for Analysis WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE COMPONENTS IMMEDIATELY AFTER _______ THE ENGINE IS SHUTDOWN. THE ENGINE COMPONENTS CAN STAY HOT FOR UP TO ONE HOUR. WARNING : WEAR GOGGLES, INSULATED GLOVES AND OTHER PROTECTIVE CLOTHES. _______ HOT OIL CAN BURN YOUR EYES AND SKIN. IF OIL TOUCHES YOUR EYES OR SKIN, GET MEDICAL AID. 1. __________________ Reason for the Job To find the cause of the oil contamination (skydrol, fuel, water, chlorine, oil, degradation and other causes). R R R
NOTE : The best location and time to get an oil sample is at the case drain ____ after operation of the engine, when the IDG oil is at the operating temperature (80 deg.C (176 deg.F)). 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No
specific specific specific specific specific
DH13PM
circuit breaker(s) safety clip(s) container 5.7 l (1.5 USgal) transparent bottle 1 l (0.26 USgal) access platform 2.5 m (8 ft. 2 in.) Torque Wrench : range 36.00 to 220.00 lbf.in (0.40 to 2.60 m.daN) 1 TANK - ENGINE OIL FILLING UP
EFF : 701-749, 12-32-24 Page 301 Config-2 Jan 01/02 SROS
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
OMAT 238
Material No. 03-002
* lockwire 0.028 to 0.031 in.(0.71 to 0.79 mm) dia. (Ref. 70-30-00) GB DEF-STAN 91-101 LUBRICATING OIL TURBINE ENGINE SYNT BASE (Ref. 20-31-00)
R R
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-13-24-612-808 24-42-00-861-801 24-42-00-862-801 71-13-00-010-805 71-13-00-410-805 78-31-00-040-805 78-31-00-440-805 12-32-24-991-002
IDG Servicing - Filling of the IDG with Oil or Addition of Oil after Level Check Energize the Ground Service Network De-energize the Ground Service Network Open the Fan Cowl Doors Close the Fan Cowl Doors Deactivation of the Thrust Reverser for Maintenance Activation of the Thrust Reverser after Maintenance Fig. 301
3. __________ Job Set-up Subtask 12-32-24-861-053 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-32-24-941-053 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure.
EFF : 701-749, 12-32-24 Page 302 Config-2 Jan 01/06 SROS
Subtask 12-32-24-010-056 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU. Subtask 12-32-24-865-056 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-32-24-010-057 E. Get Access (1) Open the fan cowl doors (Ref. TASK 71-13-00-010-805): - FOR 4030EM1 415AL, 416AR, - FOR 4030EM2 425AL, 426AR. Subtask 12-32-24-040-053 F. Deactivation of the Thrust Reverser WARNING : YOU MUST DEACTIVATE THE THRUST REVERSER BEFORE YOU DO WORK ON _______ OR AROUND IT. IF YOU DO NOT, THE THRUST REVERSER CAN OPERATE ACCIDENTALLY AND CAUSE INJURY AND/OR DAMAGE. (1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 7831-00-040-805).
EFF : 701-749, 12-32-24 Page 303 Config-2 Jan 01/06 R SROS
4. Procedure _________ (Ref. Fig. 301/TASK 12-32-24-991-002) Subtask 12-32-24-864-053 A. Depressurization of the IDG Case WARNING : POINT THE OVERFLOW DRAIN HOSE INTO A CONTAINER WHEN YOU CONNECT _______ THE HOSE TO THE OVERFLOW DRAIN VALVE. THIS WILL PREVENT BURNS FROM THE HOT OIL SPRAY. HOT OIL CAN CAUSE BURNS TO EYES AND SKIN. CAUTION : DO NOT USE DEVICES OTHER THAN THE APPROVED OVERFLOW DRAIN-HOSE _______ FITTING. HARD METAL OBJECTS SUCH AS SCREWDRIVERS CAN CAUSE DAMAGE TO THE OVERFLOW DRAIN-VALVE SEAT. (1) Put a container 5.7 l (1.5 USgal) below the IDG. (2) Remove the dust cap (4) from the overflow drain valve (2). (3) Put the end of the overflow drain hose (8) of the TANK - ENGINE OIL FILLING UP (DH13PM) in the container (7). (4) Do this step to depressurize the IDG case: (a) Connect the overflow drain hose (8) of the TANK - ENGINE OIL FILLING UP (DH13PM) to the overflow drain valve (2). NOTE : Some oil can come out of the overflow drain hose (8) of ____ the TANK - ENGINE OIL FILLING UP (DH13PM) when you connect it. Subtask 12-32-24-281-056 B. Oil Sampling WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. _______ CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU. NOTE : Make sure that the oil is not too hot. ____ (1) Cut and remove the lockwire from the case drain plug (6). (2) Loosen the case drain plug (6).
EFF : 701-749, 12-32-24 Page 304 Config-2 Jan 01/06 R SROS
IDG Oil Sampling for Analysis Figure 301/TASK 12-32-24-991-002 EFF : 701-749, 12-32-24 Page 305 Config-2 Oct 01/00 SROS
(3) Put a transparent bottle 1 l (0.26 USgal) below the case drain port (1). NOTE : The transparent bottle (3) must be clean and sterilized. ____ (4) Slowly remove the case drain plug (6) until oil flows out of the case drain port (1). (5) Fill the transparent bottle (3) with approximately 20 ml (0.0053 USgal) of oil. (6) Seal the case drain port (1). (7) Remove the O-ring (5) from the case drain plug (6) and discard it. Subtask 12-32-24-640-053 C. Lubricate the new O-ring (5) with OILS (Material No. 03-002). Subtask 12-32-24-420-053 D. Installation of the Case Drain Plug (1) Install the new O-ring (5) on the case drain plug (6). (2) Install the case drain plug (6) in the case drain port (1). (3) TORQUE the case drain plug (6) to between 55 and 75 lbf.in (0.62 and 0.84 m.daN). (4) Safety the case drain plug (6) with lockwire 0.028 to 0.031 in.(0.71 to 0.79 mm) dia. (Material No. OMAT 238). Subtask 12-32-24-281-057 E. Oil Sample Bottle (1) Send the oil sample bottle to laboratory immediately with these data: (a) Oil sampling date. (b) Type and brand of oil used. (c) Operating time since last oil sampling. (d) IDG total operating time.
EFF : 701-749, 12-32-24 Page 306 Config-2 Jan 01/06 R SROS
(e) Identification of the IDG (Serial Number). NOTE : If you do not do the analysis immediately, seal the ____ bottle. Subtask 12-32-24-020-053 F. Removal of the Overflow Drain Hose (1) Disconnect the overflow drain hose (8) of the TANK - ENGINE OIL FILLING UP (DH13PM) from the overflow drain valve (2). (2) Install the dust cap (4) on the overflow drain valve (2). Subtask 12-32-24-612-053 G. Fill the IDG with oil or add oil to the IDG after a level check (Ref. TASK 12-13-24-612-808). 5. Close-up ________ Subtask 12-32-24-440-053 A. Make the thrust reverser serviceable after maintenance (Ref. TASK 78-3100-440-805). Subtask 12-32-24-865-057 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2 Subtask 12-32-24-410-053 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Close the access door 811. (4) Remove the access platform(s).
EFF : 701-749, 12-32-24 Page 307 Config-2 Jan 01/06 R SROS
(5) Close the fan cowl doors (Ref. TASK 71-13-00-410-805): - FOR 4030EM1 415AL, 416AR, - FOR 4030EM2 425AL, 426AR. Subtask 12-32-24-862-053 D. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : 701-749, 12-32-24 Page 308 Config-2 Jan 01/06 R SROS
FUEL - SERVICING ________________ TASK 12-32-28-281-810 Operate Water Drain Valves to Drain Accumulated Water from Center, Inner, Outer and Wing Vent Surge Tanks WARNING : DO NOT GET AIRCRAFT FUEL: _______ - IN YOUR MOUTH - IN YOUR EYES - ON YOUR SKIN FOR A LONG TIME. WARNING : DO NOT GET YOUR CLOTHES SOAKED WITH FUEL. _______ AIRCRAFT FUEL IS POISONOUS AND CAN GO THROUGH YOUR SKIN INTO YOUR BODY. IF YOU ARE CONTAMINATED WASH WITH CLEAN WATER AND IF NECESSARY GET MEDICAL HELP. WARNING : MAKE SURE THAT YOU HAVE THE CORRECT FIRE FIGHTING EQUIPMENT _______ AVAILABLE. R R
CAUTION : ALWAYS USE THE CORRECT TOOL TO OPEN THE WATER DRAIN VALVE. THIS CAN _______ PREVENT DAMAGE TO THE SEALS. 1. __________________ Reason for the Job Refer to the MPD TASK: 281100-10 NOTE : If you operate the water drains more frequently than the MPD ____ interval, you can prevent these long-term problems: - decreased precision of the fuel quantity indications - the risk of corrosion from microbiological contamination. NOTE : You must operate the water drains more frequently if you find a high ____ water content when you do this procedure. NOTE : The conditions to operate the water drains are best when the fuel ____ temperature is more than 5 deg.C. NOTE : If possible, do the water drain procedure before you refuel. If you ____ refuel the aircraft before you do this procedure, the water and the fuel will mix. Because of this, you must wait one hour for the separation of the water and the fuel before you can drain the water from the tank.
R R
NOTE : For the gravity procedure AIRBUS recommends that there must be more ____ than 10% content of fuel in each tank. If you have less than 10%
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content of fuel, then the indirect water drain valves will have a decreased flow. It is recommended that you use the suction procedure when you have less than 10% content of fuel. R
NOTE : This task can contribute to fuel savings. ____ 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific No specific No specific 97A28002117002 98A28104000000
hose hydrokit suction pump transparent glass container 1 l (0.2641 USgal) container 10 l (2.6416 USgal) 1 PURGING TOOL 1 PURGER, WATER DRAIN
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-31-28-660-801 12-32-28-281-812 28-00-00-610-801 12-32-28-991-001-A 12-32-28-991-003-A
Cold Weather Maintenance Practices for the Fuel System Sample Fuel for Microbiological Contamination Analysis Fuel Safety Procedures Fig. 301 Fig. 302
3. __________ Job Set-up Subtask 12-32-28-941-061 A. Safety Precautions WARNING : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND _______ DAMAGE. (1) Obey the fuel safety procedures (Ref. TASK 28-00-00-610-801).
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R R R R
(2) If the fuel temperature is less than , -5 deg.C (+23.00 deg.F) water in the fuel tanks and/or water drain valves may be frozen). To keep the flight turnaround times, do the cold weather maintenance practices for the fuel system (Ref. TASK 12-31-28-660-801). 4. Procedure _________ (Ref. Fig. 301/TASK 12-32-28-991-001-A, 302/TASK 12-32-28-991-003-A) Subtask 12-32-28-680-062 A. Operate Water Drain Valves to Drain Accumulated Water from Center, Inner, Outer and Wing Vent Surge Tanks WARNING : MAKE SURE THE AREA AROUND THE AIRCRAFT IS SAFE BEFORE YOU START _______ A REFUEL/DEFUEL PROCEDURE. IN THIS SAFE AREA, DO NOT LET PERSONS: - SMOKE - MAKE SPARKS OR FIRE - USE ANY EQUIPMENT WHICH IS NOT APPROVED FOR THE TASK. AIRCRAFT FUEL IS FLAMMABLE. NOTE : During this procedure you must continue to operate all the drain ____ valves until no more water comes out. NOTE : AIRBUS recommends that you do a test for microbial contamination, ____ in not more than 10 days, if: - the sample you drain from the tank has a strong sulphide smell - you can see objects in the sample (Ref. TASK 12-32-28-281-812). (1) Gravity procedure
R
(a) Push the center of the applicable water drain valve with the PURGER, WATER DRAIN. Drain approximately 1.0 l (0.2641 USgal) of fuel (as a sample) from the drain valve.
R
(b) Remove the PURGER, WATER DRAIN from the drain valve. (c) Examine the drain valve for leaks. (d) Do this procedure at all of the water drain valves.
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R
Water Drain Valves - Location Figure 301/TASK 12-32-28-991-001-A
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Water Drain Valves - Location For Suction Procedure Figure 302/TASK 12-32-28-991-003-A
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(2) Suction procedure (a) On the PURGING TOOL, disconnect the funnel from the bottle. (b) Attach one end of the hose to the funnel and attach the other end of the hose to the suction pump. NOTE : The illustration shows a typical suction pump with an air ____ drill power source. The suction pump used must be a type approved for use on a fuel system and the applicable safety precautions must be taken. (c) Put the outlet of the suction pump into the container and start the suction pump. (d) Push the center of the applicable water drain valve with the funnel. Drain approximately 1.0 l (0.2641 USgal) of fuel (as a sample) from the drain valve. (e) Remove the funnel from the drain valve. (f) Examine the drain valve for leaks. (g) Do this procedure at all of the water drain valves. (h) Connect the funnel to the PURGING TOOL (97A28002117002). Subtask 12-32-28-281-059 B. Fuel/Water Sampling (1) Put the fuel sample into a transparent glass container. If you do not do the analysis immediately, seal the container. Subtask 12-32-28-750-060 R
C. Water Contamination Test (1) Let the sample become stable. (a) If the sample moves into two layers, it contains water. Continue to drain from the water drain valve until it has no water. (b) If the sample stays in one layer, it can be all fuel or all water. To find if the sample is fuel or water, do the test that follows.
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WARNING : DO THE TEST ONLY IN AN APPROVED AREA. _______ (c) Do this test: ------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------R R R
1. If you have a hydrokit available, refer to the manufacturers instructions and test the sample.
- If the powder stays white, the sample is fuel and the test is complete. or
R R R R R R R
- If the white powder changes color, refer to the color indicator comparison card. If the sample is water, you must do the test until all of the water is removed from the tank. (the powder does not change color). 2. If you do not have a hydrokit available, add water to the sample
- If the sample moves into two layers, the sample taken is all fuel and the test is complete. or - If the sample stays in one layer, the sample is water. Continue to take samples and test until all the water has been removed.
NOTE : You can use the same procedure to do an analysis on a ____ sample from a fuel tanker. Remove the sample from the supply connector of the fuel tanker. 5. Close-up ________ Subtask 12-32-28-942-061 A. Removal of Equipment (1) Make sure that the work area is clean and clear of tools and other items. NOTE : To discard the samples, refer to the local regulations. ____
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TASK 12-32-28-281-803 Operate Water Drain Valves to Drain Accumulated Water from Trim Tank and Trim Vent Surge Tank WARNING : DO NOT GET AIRCRAFT FUEL: _______ - IN YOUR MOUTH - IN YOUR EYES - ON YOUR SKIN FOR A LONG TIME. WARNING : DO NOT GET YOUR CLOTHES SOAKED WITH FUEL. _______ AIRCRAFT FUEL IS POISONOUS AND CAN GO THROUGH YOUR SKIN INTO YOUR BODY. IF YOU ARE CONTAMINATED WASH WITH CLEAN WATER AND IF NECESSARY GET MEDICAL HELP. WARNING : MAKE SURE THAT YOU HAVE THE CORRECT FIRE FIGHTING EQUIPMENT _______ AVAILABLE. WARNING : MONITOR THE MOVEMENT OF FUEL VERY CAREFULLY DURING THE GROUND FUEL _______ TRANSFER. MOVEMENT OF FUEL TO THE TRIM TANK CAN CAUSE THE AIRCRAFT TO OVERBALANCE. CAUTION : ALWAYS USE THE CORRECT TOOL TO OPEN THE WATER DRAIN VALVE. THIS CAN _______ PREVENT DAMAGE TO THE SEALS. 1. __________________ Reason for the Job Refer to the MPD TASK: 281100-02 NOTE : If possible, do the water drain procedure before you refuel. If you ____ refuel the aircraft before you do this procedure, the water and the fuel will mix. Because of this, you must wait one hour for the separation of the water and the fuel before you can drain the water from the tank. NOTE : For the gravity procedure there must be more than 1000 kg (2205 lb) ____ fuel in the trim tank. R
NOTE : This task can contribute to fuel savings. ____
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2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
R R R R
No specific No specific No specific No specific No specific No specific No specific 98A28104000000 98A28104031000
1 1 1 1 1
hot-air blower hydrokit suction pump transparent glass container 1 l (0.2641 USgal) ACCESS PLATFORM 8M (26 FT) - ADJUSTABLE CONTAINER 10 L(2 1/2 USGAL) HOSE - FUEL RESISTANT PURGER, WATER DRAIN PURGER - WATER DRAIN
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-32-28-281-812 27-40-00-866-801 28-00-00-610-801 28-25-00-869-802 12-32-28-991-009
Sample Fuel for Microbiological Contamination Analysis Operation of the THS Actuator Fuel Safety Procedures Ground Fuel Transfer To The Trim Tank Fig. 303
3. __________ Job Set-up (Ref. Fig. 303/TASK 12-32-28-991-009) Subtask 12-32-28-941-052 A. Safety Precautions WARNING : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND _______ DAMAGE. R
(1) Obey the fuel safety procedures (Ref. TASK 28-00-00-610-801).
R
(2) Put an ACCESS PLATFORM 8M (26 FT) - ADJUSTABLE in position below the applicable water drain valve.
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Trim Tank and Trim Vent Surge Tank - Location for Suction and Gravity Procedure Figure 303/TASK 12-32-28-991-009
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(3) If the fuel temperature is less than -5 deg.C (+23.00 deg.F) (and/or the water drain valves are frozen), to keep the flight turnaround times, either: - use an approved hot-air blower to warm the drain valve area or - wait until one hour after the refuel procedure.
R R
Subtask 12-32-28-860-052 B. Aircraft Maintenance Configuration (1) Put the THS to the 4 degree position (Ref. TASK 27-40-00-866-801). NOTE : The maximum angle for draining water from the THS is 5 ____ degrees. On level ground the aircraft has a 1 degree nose down attitude. 4. Procedure _________ Subtask 12-32-28-680-056 A. Operate Water Drain Valves to Drain Accumulated Water from Trim Tank and Trim Vent Surge Tank WARNING : MAKE SURE THE AREA AROUND THE AIRCRAFT IS SAFE BEFORE YOU START _______ A REFUEL/DEFUEL PROCEDURE. IN THIS SAFE AREA, DO NOT LET PERSONS: - SMOKE - MAKE SPARKS OR FIRE - USE ANY EQUIPMENT WHICH IS NOT APPROVED FOR THE TASK. AIRCRAFT FUEL IS FLAMMABLE. NOTE : Before you can do a gravity water drain procedure at the trim ____ tank, it must contain a minimum fuel level of 1000 kg (2205 lb). This makes sure that the level of fuel is sufficient to force the fuel or water up to the remote drain valve. If the fuel level is 1000 kg (2205 lb) or more: - do the gravity procedure. If the fuel level is less than 1000 kg (2205 lb): - do the suction procedure or, - do a fuel ground transfer (Ref. TASK 28-25-00-869-802) so that the fuel level is 1000 kg (2205 lb) or more and do the gravity procedure. If you do the fuel ground transfer, you must wait a minimum of one hour before you operate the water drain valves.
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NOTE : During this procedure you must continue to operate all the drain ____ valves until only fuel comes out. NOTE : AIRBUS recommends that you do a test for microbial contamination, ____ in not more than 10 days, if: - the sample you drain from the tank has a strong sulphide smell - you can see objects in the sample (Ref. TASK 12-32-28-281-812). (1) Gravity procedure R
(a) Push the center of the applicable water drain valve with the PURGER, WATER DRAIN (98A28104000000). Drain approximately 1.0 l (0.2641 USgal) of fuel (as a sample) from the drain valve.
R
(b) Remove the PURGER, WATER DRAIN from the drain valve and examine the drain valve for leaks. (c) Do this procedure at all of the water drain valves (5105QS1, 5105QS2 and 5106QS) in the Trim Tank and Trim Vent Surge Tank. (2) Suction procedure NOTE : It is possible for FIN 5105QS1 and 5105QS2 that you cannot get ____ a satisfactory seal between the standard tool and the trim tank surface to use the suction method.
R R
(a) On the PURGER - WATER DRAIN (98A28104031000), disconnect the HOSE - FUEL RESISTANT from the bottle.
R R R
(b) Connect the end of the HOSE - FUEL RESISTANT to the inlet of the suction pump. NOTE : The illustration shows a typical suction pump with an air ____ drill power source. You must use a fuel approved type of suction pump for use on a fuel system and the applicable safety precautions must be taken.
R R
(c) Put the outlet of the suction pump into the CONTAINER 10 L(2 1/2 USGAL) and start the suction pump.
R R
(d) Push the center of the applicable water drain valve with the PURGER - WATER DRAIN. Drain approximately 1.0 l (0.2641 USgal) of fuel (as a sample) from the drain valve.
R R
(e) Remove the PURGER - WATER DRAIN from the drain valve and examine the drain valve for leaks.
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(f) Do this procedure at all of the water drain valves. R
(g) Connect the hose removed at step (a), to the bottle. Subtask 12-32-28-281-052 B. Fuel/Water Sampling (1) Put the fuel sample into a transparent glass container. If you do not do the analysis immediately, seal the container. Subtask 12-32-28-750-054 C. Water Contamination Test
R
(1) Let the sample become stable. (a) If the sample moves into two layers, it contains water. Continue to drain from the water drain valve until only fuel comes out. (b) If the sample stays in one layer, it can be all fuel or all water. To identify if the sample is fuel or water, do the test that follows. WARNING : DO THE TEST ONLY IN AN APPROVED AREA. _______ (c) Do this test: ------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------1. If you have a hydrokit available, refer to the manufacturers instructions and test the sample.
- If the powder stays white, the sample is fuel and the test is complete. or - If the white powder changes color, refer to the color indicator comparison card. If the sample is water, you must do the test until all of the water is removed from the tank (the powder does not change color).
R R
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------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------2. If you do not have a hydrokit - If the sample moves into two layers, available, add water to the the sample taken is all fuel and the sample test is complete. or - If the sample stays in one layer, the sample is water. Continue to collect samples. Do the test until all the water is removed.
R R 5. Close-up ________ Subtask 12-32-28-942-053 A. Removal of Equipment
(1) Make sure that the work area is clean and clear of tools and other items. (2) Remove the access platform(s). NOTE : To discard the samples, refer to the local regulations. ____
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TASK 12-32-28-281-804 Draining of the Fuel/Air Separator WARNING : DO NOT GET AIRCRAFT FUEL: _______ - IN YOUR MOUTH - IN YOUR EYES - ON YOUR SKIN FOR A LONG TIME. WARNING : DO NOT GET YOUR CLOTHES SOAKED WITH FUEL. _______ AIRCRAFT FUEL IS POISONOUS AND CAN GO THROUGH YOUR SKIN INTO YOUR BODY. IF YOU ARE CONTAMINATED WASH WITH CLEAN WATER AND IF NECESSARY GET MEDICAL HELP. WARNING : MAKE SURE THAT YOU HAVE THE CORRECT FIRE FIGHTING EQUIPMENT _______ AVAILABLE. 1. __________________ Reason for the Job To drain the fuel/air separator for maintenance purposes. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific 98A28007570000
warning notices container 25 l (6.6042 USgal) access platform 5.0 m (16 ft. 5 in.) 1 ADAPTER - VENT AND DRAIN VALVE, APU
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B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 24-41-00-862-801
R
28-00-00-610-801 28-25-00-650-802 28-51-00-710-801 12-32-28-991-002
Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Fuel Safety Procedures Suction Defuel Procedure FCMS Fuel Valves Test Fig. 304
3. __________ Job Set-up Subtask 12-32-28-941-053 A. Safety Precautions WARNING : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND _______ DAMAGE. (1) Obey the fuel safety procedures (Ref. TASK 28-00-00-610-801). (2) Put the warning notices - on the panel 215VU to - on the panel 245VU to - on the panel 990VU to aircraft.
in these positions: tell persons not to operate the APU tell persons not to operate the fuel system tell persons not to refuel/defuel the
Subtask 12-32-28-860-050 B. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED _______ BEFORE YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT. UNWANTED ELECTRICAL POWER CAN BE DANGEROUS. (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861801). (2) Suction defuel the trim tank (Ref. TASK 28-25-00-650-802). (3) On the MCDU, get access to the FCMS VALVES TEST page (Ref. TASK 2851-00-710-801).
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(4) On the FCMS Valves Test page, put the the trim tank inlet valve (705QN valve L) to the OPEN position. NOTE : This makes sure that a vacuum will not prevent the drain ____ procedure. Subtask 12-32-28-010-050 C. Get Access (1) Put the access platform in position below the access panel 311AL. (2) Open the access panel 311AL. Subtask 12-32-28-491-050 D. Not applicable 4. Procedure _________ R
(Ref. Fig. 304/TASK 12-32-28-991-002) Subtask 12-32-28-680-055 A. Draining of the Fuel/Air Separator Procedure (1) Put the container in position on the access platform. (2) Put the end of the hose (3) into the container. (3) Remove the blanking cap (4) from the drain valve (1). (4) Connect the ADAPTER - VENT AND DRAIN VALVE, APU (98A28007570000) (2) to the drain valve (1). (5) Drain all of the fuel out of the fuel/air separator. (6) Remove the ADAPTER - VENT AND DRAIN VALVE, APU (98A28007570000) (2) from the drain valve (1). (7) Connect the blanking cap (4) to the drain valve (1). 5. Close-up ________ Subtask 12-32-28-091-050 A. Not applicable
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Fuel/Air Separator Water Drain - Location Figure 304/TASK 12-32-28-991-002
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Subtask 12-32-28-410-050 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access panel 311AL. Subtask 12-32-28-860-051 C. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED _______ BEFORE YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT. UNWANTED ELECTRICAL POWER CAN BE DANGEROUS. (1) On the MCDU, get access to the FCMS VALVES TEST page (Ref. TASK 2851-00-710-801). (2) On the FCMS Valves Test page, put the the trim tank inlet valve (705QN valve L) to the SHUT position. (3) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). Subtask 12-32-28-942-052 D. Removal of Equipment (1) Remove the access platform(s). (2) Remove the warning notice(s). NOTE : To discard the fuel, refer to the local regulations. ____
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TASK 12-32-28-281-807 Operate the Drain Valve of the Fuel/Air Separator to Drain any Accumulated Water WARNING : DO NOT GET AIRCRAFT FUEL: _______ - IN YOUR MOUTH - IN YOUR EYES - ON YOUR SKIN FOR A LONG TIME. WARNING : DO NOT GET YOUR CLOTHES SOAKED WITH FUEL. _______ AIRCRAFT FUEL IS POISONOUS AND CAN GO THROUGH YOUR SKIN INTO YOUR BODY. IF YOU ARE CONTAMINATED WASH WITH CLEAN WATER AND IF NECESSARY GET MEDICAL HELP. WARNING : MAKE SURE THAT YOU HAVE THE CORRECT FIRE FIGHTING EQUIPMENT _______ AVAILABLE. 1. __________________ Reason for the Job Refer to the MPD TASK: 282200-07 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific No specific No specific 98A28007570000
hydrokit warning notices transparent glass container 1 l (0.2641 USgal) container 25 l (6.6042 USgal) access platform 5.5 m (18 ft. 1 in.) 1 ADAPTER - VENT AND DRAIN VALVE, APU
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B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-32-28-281-803 12-32-28-680-801 12-32-28-680-802 24-41-00-861-801 24-41-00-862-801 28-00-00-610-801 28-22-43-000-802 28-22-43-400-802 28-51-00-740-803 51-78-00-615-805 R
12-32-28-991-002
Operate Water Drain Valves to Drain Accumulated Water from Trim Tank and Trim Vent Surge Tank Heating of Fuel/Air Separator - Warm Fuel Procedure Heating of Fuel/Air Separator - Hot Air Procedure Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Fuel Safety Procedures Removal of the Drain Valve (5216QA) Installation of the Drain Valve (5216QA) Interrogation of the FCMS Input Parameters Pages Aircraft Cleaning after a Fuel Leakage (for corrective action) Fig. 304
3. __________ Job Set-up Subtask 12-32-28-941-058 A. Safety Precautions WARNING : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND _______ DAMAGE. (1) Obey the fuel safety procedures (Ref. TASK 28-00-00-610-801). (2) Put the warning notices - on the panel 215VU to - on the panel 245VU to - on the panel 990VU to aircraft.
in these positions: tell persons not to operate the APU tell persons not to operate the fuel system tell persons not to refuel/defuel the
Subtask 12-32-28-860-057 B. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED _______ BEFORE YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT. UNWANTED ELECTRICAL POWER CAN BE DANGEROUS.
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(1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) On the MCDU, get access to page 10 of the FCMS input parameters page (Ref. TASK 28-51-00-740-803). (3) On the panel 215VU, push (in) the APU MASTER SW P/BSW. Make sure that the ON light comes on. (4) On the MCDU, make sure that the fwd APU fuel pump is in operation. Subtask 12-32-28-010-054 C. Get Access (1) Put the access platform in position below the access panel 311AL. (2) Open the access panel 311AL. 4. Procedure _________ R
(Ref. Fig. 304/TASK 12-32-28-991-002) Subtask 12-32-28-680-059 A. Operate the Drain Valve of the Fuel/Air Separator to Drain any Accumulated Water (1) Do a fuel leak check around the area of the drain valve. There must be no leaks. If there are signs of a leak, replace the seal (Ref. TASK 28-22-43-000-802) and (Ref. TASK 28-22-43-400-802). (2) Put the container in position. (3) Remove the cap (4) from the drain valve (1). (4) It is possible that water in the fuel/air separator has changed to ice. If there is ice in the fuel/air separator, do the heating of the fuel/air separator procedure (Ref. TASK 12-32-28-680-801) or (Ref. TASK 12-32-28-680-802). (5) On the ADAPTER - VENT AND DRAIN VALVE, APU (98A28007570000) (2), put the end of the hose (3) into the container. (6) Connect the ADAPTER - VENT AND DRAIN VALVE, APU (98A28007570000) (2) to the drain valve (1).
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(7) Drain between 8 l (2.0 USgal) and 10 l (2.5 USgal) of fuel from the fuel/air separator. (8) Remove the ADAPTER - VENT AND DRAIN VALVE, APU (98A28007570000) (2) from the drain valve (1). Subtask 12-32-28-790-051 B. Leak Check (1) Do a fuel leak check around the area of the drain valve. Leakage is not allowed. If there are signs of a leak, replace the seal (Ref. TASK 28-22-43-000-802) and (Ref. TASK 28-22-43-400-802). (2) Install the cap (4) on the drain valve (1). (3) If there was an internal spillage during the procedure, you must do the aircraft cleaning after a fuel leakage procedure (Ref. TASK 5178-00-615-805). Subtask 12-32-28-281-056 C. Fuel/Water Sampling (1) Put the fuel sample into a transparent glass container. If you do not do the analysis immediately, seal the container. NOTE : The test must be done before the next flight. ____ Subtask 12-32-28-750-057 D. Water Contamination Test (1) Let the sample become stable. (a) If the sample moves into two layers, it contains water. Continue to drain from the water drain valve until it has no water. (b) If the sample stays in one layer, it can be all fuel or all water. To find if the sample is fuel or water, do the test that follows. WARNING : DO THE TEST ONLY IN AN APPROVED AREA. _______
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INTENTIONALLY BLANK
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(c) Do this test: ------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------1. If you have a hydrokit available, put the contents into the sample
- If the powder stays white, the sample is fuel and the test is complete. or - If the white powder changes color to purple, the sample is water. Continue to take samples and test until all the water has been removed.
2. If you do not have a hydrokit available, add water to the sample
- If the sample moves into two layers, the sample taken is all fuel and the test is complete. or - If the sample stays in one layer, the sample is water. Continue to take samples and test until all the water has been removed.
3. Measure the amount of water taken from the fuel/air separator.
- If the amount of water is 0.5 l or more, do a water drain check of the trim tank (Ref. TASK 12-32-28-281803).
5. Close-up ________ Subtask 12-32-28-410-054 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access panel 311AL.
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Subtask 12-32-28-860-058 B. Aircraft Maintenance Configuration (1) On the panel 215VU, release (out) the APU MASTER SW. Make sure that the ON light goes off. (2) On the MCDU, push the line key adjacent to the RETURN indication until the MCDU Menu page comes into view. (3) On the MCDU, set the BRT knob to OFF. (4) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). Subtask 12-32-28-942-058 C. Removal of Equipment (1) Remove the access platform(s). (2) Remove the warning notice(s). NOTE : To discard the fuel, refer to the local regulations. ____
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TASK 12-32-28-680-801 Heating of Fuel/Air Separator - Warm Fuel Procedure 1. __________________ Reason for the Job To melt ice that has formed in the fuel/air separator and has blocked the drain point. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
warning notices
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-32-28-281-805 24-41-00-861-801 24-41-00-862-801 28-00-00-610-801 28-25-00-869-802 31-60-00-860-801
Draining of the Fuel/Air Separator to Remove Accumulated Water Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Fuel Safety Procedures Ground Fuel Transfer To The Trim Tank EIS Start Procedure
3. __________ Job Set-up Subtask 12-32-28-941-056 A. Safety Precautions WARNING : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND _______ DAMAGE. (1) Obey the fuel safety procedures (Ref. TASK 28-00-00-610-801).
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(2) Put the warning notices - on the panel 215VU to - on the panel 245VU to - on the panel 990VU to aircraft.
in these positions: tell persons not to operate the APU tell persons not to operate the fuel system tell persons not to refuel/defuel the
Subtask 12-32-28-860-055 B. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED _______ BEFORE YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT. UNWANTED ELECTRICAL POWER CAN BE DANGEROUS. (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Do the EIS start procedure (Ref. TASK 31-60-00-860-801). (3) On the ECAM control panel, push the FUEL icon switch. 4. Procedure _________ Subtask 12-32-28-880-050 A. Heating of the Fuel/Air Separator - Warm Fuel Procedure WARNING : MONITOR THE MOVEMENT OF FUEL VERY CAREFULLY DURING THE GROUND _______ FUEL TRANSFER. MOVEMENT OF FUEL TO THE TRIM TANK CAN CAUSE THE AIRCRAFT TO OVERBALANCE. (1) Do a fuel ground transfer of 1000 kg (2200 lb) minimum to the trim tank (Ref. TASK 28-25-00-869-802). (2) Wait for 30 minutes. (3) Try to do the draining of the fuel/air separator procedure (Ref. TASK 12-32-28-281-805). If the drain is successful, the heating procedure is complete. (4) If the draining of the fuel/air separator is not successful, continue the heating procedure.
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(5) Do a forward transfer (a) On the FUEL panel 245VU, push (in) the T TANK MODE switch. (b) On the ECAM System Display, monitor the transfer of fuel from the trim tank. (c) When the trim-tank fuel quantity is 300 kg (600 lb) less, release (out) the T TANK MODE switch. (6) Wait for 30 minutes. (7) Try to do the draining of the fuel/air separator procedure (Ref. TASK 12-32-28-281-805). If the drain is successful, the heating procedure is complete. (8) If the draining of the fuel/air separator is not successful, do the heating procedure again. Continue to do the heating procedure until the ice has melted. 5. Close-up ________ Subtask 12-32-28-860-056 A. Aircraft Maintenance Configuration (1) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). Subtask 12-32-28-942-056 B. Removal of Equipment (1) Remove the warning notice(s).
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TASK 12-32-28-680-802 Heating of Fuel/Air Separator - Hot Air Procedure 1. __________________ Reason for the Job To melt ice that has formed in the fuel/air separator and has blocked the drain point. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
hot air blower warning notices access platform 5.0 m (16 ft. 5 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-32-28-281-805 27-40-00-866-801 28-00-00-610-801
Draining of the Fuel/Air Separator to Remove Accumulated Water Operation of the THS Actuator Fuel Safety Procedures
3. __________ Job Set-up Subtask 12-32-28-941-057 A. Safety Precautions WARNING : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND _______ DAMAGE. (1) Obey the fuel safety procedures (Ref. TASK 28-00-00-610-801).
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(2) Put the warning notices in these positions: - in the cockpit to tell persons not to operate the THS - on the panel 215VU to tell persons not to operate the APU - on the panel 245VU to tell persons not to operate the fuel system - on the panel 990VU to tell persons not to refuel/defuel the aircraft. Subtask 12-32-28-860-059 B. Aircraft Maintenance Configuration (1) Put the THS to the 0 degree position (Ref. TASK 27-40-00-866-801). Subtask 12-32-28-010-053 C. Get Access (1) Put the access platform in position below the access door 312AR. (2) Open the access door 312AR. R 4. Procedure _________ Subtask 12-32-28-880-051 A. Heating of the Fuel/Air Separator - Hot Air Procedure CAUTION: MAKE SURE THAT THE TEMPERATURE OF THE HOT AIR DOES NOT EXCEED 70 DEG C. THIS PREVENTS DAMAGE TO THE VALVE AND STRUCTURE. (1) Use a pipe from a hot air blower to blow hot air onto the water drain valve area of the fuel/air separator. (2) Keep the hot air on the area of the valve for 30 minutes. (3) Try to do the draining of the fuel/air separator procedure (Ref. TASK 12-32-28-281-805). If the drain is successful, the heating procedure is complete. (4) If the draining of the fuel/air separator is not successful, repeat the heating procedure. (5) Try to do the draining of the fuel/air separator procedure (Ref. TASK 12-32-28-281-805). If the drain is successful, the heating procedure is complete.
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(6) If the draining of the fuel/air separator is not successful, do the heating procedure again. Continue to do the heating procedure until the ice has melted. 5. Close-up ________ Subtask 12-32-28-091-053 A. Removal of the Safety Locks (1) Remove the MECHANICAL INPUT - RIGGING PIN from the mechanical input of the THS actuator. Subtask 12-32-28-410-053 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access door 312AR. Subtask 12-32-28-942-057 C. Removal of Equipment (1) Remove the access platform(s). (2) Remove the warning notice(s).
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TASK 12-32-28-281-812 R
Sample Fuel for Microbiological Contamination Analysis WARNING : DO NOT GET AIRCRAFT FUEL: _______ - IN YOUR MOUTH - IN YOUR EYES - ON YOUR SKIN FOR A LONG TIME. WARNING : DO NOT GET YOUR CLOTHES SOAKED WITH FUEL. _______ AIRCRAFT FUEL IS POISONOUS AND CAN GO THROUGH YOUR SKIN INTO YOUR BODY. IF YOU ARE CONTAMINATED WASH WITH CLEAN WATER AND IF NECESSARY GET MEDICAL HELP. WARNING : MAKE SURE THAT YOU HAVE THE CORRECT FIRE FIGHTING EQUIPMENT _______ AVAILABLE. 1. __________________ Reason for the Job
R
Refer to the MPD TASK: 281100-15 This procedure lets you do a test of the sample locally or you can send it to a laboratory. Refer to Service Information Letter (SIL 28-079) for more information about microbiological contamination in fuel tanks. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific No specific
transparent fuel resistant plastic container(s) 1 MICROBMONITOR 2 TEST KIT ECHA MICROBIOLOGY UK (CAGE CODE 0HZY6) 1 FUELSTAT RESINAE TEST KIT CONIDIA BIOSCIENCE UK (CAGE CODE KE385) 1 HY-LITE JET A1 FUEL TEST KIT MERCK KGAA, GERMANY (CAGE CODE D2186)
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B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-32-28-281-801 12-32-28-281-803 12-32-28-281-807 28-00-00-610-801 28-11-00-600-814 28-11-00-600-815 28-11-00-600-818 28-11-00-600-819
R
28-11-00-600-822 12-32-28-991-008 12-32-28-991-010
Operate Water Drain Valves to Drain Accumulated Water from Center, Inner, Outer and Wing Vent Surge Tanks Operate Water Drain Valves to Drain Accumulated Water from Trim Tank and Trim Vent Surge Tank Operate the Drain Valve of the Fuel/Air Separator to Drain any Accumulated Water Fuel Safety Procedures BIOBOR Biocidal Shock Treatment - With Fuel Mixed with Biocide BIOBOR Biocidal Shock Treatment - When Fuel Mixed with Biocide is not Available (Metered Injection Rig Method) KATHON Biocidal Shock Treatment - With Fuel Mixed with Biocide KATHON Biocidal Shock Treatment - When Fuel Mixed with Biocide is not Available (Metered Injection Rig Method) Removal of The Microbiological Particles Fig. 305 Fig. 306
3. __________ Job Set-up R
(Ref. Fig. 305/TASK 12-32-28-991-008, 306/TASK 12-32-28-991-010) Subtask 12-32-28-941-063 A. Safety Precautions WARNING : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND _______ DAMAGE. (1) Obey the fuel safety procedures (Ref. TASK 28-00-00-610-801).
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R
Maintenance Plan Flowchart - Microbiological Contamination Figure 305/TASK 12-32-28-991-008
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Microbiological Contamination Test Kits - Comparison Table Figure 306/TASK 12-32-28-991-010- 12 (SHEET 1)
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Microbiological Contamination Test Kits - Comparison Table Figure 306/TASK 12-32-28-991-010- 22 (SHEET 2)
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4. Procedure _________ Subtask 12-32-28-281-061 A. Sample Fuel for Microbiological Contamination Analysis NOTE : If moderate or heavy microbiological contamination is found in the ____ samples: - all the fuel tanks may have microbiological contamination - a biocidal shock treatment must be applied to all of the fuel tanks (Ref. TASK 28-11-00-600-814) or (Ref. TASK 28-11-00-600815) or (Ref. TASK 28-11-00-600-818) or (Ref. TASK 28-11-00-600819). (1) Drain a fuel and water sample from each fuel tank (Ref. TASK 12-3228-281-801) and (Ref. TASK 12-32-28-281-803). You must use a different sample container for each fuel tank. NOTE : Do not put additives in the samples to show the water ____ contents. NOTE : Before you collect the samples, read the manufacturers ____ instructions in the test kit. Make sure you use a sample container that is specified and that it is clean and dry before use. An incorrect, dirty sample container can give an unwanted effect to the results. (2) Put the sample(s) into a transparent fuel resistant plastic container(s) with a minimum capacity of 1.0 l (0.2641 USgal) and: - seal the container(s) - make sure you can see free water and fuel in the sample(s) (for the MICROBMONITOR2 kit or the FUELSTAT RESINAE kit). (3) Identify each sample with a label that shows: - the aircraft number - the time and the date of the sample - the fuel tank the sample came from - all additives you know about.
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(4) Keep the sealed sample containers in a cool protected area. NOTE : After the test samples are collected, microbial contamination ____ in the sample could multiply or die. It is recommended that the samples are tested before 6 hours but no later than 24 hours. AIRBUS recommends that the samples are tested in no more than 6 hours.
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NOTE : Choose one microbial test kit for the complete procedure. Do ____ not compare results between the microbial detection kits. They use different methods to give results. If you need help, ask the kit manufacturer. Subtask 12-32-28-281-065 B. Not applicable Subtask 12-32-28-281-067 C. Not applicable Subtask 12-32-28-281-068 D. Fuel/Air Separator (1) Drain a fuel sample from the fuel/air separator (Ref. TASK 12-32-28281-807). Subtask 12-32-28-281-062 R
E. Sample Test - MICROBMONITOR2 Test Kit Procedure (1) Do one of the steps that follow: (a) Use the MICROBMONITOR 2 TEST KIT ECHA MICROBIOLOGY UK (CAGE CODE 0HZY6) (and the manufacturers instructions) to do a test on the WATER and FUEL samples, or (b) Send the WATER and FUEL samples to an approved laboratory. (2) Do a check of the results: NOTE : If you do only one test, it can give an incorrect indication ____ of the condition of the fuel tanks. If a test shows contamination, (moderate or heavy) do the test again, (in not more than 10 days) before you remove the aircraft from service. Use the same test kit for the second test. (a) Negligible contamination 1 _
R R R
The contamination is negligible if: - the WATER sample contents has 1000 CFU/milli liter (Colony Forming Units) or less - the FUEL sample contents has 4000 CFU/liter or less.
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2 _
Continue to monitor the fuel tanks at the scheduled inspection interval. This procedure is now complete.
(b) Moderate contamination 1 _
The contamination is moderate if: - the WATER sample contents has between 1000 and 10000 CFU/milli liter - the FUEL sample contents has between 4000 and 20000 CFU/liter.
2 _
Use the same method and do the sample test again in not more than 10 days after the first test.
3 _
If the contamination has not changed from moderate: - do the BIOBOR or KATHON biocidal shock treatment (moderate contamination procedure) to all of the fuel tanks, (Ref. TASK 28-11-00-600-814) or (Ref. TASK 28-11-00-600-815) or (Ref. TASK 28-11-00-600-818) or (Ref. TASK 28-11-00-600819).
R R R R
(c) Heavy contamination 1 _
The contamination is heavy if: - the WATER sample contents is more than 10000 CFU/milli liter - the FUEL sample contents is more than 20000 CFU/liter.
2 _
Use the same method and do the sample test again in not more than 10 days after the first test.
3 _
If the contamination has not changed from heavy: - do the BIOBOR or KATHON biocidal shock treatment (heavy contamination procedure) to all of the fuel tanks (Ref. TASK 28-11-00-600-814) or (Ref. TASK 28-11-00-600-815) or (Ref. TASK 28-11-00-600-818) or (Ref. TASK 28-11-00-600819).
R R
R R R
NOTE : When you do the heavy contamination procedure, you will ____ need to enter the applicable fuel tanks to remove the contamination (Ref. TASK 28-11-00-600-822). The MICROBMONITOR2 Test Kit Procedure is now complete go to para. 5.(Close-up).
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Subtask 12-32-28-281-064 F. Sample Test - FUELSTAT RESINAE Test Kit Procedure NOTE : The FUELSTAT RESINAE test kit shows the most frequent type of ____ contamination you can find in fuel tanks (Hormoconis Resinae). Other types of contamination will not be shown. (1) Do one of the steps that follow: (a) Use the FUELSTAT RESINAE TEST KIT CONIDIA BIOSCIENCE UK (CAGE CODE KE385) (and the manufacturers instructions) to do a test on the WATER and FUEL samples, or (b) Send the WATER and FUEL samples to an approved laboratory. (2) Do a check of the results: NOTE : If you do only one test, it can give an incorrect indication ____ of the condition of the fuel tanks. If a test shows contamination, (moderate or heavy) do the test again, (in not more than 10 days) before you remove the aircraft from service. Use the same test kit to do the second test. (a) Negligible contamination 1 _
The contamination is negligible if the indication lines (on the test kit) show a negative result.
2 _
Continue to monitor the fuel tanks at the scheduled inspection interval. This procedure is now complete.
(b) Moderate contamination 1 _
The contamination is moderate if the indication lines (on the test kit) show a low positive result. Use the same method and do the sample test again in not more than 10 days after the first test.
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2 _
If the contamination has not changed from moderate: - do the BIOBOR or KATHON biocidal shock treatment (moderate contamination procedure) to all of the fuel tanks, (Ref. TASK 28-11-00-600-814) or (Ref. TASK 28-11-00-600-815) or (Ref. TASK 28-11-00-600-818) or (Ref. TASK 28-11-00-600819).
(c) Heavy contamination 1 _
The contamination is heavy if the indication lines (on the test kit) show a high positive result.
2 _
Use the same method and do the sample test again in not more than 10 days after the first test. If the contamination has not changed from heavy: - do a BIOBOR or KATHON biocidal shock treatment (heavy contamination procedure) to all of the fuel tanks (Ref. TASK 28-11-00-600-814) or (Ref. TASK 28-11-00-600-815) or (Ref. TASK 28-11-00-600-818) or (Ref. TASK 28-11-00-600819). NOTE : When you do the heavy contamination procedure, you will ____ need to enter the applicable fuel tanks to remove the contamination (Ref. TASK 28-11-00-600-822). The FUELSTAT RESINAE Test Kit Procedure is now complete go to para.5.(Close-up).
Subtask 12-32-28-281-069 R
G. Sample Test - HY-LiTE Jet A1 Fuel Test Kit Procedure NOTE : The manufacturers recommend you only use a fuel resistant ____ transparent plastic sample container. Glass containers will give an unwanted effect to the operation of the test kit. If possible, do the test in a clean area. (1) Do one of the steps that follow: (a) Use the HY-LITE JET A1 FUEL TEST KIT MERCK KGAA, GERMANY (CAGE CODE D2186) (and the manufacturers instructions) to do a test on the WATER and FUEL samples, or (b) Send the WATER and FUEL samples to an approved laboratory.
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(2) Do a check of the results: NOTE : If you do only one test, it can give an incorrect indication ____ of the condition of the fuel tanks. If a test shows contamination, (moderate or heavy) do the test again, (in not more than 10 days) before you remove the aircraft from service. Use the same test kit to do the second test. (a) Negligible contamination 1 _
The contamination is negligible if: - the WATER/FUEL sample contents has 1000 RLU/liter (Relative Light Units) or less.
2 _
Continue to monitor the fuel tanks at the scheduled inspection interval. This procedure is now complete.
R R
(b) Moderate contamination 1 _
The contamination is moderate if: - the WATER/FUEL sample contents has between 1000 and 5000 RLU/liter
2 _
Use the same method and do the sample test again in not more than 10 days after the first test.
3 _
If the contamination has not changed from moderate: - do the BIOBOR or KATHON biocidal shock treatment (moderate contamination procedure) to all of the fuel tanks, (Ref. TASK 28-11-00-600-814) or (Ref. TASK 28-11-00-600-815) or (Ref. TASK 28-11-00-600-818) or (Ref. TASK 28-11-00-600819).
R R
(c) Heavy contamination 1 _
The contamination is heavy if: - the WATER/FUEL sample contents is more than 5000 RLU/liter
2 _
Use the same method and do the sample test again in not more than 10 days after the first test.
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3 _
If the contamination has not changed from heavy: - do the BIOBOR or KATHON biocidal shock treatment (heavy contamination procedure) to all of the fuel tanks (Ref. TASK 28-11-00-600-814) or (Ref. TASK 28-11-00-600-815) or (Ref. TASK 28-11-00-600-818) or (Ref. TASK 28-11-00-600819). NOTE : When you do the heavy contamination procedure, you will ____ need to enter the applicable fuel tanks to remove the contamination (Ref. TASK 28-11-00-600-822).
5. Close-up ________ Subtask 12-32-28-942-063 A. Make sure that the work area is clean and clear of tools and other items.
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HYDRAULIC FLUID - SERVICING ___________________________ TASK 12-32-29-281-801 Sampling for Analysis WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE _______ CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM. MOVEMENT OF THE FLIGHT CONTROL SURFACES CAN BE DANGEROUS AND/OR CAUSE DAMAGE. WARNING : MAKE SURE THAT THE CONTROLS AGREE WITH THE POSITION OF THE ITEMS THEY _______ OPERATE BEFORE YOU PRESSURIZE A HYDRAULIC SYSTEM. UNWANTED MOVEMENT OF HYDRAULICALLY OPERATED ITEMS CAN BE DANGEROUS AND/OR CAUSE DAMAGE. WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL MATERIALS _______ ONLY WITH A GOOD FLOW OF AIR THROUGH THE WORK AREA. THESE MATERIALS ARE POISONOUS AND FLAMMABLE AND SKIN IRRITANTS. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. 1. __________________ Reason for the Job Refer to the MPD TASK: 291000-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R R R
No specific No specific No specific No specific HSPA181-380J
warning notices glass sample bottle 0.2 l (0.0528 USgal) plastic sample bottle exclusively made from poly-ethylene 0.2 l (0.0528 USgal) container 1.0 l (0.2641 USgal) 1 HYDRAULIC PURIFIER
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B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R Material No. 19-017
USA AMS 5687 LOCKWIRE 1.25 MM (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-801 12-12-29-611-802 12-12-29-611-803 12-12-29-611-804 12-12-29-611-805 12-12-29-611-806 12-36-29-611-801 12-36-29-611-801 12-36-29-611-802 12-36-29-611-802 12-36-29-611-803 12-36-29-611-803 12-36-29-611-804 12-36-29-611-805 12-36-29-611-806
Fill the Green Hydraulic Reservoir with a Hydraulic Service Cart Fill the Green Hydraulic Reservoir with a Hand Pump Fill the Blue Hydraulic Reservoir with a Hydraulic Service Cart Fill the Blue Hydraulic Reservoir with a Hand Pump Fill the Yellow Hydraulic Reservoir with a Hydraulic Service Cart Fill the Yellow Hydraulic Reservoir with a Hand Pump Replacement of the Hydraulic Fluid of the Green Hydraulic System with a Fluid Replacement and Recovery Bench Replacement of the Hydraulic Fluid of the Green Hydraulic System with a Fluid Replacement and Recovery Bench Replacement of the Hydraulic Fluid of the Blue Hydraulic System with a Fluid Replacement and Recovery Bench Replacement of the Hydraulic Fluid of the Blue Hydraulic System with a Fluid Replacement and Recovery Bench Replacement of the Hydraulic Fluid of the Yellow Hydraulic System with a Fluid Replacement and Recovery Bench Replacement of the Hydraulic Fluid of the Yellow Hydraulic System with a Fluid Replacement and Recovery Bench Reclaim the Fluid in the Green Hydraulic System Reclaim the Fluid in the Blue Hydraulic System Reclaim the Fluid in the Yellow Hydraulic System
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-36-29-611-807 R R R R
12-36-29-611-808 12-36-29-611-809 12-36-29-615-801 12-36-29-615-802 12-36-29-615-803 29-00-00-863-801 29-00-00-863-802 29-00-00-863-803 29-00-00-864-801 29-00-00-864-802 29-00-00-864-803
R R
29-00-00-910-805 32-12-00-010-801 32-12-00-410-801 SIL 29-081 12-32-29-991-001
Replacement of the Hydraulic Fluid of the Green Hydraulic System with the Green Electric Pump Replacement of the Hydraulic Fluid of the Blue Hydraulic System with the Blue Electric Pump Replacement of the Hydraulic Fluid of the Yellow Hydraulic System with the Yellow Electric Pump Clean the Fluid in the Green Hydraulic System (with the Pall Purifier) Clean the Fluid in the Blue Hydraulic System (with the Pall Purifier) Clean the Fluid in the Yellow Hydraulic System (with the Pall Purifier) Pressurize the Green Hydraulic System with the Ground Hydraulic Supply Pressurize the Blue Hydraulic System with the Ground Hydraulic Supply Pressurize the Yellow Hydraulic System with the Ground Hydraulic Supply Depressurize the Green Hydraulic System (Pressurized with the Hydraulic Ground Supply) Depressurize the Blue Hydraulic System (Pressurized with the Hydraulic Ground Supply) Depressurize the Yellow Hydraulic System (Pressurized with the Hydraulic Ground Supply) Safety Procedures of the Hydraulic System Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Fig. 301
3. __________ Job Set-up R
Subtask 12-32-29-941-050
R
A. Safety Precautions
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(1) Obey the hydraulic safety procedures (Ref. TASK 29-00-00-910-805).
R R R
(2) Put the warning notices in position to tell persons not to move: - the flight controls, - the lever of the landing gear selector.
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Subtask 12-32-29-010-050 B. Get Access (1) For Green or Blue hydraulic system: - Open the left MLG door (Ref. TASK 32-12-00-010-801). (2) For Yellow hydraulic system: - Open the right MLG door (Ref. TASK 32-12-00-010-801). Subtask 12-32-29-864-050 R
C. Pressurize the concerned hydraulic systems - for Green hydraulic system (Ref. TASK 29-00-00-863-801), - for Blue hydraulic system (Ref. TASK 29-00-00-863-802), - for Yellow hydraulic system (Ref. TASK 29-00-00-863-803). 4. Procedure _________ (Ref. Fig. 301/TASK 12-32-29-991-001) Subtask 12-32-29-680-050
R
A. Flush the sampling valve (1) Remove and discard WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. _______ CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU. (a) Remove and discard the lockwire from the applicable sampling valve: - for the Green hydraulic system, sampling valve 5123JM1 - for the Blue hydraulic system, sampling valve 5123JM2 - for the Yellow hydraulic system, sampling valve 5123JM3. (2) Remove the cap (3) from sampling valve (1).
R R
(3) Put the container below the sampling valve.
R
(4) Put the notch in the head of the cap (3) below the head of the needle valve (2).
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(5) Move the cap (3) to pull the needle valve (2) down and drain 0.2 l (0.0528 USgal) into the container.
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R
(6) Remove the cap (3) from the needle valve (2).
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(7) Discard the hydraulic fluid (refer to the local regulations).
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NOTE : You must flush the sampling valve before you remove each ____ sample. Subtask 12-32-29-281-050
R
B. Remove a sample from the sampling valve
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(1) Put the clean glass sample bottle or plastic sample bottle exclusively made from poly-ethylene below the sampling valve (1). (2) Put the notch in the head of the cap (3) below the head of the needle valve (2). (3) Move the cap (3) to pull the needle valve (2) down and drain 0.2 l (0.0528 US gal) into the sample bottle.
R
(4) Remove the cap (3) from the needle valve (2). R
(5) Seal the sample bottle.
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(6) Put a tag on the sample bottle with the aircraft registration, the system identification, the date and time. (7) Send the sample bottle to the analysis laboratory. (8) Depressurize the concerned hydraulic systems: - for Green hydraulic system (Ref. TASK 29-00-00-864-801), - for Blue hydraulic system (Ref. TASK 29-00-00-864-802), - for Yellow hydraulic system (Ref. TASK 29-00-00-864-803).
R R
(9) Install the cap (3) on the sampling valve (1). R
(10) Safety the cap with MISCELLANEOUS (Material No. 19-017).
EFF : ALL 12-32-29 SROS
Page 305 Jan 01/07
Sampling Valve - Location Figure 301/TASK 12-32-29-991-001- 12 (SHEET 1) EFF : ALL 12-32-29 SROS
Page 306 Apr 01/98
Sampling Valve - Location Figure 301/TASK 12-32-29-991-001- 22 (SHEET 2) EFF : ALL 12-32-29 SROS
Page 307 Apr 01/98
Subtask 12-32-29-281-051 C. Admissible Particle Contamination of Hydraulic Fluid R R R R R R R
(1) For correct operation of hydraulic equipment, the hydraulic fluid must be clean. The number of particles contained in 100 cubic-centimeters (6 cu.in.) must not be more than the class 9 requirements of NSA 307110 specifications. The hydraulic fluid used for replenishing, topping up etc, hydraulic systems (cart reservoirs) must agree with the requirements of class 7 of the NSA 307110 specifications (initial state).
R R
(2) Reference list of maximum limits of class 7 and class 9 of NSA 307110 specification: -----------------------------------------------------------------------------NUMBER OF PARTICLES -----------------------------------------------------------------------------Particle size Class 7 Class 9 -----------------------------------------------------------------------------5 to 15 micron 32000 128000 15 to 25 micron 5700 22800 25 to 50 micron 1012 4050 50 to 100 micron 180 720 > 100 micron 32 128
R R R R
(3) If a sample analysis shows a contamination rate higher of one or more of the class 9 values:
R R
(a) Stop the hydraulic tests,
R R R R R R R
(b) clean the hydraulic fluid (Ref. TASK 12-36-29-615-801), (Ref. TASK 12-36-29-615-802) and (Ref. TASK 12-36-29-615-803). - or reclaim it with the hydraulic ground power cart (Ref. TASK 12-36-29-611-804), (Ref. TASK 12-36-29-611-805) and (Ref. TASK 12-36-29-611-806). - or change it (Ref. TASK 12-36-29-611-807), (Ref. TASK 12-36-29611-808) and (Ref. TASK 12-36-29-611-809).
EFF : ALL 12-32-29 SROS
Page 308 Jan 01/06
R R R R R
NOTE : It is possible that Airbus will give you approval for ____ aircraft dispatch, if the contamination rate is more than the given limits (please see SIL 29-081) depending on the level of contamination and given if only one system is contaminated. **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 12-32-29-281-052
R
D. Chemical analysis
R R
(1) Chemical analysis must be to NSA307110 Limit Characteristics of fluid in operation.
R R
(2) If the values of the chemical analysis are not in the limits given in the table below, do the following corrective actions:
R R R R R R R
(a) If the water or chlorine content of the fluid sample are equal or more than the values given above: - Clean the hydraulic fluid with the HYDRAULIC PURIFIER (HSPA181380J) (Ref. TASK 12-36-29-615-801), (Ref. TASK 12-36-29-615802) and (Ref. TASK 12-36-29-615-803), - or change the hydraulic fluid (Ref. TASK 12-36-29-611-801), (Ref. TASK 12-36-29-611-802) and (Ref. TASK 12-36-29-611-803).
R R R R
(b) If the acidity, density, viscosity or conductivity of the fluid sample are out of the permitted values given above: - Change the hydraulic fluid (Ref. TASK 12-36-29-611-807), (Ref. TASK 12-36-29-611-808) and (Ref. TASK 12-36-29-611-809).
R R R R R R
(3) Airbus has defined additional time limited authorizations to prevent aircraft operational impact in case of Chemical Contamination (Ref. SIL 29-081). Airbus considers the aircraft can stay in service during the additional time frames, waiting for corrective action and new results avaibility.
EFF : ALL 12-32-29 SROS
Page 309 Jan 01/06
------------------------------------------------------------------------------| NSA 307110 Requirements Additional Temporary | | Authorization | ------------------------------------------------------------------------------|Hydraulic |In Service |Corrective | Tolerance | Allowed Time | |Fluid |Limits |Action | | Frames | |Parameters | |Application | (see NOTE 1) | (see NOTE 2) | ------------------------------------------------------------------------------Acid Number
R R R
1.5mg KOH/g max
immediately
1.5 to 2.5mg KOH/g max
7 calendar days
Density 970 to 1066 at 23 +/- 3 deg kg/m3
immediately
Not Applicable
600 FH
Water Content
0.50% max
immediately
0.5% to 1% 1% to 1.5%
600 FH 7calendar days
Viscosity at 38 deg.C
6 to 12.5 CST
immediately
5.5 to 6 CST
10 calendar days or 150 FH
Chlorine Content
200 ppm max
immediately
200 to 300 ppm
10 calendar days or 150 FH
Electrical conductivity
0.30 immediately microSiemens.c minimum
lower than 0.30 600 FH microSiemens.cm min
NOTE : 1: Tolerance represent the level of contaminations allowed for ____ a limited time duration (see associated allowed time frame). NOTE : 2: Allowed Time Frames is an additional time the aircraft can ____ stay into service. It is the period from the discovery of the contamination to new results availability (including corrective action, new sample removal and new analysis).
EFF : 001-049, 201-249, 251-252, 255-299, 12-32-29 301-399, 401-449, 451-499, SROS
Page 310 Jul 01/06
**ON A/C 701-749, Subtask 12-32-29-281-052-A R
D. Chemical analysis
R R
(1) Chemical analysis must be to NSA307110 Limit Characteristics of fluid in operation.
R R
(2) If the values of the chemical analysis are not in the limits given in the table below, do the following corrective actions:
R R R R R R R
(a) If the water or chlorine content of the fluid sample are equal or more than the values given above: - Clean the hydraulic fluid with the HYDRAULIC PURIFIER (HSPA181380J) (Ref. TASK 12-36-29-615-801), (Ref. TASK 12-36-29-615802) and (Ref. TASK 12-36-29-615-803), - or change the hydraulic fluid (Ref. TASK 12-36-29-611-801), (Ref. TASK 12-36-29-611-802) and (Ref. TASK 12-36-29-611-803).
R R R R R
(b) If the acidity, density, viscosity or conductivity of the fluid sample are out of the permitted values given above: - Change the hydraulic fluid (Ref. TASK 12-36-29-611-807), (Ref. TASK 12-36-29-611-808) and (Ref. TASK 12-36-29-611-809). |end
R R R R R R
(3) Airbus has defined additional time limited authorizations to prevent aircraft operational impact in case of Chemical Contamination (Ref. SIL 29-081). Airbus considers the aircraft can stay in service during the additional time frames, waiting for corrective action and new results avaibility.
R EFF : 701-749, 12-32-29 SROS
Page 311 Jan 01/06
------------------------------------------------------------------------------| NSA 307110 Requirements Additional Temporary | | Authorization | ------------------------------------------------------------------------------|Hydraulic |In Service |Corrective | Tolerance | Allowed Time | |Fluid |Limits |Action | | Frames | |Parameters | |Application | (see NOTE 1) | (see NOTE 2) | ------------------------------------------------------------------------------Acid Number
R R R
1.5mg KOH/g max
immediately
1.5 to 2.5mg KOH/g max
7 calendar days
Density 970 to 1066 at 23 +/- 3 deg kg/m3
immediately
Not Applicable
600 FH
Water Content
0.50% max
immediately
0.5% to 1% 1% to 1.5%
600 FH 7calendar days
Viscosity at 38 deg.C
6 to 12.5 CST
immediately
5.5 to 6 CST
10 calendar days or 150 FH
Chlorine Content
200 ppm max
immediately
200 to 300 ppm
10 calendar days or 150 FH
Electrical conductivity
0.30 immediately microSiemens.c minimum
lower than 0.30 600 FH microSiemens.cm min
NOTE : 1: Tolerance represent the level of contaminations allowed for ____ a limited time duration (see associated allowed time frame). NOTE : 2: Allowed Time Frames is an additional time the aircraft can ____ stay into service. It is the period from the discovery of the contamination to new results availability (including corrective action, new sample removal and new analysis).
EFF : 701-749, 12-32-29 SROS
Page 312 Jul 01/06
**ON A/C ALL 5. Close-up ________ Subtask 12-32-29-611-050 A. Make sure that the fluid level in the hydraulic reservoir is correct. If necessary, fill the concerned reservoir: - for green reservoir (Ref. TASK 12-12-29-611-801) or (Ref. TASK 12-1229-611-802). - for blue reservoir (Ref. TASK 12-12-29-611-803) or (Ref. TASK 12-12-29611-804). - for yellow reservoir (Ref. TASK 12-12-29-611-805) or (Ref. TASK 12-1229-611-806). Subtask 12-32-29-410-050 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the MLG doors (Ref. TASK 32-12-00-410-801).
EFF : ALL 12-32-29 SROS
Page 313 Jan 01/06
APU - SERVICING _______________ TASK 12-32-49-281-801 Oil Sampling for Analysis WARNING : DO NOT TOUCH THE APU UNTIL IT IS SUFFICIENTLY COOL TO PREVENT BURNS _______ WHEN YOU DO THE MAINTENANCE TASK(S). 1. __________________ Reason for the Job R R
To find the causes of oil contamination (fuel, oil degradation and other causes).
R R
NOTE : You must get the sample 15 to 30 minutes after APU shutdown and ____ before you add oil to the tank. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No
specific specific specific specific specific specific
circuit breaker(s) safety clip(s) clean and lint-free cloth plastic bottle warning notice access platform 2.5 m (8 ft. 2 in.) access platform 7.2 m (23 ft. 7 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-13-49-612-801 24-42-00-861-801 24-42-00-862-801 29-00-00-864-804 12-32-49-991-001
Gravity Servicing of the APU Oil Reservoir Energize the Ground Service Network De-energize the Ground Service Network Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action. Fig. 301
EFF : ALL 12-32-49 SROS
Page 301 Oct 01/00
3. __________ Job Set-up Subtask 12-32-49-860-050 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). (2) Make sure that the hydraulic systems are depressurized (Ref. TASK 29-00-00-864-804). (3) Put the warning notice in position on the panel 215VU to tell persons not to start the APU. Subtask 12-32-49-010-050 B. Get Access to the Avionics Compartment (1) Put the access platform in position below the access door 811. (2) Open the access door 811. Subtask 12-32-49-865-050 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU APU FIRE SQUIB B 2WF P09 721VU APU FIRE VLV CTL 4WF P07 742VU APU START CTL 1KA C72 742VU APU FIRE SQUIB A 1WF J72 742VU APU FIRE VLV CTL 3WF J71 Subtask 12-32-49-010-051 D. Get Access (1) Put the access platform in position below the APU compartment. (2) Open the APU access door 315AL and and safety it in the open position. (3) Set the LIGHT SW 3LJ to the ON position.
EFF : ALL 12-32-49 SROS
Page 302 Jul 01/00
4. Procedure _________ (Ref. Fig. 301/TASK 12-32-49-991-001) Subtask 12-32-49-281-050 A. Get a sample CAUTION : MAKE SURE THAT THE SCUPPER OF THE OIL TANK IS CLEAN TO PREVENT _______ CONTAMINATION OF THE TANK DURING THE SERVICING OPERATION. CAUTION : USE A NEW AND VERY CLEAN PLASTIC BOTTLE WITH A NEW SCREW TOP _______ AND A NEW PLASTIC TUBE. DO NOT USE THESE ITEMS AGAIN. (1) Clean the oil tank scupper. - Clean the oil tank scupper with a clean and lint-free cloth, before you remove the oil filler cap. (2) Open the oil tank WARNING : REMOVE THE OIL TANK FILLER CAP AT LEAST 5 MINUTES AFTER _______ ENGINE SHUTDOWN TO LET TANK PRESSURE DECREASE. OTHERWISE, PRESSURIZED HOT OIL FROM THE TANK COULD CAUSE BURNS. R R R R
(a) Squeeze the plastic bottle (2) and put the free end of the tube into the oil through the filling port (3).
R R
(b) Release the pressure on the bottle to remove the oil sample by suction.
R
(3) Tag the oil sample with these data: - APU total operating time. - Operating time since the last oil sampling. - Date of sample. - Identification of the APU (Serial Number). - Type and brand of the oil used.
R R R R
(4) Send the sample for chemical or spectrometric analysis to the laboratory as soon as possible.
R
(5) Do a check of the oil level and fill the oil tank if necessary (Ref. TASK 12-13-49-612-801).
EFF : ALL 12-32-49 SROS
Page 303 Oct 01/00
Oil Sampling for Analysis Figure 301/TASK 12-32-49-991-001 EFF : ALL 12-32-49 SROS
Page 304 Jul 01/00
R
(6) Close the oil tank. 5. Close-up ________ Subtask 12-32-49-410-050 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Set the LIGHT SW 3LJ to the OFF position. (3) Close the APU access door 315AL. (4) Remove the access platform(s). Subtask 12-32-49-865-051 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1KA, 1WF, 2WF, 3WF, 4WF Subtask 12-32-49-410-051 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access door 811. (3) Remove the access platform(s). Subtask 12-32-49-860-051 D. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801) (2) Remove the warning notice(s). (3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL 12-32-49 SROS
Page 305 Oct 01/00
ENGINE OIL - SERVICING ______________________ TASK 12-32-79-281-803 Sampling of the Engine Oil. WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE AFTER THE ENGINE IS SHUTDOWN. _______ THE ENGINE CAN STAY HOT FOR A LONG TIME AFTER THE ENGINE IS SHUTDOWN. WARNING : USE PROTECTIVE CLOTHING WHEN YOU USE ENGINE OIL. OIL CAN CAUSE SKIN _______ IRRITATION. CAUTION : DO NOT OPERATE THE ENGINE WITHOUT SUFFICIENT OIL. THIS WILL CAUSE A _______ POSSIBLE INFLIGHT SHUTDOWN AND POSSIBLE DAMAGE TO THE ENGINE. CAUTION : DO NOT LET ENGINE FUEL OR OIL FALL ON THE ENGINE. YOU MUST _______ IMMEDIATELY REMOVE UNWANTED FUEL OR OIL WITH A CLOTH. THE FUEL OR OIL CAN CAUSE DAMAGE TO SOME ENGINE PARTS. 1. __________________ Reason for the Job To get a sample of engine oil to: - determine if there is fuel in the engine oil system - get warning information on the oil lube wetted parts. To determine fuel content in the oil, the recommended detection methods are: - a flash point test and - a viscosity test. If you find fuel in the oil, the suspect cause is the fuel/oil cooler located on the engine core at approximately the 9 oclock position. To get warning information for wear of oil lube wetted mechanical parts before failure, the recommended detection method is: - Spectrometric Oil Analysis Procedure (SOAP). This method is the analysis of submicroparticles suspended in oil using a direct spectrometer with automatic concentration computation.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-32-79 Page 301 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No
specific specific specific specific specific
circuit breaker(s) safety clip(s) squeeze plastic bottle 0.02 l (0.0052 USgal) adjustable access platform 1.22 m (4 ft.) access platform 2.5 m (8 ft. 2 in.) plastic hose 20 in. (0.5079 m)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-13-79-610-806 24-42-00-861-801 24-42-00-862-801
Servicing of the Engine Oil System Energize the Ground Service Network De-energize the Ground Service Network
3. __________ Job Set-up Subtask 12-32-79-861-052 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-32-79-941-053 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure and not more than 30 minutes before you do this procedure. Subtask 12-32-79-010-057 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-32-79 Page 302 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
(3) Open the protective door of the AC/DC emergency power-center 740VU. Subtask 12-32-79-865-054 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-32-79-010-058 E. Get Access (1) Put the adjustable access platform in position. (2) Open the upper left thrust reverser access door: - FOR 4030EM1 417DL - FOR 4030EM2 427DL 4. Procedure _________ Subtask 12-32-79-210-050 A. Get the Oil Sample NOTE : You must take the oil sample 30 minutes or less after the engine ____ shutdown. NOTE : Do not replenish the oil until after you take the sample. ____ NOTE : Sampling equipment must be sterile have no chemical action on oil ____ and fuel. (1) Remove the oil tank cap. (2) Put the plastic hose into the oil tank until the hose touches the bottom.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-32-79 Page 303 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
(3) Pull the hose out approximately 0.5 in. (12.6999 mm) from the bottom. (4) Using a siphon or a squeeze plastic bottle, take the oil sample from the tank. (5) Take 0.150 l (0.0396 USgal) for fuel contamination detection. (6) Take 0.015 l (0.0039 USgal) SOAP inspection. (7) Remove and discard the plastic hose. NOTE : It is important to use a new hose with each oil sample to make ____ sure of an accurate sample. (8) Install the bottle cap. (9) Install the oil tank cap as follows: (a) With the handle at open, align and install the cap to the filler neck. (b) Push down on the cap and turn the handle clockwise to close. (c) Push the handle into the cap to lock the cap. (d) Make sure that the cap is installed equally and completely. Subtask 12-32-79-610-050 B. Service the Engine Oil System (Ref. TASK 12-13-79-610-806) NOTE : Write the amount of oil that you added. ____ Subtask 12-32-79-410-056 C. Close the thrust reverser access door: FOR 4030EM1 417DL FOR 4030EM2 427DL
R EFF : 001-049, 201-249, 251-252, 255-299, 12-32-79 Page 304 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
Subtask 12-32-79-800-050 D. Miscellaneous (1) Write the information which follows on the label: (a) A/C registration number. (b) Engine serial number. (c) Date of sampling. (d) Engine hours. (e) Oil added since last sample. (2) Send the sample to the laboratory as fast as possible so that the sample is usable and the analysis is accurate. Subtask 12-32-79-210-051 E. Oil Contamination by Fuel (Acceptable Limits) NOTE : The laboratory will analyze the sample by one or all of the ____ following methods. (1) Flash Point Method Method
Acceptable Limits
ASTM D92-57
340 deg.F
(171 deg.C)
or higher SETA Flash
340 deg.F
(171 deg.C)
or higher (2) Viscosity Method Method ASTM D445
Acceptable Limits
35 percent increase from actual measured new oil viscosity at 100 deg.F (37.8 deg.C)
R EFF : 001-049, 201-249, 251-252, 255-299, 12-32-79 Page 305 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
5. Close-up ________ Subtask 12-32-79-865-055 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2 Subtask 12-32-79-410-057 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Close the access door 811. (4) Remove the access platform(s). Subtask 12-32-79-862-052 C. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-32-79 Page 306 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
ENGINE OIL - SERVICING ______________________ TASK 12-32-79-280-801 Get a Sample of Engine Oil for Analysis 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No
specific specific specific specific specific
circuit breaker(s) safety clip(s) container - oil resistant 0.5 litres (0.132 USgal) syringe - oil 0.25 litre (0.066 USgal) adjustable access platform 1.22 m (4 ft.) access platform 2.5 m (8 ft. 2 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801
Energize the Ground Service Network De-energize the Ground Service Network
3. __________ Job Set-up Subtask 12-32-79-861-053 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-32-79-941-054 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure.
EFF : 701-749, 12-32-79 Page 301 Config-2 Apr 01/02 SROS
Subtask 12-32-79-010-059 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU. Subtask 12-32-79-865-056 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-32-79-010-060 E. Get Access (1) Put the adjustable access platform in the correct position at the right side of the engine. (2) Open the access panel on the right fan cowl door: - FOR 4030EM1 416CR - FOR 4030EM2 426CR 4. Procedure _________ WARNING : YOU MUST NOT LET ENGINE OIL STAY ON YOUR SKIN. FLUSH THE OIL FROM _______ YOUR SKIN WITH WATER. THE OIL IS POISONOUS AND CAN BE ABSORBED INTO THE BODY.
EFF : 701-749, 12-32-79 Page 302 Config-2 Apr 01/02 SROS
Subtask 12-32-79-680-050 A. Get a sample of engine oil: (1) Remove the oil filler cap. (2) Use a clean syringe - oil 0.25 litre (0.066 USgal) to get approximately 0,25 litres (0.066 USgal) of oil from the engine oil tank. (3) Put the oil sample into a clean container - oil resistant 0.5 litres (0.132 USgal). Seal and identify the sample. (4) Install the oil filler cap. Subtask 12-32-79-280-050 B. Send the sample to a laboratory for analysis. The permitted levels of contamination by volume are as follows: (1) Fuel - aviation kerosine and diesel - 0.5 percent (2) Hydraulic oil - mineral and phosphate - 0.3 percent (3) Synthetic oil which is not approved - 10.0 percent (4) Mineral oil - 2.0 percent. 5. Close-up ________ Subtask 12-32-79-865-057 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2 Subtask 12-32-79-410-058 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the protective door of the AC/DC emergency power center 740VU.
EFF : 701-749, 12-32-79 Page 303 Config-2 Apr 01/02 SROS
(3) Close the access door 811. (4) Close the access panel on the right fan cowl door: - FOR 4030EM1 416CR - FOR 4030EM2 426CR (5) Remove the access platform(s). Subtask 12-32-79-862-053 C. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : 701-749, 12-32-79 Page 304 Config-2 Apr 01/02 SROS
PRE-CONDITIONING - DESCRIPTION AND OPERATION ____________________________________________ 1. _______ General You can pre-condition the aircraft on the ground with: - a ground air-supply unit through the Low Pressure (LP) ground connectors, - a ground air-supply unit through the High Pressure (HP) ground connectors, - the APU bleed air supply. For the pre-conditioning you have to open the air outflow valves 313HL and 315HL to permit an overpressure in the cabin. 2. __________________ System Description
R R
A. Pre-conditioning with the Low Pressure (LP) Ground Connector You can connect a ground air-supply unit to the LP ground connections for ventilation of the aircraft. It is not necessary to operate the air conditioning packs. There are two LP ground connectors installed on the bottom of the belly fairing (access door 191EB). Through these connectors you supply the air from a ground air-supply unit to the cabin air distribution and regulation system (Ref. 21-21-00).
R R
B. Pre-conditioning with the High Pressure (HP) Ground Connector You can connect a ground air-supply unit to the HP ground connections for ventilation of the aircraft. You have to operate the air conditioning packs for this condition. There are two HP ground connectors installed on the bottom of the belly fairing (access door 193GB). Through these connectors you supply the compressed air from a ground air-supply unit to the crossbleed duct. The air flows from the crossbleed duct to the air conditioning packs. From the air conditioning packs the air flows to the cabin air distribution and regulation system (Ref. 21-21-00).
R
C. Pre-conditioning with the APU Bleed Air Supply The APU air system supplies bleed air to the aircraft pneumatic system (Ref. 36-12-00). You have to operate the air conditioning packs for this condition. The APU load compressor supplies the APU bleed air. When the APU bleed valve is in the opened position: - the Pressure Regulating Valves (PRV) close and thus shut off the engine bleed-air supply, - the APU supplies bleed air through the APU bleed air duct to the crossbleed duct. Then the air flows from the crossbleed duct to the air conditioning packs. From the air conditioning packs the air flows to the cabin air distribution and regulation system (Ref. 21-21-00).
EFF : ALL 12-33-00 SROS
Page 1 Jul 01/06
GROUND AIR PRE-CONDITIONING - MAINTENANCE PRACTICES ___________________________________________________ TASK 12-33-21-618-801 Pre-conditioning through the Low-Pressure Ground Connection WARNING : MAKE SURE THAT THE FWD AVIONICS ACCESS DOOR 811 IS OPEN WITH A _______ WARNING PLACARD ATTACHED TO IT. THE WARNING NOTICE MUST TELL PERSONS NOT TO CLOSE THE DOOR. THIS PREVENTS ACCIDENTAL PRESSURIZATION OF THE AIRCRAFT. CAUTION : DO NOT USE CONDITIONED AIR FROM THE PACKS AT THE SAME TIME AS AIR _______ FROM THE LOW-PRESSURE GROUND UNITS. THIS CAN CAUSE DAMAGE TO THE CHECK VALVES. R R R R
CAUTION : MAKE SURE THAT THE GROUND AIR-SUPPLY UNIT IS NOT TOO NEAR THE _______ AIRCRAFT AND THAT THE ENGINE EXHAUST PIPE OF THE GROUND AIR- SUPPLY UNIT POINTS AWAY FROM THE AIRCRAFT. HEAT FROM THIS UNIT AND FROM THE EXHAUST CAN CAUSE DAMAGE TO THE AIRCRAFT STRUCTURE. 1. __________________ Reason for the Job NOTE : There are alternative methods for the pre-conditioning. This task ____ gives one of the methods. For the other methods refer to the relevant tasks in this page block. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
ground air-supply unit(s) warning notice access platform 2.5 m (8 ft. 2 in.)
EFF : ALL 12-33-21 SROS
Page 201 Jan 01/03
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 12-33-21-991-001 12-33-21-991-002
Energize the Ground Service Network De-energize the Ground Service Network Fig. 201 Fig. 202
3. __________ Job Set-up (Ref. Fig. 201/TASK 12-33-21-991-001) Subtask 12-33-21-861-050 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-33-21-010-051 B. Get Access (1) Open the access door 191EB. (2) Connect the ground air-supply unit(s) to the aircraft LP connector(s). (3) Put the access platform in position below the access door 811. (4) Open the access door 811. (5) Install a warning notice on the access door 811 to tell persons not to close the access door 811.
EFF : ALL 12-33-21 R SROS
Page 202 Jan 01/03
LP and HP Ground Connectors Figure 201/TASK 12-33-21-991-001 EFF : ALL 12-33-21 SROS
Page 203 Apr 01/98
4. Procedure _________ (Ref. Fig. 202/TASK 12-33-21-991-002) Subtask 12-33-21-618-050 A. Pre-conditioning through the LP Ground Connector(s) (1) On the panel 212VU, make sure that the CAB FANS pushbutton switch is in the on position (the OFF legend is off). (2) Start the ground air-supply unit(s) and - the airflow is max. 3.2 kg/sec (423.3 - the supplied air pressure is not more - the supplied air temperature does not deg.F).
make sure that: lb/min), than 65 mbar (0.94 psi), go above 70 deg.C (158.00
(3) Set the necessary output air temperature on the ground air-supply unit(s). Subtask 12-33-21-618-055 B. When the pre-conditioning is no longer necessary, stop the ground air-supply unit(s). 5. Close-up ________ Subtask 12-33-21-410-051 A. Close Access (1) Disconnect and remove the ground air-supply unit(s) from the aircraft LP connector(s). (2) Make sure that the work area is clean and clear of tools and other items. (3) Close the access door 191EB. (4) Close the access door 811. (5) Remove the warning notice(s). (6) Remove the access platform(s). (7) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL 12-33-21 R SROS
Page 204 Jan 01/03
Cockpit Panels 212VU and 225VU Figure 202/TASK 12-33-21-991-002 EFF : ALL 12-33-21 R SROS
Page 205 Jan 01/03
Subtask 12-33-21-862-050 B. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-33-21 R SROS
Page 206 Jan 01/03
TASK 12-33-21-618-801- 01 Pre-conditioning through the High-Pressure Ground Connection WARNING : MAKE SURE THAT THE FWD AVIONICS ACCESS DOOR 811 IS OPEN WITH A _______ WARNING PLACARD ATTACHED TO IT. THE WARNING NOTICE MUST TELL PERSONS NOT TO CLOSE THE DOOR. THIS PREVENTS ACCIDENTAL PRESSURIZATION OF THE AIRCRAFT. CAUTION : MAKE SURE THAT THE GROUND-AIR SUPPLY IF FREE FROM OIL CONTAMINATION. _______ OIL CONTAMINATION CAN CAUSE THE SMELL OF OIL IN THE CABIN AND MAKE THE AIR-CONDITIONING PACKS UNSERVICEABLE. R R R R
CAUTION : MAKE SURE THAT THE GROUND AIR-SUPPLY UNIT IS NOT TOO NEAR THE _______ AIRCRAFT AND THAT THE ENGINE EXHAUST PIPE OF THE GROUND AIR- SUPPLY UNIT POINTS AWAY FROM THE AIRCRAFT. HEAT FROM THIS UNIT AND FROM THE EXHAUST CAN CAUSE DAMAGE TO THE AIRCRAFT STRUCTURE. 1. __________________ Reason for the Job NOTE : There are alternative methods for the pre-conditioning. This task ____ gives one of the methods. For the other methods refer to the relevant tasks in this page block. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
ground air-supply unit warning notice access platform 2.5 m (8 ft. 2 in.)
EFF : ALL 12-33-21 SROS
Page 207 Jan 01/03
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 24-41-00-862-801
Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A EIS Start Procedure EIS Stop Procedure Fig. 201 Fig. 202
31-60-00-860-801 31-60-00-860-802 12-33-21-991-001 12-33-21-991-002 3. __________ Job Set-up
(Ref. Fig. 202/TASK 12-33-21-991-002) Subtask 12-33-21-865-052 A. Make sure that this(these) circuit breaker(s) is(are) closed:
R
------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------715VU L RECIRC FAN 1HG1 B54 721VU LAV+GALY EXTC FAN 1HU A02 721VU PACK 1 L1 115VAC 1HH1 F02 721VU PACK 1 L2 115VAC 3HH1 K04 721VU CAB PRESS MAN 3HL P11 721VU ZONE CTL SYS 1 1HK1 R08 721VU PACK 1 L2 28VDC 4HH1 R07 721VU PACK 1 L1 28VDC 2HH1 T08 **ON A/C 401-449, 451-499, 721VU EXTC FAN AFT CARGO
8HN
E02
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 722VU EXTC FAN FWD CARGO
11HN
EFF : ALL 12-33-21 SROS
A34
Page 208 Jan 01/06
------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------**ON A/C ALL 722VU 722VU 722VU 722VU 722VU 722VU 722VU 722VU 722VU 725VU 742VU 742VU 742VU 742VU 742VU 742VU
EXTC FAN BULK CRG PACK 2 L2 115VAC PACK 2 L1 115VAC AIR XBLEED AUTO CPC 2 CARGO VENT CTL L1 ZONE CTL SYS 2 PACK 2 L2 28VDC PACK 2 L1 28VDC R RECIRC FAN RAM AIR PACK 1 FLOW CTL CPC 1 AIR XBLEED MAN PACK 2 FLOW CTL CARGO VENT CTL L2
5HN 3HH2 1HH2 1HV 2HL 2HN 1HK2 4HH2 2HH2 1HG2 1HZ 1HB1 1HL 2HV 1HB2 1HN
A37 E44 H48 R45 U44 U43 U42 U41 U40 B23 A68 A67 A66 C75 F80 L72
Subtask 12-33-21-860-054 B. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00-860-801). (3) On the ECAM control panel, push the BLEED key (on the SD, the BLEED page comes into view). (4) On the panel 225VU make sure that: - the PACK 1 and PACK 2 pushbutton switches are in the on position (the FAULT legends are on and the OFF legends are off), - the COCKPIT and the CABIN temperature selectors are at the 12 oclock position, - the HOT AIR 1 and the HOT AIR 2 pushbutton switches are in the on position (the OFF legends are off). (5) On the panel 225VU, set the the crossbleed valve selector-switch to OPEN.
EFF : ALL 12-33-21 R SROS
Page 209 Jan 01/03
(6) On the panel 212VU, make sure that the CAB FANS pushbutton switch is in the on position (the OFF legend is off). Subtask 12-33-21-010-052 C. Get Access (Ref. Fig. 201/TASK 12-33-21-991-001) (1) Open the access door 193GB. (2) Connect the ground air-supply unit to the aircraft HP connectors 7300HA and 7302HA. (3) Put the access platform in position below the access door 811. (4) Open the access door 811. (5) Install a warning notice on the access door 811 to tell persons not to close the access door 811. 4. Procedure _________ (Ref. Fig. 202/TASK 12-33-21-991-002) Subtask 12-33-21-618-056 A. Pre-conditioning through the HP Ground Connector (1) Start the ground air-supply unit and make sure that: - the airflow is max. 3.2 kg/sec (423.3 lb/min), - the supplied air pressure is not more than 3.5 bar (50.7631 psi), - the supplied air temperature does not go above 260 deg.C (500.00 deg.F). NOTE : On the panel 225VU, the PACK 1 and PACK 2 FAULT legends go off ____ when the flow control valves open. (2) On the AIR BLEED page of the System Display, make sure that the pack discharge-temperature indication is normal (green). Subtask 12-33-21-618-057 B. When the pre-conditioning is no longer necessary stop the ground air-supply unit.
EFF : ALL 12-33-21 R SROS
Page 210 Jan 01/03
5. Close-up ________ Subtask 12-33-21-860-055 A. Put the Aircraft back to its Initial Configuration (1) On the panel 225VU, set the crossbleed valve selector-switch to AUTO. (2) Do the EIS stop procedure (Ref. TASK 31-60-00-860-802). (3) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). Subtask 12-33-21-410-052 B. Close Access (1) Disconnect and remove the ground air-supply unit from the HP connectors 7300HA and 7302HA. (2) Make sure that the work area is clean and clear of tools and other items. (3) Close the access door 193GB. (4) Close the access door 811. (5) Remove the warning notice(s). (6) Remove the access platform(s). (7) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL 12-33-21 R SROS
Page 211 Jan 01/03
TASK 12-33-21-618-801- 02 Pre-conditioning with the APU WARNING : MAKE SURE THAT THE FWD AVIONICS ACCESS DOOR 811 IS OPEN WITH A _______ WARNING PLACARD ATTACHED TO IT. THE WARNING NOTICE MUST TELL PERSONS NOT TO CLOSE THE DOOR. THIS PREVENTS ACCIDENTAL PRESSURIZATION OF THE AIRCRAFT. 1. __________________ Reason for the Job NOTE : There are alternative methods for the pre-conditioning. This task ____ gives one of the methods. For the other methods refer to the relevant tasks in this page block. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
warning notice access platform 2.5 m (8 ft. 2 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 24-41-00-862-801 31-60-00-860-801 31-60-00-860-802 49-00-00-860-801 49-00-00-860-802 12-33-21-991-002
Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A EIS Start Procedure EIS Stop Procedure Start of the APU with External Power Supply Shutdown of the APU with Power Supply from the APU Battery Fig. 202
EFF : ALL 12-33-21 R SROS
Page 212 Jan 01/03
3. __________ Job Set-up (Ref. Fig. 202/TASK 12-33-21-991-002) Subtask 12-33-21-865-053 A. Make sure that this(these) circuit breaker(s) is(are) closed:
R
------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------715VU L RECIRC FAN 1HG1 B54 721VU LAV+GALY EXTC FAN 1HU A02 721VU PACK 1 L1 115VAC 1HH1 F02 721VU PACK 1 L2 115VAC 3HH1 K04 721VU CAB PRESS MAN 3HL P11 721VU ZONE CTL SYS 1 1HK1 R08 721VU PACK 1 L2 28VDC 4HH1 R07 721VU PACK 1 L1 28VDC 2HH1 T08 **ON A/C 401-449, 451-499, 721VU EXTC FAN AFT CARGO
8HN
E02
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 722VU EXTC FAN FWD CARGO
11HN
A34
**ON A/C ALL 722VU 722VU 722VU 722VU 722VU 722VU 722VU 722VU 722VU 725VU 742VU 742VU 742VU 742VU
EXTC FAN BULK CRG PACK 2 L2 115VAC PACK 2 L1 115VAC AIR XBLEED AUTO CPC 2 CARGO VENT CTL L1 ZONE CTL SYS 2 PACK 2 L2 28VDC PACK 2 L1 28VDC R RECIRC FAN RAM AIR PACK 1 FLOW CTL CPC 1 AIR XBLEED MAN
5HN 3HH2 1HH2 1HV 2HL 2HN 1HK2 4HH2 2HH2 1HG2 1HZ 1HB1 1HL 2HV
EFF : ALL 12-33-21 SROS
A37 E44 H48 R45 U44 U43 U42 U41 U40 B23 A68 A67 A66 C75
Page 213 Jan 01/06
------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------742VU PACK 2 FLOW CTL 1HB2 F80 742VU CARGO VENT CTL L2 1HN L72 Subtask 12-33-21-860-056 B. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00-860-801). (3) On the ECAM control panel, push the BLEED key (on the SD, the BLEED page comes into view). (4) On the panel 225VU make sure that: - the PACK 1 and PACK 2 pushbutton switches are in the on position (the FAULT legends are on and the OFF legends are off), - the COCKPIT and the CABIN temperature selectors are at the 12 oclock position, - the HOT AIR 1 and the HOT AIR 2 pushbutton switches are in the on position (the OFF legends are off). (5) On the panel 225VU, set the crossbleed valve selector-switch to OPEN. (6) On the panel 212VU, make sure that the CAB FANS switch is in the on position (the OFF legend is off). Subtask 12-33-21-010-053 C. Safety Precautions (1) Put the access platform in position below the access door 811. (2) Open the access door 811. (3) Install a warning notice on the access door 811 to tell persons not to close the access door 811.
EFF : ALL 12-33-21 R SROS
Page 214 Jan 01/04
4. Procedure _________ (Ref. Fig. 202/TASK 12-33-21-991-002) Subtask 12-33-21-618-058 A. Pre-conditioning with the APU (1) Start the APU (Ref. TASK 49-00-00-860-801). NOTE : On the panel 225VU, the PACK 1 and PACK 2 FAULT legends go off ____ when the flow control valves open. (2) On the panel 225VU push the APU BLEED pushbutton switch to the on position (the ON legend comes on). (3) On the AIR BLEED page of the System Display, make sure that the pack discharge temperature-indication is normal (green). Subtask 12-33-21-618-059 B. When the pre-conditioning is no longer necessary: (1) On the panel 225VU push the APU BLEED pushbutton switch to the off position (the ON legend goes off). (2) Stop the APU (Ref. TASK 49-00-00-860-802). 5. Close-up ________ Subtask 12-33-21-860-057 A. Put the Aircraft back to its Initial Configuration (1) On the panel 225VU, set the crossbleed valve selector-switch to AUTO. (2) Do the EIS stop procedure (Ref. TASK 31-60-00-860-802). (3) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801)
EFF : ALL 12-33-21 R SROS
Page 215 Jan 01/03
Subtask 12-33-21-410-053 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Remove the warning notice(s). (3) Close the access door 811. (4) Remove the access platform(s). (5) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL 12-33-21 SROS
Page 216 Jan 01/03
GROUNDING POINTS - DESCRIPTION AND OPERATION ____________________________________________ 1. General _______ This section gives the instructions to ground the aircraft for the refuel/defuel operations or for the maintenance operations. In the other conditions, the electrostatic discharge of the aircraft is made through the tires. It includes the topic below: 12-34-24/P. Block 201.
EFF : ALL 12-34-00 SROS
Page 1 Apr 01/98
AIRCRAFT GROUNDING - MAINTENANCE PRACTICES __________________________________________ TASK 12-34-24-860-801-A Aircraft Grounding for the Refuel/Defuel and Oxygen Servicing Operations WARNING : DO NOT WEAR A HEADSET OR TOUCH CABLES/LINES CONNECTED TO THE AIRCRAFT _______ WHEN THERE IS A RISK OF LIGHTNING. LIGHTNING IS DANGEROUS. 1. __________________ Reason for the Job To electrostatically balance the aircraft during the refuel/defuel and oxygen servicing operations. NOTE : Bonding is essential, grounding is recommended. ____ 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
bonding cable ground cable
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-34-24-991-001 12-34-24-991-002
Fig. 201 Fig. 202
3. __________ Job Set-up Subtask 12-34-24-210-052 A. Safety Precautions R R
(1) Make sure that the fuel tanker or oxygen ground filling equipment is grounded.
EFF : ALL 12-34-24 SROS
Page 201 Jan 01/07
4. Procedure _________ Subtask 12-34-24-480-052 A. Connection of the Ground Cables WARNING : ALWAYS CONNECT THE GROUND CABLE TO THE PARKING GROUND POINT _______ BEFORE YOU CONNECT IT TO THE AIRCRAFT. DO NOT ATTACH THE CABLE TO THE AIRCRAFT FIRST (THERE IS A RISK OF ELECTRIC SHOCK). NOTE : For the satisfactory removal of an electrical charge from the ____ aircraft: - the aircraft ground cable must have a section of 22 mm2 (0.0033 in2) or more. - the total electrical resistance of the cable between the parking ground point and the grounding point of the landing gear must not be more than 500 milliohms. - the resistance between the end connector on the ground cable and the nearest adjacent metal part of the landing gear must not be more than 10 milliohms. (1) Connect a ground cable to the grounding point on one of the MLG legs or on the NLG leg, (Ref. Fig. 201/TASK 12-34-24-991-001) R R
(2) Connect a bonding cable between the fuel tanker or the oxygen ground filling equipment and a grounding point on one of the MLG legs or the NLG leg, (Ref. Fig. 201/TASK 12-34-24-991-001) or connect a bonding cable between the fuel tanker and the grounding point on the upper wing surface (Ref. Fig. 202/TASK 12-34-24-991-002) The aircraft wheels must be on ground. 5. Close-up ________ Subtask 12-34-24-080-052 A. Disconnect the ground and bonding cables. (1) After the refuel/defuel or oxygen servicing operation, disconnect all the grounding and bonding cables.
EFF : ALL 12-34-24 SROS
Page 202 Jan 01/07
Location of the Grounding Points on the NLG and MLG Figure 201/TASK 12-34-24-991-001 EFF : ALL 12-34-24 SROS
Page 203 Apr 01/98
Grounding Point on the Wing Upper Surface Figure 202/TASK 12-34-24-991-002 EFF : ALL 12-34-24 SROS
Page 204 Apr 01/98
TASK 12-34-24-860-802 Aircraft Grounding for the Maintenance Operations WARNING : DO NOT WEAR A HEADSET OR TOUCH CABLES/LINES CONNECTED TO THE AIRCRAFT _______ WHEN THERE IS A RISK OF LIGHTNING. LIGHTNING IS DANGEROUS. 1. __________________ Reason for the Job R
To electrostatically balance the aircraft during the maintenance operations. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
ground cable
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-34-24-991-001 12-34-24-991-002
Fig. 201 Fig. 202
3. __________ Job Set-up Subtask 12-34-24-869-051 A. Not applicable. 4. Procedure _________ Subtask 12-34-24-210-051 A. Safety Precautions R
(1) Make sure that the access platform or the step ladder are grounded.
EFF : ALL 12-34-24 SROS
Page 205 Jan 01/07
Subtask 12-34-24-480-051 B. Connection of the Ground Cables WARNING : ALWAYS CONNECT THE GROUND CABLE TO THE PARKING GROUND POINT _______ BEFORE YOU CONNECT IT TO THE AIRCRAFT. DO NOT ATTACH THE CABLE TO THE AIRCRAFT FIRST (THERE IS A RISK OF ELECTRIC SHOCK). NOTE : For the satisfactory removal of an electrical charge from the ____ aircraft: - the aircraft ground cable must have a section of 22 mm2 (0.0033 in2) or more (for copper only). - the total electrical resistance of the cable between the parking ground point and the grounding point on the landing gear must not be more than 500 milliohms. - the resistance between the end connector on the ground cable and the nearest adjacent metal part of the landing gear must not be more than 10 milliohms.
R R
R R
(1) We recommend to connect the parking or the hangar ground cable to the aircraft grounding point on one of the MLG legs or on the NLG leg, (Ref. Fig. 201/TASK 12-34-24-991-001) The aircraft wheels must be on ground. NOTE : If the aircraft is on jacks for retraction and extension ____ checks of the landing gear, connect the parking or the hangar ground cable: - to the aircraft grounding point on the wings, (Ref. Fig. 202/TASK 12-34-24-991-002)
R R R
(2) We recommend to connect the ground cable of the step ladder or the access platform to the aircraft grounding point on one of the MLG legs or the NLG leg. The aircraft wheels must be on ground. NOTE : If the aircraft is on jacks for retraction and extension ____ checks of the landing gear, connect the parking or the hangar ground cable: - to the aircraft grounding point on the wings, (Ref. Fig. 202/TASK 12-34-24-991-002)
EFF : ALL 12-34-24 SROS
Page 206 Jan 01/07
5. Close-up ________ Subtask 12-34-24-080-051 A. Disconnect the ground cables. (1) After the maintenance operation, disconnect all the grounding cables.
EFF : ALL 12-34-24 SROS
Page 207 Jan 01/07
SYSTEM LINE FLUSHING - DESCRIPTION AND OPERATION ________________________________________________ 1. General _______ This section gives the instructions related to the flushing of a system line to remove all foreign matters from the fluid and from the system line. The fluid may be used again only if its characteristics obey the applicable specifications. It includes the topics below: 12-36-29/P. Block 301 HYDRAULIC POWER
EFF : ALL 12-36-00 SROS
Page 1 Apr 01/98
HYDRAULIC POWER - SERVICING ___________________________ R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, TASK 12-36-29-170-801 Flushing of the Case-Drain line of the Green Hydraulic System WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job To flush the Green hydraulic system after a failure of the engine pump. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No No No
specific specific specific specific specific specific specific specific specific specific
adaptor adjustable access platform blanking plug circuit breaker(s) safety clip(s) hydraulic power cart strap warning notice access platform 2.5 m (8 ft. 2 in.) container 20 l (5.2833 USgal) access platform 3 m (9 ft. 10 in.)
EFF : ALL 12-36-29 SROS
Page 301 Jul 01/05
------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific 98F12303000000
container 5 l (1.3208 USgal) Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft) 1 HYDRAULIC CONNECTORS
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-801 12-12-29-611-802 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-10-00-611-801 29-11-43-600-802 29-11-44-600-801 29-14-00-614-801 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 78-30-00-040-804 78-30-00-440-804 12-36-29-991-032 12-36-29-991-013 FOR FIN 4030EM1 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801
Fill the Green Hydraulic Reservoir with a Hydraulic Service Cart Fill the Green Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Drainage of the Green Hydraulic Reservoir Servicing of the (Forward) Engine-Pump Case-Drain Filter Element 5013JM1 Servicing of the Green Reservoir LP-Filter (5011JM1) Depressurization of the Green Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Deactivation of the Thrust Reverser for Maintenance Reactivation of the Thrust Reverser after Maintenance Fig. 301 Fig. 302 Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS)
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 302 Jul 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------78-30-00-410-801 FOR FIN 4030EM2 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801 78-30-00-410-801
Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Opening of (5120EA) Closing of (5120EA) Opening of 4130KS) Closing of 4130KS)
the Aft Fan Cowl Doors (5110EA) and the Aft Fan Cowl Doors (5110EA) and the Thrust Reverser Cowl Doors (4120KS to the Thrust Reverser Cowl Doors (4120KS to
3. __________ Job Set-up Subtask 12-36-29-860-062 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Make sure that the Green hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-804). (3) Depressurize the reservoir of the Green hydraulic system (Ref. TASK 29-14-00-614-801). (4) Drain the Green hydraulic reservoir (Ref. TASK 29-10-00-611-801). Subtask 12-36-29-941-062 B. Safety Precautions (1) Make sure that the engine 1(2), shutdown occurred not less than 5 minutes before you do this procedure. (2) On the panel 225VU, make sure that the APU BLEED pushbutton switch is released (ON legend off) and install a warning notice to tell persons not to use it.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 303 Jul 01/05
(3) Put a warning notice in position to tell persons not to pressurize the hydraulic system: - on the HYD/FUEL control panel 245VU in the cockpit, - on the Green hydraulic system, access door 197CB. (4) On the panel 125VU: - make sure that the ENG MASTER switches for the two engines are in the OFF position, - put a warning notice to tell persons not to supply power to the EEC. (5) On the panel 285VU: - make sure that the ON legend of the related ENG FADEC GND PWR pushbutton switch is off, - put a warning notice to tell persons not to supply power to the FADEC system. (6) Put a container below the Green hydraulic engine pump and below the case drain filter. Subtask 12-36-29-865-076 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU HYD PUMP G CTL 9JV U09 721VU HYD PUMP G ENG 1 14JG2 X11 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 721VU HYD PUMP G CTL 9JV U09 722VU FADEC B ENG 2 13KS2 K49 722VU HYD PUMP G ENG 2 14JG1 X45 742VU FADEC A ENG 2 12KS2 Q74
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 304 Jul 01/05
Subtask 12-36-29-010-075 D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Open the fan cowl doors FOR 4030EM1 Open the door 415BL (Ref. TASK 71-13-00-010-802). FOR 4030EM2 Open the door 425BL (Ref. TASK 71-13-00-010-802). Subtask 12-36-29-040-062 E. Make the thrust reverser unserviceable for maintenance (Ref. TASK 78-3000-040-804). Subtask 12-36-29-010-132 F. Get Access (1) Open the right thrust-reverser door: FOR 4030EM1 Open the door 417AL (Ref. TASK 78-30-00-010-801). FOR 4030EM2 Open the door 427AL (Ref. TASK 78-30-00-010-801). (2) Put the access platform in position. (3) Put a container under the applicable hose. Subtask 12-36-29-010-076 G. Get access to the avionics compartment. (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the door of the AC/DC emergency power-center 740VU. (4) Put the adjustable access platform in position.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 305 Jul 01/05
4. Procedure _________ Subtask 12-36-29-860-086 A. Preparation before the flushing of the Case-Drain line (Ref. Fig. 301/TASK 12-36-29-991-032) CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE ON THE GROUND HYDRAULIC CART _______ IS SET TO A MINIMUM OF 7 BARS (101.53 PSI). CAUTION : BE CAREFUL WHEN YOU DISCONNECT THE RETURN LINE FROM THE _______ RESERVOIR. THE HYDRAULIC FLUID IN THE LINE WILL FLOW OUT. (1) Remove the two clamps (2) from the return line (1). (2) Disconnect the return line (1) from the reservoir and from the filter (5011JM1). (3) Remove the return line (1) between the reservoir and from the filter (5011JM1). (4) Put blanking plug to the reseroir. (5) Connect the return hose of the hydraulic power cart to the filter (5011JM1) with the hydraulic power cart/return line interface (98F12303000100) of the HYDRAULIC CONNECTORS (98F12303000000). (6) Attach the return of the hydraulic power cart to the aircraft structure with a strap. (7) Disconnect the case drain line from the engine pump. (8) Put a blanking plug to the case drain. (9) Connect the pressure hose of the hydraulic power cart to the case drain line with the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000). Subtask 12-36-29-170-062 B. Flushing of the Case-Drain Line (Ref. Fig. 302/TASK 12-36-29-991-013) adaptor. (1) Operate the hydraulic power cart for 2mn at 20 bars. (2) Stop the hydraulic power cart.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 306 Jul 01/05
(3) Replace the hydraulic filters, case drain and LP: - the two case drain filters 5013JM1 (Ref. TASK 29-11-43-600-802), - the LP filter 5011JM1 (Ref. TASK 29-11-44-600-801). Subtask 12-36-29-420-062 C. Connection of the Hydraulic Line (1) Remove the strap which attach the return hose of the hydraulic power cart to the aircraft structure. (2) Remove the blanking plug from the reservoir. (3) Remove the hydraulic power cart/return line interface (98F12303000100) of the HYDRAULIC CONNECTORS (98F12303000000) from the filter (5011JM1) and from the hydraulic power cart. (4) Connect the return line (1) to the reservoir and to the filter (5011JM1). (5) Install the two clamps (2) on the return line (1). (6) Remove the blanking plug from the case drain. (7) Remove the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000) from the case drain line and from the hydraulic power cart. (8) Connect the case drain line to the engine pump. (9) TORQUE the case drain line to between 2.43 and 3.16 m.daN (17.92 and 23.30 lbf.ft). Subtask 12-36-29-865-077 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 4030EM1 9JV, 14JG2, 12KS1, 13KS1 FOR 4030EM2 9JV, 14JG1, 12KS2, 13KS2 Subtask 12-36-29-611-062 E. Fill the Green hydraulic reservoir (Ref. TASK 12-12-29-611-801) or (Ref. TASK 12-12-29-611-802).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 307 Jul 01/05
Hydraulic Connections Figure 301/TASK 12-36-29-991-032- 12 (SHEET 1) R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 308 Jul 01/05
Hydraulic Connections Figure 301/TASK 12-36-29-991-032- 22 (SHEET 2) R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 309 Jul 01/05
Flushing of the Case-Drain Line of the Green Hydraulic System Figure 302/TASK 12-36-29-991-013 R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 310 Jul 01/05
Subtask 12-36-29-863-062 F. Pressurize the Green hydraulic reservoir (Ref. TASK 29-14-00-614-804). Subtask 12-36-29-410-131 G. Close the right thrust reverser : - FOR 4030EM1 close the door 417AL (Ref. TASK 78-30-00-410-801) - FOR 4030EM2 close the door 427AL (Ref. TASK 78-30-00-410-801) Subtask 12-36-29-440-062 H. Make sure that the thrust reverser is serviceable after maintenance (Ref. TASK 78-30-00-440-804). Subtask 12-36-29-410-074 J. Close the fan cowl doors FOR 4030EM1 - close the door 415BL (Ref. TASK 71-13-00-410-802) FOR 4030EM2 - close the door 425BL (Ref. TASK 71-13-00-410-802). Subtask 12-36-29-281-062 K. Sampling (1) Perform a fluid sampling for particular contamination (Ref. TASK 1232-29-281-801). (2) Perform in daily check, the check of the clogging indicators, of the case drain filters 5013JM1, HP filters 5111JM101, 5111JM102, LP filter 5011JM1. Do this operation again until the clogging indicator stay in. 5. Close-up ________ Subtask 12-36-29-410-075 A. Close Access (1) Close the door of the AC/DC emergency power-center 740VU. (2) Close the access door 811.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 311 Jul 01/05
(3) Remove the access platform(s). (4) Close the MLG doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-942-062 B. Remove the safety devices (1) Remove the warning notice(s). Subtask 12-36-29-862-062 C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 312 Jul 01/05
**ON A/C 701-749, TASK 12-36-29-170-801-A Flushing of the Case-Drain line of the Green Hydraulic System WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job To flush the Green hydraulic system after a failure of the engine pump. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No No
specific specific specific specific specific specific specific specific specific
98F12303000000
adjustable access platform blanking plug circuit breaker(s) safety clip(s) hydraulic power cart strap warning notice access platform 2.5 m (8 ft. 2 in.) container 5 l (1.3208 USgal) Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft) 1 HYDRAULIC CONNECTORS
R EFF : 701-749, 12-36-29 SROS
Page 313 Apr 01/02
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-801 12-12-29-611-802 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-10-00-611-801 29-11-43-600-807 29-11-44-600-801 29-14-00-614-801 R 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 12-36-29-991-033 12-36-29-991-019 FOR FIN 4030EM1 71-13-00-010-805 71-13-00-410-805 FOR FIN 4030EM2 71-13-00-010-805 71-13-00-410-805
Fill the Green Hydraulic Reservoir with a Hydraulic Service Cart Fill the Green Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Drainage of the Green Hydraulic Reservoir Servicing of the Engine-Pump Case Drain Filter (5013JM1) Servicing of the Green Reservoir LP-Filter (5011JM1) Depressurization of the Green Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Fig. 303 Fig. 304 Open the Fan Cowl Doors Close the Fan Cowl Doors Open the Fan Cowl Doors Close the Fan Cowl Doors
3. __________ Job Set-up Subtask 12-36-29-860-068 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Make sure that the Green hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-804).
EFF : 701-749, 12-36-29 SROS
Page 314 Apr 01/05
(3) Depressurize the reservoir of the Green hydraulic system (Ref. TASK 29-14-00-614-801). (4) Drain the Green hydraulic reservoir (Ref. TASK 29-10-00-611-801). Subtask 12-36-29-941-068 B. Safety Precautions (1) Make sure that the engine 1(2), shutdown occurred not less than 5 minutes before you do this procedure. (2) On the panel 225VU, make sure that the APU BLEED pushbutton switch is released (ON legend off) and install a warning notice to tell persons not to use it. (3) Put a warning notice in position to tell persons not to pressurize the hydraulic system: - on the HYD/FUEL control panel 245VU in the cockpit, - on the Green hydraulic system, access door 197CB. (4) On the panel 125VU: - make sure that the ENG MASTER switches for the two engines are in the OFF position, - put a warning notice to tell persons not to supply power to the EEC. (5) On the panel 285VU: - make sure that the ON legend of the related ENG FADEC GND PWR pushbutton switch is off, - put a warning notice to tell persons not to supply power to the FADEC system. (6) Put a container below the Green hydraulic engine pump and below the case drain filter.
EFF : 701-749, 12-36-29 R SROS
Page 315 Oct 01/02
Subtask 12-36-29-865-088 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU HYD PUMP G CTL 9JV U09 722VU FADEC B ENG 1 13KS1 D44 742VU HYD PUMP G ENG 1 14JG2 E67 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 721VU HYD PUMP G CTL 9JV U09 722VU FADEC B ENG 2 13KS2 K49 722VU HYD PUMP G ENG 2 14JG1 X45 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-36-29-010-087 D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Open the fan cowl doors FOR 4030EM1 Open the door 416AR (Ref. TASK 71-13-00-010-805) FOR 4030EM2 Open the door 426AR (Ref. TASK 71-13-00-010-805). Subtask 12-36-29-010-088 E. Get access to the avionics compartment. (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the door of the AC/DC emergency power-center 740VU. (4) Put the adjustable access platform in position.
R EFF : 701-749, 12-36-29 SROS
Page 316 Oct 01/04
4. Procedure _________ Subtask 12-36-29-860-092 A. Preparation before the flushing of the Case-Drain line (Ref. Fig. 303/TASK 12-36-29-991-033) R R
CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE ON THE GROUND HYDRAULIC CART _______ IS SET TO A MINIMUM OF 7 BARS (101.53 PSI). CAUTION : BE CAREFUL WHEN YOU DISCONNECT THE RETURN LINE FROM THE _______ RESERVOIR. THE HYDRAULIC FLUID IN THE LINE WILL FLOW OUT. (1) Remove the two clamps (2) from the return line (1). (2) Disconnect the return line (1) from the reservoir and from the filter (5011JM1). (3) Remove the return line (1) between the reservoir and the filter (5011JM1). (4) Put blanking plug to the reservoir. (5) Connect the return hose of the hydraulic power cart to the filter (5011JM1) with the hydraulic power cart/return line interface (98F12303000100) of the HYDRAULIC CONNECTORS (98F12303000000). (6) Attach the return hose of the hydraulic power cart to the aircraft structure with a strap. (7) Disconnect the case drain line from the engine pump. (8) Put a blanking plug to the case drain. (9) Connect the pressure hose of the hydraulic power cart to the case drain line with the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000). Subtask 12-36-29-170-068 B. Flushing of the Case-Drain Line (Ref. Fig. 304/TASK 12-36-29-991-019) (1) Operate the hydraulic power cart for 2mn at 20 bars. (2) Stop the hydraulic power cart.
EFF : 701-749, 12-36-29 SROS
Page 317 Oct 01/04
Hydraulic Connections Figure 303/TASK 12-36-29-991-033- 12 (SHEET 1) EFF : 701-749, 12-36-29 R SROS
Page 318 Oct 01/04
Hydraulic Connections Figure 303/TASK 12-36-29-991-033- 22 (SHEET 2) R EFF : 701-749, 12-36-29 SROS
Page 319 Oct 01/04
Flushing of the Case-Drain Line of the Green Hydraulic system Figure 304/TASK 12-36-29-991-019 EFF : 701-749, 12-36-29 R SROS
Page 320 Oct 01/04
INTENTIONALLY BLANK
R 12-36-29 SROS
Page 321 Oct 01/04
INTENTIONALLY BLANK
R 12-36-29 SROS
Page 322 Oct 01/04
(3) Replace the hydraulic filters, case drain and LP: - the two case drain filters 5013JM1 (Ref. TASK 29-11-43-600-807), - the LP filter 5011JM1 (Ref. TASK 29-11-44-600-801). Subtask 12-36-29-420-068 C. Connection of the Hydraulic Line (1) Remove the strap which attach the return hose of the hydraulic power cart to the aircraft structure. (2) Remove the blanking plug from the reservoir. (3) Remove the hydraulic power cart/return line interface (98F12303000100) of the HYDRAULIC CONNECTORS (98F12303000000) from the filter (5011JM) and from the hydraulic power cart. (4) Connect the return line (1) to the resevoir and to the filter (5011JM1). (5) Install the two clamps (2) on the return line (1). (6) Remove the blanking plug from the case drain. (7) Remove the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000) from the case drain line and from the hydraulic power cart. (8) Connect the case drain line to the engine pump. (9) TORQUE the case drain line to between 2.43 and 3.16 m.daN (17.92 and 23.30 lbf.ft). Subtask 12-36-29-865-089 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 4030EM1 9JV, 14JG2, 12KS1, 13KS1 FOR 4030EM2 9JV, 14JG1, 12KS2, 13KS2 Subtask 12-36-29-611-068 E. Fill the Green hydraulic reservoir (Ref. TASK 12-12-29-611-801) or (Ref. TASK 12-12-29-611-802).
EFF : 701-749, 12-36-29 R SROS
Page 323 Apr 01/01
Subtask 12-36-29-863-068 F. Pressurize the Green hydraulic reservoir (Ref. TASK 29-14-00-614-804). Subtask 12-36-29-410-086 G. Close the fan cowl doors FOR 4030EM1 - close the door 416AR (Ref. TASK 71-13-00-410-805) FOR 4030EM2 - close the door 426AR (Ref. TASK 71-13-00-410-805). Subtask 12-36-29-281-068 H. Sampling (1) Perform a fluid sampling for particular contamination (Ref. TASK 1232-29-281-801). (2) Perform in daily check, the check of the clogging indicators, of the case drain filters 5013JM1, HP filters 5111JM101, 5111JM102, LP filter 5011JM1. Do this operation again until the clogging indicator stay in. 5. Close-up ________ Subtask 12-36-29-410-087 A. Close Access (1) Close the door of the AC/DC emergency power-center 740VU. (2) Close the access door 811. (3) Remove the access platform(s). (4) Close the MLG doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-942-068 B. Remove the safety devices (1) Remove the warning notice(s).
R EFF : 701-749, 12-36-29 SROS
Page 324 Apr 01/01
Subtask 12-36-29-862-068 C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 701-749, 12-36-29 SROS
Page 325 Apr 01/01
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, TASK 12-36-29-170-802 Flushing of the HP line of the Green Hydraulic System WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job To flush the Green hydraulic system after a failure of the engine pump. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No No No
specific specific specific specific specific specific specific specific specific specific
adjustable access platform blanking plugs circuit breaker(s) safety clip(s) hydraulic power cart warning notice access platform 2.5 m (8 ft. 2 in.) container 20 l (5.2833 USgal) access platform 3 m (9 ft. 10 in.) container 5 l (1.3208 USgal) Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft)
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 326 Jul 01/05
------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific 98F12303000000
Torque Wrench : range 1.00 to 10.00 m.daN (8.00 to 75.00 lbf.ft) Torque Wrench : range 2.00 to 20.00 m.daN (15.00 to 150.00 lbf.ft) 1 HYDRAULIC CONNECTORS
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-801 12-12-29-611-802 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-11-45-600-801 29-14-00-614-801 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 78-30-00-040-804 78-30-00-440-804
Fill the Green Hydraulic Reservoir with a Hydraulic Service Cart Fill the Green Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Servicing of the Green HP Filter (5111JM101,5111JM102) Depressurization of the Green Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Deactivation of the Thrust Reverser for Maintenance Reactivation of the Thrust Reverser after Maintenance
R 12-36-29-991-035 12-36-29-991-014 FOR FIN 4030EM1 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801
Fig. 305 Fig. 306 Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS)
EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 327 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------78-30-00-410-801 FOR FIN 4030EM2 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801 78-30-00-410-801
Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Opening of (5120EA) Closing of (5120EA) Opening of 4130KS) Closing of 4130KS)
the Aft Fan Cowl Doors (5110EA) and the Aft Fan Cowl Doors (5110EA) and the Thrust Reverser Cowl Doors (4120KS to the Thrust Reverser Cowl Doors (4120KS to
3. __________ Job Set-up Subtask 12-36-29-860-063 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Make sure that the Green hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-804). (3) Depressurize the reservoir of the Green hydraulic system (Ref. TASK 29-14-00-614-801). Subtask 12-36-29-941-063 B. Safety Precautions (1) Make sure that the engine 1(2), shutdown occurred not less than 5 minutes before you do this procedure. (2) On the panel 225VU, make sure that the APU BLEED pushbutton switch is released (ON legend off) and install a warning notice to tell persons not to use it. (3) Put a warning notice in position to tell persons not to pressurize the hydraulic system: - on the HYD/FUEL control panel 245VU in the cockpit, - on the Green hydraulic system, access door 197CB.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 328 Jul 01/05
(4) On the panel 125VU: - make sure that the ENG MASTER switches for the two engines are in the OFF position, - put a warning notice to tell persons not to supply power to the EEC. (5) On the panel 285VU: - make sure that the ON legend of the related ENG FADEC GND PWR pushbutton switch is off, - put a warning notice to tell persons not to supply power to the FADEC system. (6) Put a container below the Green hydraulic engine pump and below the case drain filter. Subtask 12-36-29-865-078 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU HYD PUMP G CTL 9JV U09 721VU HYD PUMP G ENG 1 14JG2 X11 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 721VU HYD PUMP G CTL 9JV U09 722VU FADEC B ENG 2 13KS2 K49 722VU HYD PUMP G ENG 2 14JG1 X45 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-36-29-010-077 D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Open the fan cowl doors FOR 4030EM1 Open the door 415BL (Ref. TASK 71-13-00-010-802). FOR 4030EM2 Open the door 425BL (Ref. TASK 71-13-00-010-802).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 329 Jul 01/05
Subtask 12-36-29-040-063 E. Make the thrust reverser unserviceable for maintenance (Ref. TASK 78-3000-040-804). Subtask 12-36-29-010-133 F. Get Access (1) Open the right thrust-reverser door: FOR 4030EM1 Open the door 417AL (Ref. TASK 78-30-00-010-801). FOR 4030EM2 Open the door 427AL (Ref. TASK 78-30-00-010-801). (2) Put the access platform in position. (3) Put a container under the applicable hose. Subtask 12-36-29-010-078 G. Get access to the avionics compartment. (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the door of the AC/DC emergency power-center 740VU. (4) Put the adjustable access platform in position. 4. Procedure _________ Subtask 12-36-29-860-087 A. Preparation before the flushing of the HP line (Ref. Fig. 305/TASK 12-36-29-991-035) CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE ON THE GROUND HYDRAULIC CART _______ IS SET TO A MINIMUM OF 7 BARS (101.53 PSI). (1) Disconnect the case drain line from the engine pump. (2) Disconnect the pressure line from the engine pump. (3) Disconnect the case drain line from the case drain filter.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 330 Jul 01/05
Hydraulic Connections Figure 305/TASK 12-36-29-991-035 R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 331 Jul 01/05
(4) Connect the pressure line and the case drain line together with the engine pump case drain/engine pump pressure connection (98F12303000104) of the HYDRAULIC CONNECTORS (98F12303000000). (5) Connect the pressure hose of the hydraulic power cart to the case drain line with the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000). (6) Connect the return hose of the hydraulic power cart to the interface (98F12303000106) of the HYDRAULIC CONNECTORS (98F12303000000). (7) Connect the free end of the interface to the delivery ground connector 5131JM1. (8) Put blanking plugs on the disconnected line ends. (9) Close the leak measurement valve. - on the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/GREEN pushbutton switch (the OFF legend comes on). Subtask 12-36-29-170-063 B. Flushing of the HP Line (Ref. Fig. 306/TASK 12-36-29-991-014) (1) Operate the hydraulic power cart for 2mn at 20 bars. (2) Stop the hydraulic power cart. (3) Open the leak measurement valve: - on the HYD section of the maintenance panel 285VU, push the LEAK MEASUREMENT VALVES/GREEN pushbutton switch (the OFF legend goes off). R R
(4) Replace the HP filters 5111JM101 and 5111JM102 (Ref. TASK 29-11-45600-801).
R
EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 332 Jan 01/07
Flushing of the HP Line of the Green Hydraulic System Figure 306/TASK 12-36-29-991-014 R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 333 Jul 01/05
Subtask 12-36-29-420-063 C. Connection of the Hydraulic Line (1) Remove the blanking plugs from the disconnected line ends. (2) Remove the engine pump case drain/engine pump pressure connection (98F12303000104) of the HYDRAULIC CONNECTORS (98F12303000000) from the pressure line and from the case drain line. (3) Remove the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000) from the case drain line and from the hydraulic power cart. (4) Connect the pressure line to the engine pump. (5) TORQUE the pressure line to between 12.88 and 14.24 m.daN (94.98 and 105.01 lbf.ft). (6) Connect the case drain line to the engine pump. (7) TORQUE the case drain line to between 2.43 and 3.16 m.daN (17.92 and 23.30 lbf.ft). (8) Connect the pump case drain hose to the case drain. (9) TORQUE the case drain hose to between 5.31 and 6.21 m.daN (39.15 and 45.79 lbf.ft). Subtask 12-36-29-865-079 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 4030EM1 9JV, 14JG2, 12KS1, 13KS1 FOR 4030EM2 9JV, 9JV, 14JG1, 12KS2, 13KS2 Subtask 12-36-29-611-063 E. Fill the Green hydraulic reservoir (Ref. TASK 12-12-29-611-801) or (Ref. TASK 12-12-29-611-802). Subtask 12-36-29-863-063 F. Pressurize the Green hydraulic reservoir (Ref. TASK 29-14-00-614-804).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 334 Jul 01/05
Subtask 12-36-29-410-132 G. Close the right thrust reverser : - FOR 4030EM1 close the door 417AL (Ref. TASK 78-30-00-410-801) - FOR 4030EM2 close the door 427AL (Ref. TASK 78-30-00-410-801) Subtask 12-36-29-440-063 H. Make sure that the thrust reverser is serviceable after maintenance (Ref. TASK 78-30-00-440-804). Subtask 12-36-29-410-076 J. Close the fan cowl doors FOR 4030EM1 - close the door 415BL (Ref. TASK 71-13-00-410-802) FOR 4030EM2 - close the door 425BL (Ref. TASK 71-13-00-410-802). Subtask 12-36-29-281-063 K. Sampling (1) Perform a fluid sampling for particular contamination (Ref. TASK 1232-29-281-801). R R
(2) Perform in daily check of the clogging indicators of the HP filters 5111JM101 and 5111JM102. Do this operation again until the clogging indicator stay in. 5. Close-up ________ Subtask 12-36-29-410-077 A. Close Access (1) Close the door of the AC/DC emergency power-center 740VU. (2) Close the access door 811. (3) Remove the access platform(s). (4) Close the MLG doors (Ref. TASK 32-12-00-410-801).
EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 335 Jan 01/07
Subtask 12-36-29-942-063 B. Remove the safety devices (1) Remove the warning notice(s). Subtask 12-36-29-862-063 C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 336 Jul 01/05
**ON A/C 701-749, TASK 12-36-29-170-802-A Flushing of the HP line of the Green Hydraulic System WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job To flush the Green Hydraulic System after a failure of the engine pump. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No
specific specific specific specific specific specific specific specific
No specific 98F12303000000
adjustable access platform blanking plugs circuit breaker(s) safety clip(s) hydraulic power cart warning notice access platform 2.5 m (8 ft. 2 in.) container 5 l (1.3208 USgal) Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft) Torque Wrench : range 2.00 to 20.00 m.daN (15.00 to 150.00 lbf.ft) 1 HYDRAULIC CONNECTORS
EFF : 701-749, 12-36-29 R SROS
Page 337 Apr 01/01
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-801 12-12-29-611-802 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-11-45-600-801 29-14-00-614-801 R 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 78-31-41-000-803 12-36-29-991-036 12-36-29-991-020 FOR FIN 4030EM1 71-13-00-010-805 71-13-00-410-805 FOR FIN 4030EM2 71-13-00-010-805 71-13-00-410-805
Fill the Green Hydraulic Reservoir with a Hydraulic Service Cart Fill the Green Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Servicing of the Green HP Filter (5111JM101,5111JM102) Depressurization of the Green Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Removal of the Isolation Control Unit (4117KS) Fig. 307 Fig. 308 Open the Fan Cowl Doors Close the Fan Cowl Doors Open the Fan Cowl Doors Close the Fan Cowl Doors
3. __________ Job Set-up Subtask 12-36-29-860-069 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Make sure that the Green hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-804).
EFF : 701-749, 12-36-29 SROS
Page 338 Apr 01/05
(3) Depressurize the reservoir of the Green hydraulic system (Ref. TASK 29-14-00-614-801). Subtask 12-36-29-941-069 B. Safety Precautions (1) Make sure that the engine 1(2), shutdown occurred not less than 5 minutes before you do this procedure. (2) On the panel 225VU, make sure that the APU BLEED pushbutton switch is released (ON legend off) and install a warning notice to tell persons not to use it. (3) Put a warning notice in position to tell persons not to pressurize the hydraulic system: - on the HYD/FUEL control panel 245VU in the cockpit, - on the Green hydraulic system, access door 197CB. (4) On the panel 125VU: - make sure that the ENG MASTER switches for the two engines are in the OFF position, - put a warning notice to tell persons not to supply power to the ECU. (5) On the panel 285VU: - make sure that the ON legend of the related ENG FADEC GND PWR pushbutton switch is off, - put a warning notice to tell persons not to supply power to the FADEC system. (6) Put a container below the Green hydraulic engine pump and below the case drain filter.
EFF : 701-749, 12-36-29 R SROS
Page 339 Apr 01/01
Subtask 12-36-29-865-091 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU HYD PUMP G CTL 9JV U09 722VU FADEC B ENG 1 13KS1 D44 742VU HYD PUMP G ENG 1 14JG2 E67 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 721VU HYD PUMP G CTL 9JV U09 722VU FADEC B ENG 2 13KS2 K49 722VU HYD PUMP G ENG 2 14JG1 X45 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-36-29-010-089 D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Open the fan cowl doors FOR 4030EM1 Open the door 416AR (Ref. TASK 71-13-00-010-805) FOR 4030EM2 Open the door 426AR (Ref. TASK 71-13-00-010-805). Subtask 12-36-29-010-098 E. Get access to the avionics compartment. (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the door of the AC/DC emergency power-center 740VU. (4) Put the adjustable access platform in position.
EFF : 701-749, 12-36-29 R SROS
Page 340 Apr 01/01
4. Procedure _________ Subtask 12-36-29-860-093 A. Preparation before the flushing of the HP line (Ref. Fig. 307/TASK 12-36-29-991-036) R R
CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE ON THE GROUND HYDRAULIC CART _______ IS SET TO A MINIMUM OF 7 BARS (101.53 PSI). (1) Disconnect the case drain line from the engine pump. (2) Disconnect the pressure line from the engine pump. (3) Disconnect the case drain line from the case drain filter. (4) Connect the pressure line and the case drain line together with the engine pump case drain/engine pump pressure connection (98F12303000104) of the HYDRAULIC CONNECTORS (98F12303000000). (5) Connect the pressure hose of the hydraulic power cart to the case drain line with the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000). (6) Connect the return hose of the hydraulic power cart to the interface (98F12303000106) of the HYDRAULIC CONNECTORS (98F12303000000). (7) Connect the free end of the interface to the delivery ground connector 5131JM1. (8) Put blanking plugs on the disconnected line ends. (9) Close the leak measurement valve. - on the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/GREEN pushbutton switch (the OFF legend comes on). Subtask 12-36-29-170-069 B. Flushing of the HP Line (Ref. Fig. 308/TASK 12-36-29-991-020) (1) Operate the hydraulic power cart for 2mn at 20 bars. (2) Stop the hydraulic power cart.
EFF : 701-749, 12-36-29 SROS
Page 341 Oct 01/04
Hydraulic Connections Figure 307/TASK 12-36-29-991-036 EFF : 701-749, 12-36-29 R SROS
Page 342 Apr 01/01
Flushing of the HP Line of the Green Hydraulic System Figure 308/TASK 12-36-29-991-020 EFF : 701-749, 12-36-29 R SROS
Page 343 Apr 01/01
(3) Open the leak measurement valve: - on the HYD section of the maintenance panel 285VU, push the LEAK MEASUREMENT VALVES/GREEN pushbutton switch (the OFF legend goes off). (4) Replace the hydraulic filters, HP and filter element: - replace the HP filters 5111JM101, 5111JM102 (Ref. TASK 29-11-45600-801), - replace the filter element located on the Isolation Control Unit 4117KS (Ref. TASK 78-31-41-000-803). Subtask 12-36-29-420-069 C. Connection of the Hydraulic Line (1) Remove the blanking plugs from the disconnected line ends. (2) Remove the engine pump case drain/engine pump pressure connection (98F12303000104) of the HYDRAULIC CONNECTORS (98F12303000000) from the pressure line and from the case drain line. (3) Remove the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000) from the case drain line and from the hydraulic power cart. (4) Connect the pressure line to the engine pump. (5) TORQUE the pressure line to between 12.88 and 14.24 m.daN (94.98 and 105.01 lbf.ft). (6) Connect the case drain line to the engine pump. (7) Connect the pump case drain hose to the case drain. (8) TORQUE the case drain line to between 2.43 and 3.16 m.daN (17.92 and 23.30 lbf.ft). Subtask 12-36-29-865-092 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 4030EM1 9JV, 14JG2, 12KS1, 13KS1 FOR 4030EM2 9JV, 14JG1, 12KS2, 13KS2
EFF : 701-749, 12-36-29 R SROS
Page 344 Apr 01/01
Subtask 12-36-29-611-069 E. Fill the Green hydraulic reservoir (Ref. TASK 12-12-29-611-801) or (Ref. TASK 12-12-29-611-802). Subtask 12-36-29-863-069 F. Pressurize the Green hydraulic reservoir (Ref. TASK 29-14-00-614-804). Subtask 12-36-29-410-088 G. Close the fan cowl doors FOR 4030EM1 - close the door 416AR (Ref. TASK 71-13-00-410-805) FOR 4030EM2 - close the door 426AR (Ref. TASK 71-13-00-410-805). Subtask 12-36-29-281-069 H. Sampling (1) Perform a fluid sampling for particular contamination (Ref. TASK 1232-29-281-801). (2) Perform in daily check, the check of the clogging indicators of the HP filters 5111JM101, 5111JM102 and the filter element located on the Isolation Control Unit 4117KS. Do this operation again until the clogging indicator stay in. 5. Close-up ________ Subtask 12-36-29-410-089 A. Close Access (1) Close the door of the AC/DC emergency power-center 740VU. (2) Close the access door 811. (3) Remove the access platform(s). (4) Close the MLG doors (Ref. TASK 32-12-00-410-801).
R EFF : 701-749, 12-36-29 SROS
Page 345 Apr 01/01
Subtask 12-36-29-942-069 B. Remove the safety devices (1) Remove the warning notice(s). Subtask 12-36-29-862-069 C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 701-749, 12-36-29 SROS
Page 346 Apr 01/01
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, TASK 12-36-29-170-803 Flushing of the Case-Drain line of the Blue Hydraulic System WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job To flush the Blue hydraulic system after a failure of the engine pump. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No No
specific specific specific specific specific specific specific specific specific
98F12303000000
adjustable access platform blanking plug circuit breaker(s) safety clip(s) hydraulic power cart strap warning notice access platform 2.5 m (8 ft. 2 in.) container 5 l (1.3208 USgal) Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft) 1 HYDRAULIC CONNECTORS
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 347 Jul 01/05
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-803 12-12-29-611-804 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-10-00-611-802 29-11-43-600-804 29-12-44-600-801 29-12-45-600-801 29-14-00-614-802 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 78-30-00-040-804 78-30-00-440-804 12-36-29-991-038 12-36-29-991-015 FOR FIN 4030EM1 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801 78-30-00-410-801
Fill the Blue Hydraulic Reservoir with a Hydraulic Service Cart Fill the Blue Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Drainage of the Blue Hydraulic Reservoir Servicing of the (Aft) Engine-Pump Case-Drain Filter Element 5013JM2 Servicing of the Blue Reservoir LP-Filter (5011JM2) Servicing of the Blue HP Filter (5111JM2) Depressurization of the Blue Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Deactivation of the Thrust Reverser for Maintenance Reactivation of the Thrust Reverser after Maintenance Fig. 309 Fig. 310 Opening of (5120EA) Closing of (5120EA) Opening of 4130KS) Closing of 4130KS)
the Aft Fan Cowl Doors (5110EA) and the Aft Fan Cowl Doors (5110EA) and the Thrust Reverser Cowl Doors (4120KS to the Thrust Reverser Cowl Doors (4120KS to
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 348 Jul 01/05
3. __________ Job Set-up Subtask 12-36-29-860-064 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Make sure that the Blue hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-804). (3) Depressurize the reservoir of the Blue hydraulic system (Ref. TASK 29-14-00-614-802). (4) Drain the Blue hydraulic reservoir (Ref. TASK 29-10-00-611-802). Subtask 12-36-29-941-064 B. Safety Precautions (1) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure. (2) On the panel 225VU, make sure that the APU BLEED pushbutton switch is released (ON legend off) and install a warning notice to tell persons not to use it. (3) Put a warning notice in position to tell persons not to pressurize the hydraulic system: - on the HYD/FUEL control panel 245VU in the cockpit, - on the Blue hydraulic system, access door 196BB. (4) On the panel 125VU: - make sure that the ENG MASTER switches for the two engines are in the OFF position, - put a warning notice to tell persons not to supply power to the EEC. (5) On the panel 285VU: - make sure that the ON legend of the related ENG FADEC GND PWR pushbutton switch is off, - put a warning notice to tell persons not to supply power to the FADEC system.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 349 Jul 01/05
(6) Put a container below the Blue hydraulic engine pump and below the case drain filter. Subtask 12-36-29-865-080 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU HYD PUMP B ENG 1 11JB U08 721VU HYD PUMP B CTL 9JC X12 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 Subtask 12-36-29-010-079 D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Open the fan cowl doors: FOR 4030EM1 Open the door 415BL (Ref. TASK 71-13-00-010-802) Subtask 12-36-29-040-064 E. Make the thrust reverser unserviceable for maintenance (Ref. TASK 78-3000-040-804). Subtask 12-36-29-010-134 F. Get Access (1) Open the right thrust-reverser door: FOR 4030EM1 Open the door 417AL (Ref. TASK 78-30-00-010-801). Subtask 12-36-29-010-080 G. Get access to the avionics compartment. (1) Put the access platform in position at the access door 811. (2) Open the access door 811.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 350 Jul 01/05
(3) Open the door of the AC/DC emergency power-center 740VU. (4) Put the adjustable access platform in position. 4. Procedure _________ Subtask 12-36-29-860-088 A. Preparation before the flushing of the Case-Drain line (Ref. Fig. 309/TASK 12-36-29-991-038) CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE ON THE GROUND HYDRAULIC CART _______ IS SET TO A MINIMUM OF 7 BARS (101.53 PSI). CAUTION : BE CAREFUL WHEN YOU DISCONNECT THE RETURN LINE FROM THE _______ RESERVOIR. THE HYDRAULIC FLUID IN THE LINE WILL FLOW OUT. (1) Disconnect and remove the return line from the reservoir and from the filter (5011JM2). (2) Put a blanking plug on the reservoir. (3) Connect the return hose of the hydraulic power cart to the filter (5011JM2) with the hydraulic power cart/return line interface (98F12303000100) of the HYDRAULIC CONNECTORS (98F12303000000). (4) Attach the return hose of the hydraulic power cart to the aicraft structure with a strap. (5) Disconnect the case drain line from the engine pump. (6) Put a blanking plug to the case drain. (7) Connect the pressure hose of the hydraulic power cart to the case drain line with the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000). Subtask 12-36-29-170-064 B. Flushing of the Case-Drain Line (Ref. Fig. 310/TASK 12-36-29-991-015) (1) Operate the hydraulic power cart for 2mn at 20 bars. (2) Stop the hydraulic power cart.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 351 Jul 01/05
Hydraulic connections Figure 309/TASK 12-36-29-991-038- 12 (SHEET 1) R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 352 Jul 01/05
Hydraulic connections Figure 309/TASK 12-36-29-991-038- 22 (SHEET 2) R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 353 Jul 01/05
Flushing of the Case-Drain Line of the Blue Hydraulic System Figure 310/TASK 12-36-29-991-015 R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 354 Jul 01/05
(3) Replace the hydraulic filters, case drain and LP: - the case drain filter 5013JM2 (Ref. TASK 29-11-43-600-804), - the LP filter 5011JM2 (Ref. TASK 29-12-44-600-801), - the HP filter 5111JM2 (Ref. TASK 29-12-45-600-801). Subtask 12-36-29-420-064 C. Connection of the Hydraulic Line (1) Remove the strap which attach the return hose of the hydraulic power cart to the structure. (2) Remove the blanking plug from the reservoir. (3) Remove the hydraulic power cart/return line interface (98F12303000100) of the HYDRAULIC CONNECTORS (98F12303000000) from the filter (5011JM2) and from the hydraulic power cart. (4) Connect the return line to the reservoir and to the filter (5011JM2). (5) Remove the blanking plug from the case drain. (6) Remove the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000) from the case drain line and from the hydraulic power cart. (7) Connect the case drain line to the engine pump. (8) TORQUE the case drain line to between 2.43 and 3.16 m.daN (17.92 and 23.30 lbf.ft). Subtask 12-36-29-865-081 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 4030EM1 9JC, 11JB, 12KS1, 13KS1 Subtask 12-36-29-611-064 E. Fill the Blue hydraulic reservoir (Ref. TASK 12-12-29-611-803) or (Ref. TASK 12-12-29-611-804). Subtask 12-36-29-863-064 F. Pressurize the Blue hydraulic reservoir (Ref. TASK 29-14-00-614-804).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 355 Jul 01/05
Subtask 12-36-29-410-133 G. Close the right thrust reverser : - FOR 4030EM1 close the door 417AL (Ref. TASK 78-30-00-410-801) Subtask 12-36-29-440-064 H. Make sure that the thrust reverser is serviceable after maintenance (Ref. TASK 78-30-00-440-804). Subtask 12-36-29-410-078 J. Close the fan cowl doors. FOR 4030EM1 - close the door 415BL (Ref. TASK 71-13-00-410-802). Subtask 12-36-29-281-064 K. Sampling (1) Perform a fluid sampling for particular contamination (Ref. TASK 1232-29-281-801). (2) Perform in daily check, the check of the clogging indicators, of the case drain filter 5013JM2, HP filter 5111JM2, LP filter 5011JM2. Do this operation again until the clogging indicator stay in. 5. Close-up ________ Subtask 12-36-29-410-079 A. Close Access (1) Close the door of the AC/DC emergency power-center 740VU. (2) Close the access door 811. (3) Remove the access platform(s). (4) Close the MLG doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-942-064 B. Remove the safety devices. (1) Remove the warning notice(s).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 356 Jul 01/05
Subtask 12-36-29-862-064 C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 357 Jul 01/05
**ON A/C 701-749, TASK 12-36-29-170-803-A Flushing of the Case-Drain line of the Blue Hydraulic System WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job To flush the Blue hydraulic system after a failure of the engine pump. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No No
specific specific specific specific specific specific specific specific specific
98F12303000000
adjustable access platform blanking plug circuit breaker(s) safety clip(s) hydraulic power cart strap warning notice access platform 2.5 m (8 ft. 2 in.) container 5 l (1.3208 USgal) Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft) 1 HYDRAULIC CONNECTORS
EFF : 701-749, 12-36-29 R SROS
Page 358 Apr 01/01
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-803 12-12-29-611-804 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-10-00-611-802 29-11-43-600-809 29-12-44-600-801 29-12-45-600-801 29-14-00-614-802 R 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 12-36-29-991-039 12-36-29-991-021 FOR FIN 4030EM1 71-13-00-010-805 71-13-00-410-805
Fill the Blue Hydraulic Reservoir with a Hydraulic Service Cart Fill the Blue Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Drainage of the Blue Hydraulic Reservoir Servicing of the Engine Pump Case Drain Filter (5013JM2) Servicing of the Blue Reservoir LP-Filter (5011JM2) Servicing of the Blue HP Filter (5111JM2) Depressurization of the Blue Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Fig. 311 Fig. 312 Open the Fan Cowl Doors Close the Fan Cowl Doors
3. __________ Job Set-up Subtask 12-36-29-860-070 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Make sure that the Blue hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-804).
EFF : 701-749, 12-36-29 SROS
Page 359 Apr 01/05
(3) Depressurize the reservoir of the Blue hydraulic system (Ref. TASK 29-14-00-614-802). (4) Drain the Blue hydraulic reservoir (Ref. TASK 29-10-00-611-802). Subtask 12-36-29-941-070 B. Safety Precautions (1) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure. (2) On the panel 225VU, make sure that the APU BLEED pushbutton switch is released (ON legend off) and install a warning notice to tell persons not to use it. (3) Put a warning notice in position to tell persons not to pressurize the hydraulic system: - on the HYD/FUEL control panel 245VU in the cockpit, - on the Blue hydraulic system, access door 196BB. (4) On the panel 125VU: - make sure that the ENG MASTER switches for the two engines are in the OFF position, - put a warning notice to tell persons not to supply power to the ECU. (5) On the panel 285VU: - make sure that the ON legend of the related ENG FADEC GND PWR pushbutton switch is off, - put a warning notice to tell persons not to supply power to the FADEC system. (6) Put a container below the Blue hydraulic engine pump and below the case drain filter.
EFF : 701-749, 12-36-29 R SROS
Page 360 Apr 01/01
Subtask 12-36-29-865-093 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU HYD PUMP B ENG 1 11JB U08 721VU HYD PUMP B CTL 9JC X12 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 Subtask 12-36-29-010-090 D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Open the fan cowl door FOR 4030EM1 Open the door 416AR (Ref. TASK 71-13-00-010-805) Subtask 12-36-29-010-091 E. Get access to the avionics compartment. (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the door of the AC/DC emergency power-center 740VU. (4) Put the adjustable access platform in position. 4. Procedure _________ Subtask 12-36-29-860-094 A. Preparation before the flushing of the Case-Drain line (Ref. Fig. 311/TASK 12-36-29-991-039) R R
CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE ON THE GROUND HYDRAULIC CART _______ IS SET TO A MINIMUM OF 7 BARS (101.53 PSI). CAUTION : BE CAREFUL WHEN YOU DISCONNECT THE RETURN LINE FROM THE _______ RESERVOIR. THE HYDRAULIC FLUID IN THE LINE WILL FLOW OUT.
EFF : 701-749, 12-36-29 SROS
Page 361 Oct 01/04
Hydraulic Connections Figure 311/TASK 12-36-29-991-039- 12 (SHEET 1) EFF : 701-749, 12-36-29 R SROS
Page 362 Apr 01/01
Hydraulic Connections Figure 311/TASK 12-36-29-991-039- 22 (SHEET 2) EFF : 701-749, 12-36-29 R SROS
Page 363 Apr 01/01
(1) Disconnect and remove the return line from the reservoir and from the filter (5011JM2). (2) Put a blanking plug on the reservoir. (3) Connect the return hose of the hydraulic power cart to the filter (5011JM2) with the hydraulic power cart/return line interface (98F12303000100) of the HYDRAULIC CONNECTORS (98F12303000000). (4) Attach the return hose of the hydraulic power cart to the aircraft structure with a strap. (5) Disconnect the case drain line from the engine pump. (6) Put a blanking plug to the case drain. (7) Connect the pressure hose of the hydraulic power cart to the case drain line with the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000). Subtask 12-36-29-170-070 B. Flushing of the Case-Drain Line (Ref. Fig. 312/TASK 12-36-29-991-021) (1) Operate the hydraulic power cart for 2mn at 20 bars. (2) Stop the hydraulic power cart. (3) Replace the hydraulic filters, case drain and LP: - the case drain filter 5013JM2 (Ref. TASK 29-11-43-600-809), - the LP filter 5011JM2 (Ref. TASK 29-12-44-600-801), - the HP filter 5111JM2 (Ref. TASK 29-12-45-600-801). Subtask 12-36-29-420-070 C. Connection of the Hydraulic Line (1) Remove the strap which attach the return hose of the hydraulic power cart to the aircraft structure. (2) Remove the blanking plug from the reservoir. (3) Remove the hydraulic power cart/return line interface (98F12303000100) of the HYDRAULIC CONNECTORS (98F12303000000) from the filter (5011JM2) and from the hydraulic power cart.
EFF : 701-749, 12-36-29 R SROS
Page 364 Apr 01/01
Flushing of the Case-Drain line of the Blue Hydraulic System Figure 312/TASK 12-36-29-991-021 EFF : 701-749, 12-36-29 R SROS
Page 365 Apr 01/01
(4) Connect the return line to the reservoir and to the filter (5011JM2). (5) Remove the blanking plug from the case drain. (6) Remove the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000) from the case drain line and from the hydraulic power cart. (7) Connect the case drain line to the engine pump. (8) TORQUE the case drain line to between 2.43 and 3.16 m.daN (17.92 and 23.30 lbf.ft). Subtask 12-36-29-865-094 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 4030EM1 9JC, 11JB, 12KS1, 13KS1 Subtask 12-36-29-611-070 E. Fill the Blue hydraulic reservoir (Ref. TASK 12-12-29-611-803) or (Ref. TASK 12-12-29-611-804). Subtask 12-36-29-863-070 F. Pressurize the Blue hydraulic reservoir (Ref. TASK 29-14-00-614-804). Subtask 12-36-29-410-090 G. Close the fan cowl doors. FOR 4030EM1 - close the door 416AR (Ref. TASK 71-13-00-410-805). Subtask 12-36-29-281-070 H. Sampling (1) Perform a fluid sampling for particular contamination (Ref. TASK 1232-29-281-801). (2) Perform in daily check, the check of the clogging indicators, of the case drain filter 5013JM2, HP filter 5111JM2, LP filter 5011JM2. Do this operation again until the clogging indicator stay in.
R EFF : 701-749, 12-36-29 SROS
Page 366 Apr 01/01
5. Close-up ________ Subtask 12-36-29-410-091 A. Close Access (1) Close the door of the AC/DC emergency power-center 740VU. (2) Close the access door 811. (3) Remove the access platform(s). (4) Close the MLG doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-942-070 B. Remove the safety devices. (1) Remove the warning notice(s). Subtask 12-36-29-862-070 C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 701-749, 12-36-29 SROS
Page 367 Apr 01/01
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, TASK 12-36-29-170-804 Flushing of the HP line of the Blue Hydraulic System WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job To flush the Blue hydraulic system after a failure of the engine pump. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No
specific specific specific specific specific specific specific specific
No specific
adjustable access platform blanking plugs circuit breaker(s) safety clip(s) hydraulic power cart warning notice access platform 2.5 m (8 ft. 2 in.) container 5 l (1.3208 USgal) Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft) Torque Wrench : range 1.00 to 10.00 m.daN (8.00 to 75.00 lbf.ft)
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 368 Jul 01/05
------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific 98F12303000000
Torque Wrench : range 2.00 to 20.00 m.daN (15.00 to 150.00 lbf.ft) 1 HYDRAULIC CONNECTORS
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-803 12-12-29-611-804 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-12-45-600-801 29-14-00-614-802 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 78-30-00-040-804 78-30-00-440-804 78-31-11-000-801 12-36-29-991-041 12-36-29-991-016 FOR FIN 4030EM1 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801 78-30-00-410-801
Fill the Blue Hydraulic Reservoir with a Hydraulic Service Cart Fill the Blue Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Servicing of the Blue HP Filter (5111JM2) Depressurization of the Blue Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Deactivation of the Thrust Reverser for Maintenance Reactivation of the Thrust Reverser after Maintenance Removal of the Hydraulic Filter Element Fig. 313 Fig. 314 Opening of (5120EA) Closing of (5120EA) Opening of 4130KS) Closing of 4130KS)
the Aft Fan Cowl Doors (5110EA) and the Aft Fan Cowl Doors (5110EA) and the Thrust Reverser Cowl Doors (4120KS to the Thrust Reverser Cowl Doors (4120KS to
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 369 Jul 01/05
3. __________ Job Set-up Subtask 12-36-29-860-065 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Make sure that the Blue hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-804). (3) Depressurize the reservoir of the Blue hydraulic system (Ref. TASK 29-14-00-614-802). Subtask 12-36-29-941-065 B. Safety Precautions (1) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure. (2) On the panel 225VU, make sure that the APU BLEED pushbutton switch is released (ON legend off) and install a warning notice to tell persons not to use it. (3) Put a warning notice in position to tell persons not to pressurize the hydraulic system: - on the HYD/FUEL control panel 245VU in the cockpit, - on the Blue hydraulic system, access door 196BB. (4) On the panel 125VU: - make sure that the ENG MASTER switches for the two engines are in the OFF position, - put a warning notice to tell persons not to supply power to the EEC. (5) On the panel 285VU: - make sure that the ON legend of the related ENG FADEC GND PWR pushbutton switch is off, - put a warning notice to tell persons not to supply power to the FADEC system. (6) Put a container below the Blue hydraulic engine pump and below the case drain filter.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 370 Jul 01/05
Subtask 12-36-29-865-082 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU HYD PUMP B ENG 1 11JB U08 721VU HYD PUMP B CTL 9JC X12 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 Subtask 12-36-29-010-081 D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Open the fan cowl doors: FOR 4030EM1 Open the door 415BL (Ref. TASK 71-13-00-010-802) Subtask 12-36-29-040-065 E. Make the thrust reverser unserviceable for maintenance (Ref. TASK 78-3000-040-804). Subtask 12-36-29-010-135 F. Get Access (1) Open the right thrust-reverser door: FOR 4030EM1 Open the door 417AL (Ref. TASK 78-30-00-010-801). Subtask 12-36-29-010-082 G. Get access to the avionics compartment. (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the door of the AC/DC emergency power-center 740VU. (4) Put the adjustable access platform in position.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 371 Jul 01/05
4. Procedure _________ Subtask 12-36-29-860-089 A. Preparation before the flushing of the HP line (Ref. Fig. 313/TASK 12-36-29-991-041) CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE ON THE GROUND HYDRAULIC CART _______ IS SET TO A MINIMUM OF 7 BARS (101.53 PSI). (1) Disconnect the case drain line from the engine pump. (2) Disconnect the pressure line from the engine pump. (3) Disconnect the case drain line from the case drain filter. (4) Connect the pressure line and the case drain line together with the engine pump case drain/engine pump pressure connection (98F12303000104) of the HYDRAULIC CONNECTORS (98F12303000000). (5) Connect the pressure hose of the hydraulic power cart to the case drain line with the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000). (6) Connect the return hose of the hydraulic power cart to the interface (98F12303000106) of the HYDRAULIC CONNECTORS (98F12303000000). (7) Connect the free end of the interface to the delivery ground connector 5131JM2. (8) Put blanking plugs on the disconnected line ends. (9) Close the leak measurement valve. - on the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/BLUE pushbutton switch (the OFF legend comes on). Subtask 12-36-29-170-065 B. Flushing of the HP Line (Ref. Fig. 314/TASK 12-36-29-991-016) (1) Operate the hydraulic power cart for 2mn at 20 bars. (2) Stop the hydraulic power cart.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 372 Jul 01/05
Hydraulic Connections Figure 313/TASK 12-36-29-991-041 R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 373 Jul 01/05
Flushing of the HP Line of the Blue Hydraulic System Figure 314/TASK 12-36-29-991-016 R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 374 Jul 01/05
(3) Open the leak measurement valve: - on the HYD section of the maintenance panel 285VU, push the LEAK MEASUREMENT VALVES/BLUE pushbutton switch (the OFF legend goes off). (4) Replace the hydraulic filters, HP and HCU: - replace the HP filter 5111JM2 (Ref. TASK 29-12-45-600-801), - replace the HCU filter 5000EG2 (Ref. TASK 78-31-11-000-801). Subtask 12-36-29-420-065 C. Connection of the Hydraulic Line (1) Remove the blanking plugs from the disconnected line ends. (2) Remove the engine pump case drain/engine pump pressure connection (98F12303000104) of the HYDRAULIC CONNECTORS (98F12303000000) from the pressure line and from the case drain line. (3) Remove the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000) from the case drain line and from the hydraulic power cart. (4) Connect the pressure line to the engine pump. (5) TORQUE the pressure line to between 12.88 and 14.24 m.daN (94.98 and 105.01 lbf.ft). (6) Connect the case drain line to the engine pump. (7) TORQUE the case drain line to between 2.43 and 3.16 m.daN (17.92 and 23.30 lbf.ft). (8) Connect the pump case drain hose to the case drain. (9) TORQUE the case drain hose to between 5.31 and 6.21 m.daN (39.15 and 45.79 lbf.ft). Subtask 12-36-29-865-083 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 4030EM1 9JC, 11JB, 12KS1, 13KS1
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 375 Jul 01/05
Subtask 12-36-29-611-065 E. Fill the Blue hydraulic reservoir (Ref. TASK 12-12-29-611-803) or (Ref. TASK 12-12-29-611-804). Subtask 12-36-29-863-065 F. Pressurize the Blue hydraulic reservoir (Ref. TASK 29-14-00-614-804). Subtask 12-36-29-410-134 G. Close the right thrust reverser : - FOR 4030EM1 close the door 417AL (Ref. TASK 78-30-00-410-801) Subtask 12-36-29-440-065 H. Make sure that the thrust reverser is serviceable after maintenance (Ref. TASK 78-30-00-440-804). Subtask 12-36-29-410-080 J. Close the fan cowl doors. FOR 4030EM1 - close the door 415BL (Ref. TASK 71-13-00-410-802) Subtask 12-36-29-281-065 K. Sampling (1) Perform a fluid sampling for particular contamination (Ref. TASK 1232-29-281-801). (2) Perform in daily check, the check of the clogging indicators of the HP filter 5111JM2 and the HCU filter 5000EG2. Do this operation again until the clogging indicator stay in. 5. Close-up ________ Subtask 12-36-29-410-081 A. Close Access (1) Close the door of the AC/DC emergency power-center 740VU. (2) Close the access door 811.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 376 Jul 01/05
(3) Remove the access platform(s). (4) Close the MLG doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-942-065 B. Remove the safety devices. (1) Remove the warning notice(s). Subtask 12-36-29-862-065 C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 377 Jul 01/05
**ON A/C 701-749, TASK 12-36-29-170-804-A Flushing of the HP line of the Blue Hydraulic System WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job To flush the Blue hydraulic system after a failure of the engine pump. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No
specific specific specific specific specific specific specific specific
No specific 98F12303000000
adjustable access platform blanking plugs circuit breaker(s) safety clip(s) hydraulic power cart warning notice access platform 2.5 m (8 ft. 2 in.) container 5 l (1.3208 USgal) Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft) Torque Wrench : range 2.00 to 20.00 m.daN (15.00 to 150.00 lbf.ft) 1 HYDRAULIC CONNECTORS
EFF : 701-749, 12-36-29 R SROS
Page 378 Apr 01/01
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-803 12-12-29-611-804 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-12-45-600-801 29-14-00-614-802 R 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 78-31-41-000-803 12-36-29-991-042 12-36-29-991-022 FOR FIN 4030EM1 71-13-00-010-805 71-13-00-410-805
Fill the Blue Hydraulic Reservoir with a Hydraulic Service Cart Fill the Blue Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Servicing of the Blue HP Filter (5111JM2) Depressurization of the Blue Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Removal of the Isolation Control Unit (4117KS) Fig. 315 Fig. 316 Open the Fan Cowl Doors Close the Fan Cowl Doors
3. __________ Job Set-up Subtask 12-36-29-860-071 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Make sure that the Blue hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-804). (3) Depressurize the reservoir of the Blue hydraulic system (Ref. TASK 29-14-00-614-802).
EFF : 701-749, 12-36-29 SROS
Page 379 Apr 01/05
Subtask 12-36-29-941-071 B. Safety Precautions (1) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure. (2) On the panel 225VU, make sure that the APU BLEED pushbutton switch is released (ON legend off) and install a warning notice to tell persons not to use it. (3) Put a warning notice in position to tell persons not to pressurize the hydraulic system: - on the HYD/FUEL control panel 245VU in the cockpit, - on the Blue hydraulic system, access door 196BB. (4) On the panel 125VU: - make sure that the ENG MASTER switches for the two engines are in the OFF position, - put a warning notice to tell persons not to supply power to the ECU. (5) On the panel 285VU: - make sure that the ON legend of the related ENG FADEC GND PWR pushbutton switch is off, - put a warning notice to tell persons not to supply power to the FADEC system. (6) Put a container below the Blue hydraulic engine pump and below the case drain filter. Subtask 12-36-29-865-095 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU HYD PUMP B ENG 1 11JB U08 721VU HYD PUMP B CTL 9JC X12 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73
EFF : 701-749, 12-36-29 R SROS
Page 380 Apr 01/01
Subtask 12-36-29-010-092 D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Open the fan cowl doors: FOR 4030EM1 Open the door 416AR (Ref. TASK 71-13-00-010-805) Subtask 12-36-29-010-093 E. Get access to the avionics compartment. (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the door of the AC/DC emergency power-center 740VU. (4) Put the adjustable access platform in position. 4. Procedure _________ Subtask 12-36-29-860-095 A. Preparation before the flushing of the HP line (Ref. Fig. 315/TASK 12-36-29-991-042) R R
CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE ON THE GROUND HYDRAULIC CART _______ IS SET TO A MINIMUM OF 7 BARS (101.53 PSI). (1) Disconnect the case drain line from the engine pump. (2) Disconnect the pressure line from the engine pump. (3) Disconnect the case drain line from the case drain filter. (4) Connect the pressure line and the case drain line together with the engine pump case drain/engine pump pressure connection (98F12303000104) of the HYDRAULIC CONNECTORS (98F12303000000). (5) Connect the pressure hose of the hydraulic power cart to the case drain line with the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000).
EFF : 701-749, 12-36-29 SROS
Page 381 Oct 01/04
Hydraulic Connections Figure 315/TASK 12-36-29-991-042 EFF : 701-749, 12-36-29 R SROS
Page 382 Apr 01/01
(6) Connect the return hose of the hydraulic power cart to the interface (98F12303000106) of the HYDRAULIC CONNECTORS (98F12303000000). (7) Connect the free end of the interface to the delivery ground connector 5131JM2. (8) Put blanking plugs on the disconnected line ends. (9) Close the leak measurement valve. - on the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/BLUE pushbutton switch (the OFF legend comes on). Subtask 12-36-29-170-071 B. Flushing of the HP Line (Ref. Fig. 316/TASK 12-36-29-991-022) (1) Operate the hydraulic power cart for 2mn at 20 bars. (2) Stop the hydraulic power cart. (3) Open the leak measurement valve: - on the HYD section of the maintenance panel 285VU, push the LEAK MEASUREMENT VALVES/BLUE pushbutton switch (the OFF legend goes off). (4) Replace the hydraulic filters, HP and filter element: - replace the HP filter 5111JM2 (Ref. TASK 29-12-45-600-801), - remove the filter element located on the Isolation Control Unit 4117KS (Ref. TASK 78-31-41-000-803). Subtask 12-36-29-420-071 C. Connection of the Hydraulic Line (1) Remove the blanking plugs from the disconnected line ends. (2) Remove the engine pump case drain/engine pump pressure connection (98F12303000104) of the HYDRAULIC CONNECTORS (98F12303000000) from the pressure line and from the case drain line. (3) Remove the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000) from the case drain line and from the hydraulic power cart. (4) Connect the pressure line to the engine pump.
EFF : 701-749, 12-36-29 R SROS
Page 383 Apr 01/01
Flushing of the HP Line of the Blue Hydraulic System Figure 316/TASK 12-36-29-991-022 EFF : 701-749, 12-36-29 R SROS
Page 384 Apr 01/01
(5) TORQUE the pressure line to between 12.88 and 14.24 m.daN (94.98 and 105.01 lbf.ft). (6) Connect the case drain line to the engine pump. (7) Connect the pump case drain hose to the case drain. (8) TORQUE the case drain line to between 2.43 and 3.16 m.daN (17.92 and 23.30 lbf.ft). Subtask 12-36-29-865-096 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 4030EM1 9JC, 11JB, 12KS1, 13KS1 Subtask 12-36-29-611-071 E. Fill the Blue hydraulic reservoir (Ref. TASK 12-12-29-611-803) or (Ref. TASK 12-12-29-611-804). Subtask 12-36-29-863-071 F. Pressurize the Blue hydraulic reservoir (Ref. TASK 29-14-00-614-804). Subtask 12-36-29-410-092 G. Close the fan cowl doors. FOR 4030EM1 - close the door 416AR (Ref. TASK 71-13-00-410-805) Subtask 12-36-29-281-071 H. Sampling (1) Perform a fluid sampling for particular contamination (Ref. TASK 1232-29-281-801). (2) Perform in daily check, the check of the clogging indicators of the HP filter 5111JM2 and the filter element located on the Isolation Control Unit 4117KS. Do this operation again until the clogging indicator stay in.
R EFF : 701-749, 12-36-29 SROS
Page 385 Apr 01/01
5. Close-up ________ Subtask 12-36-29-410-093 A. Close Access (1) Close the door of the AC/DC emergency power-center 740VU. (2) Close the access door 811. (3) Remove the access platform(s). (4) Close the MLG doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-942-071 B. Remove the safety devices. (1) Remove the warning notice(s). Subtask 12-36-29-862-071 C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 701-749, 12-36-29 SROS
Page 386 Apr 01/01
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, TASK 12-36-29-170-805 Flushing of the Case-Drain line of the Yellow Hydraulic System WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job To flush the Yellow hydraulic system after a failure of the engine pump. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No No
specific specific specific specific specific specific specific specific specific
98F12303000000
adjustable access platform blanking plug circuit breaker(s) safety clip(s) hydraulic power cart strap warning notice access platform 2.5 m (8 ft. 2 in.) container 5 l (1.3208 USgal) Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft) 1 HYDRAULIC CONNECTORS
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 387 Jul 01/05
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-805 12-12-29-611-806 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-10-00-611-803 29-11-43-600-804 29-13-44-600-801 29-14-00-614-803 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 78-30-00-040-804 78-30-00-440-804 12-36-29-991-044 12-36-29-991-017 FOR FIN 4030EM2 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801 78-30-00-410-801
Fill the Yellow Hydraulic Reservoir with a Hydraulic Service Cart Fill the Yellow Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Drainage of the Yellow Hydraulic Reservoir Servicing of the (Aft) Engine-Pump Case-Drain Filter Element 5013JM2 Servicing of the Yellow Reservoir LP-Filter (5011JM3) Depressurization of the Yellow Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Deactivation of the Thrust Reverser for Maintenance Reactivation of the Thrust Reverser after Maintenance Fig. 317 Fig. 318 Opening of (5120EA) Closing of (5120EA) Opening of 4130KS) Closing of 4130KS)
the Aft Fan Cowl Doors (5110EA) and the Aft Fan Cowl Doors (5110EA) and the Thrust Reverser Cowl Doors (4120KS to the Thrust Reverser Cowl Doors (4120KS to
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 388 Jul 01/05
3. __________ Job Set-up Subtask 12-36-29-860-066 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Make sure that the Yellow hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-804). (3) Depressurize the reservoir of the Yellow hydraulic system (Ref. TASK 29-14-00-614-803). (4) Drain the Yellow hydraulic reservoir (Ref. TASK 29-10-00-611-803). Subtask 12-36-29-941-066 B. Safety Precautions (1) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure. (2) On the panel 225VU, make sure that the APU BLEED pushbutton switch is released (ON legend off) and install a warning notice to tell persons not to use it. (3) Put a warning notice in position to tell persons not to pressurize the hydraulic system: - on the HYD/FUEL control panel 245VU in the cockpit, - on the Yellow hydraulic system, access door 196BB. (4) On the panel 125VU: - make sure that the ENG MASTER switches for the two engines are in the OFF position, - put a warning notice to tell persons not to supply power to the EEC. (5) On the panel 285VU: - make sure that the ON legend of the related ENG FADEC GND PWR pushbutton switch is off, - put a warning notice to tell persons not to supply power to the FADEC system.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 389 Jul 01/05
(6) Put a container below the Yellow hydraulic engine pump and below the case drain filter. Subtask 12-36-29-865-084 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 722VU HYD PUMP Y CTL 9JJ R36 722VU HYD PUMP Y ENG 2 12JY T46 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-36-29-010-083 D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Open the fan cowl doors: FOR 4030EM2 Open the door 425BL (Ref. TASK 71-13-00-010-802) Subtask 12-36-29-040-066 E. Make the thrust reverser unserviceable for maintenance (Ref. TASK 78-3000-040-804). Subtask 12-36-29-010-136 F. Get Access (1) Open the right thrust-reverser door: FOR 4030EM2 Open the door 427AL (Ref. TASK 78-30-00-010-801). Subtask 12-36-29-010-084 G. Get access to the avionics compartment. (1) Put the access platform in position at the access door 811. (2) Open the access door 811.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 390 Jul 01/05
(3) Open the door of the AC/DC emergency power-center 740VU. (4) Put the adjustable access platform in position. 4. Procedure _________ Subtask 12-36-29-860-090 A. Preparation before the flushing of the Case-Drain line (Ref. Fig. 317/TASK 12-36-29-991-044) CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE ON THE GROUND HYDRAULIC CART _______ IS SET TO A MINIMUM OF 7 BARS (101.53 PSI). CAUTION : BE CAREFUL WHEN YOU DISCONNECT THE RETURN LINE FROM THE _______ RESERVOIR. THE HYDRAULIC FLUID IN THE LINE WILL FLOW OUT. (1) Disconnect and remove the return line from the reservoir and from the filter (5011JM3). (2) Put a blanking plug on the reservoir. (3) Connect the return hose of the hydraulic power cart to the filter (5011JM3) with the hydraulic power cart/return line interface (98F12303000100) of the HYDRAULIC CONNECTORS (98F12303000000). (4) Attach the return hose of the hydraulic power cart to the aircraft structure with a strap. (5) Disconnect the case drain line from the engine pump. (6) Put a blanking plug to the case drain. (7) Connect the pressure hose of the hydraulic power cart to the case drain line with the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000). Subtask 12-36-29-170-066 B. Flushing of the Case-Drain Line (Ref. Fig. 318/TASK 12-36-29-991-017) (1) Operate the hydraulic power cart for 2mn at 20 bars. (2) Stop the hydraulic power cart.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 391 Jul 01/05
Hydraulic Connections Figure 317/TASK 12-36-29-991-044- 12 (SHEET 1) R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 392 Jul 01/05
Hydraulic Connections Figure 317/TASK 12-36-29-991-044- 22 (SHEET 2) R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 393 Jul 01/05
Flushing of the Case-Drain Line of the Yellow Hydraulic System Figure 318/TASK 12-36-29-991-017 R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 394 Jul 01/05
(3) Replace the hydraulic filters, case drain and LP: - the case drain filter 5013JM2 (Ref. TASK 29-11-43-600-804), - the LP filter 5011JM3 (Ref. TASK 29-13-44-600-801). Subtask 12-36-29-420-066 C. Connection of the Hydraulic Line (1) Remove the strap which attach the return hose of the hydraulic power cart to the aircraft structure. (2) Remove the blanking plug from the reservoir. (3) Remove the hydraulic power cart/return line interface (98F12303000100) of the HYDRAULIC CONNECTORS (98F12303000000) from the filter (5011JM3) and from the hydraulic power cart. (4) Connect the return line to the reservoir and to the filter (5011JM3). (5) Remove the blanking plug from the case drain. (6) Remove the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000) from the case drain line and from the hydraulic power cart. (7) Connect the case drain line to the engine pump. (8) TORQUE the case drain line to between 2.43 and 3.16 m.daN (17.92 and 23.30 lbf.ft). Subtask 12-36-29-865-085 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 4030EM2 9JJ, 12JY, 12KS2, 13KS2 Subtask 12-36-29-611-066 E. Fill the Yellow hydraulic reservoir (Ref. TASK 12-12-29-611-805) or (Ref. TASK 12-12-29-611-806). Subtask 12-36-29-863-066 F. Pressurize the Yellow hydraulic reservoir (Ref. TASK 29-14-00-614-804).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 395 Jul 01/05
Subtask 12-36-29-410-135 G. Close the right thrust reverser : - FOR 4030EM2 close the door 427AL (Ref. TASK 78-30-00-410-801) Subtask 12-36-29-440-066 H. Make sure that the thrust reverser is serviceable after maintenance (Ref. TASK 78-30-00-440-804). Subtask 12-36-29-410-082 J. Close the fan cowl doors. FOR 4030EM2 - close the door 425BL (Ref. TASK 71-13-00-410-802). Subtask 12-36-29-281-066 K. Sampling (1) Perform a fluid sampling for particular contamination (Ref. TASK 1232-29-281-801). (2) Perform in daily check, the check of the clogging indicators, of the case drain filter 5013JM2, HP filter 5111JM3, LP filter 5011JM3. Do this operation again until the clogging indicator stay in. 5. Close-up ________ Subtask 12-36-29-410-083 A. Close Access (1) Close the door of the AC/DC emergency power-center 740VU. (2) Close the access door 811. (3) Remove the access platform(s). (4) Close the MLG doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-942-066 B. Remove the safety devices. (1) Remove the warning notice(s).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 396 Jul 01/05
Subtask 12-36-29-862-066 C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 397 Jul 01/05
**ON A/C 701-749, TASK 12-36-29-170-805-A Flushing of the Case-Drain line of the Yellow Hydraulic System WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job To flush the Yellow hydraulic system after a failure of the engine pump. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No No
specific specific specific specific specific specific specific specific specific
98F12303000000
adjustable access platform blanking plug circuit breaker(s) safety clip(s) hydraulic power cart strap warning notice access platform 2.5 m (8 ft. 2 in.) container 5 l (1.3208 USgal) Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft) 1 HYDRAULIC CONNECTORS
EFF : 701-749, 12-36-29 R SROS
Page 398 Apr 01/01
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-805 12-12-29-611-806 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-10-00-611-803 29-11-43-600-809 29-13-44-600-801 29-14-00-614-803 R 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 12-36-29-991-045 12-36-29-991-023 FOR FIN 4030EM2 71-13-00-010-805 71-13-00-410-805
Fill the Yellow Hydraulic Reservoir with a Hydraulic Service Cart Fill the Yellow Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Drainage of the Yellow Hydraulic Reservoir Servicing of the Engine Pump Case Drain Filter (5013JM2) Servicing of the Yellow Reservoir LP-Filter (5011JM3) Depressurization of the Yellow Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Fig. 319 Fig. 320 Open the Fan Cowl Doors Close the Fan Cowl Doors
3. __________ Job Set-up Subtask 12-36-29-860-072 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Make sure that the Yellow hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-804). (3) Depressurize the reservoir of the Yellow hydraulic system (Ref. TASK 29-14-00-614-803).
EFF : 701-749, 12-36-29 SROS
Page 399 Apr 01/05
(4) Drain the Yellow hydraulic reservoir (Ref. TASK 29-10-00-611-803). Subtask 12-36-29-941-072 B. Safety Precautions (1) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure. (2) On the panel 225VU, make sure that the APU BLEED pushbutton switch is released (ON legend off) and install a warning notice to tell persons not to use it. (3) Put a warning notice in position to tell persons not to pressurize the hydraulic system: - on the HYD/FUEL control panel 245VU in the cockpit, - on the Yellow hydraulic system, access door 196BB. (4) On the panel 125VU: - make sure that the ENG MASTER switches for the two engines are in the OFF position, - put a warning notice to tell persons not to supply power to the ECU. (5) On the panel 285VU: - make sure that the ON legend of the related ENG FADEC GND PWR pushbutton switch is off, - put a warning notice to tell persons not to supply power to the FADEC system. (6) Put a container below the Yellow hydraulic engine pump and below the case drain filter. Subtask 12-36-29-865-097 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 722VU HYD PUMP Y CTL 9JJ R36 722VU HYD PUMP Y ENG 2 12JY T46 742VU FADEC A ENG 2 12KS2 Q74
EFF : 701-749, 12-36-29 R SROS
Page A300 Apr 01/01
Subtask 12-36-29-010-094 D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Open the fan cowl doors: FOR 4030EM2 Open the door 426AR (Ref. TASK 71-13-00-010-805) Subtask 12-36-29-010-095 E. Get access to the avionics compartment. (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the door of the AC/DC emergency power-center 740VU. (4) Put the adjustable access platform in position. 4. Procedure _________ Subtask 12-36-29-860-096 A. Preparation before the flushing of the Case-Drain line (Ref. Fig. 319/TASK 12-36-29-991-045) R R
CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE ON THE GROUND HYDRAULIC CART _______ IS SET TO A MINIMUM OF 7 BARS (101.53 PSI). CAUTION : BE CAREFUL WHEN YOU DISCONNECT THE RETURN LINE FROM THE _______ RESERVOIR. THE HYDRAULIC FLUID IN THE LINE WILL FLOW OUT. (1) Disconnect and remove the return line from the reservoir and from the filter (5011JM3). (2) Put a blanking plug on the reservoir. (3) Connect the return hose of the hydraulic power cart to the filter (5011JM3) with the hydraulic power cart/return line interface (98F12303000100) of the HYDRAULIC CONNECTORS (98F12303000000). (4) Attach the return hose of the hydraulic power cart to the aircraft structure with a strap.
EFF : 701-749, 12-36-29 SROS
Page A301 Oct 01/04
Hydraulic Connections Figure 319/TASK 12-36-29-991-045- 12 (SHEET 1) EFF : 701-749, 12-36-29 R SROS
Page A302 Apr 01/01
Hydraulic Connections Figure 319/TASK 12-36-29-991-045- 22 (SHEET 2) EFF : 701-749, 12-36-29 R SROS
Page A303 Apr 01/01
(5) Disconnect the case drain line from the engine pump. (6) Put a blanking plug to the case drain. (7) Connect the pressure hose of the hydraulic power cart to the case drain line with the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000). Subtask 12-36-29-170-072 B. Flushing of the Case-Drain Line (Ref. Fig. 320/TASK 12-36-29-991-023) (1) Operate the hydraulic power cart for 2mn at 20 bars. (2) Stop the hydraulic power cart. (3) Replace the hydraulic filters, case drain and LP: - the case drain filter 5013JM2 (Ref. TASK 29-11-43-600-809), - the LP filter 5011JM3 (Ref. TASK 29-13-44-600-801). Subtask 12-36-29-420-072 C. Connection of the Hydraulic Line (1) Remove the strap which attach the return hose of the hydraulic power cart to the aircraft structure. (2) Remove the blanking plug from the reservoir. (3) Remove the hydraulic power cart/return line interface (98F12303000100) of the HYDRAULIC CONNECTORS (98F12303000000) from the filter (5011JM3) and from the hydraulic power cart. (4) Connect the return line to the reservoir and to the filter (5011JM3). (5) Remove the blanking plug from the case drain. (6) Remove the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000) from the case drain line and from the hydraulic power cart. (7) Connect the case drain line to the engine pump. (8) TORQUE the case drain line to between 2.43 and 3.16 m.daN (17.92 and 23.30 lbf.ft).
EFF : 701-749, 12-36-29 R SROS
Page A304 Apr 01/01
Flushing of the Case-Drain line of the Yellow Hydraulic System Figure 320/TASK 12-36-29-991-023 EFF : 701-749, 12-36-29 R SROS
Page A305 Apr 01/01
Subtask 12-36-29-865-098 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 4030EM2 9JJ, 12JY, 12KS2, 13KS2 Subtask 12-36-29-611-072 E. Fill the Yellow hydraulic reservoir (Ref. TASK 12-12-29-611-805) or (Ref. TASK 12-12-29-611-806). Subtask 12-36-29-863-072 F. Pressurize the Yellow hydraulic reservoir (Ref. TASK 29-14-00-614-804). Subtask 12-36-29-410-094 G. Close the fan cowl doors. FOR 4030EM2 - close the door 426AR (Ref. TASK 71-13-00-410-805). Subtask 12-36-29-281-072 H. Sampling (1) Perform a fluid sampling for particular contamination (Ref. TASK 1232-29-281-801). (2) Perform in daily check, the check of the clogging indicators, of the case drain filter 5013JM2, HP filter 5111JM3, LP filter 5011JM3. Do this operation again until the clogging indicator stay in. 5. Close-up ________ Subtask 12-36-29-410-095 A. Close Access (1) Close the door of the AC/DC emergency power-center 740VU. (2) Close the access door 811. (3) Remove the access platform(s). (4) Close the MLG doors (Ref. TASK 32-12-00-410-801).
R EFF : 701-749, 12-36-29 SROS
Page A306 Apr 01/01
Subtask 12-36-29-942-072 B. Remove the safety devices. (1) Remove the warning notice(s). Subtask 12-36-29-862-072 C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 701-749, 12-36-29 SROS
Page A307 Apr 01/01
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, TASK 12-36-29-170-806 Flushing of the HP line of the Yellow Hydraulic System WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job To flush the Yellow hydraulic system after a failure of the engine pump. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No
specific specific specific specific specific specific specific specific
No specific
adjustable access platform blanking plugs circuit breaker(s) safety clip(s) hydraulic power cart warning notice access platform 2.5 m (8 ft. 2 in.) container 5 l (1.3208 USgal) Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft) Torque Wrench : range 1.00 to 10.00 m.daN (8.00 to 75.00 lbf.ft)
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A308 Jul 01/05
------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific 98F12303000000
Torque Wrench : range 2.00 to 20.00 m.daN (15.00 to 150.00 lbf.ft) 1 HYDRAULIC CONNECTORS
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-805 12-12-29-611-806 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-13-45-600-801 29-14-00-614-803 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 78-30-00-040-804 78-30-00-440-804 78-31-11-000-801 12-36-29-991-047 12-36-29-991-018 FOR FIN 4030EM2 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801 78-30-00-410-801
Fill the Yellow Hydraulic Reservoir with a Hydraulic Service Cart Fill the Yellow Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Servicing of the Yellow HP Filter (5111JM3) Depressurization of the Yellow Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Deactivation of the Thrust Reverser for Maintenance Reactivation of the Thrust Reverser after Maintenance Removal of the Hydraulic Filter Element Fig. 321 Fig. 322 Opening of (5120EA) Closing of (5120EA) Opening of 4130KS) Closing of 4130KS)
the Aft Fan Cowl Doors (5110EA) and the Aft Fan Cowl Doors (5110EA) and the Thrust Reverser Cowl Doors (4120KS to the Thrust Reverser Cowl Doors (4120KS to
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A309 Jul 01/05
3. __________ Job Set-up Subtask 12-36-29-860-067 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Make sure that the Yellow hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-804). (3) Depressurize the reservoir of the Yellow hydraulic system (Ref. TASK 29-14-00-614-803). Subtask 12-36-29-941-067 B. Safety Precautions (1) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure. (2) On the panel 225VU, make sure that the APU BLEED pushbutton switch is released (ON legend off) and install a warning notice to tell persons not to use it. (3) Put a warning notice in position to tell persons not to pressurize the hydraulic system: - on the HYD/FUEL control panel 245VU in the cockpit, - on the Yellow hydraulic system, access door 197BB. (4) On the panel 125VU: - make sure that the ENG MASTER switches for the two engines are in the OFF position, - put a warning notice to tell persons not to supply power to the EEC. (5) On the panel 285VU: - make sure that the ON legend of the related ENG FADEC GND PWR pushbutton switch is off, - put a warning notice to tell persons not to supply power to the FADEC system. (6) Put a container below the Yellow hydraulic engine pump and below the case drain filter.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A310 Jul 01/05
Subtask 12-36-29-865-086 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 722VU HYD PUMP Y CTL 9JJ R36 722VU HYD PUMP Y ENG 2 12JY T46 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-36-29-010-085 D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Open the fan cowl doors: FOR 4030EM2 Open the door 425BL (Ref. TASK 71-13-00-010-802) Subtask 12-36-29-040-067 E. Make the thrust reverser unserviceable for maintenance (Ref. TASK 78-3000-040-804). Subtask 12-36-29-010-137 F. Get Access (1) Open the right thrust-reverser door: FOR 4030EM2 Open the door 427AL (Ref. TASK 78-30-00-010-801). Subtask 12-36-29-010-086 G. Get access to the avionics compartment. (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the door of the AC/DC emergency power-center 740VU. (4) Put the adjustable access platform in position.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A311 Jul 01/05
4. Procedure _________ Subtask 12-36-29-860-091 A. Preparation before the flushing of the HP line (Ref. Fig. 321/TASK 12-36-29-991-047) CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE ON THE GROUND HYDRAULIC CART _______ IS SET TO A MINIMUM OF 7 BARS (101.53 PSI). (1) Disconnect the case drain line from the engine pump. (2) Disconnect the pressure line from the engine pump. (3) Disconnect the case drain line from the case drain filter. (4) Connect the pressure line and the case drain line together with the engine pump case drain/engine pump pressure connection (98F12303000104) of the HYDRAULIC CONNECTORS (98F12303000000). (5) Connect the pressure hose of the hydraulic power cart to the case drain line with the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000). (6) Connect the return hose of the hydraulic power cart to the interface (98F12303000106) of the HYDRAULIC CONNECTORS (98F12303000000). (7) Connect the free end of the interface to the delivery ground connector 5131JM2. (8) Put blanking plugs on the disconnected line ends. (9) Close the leak measurement valve. - on the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/YELLOW pushbutton switch (the OFF legend comes on). Subtask 12-36-29-170-067 B. Flushing of the HP Line (Ref. Fig. 322/TASK 12-36-29-991-018) (1) Operate the hydraulic power cart for 2mn at 20 bars. (2) Stop the hydraulic power cart.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A312 Jul 01/05
Hydraulic Connections Figure 321/TASK 12-36-29-991-047 R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A313 Jul 01/05
Flushing of the HP Line of the Yellow Hydraulic System Figure 322/TASK 12-36-29-991-018 R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A314 Jul 01/05
(3) Open the leak measurement valve: - on the HYD section of the maintenance panel 285VU, push the LEAK MEASUREMENT VALVES/YELLOW pushbutton switch (the OFF legend goes off). (4) Replace the hydraulic filters, HP and HCU: - replace the HP filter 5111JM3 (Ref. TASK 29-13-45-600-801), - replace the HCU filter 5000EG2 (Ref. TASK 78-31-11-000-801). Subtask 12-36-29-420-067 C. Connection of the Hydraulic Line (1) Remove the blanking plugs from the disconnected line ends. (2) Remove the engine pump case drain/engine pump pressure connection (98F12303000104) of the HYDRAULIC CONNECTORS (98F12303000000) from the pressure line and from the case drain line. (3) Remove the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000) from the case drain line and from the hydraulic power cart. (4) Connect the pressure line to the engine pump. (5) TORQUE the pressure line to between 12.88 and 14.24 m.daN (94.98 and 105.01 lbf.ft). (6) Connect the case drain line to the engine pump. (7) TORQUE the case drain line to between 2.43 and 3.16 m.daN (17.92 and 23.30 lbf.ft). (8) Connect the pump case drain hose to the case drain. (9) TORQUE the case drain hose to between 5.31 and 6.21 m.daN (39.15 and 45.79 lbf.ft). Subtask 12-36-29-865-087 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 4030EM2 9JJ, 12JY, 12KS2, 13KS2
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A315 Jul 01/05
Subtask 12-36-29-611-067 E. Fill the Yellow hydraulic reservoir (Ref. TASK 12-12-29-611-805) or (Ref. TASK 12-12-29-611-806). Subtask 12-36-29-863-067 F. Pressurize the Yellow hydraulic reservoir (Ref. TASK 29-14-00-614-804). Subtask 12-36-29-410-136 G. Close the right thrust reverser : - FOR 4030EM2 close the door 427AL (Ref. TASK 78-30-00-410-801) Subtask 12-36-29-440-067 H. Make sure that the thrust reverser is serviceable after maintenance (Ref. TASK 78-30-00-440-804). Subtask 12-36-29-410-084 J. Close the fan cowl doors. FOR 4030EM2 - close the door 425BL (Ref. TASK 71-13-00-410-802). Subtask 12-36-29-281-067 K. Sampling (1) Perform a fluid sampling for particular contamination (Ref. TASK 1232-29-281-801). (2) Perform in daily check, the check of the clogging indicators of the HP filter 5111JM3 and the HCU filter 5001EG2. Do this operation again until the clogging indicator stay in. 5. Close-up ________ Subtask 12-36-29-410-085 A. Close Access (1) Close the door of the AC/DC emergency power-center 740VU. (2) Close the access door 811.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A316 Jul 01/05
(3) Remove the access platform(s). (4) Close the MLG doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-942-067 B. Remove the safety devices. (1) Remove the warning notice(s). Subtask 12-36-29-862-067 C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A317 Jul 01/05
**ON A/C 701-749, TASK 12-36-29-170-806-A Flushing of the HP line of the Yellow Hydraulic System WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job To flush the Yellow hydraulic system after a failure of the engine pump. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No
specific specific specific specific specific specific specific specific
No specific 98F12303000000
adjustable access platform blanking plugs circuit breaker(s) safety clip(s) hydraulic power cart warning notice access platform 2.5 m (8 ft. 2 in.) container 5 l (1.3208 USgal) Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft) Torque Wrench : range 2.00 to 20.00 m.daN (15.00 to 150.00 lbf.ft) 1 HYDRAULIC CONNECTORS
EFF : 701-749, 12-36-29 R SROS
Page A318 Apr 01/01
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-805 12-12-29-611-806 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-13-45-600-801 29-14-00-614-803 R 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 78-31-41-000-803 12-36-29-991-048 12-36-29-991-024 FOR FIN 4030EM2 71-13-00-010-805 71-13-00-410-805
Fill the Yellow Hydraulic Reservoir with a Hydraulic Service Cart Fill the Yellow Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Servicing of the Yellow HP Filter (5111JM3) Depressurization of the Yellow Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Removal of the Isolation Control Unit (4117KS) Fig. 323 Fig. 324 Open the Fan Cowl Doors Close the Fan Cowl Doors
3. __________ Job Set-up Subtask 12-36-29-860-073 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Make sure that the Yellow hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-804). (3) Depressurize the reservoir of the Yellow hydraulic system (Ref. TASK 29-14-00-614-803).
EFF : 701-749, 12-36-29 SROS
Page A319 Apr 01/05
Subtask 12-36-29-941-073 B. Safety Precautions (1) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure. (2) On the panel 225VU, make sure that the APU BLEED pushbutton switch is released (ON legend off) and install a warning notice to tell persons not to use it. (3) Put a warning notice in position to tell persons not to pressurize the hydraulic system: - on the HYD/FUEL control panel 245VU in the cockpit, - on the Yellow hydraulic system, access door 197BB. (4) On the panel 125VU: - make sure that the ENG MASTER switches for the two engines are in the OFF position, - put a warning notice to tell persons not to supply power to the ECU. (5) On the panel 285VU: - make sure that the ON legend of the related ENG FADEC GND PWR pushbutton switch is off, - put a warning notice to tell persons not to supply power to the FADEC system. (6) Put a container below the Yellow hydraulic engine pump and below the case drain filter. Subtask 12-36-29-865-099 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 722VU HYD PUMP Y CTL 9JJ R36 722VU HYD PUMP Y ENG 2 12JY T46 742VU FADEC A ENG 2 12KS2 Q74
EFF : 701-749, 12-36-29 R SROS
Page A320 Apr 01/01
Subtask 12-36-29-010-096 D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Open the fan cowl doors: FOR 4030EM2 Open the door 426AR (Ref. TASK 71-13-00-010-805) Subtask 12-36-29-010-097 E. Get access to the avionics compartment. (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the door of the AC/DC emergency power-center 740VU. (4) Put the adjustable access platform in position. 4. Procedure _________ Subtask 12-36-29-860-097 A. Preparation before the flushing of the HP line (Ref. Fig. 323/TASK 12-36-29-991-048) R R
CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE ON THE GROUND HYDRAULIC CART _______ IS SET TO A MINIMUM OF 7 BARS (101.53 PSI). (1) Disconnect the case drain line from the engine pump. (2) Disconnect the pressure line from the engine pump. (3) Disconnect the case drain line from the case drain filter. (4) Connect the pressure line and the case drain line together with the engine pump case drain/engine pump pressure connection (98F12303000104) of the HYDRAULIC CONNECTORS (98F12303000000). (5) Connect the pressure hose of the hydraulic power cart to the case drain line with the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000).
EFF : 701-749, 12-36-29 SROS
Page A321 Oct 01/04
Hydraulic Connections Figure 323/TASK 12-36-29-991-048 EFF : 701-749, 12-36-29 R SROS
Page A322 Apr 01/01
(6) Connect the return hose of the hydraulic power cart to the interface (98F12303000106) of the HYDRAULIC CONNECTORS (98F12303000000). (7) Connect the free end of the interface to the delivery ground connector 5131JM2. (8) Put blanking plugs on the disconnected line ends. (9) Close the leak measurement valve. - on the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/YELLOW pushbutton switch (the OFF legend comes on). Subtask 12-36-29-170-073 B. Flushing of the HP Line (Ref. Fig. 324/TASK 12-36-29-991-024) (1) Operate the hydraulic power cart for 2mn at 20 bars. (2) Stop the hydraulic power cart. (3) Open the leak measurement valve: - on the HYD section of the maintenance panel 285VU, push the LEAK MEASUREMENT VALVES/YELLOW pushbutton switch (the OFF legend goes off). (4) Replace the hydraulic filters, HP and filter element: - replace the HP filter 5111JM3 (Ref. TASK 29-13-45-600-801), - remove the filter element of the located on the Isolation Control Unit 4117KS (Ref. TASK 78-31-41-000-803). Subtask 12-36-29-420-073 C. Connection of the Hydraulic Line (1) Remove the blanking plugs from the disconnected line ends. (2) Remove the engine pump case drain/engine pump pressure connection (98F12303000104) of the HYDRAULIC CONNECTORS (98F12303000000) from the pressure line and from the case drain line. (3) Remove the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000) from the case drain line and from the hydraulic power cart. (4) Connect the pressure line to the engine pump.
EFF : 701-749, 12-36-29 R SROS
Page A323 Apr 01/01
Flushing of the HP line of the Yellow Hydraulic System Figure 324/TASK 12-36-29-991-024 EFF : 701-749, 12-36-29 R SROS
Page A324 Apr 01/01
(5) TORQUE the pressure line to between 12.88 and 14.24 m.daN (94.98 and 105.01 lbf.ft). (6) Connect the case drain line to the engine pump. (7) Connect the pump case drain hose to the case drain. (8) TORQUE the case drain line to between 2.43 and 3.16 m.daN (17.92 and 23.30 lbf.ft). Subtask 12-36-29-865-100 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 4030EM2 9JJ, 12JY, 12KS2, 13KS2 Subtask 12-36-29-611-073 E. Fill the Yellow hydraulic reservoir (Ref. TASK 12-12-29-611-805) or (Ref. TASK 12-12-29-611-806). Subtask 12-36-29-863-073 F. Pressurize the Yellow hydraulic reservoir (Ref. TASK 29-14-00-614-804). Subtask 12-36-29-410-096 G. Close the fan cowl doors. FOR 4030EM2 - close the door 426AR (Ref. TASK 71-13-00-410-805). Subtask 12-36-29-281-073 H. Sampling (1) Perform a fluid sampling for particular contamination (Ref. TASK 1232-29-281-801). (2) Perform in daily check, the check of the clogging indicators of the HP filter 5111JM3 and the filter element of the located on the Isolation Control Unit 4117KS. Do this operation again until the clogging indicator stay in.
R EFF : 701-749, 12-36-29 SROS
Page A325 Apr 01/01
5. Close-up ________ Subtask 12-36-29-410-097 A. Close Access (1) Close the door of the AC/DC emergency power-center 740VU. (2) Close the access door 811. (3) Remove the access platform(s). (4) Close the MLG doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-942-073 B. Remove the safety devices. (1) Remove the warning notice(s). Subtask 12-36-29-862-073 C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 701-749, 12-36-29 SROS
Page A326 Apr 01/01
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, TASK 12-36-29-170-807 Flushing of the Green Hydraulic System with the Aircraft Pumps WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-801 12-12-29-611-802 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-10-00-200-804 29-10-00-200-806
Fill the Green Hydraulic Reservoir with a Hydraulic Service Cart Fill the Green Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Check of the Clogging Indicators of the Hydraulic System Filter in the Hydraulics Compartment. Check of the Clogging Indicators of the Hydraulic System Filters on the Engines.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A327 Jul 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-11-43-600-802 29-11-44-600-801 29-11-45-600-801 29-14-00-614-804 31-60-00-860-801 31-60-00-860-802 71-00-00-860-801 78-31-00-710-804
Servicing of the (Forward) Engine-Pump Case-Drain Filter Element 5013JM1 Servicing of the Green Reservoir LP-Filter (5011JM1) Servicing of the Green HP Filter (5111JM101,5111JM102) Pressurization of the Hydraulic Reservoirs with external bench EIS Start Procedure EIS Stop Procedure Engine Automatic Start Thrust Reverser Cycling Test (MCDU)
R 3. __________ Job Set-up Subtask 12-36-29-860-116 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Do the EIS start procedure (EWD, SD DU only) (Ref. TASK 31-60-00-860801). (3) On the ECAM control panel, push the HYD key (on the SD, the HYD page comes into view). (4) Make sure that the SD does not show any of these conditions: - low air pressure in the Green reservoir. If this message is shown, pressurize the reservoir (Ref. TASK 29-14-00-614-804), - low fluid level in the Green reservoir. If the fluid is not correct add fluid with a service cart or with a hand pump (Ref. TASK 12-1229-611-801), (Ref. TASK 12-12-29-611-802).
EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A328 Jan 01/07
Subtask 12-36-29-865-110 B. On the ECAM control panel, push the C/B key (on the SD the C/B page comes into view). Make sure that the SD does not show this(these) circuit breaker(s) : ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU HSMU B + PART G 6JG U10 721VU HYD PUMP G ENG 1 14JG2 X11 722VU HYD SOV BUS SWTG 8JG R33 742VU HYD FIRE ENG 1 SOV 15JG2 D75 FOR 4030EM2 722VU HYD SOV ENG 2 NORM 15JY R35 722VU HSMU Y + PART G 7JG X46 722VU HYD PUMP G ENG 2 14JG1 X45 742VU HYD FIRE ENG 2 SOV 15JG1 D72 4. Procedure _________ Subtask 12-36-29-170-083 A. Flushing of the Green hydraulic system with A/C (1) Start the engine 1 (Ref. TASK 71-00-00-860-801). R
(2) During 10 minutes approximately: - operate the Captain and F/O sidestick and rudder pedals over full travel so that the controls surfaces move continuously, - operate cycles of the thrust reversers (Ref. TASK 78-31-00-710-804) in order to cause a hydraulic flow through the filter. (3) Stop the engine 1. (4) Do the check of the clogging indicators of: - the case-drain filters 5013JM1 (Ref. TASK 29-10-00-200-806), - the HP filters 5111JM101, 5111JM102 (Ref. TASK 29-10-00-200-804), - the LP filter 5011JM1 (Ref. TASK 29-10-00-200-804).
R R
(5) If necessary replace the defective filter element: - the case-drain filters 5013JM1 (Ref. TASK 29-11-43-600-802), - the HP filters 5111JM101, 5111JM102 (Ref. TASK 29-11-45-600-801), - the LP filter 5011JM1 (Ref. TASK 29-11-44-600-801).
R R
EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A329 Jan 01/07
(6) Start the engine 1 and do the step (2) again. (7) Stop the engine 1 and do the step (4) again. (8) Do the step (1) to (5) again until the clogging indicators stay in. (9) Do a fluid sampling for particles contamination (Ref. TASK 12-32-29281-801). (a) If particle contamination is out of limits do the step (1) to (5) again. 5. Close-up ________ Subtask 12-36-29-860-117 A. Do the EIS stop procedure (Ref. TASK 31-60-00-860-802). Subtask 12-36-29-862-083 B. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A330 Jul 01/05
**ON A/C 701-749, TASK 12-36-29-170-807-A Flushing of the Green Hydraulic System with the Aircraft Pumps WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-801 12-12-29-611-802 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-10-00-200-804 29-10-00-200-806
Fill the Green Hydraulic Reservoir with a Hydraulic Service Cart Fill the Green Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Check of the Clogging Indicators of the Hydraulic System Filter in the Hydraulics Compartment. Check of the Clogging Indicators of the Hydraulic System Filters on the Engines.
EFF : 701-749, 12-36-29 R SROS
Page A331 Apr 01/01
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-11-43-600-807 29-11-44-600-801 29-11-45-600-801 29-14-00-614-804 31-60-00-860-801 31-60-00-860-802 71-00-00-860-801 78-31-00-740-802 78-31-41-000-803
Servicing of the Engine-Pump Case Drain Filter (5013JM1) Servicing of the Green Reservoir LP-Filter (5011JM1) Servicing of the Green HP Filter (5111JM101,5111JM102) Pressurization of the Hydraulic Reservoirs with external bench EIS Start Procedure EIS Stop Procedure Engine Automatic Start Test of the Thrust Reverser Deployment and Stowage (Engine not Running) Removal of the Isolation Control Unit (4117KS)
3. __________ Job Set-up Subtask 12-36-29-860-104 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Do the EIS start procedure (EWD, SD DU only) (Ref. TASK 31-60-00-860801). (3) On the ECAM control panel, push the HYD key (on the SD, the HYD page comes into view). (4) Make sure that the SD does not show any of these conditions: - low air pressure in the Green reservoir. If this message is shown, pressurize the reservoir (Ref. TASK 29-14-00-614-804), - low fluid level in the Green reservoir. If the fluid is not correct add fluid with a service cart or with a hand pump (Ref. TASK 12-1229-611-801), (Ref. TASK 12-12-29-611-802).
EFF : 701-749, 12-36-29 R SROS
Page A332 Apr 01/01
Subtask 12-36-29-865-104 B. On the ECAM control panel, push the C/B key (on the SD the C/B page comes into view). Make sure that the SD does not show this(these) circuit breaker(s) : ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU HSMU B + PART G 6JG U10 722VU HYD SOV BUS SWTG 8JG R33 742VU HYD FIRE ENG 1 SOV 15JG2 D75 742VU HYD PUMP G ENG 1 14JG2 E67 FOR 4030EM2 722VU HYD SOV ENG 2 NORM 15JY R35 722VU HSMU Y + PART G 7JG X46 722VU HYD PUMP G ENG 2 14JG1 X45 742VU HYD FIRE ENG 2 SOV 15JG1 D72 4. Procedure _________ Subtask 12-36-29-170-077 A. Flushing of the Green hydraulic system with A/C (1) Start the engine 1 (Ref. TASK 71-00-00-860-801). (2) During 10mn approximately: - operate the Captain and F/O sidestick and rudder pedals over full travel so that the controls surfaces move continuously, - operate cycles of the thrust reversers (Ref. TASK 78-31-00-740-802) in order to cause a hydraulic flow through the filter. (3) Stop the engine 1. (4) Do the check of the clogging indicators of: - the case-drain filters 5013JM1 (Ref. TASK 29-10-00-200-806), - the HP filters 5111JM101, 5111JM102 (Ref. TASK 29-10-00-200-804), - the LP filter 5011JM1 (Ref. TASK 29-10-00-200-804), - the filter element located on the Isolation Control Unit 4117KS (Ref. TASK 78-31-41-000-803).
R EFF : 701-749, 12-36-29 SROS
Page A333 Apr 01/01
(5) If necessary replace the defective filter element: - the case-drain filters 5013JM1 (Ref. TASK 29-11-43-600-807), - the HP filters 5111JM101, 5111JM102 (Ref. TASK 29-11-45-600-801), - the LP filter 5011JM1 (Ref. TASK 29-11-44-600-801), - the filter element located on the Isolation Control Unit 4117KS (Ref. TASK 78-31-41-000-803). (6) Start the engine 1 and do the step (2) again. (7) Stop the engine 1 and do the step (4) again. (8) Do the step (1) to (5) again until the clogging indicators stay in. R
(9) Do a fluid sampling for particles contamination (Ref. TASK 12-32-29281-801).
R R R
(a) If particle contamination is out of limits do the step (1) to (5) again. 5. Close-up ________ Subtask 12-36-29-860-105 A. Do the EIS stop procedure (Ref. TASK 31-60-00-860-802). Subtask 12-36-29-862-077 B. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
EFF : 701-749, 12-36-29 SROS
Page A334 Oct 01/04
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, TASK 12-36-29-170-808 Flushing of the Blue Hydraulic System with the Aircraft Pump WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-803 12-12-29-611-804 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-10-00-200-804 29-10-00-200-806
Fill the Blue Hydraulic Reservoir with a Hydraulic Service Cart Fill the Blue Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Check of the Clogging Indicators of the Hydraulic System Filter in the Hydraulics Compartment. Check of the Clogging Indicators of the Hydraulic System Filters on the Engines.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A335 Jul 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-11-43-600-804 29-12-44-600-801 29-12-45-600-801 29-14-00-614-804 31-60-00-860-801 31-60-00-860-802 71-00-00-860-801 78-31-00-710-804 78-31-11-000-801
Servicing of the (Aft) Engine-Pump Case-Drain Filter Element 5013JM2 Servicing of the Blue Reservoir LP-Filter (5011JM2) Servicing of the Blue HP Filter (5111JM2) Pressurization of the Hydraulic Reservoirs with external bench EIS Start Procedure EIS Stop Procedure Engine Automatic Start Thrust Reverser Cycling Test (MCDU) Removal of the Hydraulic Filter Element
3. __________ Job Set-up Subtask 12-36-29-860-118 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Do the EIS start procedure (EWD, SD DU only) (Ref. TASK 31-60-00-860801). (3) On the ECAM control panel, push the HYD key (on the SD, the HYD page comes into view). (4) Make sure that the SD does not show any of these conditions: - low air pressure in the Blue reservoir. If this message is shown, pressurize the reservoir (Ref. TASK 29-14-00-614-804), - low fluid level in the Blue reservoir. If the fluid is not correct add fluid with a service cart or with a hand pump (Ref. TASK 12-1229-611-803), (Ref. TASK 12-12-29-611-804).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A336 Jul 01/05
Subtask 12-36-29-865-111 B. On the ECAM control panel, push the C/B key (on the SD the C/B page comes into view). Make sure that the SD does not show this(these) circuit breaker(s) : ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU HSMU B + PART G 6JG U10 721VU HYD PUMP G ENG 1 14JG2 X11 722VU HYD SOV BUS SWTG 8JG R33 742VU HYD FIRE ENG 1 SOV 15JG2 D75 4. Procedure _________ Subtask 12-36-29-170-084 A. Flushing of the Blue hydraulic system with A/C (1) Start the engine 1 (Ref. TASK 71-00-00-860-801). (2) During 10mn approximately: - operate the Captain and F/O sidestick and rudder pedals over full travel so that the controls surfaces move continuously, - operate cycles of the thrust reversers (Ref. TASK 78-31-00-710-804) in order to cause a hydraulic flow through the filter. (3) Stop the engine 1. (4) Do the check of the clogging indicators of: - the case-drain filter 5013JM2 (Ref. TASK 29-10-00-200-806), - the HP filter 5111JM2 (Ref. TASK 29-10-00-200-804), - the LP filter 5011JM2 (Ref. TASK 29-10-00-200-804), - the HCU filter 5000EG2 (Ref. TASK 78-31-11-000-801). (5) If necessary replace the defective filter element: - the case-drain filter 5013JM2 (Ref. TASK 29-11-43-600-804), - the HP filter 5111JM2 (Ref. TASK 29-12-45-600-801), - the LP filter 5011JM2 (Ref. TASK 29-12-44-600-801), - the HCU filter 5000EG2 (Ref. TASK 78-31-11-000-801). (6) Start the engine 1 and repeat step (2) again (7) Stop the engine 1 and repeat step (4) again.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A337 Jul 01/05
(8) Do the step (1) to (5) again until the clogging indicators stay in. (9) Do a fluid sampling for particles contamination (Ref. TASK 12-32-29281-801). (a) If particles contamination is out of limits do the step (1) to (5) again. 5. Close-up ________ Subtask 12-36-29-860-119 A. Do the EIS stop procedure (Ref. TASK 31-60-00-860-802). Subtask 12-36-29-862-084 B. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A338 Jul 01/05
**ON A/C 701-749, TASK 12-36-29-170-808-A Flushing of the Blue Hydraulic System with the Aircraft Pump WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-803 12-12-29-611-804 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-10-00-200-804 29-10-00-200-806
Fill the Blue Hydraulic Reservoir with a Hydraulic Service Cart Fill the Blue Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Check of the Clogging Indicators of the Hydraulic System Filter in the Hydraulics Compartment. Check of the Clogging Indicators of the Hydraulic System Filters on the Engines.
EFF : 701-749, 12-36-29 R SROS
Page A339 Apr 01/01
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-11-43-600-809 29-12-44-600-801 29-12-45-600-801 29-14-00-614-804 31-60-00-860-801 31-60-00-860-802 71-00-00-860-801 78-31-00-740-802 78-31-41-000-803
Servicing of the Engine Pump Case Drain Filter (5013JM2) Servicing of the Blue Reservoir LP-Filter (5011JM2) Servicing of the Blue HP Filter (5111JM2) Pressurization of the Hydraulic Reservoirs with external bench EIS Start Procedure EIS Stop Procedure Engine Automatic Start Test of the Thrust Reverser Deployment and Stowage (Engine not Running) Removal of the Isolation Control Unit (4117KS)
3. __________ Job Set-up Subtask 12-36-29-860-106 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Do the EIS start procedure (EWD, SD DU only) (Ref. TASK 31-60-00-860801). (3) On the ECAM control panel, push the HYD key (on the SD, the HYD page comes into view). (4) Make sure that the SD does not show any of these conditions: - low air pressure in the Blue reservoir. If this message is shown, pressurize the reservoir (Ref. TASK 29-14-00-614-804), - low fluid level in the Blue reservoir. If the fluid is not correct add fluid with a service cart or with a hand pump (Ref. TASK 12-1229-611-803), (Ref. TASK 12-12-29-611-804).
EFF : 701-749, 12-36-29 R SROS
Page A340 Apr 01/01
Subtask 12-36-29-865-105 B. On the ECAM control panel, push the C/B key (on the SD the C/B page comes into view). Make sure that the SD does not show this(these) circuit breaker(s) : ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU HSMU B + PART G 6JG U10 722VU HYD SOV BUS SWTG 8JG R33 742VU HYD FIRE ENG 1 SOV 15JG2 D75 742VU HYD PUMP G ENG 1 14JG2 E67 4. Procedure _________ Subtask 12-36-29-170-078 A. Flushing of the Blue hydraulic system with A/C (1) Start the engine 1 (Ref. TASK 71-00-00-860-801). (2) During 10mn approximately: - operate the Captain and F/O sidestick and rudder pedals over full travel so that the controls surfaces move continuously, - operate cycles of the thrust reversers (Ref. TASK 78-31-00-740-802) in order to cause a hydraulic flow through the filter. (3) Stop the engine 1. (4) Do the check of the clogging indicators of: - the case-drain filter 5013JM2 (Ref. TASK 29-10-00-200-806), - the HP filter 5111JM2 (Ref. TASK 29-10-00-200-804), - the LP filter 5011JM2 (Ref. TASK 29-10-00-200-804), - the filter element located on the Isolation Control Unit 4117KS (Ref. TASK 78-31-41-000-803). (5) If necessary replace the defective filter element: - the case-drain filter 5013JM2 (Ref. TASK 29-11-43-600-809), - the HP filter 5111JM2 (Ref. TASK 29-12-45-600-801), - the LP filter 5011JM2 (Ref. TASK 29-12-44-600-801), - the filter element located on the Isolation Control Unit 4117KS (Ref. TASK 78-31-41-000-803). (6) Start the engine 1 and repeat step (2) again
R EFF : 701-749, 12-36-29 SROS
Page A341 Apr 01/01
(7) Stop the engine 1 and repeat step (4) again. (8) Do the step (1) to (5) again until the clogging indicators stay in. R
(9) Do a fluid sampling for particles contamination (Ref. TASK 12-32-29281-801).
R R R
(a) If particles contamination is out of limits do the step (1) to (5) again. 5. Close-up ________ Subtask 12-36-29-860-107 A. Do the EIS stop procedure (Ref. TASK 31-60-00-860-802). Subtask 12-36-29-862-078 B. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
EFF : 701-749, 12-36-29 SROS
Page A342 Oct 01/04
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, TASK 12-36-29-170-809 Flushing of the Yellow Hydraulic System with the Aircraft Pump WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-805 12-12-29-611-806 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-10-00-200-804 29-10-00-200-806
Fill the Yellow Hydraulic Reservoir with a Hydraulic Service Cart Fill the Yellow Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Check of the Clogging Indicators of the Hydraulic System Filter in the Hydraulics Compartment. Check of the Clogging Indicators of the Hydraulic System Filters on the Engines.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A343 Jul 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-11-43-600-804 29-13-44-600-801 29-13-45-600-801 29-14-00-614-804 31-60-00-860-801 31-60-00-860-802 71-00-00-860-801 78-31-00-710-804 78-31-11-000-801
Servicing of the (Aft) Engine-Pump Case-Drain Filter Element 5013JM2 Servicing of the Yellow Reservoir LP-Filter (5011JM3) Servicing of the Yellow HP Filter (5111JM3) Pressurization of the Hydraulic Reservoirs with external bench EIS Start Procedure EIS Stop Procedure Engine Automatic Start Thrust Reverser Cycling Test (MCDU) Removal of the Hydraulic Filter Element
3. __________ Job Set-up Subtask 12-36-29-860-120 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Do the EIS start procedure (EWD, SD DU only) (Ref. TASK 31-60-00-860801). (3) On the ECAM control panel, push the HYD key (on the SD, the HYD page comes into view). (4) Make sure that the SD does not show any of these conditions: - low air pressure in the Yellow reservoir. If this message is shown, pressurize the reservoir (Ref. TASK 29-14-00-614-804), - low fluid level in the Yellow reservoir. If the fluid is not correct add fluid with a service cart or with a hand pump (Ref. TASK 12-12-29-611-805), (Ref. TASK 12-12-29-611-806).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A344 Jul 01/05
Subtask 12-36-29-865-112 B. On the ECAM control panel, push the C/B key (on the SD the C/B page comes into view). Make sure that the SD does not show this(these) circuit breaker(s) : ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM2 722VU HYD SOV ENG 2 NORM 15JY R35 722VU HSMU Y + PART G 7JG X46 722VU HYD PUMP G ENG 2 14JG1 X45 742VU HYD FIRE ENG 2 SOV 15JG1 D72 4. Procedure _________ Subtask 12-36-29-170-085 A. Flushing of the Yellow hydraulic system with A/C (1) Start the engine 2 (Ref. TASK 71-00-00-860-801). (2) During 10mn approximately: - operate the Captain and F/O sidestick and rudder pedals over full travel so that the controls surfaces move continuously, - operate cycles of the thrust reversers (Ref. TASK 78-31-00-710-804) in order to cause a hydraulic flow through the filter. (3) Stop the engine 2. (4) Do the check of the clogging indicators of: - the case-drain filter 5013JM2 (Ref. TASK 29-10-00-200-806), - the HP filters 5111JM3 (Ref. TASK 29-10-00-200-804), - the LP filter 5011JM3 (Ref. TASK 29-10-00-200-804), - the HCU filter 5000EG3 (Ref. TASK 78-31-11-000-801). (5) If necessary replace the defective filter element: - the case-drain filter 5013JM2 (Ref. TASK 29-11-43-600-804), - the HP filter 5111JM3 (Ref. TASK 29-13-45-600-801), - the LP filter 5011JM3 (Ref. TASK 29-13-44-600-801), - the HCU filter 5000EG3 (Ref. TASK 78-31-11-000-801). (6) Start the engine 2 and do the step (2) again. (7) Stop the engine 2 and do the step (4) again.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A345 Jul 01/05
(8) Do the step (1) to (5) again until the clogging indicators stay in. (9) Do a fluid sampling for particles contamination (Ref. TASK 12-32-29281-801). (a) If particle contamination is out of limits do the steps (1) to (5) again. 5. Close-up ________ Subtask 12-36-29-860-121 A. Do the EIS stop procedure (Ref. TASK 31-60-00-860-802). Subtask 12-36-29-862-085 B. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A346 Jul 01/05
**ON A/C 701-749, TASK 12-36-29-170-809-A Flushing of the Yellow Hydraulic System with the Aircraft Pump WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-805 12-12-29-611-806 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-10-00-200-804 29-10-00-200-806
Fill the Yellow Hydraulic Reservoir with a Hydraulic Service Cart Fill the Yellow Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Check of the Clogging Indicators of the Hydraulic System Filter in the Hydraulics Compartment. Check of the Clogging Indicators of the Hydraulic System Filters on the Engines.
EFF : 701-749, 12-36-29 R SROS
Page A347 Apr 01/01
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-11-43-600-809 29-13-44-600-801 29-13-45-600-801 29-14-00-614-804 31-60-00-860-801 31-60-00-860-802 71-00-00-860-801 78-31-00-740-802 78-31-41-000-803
Servicing of the Engine Pump Case Drain Filter (5013JM2) Servicing of the Yellow Reservoir LP-Filter (5011JM3) Servicing of the Yellow HP Filter (5111JM3) Pressurization of the Hydraulic Reservoirs with external bench EIS Start Procedure EIS Stop Procedure Engine Automatic Start Test of the Thrust Reverser Deployment and Stowage (Engine not Running) Removal of the Isolation Control Unit (4117KS)
3. __________ Job Set-up Subtask 12-36-29-860-108 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Do the EIS start procedure (EWD, SD DU only) (Ref. TASK 31-60-00-860801). (3) On the ECAM control panel, push the HYD key (on the SD, the HYD page comes into view). (4) Make sure that the SD does not show any of these conditions: - low air pressure in the Yellow reservoir. If this message is shown, pressurize the reservoir (Ref. TASK 29-14-00-614-804), - low fluid level in the Yellow reservoir. If the fluid is not correct add fluid with a service cart or with a hand pump (Ref. TASK 12-12-29-611-805), (Ref. TASK 12-12-29-611-806).
EFF : 701-749, 12-36-29 R SROS
Page A348 Apr 01/01
Subtask 12-36-29-865-106 B. On the ECAM control panel, push the C/B key (on the SD the C/B page comes into view). Make sure that the SD does not show this(these) circuit breaker(s) : ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM2 722VU HYD SOV ENG 2 NORM 15JY R35 722VU HSMU Y + PART G 7JG X46 722VU HYD PUMP G ENG 2 14JG1 X45 742VU HYD FIRE ENG 2 SOV 15JG1 D72 4. Procedure _________ Subtask 12-36-29-170-079 A. Flushing of the Yellow hydraulic system with A/C (1) Start the engine 2 (Ref. TASK 71-00-00-860-801). (2) During 10mn approximately: - operate the Captain and F/O sidestick and rudder pedals over full travel so that the controls surfaces move continuously, - operate cycles of the thrust reversers (Ref. TASK 78-31-00-740-802) in order to cause a hydraulic flow through the filter. (3) Stop the engine 2. (4) Do the check of the clogging indicators of: - the case-drain filter 5013JM2 (Ref. TASK 29-10-00-200-806), - the HP filters 5111JM3 (Ref. TASK 29-10-00-200-804), - the LP filter 5011JM3 (Ref. TASK 29-10-00-200-804), - the filter element located on the Isolation Control Unit 4117KS (Ref. TASK 78-31-41-000-803). (5) If necessary replace the defective filter element: - the case-drain filter 5013JM2 (Ref. TASK 29-11-43-600-809), - the HP filter 5111JM3 (Ref. TASK 29-13-45-600-801), - the LP filter 5011JM3 (Ref. TASK 29-13-44-600-801), - the filter element located on the Isolation Control Unit 4117KS (Ref. TASK 78-31-41-000-803). (6) Start the engine 2 and do the step (2) again.
R EFF : 701-749, 12-36-29 SROS
Page A349 Apr 01/01
(7) Stop the engine 2 and do the step (4) again. (8) Do the step (1) to (5) again until the clogging indicators stay in. R
(9) Do a fluid sampling for particles contamination (Ref. TASK 12-32-29281-801).
R R R
(a) If particle contamination is out of limits do the steps (1) to (5) again. 5. Close-up ________ Subtask 12-36-29-860-109 A. Do the EIS stop procedure (Ref. TASK 31-60-00-860-802). Subtask 12-36-29-862-079 B. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
EFF : 701-749, 12-36-29 SROS
Page A350 Oct 01/04
**ON A/C ALL TASK 12-36-29-170-810 Flushing of the Suction line of the Green Hydraulic System. WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific No specific No specific
circuit breaker(s) safety clip(s) warning notice container 70 l (18.4918 USgal)
EFF : ALL 12-36-29 SROS
Page A351 Jan 01/07
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R R R R R R R R R R
12-12-29-611-801 12-12-29-611-802 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-10-00-710-805 29-11-38-000-803 29-11-38-000-804 29-11-38-400-803 29-11-38-400-804
R R R R R
29-14-00-614-801 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 71-13-00-410-805 FOR FIN 4030EM1 71-13-00-010-805
Fill the Green Hydraulic Reservoir with a Hydraulic Service Cart Fill the Green Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Operational Test of the Electric Motor of the Engine Pump Suction Fire Shut-Off Valve Removal of the Engine Pump Suction Self Sealing (Elbow) Coupling (5135JM1) Removal of the Hydraulic System Self-Sealing Coupling (5135JM1) Installation of the Engine Pump Suction Self Sealing (Elbow) Coupling (5135JM1) Installation of the Hydraulic System Self-Sealing Coupling (5135JM1) Depressurization of the Green Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Close the Fan Cowl Doors Open the Fan Cowl Doors
EFF : ALL 12-36-29 SROS
Page A352 Jan 01/07
3. __________ Job Set-up R R
Subtask 12-36-29-860-202 A. Aircraft Maintenance Configuration
R R
(1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801).
R R R
(2) Make sure that the Green hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-804).
R R
(3) Depressurize the reservoir of the Green hydraulic system (Ref. TASK 29-14-00-614-801). Subtask 12-36-29-941-080
R
B. Safety Precautions (1) Make sure that the engine 1, 2 shutdown occurred not less than 5 minutes before you do this procedure. (2) On the panel 225VU, make sure that the APU BLEED pushbutton switch is released (ON legend off) and install a warning notice to tell persons not to use it.
R
(3) Put a warning notice in position to tell persons not to pressurize the hydraulic system: - on the HYD/FUEL control panel 245VU in the cockpit - on the Green hydraulic system, access door 197CB.
R R R R R
(4) On the panel 125VU. - Make sure that the ENG MASTER switches for the two engines are in the OFF position. - Put a warning notice to tell persons not to supply power to the ECU.
R R R R R
(5) On the panel 285VU. - Make sure that the ON legend of the related ENG FADEC GND PWR pushbutton switch is off, - Put a warning notice to tell persons not to supply power to the FADEC system. (6) Put a container below the Green hydraulic engine pump.
EFF : ALL 12-36-29 SROS
Page A353 Jan 01/07
R R R
Subtask 12-36-29-865-176 C. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s):
R R R
------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION -------------------------------------------------------------------------------
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499,
R R R R R R R R R R R
721VU HYD PUMP G ENG 1
14JG2
X11
9JV 13KS1 13KS2 14JG1 12KS2 12KS1
U09 D44 K49 X45 Q74 Q73
14JG2
E67
**ON A/C ALL 721VU 722VU 722VU 722VU 742VU 742VU
HYD PUMP G CTL FADEC B ENG 1 FADEC B ENG 2 HYD PUMP G ENG 2 FADEC A ENG 2 FADEC A ENG 1
**ON A/C 701-749, 742VU HYD PUMP G ENG 1 **ON A/C ALL Subtask 12-36-29-010-147
R
D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801).
R
(2) Open the fan cowl doors. FOR 4030EM1 - Open the door 416AR (Ref. TASK 71-13-00-010-805).
R
EFF : ALL 12-36-29 SROS
Page A354 Jan 01/07
4. Procedure _________ **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 12-36-29-860-203 A. Preparation before the flushing of the Suction Line. NOTE : Keep the suction line connect to the self sealing coupling. ____ (1) Disconnect the self-sealing coupling (5135JM) from the engine pump. Ref to the applicable step (Ref. TASK 29-11-38-000-803).
R
(2) Put blanking plug on the suction port of the hydraulic pump. R **ON A/C 701-749, Subtask 12-36-29-860-203-A A. Preparation before the flushing of the Suction Line. NOTE : Keep the suction line connect to the self sealing coupling. ____ (1) Disconnect the self-sealing coupling (5135JM) from the engine pump. Ref to the applicable step (Ref. TASK 29-11-38-000-804).
R
(2) Put blanking plug on the suction port of the hydraulic pump. R
**ON A/C ALL
R
Subtask 12-36-29-170-095
R
B. Flushing of the Suction Line.
R
(1) Put the suction line in the container.
R R
(2) Pressurize the hydraulic reservoir (Ref. TASK 29-14-00-614-804) to flush the suction line until the FSOV close.
R
(3) Depressurize the hydraulic reservoir (Ref. TASK 29-14-00-614-801).
R
(4) On the panel 742VU, reset the C/B 5JR.
EFF : ALL 12-36-29 SROS
Page A355 Jan 01/07
R R
(5) Do the operational test of the electrical motor of the FSOV (Ref. TASK 29-10-00-710-805).
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499,
R
Subtask 12-36-29-420-105
R
C. Installation of the self sealing coupling on the engine pump.
R
(1) Remove the blanking cap on the engine pump.
R R
(2) Install the self sealing coupling on the engine pump. Refer to the applicable step (Ref. TASK 29-11-38-400-803).
R
**ON A/C 701-749, Subtask 12-36-29-420-105-A
R
C. Installation of the self sealing coupling on the engine pump. (1) Remove the blanking cap on the engine pump. (2) Install the self sealing coupling on the engine pump. Refer to the applicable step (Ref. TASK 29-11-38-400-804).
R
**ON A/C ALL
R
Subtask 12-36-29-865-177
R R R R R R R R
D. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 14JG1, 14JG2, 12KS1, 12KS2, 13KS1, 13KS2 Subtask 12-36-29-611-198 E. Fill the Green hydraulic reservoir (Ref. TASK 12-12-29-611-801) or (Ref. TASK 12-12-29-611-802). Subtask 12-36-29-863-080 F. Pressurize the Green hydraulic reservoir (Ref. TASK 29-14-00-614-804).
EFF : ALL 12-36-29 SROS
Page A356 Jan 01/07
R Subtask 12-36-29-410-152 R R R R
G. Close the fan cowl doors. FOR 4030EM1 - Close the door 416AR (Ref. TASK 71-13-00-410-805). Subtask 12-36-29-281-080 H. Sampling
R R
(1) Perform a fluid sampling for particular contamination (Ref. TASK 1232-29-281-801).
R R R R
(2) Perform in daily check, the check of the clogging indicators, of the case drain filters 5013JM, HP filters 5111JM101, 5111JM102 and the LP filter 5011JM1: Do this operation again until the clogging indicator stay in. 5. Close-up ________
R R R
Subtask 12-36-29-862-107 A. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862801). Subtask 12-36-29-860-204
R
B. Put the Aircraft back to its Initial Configuration
R
(1) Close the MLG doors (Ref. TASK 32-12-00-410-801).
R
(2) Make sure that the work area is clean and clear of tools and other items.
R
(3) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 12-36-29 SROS
Page A357 Jan 01/07
TASK 12-36-29-170-811 Flushing of the Suction line of the Blue Hydraulic System. R R
WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS.
R R
WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY.
R R R R R
WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH.
R R R
CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific No specific No specific
circuit breaker(s) safety clip(s) warning notice container 70 l (18.4918 USgal)
EFF : ALL 12-36-29 SROS
Page A358 Jan 01/07
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R R R R R R R R R R R R R R R R R R R R R R R
12-12-29-611-803 12-12-29-611-804 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-10-00-710-805 29-12-38-000-802 29-12-38-000-803 29-12-38-400-802 29-12-38-400-803 29-14-00-614-802 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 71-13-00-410-803 FOR FIN 4030EM1 71-13-00-010-803
Fill the Blue Hydraulic Reservoir with a Hydraulic Service Cart Fill the Blue Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Operational Test of the Electric Motor of the Engine Pump Suction Fire Shut-Off Valve Removal of the Blue Hydraulic System Self-Sealing Coupling Removal of the Blue Engine Pump Suction Self Sealing (Elbow) Coupling Installation of the Blue Hydraulic System Self-Sealing Coupling Installation of the Blue Engine Pump Suction Self Sealing (Elbow) Coupling Depressurization of the Blue Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Closing of the Fan Cowl Doors Opening of the Fan Cowl Doors
EFF : ALL 12-36-29 SROS
Page A359 Jan 01/07
3. __________ Job Set-up R R
Subtask 12-36-29-860-205 A. Aircraft Maintenance Configuration
R R
(1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801).
R R R
(2) Make sure that the Blue hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-804).
R R
(3) Depressurize the reservoir of the Blue hydraulic system (Ref. TASK 29-14-00-614-802). Subtask 12-36-29-941-081
R
B. Safety Precautions
R R
(1) Make sure that the engine 1, 2 shutdown occurred not less than 5 minutes before you do this procedure. (2) On the panel 225VU, make sure that the APU BLEED pushbutton switch is released (ON legend off) and install a warning notice to tell persons not to use it.
R
(3) Put a warning notice in position to tell persons not to pressurize the hydraulic system: - on the HYD/FUEL control panel 245VU in the cockpit - on the Blue hydraulic system, access door ZAC 196BB.
R R R R R
(4) On the panel 125VU. - Make sure that the ENG MASTER switches for the two engines are in the OFF position. - Put a warning notice to tell persons not to supply power to the ECU.
R R R R R
(5) On the panel 285VU. - Make sure that the ON legend of the related ENG FADEC GND PWR pushbutton switch is off. - Put a warning notice to tell persons not to supply power to the FADEC system. (6) Put a container below the Blue hydraulic engine pump.
EFF : ALL 12-36-29 SROS
Page A360 Jan 01/07
R R R R R R R R R R R R
Subtask 12-36-29-865-178 C. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU HYD PUMP B ENG 1 11JB U08 721VU HYD PUMP B CTL 9JC X12 722VU FADEC B ENG 1 13KS1 D44 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 742VU FADEC A ENG 1 12KS1 Q73 Subtask 12-36-29-010-148
R
D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801).
R
(2) Open the fan cowl doors. FOR 4030EM1 - Open the door 415AL (Ref. TASK 71-13-00-010-803).
R
4. Procedure _________ **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 12-36-29-860-206 A. Preparation before the flushing of the Suction Line. NOTE : Keep the suction line connect to the self sealing coupling. ____ (1) Disconnect the self-sealing coupling (5135JM) from the engine pump. Ref to the applicable step (Ref. TASK 29-12-38-000-803).
R
(2) Put blanking plug on the suction port of the hydraulic pump. R
EFF : ALL 12-36-29 SROS
Page A361 Jan 01/07
**ON A/C 701-749, Subtask 12-36-29-860-206-A A. Preparation before the flushing of the Suction Line. NOTE : Keep the suction line connect to the self sealing coupling. ____ (1) Disconnect the self-sealing coupling (5135JM) from the engine pump. Ref to the applicable step (Ref. TASK 29-12-38-000-802).
R
(2) Put blanking plug on the suction port of the hydraulic pump. R
**ON A/C ALL
R
Subtask 12-36-29-170-096
R
B. Flushing of the Suction Line.
R
(1) Put the suction line in the container.
R R
(2) Pressurize the Blue hydraulic reservoir (Ref. TASK 29-14-00-614-804) to flush the suction line until the FSOV close.
R R
(3) Depressurize the Blue hydraulic reservoir (Ref. TASK 29-14-00-614802).
R
(4) On the panel 742VU, reset the C/B 5JR.
R R
(5) Do the operational test of the electrical motor of the FSOV (Ref. TASK 29-10-00-710-805).
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499,
R
Subtask 12-36-29-420-106
R
C. Installation of the self sealing coupling on the engine pump.
R
(1) Remove the blanking cap on the engine pump.
R R
(2) Install the self sealing coupling on the engine pump. Refer to the applicable step (Ref. TASK 29-12-38-400-803).
EFF : ALL 12-36-29 SROS
Page A362 Jan 01/07
R
**ON A/C 701-749, Subtask 12-36-29-420-106-A
R
C. Installation of the self sealing coupling on the engine pump. (1) Remove the blanking cap on the engine pump. (2) Install the self sealing coupling on the engine pump. Refer to the applicable step (Ref. TASK 29-12-38-400-802).
R R
**ON A/C ALL
R
Subtask 12-36-29-865-179
R R R R R R R R R
D. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 11JB, 9JC, 12KS1, 12KS2, 13KS1, 13KS2 Subtask 12-36-29-611-199 E. Fill the Blue hydraulic reservoir (Ref. TASK 12-12-29-611-803) or (Ref. TASK 12-12-29-611-804). Subtask 12-36-29-863-081 F. Pressurize the Blue hydraulic reservoir (Ref. TASK 29-14-00-614-804). Subtask 12-36-29-410-153
R R
G. Close the fan cowl doors. FOR 4030EM1 - Close the door 415AL (Ref. TASK 71-13-00-410-803).
R EFF : ALL 12-36-29 SROS
Page A363 Jan 01/07
R R
Subtask 12-36-29-281-081 H. Sampling
R R
(1) Perform a fluid sampling for particular contamination (Ref. TASK 1232-29-281-801).
R R R R
(2) Perform in daily check, the check of the clogging indicators, of the case drain filters 5013JM, HP filters 5111JM101, 5111JM102 and the LP filter 5011JM1. Do this operation again until the clogging indicator stay in. 5. Close-up ________
R R R
Subtask 12-36-29-862-108 A. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862801). Subtask 12-36-29-860-207
R
B. Put the Aircraft back to its Initial Configuration
R
(1) Close the MLG doors (Ref. TASK 32-12-00-410-801).
R
(2) Make sure that the work area is clean and clear of tools and other items.
R
(3) Remove all the fixtures, tools, test and support equipment used during this procedure.
R EFF : ALL 12-36-29 SROS
Page A364 Jan 01/07
TASK 12-36-29-170-812 Flushing of the Suction line of the Yellow Hydraulic System. R R
WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS.
R R
WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY.
R R R R R
WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH.
R R R
CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific No specific No specific
circuit breaker(s) safety clip(s) warning notice container 70 l (18.4918 USgal)
R EFF : ALL 12-36-29 SROS
Page A365 Jan 01/07
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R R R R R R R R R R R R R R R R R R R R R R R R R
12-12-29-611-805 12-12-29-611-806 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-10-00-710-805 29-13-38-000-802 29-13-38-000-803 29-13-38-400-802 29-13-38-400-803 29-14-00-614-802 29-14-00-614-803 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 71-13-00-410-803 FOR FIN 4030EM2 71-13-00-010-803
Fill the Yellow Hydraulic Reservoir with a Hydraulic Service Cart Fill the Yellow Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Operational Test of the Electric Motor of the Engine Pump Suction Fire Shut-Off Valve Removal of the Yellow Hydraulic System Self-Sealing Coupling Removal of the Yellow Engine Pump Suction Self Sealing (Elbow) Coupling Installation of the Yellow Hydraulic System Self-Sealing Coupling Installation of the Yellow Engine Pump Suction Self Sealing (Elbow) Coupling Depressurization of the Blue Hydraulic Reservoir with Ground Equipment Depressurization of the Yellow Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Closing of the Fan Cowl Doors Opening of the Fan Cowl Doors
R EFF : ALL 12-36-29 SROS
Page A366 Jan 01/07
3. __________ Job Set-up R R
Subtask 12-36-29-860-208 A. Aircraft Maintenance Configuration
R R
(1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801).
R R R
(2) Make sure that the Yellow hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-804).
R R
(3) Depressurize the reservoir of the Yellow hydraulic system (Ref. TASK 29-14-00-614-803). Subtask 12-36-29-941-082
R
B. Safety Precautions (1) Make sure that the engine 1 and 2 shutdown occurred not less than 5 minutes before you do this procedure. (2) On the panel 225VU, make sure that the APU BLEED pushbutton switch is released (ON legend off) and install a warning notice to tell persons not to use it.
R
(3) Put a warning notice in position to tell persons not to pressurize the hydraulic system: - on the HYD/FUEL control panel 245VU in the cockpit - on the Yellow hydraulic system, access door ZAC 196BB.
R R R R R
(4) On the panel 125VU. - Make sure that the ENG MASTER switches for the two engines are in the OFF position. - Put a warning notice to tell persons not to supply power to the ECU.
R R R R R
(5) On the panel 285VU. - Make sure that the ON legend of the related ENG FADEC GND PWR pushbutton switch is off. - Put a warning notice to tell persons not to supply power to the FADEC system. (6) Put a container below the Yellow hydraulic engine pump.
EFF : ALL 12-36-29 SROS
Page A367 Jan 01/07
R R R R R R R R R R R R
Subtask 12-36-29-865-180 C. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------722VU FADEC B ENG 1 13KS1 D44 722VU FADEC B ENG 2 13KS2 K49 722VU HYD PUMP Y CTL 9JJ R36 722VU HYD PUMP Y ENG 2 12JY T46 742VU FADEC A ENG 2 12KS2 Q74 742VU FADEC A ENG 1 12KS1 Q73 Subtask 12-36-29-010-149
R
D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801).
R
(2) Open the fan cowl doors. FOR 4030EM2 - open the door 425AL (Ref. TASK 71-13-00-010-803).
R
4. Procedure _________ **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 12-36-29-860-209 A. Preparation before the flushing of the Suction Line. NOTE : Keep the suction line connect to the self sealing coupling. ____ (1) Disconnect the self-sealing coupling (5135JM) from the engine pump. Ref to the applicable step (Ref. TASK 29-13-38-000-803).
R
(2) Put blanking plug on the suction port of the hydraulic pump. R
R EFF : ALL 12-36-29 SROS
Page A368 Jan 01/07
**ON A/C 701-749, Subtask 12-36-29-860-209-A A. Preparation before the flushing of the Suction Line. NOTE : Keep the suction line connect to the self sealing coupling. ____ (1) Disconnect the self-sealing coupling (5135JM) from the engine pump. Ref to the applicable step (Ref. TASK 29-13-38-000-802).
R
(2) Put blanking plug on the suction port of the hydraulic pump. R
**ON A/C ALL
R
Subtask 12-36-29-170-097
R
B. Flushing of the Suction Line.
R
(1) Put the suction line in the container.
R R
(2) Pressurize the hydraulic reservoir (Ref. TASK 29-14-00-614-804) to flush the suction line until the FSOV close.
R
(3) Depressurize the hydraulic reservoir (Ref. TASK 29-14-00-614-802).
R
(4) On the panel 742VU, reset the C/B 5JR.
R R
(5) Do the operational test of the electrical motor of the FSOV (Ref. TASK 29-10-00-710-805).
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499,
R
Subtask 12-36-29-420-107
R
C. Installation of the self sealing coupling on the engine pump.
R
(1) Remove the blanking cap on the engine pump.
R R
(2) Install the self sealing coupling on the engine pump. Refer to the applicable step (Ref. TASK 29-13-38-400-803).
R EFF : ALL 12-36-29 SROS
Page A369 Jan 01/07
R
**ON A/C 701-749, Subtask 12-36-29-420-107-A
R
C. Installation of the self sealing coupling on the engine pump. (1) Remove the blanking cap on the engine pump. (2) Install the self sealing coupling on the engine pump. Refer to the applicable step (Ref. TASK 29-13-38-400-802).
R R
**ON A/C ALL
R
Subtask 12-36-29-865-181
R R R R R R R R R
D. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 9JJ, 12JY, 12KS1, 12KS2, 13KS1, 13KS2 Subtask 12-36-29-611-200 E. Fill the Yellow hydraulic reservoir (Ref. TASK 12-12-29-611-805) or (Ref. TASK 12-12-29-611-806). Subtask 12-36-29-863-082 F. Pressurize the Yellow hydraulic reservoir (Ref. TASK 29-14-00-614-804). Subtask 12-36-29-410-154
R R
G. Close the fan cowl doors. FOR 4030EM2 - Close the door 425AL (Ref. TASK 71-13-00-410-803).
R EFF : ALL 12-36-29 SROS
Page A370 Jan 01/07
R R
Subtask 12-36-29-281-082 H. Sampling
R R
(1) Perform a fluid sampling for particular contamination (Ref. TASK 1232-29-281-801).
R R R R
(2) Perform in daily check, the check of the clogging indicators, of the case drain filters 5013JM, HP filters 5111JM101, 5111JM102 and the LP filter 5011JM1. Do this operation again until the clogging indicator stay in. 5. Close-up ________
R R R
Subtask 12-36-29-862-109 A. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862801). Subtask 12-36-29-860-210
R
B. Put the Aircraft back to its Initial Configuration
R
(1) Close the MLG doors (Ref. TASK 32-12-00-410-801).
R
(2) Make sure that the work area is clean and clear of tools and other items.
R
(3) Remove all the fixtures, tools, test and support equipment used during this procedure.
R EFF : ALL 12-36-29 SROS
Page A371 Jan 01/07
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, TASK 12-36-29-611-801 Replacement of the Hydraulic Fluid of the Green Hydraulic System with a Fluid Replacement and Recovery Bench WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. CAUTION : DO NOT DEPRESSURIZE THE ENGINE PUMPS DURING THE DRY MOTORING. IF YOU _______ DO, YOU CAN CAUSE DAMAGE TO THE ENGINE PUMPS. 1. __________________ Reason for the Job You must replace the fluid only if the acidity is higher than the values given into the task of the sampling for analysis (Ref. TASK 12-32-29-281-80100).
EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page A372 Jan 01/07
2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific No specific No specific No specific AGE10600A DH0501
blanking plug circuit breaker(s) safety clip(s) hydraulic ground power supply plug type E0053R8B3APNE safety devices access platform 1.80 m (5 ft. 11 in.) 1 CHECK - MOTOR GROUND, RAT 1 TOOL - HYDRAULIC FLUID CHANGE
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 02-003
F NSA 307110 TYPE 4 HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------07-11-00-581-801 07-11-00-586-801 12-12-29-611-801 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-863-801 29-10-00-611-801 29-10-00-710-805
Lifting of the Aircraft for Maintenance Operations Lowering of the Aircraft for Maintenance Operations Fill the Green Hydraulic Reservoir with a Hydraulic Service Cart Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Pressurize the Green Hydraulic System with the Ground Hydraulic Supply Drainage of the Green Hydraulic Reservoir Operational Test of the Electric Motor of the Engine Pump Suction Fire Shut-Off Valve
EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page A373 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-11-43-600-802 29-11-44-600-801 29-11-45-600-801 29-14-00-614-801 29-14-00-614-804 29-24-00-720-801
29-24-00-869-802 32-00-00-481-802 32-11-15-400-801 32-12-00-010-801 32-12-00-410-801 32-22-00-010-801 32-30-00-867-801 32-30-00-867-802 32-42-00-710-801 32-42-00-870-801 32-42-12-000-801 32-42-12-400-801 32-51-00-860-801 71-00-00-720-816 78-31-00-710-804 12-36-29-991-094 12-36-29-991-061 12-36-29-991-063 12-36-29-991-062
Servicing of the (Forward) Engine-Pump Case-Drain Filter Element 5013JM1 Servicing of the Green Reservoir LP-Filter (5011JM1) Servicing of the Green HP Filter (5111JM101,5111JM102) Depressurization of the Green Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Operational Check of RAT Manual Deployment, Functional Check of RAT followed by Inspection of Filter Element by Ref. to Diff. Press.-Indicator (with ACMS) Retraction of the Ram Air Turbine (RAT) on the Ground Installation of the Safety Devices on the Landing Gear Doors Installation of the MLG Bogie-Alignment Pitch Trimmer (Weight on Wheels) Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Open the NLG Doors for Maintenance Retraction of the Landing Gear for Maintenance Extension of the Landing Gear After Maintenance Operational Test of the Normal Braking System Bleeding the Normal Braking System at the Wheel Brakes Removal of the Hydraulic Brake Filter (5200GG) Installation of the Hydraulic Brake Filter (5200GG) Put the Nose Wheels on Greased Plates for Nose Wheel Steering (NWS) Maintenance (A/C on Ground) Test No. 2 - Engine Motor Leak Test (Dry Method) Thrust Reverser Cowl Doors Open Thrust Reverser Cycling Test (MCDU) Fig. 325 Fig. 326 Fig. 327 Fig. 328
EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page A374 Jan 01/07
3. __________ Job Set-up Subtask 12-36-29-861-062 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). Subtask 12-36-29-860-147 B. Aircraft Maintenance Configuration (1) Pressurize the Green hydraulic system (Ref. TASK 29-00-00-863-801). (2) Set the flap and slat control lever on the panel 114VU to the position 1. (3) On the ECAM Engine/Warning Display, the indication 1+F comes into view. (4) On the HYD section of the maintenance panel 285VU, make sure that the LEAK MEASUREMENT VALVES/G pushbutton switch is pushed (the OFF legend is on). (5) On the Green HP manifold 5103JM, disconnect the pressure switches 7JS1 and 19CE1, and on the free end make a short circuit between the pins A and B with a plug type E0053R8B3APNE. (Ref. Fig. 325/TASK 12-36-29-991-094) Subtask 12-36-29-865-128 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------722VU HYD SOV ENG 2 NORM 19JG R34 722VU HYD SOV BUS SWTG 8JG R33 742VU HYD FIRE ENG 1 SOV 15JG2 D75 742VU HYD FIRE ENG 2 SOV 15JG1 D72
EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page A375 Jan 01/07
Manifolds of the Green Hydraulic System Figure 325/TASK 12-36-29-991-094 R EFF : ALL 12-36-29 SROS
Page A376 Jan 01/07
Subtask 12-36-29-010-108 D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Put an access platform at the zone 147. Subtask 12-36-29-680-056 E. Drain the reservoir of the Green hydraulic system (Ref. TASK 29-10-00611-801). Subtask 12-36-29-860-148 F. Set the hydraulic ground power supply to the correct configuration: (1) Make sure that the hydraulic ground power supply reservoir is filled with new HYDRAULIC FLUIDS (Material No. 02-003). (2) Make sure that no chlorinated solvent has been used to flush the tool lines. (3) Set the hydraulic ground power supply to the cart reservoir configuration. (4) Open the by-pass valve. (5) Start the hydraulic ground power supply. (6) Adjust the hydraulic ground power supply to the minimum pressure ( 20 bar (290.0754 psi) approx.) and to a flow of 45/lmn approx. and stop the hydraulic ground power supply. Subtask 12-36-29-860-149 G. Set the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the correct configuration. (Ref. Fig. 326/TASK 12-36-29-991-061, 327/TASK 12-36-29-991-063) NOTE : Make sure that the Green reservoir depressurization valve is open ____ when you set the hydraulic fluid replacement and recovery bench to the correct configuration. (1) On the fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501): - close the valve V1.
EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page A377 Jan 01/07
Connection of Tools to the Green Hydraulic System Figure 326/TASK 12-36-29-991-061- 12 (SHEET 1) EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page A378 Jan 01/07
Connection of Tools to the Green Hydraulic System Figure 326/TASK 12-36-29-991-061- 22 (SHEET 2) EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page A379 Jan 01/07
Green Hydraulic System-Schematic Diagram Figure 327/TASK 12-36-29-991-063- 12 (SHEET 1) EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page A380 Jan 01/07
Green Hydraulic System-Schematic Diagram Figure 327/TASK 12-36-29-991-063- 22 (SHEET 2) EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page A381 Jan 01/07
(2) Connect the connector LP1 of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the LP connector of the hydraulic ground power supply. (3) Connect the HP1 connector of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the HP connector of the hydraulic ground power supply. (4) Connect the LP3 connector of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the suction connector of the ground service panel. (5) On the HP manifold 5102JM: (a) Remove the Green HP filter 5111JM101 (Ref. TASK 29-11-45-600801). (b) Install a dummy bowl of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) in place of the Green HP filter 5111JM101. (c) Connect the HP2 line to the dummy bowl and to the valve V2. (6) On the LP filter 5011JM1: (a) Disconnect the tube (1) from the LP filter 5011JM1. (b) Put a blanking plug on the Green LP filter 5011JM1. (c) Loosen the tube (1) from the Green LP manifold 5004JM. (d) Turn the tube (1) 90 deg. and connect the LP2 line. (e) Tighten the tube (1) on the Green LP manifold 5004JM. (7) Start the hydraulic ground power supply and make sure that the pressure read on the gage of the hydraulic fluid replacement and recovery bench is 4 bar (58.0150 psi). (8) Stop the hydraulic ground power supply.
EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page A382 Jan 01/07
4. Procedure _________ (Ref. Fig. 327/TASK 12-36-29-991-063) Subtask 12-36-29-611-126 A. Fill the Green reservoir. (1) Open the depressurization valve of Green reservoir (Ref. TASK 29-1400-614-801). (2) Open the valve V1 of the TOOL - HYDRAULIC FLUID CHANGE (DH0501) and start the hydraulic ground power supply. (3) Fill the Green reservoir until the fluid is at the upper limit on the visual indicator (Ref. TASK 12-12-29-611-801). (4) Close the depressurization valve. (5) Pressurize the Green hydraulic reservoir (Ref. TASK 29-14-00-614804). (6) Close the valve V1. Subtask 12-36-29-865-148 B. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU L/G SAFETY VLV 3GA S12 722VU LGCIU 2 2GA U38 742VU LGCIU 1 1GA L63 Subtask 12-36-29-020-055 C. At the zone 148 disconnect the electrical connector of the safety valve 85GA . (Ref. Fig. 325/TASK 12-36-29-991-094) Subtask 12-36-29-865-149 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GA, 2GA, 3GA
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A383 Jan 01/07
Subtask 12-36-29-611-127 E. Replacement of the Fluid in the RAT Suction and Pressure Lines (1) Install the CHECK - MOTOR GROUND, RAT (AGE10600A). (2) Turn the RAT (Ref. TASK 29-24-00-720-801) (3) Monitor the reservoir level. (4) Stop the RAT if the advisory low level comes into view on the ECAM SD. (5) If necessary fill the Green hydraulic reservoir (Ref. TASK 12-12-29611-801). (6) Open the valve V2 until you collect 45 liters of fluid. (7) Close the valve V2. (8) Stop the RAT and retract it (Ref. TASK 29-24-00-869-802). Subtask 12-36-29-611-128 F. Replacement of the Fluid in the Engine Pump Suction and Pressure Lines (1) For 4030EM1 (a) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501) open the valve V1 and keep it open during the full procedure. (b) Dry motor the engine (Ref. TASK 71-00-00-720-816). NOTE : Stop the dry motoring if the advisory low level comes into ____ view on the ECAM System Display (SD). If necessary fill the Green hydraulic reservoir (Ref. TASK 12-12-29-611801). (c) Dry motor the engine (Ref. TASK 71-00-00-720-816). (d) Open the valve V2 until you collect 45 liters of fluid. (e) Close the valve V2. (f) Stop the dry motoring.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A384 Jan 01/07
(2) For 4030EM2 (a) Do the steps (a) thru (f) again. Subtask 12-36-29-611-129-A G. Replacement of the Fluid in the Suction, Pressure and Case Drain Lines of the Electric Pump (1JV) (1) Disconnect the case drain tube from the electric pump 1JV. (2) Put blanking plug on the end of the tube. (3) Connect the case drain elec hose of the TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the electric pump 1JV. (4) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501): - make sure that the valve V1 is open. (5) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV). (6) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501): - open the valve V2 until you collect 4 liters of fluid. (7) Close the valve V2. (8) On the HYD section of the overhead panel 245VU: - release the GREEN/ELEC/AUTO pushbutton switch (8JV). Subtask 12-36-29-611-130-A H. Replacement of the Fluid in the Thrust Reverser System (1) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV). (2) Do two deploy-to-stow cycles of the thrust reverser (Ref. TASK 78-3100-710-804). (3) On the HYD section of the overhead panel 245VU: - release the GREEN/ELEC/AUTO pushbutton switch (8JV). (4) Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 15JG1, 15JG2, 19JG, 8JG
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A385 Jan 01/07
(5) On the panel 255VU: - Push the ENG1/ENG2/FIRE pushbutton switch. (6) On the ECAM SD make sure that the fire shutoff valves are closed. Subtask 12-36-29-611-131-A J. Replacement of the Fluid in the Supply and Return Lines of the Primary Servocontrols (Ref. Fig. 328/TASK 12-36-29-991-062) (1) On the FLT CTL section of the overhead panel 212VU: - push the PRIM3 pushbutton switch. (2) On the FLT CTL section of the overhead panel 241VU: - push the PRIM1 and SEC1 pushbutton switches. (3) On the ground service manifold 5109JM1 open the valves which supply the right and left wing. (Ref. Fig. 325/TASK 12-36-29-991-094) (4) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV). (5) Do 5 operations over full travel range and make sure that the surfaces move. If they do not move, do the reset of the related computers. (6) On the HYD section of the overhead panel 245VU: - release the GREEN/ELEC/AUTO pushbutton switch (8JV). (7) On the ground service manifold 5109JM1 close the valves for the right and left wing and open the valve for the aft fuselage. (8) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV). (9) Operate the elevators over full travel range four times. (10) Operate the rudder over full travel range four times. (11) On the HYD section of the overhead panel 245VU: - release the GREEN/ELEC/AUTO pushbutton switch (8JV). (12) Close the valve for the aft fuselage.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
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Flight Control Operations Figure 328/TASK 12-36-29-991-062 R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
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Subtask 12-36-29-865-129 K. Make sure that this(these) circuit breaker(s) is(are) closed: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM 10CV X14 721VU SFCC 1 NORM AVAIL 10CW X13 722VU SFCC 2 FLAP 2CV T43 722VU SFCC 2 SLAT 2CW V40 742VU SFCC 1 SLAT 1CW L62 742VU SFCC 1 FLAP 1CV L61 Subtask 12-36-29-611-132-A L. Replacement of the Fluid in the Flap and Slat Supply and Return Systems (1) Make sure that the flap and slat control lever on the panel 114VU is in the position 1. (2) On the ground service manifold 5109JM1 open the valves which supply the right and left wing. (3) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV). (4) Set the flap and slat control lever on the panel 114VU to the position 2. (5) On the HYD section of the overhead panel 245VU: - release the GREEN/ELEC/AUTO pushbutton switch (8JV). (6) On the ground service manifold 5109JM1 close the valves which supply the right and left wing. Subtask 12-36-29-611-133 M. Replacement of the Fluid in the Normal Braking System (1) Push and release the brake pedals one time (Ref. TASK 32-42-00-710801). (2) Replace the hydraulic brake filter 5200GG on the manifold 5105JM (Ref. TASK 32-42-12-000-801) and (Ref. TASK 32-42-12-400-801). (3) Push and release the brake pedals 5 times.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
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Subtask 12-36-29-611-134-A N. Replacement of the Fluid in the Nose Wheel Steering System (1) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV). (2) Operate the nose wheel steering over full travel 2 times (Ref. TASK 32-51-00-860-801). (3) On the HYD section of the overhead panel 245VU: - release the GREEN/ELEC/AUTO pushbutton switch (8JV). Subtask 12-36-29-865-150 P. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU L/G SAFETY VLV 3GA S12 722VU LGCIU 2 2GA U38 742VU LGCIU 1 1GA L63 Subtask 12-36-29-420-088 Q. At the zone 148 connect the electrical connector of the safety valve 85GA. (Ref. Fig. 325/TASK 12-36-29-991-094) Subtask 12-36-29-865-151 R. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GA, 2GA, 3GA Subtask 12-36-29-611-135-A S. Replacement of the Fluid in the Landing Gear Door System (1) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV). (2) Do 3 opening cycles of the NLG doors (Ref. TASK 32-22-00-010-801). (3) Do 3 opening cycles of the right MLG doors (Ref. TASK 32-12-00-010801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
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(4) Do 3 opening cycles of the left MLG doors (Ref. TASK 32-12-00-010801). (5) On the HYD section of the overhead panel 245VU: - release the GREEN/ELEC/AUTO pushbutton switch (8JV). (6) Install safety devices on the landing gear door actuators (Ref. TASK 32-00-00-481-802). Subtask 12-36-29-611-136 T. Replacement of the Fluid in the Landing Gear System (1) Lift the aircraft on jacks (Ref. TASK 07-11-00-581-801). (2) Start with the NLG and do 2 extension/retraction operations of the landing gear (Ref. TASK 32-30-00-867-801) and (Ref. TASK 32-30-00867-802). (3) Lower the aircraft (Ref. TASK 07-11-00-586-801). 5. Close-up ________ Subtask 12-36-29-420-080 A. Replace these hydraulic filters: - the HP filter 5111JM102 (Ref. TASK 29-11-45-600-801) - the LP filter 5011JM1 (Ref. TASK 29-11-44-600-801) - the two case drain filters 5013JM1 (Ref. TASK 29-11-43-600-802). Subtask 12-36-29-942-086 B. Aircraft Maintenance Configuration (1) On the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/G pushbutton switch (the OFF legend is off). (2) On the Green HP manifold 5103JM, remove the plug type E0053R8B3APNE from the pressure switches 7JS1 and 19CE1 and connect the pressure switches 7JS1 and 19CE1. (3) On the panel 255VU: - release the ENG1/ENG2 FIRE pushbutton switch. (4) If the engine pump suction fire shut-off valves do not open, do a reset of the C/B 5JR.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A390 Jan 01/07
(5) Do the operational test of the electric motors of the engine pump suction fire shut-off valves (2JG1) and (2JG2) (Ref. TASK 29-10-00710-805). (6) Do the bleeding of the normal braking system (Ref. TASK 32-42-00-870801). (7) Do the bleeding of the pitch trimmer (Ref. TASK 32-11-15-400-801). (8) Close the valves V1 and V2 on the recovery bench. (9) Disconnect all the lines between the aircraft and the recovery bench. (10) Disconnect all the lines between the recovery bench and the hydraulic ground power supply. (11) Replace the MP hydraulic filter 5111JM101 (Ref. TASK 29-11-45-600801). (12) Pressurize the Green hydraulic reservoir (Ref. TASK 29-14-00-614804). (13) Operate the flight controls and monitor the reservoir level. If necessary fill the Green hydraulic reservoir (Ref. TASK 12-12-29-611801). (14) Each week, do a new sampling of the fluid (Ref. TASK 12-32-29-281801). Subtask 12-36-29-942-087 C. Remove the safety precautions. (1) Remove the warning notice(s). Subtask 12-36-29-410-107 D. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Remove the access platform(s). (3) Close the landing gear doors (Ref. TASK 32-12-00-410-801).
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Subtask 12-36-29-862-092 E. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
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**ON A/C 701-749, TASK 12-36-29-611-801-A Replacement of the Hydraulic Fluid of the Green Hydraulic System with a Fluid Replacement and Recovery Bench WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. CAUTION : DO NOT DEPRESSURIZE THE ENGINE PUMPS DURING THE DRY MOTORING. IF YOU _______ DO, YOU CAN CAUSE DAMAGE TO THE ENGINE PUMPS. 1. __________________ Reason for the Job You must replace the fluid only if the acidity is higher than the values given into the task of the sampling for analysis (Ref. TASK 12-32-29-281-80100).
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2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific No specific No specific No specific AGE10600A DH0501
blanking plug circuit breaker(s) safety clip(s) hydraulic ground power supply plug type E0053R8B3APNE safety devices access platform 1.80 m (5 ft. 11 in.) 1 CHECK - MOTOR GROUND, RAT 1 TOOL - HYDRAULIC FLUID CHANGE
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 02-003
F NSA 307110 TYPE 4 HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------07-11-00-581-801 07-11-00-586-801 12-12-29-611-801 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-863-801 29-10-00-611-801 29-10-00-710-805
Lifting of the Aircraft for Maintenance Operations Lowering of the Aircraft for Maintenance Operations Fill the Green Hydraulic Reservoir with a Hydraulic Service Cart Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Pressurize the Green Hydraulic System with the Ground Hydraulic Supply Drainage of the Green Hydraulic Reservoir Operational Test of the Electric Motor of the Engine Pump Suction Fire Shut-Off Valve
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-11-43-600-807 29-11-44-600-801 29-11-45-600-801 29-14-00-614-801 29-14-00-614-804 29-24-00-720-801
29-24-00-869-802 32-00-00-481-802 32-11-15-400-801 32-12-00-010-801 32-12-00-410-801 32-22-00-010-801 32-30-00-867-801 32-30-00-867-802 32-42-00-710-801 32-42-00-870-801 32-42-12-000-801 32-42-12-400-801 32-51-00-860-801 71-00-00-720-828 78-31-00-740-802 12-36-29-991-094 12-36-29-991-064 12-36-29-991-066 12-36-29-991-065
Servicing of the Engine-Pump Case Drain Filter (5013JM1) Servicing of the Green Reservoir LP-Filter (5011JM1) Servicing of the Green HP Filter (5111JM101,5111JM102) Depressurization of the Green Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Operational Check of RAT Manual Deployment, Functional Check of RAT followed by Inspection of Filter Element by Ref. to Diff. Press.-Indicator (with ACMS) Retraction of the Ram Air Turbine (RAT) on the Ground Installation of the Safety Devices on the Landing Gear Doors Installation of the MLG Bogie-Alignment Pitch Trimmer (Weight on Wheels) Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Open the NLG Doors for Maintenance Retraction of the Landing Gear for Maintenance Extension of the Landing Gear After Maintenance Operational Test of the Normal Braking System Bleeding the Normal Braking System at the Wheel Brakes Removal of the Hydraulic Brake Filter (5200GG) Installation of the Hydraulic Brake Filter (5200GG) Put the Nose Wheels on Greased Plates for Nose Wheel Steering (NWS) Maintenance (A/C on Ground) Dry Motoring Engine Test of the Thrust Reverser Deployment and Stowage (Engine not Running) Fig. 325 Fig. 329 Fig. 330 Fig. 331
EFF : 701-749, 12-36-29 R SROS
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3. __________ Job Set-up Subtask 12-36-29-861-065 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). Subtask 12-36-29-860-156 B. Aircraft Maintenance Configuration (1) Pressurize the Green hydraulic system (Ref. TASK 29-00-00-863-801). (2) Set the flap and slat control lever on the panel 114VU to the position 1. (3) On the ECAM Engine/Warning Display, the indication 1+F comes into view. (4) On the HYD section of the maintenance panel 285VU, make sure that the LEAK MEASUREMENT VALVES/G pushbutton switch is pushed (the OFF legend is on). (5) On the Green HP manifold 5103JM, disconnect the pressure switches 7JS1 and 19CE1, and on the free end make a short circuit between the pins A and B with a plug type E0053R8B3APNE. (Ref. Fig. 325/TASK 12-36-29-991-094) Subtask 12-36-29-865-134 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------722VU HYD SOV ENG 2 NORM 19JG R34 722VU HYD SOV BUS SWTG 8JG R33 742VU HYD FIRE ENG 1 SOV 15JG2 D75 742VU HYD FIRE ENG 2 SOV 15JG1 D72
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Subtask 12-36-29-010-111 D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Put an access platform at the zone 147. Subtask 12-36-29-680-059 E. Drain the reservoir of the Green hydraulic system (Ref. TASK 29-10-00611-801). Subtask 12-36-29-860-157 F. Set the hydraulic ground power supply to the correct configuration: (1) Make sure that the hydraulic ground power supply reservoir is filled with new HYDRAULIC FLUIDS (Material No. 02-003). (2) Make sure that no chlorinated solvent has been used to flush the tool lines. (3) Set the hydraulic ground power supply to the cart reservoir configuration. (4) Open the by-pass valve. (5) Start the hydraulic ground power supply. (6) Adjust the hydraulic ground power supply to the minimum pressure ( 20 bar (290.0754 psi) approx.) and to a flow of 45/lmn approx. and stop the hydraulic ground power supply. Subtask 12-36-29-860-158 G. Set the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the correct configuration. (Ref. Fig. 329/TASK 12-36-29-991-064, 330/TASK 12-36-29-991-066) NOTE : Make sure that the Green reservoir depressurization valve is open ____ when you set the hydraulic fluid replacement and recovery bench to the correct configuration. (1) On the fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501): - close the valve V1.
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Connection of the Tools to the Green Hydraulic System Figure 329/TASK 12-36-29-991-064- 12 (SHEET 1) EFF : 701-749, 12-36-29 R SROS
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Connection of the Tools to the Green Hydraulic System Figure 329/TASK 12-36-29-991-064- 22 (SHEET 2) EFF : 701-749, 12-36-29 R SROS
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Green Hydraulic System-Schematic Diagram Figure 330/TASK 12-36-29-991-066- 12 (SHEET 1) EFF : 701-749, 12-36-29 R SROS
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Green Hydraulic System-Schematic Diagram Figure 330/TASK 12-36-29-991-066- 22 (SHEET 2) EFF : 701-749, 12-36-29 R SROS
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(2) Connect the connector LP1 of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the LP connector of the hydraulic ground power supply. (3) Connect the HP1 connector of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the HP connector of the hydraulic ground power supply. (4) Connect the LP3 connector of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the suction connector of the ground service panel. (5) On the HP manifold 5102JM (a) Remove the Green HP filter 5111JM101 (Ref. TASK 29-11-45-600801). (b) Install a dummy bowl of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) in place of the Green HP filter 5111JM101. (c) Connect the HP2 line to the dummy bowl and to the valve V2. (6) On the LP filter 5011JM1: (a) Disconnect the tube (1) from the LP filter 5011JM1. (b) Put a blanking plug on the Green LP filter 5011JM1. (c) Loosen the tube (1) from the Green LP manifold 5004JM. (d) Turn the tube (1) 90 deg. and connect the LP2 line. (e) Tighten the tube (1) on the Green LP manifold 5004JM. (7) Start the hydraulic ground power supply and make sure that the pressure read on the gage of the hydraulic fluid replacement and recovery bench is 4 bar (58.0150 psi). (8) Stop the hydraulic ground power supply.
EFF : 701-749, 12-36-29 R SROS
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4. Procedure _________ (Ref. Fig. 330/TASK 12-36-29-991-066) Subtask 12-36-29-611-152 A. Fill the Green reservoir. (1) Open the depressurization valve of Green reservoir (Ref. TASK 29-1400-614-801). (2) Open the valve V1 of the TOOL - HYDRAULIC FLUID CHANGE (DH0501) and start the hydraulic ground power supply. (3) Fill the Green reservoir until the fluid is at the upper limit on the visual indicator (Ref. TASK 12-12-29-611-801). (4) Close the depressurization valve of Green reservoir. (5) Pressurize the Green hydraulic reservoir (Ref. TASK 29-14-00-614804). (6) Close the valve V1. Subtask 12-36-29-865-152 B. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU L/G SAFETY VLV 3GA S12 722VU LGCIU 2 2GA U38 742VU LGCIU 1 1GA L63 Subtask 12-36-29-020-056 C. At the zone 148 disconnect the electrical connector of the safety valve 85GA. (Ref. Fig. 325/TASK 12-36-29-991-094) Subtask 12-36-29-865-153 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GA, 2GA, 3GA
EFF : 701-749, 12-36-29 R SROS
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Subtask 12-36-29-611-153 E. Replacement of the Fluid in the RAT Suction and Pressure Lines (1) Install the CHECK - MOTOR GROUND, RAT (AGE10600A). (2) Turn the RAT (Ref. TASK 29-24-00-720-801). (3) Monitor the reservoir level. (4) Stop the RAT if the advisory low level comes into view on the ECAM SD. (5) If necessary fill the Green hydraulic reservoir (Ref. TASK 12-12-29611-801). (6) Open the valve V2 until you collect 45 liters of fluid. (7) Close the valve V2. (8) Stop the RAT and retract it (Ref. TASK 29-24-00-869-802). Subtask 12-36-29-611-154 F. Replacement of the Fluid in the Engine Pump Suction and Pressure Lines (1) For 4030EM1 (a) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501) open the valve V1 and keep it open during the full procedure. (b) Dry motor the engine (Ref. TASK 71-00-00-720-828). NOTE : Stop the dry motoring if the advisory low level comes into ____ view on the ECAM System Display (SD). If necessary fill the Green hydraulic reservoir (Ref. TASK 12-12-29-611801). (c) Dry motor the engine (Ref. TASK 71-00-00-720-828). (d) Open the valve V2 until you collect 45 filters of fluid. (e) Close the valve V2. (f) Stop the dry motoring.
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(2) For 4030EM2 (a) Do the steps (a) thru (f) again. Subtask 12-36-29-611-155 G. Replacement of the Fluid in the Suction, Pressure and Case Drain Lines of the Electric Pump (1JV) (1) Disconnect the case drain tube from the electric pump (1JV). (2) Put blanking plug on the end of the tube. (3) Connect the case drain elec hose of the TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the electric pump (1JV). (4) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501): - make sure that the valve V1 is open. (5) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV). (6) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501): - open the valve V2 until you collect 4 liters of fluid. (7) Close the valve V2. (8) On the HYD section of the overhead panel 245VU: - release the GREEN/ELEC/AUTO pushbutton switch (8JV). Subtask 12-36-29-611-156 H. Replacement of the Fluid in the Thrust Reverser System (1) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV). (2) Do two deploy-to-stow cycles of the thrust reverser (Ref. TASK 78-3100-740-802). (3) On the HYD section of the overhead panel 245VU: - release the GREEN/ELEC/AUTO pushbutton switch (8JV). (4) Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 15JG1, 15JG2, 19JG, 8JG.
R EFF : 701-749, 12-36-29 SROS
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(5) On the panel 255VU: Push the ENG1/ENG2/FIRE pushbutton switch. (6) On the ECAM SD make sure that the fire shutoff valves are closed. Subtask 12-36-29-611-157 J. Replacement of the Fluid in the Supply and Return Lines of the Primary Servocontrols (Ref. Fig. 331/TASK 12-36-29-991-065) (1) On the FLT CTL section of the overhead panel 212VU: - push the PRIM3 pushbutton switch. (2) On the FLT CTL section of the overhead panel 241VU: - push the PRIM1 and SEC1 pushbutton switches. (3) On the ground service manifold 5109JM1 open the valves which supply the right and left wing. (Ref. Fig. 325/TASK 12-36-29-991-094) (4) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV). (5) Do 5 operations over full travel range and make sure that the surfaces move. If they do not move, do the reset of the related computers. (6) On the HYD section of the overhead panel 245VU: - release the GREEN/ELEC/AUTO pushbutton switch (8JV). (7) On the ground service manifold 5109JM1 close the valves for the right and left wing and open the valve for the aft fuselage. (8) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV). (9) Operate the elevators over full travel range four times. (10) Operate the rudder over full travel range four times. (11) On the HYD section of the overhead panel 245VU: - release the GREEN/ELEC/AUTO pushbutton switch (8JV). (12) Close the valve for the aft fuselage.
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Flight Control Operations Figure 331/TASK 12-36-29-991-065 R EFF : 701-749, 12-36-29 SROS
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Subtask 12-36-29-865-135 K. Make sure that this(these) circuit breaker(s) is(are) closed: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM 10CV X14 721VU SFCC 1 NORM AVAIL 10CW X13 722VU SFCC 2 FLAP 2CV T43 722VU SFCC 2 SLAT 2CW V40 742VU SFCC 1 SLAT 1CW L62 742VU SFCC 1 FLAP 1CV L61 Subtask 12-36-29-611-158 L. Replacement of the Fluid in the Flap and Slat Supply and Return Systems (1) Make sure that the flap and slat control lever on the panel 114VU is in the position 1. (2) On the ground service manifold 5109JM1 open the valves which supply the right and left wing. (3) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV). (4) Set the flap and slat control lever on the panel 114VU to the position 2. (5) On the HYD section of the overhead panel 245VU: - release the GREEN/ELEC/AUTO pushbutton switch (8JV). (6) On the ground service manifold 5109JM1 close the valves which supply the right and left wing. Subtask 12-36-29-611-159 M. Replacement of the Fluid in the Normal Braking System (1) Push and release the brake pedals one time (Ref. TASK 32-42-00-710801). (2) Replace the hydraulic brake filter 5200GG on the manifold 5105JM (Ref. TASK 32-42-12-000-801) and (Ref. TASK 32-42-12-400-801). (3) Push and release the brake pedals 5 times.
R EFF : 701-749, 12-36-29 SROS
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Subtask 12-36-29-611-160 N. Replacement of the Fluid in the Nose Wheel Steering System (1) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV). (2) Operate the nose wheel steering over full travel 2 times (Ref. TASK 32-51-00-860-801). (3) On the HYD section of the overhead panel 245VU: - release the GREEN/ELEC/AUTO pushbutton switch (8JV). Subtask 12-36-29-865-154 P. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU L/G SAFETY VLV 3GA S12 722VU LGCIU 2 2GA U38 742VU LGCIU 1 1GA L63 Subtask 12-36-29-420-089 Q. At the zone 148 connect the electrical connector of the safety valve 85GA. (Ref. Fig. 325/TASK 12-36-29-991-094) Subtask 12-36-29-865-155 R. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GA, 2GA, 3GA Subtask 12-36-29-611-161 S. Replacement of the Fluid in the Landing Gear Door System (1) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV). (2) Do 3 opening cycles of the NLG doors (Ref. TASK 32-22-00-010-801). (3) Do 3 opening cycles of the right MLG doors (Ref. TASK 32-12-00-010801).
R EFF : 701-749, 12-36-29 SROS
Page B309 Jan 01/07
(4) Do 3 opening cycles of the left MLG doors (Ref. TASK 32-12-00-010801). (5) On the HYD section of the overhead panel 245VU: - release the GREEN/ELEC/AUTO pushbutton switch (8JV). (6) Install safety devices on the landing gear door actuators (Ref. TASK 32-00-00-481-802). Subtask 12-36-29-611-162 T. Replacement of the Fluid in the Landing Gear System (1) Lift the aircraft on jacks (Ref. TASK 07-11-00-581-801). (2) Start with the NLG and do 2 extension/retraction operations of the landing gear (Ref. TASK 32-30-00-867-801) and (Ref. TASK 32-30-00867-802). (3) Lower the aircraft (Ref. TASK 07-11-00-586-801). 5. Close-up ________ Subtask 12-36-29-420-083 A. Replace these hydraulic filters: - the HP filter 5111JM102 (Ref. TASK 29-11-45-600-801), - the LP filter 5011JM1 (Ref. TASK 29-11-44-600-801), - the two case drain filters 5013JM1 (Ref. TASK 29-11-43-600-807). Subtask 12-36-29-942-092 B. Aircraft Maintenance Configuration (1) On the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/G pushbutton switch (the OFF legend is off). (2) On the Green HP manifold 5103JM, remove the plug type E0053R8B3APNE from the pressure switches 7JS1 and 19CE1 and connect the pressure switches 7JS1 and 19CE1. (3) On the panel 255VU: - release the ENG1/ENG2/FIRE pushbutton switch. (4) If the engine pump suction fire shut-off valves do not open, do a reset of the C/B 5JR.
R EFF : 701-749, 12-36-29 SROS
Page B310 Jan 01/07
(5) Do the operational test of the electric motors of the engine pump suction fire shut-off valves (2JG1) and (2JG2) (Ref. TASK 29-10-00710-805). (6) Do the bleeding of the normal braking system (Ref. TASK 32-42-00-870801). (7) Do the bleeding of the pitch trimmer (Ref. TASK 32-11-15-400-801). (8) Close the valves V1 and V2 on the recovery bench. (9) Disconnect all the lines between the aircraft and the recovery bench. (10) Disconnect all the lines between the recovery bench and the hydraulic ground power supply. (11) Replace the HP hydraulic filter 5111JM101 (Ref. TASK 29-11-45-600801). (12) Pressurize the Green hydraulic reservoir (Ref. TASK 29-14-00-614804). (13) Operate the flight controls and monitor the reservoir level. If necessary fill the Green hydraulic reservoir (Ref. TASK 12-12-29-611801). (14) Each week, do a new sampling of the fluid (Ref. TASK 12-32-29-281801). Subtask 12-36-29-942-093 C. Remove the safety precautions. (1) Remove the warning notice(s). Subtask 12-36-29-410-110 D. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Remove the access platform(s). (3) Close the landing gear doors (Ref. TASK 32-12-00-410-801).
R EFF : 701-749, 12-36-29 SROS
Page B311 Jan 01/07
Subtask 12-36-29-862-095 E. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 701-749, 12-36-29 SROS
Page B312 Jan 01/07
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, TASK 12-36-29-611-802 Replacement of the Hydraulic Fluid of the Blue Hydraulic System with a Fluid Replacement and Recovery Bench WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. CAUTION : DO NOT DEPRESSURIZE THE ENGINE PUMPS DURING THE DRY MOTORING. IF YOU _______ DO, YOU CAN CAUSE DAMAGE TO THE ENGINE PUMPS. 1. __________________ Reason for the Job You must replace the fluid only if the acidity is higher than the values given into the task of the sampling for analysis (Ref. TASK 12-32-29-281-80100).
EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page B313 Jan 01/07
2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific No specific No specific DH0501
blanking plug hydraulic ground power supply plug type E0053R8B3APNE access platform 1.8 m (5 ft. 11 in.) access platform 1.80 m (5 ft. 11 in.) 1 TOOL - HYDRAULIC FLUID CHANGE
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 02-003
F NSA 307110 TYPE 4 HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-803 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-863-801 29-10-00-611-802 29-10-00-710-805 29-11-43-600-804 29-12-44-600-801 29-12-45-600-801
Fill the Blue Hydraulic Reservoir with a Hydraulic Service Cart Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Pressurize the Green Hydraulic System with the Ground Hydraulic Supply Drainage of the Blue Hydraulic Reservoir Operational Test of the Electric Motor of the Engine Pump Suction Fire Shut-Off Valve Servicing of the (Aft) Engine-Pump Case-Drain Filter Element 5013JM2 Servicing of the Blue Reservoir LP-Filter (5011JM2) Servicing of the Blue HP Filter (5111JM2)
EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page B314 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-14-00-614-802 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 32-43-00-870-801 32-45-00-864-801 71-00-00-720-816 78-31-00-710-804 12-36-29-991-095 12-36-29-991-070 12-36-29-991-072 12-36-29-991-071
Depressurization of the Blue Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Bleeding the Alternate Braking System at the Wheel Brakes Release the Pressure from the Parking Brake System after Depressurization Test No. 2 - Engine Motor Leak Test (Dry Method) Thrust Reverser Cowl Doors Open Thrust Reverser Cycling Test (MCDU) Fig. 332 Fig. 333 Fig. 334 Fig. 335
3. __________ Job Set-up Subtask 12-36-29-861-063 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). Subtask 12-36-29-860-150 B. Aircraft Maintenance Configuration (1) Pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-801). (2) Set the flap and slat control lever on the panel 114VU to the position 1. (3) On the ECAM engine/warning display the indication 1+F comes into view. (4) On the HYD section of the maintenance panel 285VU, make sure that the LEAK MEASUREMENT VALVES/B pushbutton switch is pushed (the OFF legend is on).
EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page B315 Jan 01/07
(5) On the Blue HP manifold 6103JM, disconnect the pressure switches 7JS2 and 19CE2, and on the free end make a short circuit between the pin A and B with an plug type E0053R8B3APNE. (Ref. Fig. 332/TASK 12-36-29-991-095) Subtask 12-36-29-010-109-A C. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Put an access platform at the zone 147. (3) Put an access platform in position at the zone 195. (4) Remove the access panel 195CB. Subtask 12-36-29-680-057 D. Drain the reservoir of the Blue hydraulic system (Ref. TASK 29-10-00-611802). Subtask 12-36-29-860-151 E. Set the hydraulic ground power supply to the correct configuration: (1) Make sure that the hydraulic ground power supply reservoir is filled with new HYDRAULIC FLUIDS (Material No. 02-003). (2) Make sure that no chlorinated solvent has been used to flush the tool lines. (3) Set the hydraulic ground power supply to the cart reservoir configuration. (4) Open the by-pass valve. (5) Start the hydraulic ground power supply. (6) Adjust the hydraulic ground power supply to the minimum pressure (20 bar (290.0754 psi) approx.) and to a flow of 45/lmn approx. and stop the hydraulic ground power supply.
EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page B316 Jan 01/07
Manifolds of the Blue Hydraulic System Figure 332/TASK 12-36-29-991-095 R EFF : ALL 12-36-29 SROS
Page B317 Jan 01/07
Subtask 12-36-29-860-152 F. Set the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the correct configuration. (Ref. Fig. 333/TASK 12-36-29-991-070, 334/TASK 12-36-29-991-072) NOTE : Make sure that the Blue reservoir depressurization valve is open ____ when you set the hydraulic fluid replacement and recovery bench to the correct configuration. (1) On the fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501): - close the valve V1. (2) Connect the connector LP1 of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the LP connector of the hydraulic ground power supply. (3) Connect the HP1 connector of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the HP connector of the hydraulic ground power supply. (4) connect the LP3 connector of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the suction connector of the ground service panel. (5) On the HP manifold 6103JM: (a) Remove the Blue HP filter 5111JM2 (Ref. TASK 29-12-45-600-801). (b) Install a dummy bowl of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) in place of the Blue HP filter 5111JM2. (c) Connect the HP2 line to the dummy bowl and to the valve V2. (6) On the LP filter 5011JM2: (a) Disconnect the flexible hose (1) from the Blue LP manifold 6005JM, and connect the LP2 line. (7) Put a blanking plug on the Blue LP filter 5011JM2. (8) Start the hydraulic ground power supply and make sure that the pressure read on the gage of the hydraulic fluid replacement and recovery bench is 4 bar (58.0150 psi).
EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page B318 Jan 01/07
INTENTIONALLY BLANK
R 12-36-29 SROS
Page B319 Jan 01/07
Connections of Tools to the Blue Hydraulic System Figure 333/TASK 12-36-29-991-070- 12 (SHEET 1) EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page B320 Jan 01/07
Connections of Tools to the Blue Hydraulic System Figure 333/TASK 12-36-29-991-070- 22 (SHEET 2) R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B321 Jan 01/07
Blue Hydraulic System-Schematic Diagram Figure 334/TASK 12-36-29-991-072- 12 (SHEET 1) R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B322 Jan 01/07
Blue Hydraulic System-Schematic Diagram Figure 334/TASK 12-36-29-991-072- 22 (SHEET 2) R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B323 Jan 01/07
(9) Stop the hydraulic ground power supply. 4. Procedure _________ (Ref. Fig. 334/TASK 12-36-29-991-072) Subtask 12-36-29-611-137 A. Fill the Blue reservoir. (1) Open the depressurization valve of Blue reservoir (Ref. TASK 29-1400-614-802). (2) Open the valve V1 of the TOOL - HYDRAULIC FLUID CHANGE (DH0501) and start the hydraulic ground power supply. (3) Fill the Blue reservoir until the fluid is at the upper limit on the visual indicator (Ref. TASK 12-12-29-611-803). (4) Close the depressurization valve of Blue reservoir. (5) Pressurize the Blue hydraulic reservoir (Ref. TASK 29-14-00-614-804). (6) Close the valve V1. Subtask 12-36-29-611-138 B. Replacement of the Fluid in the Engine Pump Suction and Pressure Lines (1) For 4030EM1 (a) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501) open the valve V1 and keep it open during the full procedure. (b) Dry motor the engine (Ref. TASK 71-00-00-720-816). NOTE : Stop the dry motoring if the advisory low level comes into ____ view on the ECAM SYSTEM DISPLAY. If necessary fill the Blue hydraulic reservoir (Ref. TASK 12-12-29-611-803). (c) Dry motor the engine (Ref. TASK 71-00-00-720-816). (d) Open the valve V2 until you collect 40 liters of fluid. (e) Close the valve V2. (f) Stop the dry motoring.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B324 Jan 01/07
Subtask 12-36-29-611-139 C. Replacement of the Fluid in the Suction, Pressure and Case Drain Lines of the Electric Pump (1JC) (1) Disconnect the case drain tube from the electric pump (1JC). (2) Put blanking plug on the end of the tube. (3) Connect the case drain elec hose of the TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the electric pump (1JC). (4) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501): - make sure that the valve V1 is open. (5) On the HYD section of the overhead panel 245VU: - push the BLUE/ELEC pushbutton switch (4JC). (6) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501): - open the valve V2 until you collect 4 liters of fluid. (7) Close the valve V2. (8) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC). Subtask 12-36-29-611-140 D. Replacement of the Fluid in the Alternate Brake Accumulators (1) On the manifold 5401GG depressurize the brake accumulators (Ref. TASK 32-45-00-864-801). Subtask 12-36-29-611-141 E. Replacement of the Fluid in the Thrust Reverser System (1) On the HYD section of the overhead panel 245VU: - push the BLUE/ELEC pushbutton switch (4JC). (2) Do two deploy-to-stow cycles of the thrust reverser (Ref. TASK 78-3100-710-804) . (3) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B325 Jan 01/07
(4) On the panel 255VU: - Push the ENG1/FIRE pushbutton switch. On the ECAM SD make sure that the fire shutoff valve is closed. Subtask 12-36-29-611-142 F. Replacement of the Fluid in the Supply and Return Lines of the Primary Servocontrols (Ref. Fig. 335/TASK 12-36-29-991-071) (1) On the FLT CTL section of the overhead panel 212VU: - push the SEC2, PRIM2 and PRIM3 pushbutton switches. (2) On the ground service manifold 5109JM2 open the valves which supply the right and left wing. (Ref. Fig. 332/TASK 12-36-29-991-095) (3) On the HYD section of the overhead panel 245VU: - push the BLUE/ELEC pushbutton switch (4JC). (4) Do 5 operations over full travel range and make sure that the surfaces move. If they do not move, do the reset of the related computers. (5) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC). (6) On the ground service manifold 5109JM2 close the valves for the right and left wing and open the valve for the aft fuselage. (7) On the HYD section of the overhead panel 245VU: - push the BLUE/ELEC pushbutton switch (4JC). (8) Operate the elevators over full travel range four times. (9) Operate the rudder over full travel range four times. (10) Operate the THS until you collect 5 liters of fluid. (11) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC). (12) Close the valve for the aft fuselage.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B326 Jan 01/07
Flight Control Operations Figure 335/TASK 12-36-29-991-071 R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B327 Jan 01/07
Subtask 12-36-29-865-131 G. Make sure that this(these) circuit breaker(s) is(are) closed: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM AVAIL 10CW X13 722VU SFCC 2 SLAT 2CW V40 742VU SFCC 1 SLAT 1CW L62 Subtask 12-36-29-611-143 H. Replacement of the Fluid in the Flap and Slat Supply and Return Systems (1) Make sure that the flap and slat control lever on the panel 114VU is in the position 1. (2) On the ground service manifold 5109JM2 open the valves which supply the right and left wing. (3) On the HYD section of the overhead panel 245VU: - push the BLUE/ELEC pushbutton switch (4JC). (4) Set the flap and slat control lever on the panel 114VU to the position 2. (5) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC). (6) On the ground service manifold 5109JM2 close the valves which supply the right and left wing. Subtask 12-36-29-611-144 J. Replacement of the Fluid in the Alternate Braking System (1) On the panel 312VU, set the PARK BRK switch to the OFF position. (2) On the HYD section of the overhead panel 245VU: - push the BLUE/ELEC pushbutton switch (4JC). (3) Push and release the brake pedals five times. (4) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B328 Jan 01/07
5. Close-up ________ Subtask 12-36-29-420-081 A. Replace these hydraulic filters: - the LP filter 5011JM2 (Ref. TASK 29-12-44-600-801) - the case drain filter 5013JM2 (Ref. TASK 29-11-43-600-804). Subtask 12-36-29-942-088 B. Aircraft Maintenance Configuration (1) On the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/B pushbutton switch (the OFF legend is off). (2) On the Blue HP manifold 6103JM, remove the plug type E0053R8B3APNE from the pressure switches 7JS2 and 19CE2 and connect the pressure switches 7JS2 and 19CE2. (3) On the panel 255VU: - release the ENG2/FIRE pushbutton switch. (4) Do the operational test of the electric motor of the engine pump suction fire shut-off valve (4JB) (Ref. TASK 29-10-00-710-805). (5) Do the bleeding of the alternate brake system (Ref. TASK 32-43-00870-801). (6) Close the valves V1 and V2 on the recovery bench. (7) Disconnect all the lines between the aircraft and the recovery bench. (8) Disconnect all the lines between the recovery bench and the hydraulic ground power supply. (9) Replace the HP hydraulic filter 5111JM2 (Ref. TASK 29-12-45-600-801). (10) Pressurize the Blue hydraulic reservoir (Ref. TASK 29-14-00-614-804). (11) Operate the flight controls and monitor the reservoir level. If necessary fill the Blue hydraulic reservoir (Ref. TASK 12-12-29-611803). (12) Each week, do a new sampling of the fluid (Ref. TASK 12-32-29-281801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B329 Jan 01/07
Subtask 12-36-29-942-089 C. Remove the safety precautions. (1) Remove the warning notice(s). Subtask 12-36-29-410-108 D. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Remove the access platform(s). (3) Close the landing gear doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-862-093 E. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B330 Jan 01/07
**ON A/C 701-749, TASK 12-36-29-611-802-A Replacement of the Hydraulic Fluid of the Blue Hydraulic System with a Fluid Replacement and Recovery Bench WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. CAUTION : DO NOT DEPRESSURIZE THE ENGINE PUMPS DURING THE DRY MOTORING. IF YOU _______ DO, YOU CAN CAUSE DAMAGE TO THE ENGINE PUMPS. 1. __________________ Reason for the Job You must replace the fluid only if the acidity is higher than the values given into the task of the sampling for analysis (Ref. TASK 12-32-29-281-80100).
EFF : 701-749, 12-36-29 R SROS
Page B331 Jan 01/07
2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific No specific No specific DH0501
blanking plug hydraulic ground power supply plug type E0053R8B3APNE access platform 1.8 m (5 ft. 11 in.) access platform 1.80 m (5 ft. 11 in.) 1 TOOL - HYDRAULIC FLUID CHANGE
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 02-003
F NSA 307110 TYPE 4 HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-803 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-863-801 29-10-00-611-802 29-10-00-710-805 29-11-43-600-809 29-12-44-600-801 29-12-45-600-801
Fill the Blue Hydraulic Reservoir with a Hydraulic Service Cart Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Pressurize the Green Hydraulic System with the Ground Hydraulic Supply Drainage of the Blue Hydraulic Reservoir Operational Test of the Electric Motor of the Engine Pump Suction Fire Shut-Off Valve Servicing of the Engine Pump Case Drain Filter (5013JM2) Servicing of the Blue Reservoir LP-Filter (5011JM2) Servicing of the Blue HP Filter (5111JM2)
EFF : 701-749, 12-36-29 R SROS
Page B332 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-14-00-614-802 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 32-43-00-870-801 32-45-00-864-801 71-00-00-720-828 78-31-00-740-802 12-36-29-991-095 12-36-29-991-073 12-36-29-991-075 12-36-29-991-074
Depressurization of the Blue Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Bleeding the Alternate Braking System at the Wheel Brakes Release the Pressure from the Parking Brake System after Depressurization Dry Motoring Engine Test of the Thrust Reverser Deployment and Stowage (Engine not Running) Fig. 332 Fig. 336 Fig. 337 Fig. 338
3. __________ Job Set-up Subtask 12-36-29-861-066 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). Subtask 12-36-29-860-159 B. Aircraft Maintenance Configuration (1) Pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-801). (2) Set the flap and slat control lever on the panel 114VU to the position 1. (3) On the ECAM Engine/Warning Display the indication 1+F comes into view. (4) On the HYD section of the maintenance panel 285VU, make sure that the LEAK MEASUREMENT VALVES/B pushbutton switch is pushed (the OFF legend is on).
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(5) On the Blue HP manifold 6103JM, disconnect the pressure switches 7JS2 and 19CE2 and on the free end make a short circuit between the pin A and B with a plug type E0053R8B3APNE. (Ref. Fig. 332/TASK 12-36-29-991-095) Subtask 12-36-29-010-112-A C. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Put an access platform at the zone 147. (3) Put an access platform in position at the zone 195. (4) Remove the access panel 195CB. Subtask 12-36-29-680-060 D. Drain the reservoir of the Blue hydraulic system (Ref. TASK 29-10-00-611802). Subtask 12-36-29-860-160 E. Set the hydraulic ground power supply to the correct configuration: (1) Make sure that the hydraulic ground power supply reservoir is filled with new HYDRAULIC FLUIDS (Material No. 02-003). (2) Make sure that no chlorinated solvent has been used to flush the tool lines. (3) Set the hydraulic ground power supply to the cart reservoir configuration. (4) Open the by-pass valve. (5) Start the hydraulic ground power supply. (6) Adjust the hydraulic ground power supply to the minimum pressure ( 20 bar (290.0754 psi) approx.) and to a flow of 45/lmn approx. and stop the hydraulic ground power supply.
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Subtask 12-36-29-860-161 F. Set the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the correct configuration. (Ref. Fig. 336/TASK 12-36-29-991-073, 337/TASK 12-36-29-991-075) NOTE : Make sure that the Blue reservoir depressurization valve is open ____ when you set the hydraulic fluid replacement and recovery bench to the correct configuration. (1) On the fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501): - close the valve V1. (2) Connect the connector LP1 of the of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the LP connector of the hydraulic ground power supply. (3) Connect the HP1 connector of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the HP connector of the hydraulic ground power supply. (4) Connect the LP3 connector of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the suction connector of the ground service panel. (5) On the HP manifold 6103JM (a) Remove the Blue HP filter 5111JM2 (Ref. TASK 29-12-45-600-801). (b) Install a dummy bowl of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) in place on the Blue HP filter 5111JM2. (c) Connect the HP2 line to the dummy bowl and to the valve V2. (6) On the LP filter 5011JM2 (a) Disconnect the flexible hose (1) from the Blue LP manifold 6005JM, and connect the LP2 line. (7) Put a blanking plug on the Blue LP filter 5011JM2. (8) Start the hydraulic ground power supply and make sure that the pressure read on the gage of the hydraulic fluid replacement and recovery bench is 4 bar (58.0150 psi).
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Connections of Tools to the Blue Hydraulic System Figure 336/TASK 12-36-29-991-073- 12 (SHEET 1) EFF : 701-749, 12-36-29 R SROS
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Connections of Tools to the Blue Hydraulic System Figure 336/TASK 12-36-29-991-073- 22 (SHEET 2) R EFF : 701-749, 12-36-29 SROS
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Blue Hydraulic System-Schematic Diagram Figure 337/TASK 12-36-29-991-075- 12 (SHEET 1) R EFF : 701-749, 12-36-29 SROS
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Blue Hydraulic System-Schematic Diagram Figure 337/TASK 12-36-29-991-075- 22 (SHEET 2) R EFF : 701-749, 12-36-29 SROS
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(9) Stop the hydraulic ground power supply. 4. Procedure _________ (Ref. Fig. 337/TASK 12-36-29-991-075) Subtask 12-36-29-611-163 A. Fill the Blue reservoir. (1) Open the depressurization valve of Blue reservoir (Ref. TASK 29-1400-614-802). (2) Open the valve V1 of the TOOL - HYDRAULIC FLUID CHANGE (DH0501) and start the hydraulic ground power supply. (3) Fill the Blue reservoir until the fluid is at the upper limit on the visual indicator (Ref. TASK 12-12-29-611-803). (4) Close the depressurization valve of Blue reservoir. (5) Pressurize the Blue hydraulic reservoir (Ref. TASK 29-14-00-614-804). (6) Close the valve V1. Subtask 12-36-29-611-164 B. Replacement of the Fluid in the Engine Pump Suction and Pressure Lines (1) For 4030EM1 (a) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501) open the valve V1 and keep it open during the full procedure. (b) Dry motor the engine (Ref. TASK 71-00-00-720-828). NOTE : Stop the dry motoring if the advisory low level comes into ____ view on the ECAM SYSTEM DISPLAY. If necessary fill the Blue hydraulic reservoir (Ref. TASK 12-12-29-611-803). (c) Dry motor the engine (Ref. TASK 71-00-00-720-828). (d) Open the valve V2 until you collect 40 liters of fluid. (e) Close the valve V2. (f) Stop the dry motoring.
R EFF : 701-749, 12-36-29 SROS
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Subtask 12-36-29-611-165 C. Replacement of the Fluid in the Suction, Pressure and Case Drain Lines of the Electric Pump (1JC) (1) Disconnect the case drain tube from the electric pump (1JC). (2) Put blanking plug on the end of the tube. (3) Connect the case drain elec hose of the TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the electric pump (1JC). (4) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501): - make sure that the valve V1 is open. (5) On the HYD section of the overhead panel 245VU: - push the BLUE/ELEC pushbutton switch (4JC). (6) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501): - open the valve V2 until you collect 4 liters of fluid. (7) Close the valve V2. (8) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC) Subtask 12-36-29-611-166 D. Replacement of the Fluid in the Alternate Brake Accumulators (1) On the manifold 5401GG depressurize the brake accumulators (Ref. TASK 32-45-00-864-801). Subtask 12-36-29-611-167 E. Replacement of the Fluid in the Thrust Reverser System (1) On the HYD section of the overhead panel 245VU: - push the BLUE/ELEC pushbutton switch (4JC). (2) Do two deploy-to-stow cycles of the thrust reverser (Ref. TASK 78-3100-740-802). (3) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC).
R EFF : 701-749, 12-36-29 SROS
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(4) On the panel 255VU: Push the ENG1 FIRE pushbutton switch: - On the ECAM SD make sure that the fire shutoff valve is closed. Subtask 12-36-29-611-168 F. Replacement of the Fluid in the Supply and Return Lines of the Primary Servocontrols (Ref. Fig. 338/TASK 12-36-29-991-074) (1) On the FLT CTL section of the overhead panel 212VU: - push the SEC2, PRIM2 and PRIM3 pushbutton switches. (2) On the ground service manifold 5109JM2 open the valves which supply the right and left wing. (Ref. Fig. 332/TASK 12-36-29-991-095) (3) On the HYD section of the overhead panel 245VU: - push the BLUE/ELEC pushbutton switch (4JC). (4) Do 5 operations over full travel range and make sure that the surfaces move. If they do not move, do the reset of the related computers. (5) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC). (6) On the ground service manifold 5109JM2 close the valves for the right and left wing and open the valve for the aft fuselage. (7) On the HYD section of the overhead panel 245VU: - push the BLUE/ELEC pushbutton switch (4JC). (8) Operate the elevators over full travel range four times. (9) Operate the rudder over full travel range four times. (10) Operate the THS until you collect 5 liters of fluid. (11) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC). (12) Close the valve for the aft fuselage.
R EFF : 701-749, 12-36-29 SROS
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Flight Control Operations Figure 338/TASK 12-36-29-991-074 R EFF : 701-749, 12-36-29 SROS
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Subtask 12-36-29-865-137 G. Make sure that this(these) circuit breaker(s) is(are) closed: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM AVAIL 10CW X13 722VU SFCC 2 SLAT 2CW V40 742VU SFCC 1 SLAT 1CW L62 Subtask 12-36-29-611-169 H. Replacement of the Fluid in the Flap and Slat Supply and Return Systems (1) Make sure that the flap and slat control lever on the panel 114VU is in the position 1. (2) On the ground service manifold 5109JM2 open the valves which supply the right and left wing. (3) On the HYD section of the overhead panel 245VU: - push the BLUE/ELEC pushbutton switch (4JC). (4) Set the flap and slat control lever on the panel 114VU to the position 2. (5) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC). (6) On the ground service manifold 5109JM2 close the valves which supply the right and left wing. Subtask 12-36-29-611-170 J. Replacement of the Fluid in the Alternate Braking System (1) On the panel 312VU, set the PARK BRK switch to the OFF position. (2) On the HYD section of the overhead panel 245VU: - push the BLUE/ELEC pushbutton switch (4JC). (3) Push and release the brake pedals five times. (4) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC).
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5. Close-up ________ Subtask 12-36-29-420-084 A. Replace these hydraulic filters: - the LP filter 5011JM2 (Ref. TASK 29-12-44-600-801) - the case drain filter 5013JM2 (Ref. TASK 29-11-43-600-809). Subtask 12-36-29-942-094 B. Aircraft Maintenance Configuration (1) On the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/B pushbutton switch (the OFF legend is off). (2) On the Blue HP manifold 6103JM, remove the plug type E0053R8B3APNE from the pressure switches 7JS2 and 19CE2 and connect the pressure switches 7JS2 and 19CE2. (3) On the panel 255VU: - release the ENG2/FIRE pushbutton switch. (4) Do the operational test of the electric motor of the engine pump suction fire shut-off valve (4JB) (Ref. TASK 29-10-00-710-805). (5) Do the bleeding of the alternate brake system (Ref. TASK 32-43-00870-801). (6) Close the valves V1 and V2 on the recovery bench. (7) Disconnect all the lines between the aircraft and the recovery bench. (8) Disconnect all the lines between the recovery bench and the hydraulic ground power supply. (9) Replace the HP hydraulic filter 5111JM2 (Ref. TASK 29-12-45-600-801). (10) Pressurize the Blue hydraulic reservoir (Ref. TASK 29-14-00-614-804). (11) Operate the flight controls and monitor the reservoir level. If necessary fill the Blue hydraulic reservoir (Ref. TASK 12-12-29-611803). (12) Each week, do a new sampling of the fluid (Ref. TASK 12-32-29-281801).
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Subtask 12-36-29-942-095 C. Remove the safety precautions. (1) Remove the warning notice(s). Subtask 12-36-29-410-111 D. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Remove the access platform(s). (3) Close the landing doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-862-096 E. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 701-749, 12-36-29 SROS
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**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, TASK 12-36-29-611-803 Replacement of the Hydraulic Fluid of the Yellow Hydraulic System with a Fluid Replacement and Recovery Bench WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. CAUTION : DO NOT DEPRESSURIZE THE ENGINE PUMPS DURING THE DRY MOTORING. IF YOU _______ DO, YOU CAN CAUSE DAMAGE TO THE ENGINE PUMPS. 1. __________________ Reason for the Job You must replace the fluid only if the acidity is higher than the values given into the task of the sampling for analysis (Ref. TASK 12-32-29-281-80100).
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2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific No specific DH0501
blanking plug hydraulic ground power supply plug type E0053R8B3APNE access platform 1.8 m (5 ft. 11 in.) 1 TOOL - HYDRAULIC FLUID CHANGE
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 02-003
F NSA 307110 TYPE 4 HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-805 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-863-801 29-10-00-611-803 29-10-00-710-805 29-11-43-600-804 29-13-44-600-801 29-13-45-600-801
Fill the Yellow Hydraulic Reservoir with a Hydraulic Service Cart Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Pressurize the Green Hydraulic System with the Ground Hydraulic Supply Drainage of the Yellow Hydraulic Reservoir Operational Test of the Electric Motor of the Engine Pump Suction Fire Shut-Off Valve Servicing of the (Aft) Engine-Pump Case-Drain Filter Element 5013JM2 Servicing of the Yellow Reservoir LP-Filter (5011JM3) Servicing of the Yellow HP Filter (5111JM3)
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-14-00-614-803 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 52-30-00-010-801 52-30-00-410-801 71-00-00-720-816 78-31-00-710-804 12-36-29-991-096 12-36-29-991-079 12-36-29-991-081 12-36-29-991-080
Depressurization of the Yellow Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Opening of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Closing of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Test No. 2 - Engine Motor Leak Test (Dry Method) Thrust Reverser Cowl Doors Open Thrust Reverser Cycling Test (MCDU) Fig. 339 Fig. 340 Fig. 341 Fig. 342
3. __________ Job Set-up Subtask 12-36-29-861-064 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). Subtask 12-36-29-860-153 B. Aircraft Maintenance Configuration (1) Pressurize the Yellow hydraulic system (Ref. TASK 29-00-00-863-801). (2) Set the flap and slat control lever on the panel 114VU to the position 1. (3) On the ECAM engine/warning display the indication 1+F comes into view. (4) On the HYD section of the maintenance panel 285VU, make sure that the LEAK MEASUREMENT VALVES/Y pushbutton switch is pushed (the OFF legend is on).
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(5) On the Yellow HP manifold 7103JM, disconnect the pressure switches 7JS3 and 19CE3 and on the free end make a short circuit between the pin A and B with a plug type E0053R8B3APNE. (Ref. Fig. 339/TASK 12-36-29-991-096) Subtask 12-36-29-010-110-A C. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Put an access platform in position at the zone 147. (3) Put an access platform in position at the zone 196. (4) Remove the access panel 196EB. Subtask 12-36-29-680-058 D. Drain the reservoir of the Yellow hydraulic system (Ref. TASK 29-10-00611-803). Subtask 12-36-29-860-154 E. Set the hydraulic ground power supply to the correct configuration: (1) Make sure that the hydraulic ground power supply reservoir is filled with new HYDRAULIC FLUIDS (Material No. 02-003). (2) Make sure that no chlorinated solvent has been used to flush the tool lines. (3) Set the hydraulic ground power supply to the cart reservoir configuration. (4) Open the by-pass valve. (5) Start the hydraulic ground power supply. (6) Adjust the hydraulic ground power supply to the minimum pressure ( 20 bar (290.0754 psi) approx.) and to a flow of 45l/mn approx. and stop the hydraulic ground power supply.
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Manifolds of the Yellow Hydraulic System Figure 339/TASK 12-36-29-991-096 R EFF : ALL 12-36-29 SROS
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Subtask 12-36-29-860-155 F. Set the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the correct configuration. (Ref. Fig. 340/TASK 12-36-29-991-079, 341/TASK 12-36-29-991-081) NOTE : Make sure that the Yellow reservoir depressurization valve is open ____ when you set the hydraulic fluid replacement and recovery bench to the correct configuration. (1) On the fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501): - close the valve V1. (2) Connect the connector LP1 of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the LP connector of the hydraulic ground power supply. (3) Connect the HP1 connector of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the HP connector of the hydraulic ground power supply. (4) Connect the LP3 connector of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the suction connector of the ground service panel. (5) On the HP manifold 7103JM: (a) Remove the Yellow HP filter 5111JM3 (Ref. TASK 29-13-45-600-801). (b) Install a dummy bowl of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) in place of the Yellow HP filter 5111JM3. (c) Connect the HP2 line to the dummy bowl and to the valve V2. (6) On the LP filter 5011JM3: (a) Disconnect the tube (1) from the LP filter 5011JM3. (b) Put a blanking plug on the Yellow LP filter 5011JM3. (c) Loosen the tube (1) from the Yellow LP manifold 7005JM. (d) Turn the tube (1) on the Yellow LP manifold 7005JM, and connect the LP2 line.
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INTENTIONALLY BLANK
R 12-36-29 SROS
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Connections of Tools to the Yellow Hydraulic System Figure 340/TASK 12-36-29-991-079- 12 (SHEET 1) R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
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Connections of Tools to the Yellow Hydraulic System Figure 340/TASK 12-36-29-991-079- 22 (SHEET 2) R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
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Yellow Hydraulic System-Schematic Diagram Figure 341/TASK 12-36-29-991-081- 12 (SHEET 1) R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
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Yellow Hydraulic System-Schematic Diagram Figure 341/TASK 12-36-29-991-081- 22 (SHEET 2) R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
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(e) Tighten the tube (1) on the Yellow LP manifold 7005JM. (7) Start the hydraulic ground power supply and make sure that the pressure read on the gage of the hydraulic fluid replacement and recovery bench is 4 bar (58.0150 psi). (8) Stop the hydraulic ground power supply. 4. Procedure _________ (Ref. Fig. 341/TASK 12-36-29-991-081) Subtask 12-36-29-611-145 A. Fill the Yellow reservoir. (1) Open the depressurization valve of Yellow reservoir (Ref. TASK 29-1400-614-803). (2) Open the valve V1 of the TOOL - HYDRAULIC FLUID CHANGE (DH0501) and start the hydraulic ground power supply. (3) Fill the Yellow reservoir until the fluid is at the upper limit on the visual indicator (Ref. TASK 12-12-29-611-805). (4) Close the depressurization valve of Yellow reservoir. (5) Pressurize the Yellow hydraulic reservoir (Ref. TASK 29-14-00-614804). (6) Close the valve V1. Subtask 12-36-29-611-146 B. Replacement of the Fluid in the Engine Pump Suction and Pressure Lines (1) For 4030EM2 (a) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501) open the valve V1 and keep it open during the full procedure. (b) Dry motor the engine (Ref. TASK 71-00-00-720-816). NOTE : Stop the dry motoring if the advisory low level comes into ____ view on the ECAM SYSTEM DISPLAY. If necessary fill the Blue hydraulic reservoir (Ref. TASK 12-12-29-611-805).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
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(c) Dry motor the engine (Ref. TASK 71-00-00-720-816). (d) Open the valve V2 until you collect 40 liters of fluid. (e) Close the valve V2. (f) Stop the dry motoring. Subtask 12-36-29-611-147-A C. Replacement of the Fluid in the Suction, Pressure and Case Drain Lines of the Electric Pump (1JJ) (1) Disconnect the case drain tube from the electric pump (1JJ). (2) Put blanking plug on the end of the tube. (3) Connect the case drain elec hose of the TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the electric pump (1JJ). (4) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501): - make sure that the valve V1 is open. (5) On the HYD section of the overhead panel 245VU: - push the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (6) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501): - open the valve V2 until you collect 4 liters of fluid. (7) Close the valve V2. (8) On the HYD section of the overhead panel 245VU: - release the YELLOW/ELEC/AUTO pushbutton switch (6JJ). Subtask 12-36-29-611-148-A D. Replacement of the Fluid in the Thrust Reverser System (1) On the HYD section of the overhead panel 245VU: - push the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (2) Do two deploy-to-stow cycles of the thrust reverser (Ref. TASK 78-3100-710-804). (3) On the HYD section of the overhead panel 245VU: - release the YELLOW/ELEC/AUTO pushbutton switch (6JJ).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
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(4) On the panel 255VU: - Push the ENG2/FIRE pushbutton switch. (5) On the ECAM SD make sure that the fire shutoff valves are closed. Subtask 12-36-29-611-149-A E. Replacement of the Fluid in the Supply and Return Lines of the Primary Servocontrols (Ref. Fig. 342/TASK 12-36-29-991-080) (1) On the FLT CTL section of the overhead panel 212VU: - push the SEC2, PRIM2 and PRIM3 pushbutton switches. (2) On the FLT CTL section of the overhead panel 241VU: - push the SEC1 pushbutton switch. (3) On the ground service manifold 5109JM3 open the valves which supply the right and left wing. (Ref. Fig. 339/TASK 12-36-29-991-096) (4) On the HYD section of the overhead panel 245VU: - push the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (5) Do 5 operations over full travel range and make sure that the surfaces move. If they do not move, do the reset of the related computers. (6) On the HYD section of the overhead panel 245VU: - release the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (7) On the ground service manifold 5109JM3 close the valves for the right and left wing and open the valve for the aft fuselage. (8) On the HYD section of the overhead panel 245VU: - push the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (9) Operate the elevators over full travel range four times. (10) Operate the rudder over full travel range four times. (11) Operate the THS until you collect 5 liters of fluid. (12) On the HYD section of the overhead panel 245VU: - release the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (13) Close the valve for the aft fuselage.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B360 Jan 01/07
Flight Control Operations Figure 342/TASK 12-36-29-991-080 R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B361 Jan 01/07
Subtask 12-36-29-865-133 F. Make sure that this(these) circuit breaker(s) is(are) closed: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM 10CV X14 722VU SFCC 2 FLAP 2CV T43 742VU SFCC 1 FLAP 1CV L61 Subtask 12-36-29-611-150-A G. Replacement of the Fluid in the Flap and Slat Supply and Return Systems (1) Make sure that the flap and slat control lever on the panel 114VU is in the position 1. (2) On the ground service manifold 5109JM3 open the valves which supply the right and left wing. (3) On the HYD section of the overhead panel 245VU: - push the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (4) Set the flap and slat control lever on the panel 114VU to the position 2. (5) On the HYD section of the overhead panel 245VU: - release the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (6) On the ground service manifold 5109JM3 close the valves which supply the right and left wing. Subtask 12-36-29-611-151 H. Replacement of the Fluid in the Cargo Door Systems (1) Do 2 opening and closing cycles of the cargo doors (Ref. TASK 52-3000-010-801) and (Ref. TASK 52-30-00-410-801). 5. Close-up ________ Subtask 12-36-29-420-082 A. Replace these hydraulic filters: - the LP filter 5011JM3 (Ref. TASK 29-13-44-600-801) - the case drain filter 5013JM2 (Ref. TASK 29-11-43-600-804).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B362 Jan 01/07
Subtask 12-36-29-942-090 B. Aircraft Maintenance Configuration (1) On the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/Y pushbutton switch (the OFF legend is off). (2) On the Yellow HP manifold 7103JM, remove the plug type E0053R8B3APNE from the pressure switches 7JS3 and 19CE3 and connect the pressure switches 7JS3 and 19CE3. (3) On the panel 255VU: - release the ENG3/FIRE pushbutton switch. (4) Do the operational test of the electric motor of the engine pump suction fire shut-off valve (4JY) (Ref. TASK 29-10-00-710-805). (5) Close the valves V1 and V2 on the recovery bench. (6) Disconnect all the lines between the aircraft and the recovery bench. (7) Disconnect all the lines between the recovery bench and the hydraulic ground power supply. (8) Replace the HP hydraulic filter 5111JM3 (Ref. TASK 29-13-45-600-801). (9) Pressurize the Yellow hydraulic reservoir (Ref. TASK 29-14-00-614804). (10) Operate the flight controls and monitor the reservoir level. If necessary fill the Yellow hydraulic reservoir (Ref. TASK 12-12-29611-805). Each week, do a new sampling of fluid (Ref. TASK 12-32-29-281-801). Subtask 12-36-29-942-091 C. Remove the safety precautions (1) Remove the warning notice(s).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B363 Jan 01/07
Subtask 12-36-29-410-109 D. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Remove the access platform(s). (3) close the landing gear doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-862-094 E. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B364 Jan 01/07
**ON A/C 701-749, TASK 12-36-29-611-803-A Replacement of the Hydraulic Fluid of the Yellow Hydraulic System with a Fluid Replacement and Recovery Bench WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. CAUTION : DO NOT DEPRESSURIZE THE ENGINE PUMPS DURING THE DRY MOTORING. IF YOU _______ DO, YOU CAN CAUSE DAMAGE TO THE ENGINE PUMPS. 1. __________________ Reason for the Job You must replace the fluid only if the acidity is higher than the values given into the task of the sampling for analysis (Ref. TASK 12-32-29-281-80100).
EFF : 701-749, 12-36-29 R SROS
Page B365 Jan 01/07
2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific No specific No specific DH0501
blanking plug hydraulic ground power supply plug type E0053R8B3APNE access platform 1.8 m (5 ft. 11 in.) access platform 1.80 m (5 ft. 11 in.) 1 TOOL - HYDRAULIC FLUID CHANGE
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 02-003
F NSA 307110 TYPE 4 HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-805 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-863-801 29-10-00-611-803 29-10-00-710-805 29-11-43-600-809 29-13-44-600-801 29-13-45-600-801
Fill the Yellow Hydraulic Reservoir with a Hydraulic Service Cart Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Pressurize the Green Hydraulic System with the Ground Hydraulic Supply Drainage of the Yellow Hydraulic Reservoir Operational Test of the Electric Motor of the Engine Pump Suction Fire Shut-Off Valve Servicing of the Engine Pump Case Drain Filter (5013JM2) Servicing of the Yellow Reservoir LP-Filter (5011JM3) Servicing of the Yellow HP Filter (5111JM3)
EFF : 701-749, 12-36-29 R SROS
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-14-00-614-803 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 52-30-00-010-801 52-30-00-410-801 71-00-00-720-828 78-31-00-740-802 12-36-29-991-095 12-36-29-991-096 12-36-29-991-082 12-36-29-991-084 12-36-29-991-083
Depressurization of the Yellow Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Opening of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Closing of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Dry Motoring Engine Test of the Thrust Reverser Deployment and Stowage (Engine not Running) Fig. 332 Fig. 339 Fig. 343 Fig. 344 Fig. 345
3. __________ Job Set-up Subtask 12-36-29-861-067 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). Subtask 12-36-29-860-162 B. Aircraft Maintenance Configuration (1) Pressurize the Yellow hydraulic system (Ref. TASK 29-00-00-863-801). (2) Set the flap and slat control lever on the panel 114VU to the position 1. (3) On the ECAM Engine/Warning Display, the indication 1+F comes into view. (4) On the HYD section of the maintenance panel 285VU, make sure that the LEAK MEASUREMENT VALVES/Y pushbutton switch is pushed (the OFF legend is on).
EFF : 701-749, 12-36-29 R SROS
Page B367 Jan 01/07
(5) On the Yellow HP manifold 7103JM, disconnect the pressure switches 7JS3 and 19CE3, and on the free end make a short circuit between the pins A and B with a plug type E0053R8B3APNE. (Ref. Fig. 332/TASK 12-36-29-991-095) Subtask 12-36-29-010-113 C. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Put an access platform in position at the zone 147. (3) Put an access platform in position at the zone 196. (4) Remove the access panel 196AB. Subtask 12-36-29-680-061 D. Drain the reservoir of the Yellow hydraulic system (Ref. TASK 29-10-00611-803). Subtask 12-36-29-860-163 E. Set the hydraulic ground power supply to the correct configuration: (1) Make sure that the hydraulic ground power supply reservoir is filled with new HYDRAULIC FLUIDS (Material No. 02-003). (2) Make sure that no chlorinated solvent has been used to flush the tool lines. (3) Set the hydraulic ground power supply to the cart reservoir configuration. (4) Open the by-pass valve. (5) Start the hydraulic ground power supply. (6) Adjust the hydraulic ground power supply to the minimum pressure ( 20 bar (290.0754 psi) approx.) and to a flow of 45/lmn approx. and stop the hydraulic ground power supply.
EFF : 701-749, 12-36-29 R SROS
Page B368 Jan 01/07
Subtask 12-36-29-860-164 F. Set the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the correct configuration. (Ref. Fig. 343/TASK 12-36-29-991-082, 344/TASK 12-36-29-991-084) NOTE : Make sure that the Yellow reservoir depressurization valve is open ____ when you set the hydraulic fluid replacement and recovery bench to the correct configuration. (1) On the fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501): - close the valve V1. (2) Connect the connector LP1 of the hydraulic fluid replacement and recovery bench to the LP connector of the hydraulic ground power supply. (3) Connect the HP1 connector of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the HP connector of the hydraulic ground power supply. (4) Connect the LP3 connector of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the suction connector of the ground service panel. (5) On the HP manifold 7103JM (a) Remove the Yellow HP filter 5111JM3 (Ref. TASK 29-13-45-600-801). (b) Install a dummy bowl of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) in place on the Yellow HP filter 5111JM3. (c) Connect the HP2 line to the dummy bowl and to the valve V2. (6) On the LP filter 5011JM3: (a) Disconnect the tube (1) from the LP filter 5011JM3. (b) Put a blanking plug on the Yellow LP filter 5011JM3. (c) Loosen the tube (1) from the Yellow LP manifold 7005JM. (d) Turn the tube (1) on the Yellow LP manifold 7005JM, and connect the LP2 line.
EFF : 701-749, 12-36-29 R SROS
Page B369 Jan 01/07
Connections of Tools to the Yellow Hydraulic System Figure 343/TASK 12-36-29-991-082- 12 (SHEET 1) EFF : 701-749, 12-36-29 R SROS
Page B370 Jan 01/07
Connections of Tools to the Yellow Hydraulic System Figure 343/TASK 12-36-29-991-082- 22 (SHEET 2) R EFF : 701-749, 12-36-29 SROS
Page B371 Jan 01/07
Yellow Hydraulic System-Schematic Diagram Figure 344/TASK 12-36-29-991-084- 12 (SHEET 1) R EFF : 701-749, 12-36-29 SROS
Page B372 Jan 01/07
Yellow Hydraulic System-Schematic Diagram Figure 344/TASK 12-36-29-991-084- 22 (SHEET 2) R EFF : 701-749, 12-36-29 SROS
Page B373 Jan 01/07
(e) Tighten the tube (1) on the Yellow LP manifold 7005JM. (7) Start the hydraulic ground power supply and make sure that the pressure read on the gage of the hydraulic fluid replacement and recovery bench is 4 bar (58.0150 psi). (8) Stop the hydraulic ground power supply. 4. Procedure _________ (Ref. Fig. 344/TASK 12-36-29-991-084) Subtask 12-36-29-611-171 A. Fill the Yellow reservoir. (1) Open the depressurization valve of Yellow reservoir (Ref. TASK 29-1400-614-803). (2) Open the valve V1 of the TOOL - HYDRAULIC FLUID CHANGE (DH0501) and start the hydraulic ground power supply. (3) Fill the Yellow reservoir until the fluid is at the upper limit on the visual indicator (Ref. TASK 12-12-29-611-805). (4) Close the depressurization valve of Yellow reservoir. (5) Pressurize the Yellow hydraulic reservoir (Ref. TASK 29-14-00-614804). (6) Close the valve V1. Subtask 12-36-29-611-172 B. Replacement of the Fluid in the Engine Pump Suction and Pressure Lines (1) For 4030EM2 (a) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501) open the valve V1 and keep it open during the full procedure. (b) Dry motor the engine (Ref. TASK 71-00-00-720-828). NOTE : Stop the dry motoring if the advisory low level comes into ____ view on the ECAM SYSTEM DISPLAY. If necessary fill the Blue hydraulic reservoir (Ref. TASK 12-12-29-611-805).
R EFF : 701-749, 12-36-29 SROS
Page B374 Jan 01/07
(c) Dry motor the engine (Ref. TASK 71-00-00-720-828). (d) Open the valve V2 until you collect 40 liters of fluid. (e) Close the valve V2. (f) Stop the dry motoring. Subtask 12-36-29-611-173 C. Replacement of the Fluid in the Suction, Pressure and Case Drain Lines of the Electric Pump (1JJ) (1) Disconnect the case drain tube from the electric pump (1JJ). (2) Put blanking plug on the end of the tube. (3) Connect the case drain elec hose of the TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the electric pump (1JJ). (4) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501): - make sure that the valve V1 is open. (5) On the HYD section of the overhead panel 245VU: - push the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (6) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501): - open the valve V2 until you collect 4 liters of fluid. (7) Close the valve V2. (8) On the HYD section of the overhead panel 245VU: - release the YELLOW/ELEC/AUTO pushbutton switch (6JJ). Subtask 12-36-29-611-174 D. Replacement of the Fluid in the Thrust Reverser System (1) On the HYD section of the overhead panel 245VU: - push the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (2) Do two deploy-to-stow cycles of the thrust reverser (Ref. TASK 78-3100-740-802). (3) On the HYD section of the overhead panel 245VU: - release the YELLOW/ELEC/AUTO pushbutton switch (6JJ).
R EFF : 701-749, 12-36-29 SROS
Page B375 Jan 01/07
(4) On the panel 255VU: Push the ENG2 FIRE pushbutton switch. On the ECAM SD make sure that the fire shutoff valves are closed. Subtask 12-36-29-611-175 E. Replacement of the Fluid in the Supply and Return Lines of the Primary Servocontrols (Ref. Fig. 345/TASK 12-36-29-991-083) (1) On the FLT CTL section of the overhead panel 212VU: - push the SEC2 PRIM2 and PRIM3 pushbutton switches. (2) On the FLT CTL section of the overhead panel 241VU: - push the SEC1 pushbutton switch. (3) On the ground service manifold 5109JM3 open the valves which supply the right and left wing. (Ref. Fig. 339/TASK 12-36-29-991-096) (4) On the HYD section of the overhead panel 245VU: - push the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (5) Do 5 operations over full travel range and make sure that the surfaces move. If they do not move, do the reset of the related computers. (6) On the HYD section of the overhead panel 245VU: - release the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (7) On the ground service manifold 5109JM3 close the valves for the right and left wing and open the valve for the aft fuselage. (8) On the HYD section of the overhead panel 245VU: - push the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (9) Operate the elevators over full travel range four times. (10) Operate the rudder over full travel range four times. (11) Operate the THS until you collect 5 liters of fluid. (12) On the HYD section of the overhead panel 245VU: - release the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (13) Close the valve for the aft fuselage.
R EFF : 701-749, 12-36-29 SROS
Page B376 Jan 01/07
Flight Control Operations Figure 345/TASK 12-36-29-991-083 R EFF : 701-749, 12-36-29 SROS
Page B377 Jan 01/07
Subtask 12-36-29-865-139 F. Make sure that this(these) circuit breaker(s) is(are) closed: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM 10CV X14 722VU SFCC 2 FLAP 2CV T43 742VU SFCC 1 FLAP 1CV L61 Subtask 12-36-29-611-176 G. Replacement of the Fluid in the Flap and Slat Supply and Return Systems (1) Make sure that the flap and slat control lever on the panel 114VU is in the position 1. (2) On the ground service manifold 5109JM3 open the valves which supply the right and left wing. (3) On the ground service manifold 5109JM3 open the valves which supply the right and left wing. (4) On the HYD section of the overhead panel 245VU: - push the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (5) Set the flap and slat control lever on the panel 114VU to the position 2. (6) On the HYD section of the overhead panel 245VU: - release the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (7) On the ground service manifold 5109JM3 close the valves which supply the right and left wing. Subtask 12-36-29-611-177 H. Replacement of the Fluid in the Cargo Door Systems (1) Do 2 opening and closing cycles of the cargo doors (Ref. TASK 52-3000-010-801) and (Ref. TASK 52-30-00-410-801).
EFF : 701-749, 12-36-29 R SROS
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5. Close-up ________ Subtask 12-36-29-420-085 A. Replace these hydraulic filters: - the LP filter 5011JM3 (Ref. TASK 29-13-44-600-801) - the case drain filter 5013JM2 (Ref. TASK 29-11-43-600-809). Subtask 12-36-29-942-096 B. Aircraft Maintenance Configuration (1) On the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/Y pushbutton switch (the OFF legend is off). (2) On the Yellow HP manifold 7103JM, remove the plug type E0053R8B3APNE from the pressure switches 7JS3 and 19CE3 and connect the pressure switches 7JS3 and 19CE3. (3) On the panel 255VU: - release the ENG3/FIRE pushbutton switch. (4) Do the operational test of the electric motor of the engine pump suction fire shut-off valve (4JY) (Ref. TASK 29-10-00-710-805). (5) Close the valves V1 and V2 on the recovery bench. (6) Disconnect all the lines between the aircraft and the recovery bench. (7) Disconnect all the lines between the recovery bench and the hydraulic ground power supply. (8) Replace the HP hydraulic filter 5111JM3 (Ref. TASK 29-13-45-600-801). (9) Pressurize the Yellow hydraulic reservoir (Ref. TASK 29-14-00-614804). (10) Operate the flight controls and monitor the reservoir level. If necessary fill the Yellow hydraulic reservoir (Ref. TASK 12-12-29611-805). (11) Each week, do a new sampling of fluid (Ref. TASK 12-32-29-281-801).
R EFF : 701-749, 12-36-29 SROS
Page B379 Jan 01/07
Subtask 12-36-29-942-097 C. Remove the safety precautions. (1) Remove the warning notice(s). Subtask 12-36-29-410-112 D. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Remove the access platform(s). (3) Close the landing gear doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-862-097 E. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 701-749, 12-36-29 SROS
Page B380 Jan 01/07
**ON A/C ALL TASK 12-36-29-611-807 Replacement of the Hydraulic Fluid of the Green Hydraulic System with the Green Electric Pump WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job You must replace the fluid only if the acidity is higher than the values given into the task of the sampling for analysis (Ref. TASK 12-32-29-281-801).
EFF : ALL 12-36-29 R SROS
Page B381 Jan 01/07
2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R R
No specific No specific No specific No specific No specific No specific 98F12303001000 98F29103005001
blanking plug circuit breaker(s) safety clip(s) flexible hose plug type E0053R8B3APNE access platform 1.8 m (5 ft. 11 in.) container 100 l (26.4169 USgal) 1 HYDRAULIC CONNECTOR 1 TBD
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-801 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-863-801 29-10-00-611-801 29-11-43-600-802 29-11-43-600-807 29-11-44-600-801 29-11-45-600-801 29-14-00-614-804 32-11-15-400-801 32-12-00-010-801 32-12-00-410-801
Fill the Green Hydraulic Reservoir with a Hydraulic Service Cart Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Pressurize the Green Hydraulic System with the Electric Pump Drainage of the Green Hydraulic Reservoir Servicing of the (Forward) Engine-Pump Case-Drain Filter Element 5013JM1 Servicing of the Engine-Pump Case Drain Filter (5013JM1) Servicing of the Green Reservoir LP-Filter (5011JM1) Servicing of the Green HP Filter (5111JM101,5111JM102) Pressurization of the Hydraulic Reservoirs with external bench Installation of the MLG Bogie-Alignment Pitch Trimmer (Weight on Wheels) Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance
EFF : ALL 12-36-29 SROS
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-42-00-870-801
R R R
32-42-12-000-801 32-42-12-400-801 71-00-00-720-816 71-00-00-720-828 12-36-29-991-085
Bleeding the Normal Braking System at the Wheel Brakes Removal of the Hydraulic Brake Filter (5200GG) Installation of the Hydraulic Brake Filter (5200GG) Test No. 2 - Engine Motor Leak Test (Dry Method) Thrust Reverser Cowl Doors Open Dry Motoring Engine Fig. 346
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 12-36-29-991-086
Fig. 347
**ON A/C 701-749, 12-36-29-991-086-A
Fig. 347A
**ON A/C ALL 12-36-29-991-099 12-36-29-991-091
Fig. 348 Fig. 349
3. __________ Job Set-up Subtask 12-36-29-860-165 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Pressurize the Green hydraulic system (Ref. TASK 29-00-00-863-801). (3) On the panel 114VU, set the flap and slat control lever to the position 1. (4) On the ECAM Engine/Warning Display, the indication 1+F comes into view.
EFF : ALL 12-36-29 SROS
Page B383 Jan 01/07
(5) On the HYD section of the maintenance panel 285VU, make sure that the LEAK MEASUREMENT VALVES/G pushbutton switch is pushed (the OFF legend is on). (6) On the Green HP manifold 5103JM, disconnect the pressure switches 7JS1 and 19CE1. On the free end make a short circuit between the pins A and B with a plug type E0053R8B3APNE. Subtask 12-36-29-865-156 B. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------722VU HYD SOV ENG 2 NORM 19JG R34 722VU HYD SOV BUS SWTG 8JG R33 742VU HYD FIRE ENG 1 SOV 15JG2 D75 742VU HYD FIRE ENG 2 SOV 15JG1 D72 Subtask 12-36-29-010-114 C. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Put an access platform at the zone 147. Subtask 12-36-29-680-062 D. Drain the reservoir of the Green hydraulic system (Ref. TASK 29-10-00611-801). Subtask 12-36-29-420-090 R
E. Connection of the Flexible Hose to the LP Manifold 5004JM. (Ref. Fig. 346/TASK 12-36-29-991-085) **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, (Ref. Fig. 347/TASK 12-36-29-991-086)
EFF : ALL 12-36-29 SROS
Page B384 Jan 01/07
R
Hydraulic Connections for the Replacement of the Fluid Figure 346/TASK 12-36-29-991-085
EFF : ALL 12-36-29 SROS
Page B385 Jan 01/07
Green Hydraulic System-Schematic Diagram Figure 347/TASK 12-36-29-991-086 R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B386 Jan 01/07
**ON A/C 701-749, (Ref. Fig. 347A/TASK 12-36-29-991-086-A) **ON A/C ALL (1) On the LP filter 5011JM1: (a) Disconnect the tube (1) from the LP filter 5011JM1. (b) Put a blanking plug on the Green LP filter 5011JM1. (c) Loosen the tube (1) on the Green LP manifold 5004JM. (d) Turn the tube (1) 90 deg. and connect a flexible hose (2). R R R
(e) Connect at the end of the flexible hose (2) a TBD (98F29103005001) (3).
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(f) Tighten the tube (1) on the Green LP manifold 5004JM. (2) Put a container to collect the fluid. (3) Fill the Green hydraulic reservoir. (4) Pressurize the Green hydraulic reservoir (Ref. TASK 29-14-00-614804). Subtask 12-36-29-420-097 F. Connection of the Fill Cart Unit to the suction port 5132JM1. (Ref. Fig. 348/TASK 12-36-29-991-099) (1) Open the green ground service panel. (2) Connect the HYDRAULIC CONNECTOR (98F12303001000) to 5132JM1. (3) Connect the Fill Cart Unit to the adaptor 98F12303001000. (4) Operate the Fill Cart Unit. CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE FROM THE FILL UNIT CART _______ IS NOT MORE THAN 4 BARS (58.0150 PSI). TOO MUCH PRESSURE CAN CAUSE DAMAGE TO THE SYSTEM.
EFF : ALL 12-36-29 SROS
Page B387 Jan 01/07
Green Hydraulic System-Schematic Diagram Figure 347A/TASK 12-36-29-991-086-A R EFF : 701-749, 12-36-29 SROS
Page B388 Jan 01/07
Connection between the Fill Unit Cart and the Ground Service Panel Figure 348/TASK 12-36-29-991-099 EFF : ALL 12-36-29 R SROS
Page B389 Jan 01/07
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Operate the hydraulic service cart and monitor the increase of the fluid level on the reservoir hydraulic quantity indicator 5JS.
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(5) Stop the flow when the pointer is in the center position on the reservoir hydraulic quantity indicator 5JS. 4. Procedure _________ **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, (Ref. Fig. 347/TASK 12-36-29-991-086) **ON A/C 701-749, (Ref. Fig. 347A/TASK 12-36-29-991-086-A)
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**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499,
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Subtask 12-36-29-611-178-A
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A. Replacement of the Fluid in the Engine Pump Suction and Pressure Lines.
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NOTE : The quantity of fluid in the Green system is approximately 210 ____ liters. This procedure permits to replace approximately 90 percent of the fluid.
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(1) -For 4000EM1.
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(a) Dry motor the engine (Ref. TASK 71-00-00-720-816) until you collect 20 l (5.2833 USgal) approximately.
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NOTE : Stop the dry motoring if the advisory low level comes into ____ view on the ECAM system (SD). If necessary fill the reservoir.
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(b) Stop the dry motoring.
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(c) Repeat the dry motoring until you collect 45 l (11.8876 USgal) approximately.
EFF : ALL 12-36-29 SROS
Page B390 Jan 01/07
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(2) -For 4000EM2.
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(a) Dry motor the engine (Ref. TASK 71-00-00-720-816) until you collect 20 l (5.2833 USgal) approximately.
R R R
NOTE : Stop the dry motoring if the advisory low level comes into ____ view on the ECAM system (SD). If necessary fill the reservoir.
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(b) Stop the dry motoring.
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(c) Repeat the dry motoring until you collect 45 l (11.8876 USgal) approximately.
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**ON A/C 701-749,
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Subtask 12-36-29-611-178-B
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A. Replacement of the Fluid in the Engine Pump Suction and Pressure Lines.
R R R
NOTE : The quantity of fluid in the Green system is approximately 210 ____ liters. This procedure permits to replace approximately 90 percent of the fluid.
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(1) -For 4000EM1.
R R
(a) Dry motor the engine (Ref. TASK 71-00-00-720-828) until you collect 20 l (5.2833 USgal) approximately.
R R R
NOTE : Stop the dry motoring if the advisory low level comes into ____ view on the ECAM system (SD). If necessary fill the reservoir.
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(b) Stop the dry motoring.
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(c) Repeat the dry motoring until you collect 45 l (11.8876 USgal) approximately.
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(2) -For 4000EM2.
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(a) Dry motor the engine (Ref. TASK 71-00-00-720-828) until you collect 20 l (5.2833 USgal) approximately.
R R R
NOTE : Stop the dry motoring if the advisory low level comes into ____ view on the ECAM system (SD). If necessary fill the reservoir.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, 701-749, SROS
Page B391 Jan 01/07
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(b) Stop the dry motoring.
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(c) Repeat the dry motoring until you collect 45 l (11.8876 USgal) approximately.
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**ON A/C ALL Subtask 12-36-29-611-179-A B. Replacement of the Fluid in the Supply and Return Lines of the Primary Servocontrols (Ref. Fig. 349/TASK 12-36-29-991-091) (1) On the FLT CTL section of the panel 212VU, push the PRIM3 pushbutton switch (the OFF legend is off). (2) On the FLT CTL section of the panel 241VU, push the PRIM1 and SEC1 pushbutton switches (the OFF legend are off). (3) On the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/G pushbutton switch (the OFF legend is off). (4) On the ground service manifold (5109JM1), open the valves which supply the right and left wings. CAUTION : STOP THE OPERATION OF: _______ - THE HYDRAULIC USERS (FLIGHT CONTROLS, ETC.) - THE ELECTRIC PUMP WHEN THE FLUID LEVEL GETS TO THE MIDDLE OF THE AMBER ZONE. IF NOT, AIR CAN GET INTO THE HYDRAULIC SYSTEM AND CAUSE CAVITATION OF THE PUMP. (5) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV) (the ON legend is on). (6) Do 2 cycles over the full travel range and make sure that the surfaces move. If they do not move, do the reset of the related computers while the pump operates. (7) Monitor the level of the fluid in the Green reservoir. If necessary, fill the Green reservoir with the fill unit cart. (8) Do the steps (5) and (6) again and then do one more cycle.
EFF : ALL 12-36-29 SROS
Page B392 Jan 01/07
Flight Control Operations Figure 349/TASK 12-36-29-991-091 EFF : ALL 12-36-29 R SROS
Page B393 Jan 01/07
(9) On the HYD section of the overhead panel 245VU: - Release the GREEN/ELEC/AUTO pushbutton switch (8JV) (the ON legend is off).
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(10) On the ground service manifold (5109JM1), close the valves for the right and left wings and open the valve for the aft fuselage. (11) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV) (the ON legend is on). (12) Operate the elevators over the full travel range two times. (13) Monitor the level of the fluid in the Green reservoir. If necessary, fill the Green reservoir with the fill unit cart. (14) Do the steps (11) and (12) again. (15) Operate the rudder over the full travel range two times. (16) Monitor the level of the fluid in the Green reservoir. If necessary fill the Green reservoir with the fill unit cart. (17) Do the steps (14) and (15) again. (18) On the HYD section of the overhead panel 245VU: - Release the GREEN/ELEC/AUTO pushbutton switch (8JV) (the ON legend is off).
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(19) Close the valve for the aft fuselage. Subtask 12-36-29-865-157 C. Make sure that this(these) circuit breaker(s) is(are) closed: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM 10CV X14 721VU SFCC 1 NORM AVAIL 10CW X13 722VU SFCC 2 FLAP 2CV T43 722VU SFCC 2 SLAT 2CW V40 742VU SFCC 1 SLAT 1CW L62 742VU SFCC 1 FLAP 1CV L61
EFF : ALL 12-36-29 SROS
Page B394 Jan 01/07
Subtask 12-36-29-611-180-A D. Replacement of the Fluid in the Flap and Slat Supply and Return System CAUTION : STOP THE OPERATION OF: _______ - THE HYDRAULIC USERS (FLIGHT CONTROLS, ETC.) - THE ELECTRIC PUMP WHEN THE FLUID LEVEL GETS TO THE MIDDLE OF THE AMBER ZONE. IF NOT, AIR CAN GET INTO THE HYDRAULIC SYSTEM AND CAUSE CAVITATION OF THE PUMP. (1) On the panel 114VU, make sure that the flap and slat control lever is in the position 1. (2) Make sure that the level of the Green Hydraulic reservoir is at the maximum level. If necessary fill the Green hydraulic reservoir . (3) On the ground service manifold (5109JM1), open the valves which supply the right and left wings. (4) On the HYD section of the overhead panel 245VU: - Push the GREEN/ELEC/AUTO pushbutton switch (8JV).
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(5) On the panel 114VU, set the flap and slat control lever to the position 2. (6) Monitor the level of the fluid in the Green reservoir. If necessary fill the Green reservoir with the fill unit cart. (7) On the HYD section of the overhead panel 245VU: - Release the GREEN/ELEC/AUTO pushbutton switch (8JV).
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(8) On the ground service manifold (5109JM1), close the valves for the right and left wings. Subtask 12-36-29-611-181 E. Replacement of the Fluid in the Normal Braking System CAUTION : STOP THE OPERATION OF: _______ - THE HYDRAULIC USERS (FLIGHT CONTROLS, ETC.) - THE ELECTRIC PUMP WHEN THE FLUID LEVEL GETS TO THE MIDDLE OF THE AMBER ZONE. IF NOT, AIR CAN GET INTO THE HYDRAULIC SYSTEM AND CAUSE CAVITATION OF THE PUMP. (1) Push and release the brake pedals one time.
R EFF : ALL 12-36-29 SROS
Page B395 Jan 01/07
(2) Replace the hydraulic brake filter 5200GG on the manifold 5105JM (Ref. TASK 32-42-12-000-801) and (Ref. TASK 32-42-12-400-801). (3) Push and release the brake pedals 5 times. (4) Fill the Green hydraulic reservoir with the Fill Cart Unit. Subtask 12-36-29-611-182-A F. Replacement of the Fluid in the Nose Wheel Steering System CAUTION : STOP THE OPERATION OF: _______ - THE HYDRAULIC USERS (FLIGHT CONTROLS, ETC.) - THE ELECTRIC PUMP WHEN THE FLUID LEVEL GETS TO THE MIDDLE OF THE AMBER ZONE. IF NOT, AIR CAN GET INTO THE HYDRAULIC SYSTEM AND CAUSE CAVITATION OF THE PUMP. (1) On the HYD section of the overhead panel 245VU: - Push the GREEN/ELEC/AUTO pushbutton switch (8JV).
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(2) Operate the nose wheel steering over the full travel one time . (3) Monitor the level of the fluid in the Green reservoir. If necessary fill the Green hydraulic reservoir with the Fill Cart Unit. (4) Operate the nose wheel steering over full travel one time again. (5) On the HYD section of the overhead panel 245VU: - Release the GREEN/ELEC/AUTO pushbutton switch (8JV).
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Subtask 12-36-29-611-183-A G. Replacement of the Fluid in the Landing Gear Door System CAUTION : STOP THE OPERATION OF: _______ - THE HYDRAULIC USERS (FLIGHT CONTROLS, ETC.) - THE ELECTRIC PUMP WHEN THE FLUID LEVEL GETS TO THE MIDDLE OF THE AMBER ZONE. IF NOT, AIR CAN GET INTO THE HYDRAULIC SYSTEM AND CAUSE CAVITATION OF THE PUMP. (1) Remove the access platform from the zone 147. (2) Fill the Green hydraulic reservoir to the maximum level . (3) On the HYD section of the overhead panel 245VU: - Push the GREEN/ELEC/AUTO pushbutton switch (8JV).
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R EFF : ALL 12-36-29 SROS
Page B396 Jan 01/07
(4) Do 3 opening cycles of the NLG doors. (5) Monitor the level of the fluid in the Green reservoir. If necessary fill the Green hydraulic reservoir . (6) Do 3 opening cycles of the right MLG doors. (7) Monitor the level of the fluid in the Green reservoir. If necessary, fill the Green hydraulic reservoir . (8) Do 3 opening cycles of the left MLG doors. (9) Monitor the level of the fluid in the Green reservoir. If necessary fill the Green hydraulic reservoir . (10) On the HYD section of the overhead panel 245VU: - Release the GREEN/ELEC/AUTO pushbutton switch (8JV).
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(11) Install the access platform at the zone 147. 5. Close-up ________ **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 12-36-29-420-091 A. Connection of the hydraulic tube after replacement of the fluid R R
(1) Remove the flexible hose (2) and the restricting union (3). (2) Remove the blanking plug from the filter (5011JM1). (3) Loosen the tube (1), turn the tube 90 deg. and connect to the filter (5011JM1). (4) Tighten the tube (1) on the Green LP manifold (5004JM). (5) Replace these hydraulic filters: - the HP filters 5111JM101 and 5111JM102 (Ref. TASK 29-11-45-600801), - the LP filter 5011JM1 (Ref. TASK 29-11-44-600-801), - the two case drain filters 5013JM1 (Ref. TASK 29-11-43-600-802).
EFF : ALL 12-36-29 SROS
Page B397 Jan 01/07
**ON A/C 701-749, Subtask 12-36-29-420-091-A A. Connection of the hydraulic tube after replacement of the fluid R R
(1) Remove the flexible hose (2) and the restricting union (3). (2) Remove the blanking plug from the filter (5011JM1). (3) Loosen the tube (1), turn the tube 90 deg. and connect to the filter (5011JM1). (4) Tighten the tube (1) on the Green LP manifold (5004JM). (5) Replace these hydraulic filters: - the HP filters 5111JM101 and 5111JM102 (Ref. TASK 29-11-45-600801), - the LP filter 5011JM1 (Ref. TASK 29-11-44-600-801), - the two case drain filters 5013JM1 (Ref. TASK 29-11-43-600-807). **ON A/C ALL Subtask 12-36-29-020-059 B. Disconnect the Hydraulic Connector. (1) Disconnect the HYDRAULIC CONNECTOR (98F12303001000) from the port 5132JM1. (2) Disconnect the HYDRAULIC CONNECTOR (98F12303001000) from the Fill Cart Unit. Subtask 12-36-29-942-098 C. Aircraft Maintenance Configuration (1) On the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/G pushbutton switch (the OFF legend is off). (2) On the Green HP manifold 5103JM, remove the plug type E0053R8B3APNE from the pressure switches 7JS1 and 19CE1 and connect the pressure switches 7JS1 and 19CE1.
EFF : ALL 12-36-29 SROS
Page B398 Jan 01/07
Subtask 12-36-29-865-158 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 8JG, 19JG. Subtask 12-36-29-942-099 E. Aircraft Maintenance Configuration (1) If the fire shutoff valves close, do a reset of the C/B 5JR. (2) Do the bleeding of the Normal braking system (Ref. TASK 32-42-00-870801). (3) Do the bleeding of the pitch trimmer (Ref. TASK 32-11-15-400-801). (4) Fill the Green hydraulic reservoir (Ref. TASK 12-12-29-611-801). (5) Operate the flight controls and monitor the reservoir level. (6) Each week, do a new sampling of the fluid (Ref. TASK 12-32-29-281801). Subtask 12-36-29-410-113 F. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Remove the access platform(s). (3) Close the landing gear doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-862-098 G. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
EFF : ALL 12-36-29 R SROS
Page B399 Jan 01/07
TASK 12-36-29-611-808 Replacement of the Hydraulic Fluid of the Blue Hydraulic System with the Blue Electric Pump WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job You must replace the fluid only if the acidity is higher than the values given into the task of the sampling for analysis (Ref. TASK 12-32-29-281-80100).
EFF : ALL 12-36-29 R SROS
Page C300 Jan 01/07
2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R R
No specific No specific No specific No specific 98F12303001000 98F29103005001
blanking plug plug type E0053R8B3APNE access platform 1.8 m (5 ft. 11 in.) container 100 l (26.4169 USgal) 1 HYDRAULIC CONNECTOR 1 TBD
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-803 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-863-802 29-10-00-611-802 29-11-43-600-804 29-11-43-600-809 29-12-44-600-801 29-12-45-600-801 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 32-43-00-870-801 71-00-00-720-802 12-36-29-991-087
Fill the Blue Hydraulic Reservoir with a Hydraulic Service Cart Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Pressurize the Blue Hydraulic System with the Electric Pump Drainage of the Blue Hydraulic Reservoir Servicing of the (Aft) Engine-Pump Case-Drain Filter Element 5013JM2 Servicing of the Engine Pump Case Drain Filter (5013JM2) Servicing of the Blue Reservoir LP-Filter (5011JM2) Servicing of the Blue HP Filter (5111JM2) Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Bleeding the Alternate Braking System at the Wheel Brakes Dry Motoring Check Fig. 350
EFF : ALL 12-36-29 SROS
Page C301 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 12-36-29-991-088
Fig. 351
**ON A/C 701-749, 12-36-29-991-088-A
Fig. 351A
**ON A/C ALL 12-36-29-991-098 12-36-29-991-092
Fig. 352 Fig. 353
3. __________ Job Set-up Subtask 12-36-29-860-166 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-802). (3) On the panel 114VU, set the flap and slat control lever to the position 1. (4) On the ECAM Engine/Warning Display, the indication 1+F comes into view. (5) On the HYD section of the maintenance panel 285VU, make sure that the LEAK MEASUREMENT VALVES/B pushbutton switch is pushed (the OFF legend is on). (6) On the Blue HP manifold 6103JM, disconnect the pressure switches 7JS2 and 19CE2. On the free end make a short circuit between the pins A and B with a plug type E0053R8B3APNE.
EFF : ALL 12-36-29 R SROS
Page C302 Jan 01/07
Subtask 12-36-29-010-115 B. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Put an access platform at the zone 147. Subtask 12-36-29-680-063 C. Drain the reservoir of the Blue hydraulic system (Ref. TASK 29-10-00-611802). Subtask 12-36-29-420-092 R
D. Connection of the Flexible Hose to the LP Manifold 6005JM (Ref. Fig. 350/TASK 12-36-29-991-087) **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, (Ref. Fig. 351/TASK 12-36-29-991-088) **ON A/C 701-749, (Ref. Fig. 351A/TASK 12-36-29-991-088-A) **ON A/C ALL (1) On the LP filter 5011JM2: (a) Disconnect the flexible hose (2) from the Blue LP filter 5011JM2. (b) Put a blanking plug on the Blue LP filter 5011JM2.
R R R
(c) Connect at the end of the flexible hose (2) a TBD (98F29103005001) (3). (2) Put a container to collect the fluid. (3) Fill the Blue hydraulic reservoir (Ref. TASK 12-12-29-611-803). (4) Pressurize the Blue hydraulic reservoir (Ref. TASK 29-14-00-614-804).
EFF : ALL 12-36-29 SROS
Page C303 Jan 01/07
R
Hydraulic Connections for the Replacement of the Fluid Figure 350/TASK 12-36-29-991-087
EFF : ALL 12-36-29 SROS
Page C304 Jan 01/07
Blue Hydraulic System-Schematic Diagram Figure 351/TASK 12-36-29-991-088 R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page C305 Jan 01/07
Blue Hydraulic System-Schematic Diagram Figure 351A/TASK 12-36-29-991-088-A R EFF : 701-749, 12-36-29 SROS
Page C306 Jan 01/07
Subtask 12-36-29-420-098 E. Connection of the Fill Cart Unit to the suction port 5132JM2. (Ref. Fig. 352/TASK 12-36-29-991-098) (1) open the Blue ground service panel. (2) connect the HYDRAULIC CONNECTOR (98F12303001000) to the port 5132JM2 (3) connect the Fill Cart Unit to the HYDRAULIC CONNECTOR (98F12303001000). (4) operate the hydraulic service cart. CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE FROM THE FILL UNIT CART _______ IS NOT MORE THAN 4 BARS (58.0150 PSI). TOO MUCH PRESSURE CAN CAUSE DAMAGE TO THE SYSTEM. operate the hydraulic service cart and monitor the increase of the fluid level on the reservoir hydraulic quantity indicator 5JS. (5) stop the flow when the pointer is in the center position on the reservoir hydraulic quantity indicator 5JS. 4. Procedure _________ **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, (Ref. Fig. 351/TASK 12-36-29-991-088) **ON A/C 701-749, (Ref. Fig. 351A/TASK 12-36-29-991-088-A) **ON A/C ALL Subtask 12-36-29-611-184 A. Replacement of the Fluid in the Engine Pump Suction and Pressure Lines. NOTE : The quantity of fluid in the Blue system is approximately 150 ____ liters. This procedure permits to replace approximately 90 percent of the fluid.
EFF : ALL 12-36-29 R SROS
Page C307 Jan 01/07
Connection between the Fill Unit Cart and the Ground Service Panel Figure 352/TASK 12-36-29-991-098 EFF : ALL 12-36-29 R SROS
Page C308 Jan 01/07
(1) -FOR 4000EM2 (a) Dry motor the engine (Ref. TASK 71-00-00-720-802) until you collect 15 l (3.9625 USgal) NOTE : Stop the dry motoring if the advisory low level comes into ____ view on the ECAM system display (SD). If necessary fill the reservoir again. (b) Stop the dry motoring (c) Repeat the dry motoring until you collect 45 l (11.8876 USgal). Subtask 12-36-29-611-185 B. Replacement of the Fluid in the Supply and Return Lines of the Primary Servocontrols (Ref. Fig. 353/TASK 12-36-29-991-092) (1) On the panel 212VU, push the SEC2, PRIM2 and PRIM3 pushbutton switches (the OFF legend are off). (2) On the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/B pushbutton switch (the OFF legend is off). (3) On the ground service manifold 5109JM2 open the valves which supply the right and left wing. CAUTION : STOP THE OPERATION OF: _______ - THE HYDRAULIC USERS (FLIGHT CONTROLS, ETC.) - THE ELECTRIC PUMP WHEN THE FLUID LEVEL GETS TO THE MIDDLE OF THE AMBER ZONE. IF NOT, AIR CAN GET INTO THE HYDRAULIC SYSTEM AND CAUSE CAVITATION OF THE PUMP. (4) On the HYD section of the overhead panel 245VU: - push the BLUE/ELEC pushbutton switch (4JC) (the ON legend is on). (5) Do 2 cycles over the full travel range and make sure that the surfaces move. If they do not move, do the reset of the related computers while the pump operates. (6) Monitor the level of the fluid in the Blue reservoir. If necessary, fill the Blue hydraulic reservoir with the Fill Cart Unit. (7) Do the steps (4) and (5) again and then do one more cycle.
EFF : ALL 12-36-29 R SROS
Page C309 Jan 01/07
Flight Control Operations Figure 353/TASK 12-36-29-991-092 EFF : ALL 12-36-29 R SROS
Page C310 Jan 01/07
(8) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC) (the ON legend is off). (9) On the ground service manifold 5109JM2 close the valves for the right and left wing and open the valve for the aft fuselage. (10) On the HYD section of the overhead panel 245VU: - push the BLUE/ELEC pushbutton switch (4JC) (the ON legend is on). (11) Operate the elevators over the full travel range two times. (12) Monitor the level of the fluid in the Blue reservoir. If necessary fill the Blue hydraulic reservoir with the Fill Cart Unit. (13) Do the steps (8) and (9) again. (14) Operate the rudder over the full travel range two times. (15) Monitor the level of the fluid in the Blue reservoir. If necessary fill the Blue hydraulic reservoir (Ref. TASK 12-12-29-611-803). (16) Do the steps (11) and (12) again. (17) Operate the THS one time. (18) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC) (the ON legend is off). (19) Close the valve for the aft fuselage. Subtask 12-36-29-865-159 C. Make sure that this(these) circuit breaker(s) is(are) closed: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM AVAIL 10CW X13 722VU SFCC 2 SLAT 2CW V40 742VU SFCC 1 SLAT 1CW L62
R EFF : ALL 12-36-29 SROS
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Subtask 12-36-29-611-186 D. Replacement of the Fluid in the Slat Supply and Return System (Ref. Fig. 353/TASK 12-36-29-991-092) CAUTION : STOP THE OPERATION OF: _______ - THE HYDRAULIC USERS (FLIGHT CONTROLS, ETC.) - THE ELECTRIC PUMP WHEN THE FLUID LEVEL GETS TO THE MIDDLE OF THE AMBER ZONE. IF NOT, AIR CAN GET INTO THE HYDRAULIC SYSTEM AND CAUSE CAVITATION OF THE PUMP. (1) On the panel 114VU, make sure that the flap and slat control lever is in the position 1. (2) Make sure that the level of the Blue hydraulic reservoir is at the maximum level. If necessary fill the Blue hydraulic reservoir with the Fill Cart Unit. (3) On the ground service manifold 5109JM2 open the valves which supply the right and left wing. (4) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC). (5) On the panel 114VU, set the flap and slat control lever to the position 2. (6) Monitor the level of the fluid in the Blue reservoir. If necessary fill the Blue hydraulic reservoir with the Fill Cart Unit. (7) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC). (8) On the ground service manifold 5109JM2 close the valves for the right and left wing. Subtask 12-36-29-611-187 E. Replacement of the Fluid in the Alternate Brake System CAUTION : STOP THE OPERATION OF: _______ - THE HYDRAULIC USERS (FLIGHT CONTROLS, ETC.) - THE ELECTRIC PUMP WHEN THE FLUID LEVEL GETS TO THE MIDDLE OF THE AMBER ZONE. IF NOT, AIR CAN GET INTO THE HYDRAULIC SYSTEM AND CAUSE CAVITATION OF THE PUMP.
R EFF : ALL 12-36-29 SROS
Page C312 Jan 01/07
(1) On the PARK BRK control panel 117VU, set the PARK BRK switch to the OFF position. (2) On the HYD section of the panel 245VU: - push the BLUE/ELEC pushbutton switch (4JC). (3) Push and release the brake pedals five times. (4) On the HYD section of the panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC). 5. Close-up ________ **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 12-36-29-420-093 A. Connection of the hydraulic tube after replacement of the fluid R R
(1) Remove the flexible hose (2) and the restricting union (3). (2) Remove the blanking plug from the filter (5011JM2). (3) Connect the flexible hose to the filter (5011JM2). (4) Replace these hydraulic - the HP filter 5111JM2 - the LP filter 5011JM2 - the case drain filter
filters: (Ref. TASK 29-12-45-600-801), (Ref. TASK 29-12-44-600-801), 5013JM2 (Ref. TASK 29-11-43-600-804).
**ON A/C 701-749, Subtask 12-36-29-420-093-A A. Connection of the hydraulic tube after replacement of the fluid R R
(1) Remove the flexible hose (2) and the restricting union (3). (2) Remove the blanking plug from the filter (5011JM2). (3) Connect the flexible hose to the filter (5011JM2).
EFF : ALL 12-36-29 SROS
Page C313 Jan 01/07
(4) Replace these hydraulic - the HP filter 5111JM2 - the LP filter 5011JM2 - the case drain filter
filters: (Ref. TASK 29-12-45-600-801), (Ref. TASK 29-12-44-600-801), 5013JM2 (Ref. TASK 29-11-43-600-809).
**ON A/C ALL Subtask 12-36-29-020-057 B. Disconnect the Hydraulic Connector. (1) Disconnect the HYDRAULIC CONNECTOR (98F12303001000) from the port 5132JM2. (2) Disconnect the HYDRAULIC CONNECTOR (98F12303001000) from the Fill Cart Unit. Subtask 12-36-29-942-101 C. Aircraft Maintenance Configuration (1) On the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/B pushbutton switch (the OFF legend is off). (2) On the Blue HP manifold 6103JM, remove the plug type E0053R8B3APNE from the pressure switches 7JS2 and 19CE2 and connect the pressure switches 7JS2 and 19CE2. (3) Do the bleeding of the alternate brake system (Ref. TASK 32-43-00870-801). (4) Fill the Blue hydraulic reservoir (Ref. TASK 12-12-29-611-803). (5) Operate the flight controls and monitor the reservoir level. If necessary fill the Blue hydraulic reservoir (Ref. TASK 12-12-29-611803). (6) Each week, do a new sampling of the fluid (Ref. TASK 12-32-29-281801).
EFF : ALL 12-36-29 R SROS
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Subtask 12-36-29-410-114 D. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Remove the access platform(s). (3) Close the landing gear doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-862-099 E. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
EFF : ALL 12-36-29 R SROS
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TASK 12-36-29-611-809 Replacement of the Hydraulic Fluid of the Yellow Hydraulic System with the Yellow Electric Pump WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job You must replace the fluid only if the acidity is higher than the values given into the task of the sampling for analysis (Ref. TASK 12-32-29-281-80100).
EFF : ALL 12-36-29 R SROS
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2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R R
No specific No specific No specific No specific No specific 98F12303001000 98F29103005001
blanking plug flexible hose plug type E0053R8B3APNE access platform 1.8 m (5 ft. 11 in.) container 100 l (26.4169 USgal) 2 HYDRAULIC CONNECTOR 1 TBD
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-863-803 29-10-00-611-803 29-11-43-600-804 29-11-43-600-809 29-13-44-600-801 29-13-45-600-801 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 52-30-00-010-801 52-30-00-410-801 71-00-00-720-802 12-36-29-991-089
Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Pressurize the Yellow Hydraulic System with the Electric Pump Drainage of the Yellow Hydraulic Reservoir Servicing of the (Aft) Engine-Pump Case-Drain Filter Element 5013JM2 Servicing of the Engine Pump Case Drain Filter (5013JM2) Servicing of the Yellow Reservoir LP-Filter (5011JM3) Servicing of the Yellow HP Filter (5111JM3) Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Opening of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Closing of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Dry Motoring Check Fig. 354
EFF : ALL 12-36-29 SROS
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 12-36-29-991-090
Fig. 355
**ON A/C 701-749, 12-36-29-991-090-A
Fig. 355A
**ON A/C ALL 12-36-29-991-097 12-36-29-991-093
Fig. 356 Fig. 357
3. __________ Job Set-up Subtask 12-36-29-860-167 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Pressurize the Yellow hydraulic system (Ref. TASK 29-00-00-863-803). (3) On the panel 114VU, set the flap and slat control lever to the position 1. (4) On the ECAM Engine/Warning Display, the indication 1+F comes into view. (5) On the HYD section of the maintenance panel 285VU, make sure that the LEAK MEASUREMENT VALVES/Y pushbutton switch is pushed (the OFF legend is on). (6) On the Yellow HP manifold 7103JM, disconnect the pressure switches 7JS3 and 19CE3. On the free end make a short circuit between the pins A and B with a plug type E0053R8B3APNE.
EFF : ALL 12-36-29 R SROS
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Subtask 12-36-29-010-116 B. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Put an access platform at the zone 147. Subtask 12-36-29-680-064 C. Drain the Reservoir of the Yellow Hydraulic System (Ref. TASK 29-10-00611-803) Subtask 12-36-29-420-094 R
D. Connection of the Flexible Hose to the LP Filter 5011JM3 (Ref. Fig. 354/TASK 12-36-29-991-089) **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, (Ref. Fig. 355/TASK 12-36-29-991-090) **ON A/C 701-749, (Ref. Fig. 355A/TASK 12-36-29-991-090-A) **ON A/C ALL (1) On the LP filter 5011JM3: (a) Disconnect the hose (1) from the LP filter 5011JM3. (b) Put a blanking plug on the hose (1). (c) Connect the flexible hose (2) to the LP filter 5011JM3.
R R R
(d) Connect at the end of the flexible hose (2) a TBD (98F29103005001) (3). (2) Put a container to collect the fluid. (3) Fill the Yellow hydraulic reservoir at the maximum level with the Fill Cart Unit.
EFF : ALL 12-36-29 SROS
Page C319 Jan 01/07
R
Hydraulic Connections for the Replacement of the Fluid Figure 354/TASK 12-36-29-991-089
EFF : ALL 12-36-29 SROS
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Yellow Hydraulic System-Schematic Diagram Figure 355/TASK 12-36-29-991-090 R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page C321 Jan 01/07
Yellow Hydraulic System-Schematic Diagram Figure 355A/TASK 12-36-29-991-090-A R EFF : 701-749, 12-36-29 SROS
Page C322 Jan 01/07
(4) Pressurize the Yellow hydraulic reservoir (Ref. TASK 29-14-00-614804). Subtask 12-36-29-420-096 E. Connection of the FILL CART UNIT to the suction port 5132JM3. (Ref. Fig. 356/TASK 12-36-29-991-097) (1) Open the yellow ground service panel. (2) Connect the HYDRAULIC CONNECTOR (98F12303001000) to the 5132JM3. (3) Connect the FILL CART UNIT to the adaptor HYDRAULIC CONNECTOR (98F12303001000). (4) Operate the hydraulic service cart. CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE FROM THE FILL UNIT CART _______ IS NOT MORE THAN 4 BARS (58.0150 PSI). TOO MUCH PRESSURE CAN CAUSE DAMAGE TO THE SYSTEM. Operate the hydraulic service cart and monitor the increase of the fluid level in the reservoir hydraulic quantity indicator 5JS. (5) Stop the flow when the pointer is in the center position on the reservoir hydraulic quantity indicator 5JS. 4. Procedure _________ (Ref. Fig. 354/TASK 12-36-29-991-089) **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, (Ref. Fig. 355/TASK 12-36-29-991-090) **ON A/C 701-749, (Ref. Fig. 355A/TASK 12-36-29-991-090-A)
EFF : ALL 12-36-29 R SROS
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Connection between the Fill Unit Cart and the Ground Service Panel Figure 356/TASK 12-36-29-991-097 EFF : ALL 12-36-29 R SROS
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**ON A/C ALL Subtask 12-36-29-611-188 A. Replacement of the Fluid in the Engine Pump Suction and Pressure lines. NOTE : The quantity of fluid in the Yellow system is approximately 110 ____ liters. This procedure permits to replace approximately 90 percent of the fluid. (1) -For 4000EM3 (a) Dry motor the engine (Ref. TASK 71-00-00-720-802) until you collect 13l approximately. NOTE : Stop the dry motoring if the advisory low level comes into ____ view on the ECAM system display. (b) If necessary fill the reservoir again. (c) Repeat the dry motoring until you collect 40l approximately. Subtask 12-36-29-611-189-A B. Replacement of the Fluid in the Supply and Return Lines of the Primary Servocontrols (Ref. Fig. 357/TASK 12-36-29-991-093) (1) On the FLT CTL section of the panel 212VU, push the SEC2, PRIM2 and PRIM3 pushbutton switches (the OFF legend are off). (2) On the FLT CTL section of the panel 241VU, push the SEC1 pushbutton switch (the OFF legend is off). (3) On the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/Y pushbutton switch (the OFF legend is off). (4) On the ground service manifold (5109JM3), open the valves which supply the right and left wings. CAUTION : STOP THE OPERATION OF: _______ - THE HYDRAULIC USERS (FLIGHT CONTROLS, ETC.) - THE ELECTRIC PUMP WHEN THE FLUID LEVEL GETS TO THE MIDDLE OF THE AMBER ZONE. IF NOT, AIR CAN GET INTO THE HYDRAULIC SYSTEM AND CAUSE CAVITATION OF THE PUMP.
R EFF : ALL 12-36-29 SROS
Page C325 Jan 01/07
Flight Control Operations Figure 357/TASK 12-36-29-991-093 EFF : ALL 12-36-29 R SROS
Page C326 Jan 01/07
(5) On the HYD section of the overhead panel 245VU: - push the YELLOW/ELEC/AUTO pushbutton switch (6JJ) (the ON legend is on). (6) Do 2 cycles over the full travel range and make sure that the surfaces move. If they do not move, do the reset of the related computers while the pump is operates. (7) Monitor the level of the fluid in the Yellow reservoir. If necessary fill the Yellow reservoir. (8) Do the steps (5) and (6) again and then do one more cycle. (9) On the HYD section of the overhead panel 245VU: - release the YELLOW/ELEC/AUTO pushbutton switch (6JJ) (the ON legend is off). (10) On the ground service manifold (5109JM3), close the valves for the right and left wings and open the valves for the aft fuselage. (11) On the HYD section of the overhead panel 245VU: - push the YELLOW/ELEC/AUTO pushbutton switch (6JJ) (the ON legend is on). (12) Operate the elevators over the full travel range two times. (13) Monitor the level of the fluid in the Yellow reservoir. If necessary fill the Yellow reservoir with the fill unit cart. (14) Do the steps (11) and (12) again. (15) Operate the rudder over the full travel range two times. (16) Monitor the level of the fluid in the Yellow reservoir. If necessary fill the Yellow reservoir with the fill unit cart. (17) Do the steps (14) and (15) again. (18) Operate the THS one time. (19) On the HYD section of the overhead panel 245VU: - release the YELLOW/ELEC/AUTO pushbutton switch (6JJ) (the ON legend is off). (20) Close the valve for the aft fuselage.
EFF : ALL 12-36-29 R SROS
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Subtask 12-36-29-865-160 C. Make sure that this(these) circuit breaker(s) is(are) closed: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM 10CV X14 722VU SFCC 2 FLAP 2CV T43 742VU SFCC 1 FLAP 1CV L61 Subtask 12-36-29-611-190-A D. Replacement of the Fluid in the Flap Supply and Return System (Ref. Fig. 357/TASK 12-36-29-991-093) CAUTION : STOP THE OPERATION OF: _______ - THE HYDRAULIC USERS (FLIGHT CONTROLS, ETC.) - THE ELECTRIC PUMP WHEN THE FLUID LEVEL GETS TO THE MIDDLE OF THE AMBER ZONE. IF NOT, AIR CAN GET INTO THE HYDRAULIC SYSTEM AND CAUSE CAVITATION OF THE PUMP. (1) On the panel 114VU, make sure that the flap and slat control lever is in the position 1. (2) Make sure that the level of the Yellow reservoir is at the maximum level. If necessary fill the Yellow reservoir with the fill unit cart. (3) On the ground service manifold (5109JM3), open the valves which supply the right and the left wings. (4) On the HYD section of the overhead panel 245VU: - release the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (5) On the panel 114VU, set the flap and slat control lever to the position 2. (6) Monitor the level of the fluid in the Yellow reservoir. If necessary fill the Yellow reservoir with the fill unit cart. (7) On the HYD section of the overhead panel 245VU: - release the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (8) On the ground service manifold (5109JM3), close the valves for the right and left wings.
EFF : ALL 12-36-29 R SROS
Page C328 Jan 01/07
Subtask 12-36-29-611-191 E. Replacement of the Fluid in the Cargo Doors System CAUTION : STOP THE OPERATION OF: _______ - THE HYDRAULIC USERS (FLIGHT CONTROLS, ETC.) - THE ELECTRIC PUMP WHEN THE FLUID LEVEL GETS TO THE MIDDLE OF THE AMBER ZONE. IF NOT, AIR CAN GET INTO THE HYDRAULIC SYSTEM AND CAUSE CAVITATION OF THE PUMP. Do one opening and closing cycle of the cargo doors (Ref. TASK 52-30-00010-801) and (Ref. TASK 52-30-00-410-801). 5. Close-up ________ **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 12-36-29-420-095 A. Connection of the hydraulic tube after replacement of the fluid (1) Remove the flexible hose (2) from the LP filter 5011JM3. (2) Remove the blanking plug from the hose (1). (3) Connect the hose (1) to the LP filter 5011JM3. (4) Replace these hydraulic - the HP filter 5111JM3 - the LP filter 5011JM3 - the case drain filter
filters: (Ref. TASK 29-13-45-600-801), (Ref. TASK 29-13-44-600-801), 5013JM2 (Ref. TASK 29-11-43-600-804).
**ON A/C 701-749, Subtask 12-36-29-420-095-A A. Connection of the hydraulic tube after replacement of the fluid (1) Remove the flexible hose (2) from the LP filter 5011JM3. (2) Remove the blanking plug from the hose (1). (3) Connect the hose (1) to the LP filter 5011JM3.
EFF : ALL 12-36-29 R SROS
Page C329 Jan 01/07
(4) Replace these hydraulic - the HP filter 5111JM3 - the LP filter 5011JM3 - the case drain filter
filters: (Ref. TASK 29-13-45-600-801), (Ref. TASK 29-13-44-600-801), 5013JM2 (Ref. TASK 29-11-43-600-809).
**ON A/C ALL Subtask 12-36-29-020-058 B. Disconnect the Hydraulic Connector. (1) Disconnect the HYDRAULIC CONNECTOR (98F12303001000) from the port 5132JM3. (2) Disconnect the HYDRAULIC CONNECTOR (98F12303001000) from the Fill Cart Unit. Subtask 12-36-29-942-103 C. Get Access (1) On the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/Y pushbutton switch (the OFF legend is off). (2) On the Yellow HP manifold 7103JM, remove the plug type E0053R8B3APNE from the pressure switches 7JS3 and 19CE3 and connect the pressure switches 7JS3 and 19CE3. (3) Fill the Yellow hydraulic reservoir with the Fill Cart Unit. (4) Operate the flight controls and monitor the reservoir level. If necessary fill the Yellow hydraulic reservoir with the Fill Cart Unit. (5) Each week, do a new sampling of the fluid (Ref. TASK 12-32-29-281801). Subtask 12-36-29-410-115 D. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Remove the access platform(s).
R EFF : ALL 12-36-29 SROS
Page C330 Jan 01/07
(3) Close the landing gear doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-862-100 E. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
EFF : ALL 12-36-29 R SROS
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TASK 12-36-29-611-804 Reclaim the Fluid in the Green Hydraulic System WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. 1. __________________ Reason for the Job Clean the fluid when the rate of particle contamination is higher than the values of NSA 307-110 class 9 (Ref. TASK 12-32-29-281-80100). 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
ground hydraulic supply hydraulic ground power supply access platform 1.8 m (5 ft. 11 in.)
EFF : ALL 12-36-29 R SROS
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B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-801 12-12-29-611-802 12-32-29-281-801 24-41-00-861-801 29-00-00-280-801 29-00-00-280-801 29-00-00-863-801 29-00-00-864-801 29-10-00-200-804 29-10-00-200-806 29-10-00-200-806 29-14-00-614-804 31-60-00-860-801 32-12-00-010-801 32-12-00-410-801 78-31-11-200-801 78-31-41-200-802
Fill the Green Hydraulic Reservoir with a Hydraulic Service Cart Fill the Green Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A Check of the Green Hydraulic System after Operation of the Engine Pumps in Possible Starvation or Cavitation condition. Check of the Green Hydraulic System after Operation of the Engine Pumps in Possible Starvation or Cavitation Condition. Pressurize the Green Hydraulic System with the Ground Hydraulic Supply Depressurize the Green Hydraulic System (Pressurized with the Hydraulic Ground Supply) Check of the Clogging Indicators of the Hydraulic System Filter in the Hydraulics Compartment. Check of the Clogging Indicators of the Hydraulic System Filters on the Engines. Check of the Clogging Indicators of the Hydraulic System Filters on the Engines. Pressurization of the Hydraulic Reservoirs with external bench EIS Start Procedure Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Inspection of the Hydraulic Filter Assembly Element Inspection of the Thrust Reverser Isolation Control Unit
3. __________ Job Set-up Subtask 12-36-29-861-056 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801).
EFF : ALL 12-36-29 R SROS
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Subtask 12-36-29-860-132 B. Aircraft Maintenance Configuration (1) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00860-801). (2) On the ECAM control panel, push the HYD key (on the SD the HYD page comes into view). (3) On the SD make sure that: - the LO AIR PRESS indication of the Green reservoir is not shown. If it is shown, pressurize the reservoir (Ref. TASK 29-14-00-614-804). - the level index of the Green reservoir shows that the fluid level is correct. If the level of the fluid is not correct add fluid with a service cart or with a hand pump (Ref. TASK 12-12-29-611-801), (Ref. TASK 12-12-29-611-802). (4) Connect the suction and delivery lines of the hydraulic ground power supply to the aircraft connectors, access door 197CB: - 5132JM1 suction - 5131JM1 delivery. Subtask 12-36-29-010-102 C. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Put an access platform in position at the zone 147. 4. Procedure _________ **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 12-36-29-611-100 A. Clean the Fluid in the Green Hydraulic System NOTE : If the fluid is contaminated because of engine pump deterioration, ____ do the procedure for the check of the Green hydraulic system after operation of the engine pump in possible cavitation condition (Ref. TASK 29-00-00-280-801). (1) Pressurize the system that you must clean with the ground hydraulic supply (Ref. TASK 29-00-00-863-801).
EFF : ALL 12-36-29 R SROS
Page C334 Jan 01/07
(2) Operate all the flight controls and brakes to make a fluid flow in the system. (3) Do a fluid sampling for particle contamination (Ref. TASK 12-32-29281-801). (4) Continue to operate the flight controls and the brakes until you get a sample that is correct (contamination lower than NSA 307-110 class 9). (5) Do a check of the clogging indicator of: - the case drain filter 5013JM1 (Ref. TASK 29-10-00-200-806), - the HP filters 5111JM101, 5111JM102 (Ref. TASK 29-10-00-200-804), - the LP filter 5011JM1 (Ref. TASK 29-10-00-200-804), - the HCU filter 5001EG1 (Ref. TASK 78-31-11-200-801). **ON A/C 701-749, Subtask 12-36-29-611-100-A A. Clean the Fluid in the Green Hydraulic System NOTE : If the fluid is contaminated because of engine pump deterioration, ____ do the procedure for the check of the Green hydraulic system after operation of the engine pump in possible cavitation condition (Ref. TASK 29-00-00-280-801). (1) Pressurize the system that you must clean with the ground hydraulic supply (Ref. TASK 29-00-00-863-801). (2) Operate all the flight controls and brakes to make a fluid flow in the system. (3) Do a fluid sampling for particle contamination (Ref. TASK 12-32-29281-801). (4) Continue to operate the flight controls and the brakes until you get a sample that is correct (contamination lower than NSA 307-110 class 9). (5) Do a check of the clogging indicator of: - the case drain filter 5013JM1 (Ref. TASK 29-10-00-200-806), - the HP filters 5111JM101, 5111JM102 (Ref. TASK 29-10-00-200-804), - the LP filter 5011JM1 (Ref. TASK 29-10-00-200-804), - the filter element installed on the Isolation Control Unit 4117KS (Ref. TASK 78-31-41-200-802).
EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, 701-749, R SROS
Page C335 Jan 01/07
**ON A/C ALL 5. Close-up ________ Subtask 12-36-29-864-050 A. Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). Subtask 12-36-29-860-133 B. Disconnect the suction and delivery lines of the hydraulic ground power supply from the aircraft connectors, access door 197CB: - 5132JM1 suction - 5131JM1 delivery. Subtask 12-36-29-410-101 C. Close Access (1) Close the MLG doors (Ref. TASK 32-12-00-410-801) (2) Remove the access platform(s).
EFF : ALL 12-36-29 R SROS
Page C336 Jan 01/07
TASK 12-36-29-611-805 Reclaim the Fluid in the Blue Hydraulic System WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. 1. __________________ Reason for the Job Clean the fluid when the rate of particle contamination is higher than the values of NSA 307-110 class 9 (Ref. TASK 12-32-29-281-80100). 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
ground hydraulic supply hydraulic ground power supply access platform 1.8 m (5 ft. 11 in.)
EFF : ALL 12-36-29 R SROS
Page C337 Jan 01/07
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-803 12-12-29-611-804 12-32-29-281-801 24-41-00-861-801 29-00-00-280-802 29-00-00-280-802 29-00-00-863-802 29-00-00-864-802 29-10-00-200-804 29-10-00-200-806 29-10-00-200-806 29-14-00-614-804 31-60-00-860-801 32-12-00-010-801 32-12-00-410-801 78-31-11-200-801 78-31-41-200-802
Fill the Blue Hydraulic Reservoir with a Hydraulic Service Cart Fill the Blue Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A Check of the Blue Hydraulic System after Operation of the Engine Pump in Possible Starvation or Cavitation Condition. Check of the Blue Hydraulic System after Operation of the Engine Pump in Possible Starvation or Cavitation Condition. Pressurize the Blue Hydraulic System with the Ground Hydraulic Supply Depressurize the Blue Hydraulic System (Pressurized with the Hydraulic Ground Supply) Check of the Clogging Indicators of the Hydraulic System Filter in the Hydraulics Compartment. Check of the Clogging Indicators of the Hydraulic System Filters on the Engines. Check of the Clogging Indicators of the Hydraulic System Filters on the Engines. Pressurization of the Hydraulic Reservoirs with external bench EIS Start Procedure Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Inspection of the Hydraulic Filter Assembly Element Inspection of the Thrust Reverser Isolation Control Unit
3. __________ Job Set-up Subtask 12-36-29-861-057 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801).
EFF : ALL 12-36-29 R SROS
Page C338 Jan 01/07
Subtask 12-36-29-860-134 B. Aircraft Maintenance Configuration (1) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00860-801). (2) On the ECAM control panel, push the HYD key (on the SD the HYD page comes into view). (3) On the SD make sure that: - the LO AIR PRESS indication of the Blue reservoir is not shown. If it is shown, pressurize the reservoir (Ref. TASK 29-14-00-614-804), - the level index of the Blue reservoir shows that the fluid level is correct. If the level of the fluid is not correct add fluid with a service cart or with a hand pump (Ref. TASK 12-12-29-611-803), (Ref. TASK 12-12-29-611-804). (4) Connect the suction and delivery lines of the hydraulic ground power supply to the aircraft connectors, access door 195BB: - 5132JM2 suction - 5131JM2 delivery. Subtask 12-36-29-010-103 C. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Put an access platform in position at the zone 195. 4. Procedure _________ **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 12-36-29-611-101 A. Clean the Fluid in the Blue Hydraulic System NOTE : If the fluid is contaminated because of engine pump deterioration, ____ do the procedure for the check of the Blue hydraulic system after operation of the engine pump in possible cavitation condition (Ref. TASK 29-00-00-280-802). (1) Pressurize the system that you must clean with the ground hydraulic supply (Ref. TASK 29-00-00-863-802).
EFF : ALL 12-36-29 R SROS
Page C339 Jan 01/07
(2) Operate all the flight controls and brakes to make a fluid flow in the system. (3) Do a fluid sampling for particle contamination (Ref. TASK 12-32-29281-801). (4) Continue to operate the flight controls and the brakes until you get a sample that is correct (contamination lower than NSA 307-110 class 9). (5) Do a check of the clogging indicator of: - the case drain filter 5013JM2 (Ref. TASK 29-10-00-200-806), - the HP filter 5111JM2 (Ref. TASK 29-10-00-200-804), - the LP filter 5011JM1 (Ref. TASK 29-10-00-200-804), - the HCU filter 5001EG2 (Ref. TASK 78-31-11-200-801). **ON A/C 701-749, Subtask 12-36-29-611-101-A A. Clean the Fluid in the Blue Hydraulic System NOTE : If the fluid is contaminated because of engine pump deterioration, ____ do the procedure for the check of the Blue hydraulic system after operation of the engine pump in possible cavitation condition (Ref. TASK 29-00-00-280-802). (1) Pressurize the system that you must clean with the ground hydraulic supply (Ref. TASK 29-00-00-863-802). (2) Operate all the flight controls and brakes to make a fluid flow in the system. (3) Do a fluid sampling for particle contamination (Ref. TASK 12-32-29281-801). (4) Continue to operate the flight controls and the brakes until you get a sample that is correct (contamination lower than NSA 307-110 class 9). (5) Do a check of the clogging indicator of: - the case drain filter 5013JM2 (Ref. TASK 29-10-00-200-806), - the HP filter 5111JM2 (Ref. TASK 29-10-00-200-804), - the LP filter 5011JM1 (Ref. TASK 29-10-00-200-804), - the filter element installed on the Isolation Control Unit 4117KS (Ref. TASK 78-31-41-200-802).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, 701-749, SROS
Page C340 Jan 01/07
**ON A/C ALL 5. Close-up ________ Subtask 12-36-29-864-051 A. Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802). Subtask 12-36-29-860-135 B. Disconnect the suction and delivery lines of the hydraulic ground power supply from the aircraft connectors, access door 195BB: - 5132JM2 suction - 5131JM2 delivery. Subtask 12-36-29-410-102 C. Close Access (1) Close the MLG doors (Ref. TASK 32-12-00-410-801). (2) Remove the access platform(s).
EFF : ALL 12-36-29 R SROS
Page C341 Jan 01/07
TASK 12-36-29-611-806 Reclaim the Fluid in the Yellow Hydraulic System WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. 1. __________________ Reason for the Job Clean the fluid when the rate of particle contamination is higher than the values of NSA 307-110 class 9 (Ref. TASK 12-32-29-281-80100). 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
ground hydraulic supply hydraulic ground power supply access platform 1.8 m (5 ft. 11 in.)
EFF : ALL 12-36-29 R SROS
Page C342 Jan 01/07
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-805 12-12-29-611-806 12-32-29-281-801 24-41-00-861-801 29-00-00-280-803 29-00-00-863-803 29-00-00-864-803 29-10-00-200-804 29-10-00-200-806 29-14-00-614-804 31-60-00-860-801 32-12-00-010-801 32-12-00-410-801 78-31-11-200-801 78-31-41-200-802
Fill the Yellow Hydraulic Reservoir with a Hydraulic Service Cart Fill the Yellow Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A Check of the Yellow Hydraulic System after Operation of the Engine Pump in Possible Starvation or Cavitation Condition. Pressurize the Yellow Hydraulic System with the Ground Hydraulic Supply Depressurize the Yellow Hydraulic System (Pressurized with the Hydraulic Ground Supply) Check of the Clogging Indicators of the Hydraulic System Filter in the Hydraulics Compartment. Check of the Clogging Indicators of the Hydraulic System Filters on the Engines. Pressurization of the Hydraulic Reservoirs with external bench EIS Start Procedure Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Inspection of the Hydraulic Filter Assembly Element Inspection of the Thrust Reverser Isolation Control Unit
3. __________ Job Set-up Subtask 12-36-29-861-058 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801).
EFF : ALL 12-36-29 R SROS
Page C343 Jan 01/07
Subtask 12-36-29-860-136 B. Aircraft Maintenance Configuration (1) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00860-801). (2) On the ECAM control panel, push the HYD key (on the SD the HYD page comes into view). (3) On the SD make sure that: - the LO AIR PRESS indication of the Yellow reservoir is not shown. If it is shown, pressurize the reservoir (Ref. TASK 29-14-00-614804), - the level index of the Yellow reservoir shows that the fluid level is correct. If the level of the fluid is not correct add fluid with a service cart or with a hand pump (Ref. TASK 12-12-29-611-805), (Ref. TASK 12-12-29-611-806). (4) Connect the suction and delivery lines of the hydraulic ground power supply to the aircraft connectors, access door 196BB: - 5132JM3 suction - 5131JM3 delivery. Subtask 12-36-29-010-104 C. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Put an access platform in position at the zone 196. 4. Procedure _________ **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 12-36-29-611-102 A. Clean the Fluid in the Yellow Hydraulic System NOTE : If the fluid is contaminated because of engine pump deterioration, ____ do the procedure for the check of the Yellow hydraulic system after operation of the engine pump in possible cavitation condition (Ref. TASK 29-00-00-280-803).
EFF : ALL 12-36-29 R SROS
Page C344 Jan 01/07
(1) Pressurize the system that you must clean with the ground hydraulic supply (Ref. TASK 29-00-00-863-803). (2) Operate all the flight controls to make a fluid flow in the system. (3) Do a fluid sampling for particle contamination (Ref. TASK 12-32-29281-801). (4) Continue to operate the flight controls until you get a sample that is correct (contamination lower than NSA 307-110 class 9). (5) Do a check of the clogging indicator of: - the case drain filter 5013JM2 (Ref. TASK 29-10-00-200-806), - the HP filter 5111JM2 (Ref. TASK 29-10-00-200-804), - the LP filter 5011JM2 (Ref. TASK 29-10-00-200-804), - the HCU filter 5001EG2 (Ref. TASK 78-31-11-200-801). **ON A/C 701-749, Subtask 12-36-29-611-102-A A. Clean the Fluid in the Yellow Hydraulic System NOTE : If the fluid is contaminated because of engine pump deterioration, ____ do the procedure for the check of the Yellow hydraulic system after operation of the engine pump in possible cavitation condition (Ref. TASK 29-00-00-280-803). (1) Pressurize the system that you must clean with the ground hydraulic supply (Ref. TASK 29-00-00-863-803). (2) Operate all the flight controls to make a fluid flow in the system. (3) Do a fluid sampling for particle contamination (Ref. TASK 12-32-29281-801). (4) Continue to operate the flight controls until you get a sample that is correct (contamination lower than NSA 307-110 class 9). (5) Do a check of the clogging indicator of: - the case drain filter 5013JM2 (Ref. TASK 29-10-00-200-806), - the HP filter 5111JM2 (Ref. TASK 29-10-00-200-804), - the LP filter 5011JM2 (Ref. TASK 29-10-00-200-804), - the filter element installed on the Isolation Control Unit 4117KS (Ref. TASK 78-31-41-200-802).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, 701-749, SROS
Page C345 Jan 01/07
**ON A/C ALL 5. Close-up ________ Subtask 12-36-29-864-052 A. Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803). Subtask 12-36-29-860-137 B. Disconnect the suction and delivery lines of the hydraulic ground power supply from the aircraft connectors, access door 196BB: - 5132JM3 suction - 5131JM3 delivery. Subtask 12-36-29-410-103 C. Close Access (1) Close the MLG doors (Ref. TASK 32-12-00-410-801). (2) Remove the access platform(s).
EFF : ALL 12-36-29 R SROS
Page C346 Jan 01/07
TASK 12-36-29-615-801 Clean the Fluid in the Green Hydraulic System (with the Pall Purifier) WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job Clean the fluid when the chemical analysis (without the acid number check) is equal to or higher than the values of the NSA 307-110 (Ref. TASK 12-32-29-281-80100). 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------HSPA181-380J
1 HYDRAULIC PURIFIER
EFF : ALL 12-36-29 R SROS
Page C347 Jan 01/07
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-801 12-12-29-611-802 24-41-00-861-801 24-41-00-862-801 29-00-00-864-801 29-14-00-614-801 29-14-00-614-804 31-60-00-860-801
Fill the Green Hydraulic Reservoir with a Hydraulic Service Cart Fill the Green Hydraulic Reservoir with a Hand Pump Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Depressurize the Green Hydraulic System (Pressurized with the Hydraulic Ground Supply) Depressurization of the Green Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench EIS Start Procedure
3. __________ Job Set-up Subtask 12-36-29-010-117 A. Get Access (1) Open the access door 197CB. Subtask 12-36-29-860-168 B. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (3) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00860-801).
EFF : ALL 12-36-29 R SROS
Page C348 Jan 01/07
(4) On the SD, make sure that: - the LO AIR PRESS indication of the Green reservoir is not in view. If this indication is shown pressurize the reservoir (Ref. TASK 2914-00-614-801), - the level index of the Green reservoir shows that the fluid level is correct. If the level is not correct, add fluid to the reservoir with a hydraulic service cart (Ref. TASK 12-12-29-611-801) or with a hand pump (Ref. TASK 12-12-29-611-802). (5) Connect the suction and delivery lines of the hydraulic Pall Purifier to the hydraulic ground service panel: - 5132JM1 ground connector-suction, - 5131JM1 ground connector-delivery. (6) On the FLT CTL section of the overhead panel 241VU, make sure that the PRIM1 and SEC1 pushbutton switches are pushed (the OFF and FAULT legends are off). (7) On the FLT CTL section of the overhead panel 212VU make sure that the PRIM2, PRIM3 and SEC2 pushbutton switches are pushed (the OFF and FAULT legends are off). (8) On the ECAM control panel, push the F/CTL key (on the SD the F/CTL page comes into view). (9) Make sure that the IRS are not aligned. 4. Procedure _________ Subtask 12-36-29-615-050 A. Clean the Fluid in the Green Hydraulic System WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED _______ ON THE LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE _______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE. NOTE : Obey the manufacturer instructions for the hydraulic purifier. ____ (1) Set the main pump of the HYDRAULIC PURIFIER (HSPA181-380J) to ON.
EFF : ALL 12-36-29 R SROS
Page C349 Jan 01/07
(2) Operate the purifier for 30 minutes. (3) Operation of the flight controls from the CAPT side. (a) Move the side stick in the full nose-up, nose down, left roll and right roll directions: - the ailerons, the elevators, the spoiler 5 move in relation to the side stick orders. (b) Put the side stick in the neutral position: - the surfaces go back to the neutral position. (c) Push the right then the left pedal to the mechanical stop: - the rudder moves in relation to the pedals orders. (d) Put the pedals in the neutral position: - the rudder goes back to the neutral position. (e) Put the SPEED BRAKE control lever in the FULL position: - the spoilers 1 and 5 extend. (f) Put the SPEED BRAKE control lever in the RET position: - the spoilers 1 and 5 retract. (g) On the panel 114VU, put the flap and slat control lever in the FULL position: - the slats and the flaps extend. (h) On the panel 114VU, put the flap and slat control lever in the O position: - the slats and the flaps retract. (4) Do a check of the water contents indicators at the purifier. (5) If the water contents is high, continue to operate the purifier. (6) Stop the cleaning procedure, when the water contents indicator shows a low water contents. (7) Set the main pump of the HYDRAULIC PURIFIER (HSPA181-380J) to OFF. (8) Disconnect the suction and delivery lines of the hydraulic purifier from the aircraft connectors.
EFF : ALL 12-36-29 R SROS
Page C350 Jan 01/07
5. Close-up ________ Subtask 12-36-29-860-169 A. Put the aircraft back to its operational configuration. (1) On the SD, make sure that: - the LO AIR PRESS indication of the Green reservoir is not in view. If this indication is shown pressurize the Green hydraulic reservoir (Ref. TASK 29-14-00-614-804). - the level index of the Green reservoir shows that the fluid level is correct. If the level is not correct, add fluid to the reservoir with a hydraulic service cart (Ref. TASK 12-12-29-611-801) or with a hand pump (Ref. TASK 12-12-29-611-802). (2) Make sure that the work area is clean and clear of tools and other items. (3) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). Subtask 12-36-29-410-116 B. Close Access (1) Close the access door 197CB.
EFF : ALL 12-36-29 R SROS
Page C351 Jan 01/07
TASK 12-36-29-615-802 Clean the Fluid in the Blue Hydraulic System (with the Pall Purifier) WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job Clean the fluid when the chemical analysis (without the acid number check) is equal to or higher than the values of the NSA 307-110 (Ref. TASK 12-32-29-281-80100). 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------HSPA181-380J
1 HYDRAULIC PURIFIER
EFF : ALL 12-36-29 SROS
Page C352 Jan 01/07
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-803 12-12-29-611-804 24-41-00-861-801 24-41-00-862-801 29-00-00-864-802 29-14-00-614-801 29-14-00-614-804 31-60-00-860-801
Fill the Blue Hydraulic Reservoir with a Hydraulic Service Cart Fill the Blue Hydraulic Reservoir with a Hand Pump Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Depressurize the Blue Hydraulic System (Pressurized with the Hydraulic Ground Supply) Depressurization of the Green Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench EIS Start Procedure
3. __________ Job Set-up Subtask 12-36-29-010-118 A. Get Access (1) Open the access door 195BB. Subtask 12-36-29-860-170 B. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802). (3) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00860-801).
EFF : ALL 12-36-29 SROS
Page C353 Jan 01/07
(4) On the SD, make sure that: - the LO AIR PRESS indication of the Blue reservoir is not in view. If this indication is shown pressurize the reservoir (Ref. TASK 2914-00-614-801), - the level index of the Blue reservoir shows that the fluid level is correct. If the level is not correct, add fluid to the reservoir with a hydraulic service cart (Ref. TASK 12-12-29-611-803) or with a hand pump (Ref. TASK 12-12-29-611-804). (5) Connect the suction and delivery lines of the hydraulic Pall Purifier to the hydraulic ground service panel: - 5132JM2 ground connector-suction, - 5131JM2 ground connector-delivery. (6) On the FLT CTL section of the overhead panel 241VU make sure that the PRIM1 and SEC1 pushbutton switches are pushed (the OFF and FAULT legends are off). (7) On the FLT CTL section of the overhead panel 212VU make sure that the PRIM2, PRIM3 and SEC2 pushbutton switches are pushed (the OFF and FAULT legends are off). (8) On the ECAM control panel, push the F/CTL key (on the SD the F/CTL page comes into view). (9) Make sure that the IRS are not aligned. 4. Procedure _________ Subtask 12-36-29-615-051 A. Clean the Fluid in the Blue Hydraulic System WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED _______ ON THE LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE _______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE. NOTE : Obey the manufacturer instructions for the hydraulic purifier. ____ (1) Set the main pump of the HYDRAULIC PURIFIER (HSPA181-380J) to ON.
EFF : ALL 12-36-29 SROS
Page C354 Jan 01/07
(2) Operate the purifier for 30 minutes. (3) Operation of the flight controls from the CAPT side. (a) Move the side stick in the full nose-up, nose down, left roll and right roll directions: - the inboard ailerons and one elevator move in relation to the side stick orders. (b) Put the side stick in the neutral position: - the surfaces go back to the neutral position. (c) Push the right then the left pedal to the mechanical stop: - the rudder moves in relation to the pedals orders. (d) Put the pedals in the neutral position: - the rudder goes back to the neutral position. (e) On the center pedestal, move the pitch-trim control wheel in the full nose-up and nose-down directions: - the THS moves in relation to the wheel orders. (f) Put the pitch-trim control wheel in the neutral position: - the THS goes back to the neutral position. (g) Put the SPEED BRAKE control lever in the FULL position: - the spoilers 2 and 3 extend. (h) Put the SPEED BRAKE control lever in the RET position: - the spoilers 2 and 3 retract. (i) On the panel 114VU, put the flap and slat control lever in the FULL position: - the slats extend. (j) On the panel 114VU, put the flap and slat control lever in the O position: - the slats retract. (4) Do a check of the water contents indicators of the purifier. (5) If the water contents is high, continue to operate the purifier. (6) Stop the cleaning procedure when the water contents indicator shows a low water contents. (7) Set the main pump of the HYDRAULIC PURIFIER (HSPA181-380J) to OFF.
EFF : ALL 12-36-29 SROS
Page C355 Jan 01/07
(8) Disconnect the suction and delivery lines of the hydraulic purifier from the aircraft connectors. 5. Close-up ________ Subtask 12-36-29-860-171 A. Put the aircraft back to its operational configuration. (1) On the SD, make sure that: - the LO AIR PRESS indication of the Blue reservoir is not in view. If this indication is shown pressurize the Blue hydraulic reservoir (Ref. TASK 29-14-00-614-804). - the level index of the Blue reservoir shows that the fluid level is correct. If the level is not correct, add fluid to the reservoir with a hydraulic service cart (Ref. TASK 12-12-29-611-803) or with a hand pump (Ref. TASK 12-12-29-611-804). (2) Make sure that the work area is clean and clear of tools and other items. (3) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). Subtask 12-36-29-410-117 B. Close Access (1) Close the access door 195BB.
EFF : ALL 12-36-29 SROS
Page C356 Jan 01/07
TASK 12-36-29-615-803 Clean the Fluid in the Yellow Hydraulic System (with the Pall Purifier) WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job Clean the fluid when the chemical analysis (without the acid number check) is equal to or higher than the values of the NSA 307-110 (Ref. TASK 12-32-29-281-80100). 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------HSPA181-380J
1 HYDRAULIC PURIFIER
EFF : ALL 12-36-29 SROS
Page C357 Jan 01/07
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-805 12-12-29-611-806 24-41-00-861-801 24-41-00-862-801 29-00-00-864-803 29-14-00-614-801 29-14-00-614-804 31-60-00-860-801
Fill the Yellow Hydraulic Reservoir with a Hydraulic Service Cart Fill the Yellow Hydraulic Reservoir with a Hand Pump Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Depressurize the Yellow Hydraulic System (Pressurized with the Hydraulic Ground Supply) Depressurization of the Green Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench EIS Start Procedure
3. __________ Job Set-up Subtask 12-36-29-010-119 A. Get Access (1) Open the access door 196BB. Subtask 12-36-29-860-172 B. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803). (3) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00860-801).
EFF : ALL 12-36-29 SROS
Page C358 Jan 01/07
(4) On the SD make sure that: - the LO AIR PRESS indication of the Yellow reservoir is not in view. If this indication is shown pressurize the reservoir (Ref. TASK 2914-00-614-801). - the level index of the Yellow reservoir shows that the fluid level is correct. If the level is not correct, add fluid to the reservoir with a hydraulic service cart (Ref. TASK 12-12-29-611-805) or with a hand pump (Ref. TASK 12-12-29-611-806). (5) Connect the suction and delivery lines of the hydraulic Pall Purifier to the hydraulic ground service panel: - 5132JM3 ground connector-suction, - 5131JM3 ground connector-delivery. (6) On the FLT CTL section of the overhead panel 241VU make sure that the PRIM1 and SEC1 pushbutton switches are pushed (the OFF and FAULT legends are off). (7) On the FLT CTL section of the overhead panel 212VU make sure that the PRIM2, PRIM3 and SEC2 pushbutton switches are pushed (the OFF and FAULT legends are off). (8) On the ECAM control panel, push the F/CTL key (on the SD the F/CTL page comes into view). (9) Make sure that the IRS are not aligned. 4. Procedure _________ Subtask 12-36-29-615-052 A. Clean the Fluid in the Yellow Hydraulic System WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED _______ ON THE LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE _______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE. NOTE : Obey the manufacturer instructions for the hydraulic purifier. ____ (1) Set the main pump of the HYDRAULIC PURIFIER (HSPA181-380J) to ON.
EFF : ALL 12-36-29 SROS
Page C359 Jan 01/07
(2) Operate the purifier for 30 minutes. (3) Operation of the flight controls from the CAPT side. (a) Move the side stick in the full nose-up, nose-down, left roll and right roll directions: - the outboard aileron, spoilers and one elevator move in relation to the side stick orders. (b) Put the side stick in the neutral position: - the surfaces go back to the neutral position. (c) Push the right then the left pedal to the mechanical stop. - the rudder moves in relation to the pedals orders. (d) Put the pedals in the neutral position: - the rudder goes back to the neutral position. (e) On the center pedestal, move the pitch-trim control wheel in the full nose-up and nose-down directions: - the THS moves in relation to the wheel orders. (f) Put the pitch-trim control wheel in the neutral position: - the THS goes back to the neutral position. (g) Put the SPEED BRAKE control lever in the FULL position: - the spoilers 4 and 6 extend (h) Put the SPEED BRAKE control lever in the RET position. - the spoilers 4 and 6 retract. (i) On the panel 114VU, put the flap and slat control lever in the FULL position: - the flaps extend. (j) On the panel 114VU, put the flap and slat control lever in the O position: - the flaps retract. (4) Do a check of the water contents indicators at the purifier. (5) If the water contents is high, continue to operate the purifier. (6) Stop the cleaning procedure when the water contents indicator shows a low water contents. (7) Set the main pump of the HYDRAULIC PURIFIER (HSPA181-380J) to OFF.
EFF : ALL 12-36-29 SROS
Page C360 Jan 01/07
(8) Disconnect the suction and delivery lines of the hydraulic purifier from the aircraft connectors. 5. Close-up ________ Subtask 12-36-29-860-173 A. Put the aircraft back to its operational configuration. (1) On the SD, make sure that: - the LO AIR PRESS indication of the Yellow reservoir is not in view. If this indication is shown pressurize the (Ref. TASK 29-14-00-614804). - the level index of the Yellow reservoir shows that the fluid level is correct. If the level is not correct, add fluid to the reservoir with a hydraulic service cart (Ref. TASK 12-12-29-611-805) or with a hand pump (Ref. TASK 12-12-29-611-806). (2) Make sure that the work area is clean and clear of tools and other items. (3) Depressurize the aircraft hydraulic systems (Ref. TASK 24-41-00-862-801). Subtask 12-36-29-410-118 B. Close Access (1) Close the access door 196BB.
EFF : ALL 12-36-29 SROS
Page C361 Jan 01/07
L.E.P. 1-12 Revised to Reflect this revision indicating new,revised, and/or deleted pages T. OF C. Revised to reflect this revision 12, 5, 78, 1116 12-00-00 CORRECTION/ADDITION/AMPLIFICATION 202, 206 ADDED NOTE.
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12-11-28 301, 303304, 308309, 315B308
Effectivity updated CORRECTION/ADDITION/AMPLIFICATION NOTE ADDED TO INCLUDE REFUEL WITH ONE ENGINE RUNNING LAYOUT IMPROVED/MATERIAL RELOCATED
12-12-29 302- 304, 306, 309312, 317
CORRECTION/ADDITION/AMPLIFICATION REMOVED NOTE RELATED TO THE RESET OF THE C/B 5JR
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12-12-32 313, 331, 334
CORRECTION/ADDITION/AMPLIFICATION ILLUSTRATION RE-ISSUED TOOL DESIGNATION(S) DATA UPDATED
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12-13-80 01 TITLE OF TASK(S) DATA UPDATED 311, 323
001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499,
12-14-29 301- 302, 305- 306, 309- 310
CORRECTION/ADDITION/AMPLIFICATION ADDED A NOTE (TEMPERATURE COMPENSATION TIME OF THE ACCUMULATOR). TOOL DESIGNATION(S) DATA UPDATED
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12-14-32 301- 302, 304, 318,
Effectivity updated CORRECTION/ADDITION/AMPLIFICATION FINS CHANGED TO 5490GG AND 5491GG
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-------------------------------------------------------------------------------------CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES -------------------------------------------------------------------------------------323- 325, 327, 329330, 335
TOOL DESIGNATION(S) DATA UPDATED TITLE OF TASK(S) DATA UPDATED
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12-16-38 303
TECHNICAL CORRECTIONS CLERICAL CORRECTION
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12-21-11 301- 311
TECHNICAL CORRECTIONS ADDED WARNING FOR HEALTH RECOMMENDATION CORRECTION/ADDITION/AMPLIFICATION ADDED ADHESIVE-TAPE WARNING WARNING/NOTE/REASON FOR THE JOB AMENDED
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12-21-12 323- 324, 326- 328, 345, 353, 365- 366
12-21-13 701- 720
Effectivity updated MOD.45794D41610 REMOVED EQUIPMENT/FURNISHINGS-PAX COMPARTMENTINSTALL A 3 CLASS LAYOUT FOR SWR1 VERSION CORRECTION/ADDITION/AMPLIFICATION MINOR CHANGE CORRECTION/ADDITION/AMPLIFICATION ADDED CROSS REFERENCE TO ILS RECEIVER TITLE OF TASK(S) DATA UPDATED WARNING/NOTE/REASON FOR THE JOB AMENDED
ALL ALL 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, ALL ALL ALL ALL
12-22-27 305- 306, 345- 346, 348, 350390
Effectivity updated CORRECTION/ADDITION/AMPLIFICATION CAUTION ADDED.
12-22-32 312- 317, 322- 323, 328- 336, 339, 349, 356, 360365
CORRECTION/ADDITION/AMPLIFICATION ITEM 1 (2 ON ONE SIDE, 1ON THE OTHER) CHANGED TO (3 ON ONE SIDE, 2ON THE OTHER) LAYOUT IMPROVED/MATERIAL RELOCATED
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12-31-00 3
CORRECTION/ADDITION/AMPLIFICATION NOTE IN ITEM B.(4) UPDATED.
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12-31-11 201- 204, 208- 210
CORRECTION/ADDITION/AMPLIFICATION ANTI-ICING FLUID REPLACED BY ANTI-ICING/DE-ICING FLUID. TOOL DESIGNATION(S) DATA UPDATED WARNING/NOTE/REASON FOR THE JOB AMENDED
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-------------------------------------------------------------------------------------CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES -------------------------------------------------------------------------------------12-31-12 201- 203, 209- 213
TECHNICAL CORRECTIONS CLERICAL CORRECTION. CORRECTION/ADDITION/AMPLIFICATION ADDED NOTE. TOOL DESIGNATION(S) DATA UPDATED
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TECHNICAL CORRECTIONS CLERICAL CORRECTION. WARNING/NOTE/REASON FOR THE JOB AMENDED
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12-31-27 201- 203
TECHNICAL CORRECTIONS CLERICAL CORRECTION.
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12-31-32 203- 207
LAYOUT IMPROVED/MATERIAL RELOCATED
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12-31-35 202
TECHNICAL CORRECTIONS CLERICAL CORRECTION.
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12-31-38 201
WARNING/NOTE/REASON FOR THE JOB AMENDED
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12-32-28 302, 308309, 311314, 338, 341- 344
TECHNICAL CORRECTIONS CLERICAL CHANGE CORRECTION/ADDITION/AMPLIFICATION CLERICAL CHANGE WARNING/NOTE/REASON FOR THE JOB AMENDED
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12-32-29 301- 302, 304- 305
CORRECTION/ADDITION/AMPLIFICATION ADDED PLASTIC SAMPLE BOTTLE EXCLUSIVELY MADE FROM POLY-ETHYLENE
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12-34-24 201- 202, 205- 207
TECHNICAL CORRECTIONS CLERICAL CORRECTION. CORRECTION/ADDITION/AMPLIFICATION WORK-STAND REPLACED BY ACCESS PLATFORM OR STE P LADDER. WARNING/NOTE/REASON FOR THE JOB AMENDED
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12-31-24 201
12-36-29 327, 332, 335,A328A329,A351C361
Effectivity updated CORRECTION/ADDITION/AMPLIFICATION REMOVED STEPS RELATED TO THE HCU FILTER LAYOUT IMPROVED/MATERIAL RELOCATED WARNING/NOTE/REASON FOR THE JOB AMENDED
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CHAPTER 12 __________ SERVICING LIST OF EFFECTIVE PAGES _______________________ N, R or D indicates pages which are New, Revised or Deleted respectively Remove and insert the affected pages and complete the Record of Revisions and the Record of Temporary Revisions as necessary CH/SE/SU
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CH/SE/SU 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28
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DATE Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07
CH/SE/SU 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28
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DATE Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07
CH/SE/SU 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-11-28 12-12-00 12-12-00 12-12-00 12-12-00 12-12-00 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29
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CH/SE/SU 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-29 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32 12-12-32
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323 324 325 326 327 328 329 330 331 332 333 334 335 336 337 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315 316 317 318 319 320 321 322 323 324 325 326 327 328 329 330 331 332 333 334 335 336
DATE Jan01/05 Jan01/05 Jan01/05 Jan01/05 Jan01/05 Jan01/05 Jul01/06 Jan01/05 Jan01/05 Jan01/05 Jan01/05 Jan01/05 Jan01/05 Jan01/05 Jan01/05 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jan01/04 Jan01/04 Jan01/04 Jan01/04 Jul01/06 Jul01/06 Jul01/06 Jan01/07 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jan01/07 Jul01/06 Jul01/06 Jan01/07 Jul01/06 Jul01/06
CH/SE/SU
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12-12-32 12-12-32 12-12-32 12-12-32 12-13-00 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24
01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 02 02 02 02 02 02 02 02 02 02 02 02 02 02
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337 338 339 340
Jul01/06 Jul01/06 Jul01/06 Jul01/06
1 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315 316 317 318 319 320 321 322 323 324 325 326 327 328 329 330 331 301 302 303 304 305 306 307 308 309 310 311 312 313 314
Apr01/98 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jan01/06 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jan01/02 Jan01/06 Jan01/06 Jan01/06 Oct01/00 Jan01/06 Jan01/06 Jan01/06 Jan01/02 Jan01/02 Jan01/02 Jan01/02 Jan01/02 Jan01/02
CH/SE/SU
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12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-24 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27
02 02 02 02 02 02 02 02 02 02 02 02 02 02 02
315 316 317 318 319 320 321 322 323 324 325 326 327 328 329 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315 316 317 318 319 320 321 322 323 324 325 326 327 328 329 330 331 332 333 334 335 336
DATE Jul01/05 Jul01/05 Jan01/06 Apr01/04 Jan01/06 Jan01/06 Jan01/02 Jan01/02 Jan01/02 Jan01/02 Jan01/02 Jan01/02 Apr01/03 Apr01/03 Jan01/02 Jan01/05 Jul01/02 Apr01/02 Apr01/02 Jul01/06 Jan01/05 Jan01/06 Jul01/02 Oct01/01 Apr01/01 Jan01/06 Jan01/06 Jan01/05 Jul01/02 Jul01/06 Jul01/01 Apr01/02 Apr01/05 Jul01/06 Apr01/02 Jan01/06 Jul01/06 Jul01/01 Jul01/01 Apr01/05 Oct01/01 Oct01/01 Jan01/05 Jan01/02 Jul01/06 Jul01/01 Jul01/02 Oct01/01 Jul01/06 Jan01/02 Jan01/02
12-L.E.P. Page 3 Jan 01/07 SROS
CH/SE/SU 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-27 12-13-29 12-13-29 12-13-29 12-13-29 12-13-29 12-13-29 12-13-29 12-13-49 12-13-49 12-13-49 12-13-49 12-13-49 12-13-49 12-13-49 12-13-49 12-13-49 12-13-49 12-13-49 12-13-49 12-13-49 12-13-49 12-13-49
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DATE Jul01/06 Jan01/02 Jan01/02 Jan01/06 Jul01/05 Jul01/05 Jul01/05 Jul01/06 Jul01/06 Jul01/06 Jul01/05 Jul01/05 Jan01/05 Jan01/06 Jan01/06 Jan01/06 Jul01/06 Jan01/03 Jul01/06 Jul01/06 Jan01/03 Jul01/06 Jan01/03 Jul01/06 Jan01/05 Jan01/03 Jan01/03 Jan01/03 Jan01/03 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/05 Jul01/02 Apr01/02 Apr01/98 Apr01/98 Apr01/02 Jul01/02 Apr01/02 Jan01/05 Jan01/05 Jul01/02 Apr01/02 Apr01/02 Apr01/02 Apr01/02
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12-13-49 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79
01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 01 02 02 02 02 02 02 02 02 02
316 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315 316 317 318 319 320 321 322 323 324 325 326 327 328 329 330 331 332 333 334 335 336 337 338 339 340 341 301 302 303 304 305 306 307 308 309
DATE Apr01/02 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/01 Apr01/02 Jul01/01 Apr01/05 Apr01/05 Apr01/05 Apr01/05 Apr01/05 Apr01/05
CH/SE/SU
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12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-79 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80
02 02 02 02 02 02 02 02 02 02 02 02 02 02 02 01 01 01 01 01 01 01 01 01 01 01 R 01 01 01 01 01 01 01 01 01 01 01 01 R 01 01 01 01 01 01 01 01 01 01 01 01 01
310 311 312 313 314 315 316 317 318 319 320 321 322 323 324 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315 316 317 318 319 320 321 322 323 324 325 326 327 328 329 330 331 332 333 334 335 336
DATE Apr01/05 Oct01/00 Oct01/04 Jul01/03 Jul01/03 Apr01/02 Oct01/00 Jul01/04 Oct01/00 Oct01/00 Jul01/03 Oct01/00 Jul01/03 Jul01/03 Jul01/03 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jan01/07 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jan01/07 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jan01/06
12-L.E.P. Page 4 Jan 01/07 SROS
CH/SE/SU
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12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80 12-13-80
01 01 01 01 01 01 02 02 02 02 02 02 02 02 02 02 02 02 02
337 338 339 340 341 342 301 302 303 304 305 306 307 308 309 310 311 312 313
Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Apr01/05 Oct01/00 Oct01/00 Oct01/00 Oct01/00 Oct01/00 Oct01/00 Oct01/00 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04
1 301 302 303 304 305 306 307 308 309 310 311 312 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315 316 317 318
Apr01/98 Jan01/07 Jan01/07 Apr01/98 Jul01/06 Jan01/07 Jan01/07 Apr01/98 Jul01/06 Jan01/07 Jan01/07 Apr01/98 Jul01/06 Jan01/07 Jan01/07 Jan01/03 Jan01/07 Jul01/06 Apr01/04 Jul01/06 Apr01/98 Apr01/04 Jul01/04 Jul01/04 Jul01/06 Jul01/06 Jul01/06 Apr01/03 Apr01/03 Apr01/03 Jan01/07
12-14-00 12-14-29 12-14-29 12-14-29 12-14-29 12-14-29 12-14-29 12-14-29 12-14-29 12-14-29 12-14-29 12-14-29 12-14-29 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32
R R R R R R R R R
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CH/SE/SU 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-32 12-14-35 12-14-35 12-14-35 12-14-35 12-14-35 12-14-35 12-15-00 12-15-38 12-15-38 12-15-38 12-15-38
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319 320 321 322 323 324 325 326 327 328 329 330 331 332 333 334 335 336 337 338 339 340 341 342 343 344 345 346 347 348 349 350 351 352 353 354 355 356 357 301 302 303 304 305 306
Jul01/06 Jul01/06 Apr01/04 Apr01/04 Jan01/07 Jan01/07 Jan01/07 Apr01/04 Jan01/07 Apr01/04 Jan01/07 Jan01/07 Apr01/05 Apr01/04 Jul01/06 Apr01/04 Jan01/07 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jan01/05 Apr01/04 Apr01/04 Apr01/04 Apr01/04 Apr01/04 Apr01/04 Jul01/03 Jan01/05 Apr01/05 Apr01/04 Apr01/04 Jul01/03 Apr01/04 Apr01/05 Apr01/04 Jan01/06 Jul01/03 Oct01/04 Oct01/04 Apr01/00 Apr01/02 Apr01/98 Apr01/02
1 301 302 303 304
Apr01/98 Jul01/05 Jul01/06 Jul01/05 Jul01/03
CH/SE/SU
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12-15-38 12-15-38 12-15-38 12-15-38 12-15-38 12-15-38 12-15-38 12-15-38 12-15-38 12-15-38
305 306 307 308 309 310 311 312 313 314
Jul01/98 Jul01/05 Jul01/05 Jul01/03 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05
12-16-00 12-16-25 12-16-25 12-16-25 12-16-25 12-16-25 12-16-38 12-16-38 12-16-38 12-16-38 12-16-38 12-16-38 12-16-38 12-16-38
1 301 302 303 304 305 301 302 303 304 305 306 307 308
Apr01/98 Jul01/05 Jul01/05 Jul01/05 Oct01/00 Jul01/05 Oct01/04 Jul01/05 Jan01/07 Jul01/05 Jul01/05 Oct01/03 Apr01/05 Apr01/05
1 301 302 303 304
Apr01/98 Jul01/06 Jul01/05 Jan01/03 Jan01/03
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12-17-00 12-17-30 12-17-30 12-17-30 12-17-30 12-20-00 12-21-00 12-21-11 12-21-11 12-21-11 12-21-11 12-21-11 12-21-11 12-21-11 12-21-11 12-21-11 12-21-11 12-21-11 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12
1 Apr01/98 R R R R R R R R R R N
1 301 302 303 304 305 306 307 308 309 310 311 301 302 303 304 305
Apr01/98 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Apr01/05 Apr01/05 Apr01/05 Apr01/05 Apr01/05
12-L.E.P. Page 5 Jan 01/07 SROS
CH/SE/SU 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12
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306 307 308 309 310 311 312 313 314 315 316 317 318 319 320 321 322 323 324 325 326 327 328 329 330 331 332 333 334 335 336 337 338 339 340 341 342 343 344 345 346 347 348 349 350 351 352 353 354 355 356
DATE Apr01/05 Jul01/05 Jul01/05 Apr01/05 Apr01/05 Apr01/05 Jul01/06 Apr01/05 Apr01/05 Apr01/05 Apr01/05 Jul01/06 Jul01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/07 Jan01/07 Jan01/06 Jan01/07 Jan01/07 Jan01/07 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Apr01/05 Apr01/05 Apr01/05 Apr01/05 Apr01/05 Apr01/05 Jan01/06 Jul01/06 Jul01/06 Jan01/07 Jul01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jul01/06 Jul01/06 Jan01/07 Jul01/06 Jul01/06 Jan01/06
CH/SE/SU 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-12 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-21-13 12-22-00 12-22-00 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27
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357 358 359 360 361 362 363 364 365 366 367 368 369 701 702 703 704 705 706 707 708 709 710 711 712 713 714 715 716 717 718 719 720
Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/07 Jan01/07 Jan01/06 Jan01/06 Jan01/06 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07
1 2 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315
Apr01/98 Apr01/98 Jan01/05 Apr01/05 Jul01/06 Jan01/04 Jan01/07 Jan01/07 Jul01/06 Jul01/06 Jul01/06 Apr01/03 Jul01/02 Jan01/02 Jan01/02 Jul01/06 Jul01/06
CH/SE/SU 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27
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316 317 318 319 320 321 322 323 324 325 326 327 328 329 330 331 332 333 334 335 336 337 338 339 340 341 342 343 344 345 346 347 348 349 350 351 352 353 354 355 356 357 358 359 360 361 362 363 364 365 366
DATE Jan01/06 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jan01/06 Jan01/06 Jul01/06 Jul01/06 Jul01/06 Apr01/04 Apr01/04 Jan01/05 Jul01/04 Apr01/04 Jul01/04 Jul01/04 Jan01/05 Jan01/06 Oct01/03 Oct01/03 Apr01/04 Jan01/05 Jan01/06 Oct01/04 Oct01/04 Oct01/03 Oct01/03 Jan01/07 Jan01/07 Jan01/06 Jan01/07 Jan01/06 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07
12-L.E.P. Page 6 Jan 01/07 SROS
CH/SE/SU 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-27 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32
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367 368 369 370 371 372 373 374 375 376 377 378 379 380 381 382 383 384 385 386 387 388 389 390 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315 316 317 318 319 320 321 322 323 324 325 326 327
DATE Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jan01/07 Jan01/07 Jul01/06 Jul01/06 Jul01/06 Jul01/06
CH/SE/SU 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-32 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52
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328 329 330 331 332 333 334 335 336 337 338 339 340 341 342 343 344 345 346 347 348 349 350 351 352 353 354 355 356 357 358 359 360 361 362 363 364 365 366 367 368 369 370 371 372 373 301 302 303 304 305
DATE Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jul01/06 Jul01/06 Jan01/07 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jan01/07 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jan01/07 Jul01/06 Jul01/06 Jul01/06 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07
Jan01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/99
CH/SE/SU 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52 12-22-52
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12-24-00 12-24-29 12-24-29 12-24-29 12-24-29 12-24-29 12-24-34 12-24-34 12-24-38 12-24-38 12-24-38 12-24-38 12-24-38 12-24-38 12-24-38 12-24-38 12-24-38 12-24-38 12-24-38 12-24-38 12-24-38 12-24-38 12-24-38 12-24-38 12-24-38 12-24-38 12-24-38
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12-L.E.P. Page 12 Jan 01/07 SROS
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ _______ SUBJECT SERVICING - GENERAL ___________________ DESCRIPTION AND OPERATION General NO STEP Areas NO STEP Areas on the Wing NO STEP Areas on the THS Ground Service Connections Drainage Points General Hydraulic Safety Procedures Hydraulic System Pressurization Safety Instructions Applicable to Hydraulic Fluid Technical Safety Instructions
________ CH/SE/SU 12-00-00
____________________ SERVICING - GENERAL MAINTENANCE PRACTICES Installation of the Wing Safety Rope Removal of the Wing Safety Rope
12-00-00
____________ REPLENISHING DESCRIPTION AND OPERATION General
12-10-00
FUEL
12-11-00
DESCRIPTION AND OPERATION General FUEL SYSTEM SERVICING General Refuel/Defuel Safety Procedures Refuel/Defuel Safety Procedures In The Hangar Pressure Refuel with Automatic Control from the Panel 990VU Pressure Refuel With Manual Control Pressure Refuel with Automatic Control from the Cockpit Pressure Refuel with Manual Control and Override of Individual Inlet Valve(s)
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ALL ALL ALL ALL ALL ALL ALL ALL
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ALL ALL
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ALL ALL
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ALL ALL
1 1
ALL ALL
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ALL ALL
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12-CONTENTS R SROS
Page 1 Jan 01/07
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ _______ SUBJECT Overwing Refuel Procedure Procedure To Use The Fuel Magnetic Level Indicators Procedure To Use The ADIRU to Find the Pitch and Roll Data
CH/SE/SU ________
HYDRAULIC FLUIDS DESCRIPTION AND OPERATION General Specification of Phosphate Ester-Base Fluids Fluid Monitoring Hydraulic Ground Power Cart Hydraulic Fluid Property In-Service Limits Specification of Mineral-Base Fluids Safety Precautions HYDRAULIC POWER SERVICING Fill the Green Hydraulic Reservoir with a Hydraulic Service Cart Fill the Green Hydraulic Reservoir with a Hand Pump Fill the Blue Hydraulic Reservoir with a Hydraulic Service Cart Fill the Blue Hydraulic Reservoir with a Hand Pump Fill the Yellow Hydraulic Reservoir with a Hydraulic Service Cart Fill the Yellow Hydraulic Reservoir with a Hand Pump LANDING GEAR SERVICING Hydraulic Replenishment of the MLG Shock Absorber (Aircraft on Jacks) Hydraulic Replenishment of the MLG Shock Absorber (Weight on Wheels) Hydraulic Replenishment of the NLG Shock Absorber (Aircraft on Jacks)
12-12-00
OIL
12-13-00
DESCRIPTION AND OPERATION General ELECTRICAL POWER
C _
____ ___________ PAGE EFFECTIVITY A315 ALL A322 ALL B302
ALL
1 1 1
ALL ALL ALL
1 3 3
ALL ALL ALL
3
ALL
3
ALL
301 301
ALL ALL
308
ALL
314
ALL
320
ALL
327
ALL
332
ALL
301 301
ALL ALL
322
ALL
331
ALL
1 1
ALL ALL
12-12-29
12-12-32
12-13-24 12-CONTENTS
R SROS
Page 2 Jan 01/07
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ _______ SUBJECT SERVICING
CH/SE/SU ________
_ C 1
Draining of the Oil from the IDG
IDG Servicing - Filling of the IDG with Oil or Addition of Oil after a Level Check Drain IDG Oil System, Discard Filter Element and Replenish SERVICING Draining of the Oil from the IDG IDG Servicing - Filling of the IDG with Oil or Addition of Oil after Level Check Drain IDG Oil System, Discard Filter Element and Replenish FLIGHT CONTROLS SERVICING Oil Replenishing of the THS Actuator (1CS) Oil Replenishing of the Flap Power Control Unit (PCU) Gearbox (5000CV) Oil Replenishing of the Slat Power Control-Unit (PCU) Gearbox (5000CW) Drain and Refill the Rotary Actuators Oil Replenishing of the Flap System Torque Limiter (5003CV, 5081CV) Oil Replenishing of the Slat System Torque Limiter (5009CW, 5069CW) Semi-Fluid Sampling and Replenishing of the Input Gearbox (5007CV, 5022CV, 5032CV, 5042CV, 5053CV, 5085CV, 5100CV, 5110CV, 5120CV, 5131CV)
2
____ EFFECTIVITY PAGE ___________ 301 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 301 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 309 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 319 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 301 701-749, 301 701-749, 309 701-749, 318
701-749,
301 301
ALL ALL
306
ALL
313
ALL
318
ALL
328
ALL
334
ALL
340
002-049, 202-249 252-252, 255-299 301-399, 451-499 701-749,
12-13-27
12-CONTENTS R SROS
Page 3 Jul 01/06
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ _______ SUBJECT Oil Draining of the Flap/Slat PCU (5000CV, 5000CW) Oil Draining of the Flap/Slat System Torque Limiter (5003CV, 5081CV, 5009CW, 5069CW) Sampling of the SEMIFLUID from the Flap Rotary Actuator HYDRAULIC POWER SERVICING Oil Replenishment of the Ram Air Turbine (RAT) (11JR) APU SERVICING Gravity Servicing of the APU Oil Reservoir Pressure Servicing of the APU Oil Reservoir ENGINE OIL SERVICING
CH/SE/SU ________
C _
____ ___________ PAGE EFFECTIVITY 349 ALL 354
ALL
360
ALL
301 301
ALL ALL
301 301
ALL ALL
310
ALL
301
001-049, 251-252, 301-399, 451-499, 001-049, 251-252, 301-399, 451-499, 001-049, 251-252, 301-399, 451-499, 001-049, 251-252, 301-399, 451-499, 001-049, 251-252, 301-399, 451-499, 701-749, 701-749, 701-749,
12-13-29
12-13-49
12-13-79 1
Servicing of the Engine Oil System
301
Filling the Engine Oil System after the Replacement of an Oil System Component
311
Changing the Oil in the Engine Oil System
324
Flushing the Oil in the Engine Oil System.
337
SERVICING To Service the Engine Oil System Drain the Engine Oil System ENGINE STARTING SERVICING
2
301 301 311
1
301
SROS
201-249 255-299 401-449 201-249 255-299 401-449 201-249 255-299 401-449 201-249 255-299 401-449
12-13-80 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499,
12-CONTENTS R
201-249 255-299 401-449
Page 4 Jul 01/05
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ _______ SUBJECT Servicing of the Starter (Pressure and Gravity Fill - with Thrust Reverser Cowl Doors Open)
CH/SE/SU ________
C _
Change Starter Oil (with the Threaded Type Starter Magnetic Chip Detector (Vickers/Tedeco)) Change Starter Oil (with the Bayonet Type Starter Magnetic Chip Detector (Lisle)) Check and Replenish Starter Oil by Remote Fill - Through Access Door SERVICING To Service the Pneumatic Starter Oil System To Change the Oil in the Pneumatic Starter GAS DESCRIPTION AND OPERATION General HYDRAULIC POWER SERVICING Fill the Green Power Accumulator (5151JM1) with Nitrogen Fill the Blue Power Accumulator (5151JM2) with Nitrogen Fill the Yellow Power Accumulator (5151JM3) with Nitrogen LANDING GEAR SERVICING Replenishment of the Tires Gas Replenishment of the MLG Shock Absorber Gas Replenishment of the NLG Shock Absorber Pressurization of the Brake Accumulator (5258GG, 5259GG, 5490GG, 5491GG, 5426GG, 5427GG) Depressurization of the Brake Accumulator (5258GG, 5259GG, 5490GG, 5491GG, 5426GG and 5427GG)
2
____ EFFECTIVITY PAGE ___________ 301 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 311 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 323 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 336 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 301 701-749, 301 701-749, 308
701-749,
12-14-00 1 1
ALL ALL
301 301
ALL ALL
305
ALL
309
ALL
301 301 305
ALL ALL ALL
318
ALL
331
ALL
340
ALL
12-14-29
12-14-32
12-CONTENTS R SROS
Page 5 Jan 01/07
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ _______ SUBJECT Depressurization of the Nose Wheel Steering Accumulator 5110GC Pressurization of the Nose Wheel Steering Accumulator 5110GC OXYGEN SERVICING Servicing of the Oxygen Replenishing
CH/SE/SU ________
WATER DESCRIPTION AND OPERATION General POTABLE WATER SERVICING Fill the Potable Water System (Aircraft Electrical Power Available) Fill the Potable Water System (Aircraft Electrical Power not Available)
12-15-00
LAVATORY DESCRIPTION AND OPERATION General LAVATORY ARTICLE SERVICING Servicing of the Liquid Soap Dispenser TOILET SANITARY FLUID SERVICING Servicing of the Toilet System
12-16-00
RAIN REPELLENT DESCRIPTION AND OPERATION General ICE AND RAIN PROTECTION SERVICING Do a Check of Rain Repellent Fluid Can Assy For Correct Fluid Level and Pressure
12-17-00
___________________ SCHEDULED SERVICING DESCRIPTION AND OPERATION General
12-20-00
CLEANING
12-21-00
C _
____ ___________ PAGE EFFECTIVITY 348 ALL 353
ALL
301 301
ALL ALL
1 1
ALL ALL
301 301
ALL ALL
310
ALL
1 1
ALL ALL
301 301
ALL ALL
301 301
ALL ALL
1 1
ALL ALL
301 301
ALL ALL
1 1
ALL ALL
12-14-35
12-15-38
12-16-25
12-16-38
12-17-30
12-CONTENTS R SROS
Page 6 Jul 01/05
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ _______ SUBJECT DESCRIPTION AND OPERATION General EXTERNAL CLEANING SERVICING External Cleaning INTERNAL CLEANING SERVICING Cleaning of the Cockpit Display-Units Cleaning of the Cockpit Equipment/Furnishings Cleaning of the Carpets and Non-Textile Floor (NTF) Covering Cleaning of the Plastic Surfaces and Mirrors Cleaning of the Curtains Cleaning of Light Alloy and Steel Components Cleaning of the Cargo Compartments Cleaning of the Monitors and Display Screens in the Cabin Cleaning of the Plastic Wash Basin in the Lavatories Cleaning of the Seat Covers Cleaning of the Air Inlet Grids of Galleys and Lavatories Disinfection of the Aircraft Equipment and Furnishing Fumigation of the Aircraft Equipment and Furnishing Fumigation of the Fuselage Pressurized Areas with Carbon-Dioxide (CO2 Gas) Special Precautions to Apply Insecticide Agent in Auxiliary Area Compartments and Cargo Compartments, during Turn-Around DUST REMOVAL CLEANING/PAINTING Dust Removal Cleaning of Relay Box VU Panel Grids
CH/SE/SU ________
LUBRICATION DESCRIPTION AND OPERATION General
12-22-00
C _
____ ___________ PAGE EFFECTIVITY 1 ALL 1 ALL
12-21-11 301 301
ALL ALL
301 301
ALL ALL
304
ALL
309
ALL
312
ALL
319 321
ALL ALL
323 329
ALL ALL
331
ALL
336 339
ALL ALL
342
ALL
348
ALL
356
ALL
367
ALL
701 701 717
ALL ALL ALL
1 1
ALL ALL
12-21-12
12-21-13
12-CONTENTS R SROS
Page 7 Jan 01/07
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ SUBJECT _______ Lubrication Point Symbols: FLIGHT CONTROLS SERVICING Lubricate the Trimmable Horizontal Stabilizer (THS) Actuator Ball Screw Nut Lubricate the Trimmable Horizontal Stabilizer (THS) Mechanical Control Chains Lubrication of Flap Track/Carriage (1-5) Roller Bearings Lubrication of all Slat Track Roller Bearings, Pinion Bearings, Rack and Pinion Teeth and Slat Track 2 and 3 Lever Bearings Lubrication of all Spoiler Linkage Bearings fitted with Grease Nipples Lubrication of Flap Steady Bearings Lubrication of the Aileron Hinge Bearings Lubrication of Slat Rotary Actuator Type A (Track 2-3) Lubrication of Slat Rotary Actuator Type B (Track 5-16) Lubrication of Rudder Servo-Control Roller-Bearings (Rudder Side) Lubrication of the Aileron Actuator Roller Bearings Lubrication of Slat Steady Bearings Lubrication of the Elevator Actuator Roller Bearings LANDING GEAR SERVICING Lubrication of Main Landing Gear and Doors Lubrication of Nose Gear and Doors Lubrication of MLG Bogie Pivot Pin DOORS SERVICING Lubrication of the FWD Cargo-Compartment Door Hinge Arm Bearings, Locking Mechanism,
CH/SE/SU ________
C _
____ ___________ PAGE EFFECTIVITY 1 ALL
12-22-27 301 301
ALL ALL
307
ALL
316
ALL
322
ALL
329
ALL
334
ALL
339
ALL
345
ALL
352
ALL
367
ALL
373
ALL
379
ALL
385
ALL
301 301
ALL ALL
336 359
ALL ALL
301 301
ALL ALL
12-22-32
12-22-52
12-CONTENTS R SROS
Page 8 Jan 01/07
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ _______ SUBJECT Latching Mechanism and Interlock Mechanism Lubrication of the Telescopic Arm and Exterior Control Handle Lubrication of the Telescopic Arm and Exterior Control Handle Lubrication of the BULK Cargo-Compartment Door Lubrication of the AFT Cargo-Compartment Door Hinge Arm Bearings, Locking, Latching and Interlock Mechanism Lubrication of the Slider Mechanism on all Pax/Crew and Emergency Exit Doors FUSELAGE SERVICING Lubrication of the THS Hinge Line Bearings Lubrication of the THS Upper and Lower Frame Attachment Bearings STABILIZERS SERVICING Lubrication of the Rudder Bearing No. 6 WINDOWS SERVICING Servicing of the Sliding Windows
CH/SE/SU ________
DRAINAGE DESCRIPTION AND OPERATION General HYDRAULIC POWER SERVICING Servicing of the Leakage Recovery Tank (5230JM001, 5230JM002, 5230JM003) AIR DATA SYSTEM SERVICING Draining of the Standby Static Pressure-Lines POTABLE WATER SYSTEM MAINTENANCE PRACTICES Draining of the Potable Water System (with Electrical Power) Draining of the Potable Water
12-24-00
C _
PAGE ___________ ____ EFFECTIVITY 328
ALL
332
ALL
334
ALL
338
ALL
360
ALL
301 301
ALL ALL
305
ALL
301 301
ALL ALL
301 301
ALL ALL
1 1
ALL ALL
301 301
ALL ALL
301 301
ALL ALL
201 201
ALL ALL
217
ALL
12-22-53
12-22-55
12-22-56
12-24-29
12-24-34
12-24-38
12-CONTENTS R SROS
Page 9 Jul 01/06
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ _______ SUBJECT System (without Electrical Power)
CH/SE/SU ________
USE OF MANUAL MAGNETIC FUEL QUANTITY INDICATORS DESCRIPTION AND OPERATION General General
12-28-00
_____________________ UNSCHEDULED SERVICING DESCRIPTION AND OPERATION General
12-30-00
COLD WEATHER MAINTENANCE - AIRCRAFT PROTECTION DESCRIPTION AND OPERATION General Safe operation of aircraft in cold weather conditions raises specific problems. Aircraft downtime and delays in flight schedules caused by cold Procedures for cold weather servicing during cold weather must be developed by the operator. This servicing must meet their specific This topic contains information to assist the operator in defining, developing, and implementing cold weather preventive maintenance Cold Soak Definition De-icing and Anti-icing Guidelines De-Icing and Anti-Icing Glossary An aircraft performance certification is based upon that aircraft having an uncontaminated or clean structure. De-icing and/or Anti-icing Equipment and Materials ANTI-ICING PROTECTION MAINTENANCE PRACTICES Anti-Icing Protection ICE AND SNOW REMOVAL MAINTENANCE PRACTICES
12-31-00
C _
PAGE ___________ ____ EFFECTIVITY
1 1 1
ALL ALL 251-252, 701-749
1 1
ALL ALL
1 1 1
ALL ALL ALL
1
ALL
1
ALL
1 2 2 3
ALL ALL ALL ALL
4
ALL
201 201
ALL ALL
201
ALL
12-31-11 12-31-12 12-CONTENTS
R SROS
Page 10 Jul 01/06
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ _______ SUBJECT De-icing of the Aircraft Parked in an Open Area (Engines Stopped) De-icing of the Aircraft Parked in an Open Area (Engines Running) De-icing of the Aircraft after Landing with Snow on the Runways COLD WEATHER MAINTENANCE - AIR CONDITIONING MAINTENANCE PRACTICES Cold Weather Maintenance Practices for the Air Conditioning COLD WEATHER MAINTENANCE - ELECTRICAL POWER MAINTENANCE PRACTICES Cold Weather Maintenances for Electrical Power COLD WEATHER MAINTENANCE EQUIPMENT/FURNISHINGS MAINTENANCE PRACTICES Cold Weather Maintenance Practices for Equipment/Furnishings COLD WEATHER MAINTENANCE - FLIGHT CONTROLS MAINTENANCE PRACTICES Cold Weather Maintenance Procedures for Flight Controls COLD WEATHER MAINTENANCE - FUEL MAINTENANCE PRACTICES Cold Weather Maintenance Practices for the Fuel System COLD WEATHER MAINTENANCE INDICATING/RECORDING SYSTEMS AND NAVIGATION MAINTENANCE PRACTICES Cold Weather Maintenance Practices for Indicating/Recording and Navigation Systems COLD WEATHER MAINTENANCE - LANDING GEAR MAINTENANCE PRACTICES Cold Weather Maintenance Practices for the Landing Gear Cold Weather Protection for the Landing Gear Axles COLD WEATHER MAINTENANCE - OXYGEN MAINTENANCE PRACTICES
CH/SE/SU ________
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____ ___________ PAGE EFFECTIVITY 201 ALL 212
ALL
218
ALL
201 201
ALL ALL
201 201
ALL ALL
201 201
ALL ALL
201 201
ALL ALL
201 201
ALL ALL
201 201
ALL ALL
201 201
ALL ALL
203
ALL
201
ALL
12-31-21
12-31-24
12-31-25
12-31-27
12-31-28
12-31-31
12-31-32
12-31-35 12-CONTENTS
R SROS
Page 11 Jan 01/07
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ _______ SUBJECT Cold Weather Maintenance - Oxygen System COLD WEATHER MAINTENANCE - WATER/ WASTE MAINTENANCE PRACTICES Cold Weather Maintenance Practices for Water/Waste COLD WEATHER MAINTENANCE - AIRBORNE AUXILIARY POWER MAINTENANCE PRACTICES Cold Weather Maintenance Practices for the Auxiliary Power Unit COLD WEATHER MAINTENANCE - STRUCTURE MAINTENANCE PRACTICES Cold Weather Maintenance Practices for the Structure. COLD WEATHER MAINTENANCE - DOORS MAINTENANCE PRACTICES Cold Weather Maintenance Procedures for the Doors System COLD WEATHER MAINTENANCE - POWER PLANT MAINTENANCE PRACTICES Cold Weather Maintenance Practices of Engines
CH/SE/SU ________
SAMPLING FOR ANALYSIS DESCRIPTION AND OPERATION General
12-32-00
General INTEGRATED DRIVE GENERATOR OIL SERVICING
C _
12-31-38 201 201
ALL ALL
201 201
ALL ALL
201 201
ALL ALL
201 201
ALL ALL
201 201
ALL ALL
12-31-49
12-31-51
12-31-52
12-31-71
1 1
1
ALL 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 701-749,
12-32-24 1
Sampling of the IDG Oil for Analysis SERVICING Sampling of the IDG Oil for Analysis FUEL SERVICING
____ ___________ PAGE EFFECTIVITY 201 ALL
301
301 301
001-049, 251-252, 301-399, 451-499, 001-049, 251-252, 301-399, 451-499, 701-749, 701-749,
301
ALL
301
2
SROS
201-249 255-299 401-449
12-32-28 12-CONTENTS
R
201-249 255-299 401-449
Page 12 Jan 01/07
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ _______ SUBJECT Operate Water Drain Valves to Drain Accumulated Water from Center, Inner, Outer and Wing Vent Surge Tanks Operate Water Drain Valves to Drain Accumulated Water from Trim Tank and Trim Vent Surge Tank Draining of the Fuel/Air Separator Operate the Drain Valve of the Fuel/Air Separator to Drain any Accumulated Water Heating of Fuel/Air Separator Warm Fuel Procedure Heating of Fuel/Air Separator Hot Air Procedure Sample Fuel for Microbiological Contamination Analysis HYDRAULIC FLUID SERVICING Sampling for Analysis APU SERVICING Oil Sampling for Analysis ENGINE OIL SERVICING
CH/SE/SU ________
C _
308
ALL
315 320
ALL ALL
327
ALL
330
ALL
333
ALL
301 301
ALL ALL
301 301
ALL ALL
301
001-049, 251-252, 301-399, 451-499, 001-049, 251-252, 301-399, 451-499, 701-749, 701-749,
12-32-29 12-32-49 12-32-79 1
Sampling of the Engine Oil.
301
SERVICING Get a Sample of Engine Oil for Analysis PRE-CONDITIONING DESCRIPTION AND OPERATION General System Description Pre-conditioning with the Low Pressure (LP) Ground Connector Pre-conditioning with the High Pressure (HP) Ground Connector Pre-conditioning with the APU Bleed Air Supply
____ ___________ PAGE EFFECTIVITY 301 ALL
2
301 301
SROS
201-249 255-299 401-449
12-33-00 1 1 1 1
ALL ALL ALL ALL
1
ALL
1
ALL
12-CONTENTS R
201-249 255-299 401-449
Page 13 Jan 01/07
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ _______ SUBJECT GROUND AIR PRE-CONDITIONING MAINTENANCE PRACTICES Pre-conditioning through the Low-Pressure Ground Connection Pre-conditioning through the High-Pressure Ground Connection Pre-conditioning with the APU
________ CH/SE/SU 12-33-21
GROUNDING POINTS DESCRIPTION AND OPERATION General AIRCRAFT GROUNDING MAINTENANCE PRACTICES Aircraft Grounding for the Refuel/Defuel and Oxygen Servicing Operations Aircraft Grounding for the Maintenance Operations
12-34-00
SYSTEM LINE FLUSHING DESCRIPTION AND OPERATION General HYDRAULIC POWER SERVICING Flushing of the Case-Drain line of the Green Hydraulic System
12-36-00
C _
PAGE ___________ ____ EFFECTIVITY 201 201
ALL ALL
207
ALL
212
ALL
1 1
ALL ALL
201 201
ALL ALL
205
ALL
1 1
ALL ALL
12-34-24
12-36-29 301 301
Flushing of the Case-Drain line of the Green Hydraulic System Flushing of the HP line of the Green Hydraulic System
313
Flushing of the HP line of the Green Hydraulic System Flushing of the Case-Drain line of the Blue Hydraulic System
337
Flushing of the Case-Drain line of the Blue Hydraulic System Flushing of the HP line of the Blue Hydraulic System
358
326
347
368
ALL 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 701-749, 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 701-749, 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 701-749, 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499,
12-CONTENTS R SROS
Page 14 Jan 01/07
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ _______ SUBJECT Flushing of the HP line of the Blue Hydraulic System Flushing of the Case-Drain line of the Yellow Hydraulic System Flushing of the Case-Drain line of the Yellow Hydraulic System Flushing of the HP line of the Yellow Hydraulic System
CH/SE/SU ________
C _
____ ___________ PAGE EFFECTIVITY 378 701-749, 387
398 A308
Flushing of the HP line of the Yellow Hydraulic System Flushing of the Green Hydraulic System with the Aircraft Pumps
A318
Flushing of System with Flushing of System with
the the the the
Green Hydraulic Aircraft Pumps Blue Hydraulic Aircraft Pump
A331
Flushing of System with Flushing of System with
the the the the
Blue Hydraulic Aircraft Pump Yellow Hydraulic Aircraft Pump
A339
Flushing of the Yellow Hydraulic System with the Aircraft Pump Flushing of the Suction line of the Green Hydraulic System. Flushing of the Suction line of the Blue Hydraulic System. Flushing of the Suction line of the Yellow Hydraulic System. Replacement of the Hydraulic Fluid of the Green Hydraulic System with a Fluid Replacement and Recovery Bench Replacement of the Hydraulic Fluid of the Green Hydraulic System with a Fluid Replacement and Recovery Bench
A327
A335
A343
001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 701-749, 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 701-749, 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 701-749, 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 701-749,
A347
001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 701-749,
A351
ALL
A358
ALL
A365
ALL
A372
001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 701-749,
A393
12-CONTENTS R SROS
Page 15 Jan 01/07
CHAPTER 12 __________ SERVICING TABLE OF CONTENTS _________________ _______ SUBJECT Replacement of the Hydraulic Fluid of the Blue Hydraulic System with a Fluid Replacement and Recovery Bench Replacement of the Hydraulic Fluid of the Blue Hydraulic System with a Fluid Replacement and Recovery Bench Replacement of the Hydraulic Fluid of the Yellow Hydraulic System with a Fluid Replacement and Recovery Bench Replacement of the Hydraulic Fluid of the Yellow Hydraulic System with a Fluid Replacement and Recovery Bench Replacement of the Hydraulic Fluid of the Green Hydraulic System with the Green Electric Pump Replacement of the Hydraulic Fluid of the Blue Hydraulic System with the Blue Electric Pump Replacement of the Hydraulic Fluid of the Yellow Hydraulic System with the Yellow Electric Pump Reclaim the Fluid in the Green Hydraulic System Reclaim the Fluid in the Blue Hydraulic System Reclaim the Fluid in the Yellow Hydraulic System Clean the Fluid in the Green Hydraulic System (with the Pall Purifier) Clean the Fluid in the Blue Hydraulic System (with the Pall Purifier) Clean the Fluid in the Yellow Hydraulic System (with the Pall Purifier)
CH/SE/SU ________
C _
____ EFFECTIVITY PAGE ___________ B313 001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, B331 701-749,
B347
B365
001-049, 201-249 251-252, 255-299 301-399, 401-449 451-499, 701-749,
B381
ALL
C300
ALL
C316
ALL
C332
ALL
C337
ALL
C342
ALL
C347
ALL
C352
ALL
C357
ALL
12-CONTENTS R SROS
Page 16 Jan 01/07
SERVICING - GENERAL - DESCRIPTION AND OPERATION _______________________________________________ 1. _______ General This section gives the information related to the replenishing, scheduled and unscheduled servicing operations applicable to the aircraft. If includes the topics below: 12-10-00/P. Block 001 REPLENISHING 12-20-00/P. Block 001 SCHEDULED SERVICING 12-30-00/P. Block 001 UNSCHEDULED SERVICING 2. _______________ NO STEP Areas A. NO STEP Areas on the Wing (Ref. Fig. 001) B. NO STEP Areas on the THS (Ref. Fig. 002) 3. Ground __________________________ Service Connections The table gives the position of the ground service connection points. R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, (Ref. Fig. 003) **ON A/C 701-749, (Ref. Fig. 003A) **ON A/C ALL 4. Drainage _______________ Points The table gives the position of the drainage points. (Ref. Fig. 004) 5. ___________________________________ General Hydraulic Safety Procedures A. Hydraulic System Pressurization (1) Before you pressurize a hydraulic system: (a) Make sure that no person and no equipment is near flight control surfaces or landing gear doors.
EFF : ALL 12-00-00 SROS
Page 1 Jul 01/05
NO STEP Areas on the Wing Figure 001 EFF : ALL 12-00-00 SROS
Page 2 Apr 01/98
NO STEP Areas on the THS Figure 002 EFF : ALL 12-00-00 SROS
Page 3 Apr 01/98
Ground Service Points Figure 003 (SHEET 1) R EFF : 001-049, 201-249, 251-252, 255-299, 12-00-00 301-399, 401-449, 451-499, SROS
Page 4 Jul 01/05
Ground Service Points Figure 003 (SHEET 2) R EFF : 001-049, 201-249, 251-252, 255-299, 12-00-00 301-399, 401-449, 451-499, SROS
Page 5 Jul 01/05
R R
Ground Service Points Figure 003A (SHEET 1)
R EFF : 701-749, 12-00-00 SROS
Page 6 Oct 01/00
R R
Ground Service Points Figure 003A (SHEET 2)
R EFF : 701-749, 12-00-00 SROS
Page 7 Oct 01/00
Drainage Points Figure 004 (SHEET 1) EFF : ALL 12-00-00 R SROS
Page 8 Oct 01/00
Drainage Points Figure 004 (SHEET 2) EFF : ALL 12-00-00 R SROS
Page 9 Oct 01/00
(b) Use only the interphone system to get permission to pressurize the hydraulic system. B. Safety Instructions Applicable to Hydraulic Fluid (1) Do not mix phosphoric-ester-type hydraulic fluid and mineral-base hydraulic fluid: this mixture causes the formation of a gelatinous substance in the hydraulic system which can damage the system and decrease the aircraft safety. The first of these fluids is used in the hydraulic systems and the second fluid is used in the landing gear. Therefore you must obey safety precautions to prevent any mixture of fluids. (2) Before you start to work with hydraulic fluid, carefully read the following instructions and be sure that you understand them well. (a) Before you start to work, wash you hands, wrists and forearms and apply a protective cream. (b) Apply the protective cream under the finger nails and in the skin folds. (c) Put protective goggles when you do pressurization tests of systems or components or when you can get fluid into your eyes. (d) If you get hydraulic fluid in your eyes, flush it away immediately with a large quantity of clear cold water and make a report of the incident. (e) Wash your hands, wrists and forearms with soap and hot water when you could not prevent contact with hydraulic fluid. (f) Remove the clothes moist with hydraulic fluid as soon as possible. C. Technical Safety Instructions (1) Make sure that the hydraulic fluid does not cause damage to some materials such as rubber, copper, titanium, paint, plastic materials. (2) Make sure that the hydraulic fluid touches the hydraulic system components only, not the other items of the aircraft. Keep accidental spillage of hydraulic fluid to a minimum during maintenance procedures. Remove any sign of hydraulic fluid so that it does not extend to the adjacent areas and subsequently cause incorrect
EFF : ALL 12-00-00 SROS
Page 10 Oct 01/00
indications of leaks. Clean hydraulic-fluid contaminated areas with a dry cloth and solvent. (3) Use only solvent to clean metallic parts before you assemble them. Make sure that there is no more solvent when you assemble the parts. (4) Use only approved hydraulic fluid to fill hydraulic reservoirs, filter bowls, pumps or other hydraulic components before you install them. (5) Make sure that you have obeyed all precautions to prevent contamination of the hydraulic fluid by: - non-approved hydraulic fluids - fuel - oil - water - foreign bodies. (6) If a system is contaminated, keep the hydraulic fluid for analysis. (7) Before you connect the hydraulic service cart to the aircraft make sure that the specifications of the fluids of the service cart and the aircraft are the same.
EFF : ALL 12-00-00 SROS
Page 11 Oct 01/00
SERVICING - GENERAL - MAINTENANCE PRACTICES ___________________________________________ TASK 12-00-00-481-801 Installation of the Wing Safety Rope WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING _______ NOTICES ARE IN POSITION. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED ON THE _______ LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R R
No specific No specific No specific 98D27803000000 98F57004000000
warning notice square drive extension and ratchet handle 0.5 in. (12.6999 mm) access platform 5.8 m (19 ft.) 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER 1 SAFETY ROPE - WING
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------27-50-00-866-802 12-00-00-991-001
Retraction of the Flaps on the Ground Fig. 201
EFF : ALL 12-00-00 SROS
Page 201 Jan 01/02
3. __________ Job Set-up Subtask 12-00-00-866-050 A. Aircraft Maintenance Configuration R
(1) Make sure that the flaps and slats are retracted (Ref. TASK 27-50-00866-802). (2) Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) is correctly installed. Subtask 12-00-00-941-050 B. Safety Precautions (1) Put the warning notice in the cockpit, to tell persons not to operate the flap and slat control lever. Subtask 12-00-00-010-050 C. Get Access (1) Put the access platform at the leading edge. 4. Procedure _________ Subtask 12-00-00-210-050 A. Preparation for Installation (1) Make sure that the SAFETY ROPE - WING (98F57004000000) is serviceable. Subtask 12-00-00-481-050 B. Installation of the Wing Safety Rope (Ref. Fig. 201/TASK 12-00-00-991-001) (1) Put the SAFETY ROPE - WING (98F57004000000) in position on the wing, with the lashing ratchet assembly (10) inboard. (2) Remove and keep the blanking plug from Frame 43 in the fuselage. (3) Install the threaded plug (6) in Frame 43.
EFF : ALL 12-00-00 SROS
Page 202 Jan 01/07
Wing Safety Rope Figure 201/TASK 12-00-00-991-001 EFF : ALL 12-00-00 SROS
Page 203 Apr 01/98
(4) Connect the shackle (7), complete with the anchor plate (9) and the lashing ratchet assembly (10), to the threaded plug (6) with the shackle bolt (8). (5) Remove and keep the plug from the wing tip. R R
(6) Put the washer (2) in position and use the square drive extension and ratchet handle to install the screwed body assembly (1). (7) Install the shackle (5), complete with the safety rope (3), to the screwed body (1) with the shackle bolt (4). NOTE : The rope must not be loose, but do not tighten too much, it ____ can damage the aircraft. (8) Operate the lashing ratchet assembly (10) to tighten the SAFETY ROPEWING (98F57004000000). The tension must not be too loose or too tight. (9) Make sure that the safety lanyard (11) can move freely along the safety rope (3).
EFF : ALL 12-00-00 SROS
Page 204 Jan 01/02
TASK 12-00-00-081-801 Removal of the Wing Safety Rope WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING _______ NOTICES ARE IN POSITION. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED ON THE _______ LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
warning notice square drive extension and ratchet handle 0.5 in. (12.6999 mm) access platform 5.8 m (19 ft.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------27-50-00-866-802 12-00-00-991-001
Retraction of the Flaps on the Ground Fig. 201
EFF : ALL 12-00-00 SROS
Page 205 Apr 01/98
3. __________ Job Set-up Subtask 12-00-00-941-051 A. Safety Precautions R
(1) Make sure that the flaps and slats are retracted (Ref. TASK 27-50-00866-802). (2) Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) is installed. (3) Make sure that the warning notice is in the cockpit, to tell persons not the operate the flap and slat control lever. (4) Make sure that the access platform is at the leading edge at zone 560 and at zone 660. 4. Procedure _________ (Ref. Fig. 201/TASK 12-00-00-991-001) Subtask 12-00-00-081-050 A. Removal of the Wing Safety Rope (1) Operate the lashing ratchet (10) to release the tension of the SAFETY ROPE - WING (98F57004000000). (2) Remove the shackle bolt (4) and remove the shackle (5) from the screwed body (1). (3) Use the square drive extension and ratchet handle to remove the screwed body assembly (1). Remove the washer (2). (4) Install the blanking plug in the wing tip. (5) Carefully make a coil of the SAFETY ROPE - WING (98F57004000000) to the point of access. (6) Remove the shackle bolt (8) to disconnect the lashing ratchet assembly (10). Remove the threaded plug (6). (7) Install the blanking plug in the fuselage. (8) Remove the SAFETY ROPE - WING (98F57004000000) from the wing.
EFF : ALL 12-00-00 SROS
Page 206 Jan 01/07
5. Close-up ________ Subtask 12-00-00-942-050 A. Put the Aircraft back to its Initial Configuration (1) Remove the access platform. (2) Remove the warning notice. (3) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000).
EFF : ALL 12-00-00 SROS
Page 207 Apr 01/98
REPLENISHING - DESCRIPTION AND OPERATION ________________________________________ 1. _______ General This section gives the instructions related to the filling operations. It includes the topics below: 12-11-00/P. 12-12-00/P. 12-13-00/P. 12-14-00/P. 12-15-00/P. 12-16-00/P. 12-17-00/P.
Block Block Block Block Block Block Block
001 001 001 001 001 001 001
FUEL HYDRAULIC FLUIDS OIL GAS WATER TOILET SANITARY FLUID RAIN REPELLENT
EFF : ALL 12-10-00 SROS
Page 1 Apr 01/98
FUEL - DESCRIPTION AND OPERATION ________________________________ R R R R R R R R
1. General _______ This section gives the instructions and the safety precautions when you refuel the aircraft. It includes this topic: 12-11-28/P.Block 301 FUEL SYSTEM SERVICING The types of fuel that you are permitted to use in the fuel system are identified in 28-00-00/P.Block 301 FUEL - GENERAL - SERVICING.
EFF : ALL 12-11-00 SROS
Page 1 Jul 01/06
FUEL SYSTEM - SERVICING _______________________ TASK 12-11-28-650-801 General Refuel/Defuel Safety Procedures 1. __________________ Reason for the Job The procedure that follows contains information as specified in the IATA Guidance Material on Standard Into-Plane Fuelling Procedures 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-34-24-860-801 28-00-00-610-801 29-00-00-863-802 R
FCOM 2.01.30 FM 2.04.00 12-11-28-991-001
Aircraft Grounding for the Refuel/Defuel Operations Fuel Safety Procedures Pressurize the Blue Hydraulic System with the Electric Pump Fig. 301
3. __________ Job Set-up (Ref. Fig. 301/TASK 12-11-28-991-001) Subtask 12-11-28-941-058 A. Not Applicable 4. Procedure _________ Subtask 12-11-28-650-050 A. Safety Precautions R R
(1) You must obey the Fuel safety Procedures (Ref. TASK 28-00-00-610-801) when you refuel/defuel an aircraft. (2) Do not go near the aircraft until the anti-collision lights have been set to OFF.
EFF : ALL 12-11-28 SROS
Page 301 Jan 01/07
R
Refuel Safety Area Figure 301/TASK 12-11-28-991-001
EFF : ALL 12-11-28 SROS
Page 302 Apr 01/00
(3) Before you start the refuel/defuel procedure, make sure that all the electrical circuits in the fuel system are complete. (4) Do not start the refuel/defuel procedure if any part of the landing gear appears unusually hot. You must wait for the landing gear to cool. (5) Ground and bond the aircraft (Ref. TASK 12-34-24-860-801). NOTE : Bonding is essential, grounding is recommended. ____ (6) Move all equipment and material which is not necessary for the refuel/defuel procedure out of the safety area. (7) On panel 312 VU make sure that the ACCU PRESS on the triple indicator has sufficient pressure. If necessary, pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-802). (8) On the panel 117VU, make sure that the PARK BRK is ON. (9) Make sure that the chocks are in this position: (a) If the ramp does not slope: - move the aft NLG chocks away from the tires. During the refuel the NLG tires roll aft as the MLG shock absorber compresses. - make sure that the chocks do not touch the MLG tires. The weight of the fuel can lower the aircraft and cause the tires to catch the chocks (b) If the ramp slopes: - make sure that the chocks down from the tires touch the NLG and MLG tires - make sure that the chocks up from the tires do not touch the NLG and MLG tires. (10) Make sure that there is no equipment below the aircraft which can cause damage. The weight of the fuel can suddenly compress the landing gear and lower the aircraft. (11) Before you start the refuel/defuel procedure make sure that these are available: - a fuelling supervisor or fuelling safety person - the correct fire-fighting equipment - approved persons to use the fire-fighting equipment. (12) Make sure that the overboard vent lines are not blocked. If they are blocked, damage to the fuel tanks can occur. (13) Make sure that the fuel tanker (or hydrant) contains the correct fuel. The correct fuels are shown in the Flight Manual (Ref. FM 2.04.00). EFF : ALL 12-11-28 R SROS
Page 303 Jan 01/07
(14) Make sure that the fuel tanker (or, if you use a hydrant to refuel the aircraft, the pump unit) is in the correct position. (15) Make sure that, if there is an emergency, you can move the fuel tanker/pump unit and the support equipment away quickly. (16) Do not operate the aircraft main engines during a refuel/defuel procedure. R R
NOTE : In an emergency, you are permitted to refuel the aircraft with ____ one engine in operation (Ref. FCOM 2.01.30). (17) APU starts or stutdowns are permitted during refuel/defuel procedures. If it is necessary to operate the APU, the limits that follow apply: (a) An APU start is not permitted during a refuel/defuel procedure if the APU has failed to start or an automatic shutdown has occurred. (b) You must complete a normal APU shutdown if a fuel spill has occurred during the refuel/defuel procedure. (18) Make sure that all electrical equipment you use will not cause a spark. (19) Do not do a refuel/defuel procedure in bad weather conditions and electrical storms. Lightning is dangerous. (20) During the refuel/defuel procedure do not operate the aircraft external lighting. (21) During the refuel/defuel procedure do not fill the oxygen system or change the oxygen bottles. (22) During the refuel/defuel procedure do only essential aircraft maintenance and/or servicing that will not cause a spark. (23) Do not refuel the aircraft if a fire or engine overheat warning is displayed on the flight deck. (24) You are only permitted to replace or do small maintenance work on radio, radar and electrical equipment during refuelling. (25) You are not permitted to remove, install or test aircraft batteries or related equipment during refuelling.
EFF : ALL 12-11-28 SROS
Page 304 Jan 01/07
(26) Do not use the microphone on the High Frequency (HF) transmitter during refuel/defuel or fuel transfer operations. (27) Immediately flush away with water, or remove, fuel leakage. (28) Obey the safety distances for 60 meters (200 ft) from aircraft: (a) Stop the fuel tanker 60 meters (200 ft) from the aircraft nose while the weather radar operates. Do not operate the fuel tanker/pump unit until you stop operation of the weather radar. (29) Obey the safety distances for 30 meters (100 ft) from aircraft: (a) Aircraft must not be refueled/defueled less than 30 meters (100 ft) from radar or HF radio equipment under test or in operation in the aircraft or ground installation. (30) Obey the safety distances for 15 meters (50 ft) from aircraft: (Ref. Fig. 301/TASK 12-11-28-991-001) (a) Put NO SMOKING warning notices around the work area not less than 15 meters (50 ft) from the refueling/defueling equipment and aircraft and aircraft tank vents. (b) Do not connect electrical equipment to a power source less than 15 meters (50 ft) away, unless the power source has spark-proof connectors. (c) Refueling/defueling equipment and aircraft fuel-tank vents must not be nearer than 15 meters (50 ft) to a building during refuelling/defuelling. Make sure the position of the refuelling/defuelling area cannot let this occur. Because of the design of some buildings, you can do refuelling/defuelling operations nearer than 15 meters (50 ft). Examples of this type of building are nose loaders and aerobridges.
R R
(31) Obey the safety distances for 6 meters (20 ft) from aircraft (Ref. Fig. 301/TASK 12-11-28-991-001) (a) Ground power units (GPUs) can be operated when they are put not less than 6 meters (20 ft) from the aircraft filling and venting points, hydrant valves and other refueling/defueling equipment when in use. (b) Photographic flash bulbs or electronic flash equipment must not be used less than 6 meters (20 ft) of the refueling/defueling equipment or any filling or venting points of the aircraft.
EFF : ALL 12-11-28 SROS
Page 305 Jul 01/06
(c) The refueling/defueling zone must be regarded as extending not less than 6 meters (20 ft) radially from the filling and venting points on the aircraft and the fueling/defueling equipment and, when applicable, from the hydrant valve in use for refueling. When defueling is taking place, the vehicle will be venting and will generate a zone radiating from the tank vent. (d) Inside the 6 meter (20 ft) zone, radios, radio telephones (cell phones or mobile phones) and pagers as well as the operation of switches on lighting systems of other than intrinsically safe types are not allowed. Personnel in the refueling/defueling zone and those employed in refueling/defueling must not carry matches or other means of ignition or foot-wear with exposed iron or steel studs, nails or tips.
EFF : ALL 12-11-28 R SROS
Page 306 Jul 01/06
TASK 12-11-28-650-802 Refuel/Defuel Safety Procedures In The Hangar 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information Not Applicable 3. __________ Job Set-up Subtask 12-11-28-941-059 A. Not Applicable 4. Procedure _________ Subtask 12-11-28-650-051 A. Safety Precautions (1) Open all the hangar doors. Do not close the hangar doors until you have completed the refuel/defuel procedure. (2) Make the limits of the hangar the limits of the safety area. (a) The limit of the safety area is usually 15 m. But where the hangar wall is closer than 15 m, then the hangar wall is the limit of the safety area. (b) If a hangar entrance is closer than 15 m, then a safety barrier is to be positioned there. (3) To be prepared to tow the aircraft out of the hangar if an emergency occurs, do these steps: (a) Move all equipment which is not necessary for the refuel/defuel procedure from between the aircraft and the hangar exit. (b) Attach a towing vehicle to the aircraft. (4) Make sure that the driver of the fuel-tanker puts the fuel-tanker in the correct position adjacent to the aircraft. Keep the exit of the hangar clear for the fuel tanker.
EFF : ALL 12-11-28 R SROS
Page 307 Jul 01/04
TASK 12-11-28-650-803 Pressure Refuel with Automatic Control from the Panel 990VU WARNING : MAKE SURE THE AREA AROUND THE AIRCRAFT IS SAFE BEFORE YOU START A _______ REFUEL/DEFUEL PROCEDURE. IN THIS SAFE AREA, DO NOT LET PERSONS: - SMOKE - MAKE SPARKS OR FIRE - USE ANY EQUIPMENT WHICH IS NOT APPROVED FOR THE TASK. AIRCRAFT FUEL IS FLAMMABLE. WARNING : MAKE SURE THAT THE WHEEL CHOCKS ARE IN POSITION. MOVEMENTS OF THE _______ AIRCRAFT COULD BE DANGEROUS. WARNING : DO NOT SPILL FUEL ON THE ENGINES OR THE BRAKES. IF YOU SPILL FUEL ON _______ ENGINES OR BRAKES THAT ARE HOT, IT CAN CAUSE FIRES. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R
12-11-28-650-801 12-11-28-650-802 12-32-28-281-810 12-34-24-860-801 24-41-00-861-801 24-41-00-862-801 28-25-00-650-801
General Refuel/Defuel Safety Procedures Refuel/Defuel Safety Procedures In The Hangar Operate Water Drain Valves to Drain Accumulated Water from Center, Inner, Outer and Wing Vent Surge Tanks Aircraft Grounding for the Refuel/Defuel Operations Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Pressure Defuel Procedure
EFF : ALL 12-11-28 SROS
Page 308 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------28-25-00-869-801 29-00-00-863-802 34-10-00-860-801 34-10-00-860-803 12-11-28-991-001 12-11-28-991-002 12-11-28-991-003 12-11-28-991-026
Ground Fuel Transfer Procedure Pressurize the Blue Hydraulic System with the Electric Pump ADIRS Start Procedure ADIRS Stop Procedure Fig. 301 Fig. 302 Fig. 303 Fig. 304
3. __________ Job Set-up (Ref. Fig. 301/TASK 12-11-28-991-001, 302/TASK 12-11-28-991-002, 303/TASK 12-11-28-991-003, 304/TASK 12-11-28-991-026) Subtask 12-11-28-941-050 A. Safety Precautions WARNING : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND _______ DAMAGE. (1) Obey the safety procedures for the refuel procedure (Ref. TASK 12-1128-650-801) and if applicable (Ref. TASK 12-11-28-650-802). (2) On panel 312 VU make sure that the ACCU PRESS on the triple indicator has sufficiant pressure. If necessary, pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-802). (3) On the panel 117VU, make sure that the PARK BRK is ON. (4) Make sure that the chocks are in position as follows: - move the aft NLG chocks away from the tires. During the refuel the NLG tires roll aft as the MLG shock absorber compresses. - make sure that the chocks do not touch the MLG tires. The weight of the fuel can lower the aircraft and cause the tires to catch the chocks. R R
Subtask 12-11-28-281-052-A B. Water Contamination Check
R R
(1) Get a fuel sample from the fuel tanker/pump unit (Ref. TASK 12-32-28281-810) and do a check for water contamination.
EFF : ALL 12-11-28 SROS
Page 309 Jan 01/07
Refuel/Defuel Couplings Figure 302/TASK 12-11-28-991-002 EFF : ALL 12-11-28 R SROS
Page 310 Jul 01/04
Refuel/Defuel Control Panel 990VU Figure 303/TASK 12-11-28-991-003 EFF : ALL 12-11-28 R SROS
Page 311 Jul 01/04
Refuel Times - Refuel Pressure of 3.45 bar (50 psi) at the Refuel Coupling Figure 304/TASK 12-11-28-991-026 EFF : ALL 12-11-28 R SROS
Page 312 Jul 01/04
Subtask 12-11-28-860-052-A C. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT YOU GROUND THE FUEL TANKER AND THE AIRCRAFT _______ CORRECTLY. IF YOU DO NOT A DANGEROUS ELECTRICAL DISCHARGE CAN OCCUR. (1) Ground the aircraft and the fuel tanker/pump unit (Ref. TASK 12-3424-860-801). Then bond them together electrically. NOTE : Bonding is essential, grounding is recommended. ____ (2) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (3) Do the ADIRS start procedure (Ref. TASK 34-10-00-860-801). NOTE : If external electrical power or APU electrical power is not ____ available, it is possible to use the aircraft batteries to do an automatic refuel. But, on battery, the ADIRS does not send aircraft attitude information to the FCMS. Thus, on battery refuel, there could be a difference of up to 750 kg (1650 lb) between the set fuel quantity and the actual fuel quantity. Subtask 12-11-28-010-050 D. Get Access R R
NOTE : You can use 1, 2, 3 or 4 refuel hoses to do an automatic pressure ____ refuel. This procedure uses the four refuel hoses.
R R
(1) Put 2 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position, one below the access panel 522HB and one below the access panel 622HB. (2) Open the access panels 522HB and 622HB. (3) Remove the refuel/defuel coupling caps 5503QA1, 5503QA2, 5504QA1 and 5504QA2. (4) Examine the aircraft refuel/defuel couplings: WARNING : MAKE SURE THAT THE FUEL SUPPLY HOSE IS CORRECTLY CONNECTED _______ TO THE COUPLING BEFORE YOU REFUEL/DEFUEL THE AIRCRAFT. DO NOT CONNECT THE FUEL SUPPLY HOSE IF THERE ARE SIGNS OF DAMAGE TO THE AIRCRAFT COUPLING LUGS OR SLOTS.
EFF : ALL 12-11-28 SROS
Page 313 Jan 01/06
R R
(a) Visually examine the aircraft coupling lugs and slots for signs of damage or contamination.
R
(5) Make sure that the couplings of the fuel supply hoses are clean. Connect the four hoses to the aircraft refuel/defuel couplings 5502QA1 and 5502QA2.
R
(6) Open the access panel 198DB. Subtask 12-11-28-740-050 E. Do this test: ------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------On the refuel/defuel control panel 990VU: 1. If only the battery power is available, put the PWR SUPPLY switch to BAT. NOTE : During the first 30 ____ seconds after power-up, the indications at the fuel panel must be ignored. 2. Lift the guard, then push (in) and hold the HI LEVEL TEST switch 3QJ.
On the refuel/defuel control panel 990VU: - the hi-level lights (4QJ1, 4QJ2, 5QJ1, 5QJ2, 6QJ and 7QJ) and the OVERFLOW lights (8QJ1, 8QJ2 and 9QJ) go to the opposite condition - the CKPT and END lights come on - the fuel quantity, PRESELECTED and ACTUAL displays show all 8s.
3. Release (out) the HI-LEVEL TEST switch.
Wait for 10 seconds: - the lights go back to their initial condition - the fuel quantity, PRESELECTED and ACTUAL displays go back to their initial condition.
EFF : ALL 12-11-28 SROS
Page 314 Apr 01/05
4. Procedure _________ (Ref. Fig. 304/TASK 12-11-28-991-026) NOTE : An Automatic Refuel is only possible if the fuel quantity in each ____ tank at the start of the refuel is less than the expected quantity after the refuel. Subtask 12-11-28-650-063 A. Reference for Adjustment of the Fuel Distribution (if necessary) (1) If it becomes necessary to adjust the fuel distribution of the aircraft, do the (Ref. TASK 28-25-00-650-801) or the (Ref. TASK 2825-00-869-801). Subtask 12-11-28-650-052 R
B. Pressure Refuel with Automatic Control from the Panel 990VU CAUTION : DO NOT LET THE REFUEL PRESSURE GET TO MORE THAN 3.4 BAR (50 _______ PSI). THIS WILL PREVENT DAMAGE TO THE AIRCRAFT FUEL SYSTEM. (1) On the refuel/defuel control panel 990VU: (a) Put the LOAD switch 7QT to the INC position and hold it there. (b) Make sure that the numbers on the PRESELECTED display increase. (c) When the PRESELECTED display shows the necessary fuel load, release the LOAD switch. NOTE : To do a refuel, the figure set must be a minimum of 200 kg ____ (440.9244 lb) more than the FOB figure. (d) Make sure that the REFUEL VALVES switches (5QU1, 5QU2, 6QU1, 6QU2, 7QU, and 8QU) are in the NORM position and guarded. NOTE : If a switch is moved to SHUT during the automatic refuel, ____ the applicable valve closes. If a switch is moved to OPEN during the automatic refuel, the FCMS ignores the command until the automatic refuel is complete. Then, after approximately 15 seconds, the refuel will continue (in manual mode) into the applicable tank. (2) Start the pump on the fuel tanker/pump unit.
EFF : ALL 12-11-28 SROS
Page 315 Jan 01/07
(3) At the refuel/defuel control panel 990VU: (a) Put the MODE SELECT switch 3QU to the REFUEL position. NOTE : If the following switches are not in the correct ____ configuration, the END light will flash: - One or more of the inlet valve switches is in the OPEN or SHUT position - On the FUEL panel 245VU, the CTR TANK XFR switch is set to MAN - On the FUEL panel 245VU, the T TK FEED switch is set to OPEN or ISOL - On the FUEL panel 245VU, the T TANK MODE switch is set to FWD - On the FUEL panel 245VU, the OUTER TK XFR switch is set to MAN.
R R
(b) Make sure that the numbers on the fuel quantity and the ACTUAL displays increase. NOTE : The refuel times (shown in the illustration) give the ____ estimated time taken (in minutes) to refuel the aircraft from the initial (INIT) fuel quantity to the preselected fuel quantity. Each refuel-time range given makes an allowance for the densities from 0.76 kg/l to 0.82 kg/l, with a fuel pressure of 3.45 bar (50 psi) at the refuel coupling. (c) When the refuel stops, make sure that: - the END light comes on and does not flash - the numbers on the ACTUAL and the PRESELECTED displays are stable and are the same (-200 kg (-440.9244 lb) +200 kg (+440.9244 lb)). (d) Set the MODE SELECT switch to OFF. (e) If the power supply is from the battery, put the PWR SUPPLY switch to NORM. (4) Stop the pump on the fuel tanker/pump unit.
EFF : ALL 12-11-28 SROS
Page 316 Jan 01/07
5. Close-up ________ Subtask 12-11-28-410-050 A. Close Access (1) Disconnect the couplings of the four fuel supply hoses from the aircraft refuel/defuel couplings 5502QA1 and 5502QA2. (2) Install the refuel/defuel coupling caps 5503QA1, 5503QA2, 5504QA1 and 5504QA2. (3) Refuel panel closure CAUTION : DO NOT APPLY TOO MUCH FORCE TO THE OPERATING ROD WHEN YOU _______ CLOSE THE PANEL. THIS PREVENTS DAMAGE TO THE MECHANISM. (a) Close the access panels 522HB and 622HB. (4) Close the access panel 198DB. Subtask 12-11-28-860-053-A B. Aircraft Maintenance Configuration (1) If applicable, do the ADIRS stop procedure (Ref. TASK 34-10-00-860803). (2) If applicable, de-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). (3) Disconnect these ground/bonding cables: - the bonding cable between the aircraft and the fuel tanker/pump unit - if applicable, the grounding cable between the fuel tanker/pump unit and the ground - if applicable, the grounding cable between the aircraft and the ground. NOTE : The outer tank water drain valves have small holes in them to ____ prevent damage due to water freezing in the valve. These holes also let fuel flow from the outer tank to the inner tank at a rate of up to 20 kg/hour. This flow is normal and is to be expected. There is no leakage in the system.
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Subtask 12-11-28-942-050 C. Removal of Equipment (1) Put the chocks back in their original position. (2) Remove all the fixtures, tools, test and support equipment used during this procedure.
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TASK 12-11-28-650-804 Pressure Refuel With Manual Control WARNING : MAKE SURE THE AREA AROUND THE AIRCRAFT IS SAFE BEFORE YOU START A _______ REFUEL/DEFUEL PROCEDURE. IN THIS SAFE AREA, DO NOT LET PERSONS: - SMOKE - MAKE SPARKS OR FIRE - USE ANY EQUIPMENT WHICH IS NOT APPROVED FOR THE TASK. AIRCRAFT FUEL IS FLAMMABLE. WARNING : MAKE SURE THAT THE WHEEL CHOCKS ARE IN POSITION. MOVEMENTS OF THE _______ AIRCRAFT COULD BE DANGEROUS. WARNING : DO NOT SPILL FUEL ON THE ENGINES OR THE BRAKES. IF YOU SPILL FUEL ON _______ ENGINES OR BRAKES THAT ARE HOT, IT CAN CAUSE FIRES. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
2 access platforms 5.0 m (16 ft. 5 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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12-11-28-650-801 12-11-28-650-802 12-32-28-281-810 12-34-24-860-801 24-41-00-861-801 24-41-00-862-801 28-25-00-650-801
General Refuel/Defuel Safety Procedures Refuel/Defuel Safety Procedures In The Hangar Operate Water Drain Valves to Drain Accumulated Water from Center, Inner, Outer and Wing Vent Surge Tanks Aircraft Grounding for the Refuel/Defuel Operations Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Pressure Defuel Procedure
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------28-25-00-869-801 29-00-00-863-802 34-10-00-860-801 34-10-00-860-803 12-11-28-991-001 12-11-28-991-002 12-11-28-991-003 12-11-28-991-026 12-11-28-991-020-A
Ground Fuel Transfer Procedure Pressurize the Blue Hydraulic System with the Electric Pump ADIRS Start Procedure ADIRS Stop Procedure Fig. 301 Fig. 302 Fig. 303 Fig. 304 Fig. 305
**ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
12-11-28-991-020-B
Fig. 305A
**ON A/C ALL 12-11-28-991-021-A
Fig. 306
**ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
12-11-28-991-021-B
Fig. 306A
**ON A/C ALL 12-11-28-991-023-A
Fig. 307
**ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
12-11-28-991-023-B
Fig. 307A
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------**ON A/C ALL 12-11-28-991-024-A
Fig. 308
**ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
12-11-28-991-024-B
Fig. 308A
**ON A/C ALL 3. __________ Job Set-up (Ref. Fig. 301/TASK 12-11-28-991-001, 302/TASK 12-11-28-991-002, 303/TASK 12-11-28-991-003) Subtask 12-11-28-941-052 A. Safety Precautions WARNING : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND _______ DAMAGE. (1) Obey the safety procedures for the refuel procedure (Ref. TASK 12-1128-650-801) and if applicable (Ref. TASK 12-11-28-650-802). (2) On panel 312VU make sure that the ACCU PRESS on the triple indicator has sufficient pressure. If necessary, pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-802). (3) On the panel 117VU, make sure that the PARK BRK is ON. (4) Make sure that the chocks are in the position that follows: - move the aft NLG chocks away from the tires. During the refuel the NLG tires roll aft as the MLG shock absorber compresses. - make sure that the chocks do not touch the MLG tires. The weight of the fuel can lower the aircraft and cause the tires to catch the chocks.
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Subtask 12-11-28-281-054-A B. Fuel Sampling
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(1) Get a fuel sample from the fuel tanker/pump unit (Ref. TASK 12-32-28281-810) and do a check for water contamination.
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(2) If you use the manual refuel distribution graphs, use the fuel sample from the fuel tanker and measure its Specific Gravity (SG). Subtask 12-11-28-860-054 C. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT YOU GROUND THE FUEL TANKER AND THE AIRCRAFT _______ CORRECTLY. IF YOU DO NOT A DANGEROUS ELECTRICAL DISCHARGE CAN OCCUR. (1) Ground the aircraft and the fuel tanker/pump unit(s) (Ref. TASK 1234-24-860-801). Then bond them together electrically. NOTE : Bonding is essential, grounding is recommended. ____ (2) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (3) Do the ADIRS start procedure (Ref. TASK 34-10-00-860-801). NOTE : If external electrical power or APU electrical power is not ____ available, it is possible to use the aircraft batteries to do a manual refuel. But, on battery, the ADIRS do not send aircraft attitude information to the FCMS. Thus, on battery refuel, there could be a difference of up to 750 kg (1650 lb) between the set fuel quantity and the actual fuel quantity. Subtask 12-11-28-010-052 D. Get Access NOTE : You can use 1, 2, 3 or 4 refuel hoses to do a manual pressure ____ refuel. This procedure uses the four refuel hoses. (1) Put 2 access platforms in position, one below the access panel 522HB and one below the access panel 622HB. (2) Open the access panels 522HB and 622HB.
EFF : ALL 12-11-28 SROS
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(3) Remove the refuel/defuel coupling caps 5503QA1, 5503QA2, 5504QA1 and 5504QA2. (4) Examine the aircraft refuel/defuel couplings: WARNING : MAKE SURE THAT THE FUEL SUPPLY HOSE IS CORRECTLY CONNECTED _______ TO THE COUPLING BEFORE YOU REFUEL/DEFUEL THE AIRCRAFT. DO NOT CONNECT THE FUEL SUPPLY HOSE IF THERE ARE SIGNS OF DAMAGE TO THE AIRCRAFT COUPLING LUGS OR SLOTS. (a) Visually examine the aircraft coupling lugs and slots for signs of damage or contamination. (5) Make sure that the couplings of the fuel supply hoses are clean. Then connect them to the aircraft refuel/defuel couplings 5502QA1 and 5502QA2. (6) Open the access panel 198DB. Subtask 12-11-28-740-051 E. Do this test: ------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------On the refuel/defuel control panel 990VU: 1. If only battery power is available, put the PWR SUPPLY switch to BAT. 2. Lift the guard, then push (in) and hold the HI LEVEL TEST switch 3QJ.
On the refuel/defuel control panel 990VU: - the hi-level lights (4QJ1, 4QJ2, 5QJ1, 5QJ2, 6QJ and 7QJ) and the OVERFLOW lights (8QJ1, 8QJ2 and 9QJ) go to the opposite condition - the CKPT and END lights come on - the fuel quantity, PRESELECTED and ACTUAL displays show all 8s.
3. Release (out) the HI-LEVEL TEST
Wait for 10 seconds:
EFF : ALL 12-11-28 R SROS
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------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------switch. - the lights go back to their initial condition - the fuel quantity, PRESELECTED and ACTUAL displays go back to their initial condition. 4. Procedure _________ (Ref. Fig. 303/TASK 12-11-28-991-003, 304/TASK 12-11-28-991-026, 305/TASK 12-11-28-991-020-A) **ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
(Ref. Fig. 305A/TASK 12-11-28-991-020-B) **ON A/C ALL (Ref. Fig. 306/TASK 12-11-28-991-021-A) **ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
(Ref. Fig. 306A/TASK 12-11-28-991-021-B) **ON A/C ALL (Ref. Fig. 307/TASK 12-11-28-991-023-A) **ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
(Ref. Fig. 307A/TASK 12-11-28-991-023-B)
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Refuel Distribution Graphs - Density 0.77 to 0.795 Figure 305/TASK 12-11-28-991-020-A18 (SHEET 1) EFF : ALL 12-11-28 R SROS
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Refuel Distribution Graphs - Density 0.76 to 0.795 Figure 305A/TASK 12-11-28-991-020-B18 (SHEET 1) EFF : ALL 12-11-28 R SROS
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Refuel Distribution Graphs - Density 0.76 to 0.795 Figure 305A/TASK 12-11-28-991-020-B28 (SHEET 2) EFF : ALL 12-11-28 R SROS
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Refuel Distribution Graphs - Density 0.76 to 0.795 Figure 305A/TASK 12-11-28-991-020-B38 (SHEET 3) EFF : ALL 12-11-28 R SROS
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Refuel Distribution Graphs - Density 0.76 to 0.795 Figure 305A/TASK 12-11-28-991-020-B58 (SHEET 5) EFF : ALL 12-11-28 R SROS
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Refuel Distribution Graphs - Density 0.76 to 0.795 Figure 305A/TASK 12-11-28-991-020-B68 (SHEET 6) EFF : ALL 12-11-28 R SROS
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Refuel Distribution Graphs - Density 0.76 to 0.795 Figure 305A/TASK 12-11-28-991-020-B88 (SHEET 8) EFF : ALL 12-11-28 R SROS
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Refuel Distribution Graphs - Density 0.8 to 0.83 Figure 306/TASK 12-11-28-991-021-A17 (SHEET 1) EFF : ALL 12-11-28 R SROS
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Refuel Distribution Graphs - Density 0.8 to 0.83 Figure 306/TASK 12-11-28-991-021-A27 (SHEET 2) EFF : ALL 12-11-28 R SROS
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Refuel Distribution Graphs - Density 0.8 to 0.83 Figure 306A/TASK 12-11-28-991-021-B17 (SHEET 1) EFF : ALL 12-11-28 R SROS
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Refuel Distribution Tables - Density 0.76 to 0.795 Figure 307/TASK 12-11-28-991-023-A18 (SHEET 1) EFF : ALL 12-11-28 R SROS
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Manual Refuel Distribution Tables - Density 0.76 To 0.795 Figure 307A/TASK 12-11-28-991-023-B48 (SHEET 4) EFF : ALL 12-11-28 R SROS
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Manual Refuel Distribution Tables - Density 0.76 To 0.795 Figure 307A/TASK 12-11-28-991-023-B58 (SHEET 5) EFF : ALL 12-11-28 R SROS
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Manual Refuel Distribution Tables - Density 0.76 To 0.795 Figure 307A/TASK 12-11-28-991-023-B68 (SHEET 6) EFF : ALL 12-11-28 R SROS
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Manual Refuel Distribution Tables - Density 0.76 To 0.795 Figure 307A/TASK 12-11-28-991-023-B78 (SHEET 7) EFF : ALL 12-11-28 R SROS
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Manual Refuel Distribution Tables - Density 0.76 To 0.795 Figure 307A/TASK 12-11-28-991-023-B88 (SHEET 8) EFF : ALL 12-11-28 R SROS
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**ON A/C ALL (Ref. Fig. 308/TASK 12-11-28-991-024-A) **ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
(Ref. Fig. 308A/TASK 12-11-28-991-024-B) **ON A/C ALL NOTE : During the refuel procedure reference to the refuel graph can include ____ reference to the applicable fuel tables. Subtask 12-11-28-650-064 A. Reference for Adjustment of the Fuel Distribution (if necessary) (1) If it becomes necessary to adjust the fuel distribution of the aircraft, do the (Ref. TASK 28-25-00-650-801) or the (Ref. TASK 2825-00-869-801). Subtask 12-11-28-650-054 B. Pressure Refuel with Manual Control CAUTION : DO NOT LET THE REFUEL PRESSURE GET TO MORE THAN 3.4 BAR (50 _______ PSI). THIS WILL PREVENT DAMAGE TO THE AIRCRAFT FUEL SYSTEM. (1) On the refuel/defuel control panel 990VU, set the switches as follows: (a) Put the REFUEL/DEFUEL VALVE switch(es) for the fuel tank(s) you want to refuel, to the OPEN position. NOTE : To refuel the trim-tank, you must have one of these ____ conditions: - the two inner-tank inlet valves are open - the center-tank inlet valve is open. - the two inner tanks fuel quantities are above 14000 kg (30865 lb).
EFF : ALL 12-11-28 R SROS
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- one inner tank fuel quantity is above 14000 kg (30865 lb) and the other inner-tank inlet valve is open. (b) Put the REFUEL/DEFUEL VALVE switch(es) for the tank(s) you do not want to refuel, to the SHUT position. (2) Start the pump on the fuel tanker/pump unit. (3) On the refuel/defuel control panel 990VU: (a) Put the MODE SELECT switch 3QU to the REFUEL position. (b) If the refuel isolation valve(s) do not open, do the next step. 1 _
On the refuel isolation valve(s), push in and hold the override P/BSW.
(c) Monitor the fuel quantity displays. NOTE : If necessary, use the applicable manual refuel ____ distribution graph to make sure that the fuel distribution is correct for flight. (d) Make sure that the numbers on the fuel quantity and ACTUAL displays increase. (e) If the trim tank is to be refuelled, it must be done in two steps: 1 _
When the trim tank fuel quantity reaches 1000 kg (2200 lb) below that shown on the applicable graph, shut the trim tank inlet valve.
2 _
When the two inner tanks are at the target value (refuel graph), open the trim tank inlet valve. NOTE : If it is necessary to refuel the trim tank, the inner ____ tank quantity will be different from the quantity given in the manual refuel graph. An allowance for this difference must be made in the trim tank fuel quantity. This allowance will also have an effect on the cg of the aircraft (the cg change is approximately 2% MAC for each 1000 kg (2204 lb) difference from the distribution graphs for trim tank fuel quantity).
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Refuel Distribution Tables - Density 0.8 to 0.83 Figure 308/TASK 12-11-28-991-024-A17 (SHEET 1) EFF : ALL 12-11-28 R SROS
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Manual Refuel Distribution Tables - Density 0.8 To 0.83 Figure 308A/TASK 12-11-28-991-024-B17 (SHEET 1) EFF : ALL 12-11-28 R SROS
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Manual Refuel Distribution Tables - Density 0.8 To 0.83 Figure 308A/TASK 12-11-28-991-024-B27 (SHEET 2) EFF : ALL 12-11-28 R SROS
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(f) When each tank has the correct fuel quantity, put its REFUEL/DEFUEL VALVE switch to the SHUT position. NOTE : Each tank quantity can increase 100 kg (220 lb) to 200 kg ____ (440 lb) after the REFUEL/DEFUEL VALVE switch is set to SHUT. (4) When the fuel tank quantities are correct, set the refuel/defuel control on the panel 990VU as follows: (a) Put the MODE SELECT switch to the OFF position. (b) Put the applicable REFUEL VALVES switch(es) to the NORM position. (c) If the power supply is from the battery, put the PWR SUPPLY switch to NORM. (d) If it was necessary to operate the override P/BSW, do the next step. 1 _
On the refuel isolation valve(s), release the override P/BSW.
(5) Stop the pump on the fuel tanker/pump unit. 5. Close-up ________ Subtask 12-11-28-410-052 A. Close Access (1) Disconnect the couplings of the fuel supply hoses from the aircraft refuel/defuel couplings. (2) Install the refuel/defuel coupling caps 5503QA1, 5503QA2, 5504QA1 and 5504QA2. (3) Refuel panel closure: CAUTION : DO NOT APPLY TOO MUCH FORCE TO THE OPERATING ROD WHEN YOU _______ CLOSE THE PANEL. THIS PREVENTS DAMAGE TO THE MECHANISM. (a) Close the access panels 522HB and 622HB. (4) Close the access panel 198DB.
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Subtask 12-11-28-860-055 B. Aircraft Maintenance Configuration (1) If applicable, do the ADIRS stop procedure (Ref. TASK 34-10-00-860803). (2) If applicable, de-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). (3) Disconnect these ground/bonding cables: - the bonding cable between the aircraft and the fuel tanker/pump unit - if applicable, the grounding cable between the fuel tanker/pump unit and the ground - if applicable, the grounding cable between the aircraft and the ground. NOTE : The outer tank water drain valves have small holes in them to ____ prevent damage due to water freezing in the valve. These holes also let fuel flow from the outer tank to the inner tank at a rate of up to 20 kg/hour. This flow is normal and is to be expected. There is no leakage in the system. Subtask 12-11-28-942-052 C. Removal of Equipment (1) Put the chocks back in their original position. (2) Remove all the fixtures, tools, test and support equipment used during this procedure.
R EFF : ALL 12-11-28 SROS
Page 392 Jan 01/07
**ON A/C 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 701-749, TASK 12-11-28-650-807 Pressure Refuel with Automatic Control from the Cockpit WARNING : MAKE SURE THE AREA AROUND THE AIRCRAFT IS SAFE BEFORE YOU START A _______ REFUEL/DEFUEL PROCEDURE. IN THIS SAFE AREA, DO NOT LET PERSONS: - SMOKE - MAKE SPARKS OR FIRE - USE ANY EQUIPMENT WHICH IS NOT APPROVED FOR THE TASK. AIRCRAFT FUEL IS FLAMMABLE. WARNING : DO NOT SPILL FUEL ON THE ENGINES OR THE BRAKES. IF YOU SPILL FUEL ON _______ ENGINES OR BRAKES THAT ARE HOT, IT CAN CAUSE FIRES. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
two access platforms 5.0 m (16 ft. 5 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-11-28-650-801 12-11-28-650-802 12-32-28-281-806 12-34-24-860-801 24-41-00-861-801 24-41-00-862-801 28-25-00-650-801
General Refuel/Defuel Safety Procedures Refuel/Defuel Safety Procedures In The Hangar Operate Water Drain Valves to Drain Accumulated Water from Inner, Outer and Wing Vent Surge Tanks Aircraft Grounding for the Refuel/Defuel Operations Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Pressure Defuel Procedure
EFF : 201-249, 251-252, 255-299, 301-399, 12-11-28 401-449, 451-499, 701-749, R SROS
Page 393 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------28-25-00-869-801 29-00-00-863-802 31-60-00-860-801 34-10-00-860-801 34-10-00-860-803 12-11-28-991-009
Ground Fuel Transfer Procedure Pressurize the Blue Hydraulic System with the Electric Pump EIS Start Procedure ADIRS Start Procedure ADIRS Stop Procedure Fig. 309
3. __________ Job Set-up Subtask 12-11-28-941-060-A A. Safety Precautions WARNING : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND _______ DAMAGE. (1) Obey the safety procedures for the refuel procedure (Ref. TASK 12-1128-650-801) and (Ref. TASK 12-11-28-650-802). (2) Make sure that the Parking Brake System is pressurized (Ref. TASK 2900-00-863-802). (3) On the panel 117VU, make sure that the PARK BRK is ON. (4) Make sure that the chocks are in the position that follows: - move the aft NLG chocks away from the tires. During the refuel the NLG tires roll aft as the MLG shock absorber compresses - make sure that the chocks do not touch the MLG tires. The weight of the fuel can lower the aircraft and cause the tires to catch the chocks. Subtask 12-11-28-281-053-A B. Do a check for water contamination in a fuel sample removed from the fuel tanker/pump unit (Ref. TASK 12-32-28-281-806).
EFF : 201-249, 251-252, 255-299, 301-399, 12-11-28 401-449, 451-499, 701-749, R SROS
Page 394 Jan 01/07
Subtask 12-11-28-860-056-A C. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT YOU GROUND THE FUEL TANKER AND THE AIRCRAFT _______ CORRECTLY. IF YOU DO NOT A DANGEROUS ELECTRICAL DISCHARGE CAN OCCUR. (1) Ground the aircraft and the fuel tanker/pump unit (Ref. TASK 12-3424-860-801). Then bond them together electrically. NOTE : Bonding is essential, grounding is recommended. ____ (2) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (3) Do the ADIRS start procedure (Ref. TASK 34-10-00-860-801). (4) Energize the EIS (Ref. TASK 31-60-00-860-801). (5) Press the FUEL P/BSW and make sure that the FUEL page comes into view. Subtask 12-11-28-010-059 D. Get Access NOTE : You can use 1, 2, 3 or 4 refuel hoses to do an automatic pressure ____ refuel. This procedure uses four refuel hoses. (1) Put two access platforms in position, one below the access panel 522HB and one below the access panel 622HB. (2) Open the access panels 522HB and 622HB. (3) Remove the refuel/defuel coupling caps 5503QA1, 5503QA2, 5504QA1 and 5504QA2. (4) Examine the aircraft refuel/defuel couplings: WARNING : MAKE SURE THAT THE FUEL SUPPLY HOSE IS CORRECTLY CONNECTED _______ TO THE COUPLING BEFORE YOU REFUEL/DEFUEL THE AIRCRAFT. DO NOT CONNECT THE FUEL SUPPLY HOSE IF THERE ARE SIGNS OF DAMAGE TO THE AIRCRAFT COUPLING LUGS OR SLOTS. (a) Visually examine the aircraft coupling lugs and slots for signs of damage or contamination.
EFF : 201-249, 251-252, 255-299, 301-399, 12-11-28 401-449, 451-499, 701-749, R SROS
Page 395 Jan 01/07
(5) Make sure that the couplings of the fuel supply hoses are clean. Connect the four hoses to the aircraft refuel/defuel couplings 5502QA1 and 5502QA2. Subtask 12-11-28-740-052 E. Hi-Level Sense Test (1) Do this test: ------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------On the MCDU: 1. Push the line key adjacent to the LEVEL SENSE symbol.
On the MCDU: - the LEVEL SENSE TEST page shows TEST IN PROGRESS - when the test is complete the LEVEL SENSE TEST page shows TEST OK or a fault message.
(2) Push the line key adjacent to RETURN until the MCDU MENU page comes into view again. 4. Procedure _________ (Ref. Fig. 309/TASK 12-11-28-991-009) NOTE : An Automatic Refuel is only possible if the fuel quantity in each ____ tank at the start of the refuel is less than the expected quantity after the refuel. Subtask 12-11-28-650-065 A. Reference for Adjustment of the Fuel Distribution (if necessary) (1) If it becomes necessary to adjust the fuel distribution of the aircraft, do the (Ref. TASK 28-25-00-650-801) or the (Ref. TASK 2825-00-869-801).
EFF : 201-249, 251-252, 255-299, 301-399, 12-11-28 401-449, 451-499, 701-749, R SROS
Page 396 Jan 01/07
Refuel Control Panel in the Cockpit Figure 309/TASK 12-11-28-991-009 EFF : 201-249, 251-252, 255-299, 301-399, 12-11-28 401-449, 451-499, 701-749, R SROS
Page 397 Jan 01/07
Subtask 12-11-28-650-060-A B. To Input the Necessary Total Fuel Quantity (1) On the MCDU: (a) Push the INIT key and make sure that the INIT page comes into view. (b) Push the line key 2R. If a fuel quantity has not been set, an empty amber box is shown on the MCDU. (c) Use the numeric keys to set the necessary total fuel quantity. To do a refuel this quantity must be a minimum of 200 Kg (440 lb) more than the (ECAM) FOB quantity. (d) Push the line key 2R to input the set fuel quantity. To change the input fuel quantity, push the CLEAR key and the line key 2R together and do the procedure again. (e) Make sure that the INIT page now shows the correct total fuel quantity. NOTE : When you input the fuel quantity: ____ - the amber box goes out of view - on the refuel/defuel panel 990VU, the CKPT light comes on. When you have this condition, you cannot control the automatic refuel from the refuel/defuel panel 990VU. NOTE : Alternatively, the crew can use the flight plan to input ____ the necessary total fuel quantity. Subtask 12-11-28-650-061-A C. Pressure Refuel with Control from the Cockpit CAUTION : DO NOT LET THE REFUEL PRESSURE GET TO MORE THAN 3.4 BAR (50 _______ PSI). THIS WILL PREVENT DAMAGE TO THE AIRCRAFT FUEL SYSTEM. (1) Start the pump on the fuel tanker/pump unit.
EFF : 201-249, 251-252, 255-299, 301-399, 12-11-28 401-449, 451-499, 701-749, R SROS
Page 398 Jan 01/07
(2) On the FUEL panel 285VU: (a) Push (in) the REFUEL P/BSW (37QU). (b) Make sure that the ON light comes on. At the refuel/defuel coupling, the ready-to-refuel light also comes on. NOTE : When the REFUEL P/BSW is pushed in, the FCMS does an ____ automatic shut-off test. (3) On the ECAM lower SD, make sure that the tank quantities on the FUEL page increase. (4) When the refuel stops, make sure that: - the END light comes on and does not flash - on the ECAM the FOB and tank quantity displays are stable. (5) Stop the pump on the fuel tanker/pump unit. (6) On the FUEL panel 285VU: (a) Release (out) the REFUEL P/BSW. (b) Make sure that the ON and END lights go off. At the refuel/defuel coupling, the ready-to-refuel light also goes off. 5. Close-up ________ Subtask 12-11-28-410-057 A. Close Access (1) Disconnect the couplings of the four fuel supply hoses from the aircraft refuel/defuel couplings 5502QA1 and 5502QA2. (2) Install the refuel/defuel coupling caps 5503QA1, 5503QA2, 5504QA1 and 5504QA2. (3) Refuel panel closure: CAUTION : DO NOT APPLY TOO MUCH FORCE TO THE OPERATING ROD WHEN YOU _______ CLOSE THE PANEL. THIS PREVENTS DAMAGE TO THE MECHANISM. (a) Close the access panels 522HB and 622HB.
R EFF : 201-249, 251-252, 255-299, 301-399, 12-11-28 401-449, 451-499, 701-749, SROS
Page 399 Jan 01/07
Subtask 12-11-28-860-057-A B. Aircraft Maintenance Configuration (1) Put the aircraft back to its initial configuration. (a) On the ECAM control panel, set the UPPER DISPLAY and the LOWER DISPLAY potentiometers to OFF. (b) Do the ADIRS stop procedure (Ref. TASK 34-10-00-860-803). (c) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). (d) Disconnect these ground/bonding cables: - the bonding cable between the aircraft and the fuel tanker/pump unit - if applicable, the grounding cable between the fuel tanker/pump unit and the ground - if applicable, the grounding cable between the aircraft and the ground. NOTE : The outer tank water drain valves have small holes in them ____ to prevent damage due to water freezing in the valve. These holes also let fuel flow from the outer tank to the inner tank at a rate of up to 20 kg/hour. This flow is normal and is to be expected. There is no leakage in the system. Subtask 12-11-28-942-057 C. Removal of the Ground Support Equipment (1) Put the chocks back in their original position. (2) Make sure that the work area is clean and clear of tools and other items. (3) Remove the access platform(s). (4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
R EFF : 201-249, 251-252, 255-299, 301-399, 12-11-28 401-449, 451-499, 701-749, SROS
Page A300 Jan 01/07
**ON A/C ALL TASK 12-11-28-650-808 Pressure Refuel with Manual Control and Override of Individual Inlet Valve(s) WARNING : DO NOT SPILL FUEL ON THE ENGINES OR THE BRAKES. IF YOU SPILL FUEL ON _______ ENGINES OR BRAKES THAT ARE HOT, IT CAN CAUSE FIRES. 1. __________________ Reason for the Job To refuel with individual inlet valve(s) opened and closed with the deactivation tool. This will let refuel occur if the applicable actuators are inoperative. NOTE : You will need a minimum of three persons to do this task. ____ 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific D97B00-003
variable access platform access platform 3.0 m (9 ft. 10 in.) 2 access platforms 5.0 m (16 ft. 5 in.) 1 ACTUATOR MECHANICAL
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R
12-11-28-650-801 12-11-28-650-802 12-32-28-281-810 12-34-24-860-801 20-28-00-912-802 24-41-00-861-801
General Refuel/Defuel Safety Procedures Refuel/Defuel Safety Procedures In The Hangar Operate Water Drain Valves to Drain Accumulated Water from Center, Inner, Outer and Wing Vent Surge Tanks Aircraft Grounding for the Refuel/Defuel Operations Electrical Bonding of Components with Conductive Screws and Bolts and Bonding Straps Energize the Aircraft Electrical Circuits from the External Power A
EFF : ALL 12-11-28 SROS
Page A301 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-862-801 28-25-00-040-801 28-25-00-040-806 28-25-00-040-807 28-25-00-040-808 28-25-57-000-801 28-25-57-000-802 28-25-57-400-801 28-25-57-400-802 28-26-53-000-801 28-26-53-400-801 28-27-52-000-801 28-27-52-400-801 29-00-00-863-802 32-12-00-010-801 32-12-00-410-801 34-10-00-860-801 34-10-00-860-803 12-11-28-991-001 12-11-28-991-002 12-11-28-991-003 12-11-28-991-020-A
De-energize the Aircraft Electrical Circuits from the External Power A Deactivation of the Center-Tank Inlet Valve 5501QA in the Closed Position Deactivation of the Inner-Tank Inlet Valve 5603QA1(5603QA2) in the Closed Position Deactivation of the Outer-Tank Inlet Valve 5500QA1(5500QA2) in the Closed Position Deactivation of the Trim-Tank Inlet Valve 5705QA in the Closed Position Removal of the Outer-Tank Fuel Inlet-Valve Actuator 500QU1(500QU2) Removal of the Center-Tank Fuel Inlet-Valve Actuator 501QU Installation of the Outer-Tank Fuel Inlet-Valve Actuator 500QU1(500QU2) Installation of the Center-Tank Fuel Inlet-Valve Actuator 501QU Removal of the Fuel Inlet-Valve Actuator (603QL1,603QL2) Installation of the Fuel Inlet-Valve Actuator (603QL1,603QL2) Removal of the Inlet Valve Actuator 705QN Installation of the Inlet Valve Actuator 705QN Pressurize the Blue Hydraulic System with the Electric Pump Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance ADIRS Start Procedure ADIRS Stop Procedure Fig. 301 Fig. 302 Fig. 303 Fig. 305
**ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
12-11-28-991-020-B
Fig. 305A
EFF : ALL 12-11-28 R SROS
Page A302 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------**ON A/C ALL 12-11-28-991-021-A
Fig. 306
**ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
12-11-28-991-021-B
Fig. 306A
**ON A/C ALL 12-11-28-991-023-A
Fig. 307
**ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
12-11-28-991-023-B
Fig. 307A
**ON A/C ALL 12-11-28-991-024-A
Fig. 308
**ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
12-11-28-991-024-B
Fig. 308A
**ON A/C ALL 12-11-28-991-025
Fig. 310
EFF : ALL 12-11-28 R SROS
Page A303 Jan 01/07
3. __________ Job Set-up (Ref. Fig. 301/TASK 12-11-28-991-001, 302/TASK 12-11-28-991-002, 303/TASK 12-11-28-991-003) Subtask 12-11-28-941-062 A. Safety Precautions WARNING : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND _______ DAMAGE. (1) Obey the safety procedures for the refuel procedure (Ref. TASK 12-1128-650-801) and if applicable (Ref. TASK 12-11-28-650-802). (2) On panel 312VU make sure that the ACCU PRESS on the triple indicator has sufficient pressure. If necessary, pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-802). (3) On the panel 117VU, make sure that the PARK BRK is ON. (4) Make sure that the chocks are in the position that follows: - move the aft NLG chocks away from the tires. During the refuel the NLG tires roll aft as the MLG shock absorber compresses. - make sure that the chocks do not touch the MLG tires. The weight of the fuel can lower the aircraft and cause the tires to catch the chocks. R R
Subtask 12-11-28-281-056-A B. Fuel Sampling
R R
(1) Get a sample of fuel from the fuel tanker/pump unit (Ref. TASK 12-3228-281-810) and do a check for water contamination.
R R
(2) If you use the manual refuel distribution graphs, use the fuel sample from the fuel tanker and measure its Specific Gravity (SG). Subtask 12-11-28-860-058 C. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT YOU GROUND THE FUEL TANKER AND THE AIRCRAFT _______ CORRECTLY. IF YOU DO NOT A DANGEROUS ELECTRICAL DISCHARGE CAN OCCUR.
EFF : ALL 12-11-28 SROS
Page A304 Jan 01/07
(1) Ground the aircraft and the fuel tanker/pump unit(s) (Ref. TASK 1234-24-860-801). Then bond them together electrically. NOTE : Bonding is essential, grounding is recommended. ____ (2) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (3) Do the ADIRS start procedure (Ref. TASK 34-10-00-860-801). NOTE : If external electrical power or APU electrical power is not ____ available, it is possible to use the aircraft batteries to do a manual refuel. But, on battery, the ADIRS do not send aircraft attitude information to the FCMS. Thus, on battery refuel, there could be a difference of 750 kg (1650 lb) between the set fuel quantity and the actual fuel quantity. Subtask 12-11-28-010-060 D. Get Access NOTE : You can use 1, 2, 3 or 4 refuel hoses to do a manual pressure ____ refuel. This procedure uses the four refuel hoses. (1) Put 2 access platforms in position, one below the access panel 522HB and one below the access panel 622HB. (2) Open the access panels 522HB and 622HB. (3) Remove the refuel/defuel coupling caps 5503QA1, 5503QA2, 5504QA1 and 5504QA2. (4) Examine the aircraft refuel/defuel couplings: WARNING : MAKE SURE THAT THE FUEL SUPPLY HOSE IS CORRECTLY CONNECTED _______ TO THE COUPLING BEFORE YOU REFUEL/DEFUEL THE AIRCRAFT. DO NOT CONNECT THE FUEL SUPPLY HOSE IF THERE ARE SIGNS OF DAMAGE TO THE AIRCRAFT COUPLING LUGS OR SLOTS. (a) Visually examine the aircraft coupling lugs and slots for signs of damage or contamination. (5) Make sure that the couplings of the fuel supply hoses are clean. Then connect them to the aircraft refuel/defuel couplings 5502QA1 and 5502QA2. (6) Open the access panel 198DB.
EFF : ALL 12-11-28 R SROS
Page A305 Jan 01/07
Subtask 12-11-28-740-053 E. Do this test: ------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------On the refuel/defuel control panel 990VU: 1. If only battery power is available, put the PWR SUPPLY switch to BAT. 2. Lift the guard, then push (in) and hold the HI LEVEL TEST switch 3QJ.
On the refuel/defuel control panel 990VU: - the hi-level lights (4QJ1, 4QJ2, 5QJ1, 5QJ2, 6QJ and 7QJ) and the OVERFLOW lights (8QJ1, 8QJ2 and 9QJ) go to the opposite condition - the CKPT and END lights come on - the fuel quantity, PRESELECTED and ACTUAL displays show all 8s.
3. Release (out) the HI-LEVEL TEST switch.
Wait for 10 seconds: - the lights go back to their initial condition - the fuel quantity, PRESELECTED and ACTUAL displays go back to their initial condition.
Subtask 12-11-28-010-061 F. Get Access to the Applicable Refuel Valve(s) (Ref. Fig. 310/TASK 12-11-28-991-025) (1) For the inner tank inlet valve(s), do this step: (a) Open the MLG doors (Ref. TASK 32-12-00-010-801). FOR 5603QA1 open the LH MLG door FOR 5603QA2 open the RH MLG door.
EFF : ALL 12-11-28 R SROS
Page A306 Jan 01/07
Mechanical Actuator - Typical Installation Figure 310/TASK 12-11-28-991-025 EFF : ALL 12-11-28 R SROS
Page A307 Jan 01/07
(2) For the outer tank inlet valve(s), do these steps: (a) Put the access platform in position below the applicable zone 574(674), between STA 1208/RIB 18 and STA 1271/RIB 19. (b) Remove the applicable access panel: FOR the FOR the
5500QA1 panel 574FB 5500QA2 panel 674FB.
(3) For the center tank inlet valve, do this step: (a) Open one of the main landing gear doors (Ref. TASK 32-12-00-010801). (4) For the trim tank inlet valve, do this step: (a) Put the variable access platform in position at zone 319. (b) Remove the access panel 312AR. Subtask 12-11-28-480-050 G. Installation of the Mechanical Actuator Tool (Ref. Fig. 310/TASK 12-11-28-991-025) (1) Remove the applicable inlet valve actuator(s): - for the inner tanks (Ref. TASK 28-26-53-000-801) - for the outer tanks (Ref. TASK 28-25-57-000-801) - for the center tank (Ref. TASK 28-25-57-000-802) - for the trim tank (Ref. TASK 28-27-52-000-801). (2) Temporarily safety the electrical connector (1) away from the valve to prevent unwanted movement. (Ref. Fig. 310/TASK 12-11-28-991-025) (3) Install the ACTUATOR MECHANICAL (D97B00-003) (6), on the studs, with the nuts (2). (4) Connect the bonding strap (4) with the bolt (3) and the nut (5) (Ref. TASK 20-28-00-912-802).
EFF : ALL 12-11-28 R SROS
Page A308 Jan 01/07
4. Procedure _________ (Ref. Fig. 303/TASK 12-11-28-991-003, 305/TASK 12-11-28-991-020-A) **ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
(Ref. Fig. 305A/TASK 12-11-28-991-020-B) **ON A/C ALL (Ref. Fig. 306/TASK 12-11-28-991-021-A) **ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
(Ref. Fig. 306A/TASK 12-11-28-991-021-B) **ON A/C ALL (Ref. Fig. 307/TASK 12-11-28-991-023-A) **ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
(Ref. Fig. 307A/TASK 12-11-28-991-023-B) **ON A/C ALL (Ref. Fig. 308/TASK 12-11-28-991-024-A) **ON A/C ALL Post SB Post SB
28-3067 For A/C ALL 28-3079 For A/C ALL
(Ref. Fig. 308A/TASK 12-11-28-991-024-B)
EFF : ALL 12-11-28 R SROS
Page A309 Jan 01/07
**ON A/C ALL Subtask 12-11-28-650-062 A. Pressure Refuel with Manual Control CAUTION : DO NOT LET THE REFUEL PRESSURE GET TO MORE THAN 3.4 BAR (50 _______ PSI). THIS WILL PREVENT DAMAGE TO THE AIRCRAFT FUEL SYSTEM. (1) On the refuel/defuel control panel 990VU, set the switches as follows: (a) Put the REFUEL/DEFUEL VALVE switch(es) for the fuel tank(s) you want to refuel, to the OPEN position. (b) Put the REFUEL/DEFUEL VALVE switch(es) for the tank(s) you do not want to refuel, to the SHUT position. (c) Put the MODE SELECT switch 3QU to the REFUEL position. (2) For the applicable fuel tank(s), turn the ACTUATOR MECHANICAL to OPEN and lock it in that position. NOTE : To refuel the trim-tank, you must have one of these ____ conditions: - the two inner-tank inlet valves are open - the center-tank inlet valve is open - the two inner tanks fuel quantities are above 14,000 kg (30,865 lb) - one inner tank fuel quantity is above 14,000 kg (30,865 lb) and the other inner-tank inlet valve is open. (3) Start the pump on the fuel tanker/pump unit. If the refuel isolation valve(s) do not open, do the next step. (a) On the refuel isolation valve(s), push in and hold the override P/BSW. (4) On the refuel/defuel control panel 990VU: (a) Monitor the fuel quantity displays. NOTE : If necessary, use the applicable manual refuel ____ distribution graph to make sure that the fuel distribution is correct for flight.
EFF : ALL 12-11-28 R SROS
Page A310 Jan 01/07
(b) Make sure that the numbers on the fuel quantity and ACTUAL displays increase. (5) If the trim tank is to be refuelled, it must be done in two steps: (a) When the trim tank fuel quantity reaches 1000 kg (2200 lb) below that shown on the applicable graph, shut the trim tank inlet valve or (if applicable), turn the ACTUATOR MECHANICAL to SHUT and lock it in that position. (b) When the two inner tanks are at the target value (refuel graph), open the trim tank inlet valve or (if applicable), turn the ACTUATOR MECHANICAL to OPEN and lock it in that position. NOTE : If it is necessary to refuel the trim tank, the inner tank ____ quantity will be different from the quantity given in the manual refuel graph. An allowance for this difference must be made in the trim tank fuel quantity. This allowance will also have an effect on the cg of the aircraft (the cg change is approximately 2% MAC for each 1000 kg (2204 lb) difference from the distribution graphs for trim tank fuel quantity). (c) When each tank has the correct fuel quantity, put its REFUEL/DEFUEL VALVE switch to the SHUT position or (if applicable), turn the ACTUATOR MECHANICAL to SHUT and lock it in that position. NOTE : Each tank quantity can increase 100 kg (220 lb) to 200 kg ____ (440 lb) after the REFUEL/DEFUEL VALVE switch is set to SHUT or (if applicable), the ACTUATOR MECHANICAL is set to the SHUT position. (6) When the fuel tank quantities are correct, stop the pump on the fuel tanker/pump unit. If it was necessary to operate the override P/BSW, do the next step. (a) On the refuel isolation valve(s), release the override P/BSW. (7) Set the refuel/defuel control on the panel 990VU as follows: (a) Put the MODE SELECT switch to the OFF position. (b) Put the applicable REFUEL VALVES switch(es) to the NORM position. (c) If the power supply is from the battery, put the PWR SUPPLY switch to NORM.
EFF : ALL 12-11-28 R SROS
Page A311 Jan 01/07
5. Close-up ________ Subtask 12-11-28-080-050 A. Removal of the Mechanical Actuator Tool (Ref. Fig. 310/TASK 12-11-28-991-025) NOTE : Do not ____ one or - MMEL - MMEL - MMEL - MMEL
remove the applicable mechanical actuator tool if you did more of these de-activation procedures: 28-25-04-A (Ref. TASK 28-25-00-040-806) 28-25-04-B (Ref. TASK 28-25-00-040-801) 28-25-04-C (Ref. TASK 28-25-00-040-808) 28-25-04-D (Ref. TASK 28-25-00-040-807).
(1) Remove the temporary attachment from the electrical connector (1). (2) Remove the nut (5) and the bolt (3). (3) Disconnect the bonding strap (4). (4) Remove the nuts (2) and the ACTUATOR MECHANICAL (6). (5) Install the applicable inlet valve actuator(s): - for the inner tanks (Ref. TASK 28-26-53-400-801) - for the outer tanks (Ref. TASK 28-25-57-400-801) - for the center tank (Ref. TASK 28-25-57-400-802) - for the trim tank (Ref. TASK 28-27-52-400-801). Subtask 12-11-28-410-059 B. Close Access to the Applicable Refuel Valve(s) (1) For the inner tank(s) and/or center tank inlet valve(s), close the applicable MLG door (Ref. TASK 32-12-00-410-801). (2) For the outer tank inlet valve(s), do these steps: (a) Install the applicable access panel: FOR the FOR the
5500QA1 panel 574FB 5500QA2 panel 674FB.
(3) For the trim tank inlet valve, install the access panel 312AR.
EFF : ALL 12-11-28 R SROS
Page A312 Jan 01/07
Subtask 12-11-28-410-058 C. Close Access (1) Disconnect the couplings of the fuel supply hoses from the aircraft refuel/defuel couplings. (2) Install the refuel/defuel coupling caps 5503QA1, 5503QA2, 5504QA1 and 5504QA2. (3) Refuel panel closure CAUTION : DO NOT APPLY TOO MUCH FORCE TO THE OPERATING ROD WHEN YOU _______ CLOSE THE PANEL. THIS PREVENTS DAMAGE TO THE MECHANISM. (a) Close the access panels 522HB and 622HB. (4) Close the access panel 198DB. Subtask 12-11-28-860-059 D. Aircraft Maintenance Configuration (1) If applicable, do the ADIRS stop procedure (Ref. TASK 34-10-00-860803). (2) If applicable, de-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). (3) Disconnect these ground/bonding cables: - the bonding cable between the aircraft and the fuel tanker/pump unit - if applicable, the grounding cable between the fuel tanker/pump unit and the ground - if applicable, the grounding cable between the aircraft and the ground. NOTE : The outer tank water drain valves have small holes in them to ____ prevent damage due to water freezing in the valve. These holes also let fuel flow from the outer tank to the inner tank at a rate of up to 20 kg/hour. This flow is normal and is to be expected. There is no leakage in the system.
EFF : ALL 12-11-28 R SROS
Page A313 Jan 01/07
Subtask 12-11-28-942-058 E. Removal of the Ground Support Equipment (1) Put the chocks back in their original position. (2) Remove the access platform(s). (3) Remove the ground support and maintenance equipment, the special and standard tools and all other items. (4) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 12-11-28 R SROS
Page A314 Jan 01/07
TASK 12-11-28-650-805 Overwing Refuel Procedure WARNING : MAKE SURE THE AREA AROUND THE AIRCRAFT IS SAFE BEFORE YOU START A _______ REFUEL/DEFUEL PROCEDURE. IN THIS SAFE AREA, DO NOT LET PERSONS: - SMOKE - MAKE SPARKS OR FIRE - USE ANY EQUIPMENT WHICH IS NOT APPROVED FOR THE TASK. AIRCRAFT FUEL IS FLAMMABLE. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THE WHEEL CHOCKS ARE IN POSITION. MOVEMENTS OF THE _______ AIRCRAFT COULD BE DANGEROUS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific 98D27803000000
2 access platforms 5.8 m (19 ft.) 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
EFF : ALL 12-11-28 R SROS
Page A315 Jan 01/07
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-11-28-650-801 12-11-28-650-802 12-32-28-281-806 12-34-24-860-801 24-41-00-861-801 24-41-00-862-801 27-80-00-866-802 28-25-00-869-801 29-00-00-863-802 31-60-00-860-801 31-60-00-860-802 34-10-00-860-801 34-10-00-860-803 12-11-28-991-001 12-11-28-991-004
General Refuel/Defuel Safety Procedures Refuel/Defuel Safety Procedures In The Hangar Operate Water Drain Valves to Drain Accumulated Water from Inner, Outer and Wing Vent Surge Tanks Aircraft Grounding for the Refuel/Defuel Operations Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Retraction of the Slats on the Ground Ground Fuel Transfer Procedure Pressurize the Blue Hydraulic System with the Electric Pump EIS Start Procedure EIS Stop Procedure ADIRS Start Procedure ADIRS Stop Procedure Fig. 301 Fig. 311
3. __________ Job Set-up (Ref. Fig. 301/TASK 12-11-28-991-001, 311/TASK 12-11-28-991-004) Subtask 12-11-28-941-054 A. Safety Precautions WARNING : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND _______ DAMAGE. (1) Obey the safety procedures for the refuel procedure (Ref. TASK 12-1128-650-801) and if applicable (Ref. TASK 12-11-28-650-802). (2) On panel 312VU make sure that the ACCU PRESS on the triple indicator has sufficiant pressure. If necessary, pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-802). (3) On the panel 117VU, make sure that the PARK BRK is ON.
EFF : ALL 12-11-28 R SROS
Page A316 Jan 01/07
Overwing Refuel-Adaptor Cap Figure 311/TASK 12-11-28-991-004 EFF : ALL 12-11-28 R SROS
Page A317 Jan 01/07
(4) Make sure that the chocks are in the position that follows: - move the aft NLG chocks away from the tires. During the refuel the NLG tires roll aft as the MLG shock absorber compresses. - make sure that the chocks do not touch the MLG tires. The weight of the fuel can lower the aircraft and cause the tires to catch the chocks. Subtask 12-11-28-281-055 B. Make sure that a fuel sampling for water contamination check is done to the fuel in the fuel tanker/pump units (Ref. TASK 12-32-28-281-806). Subtask 12-11-28-860-050 C. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT YOU GROUND THE FUEL TANKER AND THE AIRCRAFT _______ CORRECTLY. IF YOU DO NOT A DANGEROUS ELECTRICAL DISCHARGE CAN OCCUR. (1) Ground the aircraft and the fuel tanker/pump unit(s) (Ref. TASK 1234-24-860-801). Then electrically bond them together. NOTE : Bonding is essential, grounding is recommended. ____ (2) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (3) Do the ADIRS start procedure (Ref. TASK 34-10-00-860-801). (4) Energize the EIS (Ref. TASK 31-60-00-860-801). (5) Push the FUEL pushbutton switch on the ECAM control panel. Read and make a record of the fuel contents. (6) Make sure the slats are retracted (Ref. TASK 27-80-00-866-802). (7) Installation of control locks WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE _______ WARNING NOTICES ARE IN POSITION. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. (a) Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) on the flap/slat control lever.
EFF : ALL 12-11-28 R SROS
Page A318 Jan 01/07
(b) Put a warning notice in the cockpit, to tell persons not to operate the flap/slat control. Subtask 12-11-28-941-055 D. Installation of Ground Support Equipment NOTE : The overwing refuel can be done through the LH wing, the RH wing ____ or the 2 wings. This procedure is through the 2 wings. (1) Position 2 access platforms adjacent to the wing leading edge. Put one near the overwing refuel cap 5508QA1 and one near the overwing refuel cap 5508QA2. 4. Procedure _________ WARNING : DO NOT GET AIRCRAFT FUEL: _______ - IN YOUR MOUTH - IN YOUR EYES - ON YOUR SKIN FOR A LONG TIME. WARNING : DO NOT GET YOUR CLOTHES SOAKED WITH FUEL. _______ AIRCRAFT FUEL IS POISONOUS AND CAN GO THROUGH YOUR SKIN INTO YOUR BODY. IF YOU ARE CONTAMINATED WASH WITH CLEAN WATER AND IF NECESSARY GET MEDICAL HELP. CAUTION : DO NOT LET THE REFUEL HOSE TOUCH THE SLATS. THIS WILL PREVENT _______ DAMAGE TO THE SLATS. Subtask 12-11-28-650-055-A A. Refuel Procedure CAUTION : KEEP THE RATE OF FUEL GROUND TRANSFER THE SAME AS (OR LESS _______ THAN) THE RATE OF FLOW INTO THE INNER TANK. (1) Connect the ground cables of the refuel nozzles to the wing ground connections. (2) Remove the overwing refuel caps 5508QA1 and 5508QA2. (3) Put the fuel nozzles in the overwing refuel points and start the pump on the fuel tanker/pump units.
EFF : ALL 12-11-28 R SROS
Page A319 Jan 01/07
(4) Start a ground fuel transfer from the inner tanks to the other fuel tanks (Ref. TASK 28-25-00-869-801). NOTE : You cannot use this procedure to fill the trim tank. ____ (5) Fill the inner tanks with the necessary amount of fuel. NOTE : Be careful not to overfill the tanks during refuel. There is ____ no automatic cut-out when you do the overwing refuel procedure. (6) When the fuel quantities are correct, stop the pump on the fuel tanker/pump unit. (7) Stop the ground fuel transfer (Ref. TASK 28-25-00-869-801). 5. Close-up ________ Subtask 12-11-28-410-054 A. Close Access (1) Remove the fuel nozzles from the overwing refuel points. (2) Install the overwing refuel caps 5508QA1 and 5508QA2. Make sure each cap is correctly aligned with the indicator arrow on the wing skin. (3) Disconnect the ground cables of the refuel nozzles from the wing ground connections. Subtask 12-11-28-860-051 B. Aircraft Maintenance Configuration (1) Disconnect these ground/bonding cables: - the bonding cable between the aircraft and the fuel tanker/pump unit - if applicable, the grounding cable between the fuel tanker/pump unit and the ground - if applicable, the grounding cable between the aircraft and the ground. (2) On the MCDU, push the line key adjacent to the RETURN indication until the MCDU MENU page comes into view. (3) On the MCDU, set the BRT knob to OFF.
EFF : ALL 12-11-28 R SROS
Page A320 Jan 01/07
(4) Do the EIS stop procedure (Ref. TASK 31-60-00-860-802). (5) Do the ADIRS stop procedure (Ref. TASK 34-10-00-860-803). (6) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). NOTE : The outer tank water drain valves have small holes in them to ____ prevent damage due to water freezing in the valve. These holes also let fuel flow from the outer tank to the inner tank at a rate of up to 20 kg/hour. This flow is normal and is to be expected. There is no leakage in the system. Subtask 12-11-28-942-054 C. Removal of Equipment (1) Put the chocks back in their original position. (2) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) from the flap/slat control lever and the warning notices from the cockpit. (3) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 12-11-28 R SROS
Page A321 Jan 01/07
TASK 12-11-28-650-806 Procedure To Use The Fuel Magnetic Level Indicators 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 4M (13 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-11-28-860-801 R R
12-32-28-281-810 28-51-00-740-803
Procedure To Use The ADIRU to Find the Pitch and Roll Data Operate Water Drain Valves to Drain Accumulated Water from Center, Inner, Outer and Wing Vent Surge Tanks Interrogation of the FCMS Input Parameters Pages
**ON A/C ALL Post SB
28-3078 For A/C 251-252,701-749,
12-11-28-991-007
Fig. 312
**ON A/C ALL 12-11-28-991-006-A 12-11-28-991-005 12-11-28-991-010
Fig. 313 Fig. 314 Fig. 315
EFF : ALL 12-11-28 SROS
Page A322 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------**ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
12-11-28-991-010-A
Fig. 315A
**ON A/C ALL 12-11-28-991-011
Fig. 316
**ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
12-11-28-991-011-A
Fig. 316A
**ON A/C ALL 12-11-28-991-012
Fig. 317
**ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
12-11-28-991-012-A
Fig. 317A
**ON A/C ALL 12-11-28-991-038
Fig. 318
**ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
12-11-28-991-038-A
Fig. 318A
**ON A/C ALL 12-11-28-991-014
Fig. 319
EFF : ALL 12-11-28 R SROS
Page A323 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------**ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
12-11-28-991-014-A
Fig. 319A
**ON A/C ALL 12-11-28-991-015
Fig. 320
**ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
12-11-28-991-015-A
Fig. 320A
**ON A/C ALL 12-11-28-991-016
Fig. 321
**ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
12-11-28-991-016-A
Fig. 321A
**ON A/C ALL 12-11-28-991-017
Fig. 322
**ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
12-11-28-991-017-A
Fig. 322A
**ON A/C ALL 12-11-28-991-018
Fig. 323
EFF : ALL 12-11-28 R SROS
Page A324 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------**ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
12-11-28-991-018-A
Fig. 323A
**ON A/C ALL 3. __________ Job Set-up (Ref. Fig. 312/TASK 12-11-28-991-007) Subtask 12-11-28-860-065 A. Aircraft Maintenance Configuration NOTE : The fuel quantity table for the inner tank MLI gives the fuel ____ value for the inner tank. This value includes the collector cell contents up to the same level as the adjacent inner tank. When the main fuel pumps operate, the collector cell fuel level is higher than for the inner tank. When the pumps operate (and for 10 minutes after they stop) this quantity of fuel cannot be calculated accurately. After 10 minutes, the fuel in the collector cell is at a known level and will decrease at a known rate. The Collector Cells - Correction Factor Graph identifies the quantity of fuel to add to the MLI quantity to get the correct inner tank contents. (1) Make a note of when the pumps were stopped. Use this time as the reference datum when you use the Collector Cells - Correction Factor Graph.
EFF : ALL 12-11-28 R SROS
Page A325 Jan 01/07
Collector Cells - Correction Factor Graph Figure 312/TASK 12-11-28-991-007 EFF : ALL 12-11-28 R SROS
Page A326 Jan 01/07
Subtask 12-11-28-941-061-A B. Get Access (1) Put an ACCESS PLATFORM 4M (13 FT) below the applicable fuel Magnetic Level Indicator (MLI). NOTE : The MLI in the center and inner tanks are accurate to plus or ____ minus 5% of their indication. The MLI in the outer tanks are accurate to plus or minus 7.5% of their indication. MLI values are not as accurate as the values given by the FCMC and you must not use them for comparison. Subtask 12-11-28-010-058 C. Get Access (1) Open the access panel 198DB. R R
Subtask 12-11-28-281-051-A D. Find the Specific Gravity
R R
(1) Get a fuel sample from the aircraft (Ref. TASK 12-32-28-281-810) and measure its Specific Gravity (SG).
R R
NOTE : The SG is also available on the FCMS Input Parameters Page 3 ____ (Ref. TASK 28-51-00-740-803). 4. Procedure _________ (Ref. Fig. 313/TASK 12-11-28-991-006-A, 314/TASK 12-11-28-991-005, 315/TASK 12-11-28-991-010) **ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
(Ref. Fig. 315A/TASK 12-11-28-991-010-A) **ON A/C ALL (Ref. Fig. 316/TASK 12-11-28-991-011)
EFF : ALL 12-11-28 SROS
Page A327 Jan 01/07
Magnetic Level Indicators - Location Figure 313/TASK 12-11-28-991-006-A EFF : ALL 12-11-28 R SROS
Page A328 Jan 01/07
Attitude Monitor - Location Figure 314/TASK 12-11-28-991-005 EFF : ALL 12-11-28 R SROS
Page A329 Jan 01/07
Fuel Quantity Tables - Center Tank MLI Figure 315/TASK 12-11-28-991-010- 17 (SHEET 1) EFF : ALL 12-11-28 R SROS
Page A330 Jan 01/07
Fuel Quantity Tables - Center Tank MLI Figure 315/TASK 12-11-28-991-010- 27 (SHEET 2) EFF : ALL 12-11-28 R SROS
Page A331 Jan 01/07
Fuel Quantity Tables - Center Tank MLI Figure 315/TASK 12-11-28-991-010- 37 (SHEET 3) EFF : ALL 12-11-28 R SROS
Page A332 Jan 01/07
Fuel Quantity Tables - Center Tank MLI Figure 315/TASK 12-11-28-991-010- 47 (SHEET 4) EFF : ALL 12-11-28 R SROS
Page A333 Jan 01/07
Fuel Quantity Tables - Center Tank MLI Figure 315/TASK 12-11-28-991-010- 57 (SHEET 5) EFF : ALL 12-11-28 R SROS
Page A334 Jan 01/07
Fuel Quantity Tables - Center Tank MLI Figure 315/TASK 12-11-28-991-010- 67 (SHEET 6) R EFF : ALL 12-11-28 SROS
Page A335 Jan 01/07
Fuel Quantity Tables - Center Tank MLI Figure 315/TASK 12-11-28-991-010- 77 (SHEET 7) R EFF : ALL 12-11-28 SROS
Page A336 Jan 01/07
INTENTIONALLY BLANK
R 12-11-28 SROS
Page A337 Jan 01/07
R
Fuel Quantity Tables - Center Tank MLI Figure 315A/TASK 12-11-28-991-010-A16 (SHEET 1)
EFF : 251-252, 701-749, 12-11-28 SROS
Page A338 Jan 01/07
R
Fuel Quantity Tables - Center Tank MLI Figure 315A/TASK 12-11-28-991-010-A26 (SHEET 2)
EFF : 251-252, 701-749, 12-11-28 SROS
Page A339 Jan 01/07
R
Fuel Quantity Tables - Center Tank MLI Figure 315A/TASK 12-11-28-991-010-A36 (SHEET 3)
EFF : 251-252, 701-749, 12-11-28 SROS
Page A340 Jan 01/07
R
Fuel Quantity Tables - Center Tank MLI Figure 315A/TASK 12-11-28-991-010-A46 (SHEET 4)
EFF : 251-252, 701-749, 12-11-28 SROS
Page A341 Jan 01/07
R
Fuel Quantity Tables - Center Tank MLI Figure 315A/TASK 12-11-28-991-010-A56 (SHEET 5)
R EFF : 251-252, 701-749, 12-11-28 SROS
Page A342 Jan 01/07
R
Fuel Quantity Tables - Center Tank MLI Figure 315A/TASK 12-11-28-991-010-A66 (SHEET 6)
R EFF : 251-252, 701-749, 12-11-28 SROS
Page A343 Jan 01/07
Fuel Quantity Tables - MLI No. 1 Figure 316/TASK 12-11-28-991-011- 16 (SHEET 1) EFF : ALL 12-11-28 R SROS
Page A344 Jan 01/07
Fuel Quantity Tables - MLI No. 1 Figure 316/TASK 12-11-28-991-011- 26 (SHEET 2) EFF : ALL 12-11-28 R SROS
Page A345 Jan 01/07
Fuel Quantity Tables - MLI No. 1 Figure 316/TASK 12-11-28-991-011- 36 (SHEET 3) EFF : ALL 12-11-28 R SROS
Page A346 Jan 01/07
Fuel Quantity Tables - MLI No. 1 Figure 316/TASK 12-11-28-991-011- 46 (SHEET 4) EFF : ALL 12-11-28 R SROS
Page A347 Jan 01/07
Fuel Quantity Tables - MLI No. 1 Figure 316/TASK 12-11-28-991-011- 56 (SHEET 5) EFF : ALL 12-11-28 R SROS
Page A348 Jan 01/07
Fuel Quantity Tables - MLI No. 1 Figure 316/TASK 12-11-28-991-011- 66 (SHEET 6) EFF : ALL 12-11-28 R SROS
Page A349 Jan 01/07
**ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
(Ref. Fig. 316A/TASK 12-11-28-991-011-A) **ON A/C ALL (Ref. Fig. 317/TASK 12-11-28-991-012) **ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
(Ref. Fig. 317A/TASK 12-11-28-991-012-A) **ON A/C ALL (Ref. Fig. 318/TASK 12-11-28-991-038) **ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
(Ref. Fig. 318A/TASK 12-11-28-991-038-A) **ON A/C ALL (Ref. Fig. 319/TASK 12-11-28-991-014) **ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
(Ref. Fig. 319A/TASK 12-11-28-991-014-A) **ON A/C ALL (Ref. Fig. 320/TASK 12-11-28-991-015)
R EFF : ALL 12-11-28 SROS
Page A350 Jan 01/07
**ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
(Ref. Fig. 320A/TASK 12-11-28-991-015-A) **ON A/C ALL (Ref. Fig. 321/TASK 12-11-28-991-016) **ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
(Ref. Fig. 321A/TASK 12-11-28-991-016-A) **ON A/C ALL (Ref. Fig. 322/TASK 12-11-28-991-017) **ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
(Ref. Fig. 322A/TASK 12-11-28-991-017-A) **ON A/C ALL (Ref. Fig. 323/TASK 12-11-28-991-018) **ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
(Ref. Fig. 323A/TASK 12-11-28-991-018-A)
R EFF : ALL 12-11-28 SROS
Page A351 Jan 01/07
Fuel Quantity Tables - MLI No. 1 Figure 316A/TASK 12-11-28-991-011-A16 (SHEET 1) EFF : 251-252, 701-749, 12-11-28 R SROS
Page A352 Jan 01/07
Fuel Quantity Tables - MLI No. 1 Figure 316A/TASK 12-11-28-991-011-A26 (SHEET 2) EFF : 251-252, 701-749, 12-11-28 R SROS
Page A353 Jan 01/07
Fuel Quantity Tables - MLI No. 1 Figure 316A/TASK 12-11-28-991-011-A36 (SHEET 3) EFF : 251-252, 701-749, 12-11-28 R SROS
Page A354 Jan 01/07
Fuel Quantity Tables - MLI No. 1 Figure 316A/TASK 12-11-28-991-011-A46 (SHEET 4) EFF : 251-252, 701-749, 12-11-28 R SROS
Page A355 Jan 01/07
Fuel Quantity Tables - MLI No. 1 Figure 316A/TASK 12-11-28-991-011-A56 (SHEET 5) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A356 Jan 01/07
Fuel Quantity Tables - MLI No. 1 Figure 316A/TASK 12-11-28-991-011-A66 (SHEET 6) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A357 Jan 01/07
Fuel Quantity Tables - MLI No. 2 Figure 317/TASK 12-11-28-991-012- 14 (SHEET 1) EFF : ALL 12-11-28 R SROS
Page A358 Jan 01/07
Fuel Quantity Tables - MLI No. 2 Figure 317/TASK 12-11-28-991-012- 24 (SHEET 2) EFF : ALL 12-11-28 R SROS
Page A359 Jan 01/07
Fuel Quantity Tables - MLI No. 2 Figure 317/TASK 12-11-28-991-012- 34 (SHEET 3) R EFF : ALL 12-11-28 SROS
Page A360 Jan 01/07
Fuel Quantity Tables - MLI No. 2 Figure 317/TASK 12-11-28-991-012- 44 (SHEET 4) R EFF : ALL 12-11-28 SROS
Page A361 Jan 01/07
Fuel Quantity Tables - MLI No. 2 Figure 317A/TASK 12-11-28-991-012-A14 (SHEET 1) EFF : 251-252, 701-749, 12-11-28 R SROS
Page A362 Jan 01/07
Fuel Quantity Tables - MLI No. 2 Figure 317A/TASK 12-11-28-991-012-A24 (SHEET 2) EFF : 251-252, 701-749, 12-11-28 R SROS
Page A363 Jan 01/07
Fuel Quantity Tables - MLI No. 2 Figure 317A/TASK 12-11-28-991-012-A34 (SHEET 3) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A364 Jan 01/07
Fuel Quantity Tables - MLI No. 2 Figure 317A/TASK 12-11-28-991-012-A44 (SHEET 4) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A365 Jan 01/07
Fuel Quantity Tables - MLI No. 3 Figure 318/TASK 12-11-28-991-038- 13 (SHEET 1) EFF : ALL 12-11-28 R SROS
Page A366 Jan 01/07
Fuel Quantity Tables - MLI No. 3 Figure 318/TASK 12-11-28-991-038- 23 (SHEET 2) R EFF : ALL 12-11-28 SROS
Page A367 Jan 01/07
Fuel Quantity Tables - MLI No. 3 Figure 318/TASK 12-11-28-991-038- 33 (SHEET 3) R EFF : ALL 12-11-28 SROS
Page A368 Jan 01/07
INTENTIONALLY BLANK
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Page A369 Jan 01/07
Fuel Quantity Tables - MLI No. 3 Figure 318A/TASK 12-11-28-991-038-A13 (SHEET 1) EFF : 251-252, 701-749, 12-11-28 R SROS
Page A370 Jan 01/07
Fuel Quantity Tables - MLI No. 3 Figure 318A/TASK 12-11-28-991-038-A23 (SHEET 2) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A371 Jan 01/07
Fuel Quantity Tables - MLI No. 3 Figure 318A/TASK 12-11-28-991-038-A33 (SHEET 3) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A372 Jan 01/07
INTENTIONALLY BLANK
R 12-11-28 SROS
Page A373 Jan 01/07
Fuel Quantity Tables - MLI No. 4 Figure 319/TASK 12-11-28-991-014- 13 (SHEET 1) EFF : ALL 12-11-28 R SROS
Page A374 Jan 01/07
Fuel Quantity Tables - MLI No. 4 Figure 319/TASK 12-11-28-991-014- 23 (SHEET 2) R EFF : ALL 12-11-28 SROS
Page A375 Jan 01/07
Fuel Quantity Tables - MLI No. 4 Figure 319/TASK 12-11-28-991-014- 33 (SHEET 3) R EFF : ALL 12-11-28 SROS
Page A376 Jan 01/07
INTENTIONALLY BLANK
R 12-11-28 SROS
Page A377 Jan 01/07
Fuel Quantity Tables - MLI No. 4 Figure 319A/TASK 12-11-28-991-014-A13 (SHEET 1) EFF : 251-252, 701-749, 12-11-28 R SROS
Page A378 Jan 01/07
Fuel Quantity Tables - MLI No. 4 Figure 319A/TASK 12-11-28-991-014-A23 (SHEET 2) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A379 Jan 01/07
Fuel Quantity Tables - MLI No. 4 Figure 319A/TASK 12-11-28-991-014-A33 (SHEET 3) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A380 Jan 01/07
INTENTIONALLY BLANK
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Page A381 Jan 01/07
Fuel Quantity Tables - MLI No. 5 Figure 320/TASK 12-11-28-991-015- 12 (SHEET 1) R EFF : ALL 12-11-28 SROS
Page A382 Jan 01/07
Fuel Quantity Tables - MLI No. 5 Figure 320/TASK 12-11-28-991-015- 22 (SHEET 2) R EFF : ALL 12-11-28 SROS
Page A383 Jan 01/07
Fuel Quantity Tables - MLI No. 5 Figure 320A/TASK 12-11-28-991-015-A12 (SHEET 1) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A384 Jan 01/07
Fuel Quantity Tables - MLI No. 5 Figure 320A/TASK 12-11-28-991-015-A22 (SHEET 2) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A385 Jan 01/07
Fuel Quantity Tables - MLI No. 6 Figure 321/TASK 12-11-28-991-016- 12 (SHEET 1) R EFF : ALL 12-11-28 SROS
Page A386 Jan 01/07
Fuel Quantity Tables - MLI No. 6 Figure 321/TASK 12-11-28-991-016- 22 (SHEET 2) R EFF : ALL 12-11-28 SROS
Page A387 Jan 01/07
Fuel Quantity Tables - MLI No. 6 Figure 321A/TASK 12-11-28-991-016-A12 (SHEET 1) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A388 Jan 01/07
Fuel Quantity Tables - MLI No. 6 Figure 321A/TASK 12-11-28-991-016-A22 (SHEET 2) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A389 Jan 01/07
Fuel Quantity Tables - MLI No. 7 Figure 322/TASK 12-11-28-991-017- 12 (SHEET 1) R EFF : ALL 12-11-28 SROS
Page A390 Jan 01/07
Fuel Quantity Tables - MLI No. 7 Figure 322/TASK 12-11-28-991-017- 22 (SHEET 2) R EFF : ALL 12-11-28 SROS
Page A391 Jan 01/07
Fuel Quantity Tables - MLI No. 7 Figure 322A/TASK 12-11-28-991-017-A12 (SHEET 1) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A392 Jan 01/07
Fuel Quantity Tables - MLI No. 7 Figure 322A/TASK 12-11-28-991-017-A22 (SHEET 2) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A393 Jan 01/07
Fuel Quantity Tables - MLI No. 8 Figure 323/TASK 12-11-28-991-018- 12 (SHEET 1) R EFF : ALL 12-11-28 SROS
Page A394 Jan 01/07
Fuel Quantity Tables - MLI No. 8 Figure 323/TASK 12-11-28-991-018- 22 (SHEET 2) R EFF : ALL 12-11-28 SROS
Page A395 Jan 01/07
Fuel Quantity Tables - MLI No. 8 Figure 323A/TASK 12-11-28-991-018-A12 (SHEET 1) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A396 Jan 01/07
Fuel Quantity Tables - MLI No. 8 Figure 323A/TASK 12-11-28-991-018-A22 (SHEET 2) R EFF : 251-252, 701-749, 12-11-28 SROS
Page A397 Jan 01/07
**ON A/C ALL Subtask 12-11-28-869-054-B A. Procedure to Use the Magnetic Level Indicators CAUTION : DO NOT LET THE MLIs FALL FREELY. _______ THE MLIs ARE FRAGILE. CAUTION : RETRACT THE MLIs AS SOON AS POSSIBLE. YOU CAN EASILY CAUSE _______ DAMAGE TO AN EXTENDED MLI. NOTE : Start the procedure with each of the outboard MLIs in the Outer ____ and Inner Tank. If they give no indication move inboard to each subsequent MLI until the MLI gives an indication. At the first MLI that gives an indication, use that MLI for the procedure. NOTE : If the attitude monitor is unservicable, refer to (Ref. TASK 12____ 11-28-860-801). (1) Use a screwdriver to push (in) the applicable MLI and turn it through 90 deg. (2) Hold and carefully lower the MLI fully. Then carefully lift the MLI until you feel the magnets engage. (3) Read the units mark nearest to the bottom skin of the wing and write down the number. (4) Retract the MLI and use a screwdriver to turn it through 90 deg to lock it. (5) Do this procedure for each applicable MLI. NOTE : You will only use one MLI reading from each applicable tank. ____ (6) Calculation Procedure (a) Read and write down the aircraft attitude (grid-square letter and grid-square number shown on the attitude monitor). (b) Use the table for the applicable aircraft attitude (grid-square letter and grid-square number) and the applicable MLI to find the volume of fuel in each tank.
EFF : ALL 12-11-28 R SROS
Page A398 Jan 01/07
(c) For an inner tank, there can be additional fuel in the collector-cells. Use the graph to find the additional fuel quantity in one inner tank. (Ref. Fig. 312/TASK 12-11-28-991-007) NOTE : The fuel quantity in the collector cell will decrease with ____ time. Use the applicable curve for the time since the main fuel pumps were switched off. The data taken from this curve gives a more accurate fuel quantity. (d) Add together the value from each tank to find the total volume of fuel. (e) Multiply the total volume of fuel by the SG of the fuel. The result is the total weight of fuel. NOTE : The trim tank can also contain a fuel quantity of between ____ zero and 4800 kg (10582 lb). **ON A/C 251-252, 701-749, Post SB
28-3078 For A/C 251-252,701-749,
Subtask 12-11-28-869-054-C A. Procedure to Use the Magnetic Level Indicators CAUTION : DO NOT LET THE MLIs FALL FREELY. _______ THE MLIs ARE FRAGILE. CAUTION : RETRACT THE MLIs AS SOON AS POSSIBLE. YOU CAN EASILY CAUSE _______ DAMAGE TO AN EXTENDED MLI. NOTE : Start the procedure with each of the outboard MLIs in the Outer ____ and Inner Tank. If they give no indication move inboard to each subsequent MLI until the MLI gives an indication. At the first MLI that gives an indication, use that MLI for the procedure. (1) Use a screwdriver to push (in) the applicable MLI and turn it through 90 deg. (2) Hold and carefully lower the MLI fully. Then carefully lift the MLI until you feel the magnets engage. (3) Read the units mark nearest to the bottom skin of the wing and write down the number.
EFF : ALL 12-11-28 R SROS
Page A399 Jan 01/07
(4) Retract the MLI and use a screwdriver to turn it through 90 deg to lock it. (5) Do this procedure for each applicable MLI. NOTE : You will only use one MLI reading from each applicable tank. ____ (6) Calculation Procedure (a) Use the table for the applicable ADIRS aircraft attitude data (Ref. TASK 12-11-28-860-801) and MLI to calculate the volume of fuel in each tank. (b) As an option you can use the applicable page of the FCMS Input Parameters to find the aircraft attitude (Ref. TASK 28-51-00-740803). (c) For an inner tank, there can be additional fuel in the collector-cells. Use the graph to find the additional fuel quantity in one inner tank. (Ref. Fig. 312/TASK 12-11-28-991-007) NOTE : The fuel quantity in the collector cell will decrease with ____ time. Use the applicable curve for the time since the main fuel pumps were switched off. The data taken from this curve gives a more accurate fuel quantity. (d) Add together the value from each tank to find the total volume of fuel. (e) Multiply the total volume of fuel by the SG of the fuel. The result is the total weight of fuel. NOTE : The trim tank can also contain a fuel quantity of between ____ zero and 4800 kg (10582 lb). **ON A/C ALL 5. Close-up ________ Subtask 12-11-28-410-056 A. Close Access (1) Close the access panel 198DB.
EFF : ALL 12-11-28 R SROS
Page B300 Jan 01/07
Subtask 12-11-28-942-056 B. Removal of Equipment (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 12-11-28 R SROS
Page B301 Jan 01/07
TASK 12-11-28-860-801 Procedure To Use The ADIRU to Find the Pitch and Roll Data 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
12-11-28-650-806 24-41-00-861-801 24-41-00-862-801 12-11-28-991-027
Procedure To Use The Fuel Magnetic Level Indicators Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Fig. 324
3. __________ Job Set-up Subtask 12-11-28-861-053 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). 4. Procedure _________ Subtask 12-11-28-860-060 A. Procedure (Ref. Fig. 324/TASK 12-11-28-991-027) (1) On the panel 221VU set the 3 ADIRS switches to the NAV position. (2) Do this procedure NOTE : The procedure that follows is only applicable to the MCDU 2 ____ and the MCDU 3. You cannot do this procedure with the MCDU 1. The actions and the results of this procedure occur on the MCDU used.
EFF : ALL 12-11-28 SROS
Page B302 Jan 01/07
INTENTIONALLY BLANK
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Page B303 Jan 01/07
Pitch and Roll Data Access from the ADIRUs Figure 324/TASK 12-11-28-991-027- 12 (SHEET 1) EFF : ALL 12-11-28 R SROS
Page B304 Jan 01/07
Pitch and Roll Data Access from the ADIRUs Figure 324/TASK 12-11-28-991-027- 22 (SHEET 2) EFF : ALL 12-11-28 SROS
Page B305 Jan 01/07
------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------1. On the MCDU turn the BRT knob
- the MCDU is on.
2. Push the MCDU MENU mode key
- the MCDU MENU page shows.
3. Push the line key adjacent to the ACMS indication
- the ACMS PARAMETER CALL-UP page shows.
4. Push the line key adjacent to the ALPHA indication
- the ALPHA CALL-UP CTRL page shows.
5. Push the line key adjacent to the LIST indication
- the ALPHA LIST page shows.
6. Use the ALPHA LIST that follows to find the ALPHA CODE for the ROLL and PITCH data. 7. Push the line key adjacent to the RETURN indication
- the ALPHA CALL-UP CTRL page shows.
8. Push the line key adjacent to the ALPHA MENU DISPLAY indication
- the ALPHA CALL-UP page shows.
9. On the MCDU scratchpad enter the alpha code for ROLL, and push the line key adjacent to the first line
- the ALPHA CALL-UP page shows the ROLL data.
10. On the MCDU scratchpad enter the alpha code for PITCH, and push the line key adjacent to the second line
- the ALPHA CALL-UP page shows the PITCH data.
11. If you need to copy the data, push the line key next to the PRINT indication
- after approximately 20 seconds, the screen data is printed.
12. Push the line key next to the RETURN indication
- the ALPHA CALL-UP CTRL page shows.
13. Push the line key adjacent to the CLEAR indication
- the ALPHA CALL-UP CTRL page shows the message ALL ENTRIES CLEARED.
EFF : ALL 12-11-28 SROS
Page B306 Jan 01/07
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Subtask 12-11-28-860-064 B. Procedure to Convert Data to Equivalent Attitude Monitor Value
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(1) Use the table below to find the equivalent attitude monitor value:
R
(a) Use the Pitch data to find the equivalent number.
R
(b) Use the Roll data to find the equivalent letter.
R R R R R R R R R R R
(2) Put together the number and the letter to identify the square to use in the MLI procedure.(Ref. TASK 12-11-28-650-806) Pitch 2.5 2.0 1.5 1.0 0.5 0.0 plus 0.5 minus minus minus minus minus
R
**ON A/C 251-252, 701-749,
R
Post SB
R
Subtask 12-11-28-860-064-A
R R
Roll minus 1.5 minus 1.0 minus 0.5 0.0 plus 0.5 plus 1.0 plus 1.5
Ref A B C D E F G
28-3078 For A/C 251-252,701-749,
B. Procedure to Use Pitch and Roll Data When Attitude Monitor is Not Installed
R R R
Ref 1 2 3 4 5 6 7
(1) Use the pitch and roll data to find the fuel quantity given in the tables of the MLI procedure.(Ref. TASK 12-11-28-650-806) **ON A/C ALL 5. Close-up ________ Subtask 12-11-28-860-061 A. On the panel 221VU set the 3 switching selectors of the ADIRS to the OFF position. (1) On the MCDU push the RETURN key until the PARAMETER CALL-UP PAGE shows.
EFF : ALL 12-11-28 SROS
Page B307 Jan 01/07
(2) On the MCDU control panel, push the K key. (3) Set the BRT knob to the OFF position. Subtask 12-11-28-862-053 B. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
EFF : ALL 12-11-28 SROS
Page B308 Jan 01/07
HYDRAULIC FLUIDS - DESCRIPTION AND OPERATION ____________________________________________ 1. _______ General The hydraulic fluid instructions give specification and special instructions. A. Specification of Phosphate Ester-Base Fluids (1) The aircraft hydraulic systems are filled with one of these hydraulic fluids (Type IV). The Material Numbers (Mat No.) are as follows: - 02-003, - 02-003A, - 02-003B, - 02-003C, - 02-003D, - 02-003E.
R R R
(2) All the fluids are to NSA 307110 specification and can be mixed. (3) Fluid characteristics (Ref. Fig. 001) B. Fluid Monitoring (1) Hydraulic fluid with a high degree of cleanliness is required for the correct operation of the hydraulic systems and equipment. (2) Frequent sampling, particle count (physical contamination) and check of filter clogging indicators permit to monitor the hydraulic fluid. (3) If a filter clogging indicator is out, you must: - depressurize the related hydraulic system, - replace the clogged filter, - take a sample of the system hydraulic fluid and send it for analysis. (4) On results of the analysis record (see contamination analysis by particle count of sampling procedure), clean the hydraulic fluid. NOTE : The number of particles contained in 100 cm3 (6.10 in.3) of ____ hydraulic fluid must not be more than the class 9 requirements of the NAS specification 1638 (final or rejection state). NOTE : The degree of cleanliness of the hydraulic fluid used to fill ____ the hydraulic systems and hydraulic cart reservoirs must agree with the Class 7 of the NAS specification 1638 (initial state).
EFF : ALL 12-12-00 SROS
Page 1 Jan 01/05
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Characteristics of Phosphate Ester-Base Hydraulic Fluids Figure 001
EFF : ALL 12-12-00 SROS
Page 2 Jan 01/05
C. Hydraulic Ground Power Cart Only use a hydraulic ground power cart with a hydraulic reservoir. Do a fluid sampling for contamination of the hydraulic fluid and keep the sample analysis record. D. Hydraulic Fluid Property In-Service Limits The hydraulic fluid property in-service limits are: - the physical properties, - the chemical properties. (Ref. Fig. 002) R R
NOTE : The maximum water contents is 0.8 %. We recommend to decrease the ____ limit to 0.5 % which will increase the life of the hydraulic fluid. (1) The quality of the hydraulic fluid must be in the limits given in Fig. 002. If the sample analysis shows that the properties of the hydraulic fluid are out of the in-service limits, you must replace the hydraulic fluid. E. Specification of Mineral-Base Fluids (1) Each aircraft landing-gear shock-absorber is supplied filled with a hydraulic fluid (Mat. No. 02-001) to the MIL-H-5606 specification. (2) Fluid characteristics (Ref. Fig. 003) F. Safety Precautions When you work on the hydraulic systems obey the safety procedures.
EFF : ALL 12-12-00 SROS
Page 3 Jan 01/04
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Hydraulic Fluid Property In-Service Limits Figure 002
EFF : ALL 12-12-00 SROS
Page 4 Jul 01/03
Characteristics of Mineral Fluids Figure 003 EFF : ALL 12-12-00 SROS
Page 5 Apr 01/98
HYDRAULIC POWER - SERVICING ___________________________ TASK 12-12-29-611-801 Fill the Green Hydraulic Reservoir with a Hydraulic Service Cart WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE _______ CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM. MOVEMENT OF THE FLIGHT CONTROL SURFACES CAN BE DANGEROUS AND/OR CAUSE DAMAGE. R R R
WARNING : DO NOT GET THE FLUID ON YOUR SKIN OR IN YOUR EYES. IF YOU DO: _______ - FLUSH IT AWAY WITH CLEAN WATER - GET MEDICAL AID. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
circuit breaker(s) safety clip(s) Fill Unit-Hyd Fluid access platform 2.5 m (8 ft. 2 in.)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 02-003
R
Material No. 02-003A
R
Material No. 02-003B
F NSA 307110 TYPE 4 HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00) F NSA 307110 TYPE 4 HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00) F NSA 307-110 TYPE 4 HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00)
EFF : ALL 12-12-29 SROS
Page 301 Jan 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 02-003C Material No. 02-003D Material No. 02-003E
F NSA 307-110 TYPE IV HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00) F NSA 307-110 TYPE IV HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 24-41-00-862-801 R R
29-00-00-210-801 29-00-00-864-801
Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Check for Air in the Green/Blue/Yellow Hydraulic System Depressurize the Green Hydraulic System (Pressurized with the Hydraulic Ground Supply)
R 29-10-00-200-802 29-14-00-614-804 29-14-00-614-804 31-60-00-860-801 12-12-29-991-001
Check of the Nitrogen Charging Pressure on Hydraulic Power Accumulator (5151JM1,5151JM2,5151JM3) Pressurization of the Hydraulic Reservoirs with external bench Pressurization of the Hydraulic Reservoirs with the APU EIS Start Procedure Fig. 301
3. __________ Job Set-up Subtask 12-12-29-861-050 A. Energize the aircraft electrical circuits circuits (Ref. TASK 24-41-00-861-801).
EFF : ALL 12-12-29 SROS
Page 302 Jan 01/07
Subtask 12-12-29-010-050 B. Get Access (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Put the access platform in position at the access door 197CB. (4) Open the Green ground service panel 197CB. Subtask 12-12-29-865-050 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU HYD PUMP G CTL 9JV U09 Subtask 12-12-29-865-051 D. Make sure that this(these) circuit breaker(s) is(are) closed: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU HSMU B + PART G 6JG U10 722VU HSMU Y + PART G 7JG X46 742VU HYD RAT EXT SOL 2 5JR D76 Subtask 12-12-29-860-050 E. Aircraft Maintenance Configuration (1) Make sure that the aircraft is in this configuration: - the speed brakes and the spoilers are retracted, - the thrust reversers are stowed, - the landing gear is extended and the landing gear doors are closed, - all the other hydraulic services are in the normal position.
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(2) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (3) Make sure that the Green hydraulic system accumulator is pressurized (Ref. TASK 29-10-00-200-802).
EFF : ALL 12-12-29 SROS
Page 303 Jan 01/07
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(4) Make sure that the reservoir of the Green hydraulic system is pressurized (Ref. TASK 29-14-00-614-804) or (Ref. TASK 29-14-00-614804). 4. Procedure _________ (Ref. Fig. 301/TASK 12-12-29-991-001) Subtask 12-12-29-611-050 A. Fill the hydraulic reservoir
R R R R R R R R R R R R
(1) If you replace one or more components on the high pressure and/or low pressure side or - if there is a hydraulic-fluid low level which causes loss of the system or - if there is a loss of hydraulic fluid equal to or more than 5 liters - make sure that there is no air in the Green hydraulic system (Ref. TASK 29-00-00-210-801). Use Hydraulic fluid HYDRAULIC FLUIDS (Material No. 02-003), or HYDRAULIC FLUIDS (Material No. 02-003A), or HYDRAULIC FLUIDS (Material No. 02-003B), or HYDRAULIC FLUIDS (Material No. 02-003C), or HYDRAULIC FLUIDS (Material No. 02-003D), or HYDRAULIC FLUIDS (Material No. 02-003E).
R
(2) Remove the blanking cap from the reservoir filling self-sealing ground connector 5203JM.
R
(3) Connect a Fill Unit-Hyd Fluid capable of max pressure 20 bar (290 psi) and flow rate 12l/mn to the self-sealing ground connector 5203JM.
R
(4) On the reservoir-filling manual selector-valve 4JS, select the GREEN position.
R
(5) Operate the hydraulic service cart. CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE ON THE GROUND HYDRAULIC _______ CART IS SET TO A MINIMUM OF 7 BARS (101.53 PSI). Operate the hydraulic service cart and monitor the increase of the fluid level on the reservoir hydraulic quantity indicator 5JS.
EFF : ALL 12-12-29 SROS
Page 304 Jan 01/07
Green Ground Service Panel Figure 301/TASK 12-12-29-991-001 EFF : ALL 12-12-29 SROS
Page 305 Apr 01/98
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(6) Stop the flow when the pointer is in the center position on the reservoir hydraulic quantity indicator 5JS.
R
(7) Turn the reservoir filling manual selector-valve 4JS to the NEUTRAL position (on the reservoir hydraulic quantity indicator 5JS, the pointer is in the INOP position).
R
(8) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00-860-801).
R
(9) On the ECAM control panel on the center pedestal, press the HYD pushbutton. Make sure that the HYD page is shown on the SD.
R
(10) On the SD: - check that the low indication is not in view for the Green hydraulic system - check that the fluid level index is green.
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(11) Disconnect the ground hydraulic service cart from the reservoir filling self-sealing ground connector 5203JM and install the blanking cap. 5. Close-up ________ Subtask 12-12-29-865-052 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 9JV. Subtask 12-12-29-862-050 B. Put the Aircraft back to its Initial Configuration (1) On the ECAM control panel, set the UPPER DISPLAY and LOWER DISPLAY potentiometers to OFF. (2) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). Subtask 12-12-29-410-050 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access doors 811.
EFF : ALL 12-12-29 SROS
Page 306 Jan 01/07
(3) Close the Green ground service panel 197CB. (4) Remove the access platform(s).
EFF : ALL 12-12-29 SROS
Page 307 Apr 01/98
TASK 12-12-29-611-802 Fill the Green Hydraulic Reservoir with a Hand Pump WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE _______ CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM. MOVEMENT OF THE FLIGHT CONTROL SURFACES CAN BE DANGEROUS AND/OR CAUSE DAMAGE. R R R
WARNING : DO NOT GET THE FLUID ON YOUR SKIN OR IN YOUR EYES. IF YOU DO: _______ - FLUSH IT AWAY WITH CLEAN WATER - GET MEDICAL AID. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
circuit breaker(s) safety clip(s) hydraulic fluid container access platform 2.5 m (8 ft. 2 in.)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 02-003
R
Material No. 02-003A
R
Material No. 02-003B Material No. 02-003C
F NSA 307110 HYDRAULIC FLUID (Ref. 20-31-00) F NSA 307110 HYDRAULIC FLUID (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00)
TYPE 4 (PHOSPHATE ESTER BASE) TYPE 4 (PHOSPHATE ESTER BASE) TYPE 4 (PHOSPHATE ESTER BASE) TYPE IV (PHOSPHATE ESTER BASE)
EFF : ALL 12-12-29 SROS
Page 308 Jan 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 02-003D Material No. 02-003E
F NSA 307-110 TYPE IV HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 24-41-00-862-801 R R
29-00-00-210-801 29-00-00-864-801
Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Check for Air in the Green/Blue/Yellow Hydraulic System Depressurize the Green Hydraulic System (Pressurized with the Hydraulic Ground Supply)
R 29-10-00-200-802 29-14-00-614-804 29-14-00-614-804 31-60-00-860-801 12-12-29-991-001
Check of the Nitrogen Charging Pressure on Hydraulic Power Accumulator (5151JM1,5151JM2,5151JM3) Pressurization of the Hydraulic Reservoirs with external bench Pressurization of the Hydraulic Reservoirs with the APU EIS Start Procedure Fig. 301
3. __________ Job Set-up Subtask 12-12-29-861-051 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801).
EFF : ALL 12-12-29 SROS
Page 309 Jan 01/07
Subtask 12-12-29-010-051 B. Get Access (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Put the access platform in position at the access door 197CB. (4) Open the Green ground service panel 197CB. Subtask 12-12-29-865-053 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU HYD PUMP G CTL 9JV U09 Subtask 12-12-29-865-054 D. Make sure that this(these) circuit breaker(s) is(are) closed: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU HSMU B + PART G 6JG U10 722VU HSMU Y + PART G 7JG X46 742VU HYD RAT EXT SOL 2 5JR D76 Subtask 12-12-29-860-051 E. Aircraft Maintenance Configuration R R R R
(1) Make sure that the aircraft is in this configuration: - the speed brakes and the spoilers are retracted, - the thrust reversers are stowed, - the landing gear is extended and the landing gear doors are closed, - all the other hydraulic services are in the normal position.
R
(2) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (3) Make sure that the Green hydraulic system accumulator is pressurized (Ref. TASK 29-10-00-200-802).
EFF : ALL 12-12-29 SROS
Page 310 Jan 01/07
(4) Make sure that the reservoir of the Green hydraulic system is pressurized (Ref. TASK 29-14-00-614-804) or (Ref. TASK 29-14-00-614804).
R
4. Procedure _________ (Ref. Fig. 301/TASK 12-12-29-991-001) CAUTION : MAKE SURE THAT YOU OPERATE THE HAND PUMP SLOWLY AND SMOOTHLY. THE _______ HANDLE MUST NOT HIT THE STOPS WITH TOO MUCH FORCE. IF YOU DO NOT OBEY THESE PRECAUTIONS, DAMAGE CAN OCCUR TO THE HAND PUMP AND TO THE SERVICING LINE ON THE OTHER SIDE OF THE SERVICING PANEL. Subtask 12-12-29-611-051 A. Fill the Green hydraulic reservoir R R R R R R R R R R R
(1) If you replace one or more components on the high pressure and/or low pressure side or - if there is a hydraulic-fluid low level which causes loss of the system or - if there is a loss of hydraulic fluid equal to or more than 5 liters - make sure that there is no air in the Green hydraulic system (Ref. TASK 29-00-00-210-801).
R
(2) Remove the hand pump lever 5205JM.
R
(3) Connect the hand pump lever 5205JM to the shaft of the reservoir filling hand pump 5204JM.
R
(4) Remove the reservoir filling hose 5213JM.
R
(5) Remove the blanking cap and connect the filling hose 5213JM to the filling valve 5211JM.
R
(6) Put the other end of the filling hose in the hydraulic fluid container filled with HYDRAULIC FLUIDS (Material No. 02-003), or HYDRAULIC FLUIDS (Material No. 02-003A), or HYDRAULIC FLUIDS (Material No. 02-003B), or HYDRAULIC FLUIDS (Material No. 02-003C), or HYDRAULIC FLUIDS (Material No. 02-003D). HYDRAULIC FLUIDS (Material No. 02-003E)
R
(7) On the reservoir-filling manual selector-valve 4JS, select the GREEN position.
R
(8) Operate the hand pump lever and monitor the increase of the fluid level on the reservoir hydraulic quantity indicator 5JS.
EFF : ALL 12-12-29 SROS
Page 311 Jan 01/07
R
(9) Stop the flow when the pointer is in the center position on the reservoir hydraulic quantity indicator 5JS.
R
(10) Turn the reservoir-filling manual selector-valve 4JS to the NEUTRAL position. (On the reservoir hydraulic quantity indicator 5JS, the pointer is in the INOP position).
R
(11) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00-860-801).
R
(12) On the ECAM control panel on the center pedestal, press the HYD pushbutton. Make sure that the HYD page is shown on SD.
R
(13) On the SD: - check that the low indication is not in view for the Green hydraulic system - check that the fluid level index is green.
R
(14) Remove the filling hose 5213JM and install the blanking cap on the hand pump.
R
(15) Put the filling hose back in position on its mounting.
R
(16) Remove the hand pump lever 5205JM from the hand pump 5204JM and put it in position on the Green ground service panel. 5. Close-up ________ Subtask 12-12-29-865-055 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 9JV. Subtask 12-12-29-862-051 B. Put the Aircraft back to its Initial Configuration (1) On the ECAM control panel, set the UPPER DISPLAY and LOWER DISPLAY potentiometers to OFF. (2) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
EFF : ALL 12-12-29 SROS
Page 312 Jan 01/07
Subtask 12-12-29-410-051 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access doors 811. (3) Close the Green ground service panel 197CB. (4) Remove the access platform(s).
EFF : ALL 12-12-29 SROS
Page 313 Apr 01/98
TASK 12-12-29-611-803 Fill the Blue Hydraulic Reservoir with a Hydraulic Service Cart WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE _______ CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM. MOVEMENT OF THE FLIGHT CONTROL SURFACES CAN BE DANGEROUS AND/OR CAUSE DAMAGE. R R R
WARNING : DO NOT GET THE FLUID ON YOUR SKIN OR IN YOUR EYES. IF YOU DO: _______ - FLUSH IT AWAY WITH CLEAN WATER - GET MEDICAL AID. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No
specific specific specific specific
circuit breaker(s) safety clip(s) Fill Unit-Hyd Fluid access platform 1.8 m (5 ft. 11 in.) access platform 2.5 m (8 ft. 2 in.)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 02-003
R
Material No. 02-003A
R
Material No. 02-003B Material No. 02-003C
F NSA 307110 HYDRAULIC FLUID (Ref. 20-31-00) F NSA 307110 HYDRAULIC FLUID (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00)
TYPE 4 (PHOSPHATE ESTER BASE) TYPE 4 (PHOSPHATE ESTER BASE) TYPE 4 (PHOSPHATE ESTER BASE) TYPE IV (PHOSPHATE ESTER BASE)
EFF : ALL 12-12-29 SROS
Page 314 Jan 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 02-003D
R R
Material No. 02-003E
F NSA 307-110 TYPE IV HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 24-41-00-862-801 29-00-00-863-802 29-00-00-870-805 29-14-00-614-804 29-14-00-614-804 31-60-00-860-801 12-12-29-991-001
Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Pressurize the Blue Hydraulic System with the Electric Pump Bleeding of the Blue Hydraulic System Pressurization of the Hydraulic Reservoirs with external bench Pressurization of the Hydraulic Reservoirs with the APU EIS Start Procedure Fig. 301
3. __________ Job Set-up Subtask 12-12-29-861-052 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). Subtask 12-12-29-010-052 B. Get Access (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Put the access platform in position at the access door 197CB.
EFF : ALL 12-12-29 SROS
Page 315 Jan 01/05
(4) Open the Green ground service panel 197CB. (5) Put the access platform in position at the access door 195BB. (6) Open the Blue ground service panel 195BB. Subtask 12-12-29-865-057 C. Make sure that this(these) circuit breaker(s) is(are) closed: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU HSMU B + PART G 6JG U10 721VU HYD PUMP B CTL 9JC X12 722VU HSMU Y + PART G 7JG X46 Subtask 12-12-29-860-052 D. Aircraft Maintenance Configuration (1) Make sure that the aircraft is in this configuration: - the speed brakes and the spoilers are retracted - the thrust reversers are stowed - the landing gear is extended and the landing gear doors are closed - all the other hydraulic services are in the normal position.
R
(2) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00-860-801). (3) On the ECAM control panel on the center pedestal, press the HYD pushbutton. Make sure that the HYD page is shown on SD. On the SD: Make sure that the Blue hydraulic reservoir do not give LO AIR PRESS indication.
R R R
(4) If necessary, pressurize the Blue hydraulic reservoir (Ref. TASK 2914-00-614-804) or (Ref. TASK 29-14-00-614-804). (5) On the Blue ground service panel, make sure that the pressure of the accumulators are correct according the marking on the ground service panel: - On the pressure gage (5152JS) of the Blue power accumulator. - On the pressure gage (5426GG and 5427GG) of the Blue brake accumulators.
R R
EFF : ALL 12-12-29 SROS
Page 316 Jul 01/06
(6) On the panel 117VU, set the PARK BRAKE selector switch (3GZ) on the ON position (7) Fill the brake accumulator. R R R
NOTE : The nominal fill level of the Blue hydraulic reservoir is ____ obtained with the brake accumulators filled with fluid at 3000 psi (206.8427 bar) (the brake accumulator capacity is approximately 6 liters). (8) On the overhead panel 245VU, push the HYD/BLUE/ELEC pushbutton switch: - the ON legend of this pushbutton switch comes on - the electrical pump of the Blue hydraulic system starts. - the Blue hydraulic system accumulator is filled. (9) On the center instrument panel 312VU: Make sure that the Blue brake-pressure indicator (2GK) show the ACCU PRESS at 3000 psi (206.8427 bar). If necessary pressurize the brake accumulator with Blue pump (Ref. TASK 29-00-00-863-802). (10) On the overhead panel 245VU, release the HYD/BLUE/ELEC pushbutton switch: - the ON legend of this pushbutton switch goes off - the electrical pump of the Blue hydraulic system stop. (11) Pressurize the Hydraulic reservoir during 1 minute to make sure that the nominal pressure is reached (Ref. TASK 29-14-00-614-804). Subtask 12-12-29-865-056 E. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU HYD PUMP B CTL 9JC X12
EFF : ALL 12-12-29 SROS
Page 317 Jan 01/07
4. Procedure _________ (Ref. Fig. 301/TASK 12-12-29-991-001) Subtask 12-12-29-611-052 A. Fill the hydraulic reservoir. NOTE : If you replace one or more components on the high pressure and/or ____ low pressure side, - If there is a hydraulic-fluid low level which causes loss of the system - If there is a large loss of hydraulic fluid - Do the related bleed procedure to make sure that the quantity of fluid in the system is correct:(Ref. TASK 29-00-00-870-805) Use Hydraulic fluid HYDRAULIC FLUIDS (Material No. 02-003), or HYDRAULIC FLUIDS (Material No. 02-003A), or HYDRAULIC FLUIDS (Material No. 02-003B), or HYDRAULIC FLUIDS (Material No. 02003C), or HYDRAULIC FLUIDS (Material No. 02-003D). HYDRAULIC FLUIDS (Material No. 02-003E)
R R R R R
(1) Remove the blanking cap from the reservoir filling self-sealing ground connector 5203JM. (2) Connect a Fill Unit-Hyd Fluid capable of max pressure 20 bar (290psi) and flow rate 12l/mn to the self-sealing ground connector 5203JM. (3) On the reservoir-filling manual selector-valve 4JS, select the BLUE position. (4) Operate the hydraulic service cart. CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE ON THE GROUND HYDRAULIC _______ CART IS SET TO A MINIMUM OF 7 BARS (101.53 PSI). Operate the hydraulic service cart and monitor the increase of the fluid level on the reservoir hydraulic quantity indicator 5JS. (5) Stop the flow when the pointer is in the center position on the reservoir hydraulic quantity indicator 5JS. (6) Turn the reservoir filling manual selector-valve 4JS to the NEUTRAL position (on the reservoir hydraulic quantity indicator 5JS, the pointer is in the INOP position).
EFF : ALL 12-12-29 SROS
Page 318 Jan 01/05
(7) On the ECAM control panel on the center pedestal, make sure that the HYD page is shown On the SD: - check that the low indication is not in view for the Blue hydraulic system - check that the fluid level index is green. (8) Disconnect the ground hydraulic service cart from the reservoir filling self-sealing ground connector 5203JM and install the blanking cap. 5. Close-up ________ Subtask 12-12-29-865-058 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 9JC. Subtask 12-12-29-862-052 B. Put the Aircraft back to its Initial Configuration (1) Get Access (2) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). (3) On the panel 117VU set the Park Brake selector switch (3GZ) on the OFF position. Subtask 12-12-29-410-052 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access doors 811. (3) Close the Green ground service panel 197CB. (4) Close the Blue ground service panel 195BB. (5) Remove the access platform(s).
EFF : ALL 12-12-29 R SROS
Page 319 Jan 01/05
TASK 12-12-29-611-804 Fill the Blue Hydraulic Reservoir with a Hand Pump WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE _______ CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM. MOVEMENT OF THE FLIGHT CONTROL SURFACES CAN BE DANGEROUS AND/OR CAUSE DAMAGE. R R R
WARNING : DO NOT GET THE FLUID ON YOUR SKIN OR IN YOUR EYES. IF YOU DO: _______ - FLUSH IT AWAY WITH CLEAN WATER - GET MEDICAL AID. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No
specific specific specific specific
circuit breaker(s) safety clip(s) hydraulic fluid container access platform 1.8 m (5 ft. 11 in.) access platform 2.5 m (8 ft. 2 in.)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 02-003
R
Material No. 02-003A
R
Material No. 02-003B Material No. 02-003C
F NSA 307110 HYDRAULIC FLUID (Ref. 20-31-00) F NSA 307110 HYDRAULIC FLUID (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00)
TYPE 4 (PHOSPHATE ESTER BASE) TYPE 4 (PHOSPHATE ESTER BASE) TYPE 4 (PHOSPHATE ESTER BASE) TYPE IV (PHOSPHATE ESTER BASE)
EFF : ALL 12-12-29 SROS
Page 320 Jan 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 02-003D
R R
Material No. 02-003E
F NSA 307-110 TYPE IV HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 24-41-00-862-801 29-00-00-863-802 29-00-00-870-805 29-14-00-614-804 29-14-00-614-804 31-60-00-860-801 12-12-29-991-001
Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Pressurize the Blue Hydraulic System with the Electric Pump Bleeding of the Blue Hydraulic System Pressurization of the Hydraulic Reservoirs with external bench Pressurization of the Hydraulic Reservoirs with the APU EIS Start Procedure Fig. 301
3. __________ Job Set-up Subtask 12-12-29-861-053 A. Energize the aircraft electrical circuits circuits (Ref. TASK 24-41-00-861-801). Subtask 12-12-29-010-053 B. Get Access (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Put the access platform in position at the access door 197CB.
EFF : ALL 12-12-29 SROS
Page 321 Jan 01/05
(4) Open the Green ground service panel 197CB. (5) Put the access platform in position at the access door 195BB. (6) Open the Blue ground service panel 195BB. Subtask 12-12-29-865-060 C. Make sure that this(these) circuit breaker(s) is(are) closed: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU HSMU B + PART G 6JG U10 721VU HYD PUMP B CTL 9JC X12 722VU HSMU Y + PART G 7JG X46 Subtask 12-12-29-860-053 D. Aircraft Maintenance Configuration (1) Make sure that the aircraft is in this configuration: - the speed brakes and the spoilers are retracted - the thrust reversers are stowed - the landing gear is extended and the landing gear doors are closed - all the other hydraulic services are in the normal position (2) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00-860-801). (3) On the ECAM control panel on the center pedestal, press the HYD pushbutton. make sure that the HYD page is shown on SD. On the SD: Make sure that the Blue hydraulic reservoir do not give LO AIR PRESS indication. (4) If necessary, pressurize the Blue hydraulic reservoir. (Ref. TASK 2914-00-614-804) or (Ref. TASK 29-14-00-614-804) (5) On the Blue ground service panel, make accumulators are correct according the panel : - On the pressure gage (5152JS) of the - On the two pressure gage (5426GG and accumulators
sure that the pressure of the marking on the ground service Blue power accumulator 5427GG) of the Blue brake
EFF : ALL 12-12-29 R SROS
Page 322 Jan 01/05
(6) On the panel 117VU, set the PARK BRAKE selector switch (3GZ) on the ON position. (7) Fill the brake accumulators 5426GG and 5427GG with the electrical pump of the Blue hydraulic system : NOTE : The capacity of each brake accumulator is approximately 6 ____ liters filled with hydraulic fluid at 3000 psi (206.8427 bar). (a) On the overhead panel 245VU, push the HYD/BLUE/ELEC pushbutton switch: - The ON legend of this pushbutton switch comes on, - The electrical pump of the Blue hydraulic system starts, (b) On the center instrument panel 312VU, make sure that the Blue brake -pressure indicator (2GK) show the ACCU PRESS at 3000 psi (206.8427 bar). If necessary pressurize the brake accumulator with Blue pump.(Ref. TASK 29-00-00-863-802) (c) On the overhead panel 245VU, release the HYD/BLUE/ELEC pushbutton switch: - The ON legend of this pushbutton switch goes off, - The electrical pump of the Blue hydraulic system stop. (8) Pressurize the Blue hydraulic reservoir during 1 minute to make sure that the nominal pressure is reached (Ref. TASK 29-14-00-614-804) NOTE : The nominal fill level of the Blue hydraulic reservoir is ____ obtain with the brake accumulators filled with fluid at 3000 psi (206.8427 bar). Subtask 12-12-29-865-059 E. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU HYD PUMP B CTL 9JC X12
EFF : ALL 12-12-29 R SROS
Page 323 Jan 01/05
4. Procedure _________ (Ref. Fig. 301/TASK 12-12-29-991-001) CAUTION : MAKE SURE THAT YOU OPERATE THE HAND PUMP SLOWLY AND SMOOTHLY. THE _______ HANDLE MUST NOT HIT THE STOPS WITH TOO MUCH FORCE. IF YOU DO NOT OBEY THESE PRECAUTIONS, DAMAGE CAN OCCUR TO THE HAND PUMP AND TO THE SERVICING LINE ON THE OTHER SIDE OF THE SERVICING PANEL. Subtask 12-12-29-611-053 A. Fill the Blue hydraulic reservoir NOTE : If you replace one or more components on the high pressure and/or ____ low pressure side, - If there is a hydraulic-fluid low level which causes loss of the system, - If there is a large loss of hydraulic fluid - Do the related bleed procedure to make sure that the quantity of fluid in the system is correct:(Ref. TASK 29-00-00-870-805) (1) Remove the hand pump lever 5205JM. (2) Connect the hand pump lever 5205JM to the shaft of the reservoir filling hand pump 5204JM. (3) Remove the reservoir filling hose 5213JM. (4) Remove the blanking cap and connect the filling hose 5213JM to the filling valve 5211JM. (5) Put the other end of the filling hose in the hydraulic fluid container filled with HYDRAULIC FLUIDS (Material No. 02-003), or HYDRAULIC FLUIDS (Material No. 02-003A), or HYDRAULIC FLUIDS (Material No. 02-003B), or HYDRAULIC FLUIDS (Material No. 02-003C), or HYDRAULIC FLUIDS (Material No. 02-003D) HYDRAULIC FLUIDS (Material No. 02-003E)
R R R R
(6) On the reservoir-filling manual selector-valve 4JS, select the BLUE position. (7) Operate the hand pump lever and monitor the increase of the fluid level on the reservoir hydraulic quantity indicator 5JS. (8) Stop the flow when the pointer is in the center position on the reservoir hydraulic quantity indicator 5JS.
EFF : ALL 12-12-29 SROS
Page 324 Jan 01/05
(9) Turn the reservoir-filling manual selector-valve 4JS to the NEUTRAL position. (On the reservoir hydraulic quantity indicator 5JS, the pointer is in the INOP position). (10) On the ECAM control panel on the center pedestal, make sure that the HYD page is shown on SD. (11) On the SD: - check that the low indication is not in view for the Blue hydraulic system - check that the fluid level index is green. (12) Remove the filling hose 5213JM and install the blanking cap on the hand pump. (13) Put the filling hose back in position on its mounting. (14) Remove the hand pump lever 5205JM from the hand pump 5204JM and put it in position on the Green ground service panel. 5. Close-up ________ Subtask 12-12-29-865-061 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 9JC. Subtask 12-12-29-862-053 B. Put the Aircraft back to its Initial Configuration (1) On the ECAM control panel, set the UPPER DISPLAY and LOWER DISPLAY potentiometers to OFF. (2) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). Subtask 12-12-29-410-053 C. Close Access ON the panel 117VU, set the PARK BRAKE selector switch (3GZ) on the OFF position. (1) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 12-12-29 R SROS
Page 325 Jan 01/05
(2) Close the access doors 811. (3) Close the Green ground service panel 197CB. (4) Close the Blue ground service panel 195BB. (5) Remove the access platform(s).
EFF : ALL 12-12-29 R SROS
Page 326 Jan 01/05
TASK 12-12-29-611-805 Fill the Yellow Hydraulic Reservoir with a Hydraulic Service Cart WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE _______ CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM. MOVEMENT OF THE FLIGHT CONTROL SURFACES CAN BE DANGEROUS AND/OR CAUSE DAMAGE. R R R
WARNING : DO NOT GET THE FLUID ON YOUR SKIN OR IN YOUR EYES. IF YOU DO: _______ - FLUSH IT AWAY WITH CLEAN WATER - GET MEDICAL AID. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
circuit breaker(s) safety clip(s) Fill-Unit Hyd Fluid access platform 2.5 m (8 ft. 2 in.)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 02-003
R
Material No. 02-003A
R
Material No. 02-003B Material No. 02-003C
F NSA 307110 HYDRAULIC FLUID (Ref. 20-31-00) F NSA 307110 HYDRAULIC FLUID (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00)
TYPE 4 (PHOSPHATE ESTER BASE) TYPE 4 (PHOSPHATE ESTER BASE) TYPE 4 (PHOSPHATE ESTER BASE) TYPE IV (PHOSPHATE ESTER BASE)
EFF : ALL 12-12-29 SROS
Page 327 Jan 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 02-003D
R R
Material No. 02-003E
F NSA 307-110 TYPE IV HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 24-41-00-862-801 29-00-00-864-803 29-00-00-870-806 29-10-00-200-802 29-14-00-614-804 29-14-00-614-804 31-60-00-860-801 12-12-29-991-001
Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Depressurize the Yellow Hydraulic System (Pressurized with the Hydraulic Ground Supply) Bleeding of the Yellow Hydraulic System Check of the Nitrogen Charging Pressure on Hydraulic Power Accumulator (5151JM1,5151JM2,5151JM3) Pressurization of the Hydraulic Reservoirs with external bench Pressurization of the Hydraulic Reservoirs with the APU EIS Start Procedure Fig. 301
3. __________ Job Set-up Subtask 12-12-29-861-054 A. Energize the aircraft electrical circuits circuits (Ref. TASK 24-41-00-861-801). Subtask 12-12-29-010-054 B. Get Access (1) Put the access platform in position at the access door 811. (2) Open the access door 811.
EFF : ALL 12-12-29 SROS
Page 328 Jan 01/05
R
(3) Put the access platform in position at the access door 197CB. (4) Open the Green ground service panel 197CB. Subtask 12-12-29-865-062 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------722VU HYD PUMP Y SVCE 10JJ N46 722VU HYD PUMP Y CTL 9JJ R36 Subtask 12-12-29-865-063 D. Make sure that this(these) circuit breaker(s) is(are) closed: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------722VU HSMU Y + PART G 7JG X46 Subtask 12-12-29-860-054 E. Aircraft Maintenance Configuration (1) Make sure that the aircraft is in this configuration: - the speed brakes and the spoilers are retracted - the thrust reversers are stowed - the landing gear is extended and the landing gear doors are closed - all the other hydraulic services are in the normal position - the FWD and AFT cargo-compartment doors 821, 822 are closed. (2) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803). (3) Make sure that the Yellow hydraulic system accumulator is pressurized (Ref. TASK 29-10-00-200-802). (4) Make sure that the reservoir of the Yellow hydraulic system is pressurized (Ref. TASK 29-14-00-614-804) or (Ref. TASK 29-14-00-614804)
EFF : ALL 12-12-29 SROS
Page 329 Jul 01/06
4. Procedure _________ (Ref. Fig. 301/TASK 12-12-29-991-001) Subtask 12-12-29-611-054 A. Fill the hydraulic reservoir. NOTE : If you replace one or more components on the high pressure and/or ____ low pressure side, - If there is a hydraulic-fluid low level which causes loss of the system, - If there is a large loss of hydraulic fluid, - Do the related bleed procedure to make sure that the quantity of hydraulic fluid in the system is correct (Ref. TASK 29-00-00870-806): Use hydraulic fluid HYDRAULIC FLUIDS (Material No. 02-003), or HYDRAULIC FLUIDS (Material No. 02-003A), or HYDRAULIC FLUIDS (Material No. 02-003B), or HYDRAULIC FLUIDS (Material No. 02003C), or HYDRAULIC FLUIDS (Material No. 02-003D). HYDRAULIC FLUIDS (Material No. 02-003E)
R R R R R
(1) Remove the blanking cap from the reservoir filling self-sealing ground connector (5203JM). (2) Connect a Fill-Unit Hyd Fluid with a capacity of 20 bar (290 psi) maximum and flow rate 12 l/mn to the self-sealing ground connector (5203JM). (3) On the reservoir filling manual selector valve (4JS), select the YELLOW position. (4) Operate the hydraulic service cart. CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE ON THE GROUND HYDRAULIC _______ CART IS SET TO A MINIMUM OF 7 BARS (101.53 PSI). Operate the hydraulic service cart and monitor the increase of the fluid level on the reservoir hydraulic quantity indicator (5JS). (5) Stop the flow when the pointer is in the position 0 on the reservoir hydraulic quantity indicator (5JS). (6) Turn the reservoir filling manual selector valve (4JS) to the NEUTRAL position (on the reservoir hydraulic quantity indicator (5JS), the pointer is in the INOP position).
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(7) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00-860-801). (8) On the ECAM control panel on the center pedestal: - push the HYD pushbutton (on the SD, the HYD page comes into view). (9) On the SD: - make sure that the low indication is not in view for the yellow hydraulic system - make sure that the fluid level index is green. (10) Disconnect the ground hydraulic service cart from the reservoir filling self-sealing ground connector (5203JM) and install the blanking cap. 5. Close-up ________ Subtask 12-12-29-865-064 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 9JJ, 10JJ. Subtask 12-12-29-862-054 B. Put the Aircraft back to its Initial Configuration (1) On the ECAM control panel, set the UPPER DISPLAY and LOWER DISPLAY potentiometers to OFF. (2) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). Subtask 12-12-29-410-054 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access doors 811. (3) Close the Green ground service panel 197CB. (4) Remove the access platform(s).
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TASK 12-12-29-611-806 Fill the Yellow Hydraulic Reservoir with a Hand Pump WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE _______ CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM. MOVEMENT OF THE FLIGHT CONTROL SURFACES CAN BE DANGEROUS AND/OR CAUSE DAMAGE. R R R
WARNING : DO NOT GET THE FLUID ON YOUR SKIN OR IN YOUR EYES. IF YOU DO: _______ - FLUSH IT AWAY WITH CLEAN WATER - GET MEDICAL AID. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
circuit breaker(s) safety clip(s) hydraulic fluid container access platform 2.5 m (8 ft. 2 in.)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 02-003
R
Material No. 02-003A
R
Material No. 02-003B Material No. 02-003C
F NSA 307110 HYDRAULIC FLUID (Ref. 20-31-00) F NSA 307110 HYDRAULIC FLUID (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00)
TYPE 4 (PHOSPHATE ESTER BASE) TYPE 4 (PHOSPHATE ESTER BASE) TYPE 4 (PHOSPHATE ESTER BASE) TYPE IV (PHOSPHATE ESTER BASE)
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 02-003D
R R
Material No. 02-003E
F NSA 307-110 TYPE IV HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00) F NSA 307-110 HYDRAULIC FLUID (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 24-41-00-862-801 29-00-00-864-803 29-00-00-870-806 29-10-00-200-802 29-14-00-614-804 29-14-00-614-804 31-60-00-860-801 12-12-29-991-001
Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Depressurize the Yellow Hydraulic System (Pressurized with the Hydraulic Ground Supply) Bleeding of the Yellow Hydraulic System Check of the Nitrogen Charging Pressure on Hydraulic Power Accumulator (5151JM1,5151JM2,5151JM3) Pressurization of the Hydraulic Reservoirs with external bench Pressurization of the Hydraulic Reservoirs with the APU EIS Start Procedure Fig. 301
3. __________ Job Set-up Subtask 12-12-29-861-055 A. Energize the aircraft electrical circuits circuits (Ref. TASK 24-41-00-861-801). Subtask 12-12-29-010-055 B. Get Access (1) Put the access platform in position at the access door 811. (2) Open the access door 811.
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(3) Put the access platform in position at the access door 197CB. (4) Open the Green ground service panel 197CB. Subtask 12-12-29-865-065 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------722VU HYD PUMP Y SVCE 10JJ N46 722VU HYD PUMP Y CTL 9JJ R36 Subtask 12-12-29-865-066 D. Make sure that this(these) circuit breaker(s) is(are) closed: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU HSMU B + PART G 6JG U10 722VU HSMU Y + PART G 7JG X46 Subtask 12-12-29-860-055 E. Aircraft Maintenance Configuration (1) Make sure that the aircraft is in this configuration: - the speed brakes and the spoilers are retracted - the thrust reversers are stowed - the landing gear is extended and the landing gear doors are closed - all the other hydraulic services are in the normal position - the FWD and AFT cargo compartment doors 821, 822 are closed. (2) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803) (3) Make sure that the Yellow hydraulic system accumulator is pressurized (Ref. TASK 29-10-00-200-802). (4) Make sure that the reservoir of the Yellow hydraulic system is pressurized (Ref. TASK 29-14-00-614-804) or (Ref. TASK 29-14-00-614804)
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4. Procedure _________ (Ref. Fig. 301/TASK 12-12-29-991-001) CAUTION : MAKE SURE THAT YOU OPERATE THE HAND PUMP SLOWLY AND SMOOTHLY. THE _______ HANDLE MUST NOT HIT THE STOPS WITH TOO MUCH FORCE. IF YOU DO NOT OBEY THESE PRECAUTIONS, DAMAGE CAN OCCUR TO THE HAND PUMP AND TO THE SERVICING LINE ON THE OTHER SIDE OF THE SERVICING PANEL. Subtask 12-12-29-611-055 A. Fill the Yellow hydraulic reservoir NOTE : If you replace one or more components on the high pressure and/or ____ low pressure side, - If there is a hydraulic-fluid low level which causes loss of the system, - If there is a large loss of hydraulic fluid, - Do the related bleed procedure to make sure that the quantity of hydraulic fluid in the system is correct:(Ref. TASK 29-00-00870-806) (1) Remove the hand pump lever 5205JM. (2) Connect the hand pump lever 5205JM to the shaft of the reservoir filling hand pump 5204JM. (3) Remove the reservoir filling hose 5213JM. (4) Remove the blanking cap and connect the filling hose 5213JM to the filling valve 5211JM. (5) Put the other end of the filling hose in the hydraulic fluid container filled with HYDRAULIC FLUIDS (Material No. 02-003), or HYDRAULIC FLUIDS (Material No. 02-003A), or HYDRAULIC FLUIDS (Material No. 02-003B), or HYDRAULIC FLUIDS (Material No. 02-003C), or HYDRAULIC FLUIDS (Material No. 02-003D). HYDRAULIC FLUIDS (Material No. 02-003E)
R R R R
(6) On the reservoir-filling manual selector-valve 4JS, select the YELLOW position. (7) Operate the hand pump lever and monitor the increase of the fluid level on the reservoir hydraulic quantity indicator 5JS. (8) Stop the flow when the pointer is in the center position on the reservoir hydraulic quantity indicator 5JS.
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(9) Turn the reservoir-filling manual selector-valve 4JS to the NEUTRAL position. (On the reservoir hydraulic quantity indicator 5JS, the pointer is in the INOP position). (10) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00-860-801). (11) On the ECAM control panel on the center pedestal, press the HYD pushbutton. Make sure that the HYD page is shown on SD. (12) On the SD: - check that the low indication is not in view for the Yellow hydraulic system - check that the fluid level index is green. (13) Remove the filling hose 5213JM and install the blanking cap on the hand pump. (14) Put the filling hose back in position on its mounting. (15) Remove the hand pump lever 5205JM from the hand pump 5204JM and put it in position on the Green ground service panel. 5. Close-up ________ Subtask 12-12-29-865-067 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 9JJ, 10JJ. Subtask 12-12-29-862-055 B. Put the Aircraft back to its Initial Configuration (1) On the ECAM control panel, set the UPPER DISPLAY and LOWER DISPLAY potentiometers to OFF. (2) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
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Subtask 12-12-29-410-055 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access doors 811. (3) Close the Green ground service panel 197CB. (4) Remove the access platform(s).
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LANDING GEAR - SERVICING ________________________ TASK 12-12-32-611-801 Hydraulic Replenishment of the MLG Shock Absorber (Aircraft on Jacks) WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED ON THE _______ LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
approved nitrogen supply container hose
R No specific No specific No specific No specific No specific No specific 460007156 98F32104021001
pressure gage 0 - 60 bar thermometer transparent bleed tube warning notice 3-way valve access platform 3.5 m (11 ft. 6 in.) 1 ADAPTER, CHARGING - MLG 1 COMPRESSION TOOL
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B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------No specific Material No. 02-001
lockwire, corrosion-resistant steel 0.8 mm (0.032 in) dia. USA MIL-H-5606 OIL, HYDRAULICPETROLEUM FLUID (Ref. 20-31-00)
Material No. 02-004 R R
Material No. 02-006 Material No. 05-004B Material No. 19-010
SHOCK ABSORBER FLUID (Ref. 20-31-00) USA BMS 3-32 TYPE II SHOCK ABSORBER FLUID (Ref. 20-31-00) USA MIL-L-25567 TYPE I OXYGEN LEAK DETECTOR (Ref. 20-31-00) USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------07-11-00-581-801 07-11-00-586-801 29-00-00-864-804 32-00-00-481-801 R
32-11-13-960-801 32-11-15-000-802 32-11-15-400-802 12-12-32-991-002 12-12-32-991-010 12-12-32-991-001 12-12-32-991-016 12-12-32-991-007-A
Lifting of the Aircraft for Maintenance Operations Lowering of the Aircraft for Maintenance Operations Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Installation of the Safety Devices on the Landing Gears Replacement of the MLG Shock Absorber Seals Removal of the MLG Bogie-Alignment Pitch Trimmer (Aircraft on Jacks) Installation of the MLG Bogie-Alignment Pitch Trimmer (Aircraft on Jacks) Fig. 301 Fig. 302 Fig. 303 Fig. 304 Fig. 305
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3. __________ Job Set-up Subtask 12-12-32-941-050 A. Safety Precautions (1) Put the warning notice in the cockpit, to tell persons not to operate the landing gear controls. Subtask 12-12-32-860-050 B. Aircraft Maintenance Configuration (1) Make sure that the Green hydraulic system is depressurized (Ref. TASK 29-00-00-864-804). (2) Make sure that the safety devices are installed on the L/G (Ref. TASK 32-00-00-481-801). Subtask 12-12-32-582-050 C. Lift the Aircraft (1) Lift the aircraft on jacks (Ref. TASK 07-11-00-581-801). (2) Make sure that the wheels of the applicable MLG are clear of the ground (3) Make sure that the applicable MLG shock absorber has fully extended. Subtask 12-12-32-010-050 D. Get Access (1) Put the access platform in position at the applicable zone: - for the LH MLG shock absorber at zone 731 - for the RH MLG shock absorber at zone 741. (2) Remove and discard the lockwire from the bolts (6) (Ref. Fig. 301/TASK 12-12-32-991-002) (3) Remove the bolts (6), the washers (5), the bracket (4) and the panel (3).
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MLG Shock Absorber - Inflation/Bleed Valves Figure 301/TASK 12-12-32-991-002
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Subtask 12-12-32-480-057 E. Installation of the Compression Tool on the Applicable Gear (COMPRESSION TOOL (98F32104021001)) (Ref. Fig. 302/TASK 12-12-32-991-010) (1) Install the oleo control unit: (a) Install the housing (25) in the right side of the upper torque link bore. (b) Install the spindle (43) in the left side of the upper torque link until it engages the housing (25). (c) Fully install and tighten the bolt (23). NOTE : The housing (25) and spindle (43) must be free to turn in ____ the bore. (d) Install the housing (30) in the right side of the lower torque link bore. (e) Install the spindle (38) in the left side of the lower torque link until it engages the housing (30). (f) Fully install and tighten the bolt (28). NOTE : The housing (30) and spindle (38) must be free to turn in ____ the bore. (2) Installation of the bogie control unit: (a) Make sure that the bogie control cylinder (36) is installed on the yoke (35). (b) Install the adaptor (57) on the bogie beam with the washer (62), the bolt (54), the nut (59) and the locking pin (58). (c) Put the yoke (35) (together with the assembled parts) in position on the spindle (38) and the housing (30). (d) Install the clamps (31) with the bolts (32). (e) Install the cylinder clevis (61) on the rod (63). (f) Connect the hydraulic coupling (64) to the bogie control cylinder (36).
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Compression Tool - Installation and Operation Figure 302/TASK 12-12-32-991-010- 14 (SHEET 1)
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Compression Tool - Installation and Operation Figure 302/TASK 12-12-32-991-010- 24 (SHEET 2)
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Compression Tool - Installation and Operation Figure 302/TASK 12-12-32-991-010- 34 (SHEET 3)
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Compression Tool - Installation and Operation Figure 302/TASK 12-12-32-991-010- 44 (SHEET 4)
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(g) On the compression-tool hydraulic control-panel, open the bogie beam vent valve. (h) Manually extend the rod (63) until the cylinder clevis (61) aligns with the adaptor (57). (i) Install the pin (60), the washer (55) and the locking pin (56). (3) Install the oleo control cylinders: (a) Attach the cylinder (21) to the housing (25) with the retainer nut (26). (b) Attach the other cylinder (21) to the spindle (43) with the retainer nut (42). NOTE : Make sure that the hydraulic ports (22) point aft. ____ (c) Install the clevis (27) and the clevis (41) on the applicable cylinder rod (24). (d) On the compression tool hydraulic control panel, - set the oleo descent valve to OPEN. - set the oleo directional control valve to DOWN. (e) Operate the hand pump to extend the cylinder rods (24) until: - the clevis (27) aligns with the clevis on the housing (30) - the clevis (41) aligns with the clevis on the spindle (38). (f) Install the pins (29) and (37), the washers (33) and (39) and the lock pins (34) and (40). Subtask 12-12-32-614-050 R
F. Preparation (Ref. Fig. 303/TASK 12-12-32-991-001) (1) Install the ADAPTER, CHARGING - MLG on the bleed/inflation valve (1). (2) Connect the hose between the ADAPTER, CHARGING - MLG and the 3-way valve. (3) Connect a transparent bleed tube between the 3-way valve and the container. Make sure that the free end of the bleed tube is a minimum of 400 mm (16 in.) below the bleed/inflation valve (1). (4) Connect the approved nitrogen supply to the 3-way valve.
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MLG Shock Absorber Charge - Charge and Inflation Details Figure 303/TASK 12-12-32-991-001 EFF : ALL 12-12-32 R SROS
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(5) Make sure that the pressure control valve is closed. (6) On the 3-way valve, open the bleed control valve. (7) Slowly open the bleed/inflation valve (1), to release the nitrogen from the gas chamber. Leave the bleed/inflation valve (1) open for a minimum of 2 hours. This will let the gas separate from the oil. (8) Remove the blanking cap (8). R R R
(9) Connect the hydraulic supply to the filling valve (9). Use HYDRAULIC FLUIDS (Material No. 02-001) or HYDRAULIC FLUIDS (Material No. 02004) or HYDRAULIC FLUIDS (Material No. 02-006).
R R
NOTE : Hydraulic fluids 02-001, 02-004 and 02-006 can be mixed in all ____ applicable maintenance tasks and in all quantities. Subtask 12-12-32-864-050 G. Depressurization of the Pitch Trimmer (1) Depressurize the pitch trimmer (Ref. TASK 32-11-15-000-802). 4. Procedure _________ Subtask 12-12-32-611-050 A. To Fill the Shock Absorber with Hydraulic Fluid (Ref. Fig. 304/TASK 12-12-32-991-016) WARNING : DO NOT GET THE FLUID ON YOUR SKIN OR IN YOUR EYES. IF YOU DO: _______ - FLUSH IT AWAY WITH CLEAN WATER - GET MEDICAL AID. CAUTION : MAKE SURE THAT THE FLUID DOES NOT STAY ON THE AIRCRAFT _______ STRUCTURE. IF THE FLUID GETS ON THE AIRCRAFT STRUCTURE, WASH IT OFF IMMEDIATELY WITH SOAP AND WATER. (1) Operate the COMPRESSION TOOL until the shock absorber is fully compressed. (a) On the hydraulic control panel: - set the oleo descent control valve to CLOSE - set the bogie beam vent valve to CLOSE - set the oleo directional control valve to UP.
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MLG Shock Absorber - Dimension Details Figure 304/TASK 12-12-32-991-016
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(b) Operate the hand pump until the shock absorber is fully compressed. (2) Measure the dimension H. This should be between 43.5 mm (1.7125 in.) and 52.5 mm (2.0669 in.). NOTE : The dimension H is measured between the inner faces of the ____ torque link lugs. (3) Remove and discard the lockwire from the secondary bleed valve (2). R R R R R
NOTE : Make sure you do not move the seal changeover valve when you ____ remove the lockwire from the secondary bleed valve (2) at step (3). If the seal changeover valve is moved it must be set back counterclockwise to the open position (Ref. TASK 32-11-13-960801). (4) Connect a transparent bleed tube between the secondary bleed valve (2) and the container. (5) Make sure that the bleed screw (7) is closed and correctly torqued. (6) Carefully open the secondary bleed valve (2). (7) Open the hydraulic shut off valve. (8) Open the filling valve (9). (9) Monitor the flow of fluid from the bleed hoses and slowly increase the hydraulic supply to a maximum pressure of 1.7 bar (24.0 psi). (10) When the flow of fluid from the secondary bleed valve (2) is free from air, do these steps: (a) Continue to monitor the fluid until a minimum of 5 l (1.30 USgal) has come out of the shock absorber which is free from air. (b) Close the secondary bleed valve (2). (11) When the flow of fluid from the bleed/inflation valve (1) is free from air, close the filling valve (9). (12) Close the hydraulic shut off valve.
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(13) Continue to monitor the flow of fluid from the bleed/inflation valve (1) for 10 minutes. NOTE : Make sure that the free end of the bleed tube is a minimum of ____ 400 mm (16 in.) below the bleed/inflation valve (1). (14) When the flow of fluid stops, close the bleed/inflation valve (1). (15) On the 3-way valve, close the bleed control valve. (16) Remove the clear bleed tubes and the container. (17) TORQUE the secondary bleed valve (2) to between 0.29 and 0.34 m.daN (25 and 30 lbf.in.). (18) Safety the secondary bleed valve (2) with MISCELLANEOUS (Material No. 19-010). (19) Remove the hydraulic supply line from the filling valve (9). Subtask 12-12-32-614-051 B. Inflation of the Shock Absorber (Ref. Fig. 305/TASK 12-12-32-991-007-A) WARNING : DO NOT PUT COMPRESSED GAS IN CONTACT WITH YOUR SKIN. THE GAS _______ CAN GO THROUGH THE SKIN AND MAKE BUBBLES IN THE BLOOD. THIS CONDITION CAN KILL YOU. CAUTION : DO NOT INFLATE THE MLG SHOCK ABSORBER AT THE LOWER VALVE. IF _______ YOU USE THE LOWER VALVE HYDRAULIC FLUID WILL COME OUT. CAUTION : DO NOT INSTALL A DUST CAP ON THE BLEED/INFLATION VALVE OF THE _______ MLG SHOCK ABSORBER. IF YOU DO, THERE IS A RISK THAT IT WILL FALL INTO THE SHOCK ABSORBER. NOTE : This procedure is only applicable when the hydraulic fluid level ____ was changed. For the applicable procedure to inflate the shock absorber with nitrogen only, Ref. TASK 12-14-32-614-802. (1) Use the ADAPTER, CHARGING - MLG to open the bleed/inflation valve (1). (2) On the 3-way valve, open the bleed control valve.
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MLG Shock Absorber - Pressure Extension Chart Figure 305/TASK 12-12-32-991-007-A12 (SHEET 1) EFF : ALL 12-12-32 R SROS
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MLG Shock Absorber - Pressure Extension Chart Figure 305/TASK 12-12-32-991-007-A22 (SHEET 2) EFF : ALL 12-12-32 R SROS
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(3) Operate the COMPRESSION TOOL to let the shock absorber extend fully: (a) On the hydraulic control panel: - set the oleo directional control valve to DOWN - set the oleo descent control valve to OPEN. NOTE : If the oleo does not extend, operate the hand pump until ____ movement of the oleo occurs. (b) When the shock absorber is fully extended, set the bogie beam control-cylinder vent-valve to OPEN. (c) Set the oleo directional control valve to UP (this will vent the full bore side of the oleo control cylinders (21). (4) Make sure that the shock absorber extends fully to give a dimension H of between 773.5 mm (30.45 in.) and 782.5 mm (30.81 in.). (5) On the 3-way valve, close the bleed control valve. (6) Do these steps: R R
(a) Use a thermometer to measure the surface temperature of the aluminum piston adjacent to the bleed/inflation valve (1). (b) Look at the fully extended inflation chart and find the correct inflation pressure for the temperature you measured at step (a). If your measured value is different from the chart values, use the best approximate value from the chart. (7) At the nitrogen source, set the regulator to the pressure you found at step (6)(b). (8) Open the nitrogen shut off valve. (9) On the 3-way valve, open the pressure control valve. (10) Inflate the shock absorber to the pressure you found at step (6)(b). (Use a pressure gage 0 - 60 bar). (11) Close the nitrogen shut-off valve. (12) After a minimum period of 10 minutes (to let the shock absorber become stable), measure the temperature and pressure again. (13) If the pressure is not in compliance with the fully extended inflation chart, do the steps (7) thru (9) again.
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(14) Close the bleed/inflation valve (1) and release the nitrogen supply pressure. (15) On the 3-way valve, close the pressure control valve. (16) Close the nitrogen shut-off valve. (17) Remove the nitrogen supply from the 3-way valve. (18) Remove the 3-way valve together with the hose. (19) Remove the ADAPTER, CHARGING - MLG from the bleed inflation valve (1). Subtask 12-12-32-942-050 C. Removal of Equipment (Ref. Fig. 302/TASK 12-12-32-991-010) (1) Removal of the COMPRESSION TOOL: (a) Disconnect the hydraulic lines (22) from the cylinders (21). (b) Disconnect the hydraulic line (64) from the cylinder (36). (c) Remove: - the lock pins (34) and pins (29) and (37) - the retainer nut (26), - the retainer nut (42), - the lock pin (56), the
(40), the washers (33) and (39) and the the cylinder (21) and the clevis (27). the cylinder (21) and the clevis (41). washer (55) and the pin (60).
(d) Hold the yoke assembly (35) (together with the bogie beam cylinder (36)) and remove the bolts (32) and the clamps (31). (e) Remove the yoke assembly (35). (f) Remove: - the lock pin (58), the nut (59), the bolt (54) and the adaptor (57) - the bolts (23) and (28), the spindles (38) and (43) and the housings (25) and (30). (2) Make sure that the work area is clean and clear of tools and other items.
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Subtask 12-12-32-870-050 D. Bleeding of the Pitch Trimmer (1) Do the bleed procedure for the pitch trimmer (Ref. TASK 32-11-15-400802). Subtask 12-12-32-586-050 E. Aircraft Maintenance Configuration (1) Lower the aircraft off the jacks (Ref. TASK 07-11-00-586-801). 5. Close-up ________ Subtask 12-12-32-780-050 A. Pressure/Extension Check (Ref. Fig. 305/TASK 12-12-32-991-007-A) (1) Measure: - the nitrogen pressure - the surface temperature of the aluminum piston adjacent to the bleed/inflation valve (1) - the dimension H.
R R
(2) Make sure these measurements agree with the specified data given in the Pressure Extension Chart (Aircraft Weight on Wheels). (3) TORQUE the bleed/inflation valve (1) to between 0.6 and 0.8 m.daN (50 and 70 lbf.in.). (4) Use the SPECIAL MATERIALS (Material No. 05-004B) to do a nitrogen leak test of the bleed/inflation valve (1). Leaks are not permitted. (5) TORQUE the filling valve (9) to between 0.6 and 0.8 m.daN (50 and 70 lbf.in.) (6) Install the blanking cap (8). (7) Examine the filling valve (9) for hydraulic leaks. Leaks are not permitted.
EFF : ALL 12-12-32 SROS
Page 320 Jul 01/06
Subtask 12-12-32-410-051 B. Close Access (1) Install the access panel (3) with the bracket (4), the washers (5) and the bolts (6). (2) Safety the bolts (6) with lockwire, corrosion-resistant steel 0.8 mm (0.032 in) dia. Subtask 12-12-32-942-053 C. Removal of the Ground Support Equipment (1) Remove the access platform(s). (2) Remove the warning notice(s). (3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL 12-12-32 R SROS
Page 321 Jul 01/06
TASK 12-12-32-611-804 Hydraulic Replenishment of the MLG Shock Absorber (Weight on Wheels) WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED ON THE _______ LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
container hose
R No No No No No No No No No
specific specific specific specific specific specific specific specific specific
460007156
pressure gage 0 - 200 bar safety barriers standard charging equipment thermometer transparent bleed tube warning notices 3-way valve adjustable access platform 3.5 m (11 ft. 6 in.) Torque Wrench : range 0.00 to 1.20 m.daN (0.00 to 9.00 lbf.ft) 1 ADAPTER, CHARGING - MLG
R
EFF : ALL 12-12-32 SROS
Page 322 Jul 01/06
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 02-001
USA MIL-H-5606 OIL, HYDRAULICPETROLEUM FLUID (Ref. 20-31-00)
Material No. 02-004 R R
Material No. 02-006 Material No. 05-004B Material No. 19-010
SHOCK ABSORBER FLUID (Ref. 20-31-00) USA BMS 3-32 TYPE II SHOCK ABSORBER FLUID (Ref. 20-31-00) USA MIL-L-25567 TYPE I OXYGEN LEAK DETECTOR (Ref. 20-31-00) USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-804 32-00-00-481-801 R
32-11-13-960-801 32-12-00-410-801 12-12-32-991-002 12-12-32-991-001 12-12-32-991-016 12-12-32-991-007-A
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Installation of the Safety Devices on the Landing Gears Replacement of the MLG Shock Absorber Seals Close the MLG Doors after Maintenance Fig. 301 Fig. 303 Fig. 304 Fig. 305
EFF : ALL 12-12-32 SROS
Page 323 Jul 01/06
3. __________ Job Set-up Subtask 12-12-32-941-054 A. Safety Precautions (1) Put the safety barriers in position. (2) Put the warning notices: - in the cockpit to tell persons not to operate the landing gear controls. - at the applicable ground door opening handle to tell persons not to open the MLG door. Subtask 12-12-32-860-053 B. Aircraft Maintenance Configuration (1) Make sure that the Green hydraulic system is depressurized (Ref. TASK 29-00-00-864-804). (2) Make sure that the safety devices are installed on the L/G (Ref. TASK 32-00-00-481-801). (3) MLG door configuration: CAUTION : YOU MUST CLOSE THE MLG DOORS BEFORE YOU DEFLATE THE MAIN _______ LANDING-GEAR SHOCK-ABSORBER. IF THE DOORS STAY OPEN, THEY WILL HIT THE GROUND AND DAMAGE WILL OCCUR. (a) Make sure that the applicable MLG door is closed (Ref. TASK 3212-00-410-801). Subtask 12-12-32-010-057 C. Get Access (Ref. Fig. 301/TASK 12-12-32-991-002) (1) Put the adjustable access platform at the applicable zone: - for the LH MLG shock absorber at zone 731 - for the RH MLG shock absorber at zone 741. (2) Remove and discard the lockwire from the bolts (6). (3) Remove the bolts (6), the washers (5), the bracket (4) and the panel (3).
EFF : ALL 12-12-32 R SROS
Page 324 Jul 01/06
Subtask 12-12-32-614-056 R
D. Preparation WARNING : MAKE SURE THAT THE AREA AROUND THE AIRCRAFT IS CLEAR BEFORE YOU _______ PRESSURIZE/DEPRESSURIZE THE SHOCK ABSORBER, WITH THE AIRCRAFT WEIGHT ON THE GROUND. THE MOVEMENT OF THE AIRCRAFT COULD BE DANGEROUS. (Ref. Fig. 303/TASK 12-12-32-991-001, 305/TASK 12-12-32-991-007-A) (1) Install the ADAPTER, CHARGING - MLG on the bleed/inflation valve (1). (2) Connect the hose between the ADAPTER, CHARGING - MLG and the 3-way valve. (3) Connect a transparent bleed tube between the 3-way valve and the container. Make sure that the free end of the bleed tube is a minimum of 400 mm (16 in.) below the bleed inflation valve. (4) On the 3-way valve, make sure that the pressure control valve is closed, then open the bleed control valve. (5) Open the bleed/inflation valve (1) to release the nitrogen pressure from the gas chamber. Let the weight of the aircraft compress the shock absorber. (6) Measure the dimension H. This should be between 43.5 mm (1.7125 in.) and 52.5 mm (2.0669 in.). (7) Let the bleed/inflation valve (1) stay open for a minimum of 2 hours (to let the gas separate from the oil). (8) Remove the blanking cap (8).
R R R
(9) Connect the hydraulic supply to the filling valve (9). Use HYDRAULIC FLUIDS (Material No. 02-001) or HYDRAULIC FLUIDS (Material No. 02004) or HYDRAULIC FLUIDS (Material No. 02-006).
R R
NOTE : Hydraulic fluids 02-001, 02-004 and 02-006 can be mixed in all ____ applicable maintenance tasks and in all quantities.
EFF : ALL 12-12-32 SROS
Page 325 Jul 01/06
4. Procedure _________ Subtask 12-12-32-611-054 A. Filling the Shock Absorber with Hydraulic Fluid WARNING : DO NOT GET THE FLUID ON YOUR SKIN OR IN YOUR EYES. IF YOU DO: _______ - FLUSH IT AWAY WITH CLEAN WATER - GET MEDICAL AID. WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. _______ CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU. CAUTION : MAKE SURE THAT THE FLUID DOES NOT STAY ON THE AIRCRAFT _______ STRUCTURE. IF THE FLUID GETS ON THE AIRCRAFT STRUCTURE, WASH IT OFF IMMEDIATELY WITH SOAP AND WATER. (1) Remove and discard the lockwire from the secondary bleed valve (2). R R R R R
NOTE : Make sure you do not move the seal changeover valve when you ____ remove the lockwire from the secondary bleed valve (2) at step (1). If the seal changeover valve is moved it must be set back counterclockwise to the open position (Ref. TASK 32-11-13-960801). (2) Connect a bleed hose between the secondary bleed valve (2) and the container. (3) Carefully open the secondary bleed valve (2). (4) Open the hydraulic shut off valve. (5) Open the filling valve (9). (6) Monitor the flow of fluid from the bleed hoses and slowly increase the hydraulic pressure to a maximum of 1.7 bar (25 psi). (7) When the flow of fluid from the secondary bleed valve (2) is free from air, do this procedure: (a) Continue to monitor the fluid until a minimum of 5l (1.3 US gal) has come out of the shock absorber which is free from air. (b) Close the secondary bleed valve (2).
EFF : ALL 12-12-32 SROS
Page 326 Jul 01/06
(8) When the flow of fluid from the bleed/inflation valve (1) is free from air, close the filling valve (9). (9) Close the hydraulic shut off valve. (10) Continue to monitor the flow of fluid from the bleed/inflation valve (1) for 10 minutes. (11) When the oil has drained, close the bleed/inflation valve (1). (12) On the 3-way valve, close the bleed control valve. (13) Remove the transparent bleed tubes and the container. (14) TORQUE the secondary bleed valve to between 0.29 and 0.34 m.daN (25 and 30 lbf.in.). (15) Safety the secondary bleed valve (2) with MISCELLANEOUS (Material No. 19-010). (16) Remove the hydraulic supply line from the filling valve (9). Subtask 12-12-32-614-057 R
B. Inflation of the Shock Absorber WARNING : MAKE SURE THAT THE AREA AROUND THE AIRCRAFT IS CLEAR BEFORE YOU _______ PRESSURIZE/DEPRESSURIZE THE SHOCK ABSORBER, WITH THE AIRCRAFT WEIGHT ON THE GROUND. THE MOVEMENT OF THE AIRCRAFT COULD BE DANGEROUS. WARNING : DO NOT PUT COMPRESSED GAS IN CONTACT WITH YOUR SKIN. THE GAS _______ CAN GO THROUGH THE SKIN AND MAKE BUBBLES IN THE BLOOD. THIS CONDITION CAN KILL YOU. CAUTION : DO NOT INFLATE THE MLG SHOCK ABSORBER AT THE LOWER VALVE. IF _______ YOU USE THE LOWER VALVE HYDRAULIC FLUID WILL COME OUT. CAUTION : DO NOT INSTALL A DUST CAP ON THE BLEED/INFLATION VALVE OF THE _______ MLG SHOCK ABSORBER. IF YOU DO, THERE IS A RISK THAT IT WILL FALL INTO THE SHOCK ABSORBER. NOTE : This procedure is only applicable when the hydraulic fluid level ____ was changed. For the applicable procedure to inflate the shock absorber with nitrogen only, Ref. TASK 12-14-32-614-802.
EFF : ALL 12-12-32 SROS
Page 327 Jul 01/06
NOTE : You must use a pressure gage 0 - 200 bar when you do this ____ inflation procedure. R R
(1) Install the standard charging equipment on the ADAPTER, CHARGING MLG and open the nitrogen shut off valve. (2) On the 3-way valve, open the pressure control valve. (3) Use the ADAPTER, CHARGING - MLG to open the bleed/inflation valve (1). (4) Slowly increase the nitrogen supply pressure until the dimension H starts to increase. (5) Do these steps: (a) Use a thermometer to measure the surface temperature of the aluminium piston adjacent to the bleed/inflation valve (1). Write down the temperature. (b) Measure and write down the MLG pressure at the bleed/inflation valve (1). (c) Use the recorded pressure and temperature values to read the dimension H from the inflation chart. (Ref. Fig. 304/TASK 12-12-32-991-016, 305/TASK 12-12-32-991-007A) If your measured values are different from the values given in the chart, use the best approximate chart values. (d) Open the bleed/inflation valve (1) to control the shock absorber pressure. Adjust the pressure to give approximately the dimension H you identified at step (5)(c). (e) Measure and write down the MLG pressure at the bleed/inflation valve (1) (f) Measure and write down the dimension H. (g) Use the inflation chart to find the correct pressure for the dimension H. (6) If the pressure at step (5)(e) is less than the pressure at step (5)(g), do this procedure: (a) Adjust the nitrogen source to give the necessary pressure.
EFF : ALL 12-12-32 SROS
Page 328 Jul 01/06
(b) Slowly open the bleed/inflation valve (1). (c) Inflate the shock absorber to the correct pressure shown on the inflation chart. (d) When the pressure is correct, close the bleed/inflation valve (1). If the dimension H changes before you have the correct pressure, measure dimension H again. Use the new dimension H to do the procedure again from step (5)(e). (e) Close the charge valve on the nitrogen source. Let the shock absorber pressure and its dimension H become stable for a minimum of 10 minutes. (f) Measure the pressure and dimension H again. (g) If the pressure has changed, do the steps (6)(b) thru (6)(d) again. If the dimension H has changed, do the procedure again from step (5)(e). Use the new dimension H. (h) Close the bleed/inflation valve (1). (7) If the pressure at step (5)(e) is more than the pressure at step (5)(g), do this procedure: (a) Slowly open the bleed/inflation valve (1). (b) Deflate the shock absorber to the correct pressure you identified at step (5)(g) from the inflation chart. If the dimension H changes before you have the correct pressure, measure dimension H again. Use the new dimension H to do the procedure again from step (5)(e). (c) Close the charge valve on the nitrogen source. Let the shock absorber pressure and its dimension H become stable for a minimum of 10 minutes. (d) Measure the pressure and dimension H again. (e) If the pressure has changed, do the steps (7)(a) thru (7)(d) again. If the dimension H has changed do the procedure again from step (5)(e). Use the new dimension H. (f) Close the bleed/inflation valve (1). R
(8) Remove the nitrogen source from the standard charging equipment.
EFF : ALL 12-12-32 SROS
Page 329 Jul 01/06
R
(9) Remove the standard charging equipment from the ADAPTER, CHARGING MLG. (10) TORQUE the bleed/inflation valve (1) to between 0.60 and 0.80 m.daN (53.09 and 70.79 lbf.in). (11) Remove the ADAPTER, CHARGING - MLG. (12) Use the SPECIAL MATERIALS (Material No. 05-004B) to do a leak test of the bleed/inflation valve (1) and the bleed screw (7). No leakage is permitted. (13) TORQUE the filling valve (9) 0.60 and 0.80 m.daN (53 and 70 lbf.in.). (14) Install the blanking cap (8). (15) Examine the filling valve (9) for leakage. No leakage is permitted. 5. Close-up ________ Subtask 12-12-32-410-053 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panel (3) with the bracket (4), the washers (5) and the bolts (6). (3) Safety the bolts (6) with MISCELLANEOUS (Material No. 19-010). Subtask 12-12-32-942-056 B. Removal of Equipment (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 12-12-32 SROS
Page 330 Jul 01/06
TASK 12-12-32-611-805 Hydraulic Replenishment of the NLG Shock Absorber (Aircraft on Jacks) WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED ON THE _______ LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No R
specific specific specific specific specific specific
U21891000
axle jack with a lift height of 465 mm (18.31 in) transparent bleed tube container 5 l (1.3208 USgal) 1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE 1 WARNING NOTICE Torque Wrench : range 0.00 to 1.20 m.daN (0.00 to 9.00 lbf.ft) 2 ADAPTOR - INFLATION
EFF : ALL 12-12-32 SROS
Page 331 Jan 01/07
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 02-001
USA MIL-H-5606 OIL, HYDRAULICPETROLEUM FLUID (Ref. 20-31-00)
Material No. 02-004 R R
Material No. 02-006 Material No. 05-004B
SHOCK ABSORBER FLUID (Ref. 20-31-00) USA BMS 3-32 TYPE II SHOCK ABSORBER FLUID (Ref. 20-31-00) USA MIL-L-25567 TYPE I OXYGEN LEAK DETECTOR (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------07-11-00-581-801 07-11-00-581-802 07-11-00-586-801 07-11-00-586-802 12-14-32-614-804 29-00-00-864-804 32-00-00-081-802 32-00-00-481-801 32-21-00-220-803 32-22-00-010-801 32-22-00-410-801 12-12-32-991-005 12-12-32-991-006
Lifting of the Aircraft for Maintenance Operations Lifting of the Aircraft at the Forward Jacking Point, MLG Wheels on the Ground Lowering of the Aircraft for Maintenance Operations Lowering of the Aircraft at the Forward Jacking Point, MLG Wheels on the Ground Gas Replenishment of the NLG Shock Absorber Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Removal of the Safety Devices from the Landing Gear Doors Installation of the Safety Devices on the Landing Gears Check Nose Gear Shock Absorber Nitrogen Charge Pressure Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance Fig. 306 Fig. 307
EFF : ALL 12-12-32 SROS
Page 332 Jul 01/06
3. __________ Job Set-up R R R R R
Subtask 12-12-32-941-064 A. General Information The design of your NLG shock absorber does not permit AIRBUS to give a procedure to service the shock absorber with weight on wheels. Subtask 12-12-32-941-057
R
B. Safety Precautions (1) Put the WARNING NOTICE in the cockpit to tell persons not to operate the landing gear and the nosewheel steering controls. Subtask 12-12-32-860-054
R
C. Aircraft Maintenance Configuration (1) Make sure that the Green hydraulic system is depressurized (Ref. TASK 29-00-00-864-804). (2) Make sure that the safety devices are installed on the L/G (Ref. TASK 32-00-00-481-801). Subtask 12-12-32-582-054
R
D. Lift the Aircraft (1) Make sure that the aircraft is on jacks and that the wheels of the NLG are clear of the ground (Ref. TASK 07-11-00-581-801) or (Ref. TASK 07-11-00-581-802). (2) Make sure that the shock absorber is fully extended. Subtask 12-12-32-582-053
R
E. Put the axle jack with a lift height of 465 mm (18.31 in) below the NLG jacking dome.
EFF : ALL 12-12-32 SROS
Page 333 Jul 01/06
Subtask 12-12-32-010-059 F. Get Access (1) Open the NLG forward doors (Ref. TASK 32-22-00-010-801). (2) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at zone 711. Subtask 12-12-32-614-059 G. Preparation (Ref. Fig. 306/TASK 12-12-32-991-005, 307/TASK 12-12-32-991-006) (1) Remove the blanking caps (1) and (3). R
(2) Install a ADAPTOR - INFLATION (U21891000) on each of the charging valves (2) and (4). (3) Connect the hydraulic filling hose to the FILLING ASSEMBLY at the charging valve (2) and the three-way valve. (4) Connect the transparent bleed tube between the 3-way valve and the container. (5) Connect the hydraulic supply to the 3-way valve and the FILLING ASSEMBLY. Use HYDRAULIC FLUIDS (Material No. 02-001) or HYDRAULIC FLUIDS (Material No. 02-004) or HYDRAULIC FLUIDS (Material No. 02006). NOTE : Hydraulic fluids 02-001, 02-004 and 02-006 can be mixed in all ____ applicable maintenance tasks and in all quantities. (6) Make sure that the pressure control valve on the 3-way valve is closed, then open the bleed control valve. (7) Operate the FILLING ASSEMBLY at the charging valve (4) to decrease the nitrogen pressure in the second stage (HP) pressure chamber to zero. Leave the charging valve (4) open. NOTE : This makes sure that the floating piston is on its lower stop. ____ (8) Operate the FILLING ASSEMBLY at the charging valve (2) to decrease the nitrogen pressure in the first stage (LP) pressure chamber to zero. Leave the charging valve (2) open.
EFF : ALL 12-12-32 SROS
Page 334 Jan 01/07
NLG Shock Absorber - Filling System Figure 306/TASK 12-12-32-991-005 EFF : ALL 12-12-32 R SROS
Page 335 Jul 01/06
NLG Shock Absorber - Inflation/Filling Valves Figure 307/TASK 12-12-32-991-006 EFF : ALL 12-12-32 R SROS
Page 336 Jul 01/06
4. Procedure _________ Subtask 12-12-32-611-055 R
A. Fill the Shock Absorber with Hydraulic Fluid WARNING : DO NOT GET THE FLUID ON YOUR SKIN OR IN YOUR EYES. IF YOU DO: _______ - FLUSH IT AWAY WITH CLEAN WATER - GET MEDICAL AID. CAUTION : MAKE SURE THAT THE FLUID DOES NOT STAY ON THE AIRCRAFT _______ STRUCTURE. IF THE FLUID GETS ON THE AIRCRAFT STRUCTURE, WASH IT OFF IMMEDIATELY WITH SOAP AND WATER. (1) During this step, monitor the flow of hydraulic fluid through the transparent bleed hose. (a) Close the bleed control valve and open the FILLING ASSEMBLY at the charging valve (2).
R R R R
(b) Slowly fill the first stage pressure chamber with HYDRAULIC FLUIDS (Material No. 02-001) or HYDRAULIC FLUIDS (Material No. 02-004) or HYDRAULIC FLUIDS (Material No. 02-006) pressurized to 15 bar (217 psi) maximum.
R R
NOTE : Hydraulic fluids 02-001, 02-004 and 02-006 can be mixed in ____ all applicable maintenance tasks in all quantities. (c) Decrease the pressure to zero and leave the charging valve (2) open. (2) Install a FILLING ASSEMBLY on the charging valve (4) and connect the nitrogen filling hose to the FILLING ASSEMBLY. (3) Connect the nitrogen supply hose to the nitrogen filling hose. (4) Slowly pressurize the second stage pressure chamber (HP) with nitrogen. NOTE : The floating piston goes against the upper stop and hydraulic ____ fluid is pushed out of the first stage pressure chamber (LP). (5) Increase the nitrogen pressure at the charging valve (4) to the correct pressure (Ref. TASK 12-14-32-614-804). (6) Close the charging valve (4) and TORQUE it to between 0.57 and 0.79 m.daN (50.44 and 69.91 lbf.in).
EFF : ALL 12-12-32 SROS
Page 337 Jul 01/06
(7) Use the SPECIAL MATERIALS (Material No. 05-004B) to do a leak check of the charging valve (4). Leakage must not occur. (8) Remove the FILLING ASSEMBLY from the charging valve (4) and disconnect the nitrogen filling hose. (9) Make sure that the first stage pressure chamber is full of hydraulic fluid. If necessary do step (1) again. (10) During this step monitor the flow of hydraulic fluid through the transparent bleed hose: NOTE : During these steps you will use the hydraulic supply to extend ____ the sliding tube. (a) Slowly operate the axle jack to push the sliding tube fully in to the main fitting. (b) Do the procedure in step (1) again and let the sliding tube fully extend. (c) Do the steps (a) and (b) again until the flow of hydraulic fluid from the transparent bleed tube is free from air bubbles. (11) Do the procedure in step (1) again and let the sliding tube fully extend. (12) Operate the axle jack to push the sliding tube in to the main fitting until the dimension H is between 189 and 194 mm (7.44 to 7.64 in). (13) Connect the nitrogen filling hose to the charging valve (2) and connect the nitrogen supply hose to the nitrogen filling hose. (14) Slowly pressurize the first stage pressure chamber (LP) with nitrogen and open the valve on the axle jack, in a controlled manner, to let the shock absorber fully extend. (15) Increase the nitrogen pressure to the correct pressure (Ref. TASK 1214-32-614-804). (16) Make sure that the shock absorber dimension H is between 408 and 416 mm (16.07 and 16.37 in). (17) Close the pressure control valve. (18) Use the FILLING ASSEMBLY to close the charge valve (2).
EFF : ALL 12-12-32 R SROS
Page 338 Jul 01/06
(19) Decrease the nitrogen supply pressure to zero. (20) Disconnect the nitrogen supply. (21) Use a SPECIAL MATERIALS (Material No. 05-004B) to do a leak check of the charging valve (2) and (4). Leakage must not occur. (22) Install the blanking caps on the charging valves (2) and (4). (23) Remove the axle jack. (24) Disconnect the hydraulic supply and remove the bleed hose and the container. Subtask 12-12-32-942-057 B. Removal of the Support Equipment (1) Remove the access platform. (2) Make sure that the work area is clean and clear of tools and other items. Subtask 12-12-32-586-053 C. Lower the Aircraft (1) Lower the aircraft off jacks (Ref. TASK 07-11-00-586-801) or (Ref. TASK 07-11-00-586-802). Subtask 12-12-32-780-054 D. Pressure/Extension Check (1) Do a pressure/extension check of the NLG shock absorber (Ref. TASK 32-21-00-220-803). 5. Close-up ________ Subtask 12-12-32-410-054 A. Close Access (1) Remove the safety devices from the NLG doors (Ref. TASK 32-00-00-081802). (2) Close the NLG forward doors (Ref. TASK 32-22-00-410-801).
EFF : ALL 12-12-32 R SROS
Page 339 Jul 01/06
Subtask 12-12-32-942-058 B. Removal of the Ground Equipment (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 12-12-32 R SROS
Page 340 Jul 01/06
OIL - DESCRIPTION AND OPERATION _______________________________ 1. General _______ This section gives the instructions to fill the engine, the accessories (IDG, pneumatic starter) the APU, the flight control components. It includes the topics below: 12-13-24/P. 12-13-27/P. 12-13-49/P. 12-13-79/P. 12-13-80/P.
Block Block Block Block Block
301 301 301 301 301
ELECTRICAL POWER FLIGHT CONTROLS APU ENGINE OIL ENGINE STARTING
EFF : ALL 12-13-00 SROS
Page 1 Apr 01/98
ELECTRICAL POWER - SERVICING ____________________________ TASK 12-13-24-680-804 Draining of the Oil from the IDG WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE COMPONENTS IMMEDIATELY AFTER _______ THE ENGINE IS SHUTDOWN. THE ENGINE COMPONENTS CAN STAY HOT FOR UP TO ONE HOUR. WARNING : WEAR GOGGLES, INSULATED GLOVES AND OTHER PROTECTIVE CLOTHES. _______ HOT OIL CAN BURN YOUR EYES AND SKIN. IF OIL TOUCHES YOUR EYES OR SKIN, GET MEDICAL AID. CAUTION : DO NOT DO THE SERVICING OF A DISCONNECTED IDG. CONTINUED OPERATION OF _______ A DEFECTIVE IDG CAN CAUSE DAMAGE. CAUTION : DO NOT OPERATE THE IDG: _______ - IF IT CONTAINS TOO MUCH OIL - IF IT DOES NOT CONTAIN ENOUGH OIL IF YOU DO, YOU CAN CAUSE DAMAGE TO THE IDG. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No
specific specific specific specific
DH13PM
circuit breaker(s) safety clip(s) container 5.7 l (1.5 USgal) access platform 2.5 m (8 ft. 2 in.) Torque Wrench : range 36.00 to 220.00 lbf.in (0.40 to 2.60 m.daN) 1 TANK - ENGINE OIL FILLING UP
R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-24 Page 301 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
P03-001
Material No.
P05-289
* engine oil (Ref. 70-30-00) * lockwire 0.032 in. (0.80 mm) dia. (Ref. 70-30-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------3
O-ring
24-21-51 42A-060
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-13-24-610-801 12-32-24-281-803 24-21-00-612-810 24-42-00-861-801 24-42-00-862-801 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801 78-30-00-040-804 78-30-00-410-801 78-30-00-440-804 12-13-24-991-008
IDG Servicing - Filling of the IDG with Oil or Addition of Oil after a Level Check Sampling of the IDG Oil for Analysis Servicing of the IDG after Oil Chemical Contamination Energize the Ground Service Network De-energize the Ground Service Network Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Deactivation of the Thrust Reverser for Maintenance Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Reactivation of the Thrust Reverser after Maintenance Fig. 301
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3. __________ Job Set-up Subtask 12-13-24-861-053 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-24-941-059 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure. Subtask 12-13-24-010-062 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU. Subtask 12-13-24-865-056 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU GCU 1 4XU1 Q10 722VU FADEC B ENG 1 13KS1 D44 742VU IDG 1 DISC 1XT1 A76 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 721VU GCU 2 4XU2 N06 722VU FADEC B ENG 2 13KS2 K49 742VU IDG 2 DISC 1XT2 D69 742VU FADEC A ENG 2 12KS2 Q74
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Subtask 12-13-24-010-090 E. Get Access (1) Open the aft fan cowl doors (Ref. TASK 71-13-00-010-802): - FOR 4030EM1 415BL, 416BR, - FOR 4030EM2 425BL, 426BR. Subtask 12-13-24-040-062 F. Deactivation of the Thrust Reverser WARNING : YOU MUST DEACTIVATE THE THRUST REVERSER DIRECTIONAL CONTROL _______ VALVE (DCV) BEFORE YOU WORK ON OR AROUND THE TRANSLATING COWL. IF YOU DO NOT DEACTIVATE THE DCV, YOU CAN CAUSE ACCIDENTAL THRUST REVERSER OPERATION AND INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT. (1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 7830-00-040-804). Subtask 12-13-24-010-063 G. Get Access (1) Open the thrust reverser cowl doors (Ref. TASK 78-30-00-010-801): - FOR 4030EM1 417AL, 418AR, - FOR 4030EM2 427AL, 428AR. 4. Procedure _________ (Ref. Fig. 301/TASK 12-13-24-991-008) Subtask 12-13-24-864-059 A. Depressurization of the IDG Case WARNING : POINT THE OVERFLOW DRAIN HOSE INTO A CONTAINER WHEN YOU CONNECT _______ THE HOSE TO THE OVERFLOW DRAIN VALVE. THIS WILL PREVENT BURNS FROM THE HOT OIL SPRAY. HOT OIL CAN CAUSE BURNS TO EYES AND SKIN.
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IDG Servicing - Overflow Drain Valve and Case Drain of the IDG Figure 301/TASK 12-13-24-991-008 R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-24 Page 305 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
CAUTION : DO NOT USE DEVICES OTHER THAN THE APPROVED OVERFLOW DRAIN-HOSE _______ FITTING. HARD METAL OBJECTS SUCH AS SCREWDRIVERS CAN CAUSE DAMAGE TO THE OVERFLOW DRAIN-VALVE SEAT. (1) Put a container 5.7 l (1.5 USgal) below the IDG (1). (2) Remove the dust cap (7) from the overflow drain valve (6). (3) Put the end of the overflow drain hose (4) of the TANK - ENGINE OIL FILLING UP (DH13PM) in the container (5). (4) Do this step to depressurize the IDG case: (a) Connect the overflow drain hose (4) of the TANK - ENGINE OIL FILLING UP (DH13PM) to the overflow drain valve (6). NOTE : Some oil can come out of the overflow drain hose (4) of ____ the TANK - ENGINE OIL FILLING UP (DH13PM) when you connect it. Subtask 12-13-24-680-059 B. Draining of the Oil WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. _______ CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU. (1) Cut and remove the lockwire from the case drain plug (2). NOTE : Approximately 3.8 l (1 USgal) of oil will flow into the ____ container. (2) Remove the case drain plug (2). (3) Remove the O-ring (3) and discard it. (4) Drain the oil. NOTE : If the drained oil has a fuel odor, do the servicing of the ____ IDG after oil chemical contamination (Ref. TASK 24-21-00-612810). If you think that the condition of the drained oil is not correct, do a sampling of the IDG oil for analysis (Ref. TASK 12-32-24-281-803).
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Subtask 12-13-24-640-056 C. Lubricate the new O-ring (3) with engine oil (Material No. P03-001) Subtask 12-13-24-420-068 D. Installation of the Case Drain Plug (1) Install the new O-ring (3) on the case drain plug (2). (2) Install the case drain plug (2). (3) TORQUE the case drain plug (2) to between 55 and 75 lbf.in (0.62 and 0.84 m.daN). (4) Safety the case drain plug (2) with lockwire 0.032 in. (0.80 mm) dia. (Material No. P05-289). Subtask 12-13-24-420-069 E. Installation of the Dust Cap (1) Disconnect the overflow drain hose (4) of the TANK - ENGINE OIL FILLING UP (DH13PM) from the overflow drain valve (6). (2) Install the dust cap (7) on the overflow drain valve (6). Subtask 12-13-24-612-062 F. Fill the IDG with oil or add oil to the IDG after a level check (Ref. TASK 12-13-24-610-801), if you must not remove the IDG. 5. Close-up ________ Subtask 12-13-24-410-075 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the thrust reverser cowl doors (Ref. TASK 78-30-00-410-801): - FOR 4030EM1 417AL, 418AR, - FOR 4030EM2 427AL, 428AR.
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Subtask 12-13-24-440-062 B. Make the thrust reverser serviceable after maintenance (Ref. TASK 78-3000-440-804). Subtask 12-13-24-865-057 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1, 1XT1, 4XU1 - FOR 4030EM2 12KS2, 13KS2, 1XT2, 4XU2 Subtask 12-13-24-410-059 D. Close Access (1) Close the protective door of the AC/DC emergency power center 740VU. (2) Close the access door 811. (3) Remove the access platform(s). (4) Close the aft fan cowl doors (Ref. TASK 71-13-00-410-802): - FOR 4030EM1 415BL, 416BR, - FOR 4030EM2 425BL, 426BR. Subtask 12-13-24-862-053 E. De-energize the ground service network (Ref. TASK 24-42-00-862-801)
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TASK 12-13-24-610-801 IDG Servicing - Filling of the IDG with Oil or Addition of Oil after a Level Check WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE COMPONENTS IMMEDIATELY AFTER _______ THE ENGINE IS SHUTDOWN. THE ENGINE COMPONENTS CAN STAY HOT FOR UP TO ONE HOUR. WARNING : WEAR GOGGLES, INSULATED GLOVES AND OTHER PROTECTIVE CLOTHES. _______ HOT OIL CAN BURN YOUR EYES AND SKIN. IF OIL TOUCHES YOUR EYES OR SKIN, GET MEDICAL AID. CAUTION : DO NOT OPERATE THE IDG: _______ - IF IT CONTAINS TOO MUCH OIL - IF IT DOES NOT CONTAIN ENOUGH OIL IF YOU DO, YOU CAN CAUSE DAMAGE TO THE IDG. CAUTION : USE ONLY NEW CANS OF OIL WHEN YOU FILL THE IDG WITH OIL OR ADD OIL TO _______ THE IDG. THE CONTAMINATION IN OIL THAT STAYS IN OPEN CANS CAN CAUSE FAST DETERIORATION OF THE OIL AND WILL DECREASE THE LIFE OF THE IDG. CAUTION : DO NOT USE SOLVENTS THAT CONTAIN CHLORINE TO CLEAN THE EQUIPMENT _______ (PUMP, HOSES, TANK AND FUNNEL) USED TO FILL THE IDG WITH OIL. CHLORINE CONTAMINATION OF THE OIL CAN CAUSE FAST DETERIORATION OF THE OIL AND WILL DECREASE THE LIFE OF THE IDG. CAUTION : DO NOT DO THE SERVICING OF A DISCONNECTED IDG. CONTINUED OPERATION OF _______ A DEFECTIVE IDG CAN CAUSE DAMAGE. CAUTION : DO NOT LET ENGINE OIL FALL ON THE ENGINE. UNWANTED OIL MUST BE _______ REMOVED IMMEDIATELY. THE OIL CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job You must do this procedure if you: - fill an IDG installed on the aircraft after you drained it, - fill a replacement IDG installed on the aircraft, - add oil when the oil level at the sight-glass is not correct, - add oil after replacement of the scavenge filter element, - add oil after replacement of a component of the IDG oil cooling-system.
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2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific DH13PM
circuit breaker(s) safety clip(s) container 5.7 l (1.5 USgal) access platform 2.5 m (8 ft. 2 in.) 1 TANK - ENGINE OIL FILLING UP
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 03-002
GB DEF-STAN 91-101 LUBRICATING OIL TURBINE ENGINE SYNT BASE (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 71-00-00-720-816 71-00-00-860-818 71-13-00-010-802 71-13-00-410-802 78-30-00-040-804 78-30-00-440-804 12-13-24-991-009 12-13-24-991-019
Energize the Ground Service Network De-energize the Ground Service Network Test No. 2 - Engine Motor Leak Test (Dry Method) Thrust Reverser Cowl Doors Open Normal Engine Automatic Start Procedure Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Deactivation of the Thrust Reverser for Maintenance Reactivation of the Thrust Reverser after Maintenance Fig. 302 Fig. 303
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3. __________ Job Set-up Subtask 12-13-24-861-054 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-24-941-060 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure. Subtask 12-13-24-010-064 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU. Subtask 12-13-24-865-058 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU GCU 1 4XU1 Q10 722VU FADEC B ENG 1 13KS1 D44 742VU IDG 1 DISC 1XT1 A76 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 721VU GCU 2 4XU2 N06 722VU FADEC B ENG 2 13KS2 K49 742VU IDG 2 DISC 1XT2 D69 742VU FADEC A ENG 2 12KS2 Q74
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Subtask 12-13-24-010-086 E. Get Access (1) Open the aft fan cowl doors (Ref. TASK 71-13-00-010-802): - FOR 4030EM1 415BL, 416BR, - FOR 4030EM2 425BL, 426BR. Subtask 12-13-24-040-059 F. Deactivation of the Thrust Reverser WARNING : YOU MUST DEACTIVATE THE THRUST REVERSER DIRECTIONAL CONTROL _______ VALVE (DCV) BEFORE YOU WORK ON OR AROUND THE TRANSLATING COWL. IF YOU DO NOT DEACTIVATE THE DCV, YOU CAN CAUSE ACCIDENTAL THRUST REVERSER OPERATION AND INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT. (1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 7830-00-040-804). Subtask 12-13-24-010-065 G. Get Access (1) Open the lower left thrust reverser access door: - FOR 4030EM1 417EL, - FOR 4030EM2 427EL. 4. Procedure _________ (Ref. Fig. 302/TASK 12-13-24-991-009, 303/TASK 12-13-24-991-019) Subtask 12-13-24-864-060 A. Depressurization of the IDG Case WARNING : POINT THE OVERFLOW DRAIN HOSE INTO A CONTAINER WHEN YOU CONNECT _______ THE HOSE TO THE OVERFLOW DRAIN VALVE. THIS WILL PREVENT BURNS FROM THE HOT OIL SPRAY. HOT OIL CAN CAUSE BURNS TO EYES AND SKIN.
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IDG Servicing - Oil Level System of the IDG Figure 302/TASK 12-13-24-991-009 R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-24 Page 313 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
Correct Filling of the IDG Figure 303/TASK 12-13-24-991-019 R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-24 Page 314 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
CAUTION : DO NOT USE DEVICES OTHER THAN THE APPROVED OVERFLOW DRAIN-HOSE _______ FITTING. HARD METAL OBJECTS SUCH AS SCREWDRIVERS CAN CAUSE DAMAGE TO THE OVERFLOW DRAIN-VALVE SEAT. (1) Put a container 5.7 l (1.5 USgal) below the IDG (1). (2) Remove the dust cap (3) from the overflow drain valve (2). (3) Put the end of the overflow drain hose (4) of the TANK - ENGINE OIL FILLING UP (DH13PM) in the container (5). (4) Do this step to depressurize the IDG case: (a) Connect the overflow drain hose (4) of the TANK - ENGINE OIL FILLING UP (DH13PM) to the overflow drain valve (2). NOTE : Some oil can come out of the overflow drain hose (4) of ____ the TANK - ENGINE OIL FILLING UP (DH13PM) when you connect it. Subtask 12-13-24-612-063 B. Filling of the IDG with Oil CAUTION : USE ONLY APPROVED TYPES/BRANDS OF LUBRICANTS. _______ DO NOT MIX TYPES/BRANDS OF LUBRICANTS. NOTE : In rain, fog or wet conditions, be careful to prevent water ____ contamination of the IDG oil during the filling procedure. (1) Remove the dust cap (7) from the pressure fill valve (8). (2) Connect the pressure fill hose (6) of the TANK - ENGINE OIL FILLING UP (DH13PM) to the pressure fill valve (8). (3) Fill the IDG with filtered OILS (Material No. 03-002) at a maximum pressure of 35 psi (2.41 bar). NOTE : The AMM 20-34-00 gives a list of oil brand names approved for ____ the IDG. (4) Stop the filling procedure when the quantity of oil collected from the overflow drain hose (4) of the TANK - ENGINE OIL FILLING UP (DH13PM) is 0.95 l (0.25 USgal) minimum.
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Subtask 12-13-24-020-059 C. Removal of the Hoses (1) Disconnect the pressure fill hose (6) of the TANK - ENGINE OIL FILLING UP (DH13PM) from the pressure fill valve (8). (2) Install the dust cap (7) on the pressure fill valve (8). (3) When only drops of oil come out of the overflow drain hose (4) of the TANK - ENGINE OIL FILLING UP (DH13PM), remove the hose (4). (4) Install the dust cap (3) on the overflow drain valve (2). Subtask 12-13-24-720-056 D. If you replaced a part of the oil system (filter, external system component, drain plug), do a dry motoring for leak check before inspection (Ref. TASK 71-00-00-720-816). Subtask 12-13-24-210-051 E. Inspection of the Oil Level R R R
NOTE : After an IDG oil servicing, you must do a reset of the oil level ____ sensor. To do this, release then push the related GEN pushbutton switch. NOTE : Before you do a check of the oil level, we recommend that you do ____ dry motoring for two minutes (Ref. TASK 71-00-00-720-816). Alternatively you can do the check after an engine run, at minimum idle (Ref. TASK 71-00-00-860-818). This is to make sure you get maximum filling of the external oil system. (1) Inspection of the oil level with or without a dry motoring. CAUTION : IF YOU DRY-MOTOR THE ENGINE, MAKE SURE THAT THE OIL LEVEL _______ IS STABLE BEFORE YOU DO THE INSPECTION. IN AMBIENT AIR TEMPERATURES OF LESS THAN 20⁰C, THE OIL LEVEL WILL BECOME STABLE ONLY AFTER 30 MINUTES. THUS THE LEVEL INDICATIONS ON THE SIGHTGLASS WILL NOT BE CORRECT BEFORE THE END OF THIS PERIOD. IF YOU ADD OIL WHEN IT IS NOT NECESSARY, THERE IS A RISK THAT YOU WILL CAUSE FAILURE OF THE IDG. (a) Let the oil in the IDG become stable.
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(b) Look at the oil level sight-glass of the IDG: - if the oil level is at or near the top of the green band, oil servicing is not necessary, - if the oil level is below the green band or above the green band , do the steps 4.A. thru 4.D. again. (2) Inspection of the oil level after an engine run (alternative procedure). (a) Let the oil in the IDG become stable for 5 minutes. (b) Look at the oil level sight-glass of the IDG: - if the oil level is in the green or yellow band, oil servicing is not necessary, - if the oil level is below the green band or above the yellow band, do the steps 4.A. thru 4.D. again. 5. Close-up ________ Subtask 12-13-24-410-071 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the lower left thrust reverser access door: - FOR 4030EM1 417EL, - FOR 4030EM2 427EL. Subtask 12-13-24-440-059 B. Make the thrust reverser serviceable after maintenance (Ref. TASK 78-3000-440-804). Subtask 12-13-24-865-059 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1, 1XT1, 4XU1 - FOR 4030EM2 12KS2, 13KS2, 1XT2, 4XU2
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R R R
Subtask 12-13-24-860-050 D. Do a reset of the oil level sensor To do this, release then push the related GEN pushbutton switch. Subtask 12-13-24-410-060
R
E. Close Access (1) Close the protective door of the AC/DC emergency power center 740VU. (2) Close the access door 811. (3) Remove the access platform(s). (4) Close the aft fan cowl doors (Ref. TASK 71-13-00-410-802): - FOR 4030EM1 415BL, 416BR, - FOR 4030EM2 425BL, 426BR. Subtask 12-13-24-862-054
R
F. De-energize the ground service network (Ref. TASK 24-42-00-862-801)
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TASK 12-13-24-612-807 Drain IDG Oil System, Discard Filter Element and Replenish WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE COMPONENTS IMMEDIATELY AFTER _______ THE ENGINE IS SHUTDOWN. THE ENGINE COMPONENTS CAN STAY HOT FOR UP TO ONE HOUR. WARNING : WEAR GOGGLES, INSULATED GLOVES AND OTHER PROTECTIVE CLOTHES. _______ HOT OIL CAN BURN YOUR EYES AND SKIN. IF OIL TOUCHES YOUR EYES OR SKIN, GET MEDICAL AID. CAUTION : USE ONLY NEW CANS OF OIL WHEN YOU FILL THE IDG WITH OIL OR ADD OIL TO _______ THE IDG. THE CONTAMINATION IN OIL THAT STAYS IN OPEN CANS CAN CAUSE FAST DETERIORATION OF THE OIL AND WILL DECREASE THE LIFE OF THE IDG. CAUTION : DO NOT USE SOLVENTS THAT CONTAIN CHLORINE TO CLEAN THE EQUIPMENT _______ (PUMP, HOSES, TANK AND FUNNEL) USED TO FILL THE IDG WITH OIL. CHLORINE CONTAMINATION OF THE OIL CAN CAUSE FAST DETERIORATION OF THE OIL AND WILL DECREASE THE LIFE OF THE IDG. CAUTION : DO NOT OPERATE THE IDG: _______ - IF IT CONTAINS TOO MUCH OIL - IF IT DOES NOT CONTAIN ENOUGH OIL IF YOU DO, YOU CAN CAUSE DAMAGE TO THE IDG. CAUTION : DO NOT DO THE SERVICING OF A DISCONNECTED IDG. CONTINUED OPERATION OF _______ A DEFECTIVE IDG CAN CAUSE DAMAGE. 1. __________________ Reason for the Job Refer to the MPD TASK: 242100-13 To drain the IDG, replace the IDG oil filter element and fill the IDG with oil.
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2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No
specific specific specific specific specific
blanking plug circuit breaker(s) safety clip(s) container 5.7 l (1.5 USgal) access platform 2.5 m (8 ft. 2 in.) Torque Wrench : range 2.00 to 26.00 lbf.ft (0.20 to 3.60 m.daN) Torque Wrench : range 36.00 to 220.00 lbf.in (0.40 to 2.60 m.daN) 1 TANK - ENGINE OIL FILLING UP
No specific DH13PM
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
P05-289
Material No. 03-002
* lockwire 0.032 in. (0.80 mm) dia (Ref. 70-30-00) GB DEF-STAN 91-101 LUBRICATING OIL TURBINE ENGINE SYNT BASE (Ref. 20-31-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------2 3 3 4
O-ring O-ring filter element O-ring
24-21-51 24-21-51 24-21-51 24-21-51
42A-220 42A-060 42A-230 42A-240
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D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-13-24-610-801 12-32-24-281-803 24-21-00-210-814 24-21-00-612-810 24-42-00-861-801 24-42-00-862-801 71-00-00-720-816 71-00-00-860-818 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801 78-30-00-040-804 78-30-00-410-801 78-30-00-440-804 12-13-24-991-011 12-13-24-991-022
IDG Servicing - Filling of the IDG with Oil or Addition of Oil after a Level Check Sampling of the IDG Oil for Analysis Inspection of the Filter Element Servicing of the IDG after Oil Chemical Contamination Energize the Ground Service Network De-energize the Ground Service Network Test No. 2 - Engine Motor Leak Test (Dry Method) Thrust Reverser Cowl Doors Open Normal Engine Automatic Start Procedure Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Deactivation of the Thrust Reverser for Maintenance Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Reactivation of the Thrust Reverser after Maintenance Fig. 304 Fig. 305
3. __________ Job Set-up Subtask 12-13-24-861-058 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-24-941-061 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure.
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Subtask 12-13-24-010-069 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU. Subtask 12-13-24-865-066 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU GCU 1 4XU1 Q10 722VU FADEC B ENG 1 13KS1 D44 742VU IDG 1 DISC 1XT1 A76 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 721VU GCU 2 4XU2 N06 722VU FADEC B ENG 2 13KS2 K49 742VU IDG 2 DISC 1XT2 D69 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-13-24-010-081 E. Get Access (1) Open the aft fan cowl doors (Ref. TASK 71-13-00-010-802): - FOR 4030EM1 415BL, 416BR, - FOR 4030EM2 425BL, 426BR. Subtask 12-13-24-040-057 F. Deactivation of the Thrust Reverser WARNING : YOU MUST DEACTIVATE THE THRUST REVERSER DIRECTIONAL CONTROL _______ VALVE (DCV) BEFORE YOU WORK ON OR AROUND THE TRANSLATING COWL. IF YOU DO NOT DEACTIVATE THE DCV, YOU CAN CAUSE ACCIDENTAL THRUST REVERSER OPERATION AND INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.
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(1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 7830-00-040-804). Subtask 12-13-24-010-070 G. Get Access (1) Open the thrust reverser cowl doors (Ref. TASK 78-30-00-010-801): - FOR 4030EM1 417AL, 418AR, - FOR 4030EM2 427AL, 428AR. 4. Procedure _________ (Ref. Fig. 304/TASK 12-13-24-991-011, 305/TASK 12-13-24-991-022) Subtask 12-13-24-864-061 A. Depressurization of the IDG Case (Ref. Fig. 304/TASK 12-13-24-991-011) WARNING : POINT THE OVERFLOW DRAIN HOSE INTO A CONTAINER WHEN YOU CONNECT _______ THE HOSE TO THE OVERFLOW DRAIN VALVE. THIS WILL PREVENT BURNS FROM THE HOT OIL SPRAY. HOT OIL CAN CAUSE BURNS TO EYES AND SKIN. CAUTION : DO NOT USE DEVICES OTHER THAN THE APPROVED OVERFLOW DRAIN-HOSE _______ FITTING. HARD METAL OBJECTS SUCH AS SCREWDRIVERS CAN CAUSE DAMAGE TO THE OVERFLOW DRAIN-VALVE SEAT. (1) Put a container 5.7 l (1.5 USgal) below the IDG (1). (2) Remove the dust cap (5) from the overflow drain valve (4). (3) Put the end of the overflow drain hose (6) of the TANK - ENGINE OIL FILLING UP (DH13PM) in the container (7). (4) Do this step to depressurize the IDG case: (a) Connect the overflow drain hose (6) of the TANK - ENGINE OIL FILLING UP (DH13PM) to the overflow drain valve (4). NOTE : Some oil may come out of the overflow drain hose (6) of ____ the TANK - ENGINE OIL FILLING UP (DH13PM) when you connect it.
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Draining and Filling of the IDG Figure 304/TASK 12-13-24-991-011 R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-24 Page 324 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
IDG Oil Filter Figure 305/TASK 12-13-24-991-022 R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-24 Page 325 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
Subtask 12-13-24-680-060 B. Draining of the Oil (Ref. Fig. 304/TASK 12-13-24-991-011) WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. _______ CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU. (1) Cut and remove the lockwire from the case drain plug (2). NOTE : Be prepared to catch approximately 3.8 l (1 USgal) of oil in ____ the container. (2) Remove the case drain plug (2). (3) Remove the O-ring (3) and discard it. (4) Drain the oil. NOTE : If the drained oil has a fuel odor, do the servicing of the ____ IDG after oil chemical contamination (Ref. TASK 24-21-00-612810). If you think that the condition of the drained oil is not correct, do a sampling of the IDG oil for analysis (Ref. TASK 12-32-24-281-803). Subtask 12-13-24-020-067 C. Removal of the IDG Oil Filter (Ref. Fig. 305/TASK 12-13-24-991-022) WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. _______ CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU. (1) Cut and remove the lockwire from the filter cover (1). NOTE : Put a container 5.7 l (1.5 USgal) below the filter cavity. ____ (2) Loosen and remove the filter cover (1). (3) Remove and discard the O-ring (2) from the filter cover (1). (4) Remove the filter element (3). (5) Remove and discard the O-ring (4) from the filter element (3).
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(6) Install a blanking plug on the filter cavity port. Subtask 12-13-24-210-064 D. Inspection of the IDG Oil Filter (1) Do the inspection of the filter element (Ref. TASK 24-21-00-210-814). NOTE : We recommend you do a visual inspection of the IDG oil filter ____ for possible contamination, debris. Subtask 12-13-24-640-057 E. Lubrication of the Expendable Parts (1) Lubricate the new O-ring (3) with OILS (Material No. 03-002). (2) Lubricate the new O-ring (4) with OILS (Material No. 03-002). (3) Lubricate the new O-ring (2) with OILS (Material No. 03-002). Subtask 12-13-24-420-071 F. Installation of the Case Drain Plug (Ref. Fig. 304/TASK 12-13-24-991-011) WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. _______ CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU. (1) Install the new O-ring (3) on the case drain plug (2). (2) Install the case drain plug (2). (3) TORQUE the case drain plug (2) to between 55 and 75 lbf.in (0.62 and 0.84 m.daN). (4) Safety the case drain plug (2) with lockwire 0.032 in. (0.80 mm) dia (Material No. P05-289).
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Subtask 12-13-24-420-081 G. Installation of the IDG Oil Filter (Ref. Fig. 305/TASK 12-13-24-991-022) WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. _______ CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU. CAUTION : MAKE SURE THE COMPONENTS ARE SEATED IN THE IDG SCAVENGE FILTER _______ CAVITY BEFORE YOU INSTALL THE FILTER COVER. DO NOT TIGHTEN THE FILTER COVER SCREWS TO FORCE THE FILTER COMPONENTS INTO THE HOUSING. (1) Install the new O-ring (4) on the filter element (3). (2) Install the new O-ring (2) on the filter cover (1). (3) Put the filter element (3) in the filter cavity. (4) Install the filter cover (1). (5) TORQUE the filter cover (1) to between 13 and 15 lbf.ft (1.76 and 2.03 m.daN). (6) Safety the filter cover (1) with lockwire 0.032 in. (0.80 mm) dia (Material No. P05-289). Subtask 12-13-24-612-066 H. Filling of the IDG with Oil (Ref. Fig. 304/TASK 12-13-24-991-011) CAUTION : USE ONLY APPROVED TYPES/BRANDS OF LUBRICANTS. _______ DO NOT MIX TYPES/BRANDS OF LUBRICANTS. NOTE : In rain, fog or wet conditions, be careful to prevent water ____ contamination of the IDG oil during the filling procedure. (1) Remove the dust cap (9) from the pressure fill valve (10). (2) Connect the pressure fill hose (8) of the TANK - ENGINE OIL FILLING UP (DH13PM) to the pressure fill valve (10).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-24 Page 328 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
(3) Fill the IDG with the filtered OILS (Material No. 03-002) at a maximum pressure of 35 psi (2.41 bar). NOTE : The AMM 20-34-00 gives a list of oil brand names approved for ____ IDG. (4) Stop the filling procedure when the quantity of oil collected from the overflow drain hose (6) of the TANK - ENGINE OIL FILLING UP (DH13PM) is 0.95 l (0.25 USgal) minimum. Subtask 12-13-24-020-061 J. Removal of the Hoses (Ref. Fig. 304/TASK 12-13-24-991-011) (1) Disconnect the pressure fill hose (8) of the TANK - ENGINE OIL FILLING UP (DH13PM) from the pressure fill valve (10). (2) Install the dust cap (9) on the pressure fill valve (10). (3) When only drops of oil come out of the overflow drain hose (6) of the TANK - ENGINE OIL FILLING UP (DH13PM), disconnect the hose (6). (4) Install the dust cap (5) on the overflow drain valve (4). Subtask 12-13-24-720-052 K. If you replaced a part of the oil system (filter, external system component, drain plug), do a dry motoring for leak check before inspection (Ref. TASK 71-00-00-720-816). Subtask 12-13-24-210-057 L. Inspection of the Oil Level (Ref. Fig. 304/TASK 12-13-24-991-011) NOTE : Before you do a check of the oil level, we recommend that you do ____ dry motoring for two minutes (Ref. TASK 71-00-00-720-816). Alternatively, you can do the check after an engine start at minimum idle (Ref. TASK 71-00-00-860-818). This is to make sure you get maximum filling of the external oil system.
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(1) Inspection of the oil level after dry motoring. CAUTION : IF YOU DRY-MOTOR THE ENGINE, MAKE SURE THAT THE OIL LEVEL _______ IS STABLE BEFORE YOU DO THE INSPECTION. IN AMBIENT AIR TEMPERATURES OF LESS THAN 20⁰C, THE OIL LEVEL WILL BECOME STABLE ONLY AFTER 30 MINUTES. THUS THE LEVEL INDICATIONS ON THE SIGHTGLASS WILL NOT BE CORRECT BEFORE THE END OF THIS PERIOD. IF YOU ADD OIL WHEN IT IS NOT NECESSARY, THERE IS A RISK THAT YOU WILL CAUSE FAILURE OF THE IDG. (a) Let the oil in the IDG become stable. (b) Look at the oil level sight-glass of the IDG: - if the oil level is at or near the top of the green band, oil servicing is not necessary, - if the oil level is below the green band or above the green band , do the filling of the IDG with oil or addition of oil after level check (Ref. TASK 12-13-24-610-801). (2) Inspection of the oil level after an engine start (alternative procedure). (a) Let the oil in the IDG become stable for 5 minutes. (b) Look at the oil level sight-glass of the IDG: - if the oil level is in the green or yellow band, oil servicing is not necessary, - if the oil level is below the green band or above the yellow band, do the filling of the IDG with oil or addition of oil after level check (Ref. TASK 12-13-24-610-801). 5. Close-up ________ Subtask 12-13-24-410-067 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the thrust reverser cowl doors (Ref. TASK 78-30-00-410-801): - FOR 4030EM1 417AL, 418AR, - FOR 4030EM2 427AL, 428AR.
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Subtask 12-13-24-440-057 B. Make the thrust reverser serviceable after maintenance (Ref. TASK 78-3000-440-804). Subtask 12-13-24-865-067 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1, 1XT1, 4XU1 - FOR 4030EM2 12KS2, 13KS2, 1XT2, 4XU2 Subtask 12-13-24-410-061 D. Close Access (1) Close the protective door of the AC/DC emergency power center 740VU. (2) Close the access door 811. (3) Remove the access platform(s). (4) Close the aft fan cowl doors (Ref. TASK 71-13-00-410-802): - FOR 4030EM1 415BL, 416BR, - FOR 4030EM2 425BL, 426BR. Subtask 12-13-24-862-058 E. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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ELECTRICAL POWER - SERVICING ____________________________ TASK 12-13-24-680-805 R
Draining of the Oil from the IDG WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE COMPONENTS IMMEDIATELY AFTER _______ THE ENGINE IS SHUTDOWN. THE ENGINE COMPONENTS CAN STAY HOT FOR UP TO ONE HOUR. WARNING : WEAR GOGGLES, INSULATED GLOVES AND OTHER PROTECTIVE CLOTHES. _______ HOT OIL CAN BURN YOUR EYES AND SKIN. IF OIL TOUCHES YOUR EYES OR SKIN, GET MEDICAL AID. CAUTION : DO NOT DO THE SERVICING OF A DISCONNECTED IDG. CONTINUED OPERATION OF _______ A DEFECTIVE IDG CAN CAUSE DAMAGE. CAUTION : DO NOT OPERATE THE IDG: _______ - IF IT CONTAINS TOO MUCH OIL - IF IT DOES NOT CONTAIN ENOUGH OIL IF YOU DO, YOU CAN CAUSE DAMAGE TO THE IDG. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No
specific specific specific specific
DH13PM
circuit breaker(s) safety clip(s) container 5.7 l (1.5 USgal) access platform 2.5 m (8 ft. 2 in.) Torque Wrench : range 36.00 to 220.00 lbf.in (0.40 to 2.60 m.daN) 1 TANK - ENGINE OIL FILLING UP
EFF : 701-749, 12-13-24 Page 301 Config-2 Jan 01/02 SROS
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
OMat 1011
Material No.
OMAT 238
* engine oil (Ref. 70-30-00) * lockwire 0.028 to 0.031 in. (0.71 to 0.79 mm) dia. (Ref. 70-30-00)
R R
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-13-24-612-808 12-32-24-281-804 24-21-00-612-814 24-42-00-861-801 24-42-00-862-801 71-13-00-010-805 71-13-00-410-805 78-31-00-040-805 78-31-00-440-805 12-13-24-991-012
IDG Servicing - Filling of the IDG with Addition of Oil after Level Check Sampling of the IDG Oil for Analysis Servicing of the IDG after Oil Chemical Energize the Ground Service Network De-energize the Ground Service Network Open the Fan Cowl Doors Close the Fan Cowl Doors Deactivation of the Thrust Reverser for Activation of the Thrust Reverser after Fig. 301
Oil or Contamination
Maintenance Maintenance
3. __________ Job Set-up Subtask 12-13-24-861-059 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-24-941-062 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure.
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Subtask 12-13-24-010-071 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU. Subtask 12-13-24-865-068 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU GCU 1 4XU1 Q10 722VU FADEC B ENG 1 13KS1 D44 742VU IDG 1 DISC 1XT1 A76 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 721VU GCU 2 4XU2 N06 722VU FADEC B ENG 2 13KS2 K49 742VU IDG 2 DISC 1XT2 D69 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-13-24-010-072 E. Get Access (1) Open the fan cowl doors (Ref. TASK 71-13-00-010-805): - FOR 4030EM1 415AL, 416AR, - FOR 4030EM2 425AL, 426AR. Subtask 12-13-24-040-063 F. Deactivation of the Thrust Reverser WARNING : YOU MUST DEACTIVATE THE THRUST REVERSER BEFORE YOU DO WORK ON _______ OR AROUND IT. IF YOU DO NOT, THE THRUST REVERSER CAN OPERATE ACCIDENTALLY AND CAUSE INJURY AND/OR DAMAGE.
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(1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 7831-00-040-805). 4. Procedure _________ (Ref. Fig. 301/TASK 12-13-24-991-012) Subtask 12-13-24-864-062 A. Depressurization of the IDG Case WARNING : POINT THE OVERFLOW DRAIN HOSE INTO A CONTAINER WHEN YOU CONNECT _______ THE HOSE TO THE OVERFLOW DRAIN VALVE. THIS WILL PREVENT BURNS FROM THE HOT OIL SPRAY. HOT OIL CAN CAUSE BURNS TO EYES AND SKIN. CAUTION : DO NOT USE DEVICES OTHER THAN THE APPROVED OVERFLOW DRAIN-HOSE _______ FITTING. HARD METAL OBJECTS SUCH AS SCREWDRIVERS CAN CAUSE DAMAGE TO THE OVERFLOW DRAIN-VALVE SEAT. (1) Put a container 5.7 l (1.5 USgal) below the IDG (1). (2) Remove the dust cap (3) from the overflow drain valve (2). (3) Put the end of the overflow drain hose (4) of the TANK - ENGINE OIL FILLING UP (DH13PM) in the container (5). (4) Do this step to depressurize the IDG case: (a) Connect the overflow drain hose (4) of the TANK - ENGINE OIL FILLING UP (DH13PM) to the overflow drain valve (2). NOTE : Some oil can come out of the overflow drain hose (4) of ____ the TANK - ENGINE OIL FILLING UP (DH13PM) when you connect it. Subtask 12-13-24-680-061 B. Draining of the Oil WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. _______ CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU.
EFF : 701-749, 12-13-24 Page 304 Config-2 Jan 01/06 R SROS
IDG Servicing - Overflow Drain Valve and Case Drain of the IDG Figure 301/TASK 12-13-24-991-012 EFF : 701-749, 12-13-24 Page 305 Config-2 Oct 01/00 SROS
(1) Cut and remove the lockwire from the case drain plug (7). NOTE : Approximately 3.8 l (1 USgal) of oil will flow into the ____ container. (2) Remove the case drain plug (7). (3) Remove the O-ring (6) and discard it. (4) Drain the oil. NOTE : If the drained oil has a fuel odor, do the servicing of the ____ IDG after oil chemical contamination (Ref. TASK 24-21-00-612814). If you think that the condition of the drained oil is not correct, do a sampling of the IDG oil for analysis (Ref. TASK 12-32-24-281-804). Subtask 12-13-24-640-058 C. Lubricate the new O-ring (6) with engine oil (Material No. OMat 1011). Subtask 12-13-24-420-074 D. Installation of the Case Drain Plug (1) Install the new O-ring (6) on the case drain plug (7). (2) Install the case drain plug (7). (3) TORQUE the case drain plug (7) to between 55 and 75 lbf.in (0.62 and 0.84 m.daN). (4) Safety the case drain plug (7) with lockwire 0.028 to 0.031 in. (0.71 to 0.79 mm) dia. (Material No. OMAT 238). Subtask 12-13-24-420-075 E. Installation of the Dust Cap (1) Disconnect the overflow drain hose (4) of the TANK - ENGINE OIL FILLING UP (DH13PM) from the overflow drain valve (2). (2) Install the dust cap (3) on the overflow drain valve (2).
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Subtask 12-13-24-612-067 F. Fill the IDG with oil or add oil to the IDG after a level check (Ref. TASK 12-13-24-612-808), if you must not remove the IDG. 5. Close-up ________ Subtask 12-13-24-440-063 A. Make the thrust reverser serviceable after maintenance (Ref. TASK 78-3100-440-805). Subtask 12-13-24-865-069 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1, 1XT1, 4XU1 - FOR 4030EM2 12KS2, 13KS2, 1XT2, 4XU2 Subtask 12-13-24-410-062 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Close the access door 811. (4) Remove the access platform(s). (5) Close the fan cowl doors (Ref. TASK 71-13-00-410-805): - FOR 4030EM1 415AL, 416AR, - FOR 4030EM2 425AL, 426AR. Subtask 12-13-24-862-059 D. De-energize the ground service network (Ref. TASK 24-42-00-862-801)
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INTENTIONALLY BLANK
R 12-13-24 Page 308 Config-2 Jan 01/06 SROS
TASK 12-13-24-612-808 R R
IDG Servicing - Filling of the IDG with Oil or Addition of Oil after Level Check WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE COMPONENTS IMMEDIATELY AFTER _______ THE ENGINE IS SHUTDOWN. THE ENGINE COMPONENTS CAN STAY HOT FOR UP TO ONE HOUR. WARNING : WEAR GOGGLES, INSULATED GLOVES AND OTHER PROTECTIVE CLOTHES. _______ HOT OIL CAN BURN YOUR EYES AND SKIN. IF OIL TOUCHES YOUR EYES OR SKIN, GET MEDICAL AID. CAUTION : DO NOT OPERATE THE IDG: _______ - IF IT CONTAINS TOO MUCH OIL - IF IT DOES NOT CONTAIN ENOUGH OIL IF YOU DO, YOU CAN CAUSE DAMAGE TO THE IDG. CAUTION : USE ONLY NEW CANS OF OIL WHEN YOU FILL THE IDG WITH OIL OR ADD OIL TO _______ THE IDG. THE CONTAMINATION IN OIL THAT STAYS IN OPEN CANS CAN CAUSE FAST DETERIORATION OF THE OIL AND WILL DECREASE THE LIFE OF THE IDG. CAUTION : DO NOT USE SOLVENTS THAT CONTAIN CHLORINE TO CLEAN THE EQUIPMENT _______ (PUMP, HOSES, TANK AND FUNNEL) USED TO FILL THE IDG WITH OIL. CHLORINE CONTAMINATION OF THE OIL CAN CAUSE FAST DETERIORATION OF THE OIL AND WILL DECREASE THE LIFE OF THE IDG. CAUTION : DO NOT DO THE SERVICING OF A DISCONNECTED IDG. CONTINUED OPERATION OF _______ A DEFECTIVE IDG CAN CAUSE DAMAGE. 1. __________________ Reason for the Job You must do this procedure if you: - fill an IDG installed on the aircraft after you drained it, - fill a replacement IDG installed on the aircraft, - add oil when the oil level at the sight-glass is not correct, - add oil after replacement of the scavenge filter element, - add oil after replacement of a component of the IDG oil cooling-system.
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2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific DH13PM
circuit breaker(s) safety clip(s) container 5.7 l (1.5 USgal) access platform 2.5 m (8 ft. 2 in.) 1 TANK - ENGINE OIL FILLING UP
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 03-002
GB DEF-STAN 91-101 LUBRICATING OIL TURBINE ENGINE SYNT BASE (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 71-00-00-720-828 71-00-00-860-810 71-13-00-010-805 71-13-00-410-805 78-31-00-040-805 78-31-00-440-805 12-13-24-991-013 12-13-24-991-020
Energize the Ground Service Network De-energize the Ground Service Network Dry Motoring Engine Engine Automatic Start Open the Fan Cowl Doors Close the Fan Cowl Doors Deactivation of the Thrust Reverser for Maintenance Activation of the Thrust Reverser after Maintenance Fig. 302 Fig. 303
3. __________ Job Set-up Subtask 12-13-24-861-060 A. Energize the ground service network (Ref. TASK 24-42-00-861-801).
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Subtask 12-13-24-941-063 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure. Subtask 12-13-24-010-073 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU. Subtask 12-13-24-865-070 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU GCU 1 4XU1 Q10 722VU FADEC B ENG 1 13KS1 D44 742VU IDG 1 DISC 1XT1 A76 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 721VU GCU 2 4XU2 N06 722VU FADEC B ENG 2 13KS2 K49 742VU IDG 2 DISC 1XT2 D69 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-13-24-010-074 E. Get Access (1) Open the fan cowl doors (Ref. TASK 71-13-00-010-805): - FOR 4030EM1 415AL, 416AR, - FOR 4030EM2 425AL, 426AR.
EFF : 701-749, 12-13-24 Page 311 Config-2 Jan 01/02 R SROS
Subtask 12-13-24-040-060 F. Deactivation of the Thrust Reverser WARNING : YOU MUST DEACTIVATE THE THRUST REVERSER BEFORE YOU DO WORK ON _______ OR AROUND IT. IF YOU DO NOT, THE THRUST REVERSER CAN OPERATE ACCIDENTALLY AND CAUSE INJURY AND/OR DAMAGE. (1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 7831-00-040-805). 4. Procedure _________ (Ref. Fig. 302/TASK 12-13-24-991-013, 303/TASK 12-13-24-991-020) Subtask 12-13-24-864-063 A. Depressurization of the IDG Case WARNING : POINT THE OVERFLOW DRAIN HOSE INTO A CONTAINER WHEN YOU CONNECT _______ THE HOSE TO THE OVERFLOW DRAIN VALVE. THIS WILL PREVENT BURNS FROM THE HOT OIL SPRAY. HOT OIL CAN CAUSE BURNS TO EYES AND SKIN. CAUTION : DO NOT USE DEVICES OTHER THAN THE APPROVED OVERFLOW DRAIN-HOSE _______ FITTING. HARD METAL OBJECTS SUCH AS SCREWDRIVERS CAN CAUSE DAMAGE TO THE OVERFLOW DRAIN-VALVE SEAT. (1) Put a container 5.7 l (1.5 USgal) below the IDG (1). (2) Remove the dust cap (3) from the overflow drain valve (2). (3) Put the end of the overflow drain hose (5) of the TANK - ENGINE OIL FILLING UP (DH13PM) in the container (6). (4) Do this step to depressurize the IDG case: (a) Connect the overflow drain hose (5) of the TANK - ENGINE OIL FILLING UP (DH13PM) to the overflow drain valve (2). NOTE : Some oil can come out of the overflow drain hose (5) of ____ the TANK - ENGINE OIL FILLING UP (DH13PM) when you connect it.
EFF : 701-749, 12-13-24 Page 312 Config-2 Jan 01/02 R SROS
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IDG Servicing - IDG Drain and Fill Ports Figure 302/TASK 12-13-24-991-013
EFF : 701-749, 12-13-24 Page 313 Config-2 Jan 01/02 SROS
Correct Filling of the IDG Figure 303/TASK 12-13-24-991-020 EFF : 701-749, 12-13-24 Page 314 Config-2 Jan 01/02 R SROS
Subtask 12-13-24-612-068 B. Filling of the IDG with Oil CAUTION : USE ONLY APPROVED TYPES/BRANDS OF LUBRICANTS. _______ DO NOT MIX TYPES/BRANDS OF LUBRICANTS. NOTE : In rain, fog or wet conditions, be careful to prevent water ____ contamination of the IDG oil during the filling procedure. (1) Remove the dust cap (4) from the pressure fill valve (8). (2) Connect the pressure fill hose (7) of the TANK - ENGINE OIL FILLING UP (DH13PM) to the pressure fill valve (8). (3) Fill the IDG with filtered OILS (Material No. 03-002) at a maximum pressure of 35 psi (2.41 bar). NOTE : The AMM 20-34-00 gives a list of oil brand names approved for ____ the IDG. (4) Stop the filling procedure when the quantity of oil collected from the overflow drain hose (5) of the TANK - ENGINE OIL FILLING UP (DH13PM) is 0.95 l (0.25 USgal) minimum. Subtask 12-13-24-020-062 C. Removal of the Hoses (1) Disconnect the pressure fill hose (7) of the TANK - ENGINE OIL FILLING UP (DH13PM) from the pressure fill valve (8). (2) Install the dust cap (4) on the pressure fill valve (8). (3) When only drops of oil come out of the overflow drain hose (5) of the TANK - ENGINE OIL FILLING UP (DH13PM), remove the hose (5). (4) Install the dust cap (3) on the overflow drain valve (2). Subtask 12-13-24-720-057 D. If you replaced a part of the oil system (filter, external system component, drain plug), do dry motoring for leak check before inspection (Ref. TASK 71-00-00-720-828). Subtask 12-13-24-210-053 E. Inspection of the Oil Level R R R
NOTE : After an IDG oil servicing, you must do a reset of the oil level ____ sensor. To do this, release then push the related GEN pushbutton switch.
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NOTE : Before you do a check of the oil level, we recommend that you do ____ dry motoring for two minutes (Ref. TASK 71-00-00-720-828). Alternatively, you can do the check after an engine run at minimum idle (Ref. TASK 71-00-00-860-810). This is to make sure that you get maximum filling of the external oil system. (1) Inspection of the oil level with or without dry motoring. CAUTION : IF YOU DRY-MOTOR THE ENGINE, MAKE SURE THAT THE OIL LEVEL _______ IS STABLE BEFORE YOU DO THE INSPECTION. IN AMBIENT AIR TEMPERATURES OF LESS THAN 20⁰C, THE OIL LEVEL WILL BECOME STABLE ONLY AFTER 30 MINUTES. THUS THE LEVEL INDICATIONS ON THE SIGHTGLASS WILL NOT BE CORRECT BEFORE THE END OF THIS PERIOD. IF YOU ADD OIL WHEN IT IS NOT NECESSARY, THERE IS A RISK THAT YOU WILL CAUSE FAILURE OF THE IDG. (a) Let the oil in the IDG become stable. (b) Look at the oil level sight-glass of the IDG: - if the oil level is at or near the top of the green band, oil servicing is not necessary, - if the oil level is below the green band or above the green band , do the steps 4.A. thru 4.D. again. (2) Inspection of the oil level after an engine run (alternative procedure). (a) Let the oil in the IDG become stable for 5 minutes. (b) Look at the oil level sight-glass of the IDG: - if the oil level is in the green or yellow band, oil servicing is not necessary, - if the oil level is below the green band or above the yellow band, do the steps 4.A. thru 4.D. again. 5. Close-up ________ Subtask 12-13-24-440-060 A. Make the thrust reverser serviceable after maintenance (Ref. TASK 78-3100-440-805).
EFF : 701-749, 12-13-24 Page 316 Config-2 Jul 01/05 R SROS
Subtask 12-13-24-865-071 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1, 1XT1, 4XU1 - FOR 4030EM2 12KS2, 13KS2, 1XT2, 4XU2 R R R
Subtask 12-13-24-860-053 C. Do a reset of the oil level sensor To do this, release then push the related GEN pushbutton switch. Subtask 12-13-24-410-063
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D. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Close the access door 811. (4) Remove the access platform(s). (5) Close the fan cowl doors (Ref. TASK 71-13-00-410-805): - FOR 4030EM1 415AL, 416AR, - FOR 4030EM2 425AL, 426AR. Subtask 12-13-24-862-060
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E. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : 701-749, 12-13-24 Page 317 Config-2 Jan 01/06 SROS
TASK 12-13-24-612-809 R
Drain IDG Oil System, Discard Filter Element and Replenish WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE COMPONENTS IMMEDIATELY AFTER _______ THE ENGINE IS SHUTDOWN. THE ENGINE COMPONENTS CAN STAY HOT FOR UP TO ONE HOUR. WARNING : WEAR GOGGLES, INSULATED GLOVES AND OTHER PROTECTIVE CLOTHES. _______ HOT OIL CAN BURN YOUR EYES AND SKIN. IF OIL TOUCHES YOUR EYES OR SKIN, GET MEDICAL AID. CAUTION : USE ONLY NEW CANS OF OIL WHEN YOU FILL THE IDG WITH OIL OR ADD OIL TO _______ THE IDG. THE CONTAMINATION IN OIL THAT STAYS IN OPEN CANS CAN CAUSE FAST DETERIORATION OF THE OIL AND WILL DECREASE THE LIFE OF THE IDG. CAUTION : DO NOT USE SOLVENTS THAT CONTAIN CHLORINE TO CLEAN THE EQUIPMENT _______ (PUMP, HOSES, TANK AND FUNNEL) USED TO FILL THE IDG WITH OIL. CHLORINE CONTAMINATION OF THE OIL CAN CAUSE FAST DETERIORATION OF THE OIL AND WILL DECREASE THE LIFE OF THE IDG. CAUTION : DO NOT OPERATE THE IDG: _______ - IF IT CONTAINS TOO MUCH OIL - IF IT DOES NOT CONTAIN ENOUGH OIL IF YOU DO, YOU CAN CAUSE DAMAGE TO THE IDG. CAUTION : DO NOT DO THE SERVICING OF A DISCONNECTED IDG. CONTINUED OPERATION OF _______ A DEFECTIVE IDG CAN CAUSE DAMAGE. 1. __________________ Reason for the Job Refer to the MPD TASK: 242100-18 To drain the IDG, replace the IDG oil filter element and fill the IDG with oil.
EFF : 701-749, 12-13-24 Page 318 Config-2 Apr 01/04 SROS
2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No
specific specific specific specific specific
blanking plug circuit breaker(s) safety clip(s) container 5.7 l (1.5 USgal) access platform 2.5 m (8 ft. 2 in.) Torque Wrench : range 2.00 to 26.00 lbf.ft (0.20 to 3.60 m.daN) Torque Wrench : range 36.00 to 220.00 lbf.in (0.40 to 2.60 m.daN) 1 TANK - ENGINE OIL FILLING UP
No specific DH13PM
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
OMAT 1011
Material No.
OMAT 238
Material No. 03-002
* engine lubricating oil (Ref. 70-30-00) * lockwire 0.028 to 0.031 in.(0.71 to 0.79 mm) dia. (Ref. 70-30-00) GB DEF-STAN 91-101 LUBRICATING OIL TURBINE ENGINE SYNT BASE (Ref. 20-31-00)
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EFF : 701-749, 12-13-24 Page 319 Config-2 Jan 01/06 SROS
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C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-13-24-612-808 12-32-24-281-804 24-21-00-210-810 24-21-00-612-814 24-42-00-861-801 24-42-00-862-801 71-00-00-720-828 71-00-00-860-810 71-13-00-010-805 71-13-00-410-805 78-31-00-040-805 78-31-00-440-805 12-13-24-991-014 12-13-24-991-023
IDG Servicing - Filling of the IDG with Addition of Oil after Level Check Sampling of the IDG Oil for Analysis Inspection of the Filter Element Servicing of the IDG after Oil Chemical Energize the Ground Service Network De-energize the Ground Service Network Dry Motoring Engine Engine Automatic Start Open the Fan Cowl Doors Close the Fan Cowl Doors Deactivation of the Thrust Reverser for Activation of the Thrust Reverser after Fig. 304 Fig. 305
Oil or
Contamination
Maintenance Maintenance
3. __________ Job Set-up Subtask 12-13-24-861-061 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-24-941-064 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure. Subtask 12-13-24-010-075 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU.
EFF : 701-749, 12-13-24 Page 320 Config-2 Jan 01/06 SROS
Subtask 12-13-24-865-072 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU GCU 1 4XU1 Q10 722VU FADEC B ENG 1 13KS1 D44 742VU IDG 1 DISC 1XT1 A76 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 721VU GCU 2 4XU2 N06 722VU FADEC B ENG 2 13KS2 K49 742VU IDG 2 DISC 1XT2 D69 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-13-24-010-076 E. Get Access (1) Open the fan cowl doors (Ref. TASK 71-13-00-010-805): - FOR 4030EM1 415AL, 416AR, - FOR 4030EM2 425AL, 426AR. Subtask 12-13-24-040-054 F. Deactivation of the Thrust Reverser WARNING : YOU MUST DEACTIVATE THE THRUST REVERSER BEFORE YOU DO WORK ON _______ OR AROUND IT. IF YOU DO NOT, THE THRUST REVERSER CAN OPERATE ACCIDENTALLY AND CAUSE INJURY AND/OR DAMAGE. (1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 7831-00-040-805).
EFF : 701-749, 12-13-24 Page 321 Config-2 Jan 01/02 R SROS
4. Procedure _________ (Ref. Fig. 304/TASK 12-13-24-991-014, 305/TASK 12-13-24-991-023) Subtask 12-13-24-864-064 A. Depressurization of the IDG Case (Ref. Fig. 304/TASK 12-13-24-991-014) WARNING : POINT THE OVERFLOW DRAIN HOSE INTO A CONTAINER WHEN YOU CONNECT _______ THE HOSE TO THE OVERFLOW DRAIN VALVE. THIS WILL PREVENT BURNS FROM THE HOT OIL SPRAY. HOT OIL CAN CAUSE BURNS TO EYES AND SKIN. CAUTION : DO NOT USE DEVICES OTHER THAN THE APPROVED OVERFLOW DRAIN-HOSE _______ FITTING. HARD METAL OBJECTS SUCH AS SCREWDRIVERS CAN CAUSE DAMAGE TO THE OVERFLOW DRAIN-VALVE SEAT. (1) Put a container 5.7 l (1.5 USgal) below the IDG (10). (2) Remove the dust cap (4) from the overflow drain valve (3). (3) Put the end of the overflow drain hose (6) of the TANK - ENGINE OIL FILLING UP (DH13PM) in the container (7). (4) Do this step to depressurize the IDG case: (a) Connect the overflow drain hose (6) of the TANK - ENGINE OIL FILLING UP (DH13PM) to the overflow drain valve (3). NOTE : Some oil can come out of the overflow drain hose (6) of ____ the TANK - ENGINE OIL FILLING UP (DH13PM) when you connect it. Subtask 12-13-24-680-062 B. Draining of the Oil (Ref. Fig. 304/TASK 12-13-24-991-014) WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. _______ CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU. (1) Cut and remove the lockwire from the case drain plug (2). R R
NOTE : Approximately 3.8 l (1 USgal) of oil will flow into the ____ container.
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Draining and Filling of the IDG Figure 304/TASK 12-13-24-991-014 EFF : 701-749, 12-13-24 Page 323 Config-2 Jan 01/02 R SROS
IDG Oil Filter Figure 305/TASK 12-13-24-991-023 EFF : 701-749, 12-13-24 Page 324 Config-2 Jan 01/02 R SROS
(2) Remove the case drain plug (2). (3) Remove the seal-ring (1) and discard it. (4) Drain the oil. NOTE : If the drained oil has a fuel odor, do the servicing of the ____ IDG after oil chemical contamination (Ref. TASK 24-21-00-612814). If you think that the condition of the drained oil is not correct, do a sampling of the IDG oil for analysis (Ref. TASK 12-32-24-281-804). Subtask 12-13-24-020-068 C. Removal of the IDG Oil Filter (Ref. Fig. 305/TASK 12-13-24-991-023) WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. _______ CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU. (1) Cut and remove the lockwire from the filter cover (1). NOTE : Put a container 5.7 l (1.5 USgal) below the filter cavity. ____ R
(2) Remove the filter cover (1). (3) Remove and discard the O-ring (2) from the filter cover (1). (4) Remove the filter element (3). (5) Remove and discard the O-ring (4) from the filter element (3).
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(6) Install a blanking plug on the filter cavity port. Subtask 12-13-24-210-065 D. Inspection of the IDG Oil Filter (1) Do the inspection of the filter element (Ref. TASK 24-21-00-210-810). NOTE : We recommend you do a visual inspection of the IDG oil filter ____ for possible contamination, debris.
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Subtask 12-13-24-640-059 E. Lubrication of the Expendable Parts (1) Lubricate the new seal-ring (1) with engine lubricating oil (Material No. OMAT 1011). R
(2) Lubricate the new O-ring (4) with OILS (Material No. 03-002).
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(3) Lubricate the new O-ring (2) with OILS (Material No. 03-002). Subtask 12-13-24-420-077 F. Installation of the Case Drain Plug (Ref. Fig. 304/TASK 12-13-24-991-014)
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WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. _______ CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU. (1) Install the new seal-ring (1) on the case drain plug (2). (2) Install the case drain plug (2). (3) TORQUE the case drain plug (2) to between 55 and 75 lbf.in (0.62 and 0.84 m.daN). (4) Safety the case drain plug (2) with lockwire 0.028 to 0.031 in.(0.71 to 0.79 mm) dia. (Material No. OMAT 238). Subtask 12-13-24-420-082 G. Installation of the IDG Oil Filter (Ref. Fig. 305/TASK 12-13-24-991-023)
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WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. _______ CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU. CAUTION : MAKE SURE THE COMPONENTS ARE SEATED IN THE IDG SCAVENGE FILTER _______ CAVITY BEFORE YOU INSTALL THE FILTER COVER. DO NOT TIGHTEN THE FILTER COVER SCREWS TO FORCE THE FILTER COMPONENTS INTO THE HOUSING. (1) Install the new O-ring (4) on the filter element (3). (2) Install the new O-ring (2) on the filter cover (1).
EFF : 701-749, 12-13-24 Page 326 Config-2 Jan 01/02 SROS
(3) Put the filter element (3) in the filter cavity. (4) Install the filter cover (1). (5) TORQUE the filter cover (1) to between 13 and 15 lbf.ft (1.76 and 2.03 m.daN). (6) Safety the filter cover (1) with the lockwire 0.028 to 0.031 in.(0.71 to 0.79 mm) dia. (Material No. OMAT 238). Subtask 12-13-24-612-071 H. Filling of the IDG with Oil (Ref. Fig. 304/TASK 12-13-24-991-014) CAUTION : USE ONLY APPROVED TYPES/BRANDS OF LUBRICANTS. _______ DO NOT MIX TYPES/BRANDS OF LUBRICANTS. NOTE : In rain, fog or wet conditions, be careful to prevent water ____ contamination of the IDG oil during the filling procedure. (1) Remove the dust cap (5) from the pressure fill valve (9). (2) Connect the pressure fill hose (8) of the TANK - ENGINE OIL FILLING UP (DH13PM) to the pressure fill valve (9). (3) Fill the IDG with the filtered OILS (Material No. 03-002) at a maximum pressure of 35 psi (2.41 bar). NOTE : The AMM 20-34-00 gives a list of oil brand names approved for ____ the IDG. (4) Stop this operation when the quantity of oil collected from the overflow drain hose (6) of the TANK - ENGINE OIL FILLING UP (DH13PM) is 0.95 l (0.25 USgal) minimum. Subtask 12-13-24-020-064 J. Removal of the Hoses (Ref. Fig. 304/TASK 12-13-24-991-014) (1) Disconnect the pressure fill hose (8) of the TANK - ENGINE OIL FILLING UP (DH13PM) from the pressure fill valve (9). (2) Install the dust cap (5) on the pressure fill valve (9). (3) When only drops of oil come out of the overflow drain hose (6) of the TANK - ENGINE OIL FILLING UP (DH13PM), disconnect the hose (6). (4) Install the dust cap (4) on the overflow drain valve (3).
EFF : 701-749, 12-13-24 Page 327 Config-2 Apr 01/03 R SROS
Subtask 12-13-24-720-050 K. If you replaced a part of the oil system (filter, external system component, drain plug), do a dry motoring for leak check before inspection (Ref. TASK 71-00-00-720-828). Subtask 12-13-24-210-055 L. Inspection of the Oil Level (Ref. Fig. 304/TASK 12-13-24-991-014) NOTE : Before you do a check of the oil level, we recommend that you do ____ dry motoring for two minutes (Ref. TASK 71-00-00-720-828). Alternatively, you can do the check after an engine start at minimum idle (Ref. TASK 71-00-00-860-810). This is to make sure you get maximum filling of the external oil system.
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(1) Inspection of the oil level after dry motoring. R R R R R R R
CAUTION : IF YOU DRY-MOTOR THE ENGINE, MAKE SURE THAT THE OIL LEVEL _______ IS STABLE BEFORE YOU DO THE INSPECTION. IN AMBIENT AIR TEMPERATURES OF LESS THAN 20⁰C, THE OIL LEVEL WILL BECOME STABLE ONLY AFTER 30 MINUTES. THUS THE LEVEL INDICATIONS ON THE SIGHTGLASS WILL NOT BE CORRECT BEFORE THE END OF THIS PERIOD. IF YOU ADD OIL WHEN IT IS NOT NECESSARY, THERE IS A RISK THAT YOU WILL CAUSE FAILURE OF THE IDG.
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(a) Let the oil in the IDG become stable. (b) Look at the oil level sight-glass of the IDG: - if the oil level is at or near the top of the green band, oil servicing is not necessary, - if the oil level is below the green band or above the green band, do the filling of the IDG with oil or addition of oil after level check (Ref. TASK 12-13-24-612-808). (2) Inspection of the oil level after an engine start (alternative procedure). (a) Let the oil in the IDG become stable for 5 minutes. (b) Look at the oil level sight-glass of the IDG: - if the oil level is in the green or yellow band, oil servicing is not necessary, - if the oil level is below the green band or above the yellow band, do the filling of the IDG with oil or addition of oil after level check (Ref. TASK 12-13-24-612-808).
EFF : 701-749, 12-13-24 Page 328 Config-2 Apr 01/03 SROS
5. Close-up ________ Subtask 12-13-24-440-054 A. Make the thrust reverser serviceable after maintenance (Ref. TASK 78-3100-440-805). Subtask 12-13-24-865-073 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1, 1XT1, 4XU1 - FOR 4030EM2 12KS2, 13KS2, 1XT2, 4XU2 Subtask 12-13-24-410-064 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Close the access door 811. (4) Remove the access platform(s). (5) Close the fan cowl doors (Ref. TASK 71-13-00-410-805): - FOR 4030EM1 415AL, 416AR, - FOR 4030EM2 425AL, 426AR. Subtask 12-13-24-862-061 D. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : 701-749, 12-13-24 Page 329 Config-2 Jan 01/02 SROS
FLIGHT CONTROLS - SERVICING ___________________________ TASK 12-13-27-612-801 Oil Replenishing of the THS Actuator (1CS) WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific No specific 0U190363 0U190364
circuit breaker(s) safety clip(s) 1 ACCESS PLATFORM 5M (16 FT) 1 TOOL - OIL FILLING, THS ACTUATOR 1 TOOL - OIL DRAINING, THS ACTUATOR
EFF : ALL 12-13-27 SROS
Page 301 Jan 01/05
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 03-003 Material No. 19-003
USA MIL-PRF-7808 LUBRICATING OIL TURBINE SYNTHETIC BASE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------4
packing
27-44-51 02 -100
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 27-40-00-866-801 29-00-00-864-804 R 12-13-27-991-001
Energize the Ground Service Network De-energize the Ground Service Network Operation of the THS Actuator Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Fig. 301
3. __________ Job Set-up Subtask 12-13-27-860-052 A. Aircraft Maintenance Configuration (1) Move the THS actuator five times fully up and down and then in the 0⁰ position (Ref. TASK 27-40-00-866-801). (2) Energize the ground service network (Ref. TASK 24-42-00-861-801). (3) Make sure that the hydraulic systems are depressurized (Ref. TASK 29-00-00-864-804).
EFF : ALL 12-13-27 SROS
Page 302 Jul 01/02
Subtask 12-13-27-865-050 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU FCPC3 STBY COM 7CE6 R20 721VU FCPC3 STBY MON 7CE5 R19 722VU FCPC 3 7CE3 V42 722VU FCPC 2 NORM 7CE2 V41 722VU FCPC 3 7CE4 V38 742VU FCPC 1 NORM 7CE1 C69 742VU FCPC 1 STBY 11CE K69 Subtask 12-13-27-010-050 C. Put the ACCESS PLATFORM 5M (16 FT) in position below the access door 312AR and open the access door 312AR. 4. Procedure _________ (Ref. Fig. 301/TASK 12-13-27-991-001) NOTE : Wait one hour after movement of the THS Actuator before you do the ____ check of the oil level. Subtask 12-13-27-612-050 A. Oil Replenishing of the THS Actuator WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Remove the manual cranking plug (3) between the two hydraulic motors and remove and discard the packing (4). (2) Remove the cap (1) from the oil fill plug (2) and install the TOOL OIL FILLING, THS ACTUATOR on the oil fill plug (2). R R
(3) Monitor the oil level indicator (5) and fill the THS actuator with OILS (Material No. 03-003), until the quantity is correct. The correct quantity is when the oil level is in the middle position between the MINI and the MAXI marks.
EFF : ALL 12-13-27 SROS
Page 303 Apr 01/02
R
THS Actuator Figure 301/TASK 12-13-27-991-001
EFF : ALL 12-13-27 SROS
Page 304 Apr 01/02
NOTE : The volume between MINI and MAXI indication on the oil level ____ indicator is 0.2 l (0.0528 USgal). (4) If the gearbox oil level is too much, drain the oil which is too much from the gearbox. (a) Remove the drain plug (6) from the gearbox and install the TOOL OIL DRAINING, THS ACTUATOR (0U190364) in the gearbox and let the oil drain until the oil level is correct. (b) Remove the TOOL - OIL DRAINING, THS ACTUATOR (0U190364) from the gearbox and install the drain plug (6). (5) Remove the TOOL - OIL FILLING, THS ACTUATOR and clean the cap (1) with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003). (6) Install the new packing (4) on the manual cranking plug (3) and install the cap (1) and the manual cranking plug (3). 5. Close-up ________ Subtask 12-13-27-865-051 A. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 7CE1, 7CE2, 7CE3, 7CE4, 7CE5, 7CE6, 11CE. Subtask 12-13-27-410-050 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. R
(2) Close the access door 312AR and remove the access platform. (3) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-13-27-860-053 C. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-13-27 SROS
Page 305 Jul 01/06
TASK 12-13-27-612-802 Oil Replenishing of the Flap Power Control Unit (PCU) Gearbox (5000CV) WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No No No No
specific specific specific specific
circuit breaker(s) safety clip(s) 1 CONTAINER 1 L (1/4 USGAL) 1 WARNING NOTICE Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft)
EFF : ALL 12-13-27 SROS
Page 306 Jan 01/05
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 03-003 Material No. 19-003 R
USA MIL-PRF-7808 LUBRICATING OIL TURBINE SYNTHETIC BASE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Expendable Parts
R R R
------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
R
2
R
preformed packing
27-54-51 01 -110
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 27-50-00-866-801 27-50-00-866-802 32-12-00-010-801 32-12-00-410-801 27-54-51-000-801 27-54-51-400-801 12-13-27-991-002
Energize the Ground Service Network De-energize the Ground Service Network Extension of the Flaps on the Ground Retraction of the Flaps on the Ground Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Removal of the Flaps Power Control-Unit (PCU) (5000CV) (for corrective action) Installation of the Flaps Power Control-Unit (PCU) (5000CV) (for corrective action) Fig. 302
3. __________ Job Set-up Subtask 12-13-27-860-054 A. Energize the ground service network (Ref. TASK 24-42-00-861-801).
EFF : ALL 12-13-27 SROS
Page 307 Jan 01/06
INTENTIONALLY BLANK
R 12-13-27 SROS
Page 308 Jul 01/02
Subtask 12-13-27-865-052 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM 10CV X14 722VU SFCC 2 FLAP 2CV T43 742VU SFCC 1 FLAP 1CV L61 Subtask 12-13-27-010-051 C. Get Access (1) Open the right MLG door (Ref. TASK 32-12-00-010-801). (2) Put the CONTAINER 1 L (1/4 USGAL) in position below the flap PCU. (3) Put the WARNING NOTICE in position to tell persons not to operate the flap/slat system. 4. Procedure _________ (Ref. Fig. 302/TASK 12-13-27-991-002) Subtask 12-13-27-612-051 A. Oil Replenishing of the Flap Power Control Unit (PCU) Gearbox WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. R R R
NOTE : After installation of a new PCU (5000CV), extend and retract the ____ flaps before you do the oil replenishing (Ref. TASK 27-50-00-866801) and (Ref. TASK 27-50-00-866-802). (1) Remove the oil-fill plug (1) and remove and discard the preformed packing (2).
EFF : ALL 12-13-27 SROS
Page 309 Oct 01/01
Flap PCU Figure 302/TASK 12-13-27-991-002 EFF : ALL 12-13-27 R SROS
Page 310 Apr 01/01
(2) Slowly add the OILS (Material No. 03-003) to the flap PCU gearbox until it comes out of the oil-fill hole. NOTE : If the added oil quantity is between 50 cm3 (3.05 in.3) and 70 ____ cm3 (4.27 in.3) and there is no leak visible, check the oil level at the next A-Check and top-up as necessary: - if you add up to 50 cm3 (3.05 in.3) replace the PCU, but not later than the next A-Check (Ref. TASK 27-54-51-000-801) and (Ref. TASK 27-54-51-400-801). - if you add more than 50 cm3 (3.05 in.3) replace the PCU before the next 20 flights (Ref. TASK 27-54-51-000-801) and (Ref. TASK 27-54-51-400-801). R R
(3) Clean the oil-fill plug (1) with a clean lint-free cloth, MISCELLANEOUS (Material No. 19-003).
R R R
(4) Apply the OILS (Material No. 03-003) to the new preformed packing (2).
R R R
(5) Install the preformed packing (2) on the oil-fill plug (1) and install the oil-fill plug (1)
R
(6) TORQUE the oil-fill plug (1) to between 2.0 and 2.5 m.daN (14.74 and 18.43 lbf.ft).
R R
(7) Remove the unwanted oil from the area of the oil-fill plug (1) with a lint-free cloth, MISCELLANEOUS (Material No. 19-003).
R R
(8) Make sure that there is no oil leakage at the preformed packing (2). 5. Close-up ________ Subtask 12-13-27-865-053 A. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1CV, 2CV, 10CV.
EFF : ALL 12-13-27 SROS
Page 311 Jan 01/06
Subtask 12-13-27-410-051 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the right MLG door (Ref. TASK 32-12-00-410-801). (3) Remove the access platform(s). (4) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-13-27-860-055 C. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-13-27 R SROS
Page 312 Jan 01/06
TASK 12-13-27-612-803 Oil Replenishing of the Slat Power Control-Unit (PCU) Gearbox (5000CW) WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No No No No No
specific specific specific specific specific
circuit breaker(s) safety clip(s) 1 ACCESS PLATFORM 2M (6 FT) 1 CONTAINER 1 L (1/4 USGAL) 1 WARNING NOTICE Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft)
EFF : ALL 12-13-27 SROS
Page 313 Jan 01/05
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 03-003 Material No. 19-003
USA MIL-PRF-7808 LUBRICATING OIL TURBINE SYNTHETIC BASE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------2
preformed packing
27-84-03 01 -320
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R R
24-42-00-861-801 24-42-00-862-801 53-35-13-000-802 53-35-13-400-802 27-84-51-000-801 27-84-51-400-801 12-13-27-991-003
Energize the Ground Service Network De-energize the Ground Service Network Removal of the Belly Fairing Access Panels Installation of the Belly Fairing Access Panels Removal of the Slat Power Control-Unit (PCU) (5000CW) (for corrective action) Installation of the Slat Power Control-Unit (PCU) (5000CW) (for corrective action) Fig. 303
3. __________ Job Set-up Subtask 12-13-27-860-056 A. Energize the ground service network (Ref. TASK 24-42-00-861-801).
EFF : ALL 12-13-27 SROS
Page 314 Jul 01/02
Subtask 12-13-27-865-054 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM AVAIL 10CW X13 722VU SFCC 2 SLAT 2CW V40 742VU SFCC 1 SLAT 1CW L62 Subtask 12-13-27-010-052 C. Get Access (1) Put the WARNING NOTICE in position to tell persons not to operate the flap/slat system. (2) Put the ACCESS PLATFORM 2M (6 FT) in position below the access panel 195CB and remove the access panel 195CB (Ref. TASK 53-35-13-000-802). (3) Put the CONTAINER 1 L (1/4 USGAL) in position below the slat PCU. 4. Procedure _________ (Ref. Fig. 303/TASK 12-13-27-991-003) Subtask 12-13-27-612-052 R
A. Oil Replenishing of Slat Power Control Unit (PCU) Gearbox WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Remove the oil-fill plug (1) and remove and discard the preformed packing (2). (2) Slowly add the OILS (Material No. 03-003) to the slat PCU gearbox until it comes out of the oil-fill hole. NOTE : If the added oil quantity is between 50 cm3 (3.05 in.3) and 70 ____ cm3 (4.27 in.3) and there is no leak visible, check the oil level at the next A-Check and top-up as necessary: - if you add up to 50 cm3 (3.05 in.3) replace the PCU, but not later than the next A-Check (Ref. TASK 27-84-51-000-801) and (Ref. TASK 27-84-51-400-801), - if you add more than 50 cm3 (3.05 in.3) replace the PCU before the next 20 flights (Ref. TASK 27-84-51-000-801) and (Ref. TASK 27-84-51-400-801).
EFF : ALL 12-13-27 SROS
Page 315 Jul 01/06
Slat PCU Figure 303/TASK 12-13-27-991-003 EFF : ALL 12-13-27 R SROS
Page 316 Jul 01/01
(3) Clean the oil-fill plug (1) with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003) and apply the OILS (Material No. 03-003) to the new preformed packing (2). (4) Install the preformed packing (2) on the oil-fill plug (1) and install the oil-fill plug (1) (5) TORQUE the oil-fill plug (1) to between 2.0 and 2.5 m.daN (14.74 and 18.43 lbf.ft) and remove the unwanted oil from near the oil-fill plug (1) with a lint-free cloth MISCELLANEOUS (Material No. 19-003). (6) Examine the preformed packing (2) for signs of oil leakage. NOTE : Leaks are not permitted. ____ 5. Close-up ________ Subtask 12-13-27-865-055 A. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1CW, 2CW, 10CW. Subtask 12-13-27-410-052 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panel 195CB (Ref. TASK 53-35-13-400-802). (3) Remove the access platform(s). (4) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-13-27-860-057 C. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-13-27 R SROS
Page 317 Apr 01/02
TASK 12-13-27-612-804 Drain and Refill the Rotary Actuators WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Refer to the MPD TASK: 275400-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R R
No No No No No No No No
specific specific specific specific specific specific specific specific
1 2 1 1 1
No specific 1X56176802
1
circuit breaker(s) safety clip(s) TRANSPARENT TUBE WITH A MALE 3/8 in. FITTING ACCESS PLATFORM 3M (10 FT) CONTAINER 3 L(3/4 USGAL) GUN - GREASE, DIA 3/8 IN FEMALE ADAPTER HOSE - HIGH PRESSURE, DIA 3/8 MALE FITTINGS WARNING NOTICE Torque Wrench : range 0.00 to 1.20 m.daN (0.00 to 9.00 lbf.ft) Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft) FILLER
EFF : ALL 12-13-27 SROS
Page 318 Apr 01/05
------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------98D27803000000 FOR FIN 5122CV 98F29208217000
1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER 1 SAFETY PIN - RAT
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 04-022
USA MIL-PRF-81322 SYNTHE.HYDROCARBON GREASE HIGH PRESSURE (Ref. 20-31-00)
Material No. 04-025 Material No. 19-003
LUBRICANT, SEMIFLUID (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------R
2 2
packing packing
27-54-59 04 -040 27-54-59 04 -040A
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 57-56-11-000-807 57-56-11-400-807 27-50-00-866-801 27-50-00-866-802
Energize the Ground Service Network De-energize the Ground Service Network Removal of the Movable Flap Track Fairings Nos. 2 thru 5 for Access Installation of the Movable Flap Track Fairings Nos. 2 thru 5 after Access Extension of the Flaps on the Ground (for corrective action) Retraction of the Flaps on the Ground (for corrective action)
EFF : ALL 12-13-27 SROS
Page 319 Jul 01/06
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------27-54-59-000-801 27-54-59-000-802 27-54-59-400-801 27-54-59-400-802
Removal of the Rotary Actuator (5009CV, 5087CV) (for corrective action) Removal of the Rotary Actuator (5024CV, 5034CV, 5044CV, 5055CV, 5102CV, 5112CV, 5122CV, 5133CV) (for corrective action) Installation of the Rotary Actuator (5009CV, 5087CV) (for corrective action) Installation of the Rotary Actuator (5024CV, 5034CV, 5044CV, 5055CV, 5102CV, 5112CV, 5122CV, 5133CV) (for corrective action) Fig. 304 Fig. 305
12-13-27-991-004 12-13-27-991-007 FOR FIN 5009CV, 5087CV 27-50-00-866-801 Extension of the Flaps on the Ground 27-50-00-866-802 Retraction of the Flaps on the Ground 32-12-00-010-801 Open the MLG Doors for Maintenance 32-12-00-410-801 Close the MLG Doors after Maintenance FOR FIN 5122CV 29-24-00-081-801 Removal of the RAT Safety Pin 29-24-00-481-801 Installation of the RAT Safety Pin FOR FIN 5024CV, 5034CV, 5044CV, 5055CV, 5102CV, 5112CV, 5122CV, 5133CV 27-50-00-866-802 Retraction of the Flaps on the Ground 3. __________ Job Set-up Subtask 12-13-27-860-050 A. Aircraft Maintenance Configuration (1) If the ambient temperature is aircraft is on the ground for least 15 time to increase the more than 20 times (Ref. TASK 00-866-802).
below 15 DEG.C (59.00 DEG.F) or the less than 10 hours, cycle the flaps at temperature. But do not cycle the flaps 27-50-00-866-801) and (Ref. TASK 27-50-
(2) Energize the ground service network (Ref. TASK 24-42-00-861-801).
EFF : ALL 12-13-27 R SROS
Page 320 Apr 01/02
Subtask 12-13-27-010-053 B. Get Access (1) FOR 5009CV, 5087CV open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Put the ACCESS PLATFORM 3M (10 FT) in position below the applicable access panel. (3) FOR 5122CV - install the SAFETY PIN - RAT (Ref. TASK 29-24-00-481-801). (4) Remove the applicable movable 000-807): - FOR 5024CV, 5102CV remove the No. 2 flap track - FOR 5034CV, 5112CV remove the No. 3 flap track - FOR 5044CV, 5122CV remove the No. 4 flap track - FOR 5055CV, 5133CV remove the No. 5 flap track
flap track fairing (Ref. TASK 57-56-11fairing, fairing, fairing, fairing.
(5) Put a CONTAINER 3 L(3/4 USGAL) in position below the applicable rotary actuator. Subtask 12-13-27-860-062 C. Aircraft Maintenance Configuration
R
(1) Put the flaps in position: - FOR 5024CV, 5034CV, 5044CV, 5055CV, 5102CV, 5112CV, 5122CV, 513 make sure that the flaps are retracted (Ref. TASK 27-50-00-866-802) - FOR 5009CV, 5087CV extend the flaps to the position 2 (Ref. TASK 27-50-00-866-801).
R R
NOTE : The two different flap positions are necessary for the correct ____ access to the applicable actuator.
R R
(2) Attach the LOCKING TOOL - FLAP/SLAT CONTROL LEVER to the flap/slat control lever on the panel 114VU.
R R
(3) Put the WARNING NOTICE in position on the panel 114VU to tell persons not to operate the flap/slat controls.
EFF : ALL 12-13-27 SROS
Page 321 Jan 01/06
Subtask 12-13-27-865-056 D. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM 10CV X14 722VU SFCC 2 FLAP 2CV T43 742VU SFCC 1 FLAP 1CV L61 4. Procedure _________ (Ref. Fig. 304/TASK 12-13-27-991-004, 305/TASK 12-13-27-991-007) NOTE : The SEMIFLUID must have a temperature of at least 15 DEG.C (59 DEG.F) ____ but not more than 40 DEG.C (104 DEG.F). If the temperature is too high the SEMIFLUID becomes too thin and will not coat the actuator gears correctly. R
NOTE : Before you use the SEMIFLUID, you must stir it fully. This make sure ____ that the SEMIFLUID has its original viscosity. NOTE : To drain and fill the 10 actuators, you need approximately 25 l (6.6 ____ USgal) SEMIFLUID. Subtask 12-13-27-612-053 A. Drain and refill the Rotary Actuator to confirm the SEMIFLUID Level WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Clean all the rotary actuator (3). (2) Draining (a) Remove the top plugs (1) and the bottom plug (6). Some SEMIFLUID may flow through the bottom hole. (b) Examine the packing (2) and replace them if necessary packing (2). (c) When the flow of SEMIFLUID stops, install the bottom plug (6) but do not tighten at this time.
EFF : ALL 12-13-27 SROS
Page 322 Jul 01/06
Flap Rotary Actuator Figure 304/TASK 12-13-27-991-004 EFF : ALL 12-13-27 R SROS
Page 323 Jul 01/01
R
Rotary Actuator Filling Set-up Figure 305/TASK 12-13-27-991-007
EFF : ALL 12-13-27 SROS
Page 324 Jul 01/01
(3) Refill (a) Install a TRANSPARENT TUBE WITH A MALE 3/8 in. FITTING on the upper hole and put a CONTAINER 3 L(3/4 USGAL) in position below the tube for the used fluid. (b) Remove the plug (5) with the lubrication plate and install the FILLER (1X56176802) (4) in the actuator (3). Only apply hand force for the installation of the FILLER (4). NOTE : It is recommended to use a HOSE - HIGH PRESSURE, DIA 3/8 ____ MALE FITTINGS with between the grease gun and the FILLER. (c) Make sure that the SEMIFLUID has a temperature of at least 15 DEG.C (59 DEG.F) but not more than 40 DEG.C (104 DEG.F). If the temperature is too high the SEMIFLUID becomes too thin and will not coat the actuator gears correctly. R
(d) Attach a GUN - GREASE, DIA 3/8 IN FEMALE ADAPTER with the flexible HP tube on the FILLER (4) and fill the rotary actuator with SEMIFLUID GREASE COMMON GREASE (Material No. 04-025) until: - for the flap drive station 1, 4 and 5, approx. 500ml, - for the flap drive station 2 and 3, approx. 1000ml, of the SEMIFLUID flows through the top hole and the transparent tube into the container. During the filling of the rotary actuator, examine the rotary actuator for leaks. (e) Disconnect the grease gun and the HP tube from the FILLER (4) and remove the FILLER (1X56176802) (4) from the actuator (3). (f) Disconnect the transparent tube from the upper hole. (g) Apply COMMON GREASE (Material No. 04-022) to the threads of the plug (5) and install the plug (5) with the lubrication plate on the actuator (3). (h) TORQUE the plug (5) to between 0.68 and 0.92 m.daN (60.17 and 81.41 lbf.in). (i) Remove the bottom plug (6) and monitor the fluid that comes out. (j) Apply COMMON GREASE (Material No. 04-022) to the thread of the plugs (1) and (6).
EFF : ALL 12-13-27 SROS
Page 325 Apr 01/05
(k) When the flow of fluid decreases and only drops come out, install the bottom plug (6). NOTE : The remaining SEMIFLUID is sufficient to lubricate the ____ actuator. (l) Install the top plug (1). (m) TORQUE the top and the bottom plugs (1) and (6) to between 1.45 and 1.95 m.daN (10.69 and 14.38 lbf.ft). (n) Remove the unwanted fluid from the actuator (3) with a cloth MISCELLANEOUS (Material No. 19-003). (4) Examine the actuator (3) for leakage. NOTE : If leakage is detected, do the subsequent steps: ____ - make sure that all three plugs are tight, - clean the actuator, - examine the actuator for leakage again. If there is no significant leakage, no further maintenance action is necessary. If there is still a leakage more than 1 drop thin liquid fluid per 1 hour or any else than thin liquid fluid (i.e. semifluid), replace the rotary actuator with the next C check (Ref. TASK 27-54-59-000-801) and (Ref. TASK 2754-59-400-801) or (Ref. TASK 27-54-59-000-802) and (Ref. TASK 27-54-59-400-802). 5. Close-up ________ Subtask 12-13-27-865-057 A. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1CV, 2CV, 10CV. Subtask 12-13-27-410-053 B. Close Access (1) FOR 5009CV, 5087CV close the MLG doors (Ref. TASK 32-12-00-410-801). (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 12-13-27 R SROS
Page 326 Oct 01/01
(3) Install the applicable movable 11-400-807): - FOR 5024CV, 5102CV install the No. 2 flap track - FOR 5034CV, 5112CV install the No. 3 flap track - FOR 5044CV, 5122CV install the No. 4 flap track - FOR 5055CV, 5133CV install the No. 5 flap track
flap track fairing (Ref. TASK 57-56fairing, fairing, fairing, fairing.
(4) FOR 5122CV - remove the SAFETY PIN - RAT (Ref. TASK 29-24-00-081-801). (5) Remove the access platform(s). (6) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-13-27-860-051 C. Aircraft Maintenance Configuration (1) Remove the warning notice(s). (2) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever on panel 114VU. (3) FOR 5009CV, 5087CV retract the flaps (Ref. TASK 27-50-00-866-802). (4) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-13-27 R SROS
Page 327 Oct 01/01
TASK 12-13-27-612-805 Oil Replenishing of the Flap System Torque Limiter (5003CV, 5081CV) WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No No No No
specific specific specific specific
98D27803000000
circuit breaker(s) safety clip(s) 1 CAN - OIL 1 CONTAINER 1 L (1/4 USGAL) Torque Wrench : range 1.00 to 10.00 m.daN (8.00 to 75.00 lbf.ft) 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
EFF : ALL 12-13-27 SROS
Page 328 Jan 01/05
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R
Material No. 02-001 Material No. 02-001A Material No. 19-003
USA MIL-H-5606 OIL, HYDRAULICPETROLEUM FLUID (Ref. 20-31-00) USA MIL-H-6083D OIL, HYDRAULICPETROLEUM FLUID (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------2
packing
27-54-42 01 -020
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 27-50-00-866-802 32-12-00-010-801 32-12-00-410-801 27-54-42-000-801 27-54-42-400-801 12-13-27-991-005
Energize the Ground Service Network De-energize the Ground Service Network Retraction of the Flaps on the Ground Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Removal of the System Torque Limiter (5003CV, 5081CV) (for corrective action) Installation of the System Torque Limiter (5003CV, 5081CV) (for corrective action) Fig. 306
EFF : ALL 12-13-27 SROS
Page 329 Jan 01/02
3. __________ Job Set-up Subtask 12-13-27-860-058 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). (2) Make sure that the flaps are retracted (Ref. TASK 27-50-00-866-802). (3) Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER on the slat/flap control lever. Subtask 12-13-27-865-058 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM 10CV X14 722VU SFCC 2 FLAP 2CV T43 742VU SFCC 1 FLAP 1CV L61 Subtask 12-13-27-010-059 C. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Put the CONTAINER 1 L (1/4 USGAL) in position below the system torque limiter. 4. Procedure _________ (Ref. Fig. 306/TASK 12-13-27-991-005) Subtask 12-13-27-612-054 R
A. Oil Replenishing of the Flap System Torque-Limiter WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES.
EFF : ALL 12-13-27 SROS
Page 330 Jul 01/06
Flap System Torque Limiter Figure 306/TASK 12-13-27-991-005 EFF : ALL 12-13-27 R SROS
Page 331 Jul 01/01
(1) Remove the oil-fill plug (1) and remove and discard the packing (2). (2) Use a CAN - OIL and slowly add the HYDRAULIC FLUIDS (Material No. 02001A) to the flap system torque limiter until it comes out of the oil-fill hole. NOTE : HYDRAULIC FLUIDS (Material No. 02-001A) is preferable, but ____ HYDRAULIC FLUIDS (Material No. 02-001) can also be used. R R R R R R R R R
NOTE : If the added oil quantity is between 50 cm3 (3.05 in.3) and 70 ____ cm3 (4.27 in.3) and there is no leak visible, check the oil level at the next A-Check and top-up as necessary: - if you add up to 50 cm3 (3.05 in.3) replace the STL, but not later than the next A-Check (Ref. TASK 27-54-42-000-801) and (Ref. TASK 27-54-42-400-801), - if you add more than 50 cm3 (3.05 in.3) replace the STL before the next 20 flights (Ref. TASK 27-54-42-000-801) and (Ref. TASK 27-54-42-400-801). (3) Clean the oil-fill plug (1) with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003). (4) Apply the HYDRAULIC FLUIDS (Material No. 02-001A) to the new packing (2) and install the packing (2) on the oil-fill plug (1). (5) Install the oil-fill plug (1) in the system torque limiter.
R R
(6) TORQUE the oil-fill plug (1) to between 3.05 and 3.73 m.daN (22.49 and 27.50 lbf.ft). (7) Remove the unwanted oil from near the oil-fill plug (1) with a clean cloth MISCELLANEOUS (Material No. 19-003). (8) Examine the oil fill plug (1) for signs of oil leakage. NOTE : Leaks are not permitted. ____ 5. Close-up ________ Subtask 12-13-27-865-059 A. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1CV, 2CV, 10CV.
EFF : ALL 12-13-27 SROS
Page 332 Jul 01/02
Subtask 12-13-27-410-054 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the MLG doors (Ref. TASK 32-12-00-410-801). (3) Remove the access platform(s). (4) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-13-27-860-059 C. Put the Aircraft back to its Initial Configuration (1) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever. (2) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-13-27 R SROS
Page 333 Oct 01/01
TASK 12-13-27-612-806 R
Oil Replenishing of the Slat System Torque Limiter (5009CW, 5069CW) WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No
specific specific specific specific specific
98D27803000000
circuit breaker(s) safety clip(s) 1 ACCESS PLATFORM 2M (6 FT) 1 CAN - OIL 1 CONTAINER 1 L (1/4 USGAL) Torque Wrench : range 1.00 to 10.00 m.daN (8.00 to 75.00 lbf.ft) 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
EFF : ALL 12-13-27 SROS
Page 334 Jul 01/06
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R
Material No. 02-001 Material No. 02-001A Material No. 19-003
USA MIL-H-5606 OIL, HYDRAULICPETROLEUM FLUID (Ref. 20-31-00) USA MIL-H-6083D OIL, HYDRAULICPETROLEUM FLUID (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------2
packing
27-84-42 01 -020
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801
Energize the Ground Service Network De-energize the Ground Service Network
53-35-13-000-802 53-35-13-400-802 27-80-00-866-802
Removal of the Belly Fairing Access Panels Installation of the Belly Fairing Access Panels Retraction of the Slats on the Ground (for corrective action) Removal of the System Torque Limiter (5009CW, 5069CW) (for corrective action) Installation of the System Torque Limiter (5009CW, 5069CW) (for corrective action) Fig. 307
R R R
27-84-42-000-801 27-84-42-400-801 R
12-13-27-991-006-A
EFF : ALL 12-13-27 SROS
Page 335 Jan 01/02
3. __________ Job Set-up Subtask 12-13-27-860-060 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). R
(2) Make sure that the slats are retracted (Ref. TASK 27-80-00-866-802). (3) Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER on the slat/flap control lever. Subtask 12-13-27-865-060 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM AVAIL 10CW X13 722VU SFCC 2 SLAT 2CW V40 742VU SFCC 1 SLAT 1CW L62 Subtask 12-13-27-010-061 C. Get Access (1) Put the ACCESS PLATFORM 2M (6 FT) in position below the access panel 193FB. (2) Remove the access panel 193FB (Ref. TASK 53-35-13-000-802). (3) Put the CONTAINER 1 L (1/4 USGAL) in position below the system torque limiter.
EFF : ALL 12-13-27 SROS
Page 336 Jan 01/02
4. Procedure _________ (Ref. Fig. 307/TASK 12-13-27-991-006-A) Subtask 12-13-27-612-055 R
A. Oil Replenishing of the Slat System Torque-Limiter WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Remove the oil-fill plug (1) and remove and discard the packing (2). (2) Use a CAN - OIL Slowly add the HYDRAULIC FLUIDS (Material No. 02001A) to the slat system torque limiter until it comes out of the oil-fill hole. NOTE : HYDRAULIC FLUIDS (Material No. 02-001A) is preferable, but ____ HYDRAULIC FLUIDS (Material No. 02-001) can also be used. NOTE : If the added oil quantity is between 50 cm3 (3.05 in.3) and 70 ____ cm3 (4.27 in.3) and there is no leak visible, check the oil level at the next A-Check and top-up as necessary: - if you add up to 50 cm3 (3.05 in.3) replace the STL, but not later than the next A-Check (Ref. TASK 27-84-42-000-801) and (Ref. TASK 27-84-42-400-801), - if you add more than 50 cm3 (3.05 in.3) replace the STL before the next 20 flights (Ref. TASK 27-84-42-000-801) and (Ref. TASK 27-84-42-400-801). (3) Clean the oil-fill plug (1) with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003). (4) Apply the HYDRAULIC FLUIDS (Material No. 02-001A) to the new packing (2) and install the packing (2) on the oil-fill plug (1) (5) Install the oil-fill plug (1) in the system torque limiter. (6) TORQUE the oil-fill plug (1) to between 3.05 and 3.73 m.daN (22.49 and 27.50 lbf.ft). (7) Remove the unwanted oil from near the oil-fill plug (1) with a clean cloth.
EFF : ALL 12-13-27 SROS
Page 337 Jul 01/06
R R
Slat System Torque Limiter Figure 307/TASK 12-13-27-991-006-A
EFF : ALL 12-13-27 SROS
Page 338 Jan 01/02
(8) Examine the oil fill plug (1) for signs of oil leakage. NOTE : Leaks are not permitted. ____ 5. Close-up ________ Subtask 12-13-27-865-061 A. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1CW, 2CW, 10CW. Subtask 12-13-27-410-055 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panel 193FB (Ref. TASK 53-35-13-400-802) and remove the access platform. (3) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-13-27-860-061 C. Put the Aircraft back to its Initial Configuration (1) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever. (2) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-13-27 R SROS
Page 339 Jan 01/02
**ON A/C 002-049, 202-249, 252-252, 255-299, 301-399, 451-499, 701-749, TASK 12-13-27-612-807 R
Semi-Fluid Sampling and Replenishing of the Input Gearbox (5007CV, 5022CV, 5032CV, 5042CV, 5053CV, 5085CV, 5100CV, 5110CV, 5120CV, 5131CV) WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Self Explanatory
EFF : 002-049, 202-249, 252-252, 255-299, 12-13-27 301-399, 451-499, 701-749, SROS
Page 340 Jan 01/06
2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No No
specific specific specific specific specific specific specific specific specific
1 1 1
circuit breaker(s) safety clip(s) container commercial 50 ml GREASE GUN THREAD ADAPTER (0.500-20UNF) TRANSPARENT TUBE WITH A MALE 3/8 in. FITTING ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE CONTAINER 1 L (1/4 USGAL) WARNING NOTICE Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft) LOCKING TOOL - FLAP/SLAT CONTROL LEVER
98D27803000000 FOR FIN 5120CV 98F29208217000
1
1 SAFETY PIN - RAT
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 04-025 Material No. 19-003
LUBRICANT, SEMIFLUID (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------2
packing
27-54-57 01 -020
R EFF : 002-049, 202-249, 252-252, 255-299, 12-13-27 301-399, 451-499, 701-749, SROS
Page 341 Jul 01/05
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 27-50-00-866-801 32-12-00-010-801 32-12-00-410-801 57-56-11-000-807 57-56-11-400-807 27-50-00-866-801 27-50-00-866-802 12-13-27-991-008 FOR FIN 5120CV 29-24-00-081-801 29-24-00-481-801 FOR FIN 5009CV, 5087CV 27-50-00-866-802
Energize the Ground Service Network De-energize the Ground Service Network Extension of the Flaps on the Ground Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Removal of the Movable Flap Track Fairings Nos. 2 thru 5 for Access Installation of the Movable Flap Track Fairings Nos. 2 thru 5 after Access Extension of the Flaps on the Ground (for corrective action) Retraction of the Flaps on the Ground (for corrective action) Fig. 308 Removal of the RAT Safety Pin Installation of the RAT Safety Pin Retraction of the Flaps on the Ground
3. __________ Job Set-up Subtask 12-13-27-860-070 A. Aircraft Maintenance Configuration (1) If the ambient temperature is aircraft is on the ground for least 15 time to increase the more than 20 times (Ref. TASK 00-866-802).
below 15 DEG.C (59.00 DEG.F) or the less than 10 hours, cycle the flaps at temperature. But do not cycle the flaps 27-50-00-866-801) and (Ref. TASK 27-50-
(2) Fully extend the flaps (Ref. TASK 27-50-00-866-801) and install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000). (3) Energize the ground service network (Ref. TASK 24-42-00-861-801). (4) Put WARNING NOTICE in position to tell persons not to operate the slat/flap system.
R EFF : 002-049, 202-249, 252-252, 255-299, 12-13-27 301-399, 451-499, 701-749, SROS
Page 342 Jul 01/05
Subtask 12-13-27-865-069 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM 10CV X14 722VU SFCC 2 FLAP 2CV T43 742VU SFCC 1 FLAP 1CV L61 Subtask 12-13-27-010-068 C. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801): - FOR 5007CV open 734, - FOR 5085CV open 744. (2) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position. R
(3) FOR 5120CV - install the SAFETY PIN - RAT (Ref. TASK 29-24-00-481-801). (4) Remove the access panels: - FOR 5022CV remove 573BB, 573FB, 531EL, - FOR 5032CV remove 574BB, 574CB, 532EL, - FOR 5042CV remove 574EB, 574FB, 533EL, - FOR 5053CV remove 574KB, 574LB, 534EL, - FOR 5100CV remove 673BB, 673FB, 631ER, - FOR 5110CV remove 674BB, 674CB, 632ER, - FOR 5120CV remove 674EB, 674FB, 633ER, - FOR 5131CV remove 674MB, 674LB, 634ER. (5) Remove the related flap track fairing (Ref. TASK 57-56-11-000-807).
R EFF : 002-049, 202-249, 252-252, 255-299, 12-13-27 301-399, 451-499, 701-749, SROS
Page 343 Jul 01/05
4. Procedure _________ (Ref. Fig. 308/TASK 12-13-27-991-008) Subtask 12-13-27-612-058 R
A. Semi-Fluid Sampling and Replenishing of the Input Gearbox WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Clean the input gearbox. (2) Put the CONTAINER 1 L (1/4 USGAL) in position below the input gearbox (3). (3) Remove the top plug (1) and the bottom plug (1) and let at least 20 cm3 (1.22 in.3) of the first SEMIFLUID into a container commercial 50 ml. NOTE : If the SEMIFLUID does not drain, apply a pressure up to 7 psi ____ (0.4826 bar) to the top plug. (4) Let the remaining SEMIFLUID drain into the container. (5) When the flow of SEMIFLUID stops, install the THREAD ADAPTER (0.50020UNF) (4) in the lower hole of the actuator (3). Only apply hand force for the installation of the THREAD ADAPTER (4). (6) Sampling (a) Put a label with the subsequent information on the sample container: - P/N and Serial No. of the affected input gearbox, - sample date, - date of installation of the input gearbox, - wing position (station) of the input gearbox, - number of cycles/flight hours of the input gearbox. (b) Send the sample to any Laboratory for analysis for water content. NOTE : The analysis is in accordance with Karl Fischer-Direct ____ Method; ASTM D1744.If the water content in the SEMIFLUID is more than 12%, the input gearbox must be replaced within the next 100 flights latest.
EFF : 002-049, 202-249, 252-252, 255-299, 12-13-27 301-399, 451-499, 701-749, SROS
Page 344 Jul 01/06
R
Flap Input Gearbox Figure 308/TASK 12-13-27-991-008
EFF : 002-049, 202-249, 252-252, 255-299, 12-13-27 301-399, 451-499, 701-749, SROS
Page 345 Jul 01/06
(7) Examine the packings (2) and replace them if necessary packing (2). (8) Install a TRANSPARENT TUBE WITH A MALE 3/8 in. FITTING on the upper hole and put a CONTAINER 1 L (1/4 USGAL) in position below the tube for the used fluid. (9) Make sure that the SEMIFLUID has a temperature of at least 15 DEG.C (59 DEG.F) but not more than 40 DEG.C (104 DEG.F). If the temperature is too high the SEMIFLUID becomes too thin and will not coat the gearbox gears correctly. R R
(10) Attach a GREASE GUN on the THREAD ADAPTER (4) and fill the input gearbox with SEMIFLUID GREASE COMMON GREASE (Material No. 04-025) until the SEMIFLUID flows through the top hole and the transparent tube into the container. During the filling of the input gearbox, examine the input gearbox for leaks. (11) Disconnect the grease gun and the THREAD ADAPTER (4) from the input gearbox (3) and let approx. 0.175 l (0.0462 USgal) SEMIFLUID drain into the container. (12) Install the lower plug (1) with the O-ring (2). (13) Disconnect the transparent tube from the upper hole and install the top plug (1) with the O-ring (2). (14) TORQUE the plugs (1) to 1.69 m.daN (12.46 lbf.ft). (a) Remove the unwanted fluid from the actuator (3) with a cloth MISCELLANEOUS (Material No. 19-003). (15) Examine the actuator (3) for leakage. NOTE : If leakage is detected, do the subsequent steps: ____ - make sure that all plugs are tight, - clean the actuator, - examine the actuator for leakage again. (16) Remove the container.
EFF : 002-049, 202-249, 252-252, 255-299, 12-13-27 301-399, 451-499, 701-749, SROS
Page 346 Jul 01/06
5. Close-up ________ Subtask 12-13-27-010-069 A. Close Access (1) Install the flap track fairing (Ref. TASK 57-56-11-400-807). (2) Close the MLG doors (Ref. TASK 32-12-00-410-801). - FOR 5007CV close 734, - FOR 5085CV close 744. (3) Install the access panels: - FOR 5022CV install 573BB, 573FB, 531EL, - FOR 5032CV install 574BB, 574CB, 532EL, - FOR 5042CV install 574EB, 574FB, 533EL, - FOR 5053CV install 574KB, 574LB, 534EL, - FOR 5100CV install 673BB, 673FB, 631ER, - FOR 5110CV install 674BB, 674CB, 632ER, - FOR 5120CV install 674EB, 674FB, 633ER, - FOR 5131CV install 674MB, 674LB, 634ER. R
(4) FOR 5120CV - remove the SAFETY PIN - RAT (Ref. TASK 29-24-00-081-801). (5) Remove the access platform(s). (6) De-energize the ground service network (Ref. TASK 24-42-00-862-801). Subtask 12-13-27-865-070 B. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1CV, 2CV, 10CV.
R EFF : 002-049, 202-249, 252-252, 255-299, 12-13-27 301-399, 451-499, 701-749, SROS
Page 347 Jul 01/05
Subtask 12-13-27-860-071 C. Put the Aircraft back to its Initial Configuration (1) Remove the warning notice(s). (2) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever on panel 114VU. R
(3) FOR 5009CV, 5087CV retract the flaps (Ref. TASK 27-50-00-866-802). (4) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
R EFF : 002-049, 202-249, 252-252, 255-299, 12-13-27 301-399, 451-499, 701-749, SROS
Page 348 Jul 01/05
**ON A/C ALL TASK 12-13-27-680-801 Oil Draining of the Flap/Slat PCU (5000CV, 5000CW) WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific No specific No specific FOR FIN 5000CW No specific No specific
circuit breaker(s) safety clip(s) 1 CONTAINER 1 L (1/4 USGAL) 1 WARNING NOTICE 1 ACCESS PLATFORM 2M (6 FT) Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft)
EFF : ALL 12-13-27 SROS
Page 349 Jan 01/05
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------FOR FIN 5000CW Material No. 19-010
R
USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
C. Expendable Parts
R R R
------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
R R R R
FOR FIN 5000CV 4 preformed packing FOR FIN 5000CW 4 preformed packing
R
D. Referenced Information
27-54-51 01 -110 27-84-51 03 -020
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 12-13-27-991-002 12-13-27-991-003 FOR FIN 5000CV 12-13-27-612-802 32-12-00-010-801 32-12-00-410-801 FOR FIN 5000CW 12-13-27-612-803 53-35-13-000-802 53-35-13-400-802
Energize the Ground Service Network De-energize the Ground Service Network Fig. 302 Fig. 303 Oil Replenishing of the Flap Power Control Unit (PCU) Gearbox (5000CV) Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Oil Replenishing of the Slat Power Control-Unit (PCU) Gearbox (5000CW) Removal of the Belly Fairing Access Panels Installation of the Belly Fairing Access Panels
EFF : ALL 12-13-27 SROS
Page 350 Jan 01/06
3. __________ Job Set-up Subtask 12-13-27-860-063 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-27-865-063 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 5000CV 721VU SFCC 1 NORM 10CV X14 722VU SFCC 2 FLAP 2CV T43 742VU SFCC 1 FLAP 1CV L61 FOR 5000CW 721VU SFCC 1 NORM AVAIL 10CW X13 722VU SFCC 2 SLAT 2CW V40 742VU SFCC 1 SLAT 1CW L62 Subtask 12-13-27-010-063 C. Get Access (1) Put the WARNING NOTICE in position to tell persons not to operate the flap/slat system. (2) FOR 5000CV (a) Open the right MLG door (Ref. TASK 32-12-00-010-801). (3) FOR 5000CW (a) Put the ACCESS PLATFORM 2M (6 FT) in position below the access panel 195CB. (b) Remove the access panel 195CB (Ref. TASK 53-35-13-000-802). (4) Put the CONTAINER 1 L (1/4 USGAL) in position below the related PCU.
EFF : ALL 12-13-27 R SROS
Page 351 Jan 01/06
4. Procedure _________ (Ref. Fig. 302/TASK 12-13-27-991-002, 303/TASK 12-13-27-991-003) Subtask 12-13-27-680-050 A. Oil Drainage of the Flap/Slat PCU. WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Remove the oil-fill plug (1) and remove and discard the preformed packing (2). (2) Remove and discard the lockwire from the oil-drain plug (3). (3) Remove the oil-drain plug (3) and remove and discard the preformed packing (4) and let the oil drain into an empty container. R R
(4) FOR 5000CV
R R R
(a) When the oil is fully drained, install the new preformed packing (4) and the oil-drain plug (3) in the flap PCU.
R R
(b) Measure the quantity of the oil.
R
1 _
Make sure that the drained oil quantity is not less than 100 cm3 (6.10 in.3). NOTE : If the oil quantity is less than 100 cm3 (6.10 in.3), ____ replace the PCU within the next 20 flights.
R R
(5) FOR 5000CW
R R
(a) When the oil is fully drained, install the new preformed packing (4) and the oil-drain plug (3) in the slat PCU.
R
(6) TORQUE the oil-drain plug (3) to between 2 and 2.5 m.daN (14.74 and 18.43 lbf.ft).
R
(7) Safety the oil-drain plug (3) with the lockwire, MISCELLANEOUS (Material No. 19-010).
EFF : ALL 12-13-27 SROS
Page 352 Jan 01/06
Subtask 12-13-27-612-056 R
B. Do the oil replenishing of the PCU: - FOR 5000CV (Ref. TASK 12-13-27-612-802), - FOR 5000CW (Ref. TASK 12-13-27-612-803). 5. Close-up ________ Subtask 12-13-27-865-064 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 5000CV 1CV, 2CV, 10CV, FOR 5000CW 1CW, 2CW, 10CW. Subtask 12-13-27-410-056 B. Close Access (1) Remove the container. (2) Remove the warning notice(s). (3) Make sure that the work area is clean and clear of tools and other items. (4) FOR 5000CV (a) Close the right MLG door (Ref. TASK 32-12-00-410-801). (5) FOR 5000CW (a) Install the access panel 195CB (Ref. TASK 53-35-13-400-802). (6) Remove the access platform(s). (7) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-13-27-860-064 C. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-13-27 SROS
Page 353 Jul 01/06
TASK 12-13-27-680-802 Oil Draining of the Flap/Slat System Torque Limiter (5003CV, 5081CV, 5009CW, 5069CW) WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. 1. __________________ Reason for the Job Self Explanatory
EFF : ALL 12-13-27 R SROS
Page 354 Jan 01/03
2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific 98D27803000000 FOR FIN 5000CW No specific
circuit breaker(s) safety clip(s) 1 ACCESS PLATFORM 2M (6 FT) 1 CONTAINER 1 L (1/4 USGAL) 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------FOR FIN 5000CW Material No. 19-010
USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------R R R
FOR FIN 5000CV 4 plug preformed packing
27-54-42 01 -020
FOR FIN 5000CW 4 plug preformed packing
27-84-42 01 -020
EFF : ALL 12-13-27 SROS
Page 355 Jul 01/06
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 27-50-00-866-802 27-80-00-866-802 12-13-27-991-005 12-13-27-991-006-A FOR FIN 5003CV, 5081CV 12-13-27-612-805
R
32-12-00-010-801 32-12-00-410-801 FOR FIN 5009CW, 5069CW 12-13-27-612-806 53-35-13-000-802 53-35-13-400-802
Energize the Ground Service Network De-energize the Ground Service Network Retraction of the Flaps on the Ground Retraction of the Slats on the Ground Fig. 306 Fig. 307 Oil Replenishing of the Flap System Torque Limiter (5003CV, 5081CV) Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Oil Replenishing of the Slat System Torque Limiter (5009CW, 5069CW) Removal of the Belly Fairing Access Panels Installation of the Belly Fairing Access Panels
3. __________ Job Set-up Subtask 12-13-27-860-065 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). (2) Make sure that the flaps and slats are retracted (Ref. TASK 27-50-00866-802) and (Ref. TASK 27-80-00-866-802). (3) Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER on the slat/flap control lever.
EFF : ALL 12-13-27 SROS
Page 356 Jul 01/06
Subtask 12-13-27-865-065 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 5003CV, 5081CV 721VU SFCC 1 NORM 10CV X14 722VU SFCC 2 FLAP 2CV T43 742VU SFCC 1 FLAP 1CV L61 FOR 5009CW, 5069CW 721VU SFCC 1 NORM AVAIL 10CW X13 722VU SFCC 2 SLAT 2CW V40 742VU SFCC 1 SLAT 1CW L62 Subtask 12-13-27-010-065 C. Get Access (1) Put the ACCESS PLATFORM 2M (6 FT) in position below the access panel 193BB. (2) FOR 5003CV, 5081CV open the MLG doors (Ref. TASK 32-12-00-010-801). (3) FOR 5009CW, 5069CW remove the access panel 193FB (Ref. TASK 53-35-13-000-802). (4) Put the CONTAINER 1 L (1/4 USGAL) in position below the system torque limiter. 4. Procedure _________ (Ref. Fig. 306/TASK 12-13-27-991-005, 307/TASK 12-13-27-991-006-A) Subtask 12-13-27-680-051 A. Oil Drainage of the Flap/Slat System Torque Limiter (1) Remove the oil-fill plug (1) and remove and discard the preformed packing (2). (2) Remove and discard the lockwire from the oil-drain plug (3).
EFF : ALL 12-13-27 R SROS
Page 357 Jan 01/03
(3) Remove the oil-drain plug (3) and remove and discard the preformed packing (4) and let the oil drain into the container. (4) Measure the quantity of the oil. R R R
(5) FOR 5000CV after the oil has completely drained, install the new plug preformed packing (4) and the oil-drain (3) into the flap system torque limiter.
R R R
(6) FOR 5000CW after the oil has completely drained, install the new plug preformed packing (4) and the oil-drain (3) into the slat system torque limiter. (7) TORQUE the oil drain plug to between 1.23 and 1.5 m.daN (108.84 and 132.74 lbf.in). (8) Safety the oil-drain plug with MISCELLANEOUS (Material No. 19-010). Subtask 12-13-27-612-057
R
B. Do the oil replenishing of the system torque limiter: - FOR 5003CV, 5081CV (Ref. TASK 12-13-27-612-805), - FOR 5009CW, 5069CW (Ref. TASK 12-13-27-612-806). 5. Close-up ________ Subtask 12-13-27-865-066 A. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 5003CV, 5081CV 1CV, 2CV, 10CV, FOR 5009CW, 5069CW 1CV, 2CV, 10CV. Subtask 12-13-27-410-057 B. Close Access (1) Remove the container. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 12-13-27 SROS
Page 358 Jul 01/06
(3) FOR 5003CV, 5081CV close the MLG doors (Ref. TASK 32-12-00-410-801). (4) FOR 5009CW, 5069CW install the access panel 193FB (Ref. TASK 53-35-13-400-802). (5) Remove the access platform(s). (6) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-13-27-860-066 C. Put the Aircraft back to its Initial Configuration (1) Remove the warning notice(s). (2) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever. (3) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-13-27 R SROS
Page 359 Jan 01/03
TASK 12-13-27-281-801 Sampling of the SEMIFLUID from the Flap Rotary Actuator WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. 1. __________________ Reason for the Job R R
To analyze the SEMIFLUID for water content, if the flap actuator is suspected for water ingress
EFF : ALL 12-13-27 SROS
Page 360 Jul 01/06
2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific No specific No specific No specific 98D27803000000 FOR FIN 5122CV 98F29208217000
circuit breaker(s) safety clip(s) container commercial 50 ml 1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE 1 WARNING NOTICE 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER 1 SAFETY PIN - RAT
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-13-27-612-804 24-42-00-861-801 24-42-00-862-801 57-56-11-000-807 57-56-11-400-807 27-50-00-866-801 27-50-00-866-802
Drain and Refill the Rotary Actuators Energize the Ground Service Network De-energize the Ground Service Network Removal of the Movable Flap Track Fairings Nos. 2 thru 5 for Access Installation of the Movable Flap Track Fairings Nos. 2 thru 5 after Access Extension of the Flaps on the Ground (for corrective action) Retraction of the Flaps on the Ground (for corrective action) Fig. 304
12-13-27-991-004 FOR FIN 5009CV, 5087CV 27-50-00-866-801 Extension of the Flaps on the Ground 27-50-00-866-802 Retraction of the Flaps on the Ground 32-12-00-010-801 Open the MLG Doors for Maintenance 32-12-00-410-801 Close the MLG Doors after Maintenance FOR FIN 5122CV 29-24-00-081-801 Removal of the RAT Safety Pin 29-24-00-481-801 Installation of the RAT Safety Pin FOR FIN 5024CV, 5034CV, 5044CV, 5055CV, 5102CV, 5112CV, 5122CV, 5133CV 27-50-00-866-802 Retraction of the Flaps on the Ground
EFF : ALL 12-13-27 SROS
Page 361 Jan 01/05
3. __________ Job Set-up Subtask 12-13-27-860-067 A. Aircraft Maintenance Configuration (1) If the ambient temperature is aircraft is on the ground for least 15 time to increase the more than 20 times (Ref. TASK 00-866-802).
below 15 DEG.C (59.00 DEG.F) or the less than 10 hours, cycle the flaps at temperature. But do not cycle the flaps 27-50-00-866-801) and (Ref. TASK 27-50-
(2) Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-27-010-066 B. Get Access (1) FOR 5009CV, 5087CV open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position below the applicable access panel. (3) FOR 5122CV - install the SAFETY PIN - RAT (Ref. TASK 29-24-00-481-801). (4) Remove the applicable movable 000-807): - FOR 5024CV, 5102CV remove the No. 2 flap track - FOR 5034CV, 5112CV remove the No. 3 flap track - FOR 5044CV, 5122CV remove the No. 4 flap track - FOR 5055CV, 5133CV remove the No. 5 flap track
flap track fairing (Ref. TASK 57-56-11fairing, fairing, fairing, fairing.
EFF : ALL 12-13-27 R SROS
Page 362 Jan 01/03
Subtask 12-13-27-860-068 C. Aircraft Maintenance Configuration (1) Put the flaps in position: - FOR 5024CV, 5034CV, 5044CV, 5055CV, 5102CV, 5112CV, 5122CV, 513 make sure that the flaps are retracted (Ref. TASK 27-50-00-866802), - FOR 5009CV, 5087CV extend the flaps to the position 2 (Ref. TASK 27-50-00-866-801). (2) Attach the LOCKING TOOL - FLAP/SLAT CONTROL LEVER to the flap/slat control lever on panel 114VU. (3) Put the WARNING NOTICE in position on panel 114VU to tell persons not to operate the flap/slat controls. Subtask 12-13-27-865-067 D. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM 10CV X14 722VU SFCC 2 FLAP 2CV T43 742VU SFCC 1 FLAP 1CV L61 4. Procedure _________ Subtask 12-13-27-281-050 A. Sampling of the SEMIFLUID of the Flap Rotary Actuator (Ref. Fig. 304/TASK 12-13-27-991-004) (1) Clean all the rotary actuator (3). (2) Remove the bottom plug (6) and if necessary the top plug (1). (3) Let at least 20 ml of SEMIFLUID flow into a container commercial 50 ml. (4) Examine the O-rings (2) and replace them if necessary. (5) Install the bottom plug (6) but do not tighten at this time.
EFF : ALL 12-13-27 R SROS
Page 363 Jan 01/03
(6) Put a label with the subsequent information on the sample container: - P/N and Serial No. of the affected actuator, - sample date, - date of installation of the actuator, - wing position (station) of the actuator, - number of cycles/flight hours of the actuator. (7) Send the sample to any Laboratory for analysis for water content. NOTE : The analysis is in accordance with Karl Fischer-Direct Method; ____ ASTM D1744. The rotary actuator must be replaced if the water content in the SEMIFLUID is more than 12%. (8) Do the drain and refill procedure (Ref. TASK 12-13-27-612-804). NOTE : After correct draining and filling of the actuator, a faulty ____ actuator will operate at least 500 flight cycles without any low-temperature performance problems. 5. Close-up ________ Subtask 12-13-27-865-068 A. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1CV, 2CV, 10CV. Subtask 12-13-27-410-058 B. Close Access (1) FOR 5009CV, 5087CV close the MLG doors (Ref. TASK 32-12-00-410-801). (2) Make sure that the work area is clean and clear of tools and other items. (3) Install the applicable movable 11-400-807): - FOR 5024CV, 5102CV install the No. 2 flap track - FOR 5034CV, 5112CV install the No. 3 flap track - FOR 5044CV, 5122CV install the No. 4 flap track - FOR 5055CV, 5133CV
flap track fairing (Ref. TASK 57-56fairing, fairing, fairing,
EFF : ALL 12-13-27 R SROS
Page 364 Jan 01/03
install the No. 5 flap track fairing. (4) FOR 5122CV - remove the SAFETY PIN - RAT (Ref. TASK 29-24-00-081-801). (5) Remove the access platform(s). (6) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-13-27-860-069 C. Aircraft Maintenance Configuration (1) Remove the warning notice(s). (2) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever on panel 114VU. (3) FOR 5009CV, 5087CV retract the flaps (Ref. TASK 27-50-00-866-802). (4) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-13-27 SROS
Page 365 Jan 01/03
HYDRAULIC POWER - SERVICING ___________________________ TASK 12-13-29-612-801 Oil Replenishment of the Ram Air Turbine (RAT) (11JR) WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No
specific specific specific specific specific specific
circuit breaker(s) safety clip(s) safety barriers 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 CAN - OIL 1 WARNING NOTICE Torque Wrench : range 2.00 to 26.00 lbf.ft (0.20 to 3.60 m.daN)
EFF : ALL 12-13-29 R SROS
Page 301 Jan 01/06
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 03-003 Material No. 19-003 Material No. 19-010
USA MIL-PRF-7808 LUBRICATING OIL TURBINE SYNTHETIC BASE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00) USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------R R
2 2 2 3 3 3
packing packing packing packing packing packing
29-24-54 29-24-54 29-24-54 29-24-54 29-24-54 29-24-54
02 -020 02A-020 02B-020 03 -020 03A-020 03B-020
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-24-00-869-801 29-24-00-869-802 12-13-29-991-001
Extension of the Ram Air Turbine (RAT) on the Ground Retraction of the Ram Air Turbine (RAT) on the Ground Fig. 301
EFF : ALL 12-13-29 SROS
Page 302 Jan 01/06
3. __________ Job Set-up Subtask 12-13-29-010-050 A. Get Access (1) Put the safety barriers in position. (2) Put the WARNING NOTICE in position to tell persons not to operate the RAT. (3) Extend the RAT (Ref. TASK 29-24-00-869-801). (4) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the RAT. (5) Remove the access panel 633HB. Subtask 12-13-29-865-050 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------742VU RAT STOW CTL 1JR D77
EFF : ALL 12-13-29 R SROS
Page 303 Jan 01/06
4. Procedure _________ (Ref. Fig. 301/TASK 12-13-29-991-001) **ON A/C 001-001, 201-207, 251-252, 255-299, 401-449, Subtask 12-13-29-612-050 A. Oil Replenishment of the Upper and/or Lower RAT Gearbox WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK _______ AREA WHEN YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. (1) Remove and discard the lockwire from the oil fill plug (1). (2) Remove the oil fill plug (1) and the packing (2) and/or (3). (3) Discard the packing (2) and/or (3). R R
(4) Fill the RAT gearbox with the OILS (Material No. 03-003) with a CAN OIL , until it comes out of the fill port. (5) Clean the oil fill plug (1) with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003).
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(6) Install the oil fill plug: - for the upper RAT gearbox, install the new packing (2) and the oil fill plug (1) - for the lower RAT gearbox,install the new packing (3) and the oil fill plug (1). (7) TORQUE the fill plug (1) to between 9.2 and 12.5 lbf.ft (1.24 and 1.69 m.daN).
EFF : ALL 12-13-29 SROS
Page 304 Jan 01/06
RAT Oil Fill Ports - Location Figure 301/TASK 12-13-29-991-001 R EFF : ALL 12-13-29 SROS
Page 305 Jan 01/06
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(8) Safety the oil fill plug (1) with the lockwire, MISCELLANEOUS (Material No. 19-010) **ON A/C 002-049, 208-249, 301-399, 451-499, 701-749, Subtask 12-13-29-612-050-A A. Oil Replenishment of the Upper and/or Lower RAT Gearbox (1) Remove and discard the lockwire from the oil fill plug (1). (2) Remove the oil fill plug (1) and the packing (2) and/or (3). (3) Discard the packing (2) and/or (3). (4) Fill the RAT gearbox WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE _______ THIS/THESE MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. - Fill the RAT gearbox with OILS (Material No. 03-003) with a CAN OIL, until it spills from the fill port. (5) Clean the oil fill plug (1) with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003). (6) Install for: - the upper RAT gearbox, the new packing (2) and the oil fill plug (1), - for the lower RAT gearbox, the new packing (3) and the oil fill plug (1). (7) TORQUE the fill plug CAUTION : YOU MUST NOT TIGHTEN MORE THAN THE MAXIMUM TORQUE VALUE. _______ IF YOU DO YOU CAN CAUSE DAMAGE. - TORQUE the fill plug (1) to between 9.2 and 12.5 lbf.ft (1.24 and 1.69 m.daN). (8) Safety the oil fill plug (1) with lockwire MISCELLANEOUS (Material No. 19-010)
R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-29 301-399, 401-449, 451-499, 701-749, SROS
Page 306 Jan 01/06
**ON A/C ALL 5. Close-up ________ Subtask 12-13-29-865-051 A. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1JR. Subtask 12-13-29-410-050 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panel 633HB. (3) Retract the RAT (Ref. TASK 29-24-00-869-802). (4) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 12-13-29 SROS
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APU - SERVICING _______________ TASK 12-13-49-612-801 Gravity Servicing of the APU Oil Reservoir WARNING : DO NOT TOUCH THE APU UNTIL IT IS SUFFICIENTLY COOL TO PREVENT BURNS _______ WHEN YOU DO THE MAINTENANCE TASK(S). WARNING : USE THE CORRECT PERSONAL PROTECTION. OIL CAN HAVE AN ADDITIVE CALLED _______ TRICRESYL PHOSPHATE IN IT. THIS CHEMICAL IS AN ASPHYXIANT, IT IS POISONOUS AND CAN BE ABSORBED THROUGH THE SKIN. USE CARE WHEN ENGINE OIL IS DRAINED. HOT OIL CAN POSSIBLY CAUSE BAD BURNS. CAUTION : OIL CONSUMPTION IS THE TERM USED FOR THE INTERNAL LOSS OF OIL FROM _______ BEARING SEALS AND AIR/OIL SEPARATOR DURING APU OPERATION. EXTERNAL LEAKS ARE NOT PERMITTED. YOU MUST CORRECT EXTERNAL LEAKS AND CLEAN THE APU, APU COMPARTMENT AND APU AIR INTAKE IMMEDIATELY IF CONTAMINATED. IF THE OIL CONSUMPTION IS HIGHER THAN THE GRAPH A LIMIT, OR THERE IS A SUDDEN INCREASE IN OIL CONSUMPTION, YOU MUST DO THE OIL CONSUMPTION MONITORING VERY CAREFULLY TO PREVENT BAD APU DAMAGE. 1. __________________ Reason for the Job Add oil to the APU oil reservoir, which is integral with the accessory drive gearbox (referred to as the gear box), - if the oil level check shows that you must add oil, - if the APU oil reservoir was drained, - if you prepare a replacement APU for installation. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No No No No
specific specific specific specific
circuit breaker(s) safety clip(s) warning notice container 3 l (0.7925 USgal) access platform 7.2 m (23 ft. 7 in.)
EFF : ALL 12-13-49 SROS
Page 301 Jan 01/05
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------No specific
lint-free cloth
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 29-00-00-864-804 R 49-91-00-600-801 12-13-49-991-001 12-13-49-991-002
Energize the Ground Service Network De-energize the Ground Service Network Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Oil Change Fig. 301 Fig. 302
3. __________ Job Set-up Subtask 12-13-49-860-050 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). (2) Make sure that the hydraulic systems are depressurized (Ref. TASK 29-00-00-864-804). (3) Put the warning notice in position on the panel 215VU to tell persons not to start the APU. NOTE : To get an accurate oil level indication, do not wait longer ____ than 5 to 15 minutes after APU shutdown before you do the APU oil level check.
EFF : ALL 12-13-49 SROS
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Subtask 12-13-49-865-050 R R
B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU APU FIRE SQUIB B 2WF P09 721VU APU FIRE VLV CTL 4WF P07 742VU APU START CTL 1KA C72 742VU APU FIRE SQUIB A 1WF J72 742VU APU FIRE VLV CTL 3WF J71 Subtask 12-13-49-010-050
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C. Get Access (1) Put the access platform in position below the APU compartment. (2) Open the APU access doors 315AL and 316AR and safety them in the open position. (3) Set the LIGHT switch 3LJ to the on position. 4. Procedure _________ Subtask 12-13-49-612-050 A. Add Oil to the APU Oil Reservoir (Ref. Fig. 301/TASK 12-13-49-991-001, 302/TASK 12-13-49-991-002) WARNING : USE THE CORRECT PERSONAL PROTECTION. OIL CAN HAVE AN ADDITIVE _______ CALLED TRICRESYL PHOSPHATE IN IT. THIS CHEMICAL IS AN ASPHYXIANT, IT IS POISONOUS AND CAN BE ABSORBED THROUGH THE SKIN. USE CARE WHEN ENGINE OIL IS DRAINED. HOT OIL CAN POSSIBLY CAUSE BAD BURNS. WARNING : DO NOT REMOVE OIL FILLER CAP WHEN OIL IS HOT AND OIL LEVEL IS _______ ABOVE ADD RANGE ON SIGHT GLASS. HOT OIL CAN CAUSE SEVERE BURNS. (1) Do an oil level check on the oil sight glass. NOTE : To get an accurate oil level indication, do not wait longer ____ than 5 to 15 minutes after APU shutdown before you do the APU oil level check.
EFF : ALL 12-13-49 SROS
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APU Oil-Servicing Ports Figure 301/TASK 12-13-49-991-001 EFF : ALL 12-13-49 SROS
Page 304 Apr 01/98
Guideline for Oil Consumption of GTCP 331-350 APUs In Service Figure 302/TASK 12-13-49-991-002 EFF : ALL 12-13-49 SROS
Page 305 Apr 01/98
If the oil level is at the FULL mark on the oil sight glass, do not add oil to the APU oil reservoir. (2) Put the container in position below the gearbox to collect oil leakage. (3) Make sure that the oil scupper and the oil filler cap are clean. Make them clean with a lint-free cloth, if they are dirty. (4) Open the oil filler cap. WARNING : DO NOT REMOVE OIL FILLER CAP WHEN OIL IS HOT AND OIL LEVEL _______ IS ABOVE ADD RANGE ON SIGHT GLASS. HOT OIL CAN CAUSE SEVERE BURNS. (a) Open the lock and slowly loosen the oil filler cap to release remaining pressure from the oil reservoir. (b) Remove the oil filler cap and make it dry with a lint-free cloth.
EFF : ALL 12-13-49 R SROS
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(5) Add the oil. WARNING : PUT THE OIL INTO THE GRAVITY-FILL PORT SLOWLY. THIS WILL _______ PREVENT A BLOW-BACK OF HOT OIL WHICH CAN BURN YOU. CAUTION : WHEN YOU DO THE SERVICING OF THE APU OIL RESERVOIR, MAKE _______ SURE YOU USE AN APPROVED ENGINE OIL OF THE SAME TYPE AND BRAND. IF YOU MIX DIFFERENT OILS YOU CAN DAMAGE THE APU. CAUTION : MAKE SURE OIL SERVICING STOPS WHEN GRAVITY-FILL CAP OPENING _______ STARTS TO OVERFLOW OR WHEN OIL FLOWS FROM PRESSURE SYSTEM OVERFILL FITTINGS. OVER-SERVICING CAN CAUSE FOAMING OF OIL WHICH CAN CAUSE LOP SHUTDOWN OF ENGINE. (a) Make sure that the oil-can(s) is(are) clean and the oil does not contain unwanted materials. (b) Use the following oil brands and types
R
-------------------------------------------------------------------------BRAND NAME OIL TYPE -------------------------------------------------------------------------AeroShell Turbine Oil 390 1 Castrol 325 1 Castrol 399 1 BP Exxon Turbo Oil 2389 1 -------------------------------------------------------------------------AeroShell Turbinen Oil 500 2 AeroShell 555 2 AeroShell Turbine Oil 560 2 Castrol Aero 5000 2 Castrol Aero 5050 2 Exxon/Esso Turbo Oil 25 2 Exxon/Esso Turbo Oil 2380 2 BP/Exxon Turbine Oil 2197 2 Hatco 3211 2 Hatco 3611 2 Mobil Jet Oil II 2 Mobil 254 2 Royco Turbine Oil 500 2 Royco 555 2 Royco Turbine Oil 560 2 Royco 899 2
EFF : ALL 12-13-49 SROS
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(c) Carefully add the oil until the oil level in the oil reservoir is at the FULL mark on the oil sight glass. NOTE : If the oil which is available for the oil servicing is of ____ a different type or brand than the oil which is in the APU oil reservoir, you can change the oil in the reservoir (Ref. TASK 49-91-00-600-801), or you apply the replenishment method approved by the OEM. Add the new approved oil to the reservoir as necessary, at each routine oil servicing interval, to complete the oil change.
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(6) Install and lock the oil filler cap. NOTE : Make sure that the oil filler cap is tight and locked ____ correctly. (7) Remove the oil from the oil scupper and make it dry with a lint-free cloth. (8) Remove the container. (9) If oil fell on the APU, the air intake duct and/or the adjacent area, remove it and make the area dry with a lint-free cloth. (10) Make an entry in the applicable logbook(s). (Ref. Fig. 302/TASK 12-13-49-991-002) CAUTION : OIL CONSUMPTION IS THE TERM USED FOR THE INTERNAL LOSS OF _______ OIL FROM BEARING SEALS AND AIR/OIL SEPARATOR DURING APU OPERATION. EXTERNAL LEAKS ARE NOT PERMITTED. YOU MUST CORRECT EXTERNAL LEAKS AND CLEAN THE APU, APU COMPARTMENT AND APU AIR INTAKE IMMEDIATELY IF CONTAMINATED. IF THE OIL CONSUMPTION IS HIGHER THAN THE GRAPH A LIMIT, OR THERE IS A SUDDEN INCREASE IN OIL CONSUMPTION, YOU MUST DO THE OIL CONSUMPTION MONITORING VERY CAREFULLY TO PREVENT BAD APU DAMAGE. (a) Make an entry in the applicable logbook(s) to tell people the quantity of the oil which you have added to the APU oil reservoir.
EFF : ALL 12-13-49 SROS
Page 308 Apr 01/02
5. Close-up ________ Subtask 12-13-49-410-050 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Set the LIGHT switch 3LJ to the off position. (3) Close the APU access doors 315AL and 316AR. (4) Remove the access platform(s). Subtask 12-13-49-865-051 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1KA, 1WF, 2WF, 3WF, 4WF Subtask 12-13-49-860-053 C. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801) (2) Remove the warning notice(s). (3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL 12-13-49 R SROS
Page 309 Jan 01/05
TASK 12-13-49-612-801- 01 Pressure Servicing of the APU Oil Reservoir WARNING : DO NOT TOUCH THE APU UNTIL IT IS SUFFICIENTLY COOL TO PREVENT BURNS _______ WHEN YOU DO THE MAINTENANCE TASK(S). WARNING : USE THE CORRECT PERSONAL PROTECTION. OIL CAN HAVE AN ADDITIVE CALLED _______ TRICRESYL PHOSPHATE IN IT. THIS CHEMICAL IS AN ASPHYXIANT, IT IS POISONOUS AND CAN BE ABSORBED THROUGH THE SKIN. USE CARE WHEN ENGINE OIL IS DRAINED. HOT OIL CAN POSSIBLY CAUSE BAD BURNS. CAUTION : OIL CONSUMPTION IS THE TERM USED FOR THE INTERNAL LOSS OF OIL FROM _______ BEARING SEALS AND AIR/OIL SEPARATOR DURING APU OPERATION. EXTERNAL LEAKS ARE NOT PERMITTED. YOU MUST CORRECT EXTERNAL LEAKS AND CLEAN THE APU, APU COMPARTMENT AND APU AIR INTAKE IMMEDIATELY IF CONTAMINATED. IF THE OIL CONSUMPTION IS HIGHER THAN THE GRAPH A LIMIT, OR THERE IS A SUDDEN INCREASE IN OIL CONSUMPTION, YOU MUST DO THE OIL CONSUMPTION MONITORING VERY CAREFULLY TO PREVENT BAD APU DAMAGE. 1. __________________ Reason for the Job Add oil to the APU oil reservoir, which is integral with the accessory drive gearbox (referred to as the gear box), - if the oil level check shows that you must add oil, - if the oil reservoir was drained, - if you prepare a replacement APU for installation. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific No specific No specific No specific DH13PM
circuit breaker(s) safety clip(s) warning notice container 10.0 l (2.6416 USgal) access platform 7.2 m (23 ft. 7 in.) 1 TANK - ENGINE OIL FILLING UP
EFF : ALL 12-13-49 SROS
Page 310 Jan 01/05
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------No specific
lint-free cloth
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 29-00-00-864-804 R 49-91-00-600-801 12-13-49-991-001 12-13-49-991-002
Energize the Ground Service Network De-energize the Ground Service Network Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Oil Change Fig. 301 Fig. 302
3. __________ Job Set-up Subtask 12-13-49-860-054 A. Aircraft Maintenance Configuration (1) Put the warning notice in position on the panel 215VU to tell persons not to start the APU. (2) Energize the ground service network (Ref. TASK 24-42-00-861-801). (3) Make sure that the hydraulic systems are depressurized (Ref. TASK 29-00-00-864-804).
EFF : ALL 12-13-49 SROS
Page 311 Jul 01/02
Subtask 12-13-49-865-054 R R
B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU APU FIRE SQUIB B 2WF P09 721VU APU FIRE VLV CTL 4WF P07 742VU APU START CTL 1KA C72 742VU APU FIRE SQUIB A 1WF J72 742VU APU FIRE VLV CTL 3WF J71 Subtask 12-13-49-010-055
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C. Get Access (1) Put the access platform in position below the APU compartment. (2) Open the APU access doors 315AL and 316AR and safety them in the open position. (3) Set the LIGHT switch 3LJ to the on position. 4. Procedure _________ Subtask 12-13-49-612-052 A. Add Oil to the APU Oil Reservoir (Ref. Fig. 301/TASK 12-13-49-991-001, 302/TASK 12-13-49-991-002) WARNING : USE THE CORRECT PERSONAL PROTECTION. OIL CAN HAVE AN ADDITIVE _______ CALLED TRICRESYL PHOSPHATE IN IT. THIS CHEMICAL IS AN ASPHYXIANT, IT IS POISONOUS AND CAN BE ABSORBED THROUGH THE SKIN. USE CARE WHEN ENGINE OIL IS DRAINED. HOT OIL CAN POSSIBLY CAUSE BAD BURNS. WARNING : DO NOT REMOVE OIL FILLER CAP WHEN OIL IS HOT AND OIL LEVEL IS _______ ABOVE ADD RANGE ON SIGHT GLASS. HOT OIL CAN CAUSE SEVERE BURNS. (1) Do an oil level check on the oil sight glass. NOTE : To get an accurate oil level indication, do not wait longer ____ than 5 to 15 minutes after APU shutdown before you do the APU oil level check.
EFF : ALL 12-13-49 SROS
Page 312 Apr 01/02
If the oil level is at the FULL mark on the oil sight glass, do not add oil to the APU oil reservoir. (2) Put the container in position below the gearbox to collect oil leakage. (3) Put the TANK - ENGINE OIL FILLING UP in position below the APU gearbox. R CAUTION : WHEN YOU DO THE SERVICING OF THE APU OIL RESERVOIR, MAKE _______ SURE YOU USE AN APPROVED ENGINE OIL OF THE SAME TYPE AND BRAND. IF YOU MIX DIFFERENT OILS YOU CAN DAMAGE THE APU. (a) Make sure that the TANK - ENGINE OIL FILLING UP is filled with clean and approved oil which is of the same type and brand than the oil which is in the APU oil reservoir. NOTE : If the oil which is in the TANK - ENGINE OIL FILLING UP is ____ of a different type or brand than the oil which is in the APU oil reservoir, you can change the oil in the TANK ENGINE OIL FILLING UP or in the APU oil reservoir (Ref. TASK 49-91-00-600-801) or you can apply the replenishment methode approved by the OEM. Add the new approved oil to the reservoir as necessary at each routine oil servicing interval to complete the oil change.
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Use the following oil brands and types
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-------------------------------------------------------------------------BRAND NAME OIL TYPE -------------------------------------------------------------------------AeroShell 390 1 Brayco 880 1
R R R
Castrol 325 Castrol 399
1 1
BP Exxon Turbo Oil 2389
1
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R R R R R R R R R R
-------------------------------------------------------------------------BRAND NAME OIL TYPE -------------------------------------------------------------------------AeroShell Turbine Oil 500 2 AeroShell Turbine Oil 555 2 AeroShell Turbine Oil 560 2 Castrol Aero 5000 2 Castrol Aero 5050 2 BP Exxon Turbo Oil 25 2 BP Exxon Turbo Oil 2380 2 Hatco Hatco Mobil Mobil Royco Royco Royco Royco
R
3211 3611 Jet Oil Jet Oil Turbine 555 Turbine 899
2 2 2 2 2 2 2 2
II 254 Oil 500 Oil 560
(4) Connect the overflow hose and the pressure fill hose. CAUTION : POINT THE OVERFLOW DRAIN HOSE IN A CORRECT CONTAINER WHEN _______ YOU CONNECT IT. (a) Clean the caps on the overflow port and the pressure fill port with a lint-free cloth and then remove them from the ports.
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(5) Clean the connectors of the overflow hose and the pressure fill hose with a lint-free cloth and make sure that they are serviceable. (a) Put the outlet of the overflow hose into the container. (b) Connect the overflow hose to the overflow port. (c) Connect the pressure fill hose to the pressure fill port.
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(6) Add oil. CAUTION : MAKE SURE OIL SERVICING STOPS WHEN GRAVITY-FILL CAP OPENING _______ STARTS TO OVERFLOW OR WHEN OIL FLOWS FROM PRESSURE SYSTEM OVERFILL FITTINGS. OVER-SERVICING CAN CAUSE FOAMING OF OIL WHICH CAN CAUSE LOP SHUTDOWN OF ENGINE. CAUTION : DO NOT OVERFILL APU RESERVOIR. TO REMOVE OVERFILL HOSE _______ BEFORE OIL HAS BECOME STABLE, OR PRESSURE-FILL WITHOUT OVERFILL HOSE VENTING, CAN CAUSE ENGINE DAMAGE.
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(a) Operate the TANK - ENGINE OIL FILLING UP (DH13PM) and slowly add oil until it flows from the overfill hose into the container. NOTE : Make sure that the outlet end of the overflow hose is ____ above the fluid level in the container and not blocked. Keep the overflow hose connected for approximately 2 minutes, after you have stopped to add the oil. This makes sure that the oil level in the APU oil reservoir becomes stable and the oil which was added too much is drained. R
(7) Disconnect the overflow hose and the pressure fill hose. (a) Remove the pressure fill hose from the pressure fill port. (b) Remove the overflow hose from the overflow port. (c) Clean the ports with a lint-free cloth. (d) Make sure that the caps are clean and in the correct condition and install them onto the ports. NOTE : Make sure that the caps on the pressure fill port and the ____ overflow port are installed correctly and tight.
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(8) Remove the TANK - ENGINE OIL FILLING UP.
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(9) Remove the container.
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(10) If oil fell on the APU, the air intake duct and/or the adjacent area during the oil servicing, remove it and make the area dry with a lint-free cloth.
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(11) Make an entry in the applicable logbook(s). (Ref. Fig. 302/TASK 12-13-49-991-002) CAUTION : OIL CONSUMPTION IS THE TERM USED FOR THE INTERNAL LOSS OF _______ OIL FROM BEARING SEALS AND AIR/OIL SEPARATOR DURING APU OPERATION. EXTERNAL LEAKS ARE NOT PERMITTED. YOU MUST CORRECT EXTERNAL LEAKS AND CLEAN THE APU, APU COMPARTMENT AND APU AIR INTAKE IMMEDIATELY IF CONTAMINATED. IF THE OIL CONSUMPTION IS HIGHER THAN THE GRAPH A LIMIT, OR THERE IS A SUDDEN INCREASE IN OIL CONSUMPTION, YOU MUST DO THE OIL CONSUMPTION MONITORING VERY CAREFULLY TO PREVENT BAD APU DAMAGE.
EFF : ALL 12-13-49 SROS
Page 315 Apr 01/02
(a) Make an entry in the applicable logbook(s) to tell people the quantity of the oil which you have added to the APU oil reservoir. 5. Close-up ________ Subtask 12-13-49-410-054 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Set the LIGHT switch 3LJ to the off position. (3) Close the APU access doors 315AL and 316AR. (4) Remove the access platform(s). Subtask 12-13-49-865-055 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1KA, 1WF, 2WF, 3WF, 4WF Subtask 12-13-49-410-055 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access door 811. (3) Remove the access platform(s). Subtask 12-13-49-860-055 D. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801) (2) Remove the warning notice(s). (3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL 12-13-49 R SROS
Page 316 Apr 01/02
ENGINE OIL - SERVICING ______________________ TASK 12-13-79-610-806 Servicing of the Engine Oil System WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE AFTER THE ENGINE IS SHUTDOWN. _______ THE ENGINE CAN STAY HOT FOR A LONG TIME AFTER THE ENGINE IS SHUTDOWN. WARNING : USE PROTECTIVE CLOTHING WHEN YOU USE ENGINE OIL. OIL CAN CAUSE SKIN _______ IRRITATION. CAUTION : YOU MUST EXAMINE THE OIL LEVEL BETWEEN 15 MINUTES AND 2 HOURS AFTER _______ SHUTDOWN. IF YOU DO NOT, THE OIL LEVEL SIGHTGLASS INDICATION WILL NOT BE ACCURATE. CAUTION : DO NOT OPERATE THE ENGINE WITHOUT SUFFICIENT OIL. THIS WILL CAUSE A _______ POSSIBLE INFLIGHT SHUTDOWN AND POSSIBLE DAMAGE TO THE ENGINE. CAUTION : YOU MUST DO THIS SERVICING PROCEDURE TO PREVENT TOO MUCH OIL IN THE _______ OIL SYSTEM. DO NOT OPERATE THE ENGINE WITH TOO MUCH OIL. THIS WILL CAUSE A POSSIBLE IN FLIGHT SHUTDOWN AND POSSIBLE DAMAGE TO THE ENGINE. CAUTION : DO NOT LET ENGINE FUEL OR OIL FALL ON THE ENGINE. YOU MUST _______ IMMEDIATELY REMOVE UNWANTED FUEL OR OIL WITH A CLOTH. THE FUEL OR OIL CAN CAUSE DAMAGE TO SOME ENGINE PARTS. CAUTION : OPERATORS MUST MAKE SURE THE OIL TANK _______ GOOD WORKING ORDER PRIOR TO OPERATING FLAPPER VALVE. IF YOU DO NOT DO THIS, INFLIGHT SHUTDOWN AND POSSIBLE DAMAGE
CAP IS SECURELY LATCHED AND IN WITH A DAMAGED OR BROKEN IT WILL CAUSE A POSSIBLE TO THE ENGINE.
1. __________________ Reason for the Job To make a check of the engine oil level. To fill the engine oil system to get the correct oil level. NOTE : Do not use this servicing task for filling the engine oil system ____ after the replacement of an oil system component. To fill the engine oil system after the replacement of an oil system component (Ref. TASK 12-13-79-610-80700). NOTE : Do not use this servicing task for changing the engine oil. To change ____ the engine oil (Ref. TASK 12-13-79-610-80800).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-79 Page 301 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
NOTE : If you see black oil in the oil system, refer to Inspection for ____ Black Oil (Ref. TASK 79-00-00-280-80400). Black oil may be an indication of a serious problem or it can be a condition that requires no maintenance action. If you notice a damaged or broken oil tank flapper valve during servicing the following conditions apply. NOTE : It is permitted to fly with a damaged valve if: ____ - The flapper valve is replaced at the next visit to a maintenance facility, not to exceed 5 cycles. - The damaged or broken flapper valve does not pose a risk of contamination of the oil system. - The engine is not experiencing oil loss due to oil leakage from the oil tank cap or flapper valve. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No
specific specific specific specific specific specific specific specific
circuit breaker(s) safety clip(s) drain hose dust cover flashlight pressure fill service unit fluid drain collector/container 10 USgal (37.8544 l) access platform 2.5 m (8 ft. 2 in.) adjustable access platform 3.7 m (12 ft. 2 in.)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
P03-001
Material No.
P05-005
Material No.
P05-421
Material No.
P05-422
* oil, lubricating, turbine engine (Ref. 70-30-00) * cloth, cotton, lint free (Ref. 70-30-00) * Nylon Pads and Rolls, Abrasive impregnated (Ref. 70-30-00) *
R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-79 Page 302 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Scrub Pad (Ref. 70-30-00) C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 70-57-00-910-802 71-00-00-720-816 12-13-79-991-006
Energize the Ground Service Network De-energize the Ground Service Network Degreasing of Parts by Solvent Wipe (SPOP 208) Test No. 2 - Engine Motor Leak Test (Dry Method) Thrust Reverser Cowl Doors Open Fig. 301
3. __________ Job Set-up Subtask 12-13-79-861-055 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-79-941-055 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure. Subtask 12-13-79-010-062 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU.
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Subtask 12-13-79-865-060 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-13-79-010-063 E. Get Access (1) Open the upper left thrust reverser access door: - FOR 4030EM1 417DL - FOR 4030EM2 427DL (2) Put the adjustable access platform in position. 4. Procedure _________ (Ref. Fig. 301/TASK 12-13-79-991-006) Subtask 12-13-79-210-052 A. Make a Check of the Engine Oil Level WARNING : IT IS NOT NECESSARY TO REMOVE THE OIL TANK CAP TO EXAMINE THE _______ OIL LEVEL. IF YOU DO NEED TO REMOVE THE OIL TANK CAP, YOU MUST WAIT A MINIMUM OF 5 MINUTES AFTER SHUTDOWN TO LET THE OIL PRESSURE BLEED OFF. THE HOT OIL CAN BURN YOUR EYES AND SKIN. CAUTION : YOU MUST EXAMINE THE OIL LEVEL BETWEEN 15 MINUTES AND 2 HOURS _______ AFTER SHUTDOWN. IF YOU DO NOT, THE OIL LEVEL SIGHTGLASS INDICATION WILL NOT BE ACCURATE.
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Engine Oil System Level Servicing Figure 301/TASK 12-13-79-991-006 R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-79 Page 305 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
(1) Examine the oil level between 15 minutes and 2 hours of shutdown. If the engine shutdown was more than two hours ago, you must dry motor the engine so that the engine oil pressure is stable (Ref. TASK 7100-00-720-816). This is necessary so that the oil in the system returns to the oil tank and so that the level indication is accurate. (2) Use a flashlight and find the engine oil level sightglass on the oil tank. (3) If necessary, clean the sightglass with one of the methods as follows: (a) Use a cloth, cotton, lint free (Material No. P05-005) and wipe the sightglass so that it is clean. (b) Or Use SPOP 208 (Ref. TASK 70-57-00-910-802) with Nylon Pads and Rolls, Abrasive impregnated (Material No. P05-421) a or Scrub Pad (Material No. P05-422) to clean the sightglass so that it is clean. (4) Examine the oil level in the sightglass as follows: CAUTION : YOU MUST EXAMINE THE OIL LEVEL BETWEEN 15 MINUTES AND 2 _______ HOURS AFTER SHUTDOWN. IF YOU DO NOT, THE OIL LEVEL SIGHTGLASS INDICATION WILL NOT BE ACCURATE. (a) If the oil level is in the green area, do not add oil and close the access door: - FOR 4030EM1 417DL FOR 4030EM2 427DL (b) If the oil level is below the green area, service the engine oil system as follows. NOTE : The oil can expand from heat during engine operation. This ____ can cause the oil level indication to be above the full mark. This is acceptable. NOTE : If the aircraft is not parked level, the oil level ____ indication in the sightglass is affected and may be above the full mark. This is acceptable.
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Subtask 12-13-79-610-054 B. Service the Engine Oil System (Without Pressure Fill Equipment) WARNING : BEFORE YOU REMOVE THE OIL TANK CAP, YOU MUST WAIT A MINIMUM OF _______ 5 MINUTES AFTER SHUTDOWN TO LET THE OIL PRESSURE BLEED OFF. THE HOT OIL CAN BURN YOUR EYES AND SKIN. WARNING : DO NOT OPEN THE OIL TANK CAP IF THE SIGHTGLASS OIL INDICATION _______ IS ABOVE THE FULL MARK. IF YOU DO OPEN THE CAP WHEN THE OIL IS ABOVE FULL, THE HOT OIL WILL SPILL FROM THE FILLER OPENING. THE HOT OIL CAN BURN YOUR EYES AND SKIN. (1) Wait a minimum of five minutes after shutdown before you open the oil tank cap. (2) Loosen and remove the oil tank cap only if the oil level in the sightglass is below the green area. (3) Add the oil: CAUTION : WE RECOMMEND THAT YOU DO NOT MIX DIFFERENT BRANDS OF OIL. _______ IF YOU DO, ENGINE DAMAGE CAN BE THE RESULT. (a) Add the correct oil, lubricating, turbine engine (Material No. P03-001) into the filler neck until no more oil can be added without overflow into the scupper drain. NOTE : It is permitted to mix different brands of oil when you ____ service the engine oil system as specified in Service Bulletin N⁰. 238. NOTE : The stable oil level in the sightglass will now be in the ____ green area. NOTE : If the aircraft is not parked level, the oil level ____ indication in the sightglass is affected and may be above the full mark. This is acceptable. The oil system is serviced correctly if no more oil can be added without overflow into the scupper drain. (4) Install the oil tank cap as follows: (a) With the handle at open, align and install the cap to the filler neck. (b) Push down on the cap and turn the handle clockwise to close.
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(c) Push the handle into the cap to lock the cap. (d) Make sure that the cap is installed equally and completely. (5) Close the upper thrust reverser access door: - FOR 4030EM1 417DL - FOR 4030EM2 427DL. (6) Write the amount of oil that you added. Subtask 12-13-79-610-055 C. Service the Engine Oil System (With Pressure Fill Equipement): WARNING : DO NOT OPEN THE OIL TANK CAP IF THE SIGHTGLASS OIL INDICATION _______ IS ABOVE THE FULL MARK. IF YOU DO OPEN THE CAP WHEN THE OIL IS ABOVE FULL, THE HOT OIL WILL SPILL FROM THE FILLER OPENING. THE HOT OIL CAN BURN YOUR EYES AND SKIN. (1) Do not open the oil tank cap for this pressure fill procedure. (2) Lift the lever and remove the dust cover from the oil pressure fill valve. (3) Drain the hose: WARNING : YOU MUST CONNECT THE DRAIN HOSE TO THE OVERFLOW DRAIN _______ CONNECTOR AND PUT THE DRAIN HOSE INTO A COLLECTOR/CONTAINER BEFORE YOU CONNECT THE PRESSURE FILL HOSE TO THE ENGINE OIL FILL CONNECTOR. MAKE THE DRAIN HOSE HANG STRAIGHT DOWN. MAKE SURE THAT THE HOSE IS ABOVE AND NOT INTO THE FLUID IN THE COLLECTOR/CONTAINER. WHEN YOU CONNECT THE PRESSURE FILL HOSE, THE DRAIN CONNECTOR (LINE) OPENS AUTOMATICALLY AND RELEASES THE PRESSURE IN THE OIL SYSTEM. WHEN YOU RELEASE THE PRESSURE, OIL AND AIR CAN SPRAY FROM THE OVERFLOW CONNECTOR. (a) Put the drain hose into the fluid drain collector/container and make sure that the end of the hose is not in the fluid. (4) Connect the drain hose to the (larger) overflow connector before you connect the pressure fill hose. NOTE : Some oil can come out of the overflow connector if you connect ____ the pressure fill hose first.
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(5) Connect the pressure fill hose from the pressure fill service unit to the (smaller) pressure fill connector. (6) Add the oil: CAUTION : DO NOT MIX TYPES OF OIL WHEN YOU ADD OR REPLACE THE ENGINE _______ OIL. (a) Use the pressure fill service unit and add the correct oil, lubricating, turbine engine (Material No. P03-001) at a maximum pressure of 100 psi (6.8947 bar). (7) Fill the oil tank until oil comes out the drain hose. NOTE : If the aircraft is not parked level, the oil level indication ____ in the sightglass is affected and may be above the full mark. This is acceptable. The oil system is serviced correctly if no more oil can be added without overflow from the drain hose. NOTE : The oil fill pressure connector has a restrictor so that the ____ rate of oil pressure fill is less then the rate of the gravity drain. This prevents you from putting too much oil in the system. (8) Remove the pressure hose from the pressure fill valve. (9) After the oil drains, remove the drain hose. (10) Install the dust cover to the pressure fill valve assembly and turn the handle to lock the cover. (11) Close the upper thrust reverser access door: - FOR 4030EM1 417DL - FOR 4030EM2 427DL. (12) Write the amount of oil that you added.
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5. Close-up ________ Subtask 12-13-79-865-061 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2 Subtask 12-13-79-410-058 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Close the access door 811. (4) Remove the access platform(s). Subtask 12-13-79-862-065 C. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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TASK 12-13-79-610-807 Filling the Engine Oil System after the Replacement of an Oil System Component WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE AFTER THE ENGINE IS SHUTDOWN. _______ THE ENGINE CAN STAY HOT FOR A LONG TIME AFTER THE ENGINE IS SHUTDOWN. WARNING : USE PROTECTIVE CLOTHING WHEN YOU USE ENGINE OIL. OIL CAN CAUSE SKIN _______ IRRITATION. CAUTION : DO NOT OPERATE THE ENGINE WITHOUT SUFFICIENT OIL. THIS WILL CAUSE A _______ POSSIBLE INFLIGHT SHUTDOWN AND POSSIBLE DAMAGE TO THE ENGINE. CAUTION : YOU MUST DO THIS SERVICING PROCEDURE TO PREVENT TOO MUCH OIL IN THE _______ OIL SYSTEM. DO NOT OPERATE THE ENGINE WITH TOO MUCH OIL. THIS WILL CAUSE A POSSIBLE IN FLIGHT SHUTDOWN AND POSSIBLE DAMAGE TO THE ENGINE. CAUTION : DO NOT LET ENGINE FUEL OR OIL FALL ON THE ENGINE. YOU MUST _______ IMMEDIATELY REMOVE UNWANTED FUEL OR OIL WITH A CLOTH. THE FUEL OR OIL CAN CAUSE DAMAGE TO SOME ENGINE PARTS. CAUTION : DO NOT MOTOR THE ENGINE WITHOUT OIL IN THE OIL TANK. IF THE OIL WAS _______ DRAINED DURING MAINTENANCE, YOU WILL FILL THE TANK BEFORE YOU MOTOR THE ENGINE. IF YOU DO NOT DO THIS, DAMAGE TO THE ENGINE CAN OCCUR. 1. __________________ Reason for the Job To fill the engine oil system after the replacement of an oil system component. NOTE : Do not use this filling task for normal servicing of the engine oil. ____ To service the engine oil system for normal maintenance (Ref. TASK 12-13-79-610-80600). NOTE : Do not use this filling task for changing the engine oil. To change ____ the engine oil (Ref. TASK 12-13-79-610-80800). NOTE : If the engine oil tank was not drained, begin this task in step 4. C. ____ NOTE : If you see black oil in the oil system, refer to Inspection for ____ Black Oil (Ref. TASK 79-00-00-280-80400). Black oil may be an indication of a serious problem or it can be a condition that requires no maintenance action.
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2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No
specific specific specific specific specific specific
circuit breaker(s) safety clip(s) drain hose pressure fill service unit adjustable access platform 1.22 m (4 ft.) fluid drain container 10 USgal (37.8544 l) access platform 2.5 m (8 ft. 2 in.)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
P03-001
* oil, lubricating, turbine engine (Ref. 70-30-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-13-79-610-806 24-42-00-861-801 24-42-00-862-801 71-00-00-720-816 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801 78-30-00-040-804 78-30-00-410-801 78-30-00-440-804 12-13-79-991-007
Servicing of the Engine Oil System Energize the Ground Service Network De-energize the Ground Service Network Test No. 2 - Engine Motor Leak Test (Dry Method) Thrust Reverser Cowl Doors Open Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Deactivation of the Thrust Reverser for Maintenance Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Reactivation of the Thrust Reverser after Maintenance Fig. 302
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3. __________ Job Set-up Subtask 12-13-79-860-050 A. Aircraft Maintenance Configuration (1) Make sure that the ground service network is energized (Ref. TASK 24-42-00-861-801). (2) Make sure that the engine 1, (2) shut-down occurred not less than 5 minutes before you do this procedure. Subtask 12-13-79-010-088 B. Get Access (1) Make sure that the access platform is in position at the access door 811. (2) Make sure that the access door 811 is open. (3) Make sure that the protective door of the AC/DC emergency power center 740VU is open. (4) Make sure that the left and right aft fan cowl doors is open: (Ref. TASK 71-13-00-010-802) - FOR 4030EM1 415BL, 416BR - FOR 4030EM2 425BL, 426BR (5) Make sure that the left thrust reverser is open: (Ref. TASK 78-30-00010-801) - FOR 4030EM1 417AL - FOR 4030EM2 427AL (6) Make sure that the adjustable access platform is in position. Subtask 12-13-79-040-056 C. Make sure that the thrust reverser is unserviceable (Ref. TASK 78-30-00040-804)
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Subtask 12-13-79-865-063 D. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 4. Procedure _________ (Ref. Fig. 302/TASK 12-13-79-991-007) Subtask 12-13-79-610-067 A. If the oil tank was drained during maintenance, fill the oil tank (without pressure fill equipment) as follows: NOTE : If you use the pressure fill equipment go to step B. ____ (1) Loosen and remove the oil tank cap. (2) Add the engine oil: CAUTION : WE RECOMMEND THAT YOU DO NOT MIX DIFFERENT BRANDS OF OIL. _______ IF YOU DO, ENGINE DAMAGE CAN BE THE RESULT. (a) Add the correct oil, lubricating, turbine engine (Material No. P03-001) into the filler neck until no more oil can be added without overflow into the scupper drain. NOTE : It is permitted to mix different brands of oil when you ____ service the engine oil system as specified in Service Bulletin No. 238. NOTE : The stable oil level in the sightglass will now be in the ____ green area.
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Engine Oil Filling after Replacement of an Oil System Component Figure 302/TASK 12-13-79-991-007 R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-79 Page 315 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
NOTE : If the aircraft is not parked level, the oil level ____ indication in the sightglass is affected. The oil engine system is serviced correctly if no more oil can be added without overflow into the scupper drain. (3) Install the oil tank cap as follows: (a) With the handle at open, align and install the cap to the filler neck (b) Push down on the cap and turn the handle clockwise to close (c) Push the handle into the cap to lock the cap (d) Make sure that the cap is installed equally and completely. (4) Write the amount of oil that you added. Subtask 12-13-79-610-068 B. If the oil tank was drained during maintenance, fill the oil tank (with pressure fill equipment) as follows: (1) If removed, install the oil tank cap for this pressure fill procedure as follows: (a) With the handle at open, align and install the cap to the filler neck (b) Push down on the cap and turn the handle clockwise to close (c) Push the handle into the cap to lock the cap (d) Make sure that the cap is installed equally and completely. (2) Lift the lever and remove the dust cover from the oil pressure fill valve.
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(3) Install and connect the drain hose: WARNING : YOU MUST CONNECT THE DRAIN HOSE TO THE OVERFLOW DRAIN _______ CONNECTOR AND PUT THE DRAIN HOSE INTO A COLLECTOR/CONTAINER BEFORE YOU CONNECT THE PRESSURE FILL HOSE TO THE ENGINE OIL FILL CONNECTOR. MAKE THE DRAIN HOSE HANG STRAIGHT DOWN. MAKE SURE THAT THE HOSE IS ABOVE AND NOT INTO THE FLUID IN THE COLLECTOR/CONTAINER. WHEN YOU CONNECT THE PRESSURE FILL HOSE, THE DRAIN CONNECTOR (LINE) OPENS AUTOMATICALLY AND RELEASES THE PRESSURE IN THE OIL SYSTEM. WHEN YOU RELEASE THE PRESSURE, OIL AND AIR CAN SPRAY FROM THE OVERFLOW CONNECTOR. (a) Put the drain hose into the fluid drain container and make sure that the end of the hose is not in the fluid. (4) Connect the drain hose to the (larger) overflow connector before you connect the pressure fill hose. NOTE : Some oil can come out of the overflow connector if you connect ____ the pressure fill hose first. (5) Connect the pressure fill hose from the pressure fill service unit to the (smaller) pressure fill connector. (6) Add the engine oil: CAUTION : WE RECOMMEND THAT YOU DO NOT MIX DIFFERENT BRANDS OF OIL. _______ IF YOU DO, ENGINE DAMAGE CAN BE THE RESULT. (a) Use the pressure fill service unit and add the correct oil, lubricating, turbine engine (Material No. P03-001) at a maximum pressure of 100 psi (6.90 bar). (7) Fill the oil tank until oil comes out the drain hose. NOTE : It is permitted to mix different brands of oil when you ____ service the engine oil system as specified in Service Bulletin No. 238. NOTE : The oil fill pressure connector has a restrictor so that the ____ rate of oil pressure fill is less than the rate of the gravity drain. This prevents you from putting too much oil in the system. NOTE : If the aircraft is not parked level, the oil level indication ____ in the sightglass is affected. The engine oil system is
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serviced correctly if no more oil can be added without overflow from the drain hose. (8) Remove the pressure hose from the pressure fill valve. (9) After the oil drains, remove the drain hose. (10) Install the dust cover to the pressure fill valve assembly and turn the handle to lock the cover. (11) Write the amount of oil that you added. Subtask 12-13-79-410-075 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the left thrust reverser: (Ref. TASK 78-30-00-410-801) - FOR 4030EM1 417AL - FOR 4030EM2 427AL Subtask 12-13-79-865-062 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2 Subtask 12-13-79-700-050 E. Turn the engine: CAUTION : DO NOT OPERATE THE ENGINE. YOU CAN ONLY TURN THE ENGINE WITH _______ THE STARTER LONG ENOUGH TO: - PUMP THE OIL INTO THE OIL TANK - REMOVE ANY UNWANTED AIR FROM THE OIL SYSTEM. (1) Turn (dry motor) the power plant so that the engine oil pressure is stable (Ref. TASK 71-00-00-720-816). NOTE : Do not exceed 5 minutes of starter operation. ____
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Subtask 12-13-79-865-086 F. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-13-79-010-089 G. Get Access (1) Open the left thrust reverser: (Ref. TASK 78-30-00-010-801) - FOR 4030EM1 417AL - FOR 4030EM2 427AL Subtask 12-13-79-610-056 H. Fill the Engine Oil System (Without Pressure Fill Equipment) NOTE : If you use pressure fill equipment go to step J. ____ (1) Loosen and remove the oil tank cap. (2) Add the engine oil: CAUTION : DO NOT MIX TYPES OF OIL WHEN YOU ADD OR REPLACE THE ENGINE _______ OIL. (a) Add the correct oil, lubricating, turbine engine (Material No. P03-001) into the filler neck until no more oil can be added without overflow into the scupper drain. NOTE : The stable oil level in the sightglass will now be in the ____ green area. NOTE : If the aircraft is not parked level, the oil level ____ indication in the sightglass is affected. The oil engine
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system is serviced correctly if no more oil can be added without overflow into the scupper drain. (3) Install the oil tank cap as follows: (a) With the handle at open, align and install the cap to the filler neck (b) Push down on the cap and turn the handle clockwise to close (c) Push the handle into the cap to lock the cap (d) Make sure that the cap is installed equally and completely. (4) Write the amount of oil that you added. Subtask 12-13-79-610-057 J. Fill the Engine Oil System (With Pressure Fill Equipment) (1) If removed, install the oil tank cap for this pressure fill procedure as follows: (a) With the handle at open, align and install the cap to the filler neck (b) Push down on the cap and turn the handle clockwise to close (c) Push the handle into the cap to lock the cap (d) Make sure that the cap is installed equally and completely. (2) Lift the lever and remove the dust cover from the oil pressure fill valve. (3) Install and connect the drain hose: WARNING : YOU MUST CONNECT THE DRAIN HOSE TO THE OVERFLOW DRAIN _______ CONNECTOR AND PUT THE DRAIN HOSE INTO A COLLECTOR/CONTAINER BEFORE YOU CONNECT THE PRESSURE FILL HOSE TO THE ENGINE OIL FILL CONNECTOR. MAKE THE DRAIN HOSE HANG STRAIGHT DOWN. MAKE SURE THAT THE HOSE IS ABOVE AND NOT INTO THE FLUID IN THE COLLECTOR/CONTAINER. WHEN YOU CONNECT THE PRESSURE FILL HOSE, THE DRAIN CONNECTOR (LINE) OPENS AUTOMATICALLY AND RELEASES THE PRESSURE IN THE OIL SYSTEM. WHEN YOU RELEASE THE PRESSURE, OIL AND AIR CAN SPRAY FROM THE OVERFLOW CONNECTOR.
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(a) Put the drain hose into the fluid drain container and make sure that the end of the hose is not in the fluid. (4) Connect the drain hose to the (larger) overflow connector before you connect the pressure fill hose. NOTE : Some oil can come out of the overflow connector if you connect ____ the pressure fill hose first. (5) Connect the pressure fill hose from the pressure fill service unit to the (smaller) pressure fill connector. (6) Add the engine oil: CAUTION : WE RECOMMEND THAT YOU DO NOT MIX DIFFERENT BRANDS OF OIL. _______ IF YOU DO, ENGINE DAMAGE CAN BE THE RESULT. (a) Use the pressure fill service unit and add the correct oil, lubricating, turbine engine (Material No. P03-001) at a maximum pressure of 100 psi (6.90 bar). (7) Fill the oil tank until oil comes out the drain hose. NOTE : It is permitted to mix different brands of oil when you ____ service the engine oil system as specified in Service Bulletin No. 238. NOTE : The oil fill pressure connector has a restrictor so that the ____ rate of oil pressure fill is less than the rate of the gravity drain. This prevents you from putting too much oil in the system. NOTE : If the aircraft is not parked level, the oil level indication ____ in the sightglass is affected. The engine oil system is serviced correctly if no more oil can be added without overflow from the drain hose. (8) Remove the pressure hose from the pressure fill valve. (9) After the oil drains, remove the drain hose. (10) Install the dust cover to the pressure fill valve assembly and turn the handle to lock the cover. (11) Write the amount of oil that you added.
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Subtask 12-13-79-410-076 K. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the left thrust reverser: (Ref. TASK 78-30-00-410-801) - FOR 4030EM1 417AL - FOR 4030EM2 427AL Subtask 12-13-79-865-064 L. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2 Subtask 12-13-79-700-051 M. Turn (dry motor) the power plant so that the engine oil pressure is stable (Ref. TASK 71-00-00-720-816). NOTE : Do not exceed 5 minutes of starter operation. ____ Subtask 12-13-79-610-058 N. Service the engine oil system again. See servicing of the engine oil system (Ref. TASK 12-13-79-610-806). 5. Close-up ________ Subtask 12-13-79-440-056 A. Make the thrust reverser serviceable (Ref. TASK 78-30-00-440-804)
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Subtask 12-13-79-410-077 B. Close Access (1) Close the left and right aft fan cowl doors: (Ref. TASK 71-13-00-410802) - FOR 4030EM1 415BL, 416BR - FOR 4030EM2 425BL, 426BR (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Close the access door 811. (4) Remove the access platform(s). Subtask 12-13-79-862-064 C. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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TASK 12-13-79-610-808 Changing the Oil in the Engine Oil System WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE AFTER THE ENGINE IS SHUTDOWN. _______ THE ENGINE CAN STAY HOT FOR A LONG TIME AFTER THE ENGINE IS SHUTDOWN. WARNING : USE PROTECTIVE CLOTHING WHEN YOU USE ENGINE OIL. OIL CAN CAUSE SKIN _______ IRRITATION. CAUTION : DO NOT OPERATE THE ENGINE WITHOUT SUFFICIENT OIL. THIS WILL CAUSE A _______ POSSIBLE INFLIGHT SHUTDOWN AND POSSIBLE DAMAGE TO THE ENGINE. CAUTION : YOU MUST DO THIS SERVICING PROCEDURE TO PREVENT TOO MUCH OIL IN THE _______ OIL SYSTEM. DO NOT OPERATE THE ENGINE WITH TOO MUCH OIL. THIS WILL CAUSE A POSSIBLE IN FLIGHT SHUTDOWN AND POSSIBLE DAMAGE TO THE ENGINE. CAUTION : DO NOT LET ENGINE FUEL OR OIL FALL ON THE ENGINE. YOU MUST _______ IMMEDIATELY REMOVE UNWANTED FUEL OR OIL WITH A CLOTH. THE FUEL OR OIL CAN CAUSE DAMAGE TO SOME ENGINE PARTS. 1. __________________ Reason for the Job To change the engine oil. NOTE : Do not use this oil changing task for normal servicing of the engine ____ oil. To service the engine oil system for normal maintenance (Ref. TASK 12-13-79-610- 80600). NOTE : Do not use this oil changing task for filling the engine with oil ____ after replacement on an oil system component. To fill the oil the engine oil system after the replacement of an oil system component (Ref. TASK 12-13-79-610-80700). NOTE : If you see black oil in the oil system, refer to Inspection for ____ Black Oil (Ref. TASK 79-00-00-280-80400). Black oil may be an indication of a serious problem or it can a condition that requires no maintenance action.
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2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No
specific specific specific specific specific specific specific
circuit breaker(s) safety clip(s) drain hose pressure fill service unit adjustable access platform 1.22 m (4 ft.) fluid drain container 10 USgal (37.8544 l) access platform 2.5 m (8 ft. 2 in.) Torque Wrench : range 36.00 to 220.00 lbf.in (0.40 to 2.60 m.daN)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
P03-001
Material No.
P11-027
* oil, lubricating, turbine engine (Ref. 70-30-00) * solvent, petroleum (Ref. 70-30-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------3
packing
72-62-11 43 -060
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D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-13-79-610-806 24-42-00-861-801 24-42-00-862-801 71-00-00-720-816 71-13-00-010-802 71-13-00-410-802 72-34-13-000-801 72-34-13-400-801 78-30-00-010-801 78-30-00-040-804 78-30-00-410-801 78-30-00-440-804 79-21-22-000-801 79-21-22-400-801 79-22-11-000-801 79-22-11-400-801 12-13-79-991-008 12-13-79-991-009
Servicing of the Engine Oil System Energize the Ground Service Network De-energize the Ground Service Network Test No. 2 - Engine Motor Leak Test (Dry Method) Thrust Reverser Cowl Doors Open Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Removal of the Fan Exit Liner (Inner) Segments Installation of the Fan Exit Liner (Inner) Segments Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Deactivation of the Thrust Reverser for Maintenance Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Reactivation of the Thrust Reverser after Maintenance Removal of the Main Oil Filter Element (5010EN) Installation of the Main Oil Filter Element (5010EN) Removal of the Magnetic Chip Detectors (5006EN) Installation of the Magnetic Chip Detectors (5006EN) Fig. 303 Fig. 304
3. __________ Job Set-up Subtask 12-13-79-861-064 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-79-941-064 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure.
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Subtask 12-13-79-010-085 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU. Subtask 12-13-79-865-065 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-13-79-010-086 E. Get Access (1) Open the left and right aft fan cowl doors: (Ref. TASK 71-13-00-010802) - FOR 4030EM1 415BL, 416BR - FOR 4030EM2 425BL, 426BR Subtask 12-13-79-040-055 F. Make the thrust reverser unserviceable (Ref. TASK 78-30-00-040-804)
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Subtask 12-13-79-010-087 G. Get Access (1) Open the left and right thrust reverser: (Ref. TASK 78-30-00-010-801) - FOR 4030EM1 417AL, 418AR - FOR 4030EM2 427AL, 428AR (2) Put the adjustable access platform in position. 4. Procedure _________ (Ref. Fig. 303/TASK 12-13-79-991-008, 304/TASK 12-13-79-991-009) Subtask 12-13-79-680-052 A. Drain the oil from the engine oil system WARNING : BEFORE YOU REMOVE THE OIL TANK CAP, YOU MUST WAIT A MINIMUM OF _______ 5 MINUTES AFTER SHUTDOWN TO LET THE OIL PRESSURE BLEED OFF. THE HOT OIL CAN BURN YOUR EYES AND SKIN. WARNING : DO NOT OPEN THE OIL TANK CAP IF THE SIGHTGLASS OIL INDICATION _______ IS ABOVE THE FULL MARK. IF YOU DO OPEN THE CAP WHEN THE OIL IS ABOVE FULL, THE HOT OIL WILL SPILL FROM THE FILLER OPENING. THE HOT OIL CAN BURN YOUR EYES AND SKIN. CAUTION : INSTALL PROTECTION COVERS OVER ALL OPENINGS AS SOON AS POSSIBLE _______ TO PREVENT ENGINE DAMAGE. CAUTION : DO NOT MOTOR THE ENGINE WHEN THE ENGINE OIL IS DRAINED. IF IT _______ IS MOTORED WITHOUT ANY OIL, DAMAGE TO THE ENGINE CAN OCCUR. (1) Wait a minimum of five minutes after shutdown before you open the oil tank cap. (2) Loosen and remove the oil tank cap. NOTE : Some hot oil can drain out of the filler neck if the oil level ____ is above the full mark on the oil level sightglass. (3) Drain the oil tank as follows: (a) Remove the magnetic chip detector from the oil tank and let the oil drain (Ref. TASK 79-22-11-000-801).
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Engine Oil Changing Figure 303/TASK 12-13-79-991-008 R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-79 Page 329 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
Engine Oil Changing Figure 304/TASK 12-13-79-991-009 R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-79 Page 330 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
(4) Install oil tank cap loosely as follows: (a) Put the oil tank cap over the fill opening (b) Do not push and engage the cap to the filler neck (c) Do not turn and lock the cap in position. NOTE : This prevents dirt and dust in the oil tank. ____ (5) Remove the magnetic chip detector from the front of the main gearbox and let the oil drain (Ref. TASK 79-22-11-000-801). NOTE : You must remove the detail probe and the valve from the main ____ gearbox. (6) Drain the angle gearbox as follows: (a) Remove the fan exit liner segment (inner) at 6 oclock position (Ref. TASK 72-34-13-000-801). (b) Put the fluid drain container under the angle gearbox (c) Remove the two bolts (1), washers (2) and the plug (4) from the right side of the angle gearbox. (d) Discard the packing (3) from the plug. (e) Let all the oil drain from the angle gearbox. (7) Remove the main oil filter element and let the oil drain (Ref. TASK 79-21-22-000-801). (8) Remove the four magnetic chip detectors from the lubrication and scavenge oil pump and let the oil drain (Ref. TASK 79-22-11-000-801). NOTE : You must remove the detail probes and the valves from the oil ____ pump. (9) Clean all the magnetic chip detectors with solvent, petroleum (Material No. P11-027), then dry them with a clean cloth. (10) Let the engine oil drain for a minimum of 30 minutes. NOTE : This will let the engine oil completely drain from all the ____ components.
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Subtask 12-13-79-420-050 B. Install the Engine Parts after Draining CAUTION : REMOVE THE PROTECTION COVERS FROM THE OPENINGS AS NECESSARY TO _______ PREVENT ENGINE DAMAGE. (1) Install the magnetic chip detectors (Ref. TASK 79-22-11-400-801). (2) Install the main oil filter element (Ref. TASK 79-21-22-400-801). (3) Install the plug (4) to the angle gearbox as follows: (a) Apply oil, lubricating, turbine engine (Material No. P03-001) to the two bolts (1) and the new packing (3) (b) Install the new packing (3) to the plug (4) (c) Install the plug (4) with the two washers (2) and bolts (1) to the right side of the angle gearbox. (d) TORQUE the bolts (1) to between 85 and 95 lbf.in (0.96 and 1.07 m.daN). (e) Install the fan exit liner segment (inner) at 6 oclock position (Ref. TASK 72-34-13-400-801). Subtask 12-13-79-610-059 C. Fill the Engine Oil System (Without Pressure Fill Equipment). (1) Loosen and remove the oil tank cap. (2) Add the engine oil: CAUTION : WE RECOMMEND THAT YOU DO NOT MIX DIFFERENT BRANDS OF OIL. _______ IF YOU DO, ENGINE DAMAGE CAN BE THE RESULT. (a) Add the correct oil, lubricating, turbine engine (Material No. P03-001) into the filler neck until no more oil can be added without overflow into the scupper drain. NOTE : It is permitted to mix different brands of oil when you ____ service the engine oil system as specified in Service Bulletin No. 238.
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NOTE : The stable oil level in the sightglass will now be in the ____ green area. NOTE : If the aircraft is not parked level, the oil level ____ indication in the sightglass is affected. The engine oil system is serviced correctly if no more oil can be added without overflow into the scupper drain. (3) Install the oil tank cap as follows: (a) With the handle at open, align and install the cap to the filler neck (b) Push down on the cap and turn the handle clockwise to close (c) Push the handle into the cap to lock the cap (d) Make sure that the cap is installed equally and completely. (4) Write the amount of oil that you added. Subtask 12-13-79-610-060 D. Fill the Engine Oil System (With Pressure Fill Equipment). (1) Install the oil tank cap for this pressure fill procedure as follows: (a) With the handle at open, align and install the cap to the filler neck. (b) Push down on the cap and turn the handle clockwise to close. (c) Push the handle into the cap to lock the cap. (d) Make sure that the cap is installed equally and completely. (2) Lift the lever and remove the dust cover from the oil pressure fill valve.
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(3) Install and connect the drain hose: WARNING : YOU MUST CONNECT THE DRAIN HOSE TO THE OVERFLOW DRAIN _______ CONNECTOR AND PUT THE DRAIN HOSE INTO A COLLECTOR/CONTAINER BEFORE YOU CONNECT THE PRESSURE FILL HOSE TO THE ENGINE OIL FILL CONNECTOR. MAKE THE DRAIN HOSE HANG STRAIGHT DOWN. MAKE SURE THAT THE HOSE IS ABOVE AND NOT INTO THE FLUID IN THE COLLECTOR/CONTAINER. WHEN YOU CONNECT THE PRESSURE FILL HOSE, THE DRAIN CONNECTOR (LINE) OPENS AUTOMATICALLY AND RELEASES THE PRESSURE IN THE OIL SYSTEM. WHEN YOU RELEASE THE PRESSURE, OIL AND AIR CAN SPRAY FROM THE OVERFLOW CONNECTOR. (a) Put the drain hose into the fluid drain container and make sure that the end of the hose is not in the fluid. (4) Connect the drain hose to the (larger) overflow connector before you connect the pressure fill hose. NOTE : Some oil can come out of the overflow connector if you connect ____ the pressure fill hose first. (5) Connect the pressure fill hose from the pressure fill service unit to the (smaller) pressure fill connector. (6) Add the engine oil: CAUTION : DO NOT MIX TYPES OF OIL WHEN YOU ADD OR REPLACE THE ENGINE _______ OIL. (a) Use the pressure fill service unit and add the correct oil, lubricating, turbine engine (Material No. P03-001) at a maximum pressure of 100 psi (6.90 bar). (7) Fill the oil tank until oil comes out the drain hose. NOTE : The oil fill pressure connector has a restrictor so that the ____ rate of oil pressure fill is less then the rate of the gravity drain. This prevents you from putting too much oil in the system. NOTE : If the aircraft is not parked level, the oil level indication ____ in the sightglass is affected. The engine oil system is serviced correctly if no more oil can be added without overflow from the drain hose. (8) Remove the pressure hose from the pressure fill valve.
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(9) After the oil drains, remove the drain hose. (10) Install the dust cover to the oil pressure fill valve assembly and turn the handle to lock the cover. (11) Write the amount of oil that you added. Subtask 12-13-79-410-073 E. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the left and right thrust reverser: (Ref. TASK 78-30-00-410801) - FOR 4030EM1 417AL, 418AR - FOR 4030EM2 427AL, 428AR Subtask 12-13-79-440-055 F. Make the thrust reverser serviceable (Ref. TASK 78-30-00-440-804) Subtask 12-13-79-865-066 G. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2 Subtask 12-13-79-700-052 H. Turn (dry motor) the power plant so that the engine oil pressure is stable (Ref. TASK 71-00-00-720-816). NOTE : Do not exceed 5 minutes of starter operation. ____ Subtask 12-13-79-610-061 J. Service the engine oil system again. See servicing of the engine oil system (Ref. TASK 12-13-79-610-806).
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5. Close-up ________ Subtask 12-13-79-410-074 A. Close Access (1) Close the left and right aft fan cowl doors: (Ref. TASK 71-13-00-410802) - FOR 4030EM1 415BL, 416BR - FOR 4030EM2 425BL, 426BR (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Close the access door 811. (4) Remove the access platform(s). Subtask 12-13-79-862-063 B. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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TASK 12-13-79-170-802 Flushing the Oil in the Engine Oil System. WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE AFTER THE ENGINE IS SHUTDOWN. _______ THE ENGINE CAN STAY HOT FOR A LONG TIME AFTER THE ENGINE IS SHUTDOWN. WARNING : USE PROTECTIVE CLOTHING WHEN YOU USE ENGINE OIL. OIL CAN CAUSE SKIN _______ IRRITATION. CAUTION : DO NOT OPERATE THE ENGINE WITHOUT SUFFICIENT OIL. THIS WILL CAUSE A _______ POSSIBLE INFLIGHT SHUTDOWN AND POSSIBLE DAMAGE TO THE ENGINE. CAUTION : YOU MUST DO THIS SERVICING PROCEDURE TO PREVENT TOO MUCH OIL IN THE _______ OIL SYSTEM. DO NOT OPERATE THE ENGINE WITH TOO MUCH OIL. THIS WILL CAUSE A POSSIBLE IN FLIGHT SHUTDOWN AND POSSIBLE DAMAGE TO THE ENGINE. CAUTION : DO NOT LET ENGINE FUEL OR OIL FALL ON THE ENGINE. YOU MUST _______ IMMEDIATELY REMOVE UNWANTED FUEL OR OIL WITH A CLOTH. THE FUEL OR OIL CAN CAUSE DAMAGE TO SOME ENGINE PARTS. 1. __________________ Reason for the Job To flush the engine oil. NOTE : It is only necessary to flush the engine oil system for these ____ reasons: A different type or brand of oil is to be used. The engine has oil system contamination. Preservation for 60 days or less (Method I). 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
circuit breaker(s) safety clip(s) adjustable access platform 1.22 m (4 ft.) access platform 2.5 m (8 ft. 2 in.)
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B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-13-79-610-808 24-42-00-861-801 24-42-00-862-801 71-00-00-720-824 71-00-00-860-818 71-00-00-860-820 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801 78-30-00-040-804 78-30-00-410-801 78-30-00-440-804
Changing the Oil in the Engine Oil System Energize the Ground Service Network De-energize the Ground Service Network Test No. 3A - Idle Power Test (Reverser Open) Normal Engine Automatic Start Procedure Engine Shutdown Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Deactivation of the Thrust Reverser for Maintenance Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Reactivation of the Thrust Reverser after Maintenance
3. __________ Job Set-up Subtask 12-13-79-861-063 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-79-941-063 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure. Subtask 12-13-79-010-082 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU.
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Subtask 12-13-79-865-083 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-13-79-010-083 E. Get Access (1) Open the left and right aft fan cowl doors: (Ref. TASK 71-13-00-010802) - FOR 4030EM1 415BL, 416BR - FOR 4030EM2 425BL, 426BR Subtask 12-13-79-040-054 F. Make the thrust reverser unserviceable (Ref. TASK 78-30-00-040-804) Subtask 12-13-79-010-084 G. Get Access (1) Open the left and right thrust reverser: (Ref. TASK 78-30-00-010-801) - FOR 4030EM1 417AL, 418AR - FOR 4030EM2 427AL, 428AR (2) Put the adjustable access platform in position. Subtask 12-13-79-610-065 H. Change the oil in the engine oil system (Ref. TASK 12-13-79-610-808). NOTE : When you change the oil, you drain the system, install a new oil ____ filter element, and fill the system.
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4. Procedure _________ Subtask 12-13-79-710-051 A. Operate the Engine (1) Start and operate the engine at idle power for 2 - 5 minutes (Ref. TASK 71-00-00-860-818) and (Ref. TASK 71-00-00-720-824). (2) Shut down the engine by shutdown procedures (Ref. TASK 71-00-00-860820). Subtask 12-13-79-610-066 B. Change the oil in the engine oil system again (Ref. TASK 12-13-79-610808). NOTE : When you change the oil, you drain the system, install a new oil ____ filter element, and fill the system. 5. Close-up ________ Subtask 12-13-79-410-071 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the left and right thrust reverser: (Ref. TASK 78-30-00-410801) - FOR 4030EM1 417AL, 418AR - FOR 4030EM2 427AL, 428AR Subtask 12-13-79-440-054 B. Make the thrust reverser serviceable (Ref. TASK 78-30-00-440-804)
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Subtask 12-13-79-865-084 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2 Subtask 12-13-79-410-072 D. Close Access (1) Close the left and right aft fan cowl doors: (Ref. TASK 71-13-00-410802) - FOR 4030EM1 415BL, 416BR - FOR 4030EM2 425BL, 426BR (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Close the access door 811. (4) Remove the access platform(s). Subtask 12-13-79-862-062 E. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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ENGINE OIL - SERVICING ______________________ TASK 12-13-79-610-809 To Service the Engine Oil System WARNING : YOU MUST BE CAREFUL WHEN YOU DO WORK ON THE ENGINE PARTS AFTER THE _______ ENGINE IS SHUTDOWN. THE ENGINE PARTS CAN STAY HOT FOR ALMOST 1 HOUR. R R R
WARNING : YOU MUST NOT LET ENGINE OIL STAY ON YOUR SKIN. FLUSH THE OIL FROM _______ YOUR SKIN WITH WATER. THE OIL IS POISONOUS AND CAN BE ABSORBED INTO THE BODY.
R R R R
CAUTION : YOU MUST NOT LET ENGINE FUEL OR OIL FALL ON THE ENGINE. UNWANTED FUEL _______ OR OIL MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT-FREE CLOTH. THE FUEL OR OIL CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job The procedure that follows tells you how to fill the engine oil system with approved oil. This can be done by the gravity fill procedure or the pressure fill procedure. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R R
No specific No specific No specific No specific No specific No specific UT954 U999092 3409536
circuit breaker(s) safety clip(s) drain hose pressure fill service unit clean container 0.5 USgal (1.8927 l) adjustable access platform 1.22 m (4 ft.) access platform 2.5 m (8 ft. 2 in.) 1 ADAPTER - OIL TANK 1 HOSE - OIL TANK 1 GUN - OIL TANK
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B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
OMAT 1011
Material No.
OMAT 238
* engine lubricating, oil (synthetic) (Ref. 70-30-00) * lockwire 0.028 to 0.031 in. (0.71 to 0.79 m) dia (Ref. 70-30-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R
24-42-00-861-801 24-42-00-862-801 71-00-00-860-810 71-00-00-860-814 72-61-00-000-801 79-00-00-280-805 12-13-79-991-011 12-13-79-991-019
Energize the Ground Service Network De-energize the Ground Service Network Engine Automatic Start Engine Shutdown Removal of the External Gearbox Module Do a Check for Fuel Contamination of the Engine Oil Fig. 301 Fig. 302
3. __________ Job Set-up Subtask 12-13-79-861-058 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-79-941-058 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure. Subtask 12-13-79-010-068 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811.
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(3) Open the protective door of the AC/DC emergency power-center 740VU. Subtask 12-13-79-865-073 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-13-79-010-069 E. Get Access (1) Put the adjustable access platform in the correct position at the right side of the engine position. (2) Open the access panel on the right fan cowl door: - FOR 4030EM1 416CR - FOR 4030EM2 426CR Subtask 12-13-79-612-055 F. Do a Check of the Engine Oil Level in the Oil Tank Sight Glass NOTE : You must wait a minimum of 10 minutes after the engine has stopped ____ before you do a check of the oil level. This will let the oil level become stable. (1) If the engine has been stopped for less than 6 hours and the oil level is low, fill the engine oil tank. (2) If the engine has been stopped for more than 6 hours and the oil level is low, but above the 5 US QUARTS (4.73 l) REQUIRED level: (a) Do not fill the engine oil system. (b) Start the engine (Ref. TASK 71-00-00-860-810).
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(c) Run the engine at idle for 2 minutes. R R
(d) Shut down the engine (Ref. TASK 71-00-00-860-814).
R
(e) Do a check of the engine oil level again. If the oil level is low, fill the engine oil tank. NOTE : You must wait a minimum of 10 minutes after the engine has ____ stopped before you do a check of the oil level. This will let the oil level become stable.
R
(3) If the engine has been stopped for more than 6 hours and the oil level is below the 5 US QUARTS (4.73 l) REQUIRED level: (a) Drain the external gearbox (Ref. TASK 72-61-00-000-801). (b) Fill the engine oil tank. (c) Start the engine (Ref. TASK 71-00-00-860-810). (d) Run the engine at idle for 2 minutes.
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(e) Shut down the engine (Ref. TASK 71-00-00-860-814).
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(f) Do a check of the engine oil level again. If the oil level is low, fill the engine oil tank. NOTE : You must wait a minimum of 10 minutes after the engine has ____ stopped before you do a check of the oil level. This will let the oil level become stable.
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(4) If the oil level is low after you do a dry or wet motor procedure, do the steps that follow:
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CAUTION : YOU MUST NOT ADD OIL TO THE ENGINE AFTER YOU DO A DRY OR _______ WET MOTOR PROCEDURE. THE OIL WILL NOT GO BACK TO THE OIL TANK FULLY AND WILL SHOW AN INCORRECT OIL LEVEL. TOO MUCH OIL IN THE ENGINE CAN CAUSE DAMAGE TO THE ENGINE.
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(a) Do not fill the oil system.
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(b) Start the engine (Ref. TASK 71-00-00-860-810).
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(c) Run the engine at idle for 2 minutes.
EFF : 701-749, 12-13-79 Page 304 Config-2 Apr 01/05 SROS
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(d) Shut down the engine (Ref. TASK 71-00-00-860-814).
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(e) Do a check of the engine oil level after a minimum of 10 minutes. If the oil level is low, fill the engine oil tank. 4. Procedure _________ (Ref. Fig. 301/TASK 12-13-79-991-011, 302/TASK 12-13-79-991-019) Subtask 12-13-79-612-056 A. Fill the Engine Oil Tank (Gravity Fill Procedure) CAUTION : IF YOU CHANGE TO A DIFFERENT APPROVED OIL TYPE, YOU MUST ADD _______ THE REPLACEMENT OIL TO THE TANK DURING THE REGULAR SERVICING OF THE ENGINE. IT IS VERY IMPORTANT THAT YOU DO NOT DRAIN THE OIL SYSTEM AND FILL IT WITH THE REPLACEMENT OIL IN ONE OPERATION. IF YOU DO NOT OBEY THIS INSTRUCTION, YOU CAN CAUSE DAMAGE TO THE ENGINE. NOTE : It is recommended that you use the same oil type, when you fill ____ the engine oil system. If there is no oil of the same type available, use one of the other oils from the approved list. (1) Remove the oil filler cap (1) from the oil tank. (2) If you can smell fuel in the oil tank when you remove the oil filler cap, do a check for fuel contamination of the engine oil (Ref. TASK 79-00-00-280-805). (3) Add engine lubricating, oil (synthetic) (Material No. OMAT 1011) to the engine oil tank. (a) Add clean, approved engine lubricating, oil (synthetic) (Material No. OMAT 1011) to the engine oil tank. Make sure the correct level can be seen in the oil tank sight indicator. (b) Install the oil filler cap (1) to the engine oil tank. NOTE : Make sure the seal ring (2) is fully engaged in the groove ____ of the oil filler cap (1). If it is loose, replace the seal ring. This will make sure of the correct installation of the filler cap and prevent oil tank leaks.
EFF : 701-749, 12-13-79 Page 305 Config-2 Apr 01/05 SROS
Engine Oil Tank-Oil Fill Location Figure 301/TASK 12-13-79-991-011 EFF : 701-749, 12-13-79 Page 306 Config-2 Apr 01/05 R SROS
Engine Oil Tank-Oil Fill Location (SB79-C455) Figure 302/TASK 12-13-79-991-019 EFF : 701-749, 12-13-79 Page 307 Config-2 Apr 01/05 R SROS
Subtask 12-13-79-612-057 B. Fill the Engine Oil Tank (Pressure Fill Procedure) CAUTION : IF YOU CHANGE TO A DIFFERENT APPROVED OIL TYPE, YOU MUST ADD _______ THE REPLACEMENT OIL TO THE TANK DURING THE REGULAR SERVICING OF THE ENGINE. IT IS VERY IMPORTANT THAT YOU DO NOT DRAIN THE OIL SYSTEM AND FILL IT WITH THE REPLACEMENT OIL IN ONE OPERATION. IF YOU DO NOT OBEY THIS INSTRUCTION, YOU CAN CAUSE DAMAGE TO THE ENGINE. NOTE : It is recommended that you use the same oil type, when you fill ____ the engine oil system. If there is no oil of the same type available, use one of the other oils from the approved list. PRE SB79-C455 (1) Remove the lockwire from the pressure fill (3) and overflow (2) couplings. (2) Remove the dust caps from the pressure fill (3) and overflow (2) couplings. (3) Install the drain hose to the overflow coupling (2). (4) If you can smell fuel when you install the drain hose, do para 4.C. (5) Add engine lubricating, oil (synthetic) (Material No. OMAT 1011) to the engine oil tank. (a) Get the pressure fill service unit or the GUN - OIL TANK (3409536), HOSE - OIL TANK (U999092), and the ADAPTER - OIL TANK (UT954). (b) Put the open end of the overflow drain hose in to the clean container. (c) If a pressure fill service unit is to be used, do the steps that follow: 1 _
Connect the pressure fill service unit to the pressure fill coupling (3) on the oil tank.
2 _
Add approved, clean engine lubricating, oil (synthetic) (Material No. OMAT 1011) to the tank until the correct level is seen in the oil tank sight indicator.
EFF : 701-749, 12-13-79 Page 308 Config-2 Apr 01/05 R SROS
NOTE : A small quantity of oil will drain from the overflow ____ drain hose when the oil is at the correct level. 3 _
Disconnect the pressure fill service unit from the pressure fill coupling (3).
4 _
Disconnect the overflow drain hose from the overflow coupling (2).
5 _
Install the dust caps on the pressure fill (3) and overflow (2) couplings.
6 _
Safety the dust caps together with lockwire 0.028 to 0.031 in. (0.71 to 0.79 m) dia (Material No. OMAT 238).
(d) If the GUN - OIL TANK (3409536) is to be used, do the steps that follow: 1 _
Install the ADAPTER - OIL TANK (UT954) to the pressure fill coupling (3).
2 _
Connect the HOSE - OIL TANK (U999092) to the ADAPTER - OIL TANK (UT954), on the pressure fill coupling (3).
3 _
Connect the GUN - OIL TANK (3409536), to the HOSE - OIL TANK (U999092).
4 _
Use the GUN - OIL TANK (3409536) to add clean engine lubricating, oil (synthetic) (Material No. OMAT 1011) to the tank until the correct level is seen in the oil tank sight indicator. NOTE : A small quantity of oil will drain from the overflow ____ drain hose when the oil is at the correct level.
5 _
Disconnect the GUN - OIL TANK (3409536) from the HOSE - OIL TANK (U999092) and disconnect the HOSE - OIL TANK (U999092) from the ADAPTER - OIL TANK (UT954).
6 _
Disconnect the ADAPTER - OIL TANK (UT954) from the pressure fill coupling (3).
7 _
Disconnect the overflow drain hose from the overflow coupling (2).
8 _
Install the dust caps on the pressure fill (3) and overflow (2) couplings.
EFF : 701-749, 12-13-79 Page 309 Config-2 Apr 01/05 R SROS
9 _
Safety the dust caps together, with lockwire 0.028 to 0.031 in. (0.71 to 0.79 m) dia (Material No. OMAT 238).
5. Close-up ________ Subtask 12-13-79-865-074 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2 Subtask 12-13-79-410-062 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Close the access door 811. (4) Close the access panel on the right fan cowl door: - FOR 4030EM1 416CR - FOR 4030EM2 426CR (5) Remove the access platform(s). Subtask 12-13-79-862-057 C. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : 701-749, 12-13-79 Page 310 Config-2 Apr 01/05 R SROS
TASK 12-13-79-680-801 Drain the Engine Oil System WARNING : YOU MUST BE CAREFUL WHEN YOU DO WORK ON THE ENGINE PARTS AFTER THE _______ ENGINE IS SHUTDOWN. THE ENGINE PARTS CAN STAY HOT FOR ALMOST 1 HOUR. WARNING : YOU MUST NOT TOUCH HOT PARTS WITHOUT APPLICABLE GLOVES. HOT PARTS CAN _______ CAUSE AN INJURY. IF YOU GET AN INJURY PUT IT IN COLD WATER FOR 10 MINUTES AND GET MEDICAL AID. WARNING : YOU MUST NOT LET ENGINE OIL STAY ON YOUR SKIN. FLUSH THE OIL FROM _______ YOUR SKIN WITH WATER. THE OIL IS POISONOUS AND CAN BE ABSORBED INTO THE BODY. CAUTION : YOU MUST NOT MOTOR THE ENGINE AFTER THE OIL TANK IS DRAINED. IF YOU _______ MOTOR THE ENGINE THE OIL TANK IS DRAINED, DAMAGE TO THE ENGINE CAN OCCUR. CAUTION : YOU MUST NOT PUT OIL THAT HAS BEEN DRAINED FROM THE ENGINE BACK INTO _______ THE OIL SYSTEM. CONTAMINATION IN THE OIL CAN CAUSE DAMAGE TO SOME PARTS OR FAILURE OF THE OIL. CAUTION : YOU MUST NOT LET ENGINE FUEL OR OIL FALL ON THE ENGINE. UNWANTED FUEL _______ OR OIL MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT-FREE CLOTH. THE FUEL OR OIL CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No
specific specific specific specific
circuit breaker(s) safety clip(s) container 10 USgal (40 liter) access platform 2.5 m (8 ft. 2 in.) Torque Wrench : range 36.00 to 220.00 lbf.in (0.40 to 2.60 m.daN)
EFF : 701-749, 12-13-79 Page 311 Config-2 Oct 01/00 SROS
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
OMat 2-142
Material No.
OMat 238
Material No.
OMat2-142
* Safety Cable (Ref. 70-30-00) * lockwire 0.028 to 0.031 in. (0.71 to 0.79 mm) (Ref. 70-30-00) * Safety Cable (Ref. 70-30-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
R
1 1 1 1 1 2 2 2 2 2
seal ring seal ring seal ring seal ring seal ring seal ring washer washer washer washer
79-21-41 79-22-46 79-22-46 79-22-46 79-22-46 72-61-00 79-22-51 79-22-51 79-22-51 79-22-51
60 -150 61 -030 61A-030 61B-030 61C-030 61 -020 61 -020 61 -020A 61 -020B 61 -070
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 70-02-01-910-801 70-12-04-910-804 70-12-04-910-806 71-13-00-010-805 71-13-00-410-805 79-22-43-100-801 79-22-45-920-801 12-13-79-991-013
Energize the Ground Service Network De-energize the Ground Service Network Identification, Lubrication and Fitting of Flexible Seal Rings Locking Techniques - Wire locking Locking Techniques - Safety Cable Open the Fan Cowl Doors Close the Fan Cowl Doors Cleaning of the Pressure Oil Filter Element (5004EN) Remove, Discard and Replace Oil Scavenge Filter Fig. 303
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-13-79-991-014 12-13-79-991-015 12-13-79-991-016 12-13-79-991-017 12-13-79-991-018
Fig. Fig. Fig. Fig. Fig.
304 305 306 307 308
3. __________ Job Set-up Subtask 12-13-79-861-065 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-79-941-065 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure. Subtask 12-13-79-010-090 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU. Subtask 12-13-79-865-087 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74
EFF : 701-749, 12-13-79 Page 313 Config-2 Jul 01/03 R SROS
Subtask 12-13-79-010-091 E. Get Access (1) Open the fan cowl doors (Ref. TASK 71-13-00-010-805): - FOR 4030EM1 415AL, 416AR - FOR 4030EM2 425AL, 426AR 4. Procedure _________ Subtask 12-13-79-680-054 A. Drain the Engine Oil System (1) Drain the oil tank (Ref. Fig. 303/TASK 12-13-79-991-013) (a) Put the clean container 10 USgal (40 liter) in position to catch the oil. R R
(b) Remove the drain plug (1) from the oil tank and let all the oil drain into the container.
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(c) Remove and discard the washer (2).
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(d) Install a new washer (2) on the drain plug (1) (Ref. TASK 70-0201-910-801).
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(e) Install the drain plug (1) in the oil tank.
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(f) TORQUE the drain plug (1) to 205 lbf.in (2.31 m.daN). (2) Drain the Air/Oil Heat Exchanger (AOHE). (Ref. Fig. 304/TASK 12-13-79-991-014) (a) Put the container 10 USgal (40 liter) in position to catch the oil.
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(b) Remove and discard the safety cable/lockwire from the drain plug (1) on the AOHE. (c) Remove the drain plug (1) from the AOHE and let all the oil drain into the container.
EFF : 701-749, 12-13-79 Page 314 Config-2 Jul 01/03 SROS
Drain Plug on the Oil Tank Figure 303/TASK 12-13-79-991-013 EFF : 701-749, 12-13-79 Page 315 Config-2 Apr 01/02 R SROS
Drain Plug on the Air/Oil Heat Exchanger Figure 304/TASK 12-13-79-991-014 EFF : 701-749, 12-13-79 Page 316 Config-2 Oct 01/00 SROS
(d) Remove and discard the washer (2). (e) Install a new washer (2) on the drain plug (1) (Ref. TASK 70-0201-910-801). (f) Install the drain plug (1) in the AOHE. (g) TORQUE the drain plug (1) to between 40 and 50 lbf.in (0.45 and 0.56 m.daN). (h) Safety the drain plug (1) with safety cable 0.032 in.(0.81 mm) Safety Cable (Material No. OMat 2-142), (Ref. TASK 70-12-04-910806), or with the lockwire 0.028 to 0.031 in. (0.71 to 0.79 mm) (Material No. OMat 238), (Ref. TASK 70-12-04-910-804). (3) Drain the external gearbox module (Ref. Fig. 305/TASK 12-13-79-991-015) (a) Put the container 10 USgal (40 liter) in position to catch the oil. (b) Remove and discard the safety cable/lockwire from the drain plug (1) on the gearbox module. (c) Remove the drain plug (1) from the gearbox module and let all the oil drain into the container. (d) Remove and discard the seal ring (2). R
(e) Install a new seal ring (2) on the drain plug (1) (Ref. TASK 7002-01-910-801). (f) Install the drain plug (1) in the gearbox module. (g) TORQUE the drain plug (1) to between 202 and 220 lbf.in (2.28 and 2.48 m.daN). (h) Safety the drain plug (1) with safety cable 0.032 in.(0.81 mm) Safety Cable (Material No. OMat2-142), (Ref. TASK 70-12-04-910806), or with the lockwire 0.028 to 0.031 in. (0.71 to 0.79 mm) (Material No. OMat 238), (Ref. TASK 70-12-04-910-804). (4) Drain the bevel gears housing (Ref. Fig. 306/TASK 12-13-79-991-016) (a) Put the container 10 USgal (40 liter) in position to catch the oil.
EFF : 701-749, 12-13-79 Page 317 Config-2 Jul 01/04 SROS
Drain Plug on the External Gearbox Module Figure 305/TASK 12-13-79-991-015 EFF : 701-749, 12-13-79 Page 318 Config-2 Oct 01/00 SROS
Drain Plug on the Bevel Gears Housing Figure 306/TASK 12-13-79-991-016 EFF : 701-749, 12-13-79 Page 319 Config-2 Oct 01/00 SROS
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(b) Remove and discard the safety cable/lockwire from the drain plug (1) on the housing. (c) Remove the drain plug (1) from the housing and let all the oil drain into the container. (d) Remove and discard the seal ring (2). (e) Install a new seal ring (2) on the drain plug (1) (Ref. TASK 7002-01-910-801). (f) Install the drain plug (1) in the housing. (g) TORQUE the drain plug (1) to between 202 and 220 lbf.in (2.28 and 2.48 m.daN).
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(h) Safety the drain plug (1) with safety cable 0.032 in.(0.81 mm) Safety Cable (Material No. OMat 2-142), (Ref. TASK 70-12-04-910806), or with the lockwire 0.028 to 0.031 in. (0.71 to 0.79 mm) (Material No. OMat 238), (Ref. TASK 70-12-04-910-804). (5) Clean the pressure filter element (Ref. TASK 79-22-43-100-801). (6) Replace the scavenge filter element (Ref. TASK 79-22-45-920-801). (7) Drain the oil from the Fuel Oil Heat Exchanger (FOHE) (Ref. Fig. 307/TASK 12-13-79-991-017) (a) Put the container 10 USgal (40 liter) in position to catch the oil.
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(b) Remove and discard the safety cable/lockwire from the drain plug (2). (c) Remove the drain plug (2) from the FOHE and let all the oil drain into the container. (d) Remove and discard the seal ring (1). (e) Install a new seal ring (1) and the drain plug (2) (Ref. TASK 7002-01-910-801). (f) Install the drain plug (2) in the FOHE. (g) TORQUE the drain plug (2) to between 110 and 120 lbf.in (1.24 and 1.35 m.daN).
EFF : 701-749, 12-13-79 Page 320 Config-2 Jul 01/03 SROS
Drain Plug on Fuel/Oil Heat Exchanger Figure 307/TASK 12-13-79-991-017 EFF : 701-749, 12-13-79 Page 321 Config-2 Oct 01/00 SROS
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(h) Safety the drain plug (2) with safety cable 0.032 in.(0.81 mm) Safety Cable (Material No. OMat 2-142), (Ref. TASK 70-12-04-910806), or with the lockwire 0.028 to 0.031 in. (0.71 to 0.79 mm) (Material No. OMat 238), (Ref. TASK 70-12-04-910-804). (8) Drain the oil from the oil pump assembly (Ref. Fig. 308/TASK 12-13-79-991-018) (a) Put the container 10 USgal (40 liter) in position to catch the oil. (b) Remove the bolts (4) and the washers (3) from each of the Magnetic Chip Detector (MCD) housing blanks (2). (c) Remove the MCD housing blanks (2) and let all the oil drain into the container. (d) Remove and discard the seal rings (1) from the housing blanks (2). (e) Install a new seal ring (1) on each housing blank (2) (Ref. TASK 70-02-01-910-801). (f) Put the housing blanks (2) in position and install the bolts (4) and the washers (3). (g) TORQUE the bolts (4) to 100 lbf.in (1.13 m.daN). Subtask 12-13-79-865-088 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2 5. Close-up ________ Subtask 12-13-79-410-078 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the protective door of the AC/DC emergency power center 740VU.
EFF : 701-749, 12-13-79 Page 322 Config-2 Jul 01/03 SROS
Magnetic Chip Detector - Housing Blank Figure 308/TASK 12-13-79-991-018 EFF : 701-749, 12-13-79 Page 323 Config-2 Jul 01/03 R SROS
(3) Close the access door 811. (4) Close the fan cowl doors (Ref. TASK 71-13-00-410-805): - FOR 4030EM1 415AL, 416AR - FOR 4030EM2 425AL, 426AR (5) Remove the access platform(s). Subtask 12-13-79-862-066 B. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : 701-749, 12-13-79 Page 324 Config-2 Jul 01/03 R SROS
ENGINE STARTING - SERVICING ___________________________ TASK 12-13-80-612-802 Servicing of the Starter (Pressure and Gravity Fill - with Thrust Reverser Cowl Doors Open) WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE AFTER THE ENGINE IS SHUTDOWN. _______ THE ENGINE CAN STAY HOT FOR A LONG TIME AFTER THE ENGINE IS SHUTDOWN. WARNING : USE PROTECTIVE CLOTHING WHEN YOU USE ENGINE OIL. OIL CAN CAUSE SKIN _______ IRRITATION. CAUTION : DO NOT OPERATE THE STARTER WITHOUT SUFFICIENT OIL. THIS WILL CAUSE _______ DAMAGE TO THE STARTER. CAUTION : DO NOT OPERATE THE STARTER WITH TOO MUCH OIL. THIS WILL CAUSE DAMAGE _______ TO THE STARTER. CAUTION : DO NOT LET ENGINE FUEL OR OIL FALL ON THE ENGINE. YOU MUST _______ IMMEDIATELY REMOVE UNWANTED FUEL OR OIL WITH A CLOTH. THE FUEL OR OIL CAN CAUSE DAMAGE TO SOME ENGINE PARTS. 1. __________________ Reason for the Job Replenish starter oil with the thrust reverser open. NOTE : Do not use this servicing task for draining and filling the starter. ____ To drain and fill the starter oil (Ref. TASK 12-13-80-610-803). 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No
specific specific specific specific specific specific specific specific
circuit breaker(s) safety clip(s) drain hose flashlight fluid drain container 5 USgal (19 l) pressure fill service unit squeeze bottle adjustable access platform 1.22 m (4 ft.) access platform 2.5 m (8 ft. 2 in.)
R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-80 Page 301 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
Torque Wrench : range 5.00 to 35.00 lbf.in (0.05 to 0.40 m.daN)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
P03-001
Material No.
P05-287
* oil, lubricating, turbine engine (Ref. 70-30-00) * lockwire 0.020 in. (0.50 mm) dia. (Ref. 70-30-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------16 16
packing packing
80-11-11 40 -190 80-11-11 40A-190
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801 78-30-00-040-804 78-30-00-410-801 78-30-00-440-804 12-13-80-991-002
Energize the Ground Service Network De-energize the Ground Service Network Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Deactivation of the Thrust Reverser for Maintenance Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Reactivation of the Thrust Reverser after Maintenance Fig. 301
R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-80 Page 302 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
3. __________ Job Set-up Subtask 12-13-80-861-054 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-80-941-055 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure. Subtask 12-13-80-010-062 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU. Subtask 12-13-80-865-058 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-13-80-010-063 E. Get Access (1) Open the left and right aft fan cowl doors (Ref. TASK 71-13-00-010802): - FOR 4030EM1 415BL, 416BR - FOR 4030EM2
R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-80 Page 303 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
425BL, 426BR Subtask 12-13-80-040-053 F. Deactivation of the Thrust Reverser. WARNING : YOU MUST DEACTIVATE THE THRUST REVERSER DIRECTIONAL CONTROL _______ VALVE (DCV) BEFORE YOU WORK ON OR AROUND THE TRANSLATING COWL. IF YOU DO NOT DEACTIVATE THE DCV, YOU CAN CAUSE ACCIDENTAL THRUST REVERSER OPERATION AND INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT. (1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 7830-00-040-804). Subtask 12-13-80-010-064 G. Get Access (1) Open the left and right thrust reverser cowl doors (Ref. TASK 78-3000-010-801): - FOR 4030EM1 417AL, 418AR - FOR 4030EM2 427AL, 428AR (2) Put the adjustable access platform in position. 4. Procedure _________ (Ref. Fig. 301/TASK 12-13-80-991-002) Subtask 12-13-80-210-052 A. Make a Check of the Starter Oil Level (1) Use a flashlight and find the oil level sightglass on the right side of the starter attached to the rear of the main gearbox. (2) If necessary, wipe the sightglass to make it clean. (3) Examine the oil level in the starter as follows: (a) If the oil level in the sightglass is between three quarters and seven eighths, do not fill the starter.
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(b) If the oil level in the sightglass is at approximately three quarters or below, you must service the starter as follows. (c) If the oil level in the sightglass is above the sightglass, the oil level in the starter is more than necessary and you must service the starter as follows. NOTE : The starter is full when the oil level shows approximately ____ seven eighths full on the sightglass. Subtask 12-13-80-612-053 B. Service the Starter (without Pressure Fill Equipment) CAUTION : INSTALL PROTECTION COVERS OVER ALL OPENINGS AS SOON AS POSSIBLE _______ TO PREVENT ENGINE DAMAGE. (1) Put the fluid drain container 5 USgal (19 l) under the starter. (2) Remove the lockwire and fill plug (15). (3) Discard the packing (16) from the plug (15). (4) If the oil in the starter is more than necessary, let the oil drain from the fill port until it only drips. NOTE : The oil level in the sightglass will now show at approximately ____ seven eighths. The starter is full when the oil level shows approximately seven eighths full on the sightglass. (5) If the oil in the starter is less than necessary, fill the starter to an acceptable level as follows: (a) Fill a standard squeeze bottle with clean oil, lubricating, turbine engine (Material No. P03-001). (b) Attach a piece of flex hose approximately 6 in. (152.40 mm) long to the squeeze bottle. (c) Put the flex hose into the fill port of the starter and squeeze the oil into the starter until oil drips from the fill port. NOTE : The oil level in the sightglass will now show at ____ approximately seven eighths. The starter is full when the oil level shows approximately seven eighths full on the sightglass.
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Starter Oil Level Servicing - Thrust Reverser Cowl Doors Open Figure 301/TASK 12-13-80-991-002- 12 (SHEET 1) R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-80 Page 306 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
Starter Oil Level Servicing - Thrust Reverser Cowl Doors Open Figure 301/TASK 12-13-80-991-002- 22 (SHEET 2) R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-80 Page 307 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
(6) Install the fill plug (15) as follows: CAUTION : REMOVE THE PROTECTION COVERS FROM THE OPENINGS AS NECESSARY _______ TO PREVENT ENGINE DAMAGE. (a) Apply oil, lubricating, turbine engine (Material No. P03-001) to the new packing (16) and the threads of the plug (15). (b) Install the new packing (16) to the plug (15). (c) Install the plug (15) to the fill port. (d) TORQUE the plug (15) to between 20 and 30 lbf.in (0.22 and 0.33 m.daN). (e) Safety the plug (15) with lockwire 0.020 in. (0.50 mm) dia. (Material No. P05-287). Subtask 12-13-80-612-054 C. Service the Starter (with Pressure Fill Equipment) (1) Remove the coupling covers from the overflow drain quick disconnect coupling and the pressure fill quick disconnect coupling on the air starter duct bracket. (2) Put the end of the drain hose in the fluid drain container 5 USgal (19 l). (3) Connect the drain hose fitting to the overflow drain quick disconnect (larger) coupling on the air starter duct bracket. NOTE : Some oil can come out of the drain hose when you connect the ____ drain hose. (4) Connect the pressure fill hose from the pressure fill service unit to the pressure fill quick disconnect (smaller) coupling on the air starter duct bracket. (5) Fill the starter as follows: CAUTION : MAKE SURE THAT YOU ATTACH THE DRAIN HOSE TO THE OVERFLOW _______ DRAIN QUICK DISCONNECT COUPLING BEFORE YOU TRY AND FILL THE STARTER. IF YOU DO NOT CONNECT THE DRAIN HOSE FIRST, YOU CAN PUT TOO MUCH PRESSURE INSIDE THE STARTER AND DAMAGE CAN OCCUR.
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(a) Use the pressure fill service unit and add the correct oil, lubricating, turbine engine (Material No. P03-001) until the oil comes out of the drain hose. (6) Remove the pressure hose from the coupling at the air starter duct bracket. (7) Install the coupling cover to the pressure fill quick disconnect coupling. (8) When the oil from the drain hose decreases to a drip, disconnect the drain hose from the overflow drain quick disconnect coupling on the air starter duct bracket. (9) Install the coupling cover to the overflow drain quick disconnect coupling. NOTE : The oil level in the sightglass will now show at approximately ____ seven eighths. The starter is full when the oil level shows approximately seven eighths full on the sightglass. 5. Close-up ________ Subtask 12-13-80-410-062 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the left and right thrust reverser cowl doors (Ref. TASK 78-3000-410-801): - FOR 4030EM1 417AL, 418AR - FOR 4030EM2 427AL, 428AR Subtask 12-13-80-440-053 B. Make the thrust reverser serviceable (Ref. TASK 78-30-00-440-804).
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Subtask 12-13-80-865-059 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2 Subtask 12-13-80-410-064 D. Close Access (1) Close the left and right aft fan cowl doors (Ref. TASK 71-13-00-410802): - FOR 4030EM1 415BL, 416BR - FOR 4030EM2 425BL, 426BR (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Close the access door 811. (4) Remove the access platform(s). Subtask 12-13-80-862-057 E. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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TASK 12-13-80-610-803 R R
Change Starter Oil (with the Threaded Type Starter Magnetic Chip Detector (Vickers/Tedeco)) WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE AFTER THE ENGINE IS SHUTDOWN. _______ THE ENGINE CAN STAY HOT FOR A LONG TIME AFTER THE ENGINE IS SHUTDOWN. WARNING : USE PROTECTIVE CLOTHING WHEN YOU USE ENGINE OIL. OIL CAN CAUSE SKIN _______ IRRITATION. CAUTION : DO NOT OPERATE THE STARTER WITHOUT SUFFICIENT OIL. THIS WILL CAUSE _______ DAMAGE TO THE STARTER. CAUTION : DO NOT OPERATE THE STARTER WITH TOO MUCH OIL. THIS WILL CAUSE DAMAGE _______ TO THE STARTER. CAUTION : DO NOT LET ENGINE FUEL OR OIL FALL ON THE ENGINE. YOU MUST _______ IMMEDIATELY REMOVE UNWANTED FUEL OR OIL WITH A CLOTH. THE FUEL OR OIL CAN CAUSE DAMAGE TO SOME ENGINE PARTS. CAUTION : WHEN YOU REPLACE THE STARTER DUE TO FAILURE OR OIL CONTAMINATION, YOU _______ MUST REPLACE ALL OIL SERVICING HARDWARE INCLUDING THE OIL SERVICE LINES, PLUGS, AND FITTINGS. IF YOU DO NOT DO THIS, YOU CAN TRANSFER THE OIL CONTAMINATION INTO THE NEW STARTER. 1. __________________ Reason for the Job Refer to the MPD TASK: 800000-P2 To change (drain and fill) the starter oil. To drain and fill the starter oil for replacement of the starter. To drain and fill the starter oil after fluid contamination.
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2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No
specific specific specific specific specific specific specific specific
circuit breaker(s) safety clip(s) drain hose fluid drain container 5 USgal (19 l) pressure fill service unit squeeze bottle adjustable access platform 1.22 m (4 ft.) access platform 2.5 m (8 ft. 2 in.) Torque Wrench : range 5.00 to 35.00 lbf.in (0.05 to 0.40 m.daN)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
P03-001
Material No.
P05-287
* oil, lubricating, turbine engine (Ref. 70-30-00) * lockwire 0.020 in. (0.50 mm) dia. (Ref. 70-30-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------39 39 39 41 41 46 46
packing packing packing packing packing packing packing
80-11-18 80-11-18 80-11-18 80-11-18 80-11-18 80-11-11 80-11-11
40 -030 40 -030A 40A-030 40 -010 40A-010 40 -190 40A-190
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D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-13-80-612-802 24-42-00-861-801 24-42-00-862-801 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801 78-30-00-040-804 78-30-00-410-801 78-30-00-440-804 80-11-11-000-801 80-11-11-400-801 12-13-80-991-003
Servicing of the Starter (Pressure and Gravity Fill with Thrust Reverser Cowl Doors Open) Energize the Ground Service Network De-energize the Ground Service Network Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Deactivation of the Thrust Reverser for Maintenance Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Reactivation of the Thrust Reverser after Maintenance Removal of the Starter (5000ES) Installation of the Starter (5000ES) Fig. 302
3. __________ Job Set-up Subtask 12-13-80-861-052 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-80-941-053 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure. Subtask 12-13-80-010-056 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU.
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Subtask 12-13-80-865-054 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-13-80-010-057 E. Get Access (1) Open the left and right aft fan cowl doors (Ref. TASK 71-13-00-010802): - FOR 4030EM1 415BL, 416BR - FOR 4030EM2 425BL, 426BR Subtask 12-13-80-040-051 F. deactivation of the Thrust Reverser. WARNING : YOU MUST DEACTIVATE THE THRUST REVERSER DIRECTIONAL CONTROL _______ VALVE (DCV) BEFORE YOU WORK ON OR AROUND THE TRANSLATING COWL. IF YOU DO NOT DEACTIVATE THE DCV, YOU CAN CAUSE ACCIDENTAL THRUST REVERSER OPERATION AND INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT. (1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 7830-00-040-804). Subtask 12-13-80-010-058 G. Get Access (1) Open the right thrust reverser cowl door (Ref. TASK 78-30-00-010801): - FOR 4030EM1 418AR - FOR 4030EM2
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428AR (2) Open the lower left thrust reverser access door: - FOR 4030EM1 417EL - FOR 4030EM2 427EL (3) Put the adjustable access platform in position. 4. Procedure _________ (Ref. Fig. 302/TASK 12-13-80-991-003) Subtask 12-13-80-680-051 A. Drain the Oil from the Starter WARNING : BE CAREFUL WHEN YOU DRAIN OIL FROM A HOT ENGINE. HOT OIL IS _______ DANGEROUS. IF IT TOUCHES YOUR BODY OR EYES IT WILL BURN BADLY. CAUTION : WHEN YOU REPLACE THE STARTER DUE TO FAILURE OR OIL _______ CONTAMINATION, YOU MUST REPLACE ALL OIL SERVICING HARDWARE INCLUDING THE OIL SERVICE LINES, PLUGS, AND FITTINGS. IF YOU DO NOT DO THIS, YOU CAN TRANSFER THE OIL CONTAMINATION INTO THE NEW STARTER. CAUTION : INSTALL PROTECTION COVERS OVER ALL OPENINGS AS SOON AS POSSIBLE _______ TO PREVENT ENGINE DAMAGE. NOTE : Do not use this draining and filling task for normal oil ____ servicing. To make a check of the starter oil level (Ref. TASK 1213-80-612-802). (1) Remove the chip detector (Threaded Type - Vickers/Tedeco) from the starter as follows: (a) Put the fluid drain container 5 USgal (19 l) under the starter. CAUTION : DO NOT PUT CONTAMINATED OIL DRAINED FROM THE STARTER _______ BACK INTO THE OIL CART. IF YOU DO NOT DO THIS, YOU CAN TRANSFER THE OIL CONTAMINATION INTO THE OIL CART. (b) Remove the lockwire from the magnetic chip detector probe (38). (c) Remove the magnetic chip detector probe (38) from the valve (40).
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R
Starter Oil Draining and Filling Figure 302/TASK 12-13-80-991-003- 12 (SHEET 1)
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R
Starter Oil Draining and Filling Figure 302/TASK 12-13-80-991-003- 22 (SHEET 2)
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(d) Discard the packing (39) from the probe (38). (2) Examine the magnetic chip detector probe (38) as follows: (a) If you find metallic chips larger than 0.100 in. (2.54 mm) you must remove the starter (Ref. TASK 80-11-11-000-801). (b) If you find metallic chips smaller than 0.100 in. (2.54 mm), remove the chips from the probe (38) and proceed with step (3). (c) If you find no chips, proceed with step (3). (3) Remove the valve from the starter as follows: (a) Remove the lockwire from the valve (40). (b) Discard the packing (41) from the valve (40). (c) Let the oil drain from the starter. (d) Write down the quantity of the drained oil: If the quantity of the drained oil is less than 7 OZF (207.0 ml), replace the starter (Ref. TASK 80-11-11-000-801), (Ref. TASK 8011-11-400-801). (4) Install the starter magnetic chip detector (Threaded Type Vickers/Tedeco) as follows: CAUTION : REMOVE THE PROTECTION COVERS FROM THE OPENINGS AS NECESSARY _______ TO PREVENT ENGINE DAMAGE. (a) Apply oil, lubricating, turbine engine (Material No. P03-001) to the new packing (39) and to the new packing (41). (b) Install the new packings (39) and (41) to the chip detector probe (38) and the valve (40). (c) Install the valve (40) to the starter. (d) Torque the valve as follows: CAUTION : DO NOT TORQUE THE VALVE TOO MUCH. _______ IF YOU DO, YOU WILL BREAK OFF THE END OF THE VALVE. 1 _
TORQUE the valve (40) to between 10 and 25 lbf.in (0.11 and 0.28 m.daN).
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(e) Safety the valve (40) with lockwire 0.020 in. (0.50 mm) dia. (Material No. P05-287). (f) Install the chip detector probe (38) into the valve (40). (g) Torque the probe as follows: CAUTION : DO NOT TORQUE THE PROBE TOO MUCH. _______ IF YOU DO, YOU WILL BREAK OFF THE END OF THE PROBE. 1 _
TORQUE the chip detector probe (38) to between 5 and 15 lbf.in (0.05 and 0.16 m.daN).
(h) Safety the chip detector probe (38) with lockwire 0.020 in. (0.50 mm) dia. (Material No. P05-287). Subtask 12-13-80-612-062 B. Fill the Starter (without Pressure Fill Equipment) CAUTION : WHEN YOU REPLACE THE STARTER DUE TO FAILURE OR OIL _______ CONTAMINATION, YOU MUST REPLACE ALL OIL SERVICING HARDWARE INCLUDING THE OIL SERVICE LINES, PLUGS, AND FITTINGS. IF YOU DO NOT DO THIS, YOU CAN TRANSFER THE OIL CONTAMINATION INTO THE NEW STARTER. CAUTION : INSTALL PROTECTION COVERS OVER ALL OPENINGS AS SOON AS POSSIBLE _______ TO PREVENT ENGINE DAMAGE. (1) Remove the lockwire and fill plug (47). (2) Discard the packing (46) from the fill plug (47). (3) Fill the starter to an acceptable level as follows: (a) Fill a standard squeeze bottle with clean oil, lubricating, turbine engine (Material No. P03-001). (b) Attach a piece of flex hose approximately 6 in. (152.4 mm) long to the squeeze bottle. (c) Put the flex hose into the fill port of the starter and squeeze the oil into the starter until oil drips from the fill port. NOTE : The oil level in the sightglass will now show at ____ approximately seven eighths. The starter is full when the
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oil level shows approximately seven eighths full on the sightglass. (4) Install the fill plug (47) as follows: CAUTION : REMOVE THE PROTECTION COVERS FROM THE OPENINGS AS NECESSARY _______ TO PREVENT ENGINE DAMAGE. (a) Apply oil, lubricating, turbine engine (Material No. P03-001) to the new packing (46) and the threads of the plug (47). (b) Install the new packing (46) to the plug (47). (c) Install the plug (47) to the fill port. (d) TORQUE the plug (47) to between 20 and 30 lbf.in (0.22 and 0.33 m.daN). (e) Safety the plug with lockwire 0.020 in. (0.50 mm) dia. (Material No. P05-287). Subtask 12-13-80-612-063 C. Fill the Starter (with Pressure Fill Equipment) CAUTION : WHEN YOU REPLACE THE STARTER DUE TO FAILURE OR OIL _______ CONTAMINATION, YOU MUST REPLACE ALL OIL SERVICING HARDWARE INCLUDING THE OIL SERVICE LINES, PLUGS, AND FITTINGS. IF YOU DO NOT DO THIS, YOU CAN TRANSFER THE OIL CONTAMINATION INTO THE NEW STARTER. (1) Remove the coupling covers from the overflow drain quick disconnect couplind and the pressure fill quick disconnect coupling on the air starter duct bracket. (2) Put the end of the drain hose in the fluid drain container 5 USgal (19 l). (3) Connect the drain hose to the overflow drain quick disconnect (larger) coupling on the air starter duct bracket. NOTE : Some oil can come out of the drain hose when you connect the ____ drain hose. (4) Connect the pressure fill hose from the pressure fill service unit to the pressure fill quick disconnect (smaller) coupling on the air starter duct bracket.
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(5) Fill the starter as follows: CAUTION : MAKE SURE THAT YOU ATTACH THE DRAIN HOSE TO THE OVERFLOW _______ DRAIN QUICK DISCONNECT COUPLING BEFORE YOU TRY AND FILL THE STARTER. IF YOU DO NOT CONNECT THE DRAIN HOSE FIRST, YOU CAN PUT TOO MUCH PRESSURE INSIDE THE STARTER AND DAMAGE CAN OCCUR. (a) Use the pressure fill service unit and add the correct oil, lubricating, turbine engine (Material No. P03-001) until the oil comes out of the drain hose. (6) Remove the pressure hose from the coupling on the air starter duct bracket. (7) Install the coupling cover to the pressure fill quick disconnect coupling. (8) When the oil from the drain hose decreases to a drip, disconnect the drain hose from the overflow drain quick disconnect coupling on the air starter duct bracket. (9) Install the coupling cover to the overflow drain quick disconnect coupling. NOTE : The oil level in the sightglass will now show at approximately ____ seven eighths. The starter is full when the oil level shows approximately seven eighths full on the sightglass. 5. Close-up ________ Subtask 12-13-80-410-057 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Remove the fluid drain container. (3) Close the lower left thrust reverser access door: - FOR 4030EM1 417EL - FOR 4030EM2 427EL
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(4) Close the right thrust reverser cowl door (Ref. TASK 78-30-00-410801): - FOR 4030EM1 418AR - FOR 4030EM2 428AR Subtask 12-13-80-440-051 B. Make the thrust reverser serviceable (Ref. TASK 78-30-00-440-804). Subtask 12-13-80-865-055 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2 Subtask 12-13-80-410-059 D. Close Access (1) Close the left and right aft fan cowl doors (Ref. TASK 71-13-00-410802): - FOR 4030EM1 415BL, 416BR - FOR 4030EM2 425BL, 426BR (2) Close the protective door of the AC/DC emergency power-center 740VU. (3) Close the access door 811. (4) Remove the access platform(s). Subtask 12-13-80-862-058 E. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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TASK 12-13-80-610-803- 01 R R
Change Starter Oil (with the Bayonet Type Starter Magnetic Chip Detector (Lisle)) WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE AFTER THE ENGINE IS SHUTDOWN. _______ THE ENGINE CAN STAY HOT FOR A LONG TIME AFTER THE ENGINE IS SHUTDOWN. WARNING : USE PROTECTIVE CLOTHING WHEN YOU USE ENGINE OIL. OIL CAN CAUSE SKIN _______ IRRITATION. CAUTION : DO NOT OPERATE THE STARTER WITHOUT SUFFICIENT OIL. THIS WILL CAUSE _______ DAMAGE TO THE STARTER. CAUTION : DO NOT OPERATE THE STARTER WITH TOO MUCH OIL. THIS WILL CAUSE DAMAGE _______ TO THE STARTER. CAUTION : DO NOT LET ENGINE FUEL OR OIL FALL ON THE ENGINE. YOU MUST _______ IMMEDIATELY REMOVE UNWANTED FUEL OR OIL WITH A CLOTH. THE FUEL OR OIL CAN CAUSE DAMAGE TO SOME ENGINE PARTS. CAUTION : WHEN YOU REPLACE THE STARTER DUE TO FAILURE OR OIL CONTAMINATION, YOU _______ MUST REPLACE ALL OIL SERVICING HARDWARE INCLUDING THE OIL SERVICE LINES, PLUGS, AND FITTINGS. IF YOU DO NOT DO THIS, YOU CAN TRANSFER THE OIL CONTAMINATION INTO THE NEW STARTER. 1. __________________ Reason for the Job Refer to the MPD TASK: 800000-P2 To change (drain and fill) the starter oil. To drain and fill the starter oil for replacement of the starter. To drain and fill the starter oil after fluid contamination.
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2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No
specific specific specific specific specific specific specific specific
circuit breaker(s) safety clip(s) drain hose fluid drain container 5 USgal (19 l) pressure fill service unit squeeze bottle adjustable access platform 1.22 m (4 ft.) access platform 2.5 m (8 ft. 2 in.) Torque Wrench : range 5.00 to 35.00 lbf.in (0.05 to 0.40 m.daN)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
P03-001
Material No.
P05-287
* oil, lubricating, turbine engine (Ref. 70-30-00) * lockwire 0.020 in. (0.50 mm) dia. (Ref. 70-30-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------41 41 43 44 44 44 46 46
packing packing packing packing packing packing packing packing
80-11-18 80-11-18 80-11-18 80-11-18 80-11-18 80-11-18 80-11-11 80-11-11
40 -010 40A-010 40A-040 40 -030 40 -030A 40A-030 40 -190 40A-190
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D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-13-80-612-802 24-42-00-861-801 24-42-00-862-801 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801 78-30-00-040-804 78-30-00-410-801 78-30-00-440-804 80-11-11-000-801 80-11-11-400-801 12-13-80-991-008
Servicing of the Starter (Pressure and Gravity Fill with Thrust Reverser Cowl Doors Open) Energize the Ground Service Network De-energize the Ground Service Network Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Deactivation of the Thrust Reverser for Maintenance Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Reactivation of the Thrust Reverser after Maintenance Removal of the Starter (5000ES) Installation of the Starter (5000ES) Fig. 303
3. __________ Job Set-up Subtask 12-13-80-861-059 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-80-941-060 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure. Subtask 12-13-80-010-076 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU.
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Subtask 12-13-80-865-068 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-13-80-010-077 E. Get Access (1) Open the left and right aft fan cowl doors (Ref. TASK 71-13-00-010802): - FOR 4030EM1 415BL, 416BR - FOR 4030EM2 425BL, 426BR Subtask 12-13-80-040-057 F. Deactivation of the Thrust Reverser. WARNING : YOU MUST DEACTIVATE THE THRUST REVERSER DIRECTIONAL CONTROL _______ VALVE (DCV) BEFORE YOU WORK ON OR AROUND THE TRANSLATING COWL. IF YOU DO NOT DEACTIVATE THE DCV, YOU CAN CAUSE ACCIDENTAL THRUST REVERSER OPERATION AND INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT. (1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 7830-00-040-804). Subtask 12-13-80-010-078 G. Get Access (1) Open the right thrust reverser cowl door (Ref. TASK 78-30-00-010801): - FOR 4030EM1 418AR - FOR 4030EM2
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428AR (2) Open the lower left thrust reverser access door: - FOR 4030EM1 417EL - FOR 4030EM2 427EL (3) Put the adjustable access platform in position. 4. Procedure _________ (Ref. Fig. 303/TASK 12-13-80-991-008) Subtask 12-13-80-680-052 A. Drain the Oil from the Starter WARNING : BE CAREFUL WHEN YOU DRAIN OIL FROM A HOT ENGINE. HOT OIL IS _______ DANGEROUS. IF IT TOUCHES YOUR BODY OR EYES IT WILL BURN BADLY. CAUTION : DO NOT REMOVE OR INSTALL THE CHIP DETECTOR AS AN ASSEMBLY. YOU _______ MUST REMOVE THE MAGNETIC PROBE FROM THE VALVE. IF YOU DO NOT DO THIS, YOU CAN DAMAGE THE ASSEMBLY. CAUTION : DO NOT USE TOOLS TO REMOVE OR INSTALL THE CHIP DETECTOR PROBE. _______ IF YOU DO, YOU CAN DAMAGE THE PROBE. CAUTION : WHEN YOU REPLACE THE STARTER DUE TO FAILURE OR OIL _______ CONTAMINATION, YOU MUST REPLACE ALL OIL SERVICING HARDWARE INCLUDING THE OIL SERVICE LINES, PLUGS, AND FITTINGS. IF YOU DO NOT DO THIS, YOU CAN TRANSFER THE OIL CONTAMINATION INTO THE NEW STARTER. CAUTION : INSTALL PROTECTION COVERS OVER ALL OPENINGS AS SOON AS POSSIBLE _______ TO PREVENT ENGINE DAMAGE. NOTE : Do not use this draining and filling task for normal oil ____ servicing. To make a check of the starter oil level (Ref. TASK 1213-80-612-802).
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Starter Oil Draining and Filling Figure 303/TASK 12-13-80-991-008- 12 (SHEET 1) R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-80 Page 328 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
Starter Oil Draining and Filling Figure 303/TASK 12-13-80-991-008- 22 (SHEET 2) R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-80 Page 329 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
(1) Remove the chip detector (Bayonnet Type - Lisle) from the starter as follows: (a) Put the fluid drain container 5 USgal (19 l) under the starter. CAUTION : DO NOT PUT CONTAMINATED OIL DRAINED FROM THE STARTER _______ BACK INTO THE OIL CART. IF YOU DO NOT DO THIS, YOU CAN TRANSFER THE OIL CONTAMINATION INTO THE OIL CART. (b) Hold the magnetic probe (42) by the grip. (c) Push the probe (42) in and turn it counterclockwise. (d) Pull the probe (42) out. (2) Examine the magnetic chip detector probe (42) as follows: (a) If you find metallic chips larger than 0.100 in. (2.54 mm) you must remove the starter (Ref. TASK 80-11-11-000-801). (b) If you find metallic chips smaller than 0.100 in. (2.54 mm), remove the chips from the probe (42) and proceed with step (3). (c) If you find no chips, proceed with step (3). (3) Remove the valve (45) from the starter as follows: (a) Remove the lockwire from the magnetic chip detector valve (45). (b) Remove the valve (45) from the starter. (c) Discard the packing (43) from the probe (42). R
(d) Discard the packing (41) from the valve (45). (e) Let the oil drain from the starter. (f) Write down the quantity of the drained oil: If the quantity of the drained oil is less than 7 OZF (207.0 ml), replace the starter (Ref. TASK 80-11-11-000-801), (Ref. TASK 8011-11-400-801) (4) Install the starter magnetic chip detector (Bayonnet Type-Lisle) as follows: CAUTION : REMOVE THE PROTECTION COVERS FROM THE OPENINGS AS NECESSARY _______ TO PREVENT ENGINE DAMAGE.
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CAUTION : DO NOT REMOVE OR INSTALL THE CHIP DETECTOR AS AN ASSEMBLY. _______ YOU MUST REMOVE THE MAGNETIC PROBE FROM THE VALVE. IF YOU DO NOT DO THIS, YOU CAN DAMAGE THE ASSEMBLY. CAUTION : DO NOT USE TOOLS TO REMOVE OR INSTALL THE CHIP DETECTOR _______ PROBE. IF YOU DO, YOU CAN DAMAGE THE PROBE. (a) Apply oil, lubricating, turbine engine (Material No. P03-001) to the new packing (41). (b) Install the new packing (41) to the washer face of the valve (45). (c) Apply oil, lubricating, turbine engine (Material No. P03-001) to the new packing (44). R R
(d) Install the valve (45) to the starter.
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(e) Torque the valve as follows: CAUTION : DO NOT TORQUE THE VALVE TOO MUCH. _______ IF YOU DO, YOU WILL BREAK OFF THE END OF THE VALVE. 1 _
TORQUE the valve (45) to between 10 and 25 lbf.in (0.11 and 0.28 m.daN).
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(f) Safety the valve (45) with lockwire 0.020 in. (0.50 mm) dia. (Material No. P05-287).
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(g) Apply oil, lubricating, turbine engine (Material No. P03-001) to the new packing (43).
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(h) Install the new packing (43) to the magnetic probe (42).
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(i) Install the magnetic probe (42) into the valve (45).
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(j) Push the magnetic probe (42) in and turn it clockwise until it locks.
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(k) Pull the magnetic probe (42) to make sure it is locked. NOTE : The magnetic probe is correctly installed when you align ____ the red marks on the probe with the red marks on the valve.
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Subtask 12-13-80-612-064 B. Fill the Starter (without Pressure Fill Equipment) CAUTION : WHEN YOU REPLACE THE STARTER DUE TO FAILURE OR OIL _______ CONTAMINATION, YOU MUST REPLACE ALL OIL SERVICING HARDWARE INCLUDING THE OIL SERVICE LINES, PLUGS, AND FITTINGS. IF YOU DO NOT DO THIS, YOU CAN TRANSFER THE OIL CONTAMINATION INTO THE NEW STARTER. CAUTION : INSTALL PROTECTION COVERS OVER ALL OPENINGS AS SOON AS POSSIBLE _______ TO PREVENT ENGINE DAMAGE. (1) Remove the lockwire and fill plug (47). (2) Discard the packing (46) from the fill plug (47). (3) Fill the starter to an acceptable level as follows: (a) Fill a standard squeeze bottle with clean oil, lubricating, turbine engine (Material No. P03-001). (b) Attach a piece of flex hose approximately 6 in. (152.4 mm) long to the squeeze bottle. (c) Put the flex hose into the fill port of the starter and squeeze the oil into the starter until oil drips from the fill port. NOTE : The oil level in the sightglass will now show at ____ approximately seven eighths. The starter is full when the oil level shows approximately seven eighths full on the sightglass. (4) Install the fill plug (47) as follows: CAUTION : REMOVE THE PROTECTION COVERS FROM THE OPENINGS AS NECESSARY _______ TO PREVENT ENGINE DAMAGE. (a) Apply oil, lubricating, turbine engine (Material No. P03-001) to the new packing (46) and the threads of the plug (47). (b) Install the new packing (46) to the plug (47). (c) Install the plug (47) to the fill port. (d) TORQUE the plug (47) to between 20 and 30 lbf.in (0.22 and 0.33 m.daN).
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(e) Safety the plug with lockwire 0.020 in. (0.50 mm) dia. (Material No. P05-287). Subtask 12-13-80-612-065 C. Fill the Starter (with Pressure Fill Equipment) CAUTION : WHEN YOU REPLACE THE STARTER DUE TO FAILURE OR OIL _______ CONTAMINATION, YOU MUST REPLACE ALL OIL SERVICING HARDWARE INCLUDING THE OIL SERVICE LINES, PLUGS, AND FITTINGS. IF YOU DO NOT DO THIS, YOU CAN TRANSFER THE OIL CONTAMINATION INTO THE NEW STARTER. (1) Remove the coupling covers from the overflow drain quick disconnect coupling and the pressure fill quick disconnect coupling on the air starter duct bracket. (2) Put the end of the drain hose in the fluid drain container 5 USgal (19 l). (3) Connect the drain hose to the overflow drain quick disconnect (larger) coupling on the air starter duct bracket. NOTE : Some oil can come out of the drain hose when you connect the ____ drain hose. (4) Connect the pressure fill hose from the pressure fill service unit to the pressure fill quick disconnect (smaller) coupling on the air starter duct bracket. (5) Fill the starter as follows: CAUTION : MAKE SURE THAT YOU ATTACH THE DRAIN HOSE TO THE OVERFLOW _______ DRAIN QUICK DISCONNECT COUPLING BEFORE YOU TRY AND FILL THE STARTER. IF YOU DO NOT CONNECT THE DRAIN HOSE FIRST, YOU CAN PUT TOO MUCH PRESSURE INSIDE THE STARTER AND DAMAGE CAN OCCUR. (a) Use the pressure fill service unit and add the correct oil, lubricating, turbine engine (Material No. P03-001) until the oil comes out of the drain hose. (6) Remove the pressure hose from the coupling on the air starter duct bracket. (7) Install the coupling cover to the pressure fill quick disconnect coupling.
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(8) When the oil from the drain hose decreases to a drip, disconnect the drain hose from the overflow drain quick disconnect coupling on the air starter duct bracket. (9) Install the coupling cover to the overflow drain quick disconnect coupling. NOTE : The oil level in the sightglass will now show at approximately ____ seven eighths. The starter is full when the oil level shows approximately seven eighths full on the sightglass. 5. Close-up ________ Subtask 12-13-80-410-073 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Remove the fluid drain container. (3) Close the lower left thrust reverser access door: - FOR 4030EM1 417EL - FOR 4030EM2 427EL (4) Close the right thrust reverser cowl door (Ref. TASK 78-30-00-410801): - FOR 4030EM1 418AR - FOR 4030EM2 428AR Subtask 12-13-80-440-057 B. Make the thrust reverser serviceable (Ref. TASK 78-30-00-440-804). Subtask 12-13-80-865-069 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2
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Subtask 12-13-80-410-074 D. Close Access (1) Close the left and right aft fan cowl doors (Ref. TASK 71-13-00-410802): - FOR 4030EM1 415BL, 416BR - FOR 4030EM2 425BL, 426BR (2) Close the protective door of the AC/DC emergency power-center 740VU. (3) Close the access door 811. (4) Remove the access platform(s). Subtask 12-13-80-862-059 E. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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TASK 12-13-80-612-803 Check and Replenish Starter Oil by Remote Fill - Through Access Door WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE AFTER THE ENGINE IS SHUTDOWN. _______ THE ENGINE CAN STAY HOT FOR A LONG TIME AFTER THE ENGINE IS SHUTDOWN. WARNING : USE PROTECTIVE CLOTHING WHEN YOU USE ENGINE OIL. OIL CAN CAUSE SKIN _______ IRRITATION. CAUTION : DO NOT OPERATE THE STARTER WITHOUT SUFFICIENT OIL. THIS WILL CAUSE _______ DAMAGE TO THE STARTER. CAUTION : DO NOT OPERATE THE STARTER WITH TOO MUCH OIL. THIS WILL CAUSE DAMAGE _______ TO THE STARTER. CAUTION : DO NOT LET ENGINE FUEL OR OIL FALL ON THE ENGINE. YOU MUST _______ IMMEDIATELY REMOVE UNWANTED FUEL OR OIL WITH A CLOTH. THE FUEL OR OIL CAN CAUSE DAMAGE TO SOME ENGINE PARTS. 1. __________________ Reason for the Job R NOTE : Do not use this servicing task for draining and filling the starter. ____ To drain and fill the starter oil (Ref. TASK 12-13-80-610-803). 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No
specific specific specific specific specific specific
circuit breaker(s) safety clip(s) drain hose fluid drain container 5 USgal (19 l) pressure fill service unit adjustable access platform 1.22 m (4 ft.) access platform 2.5 m (8 ft. 2 in.)
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B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
P03-001
* oil, lubricating, turbine engine (Ref. 70-30-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 71-13-00-010-802 71-13-00-410-802 78-30-00-040-804 78-30-00-440-804 12-13-80-991-006
Energize the Ground Service Network De-energize the Ground Service Network Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Deactivation of the Thrust Reverser for Maintenance Reactivation of the Thrust Reverser after Maintenance Fig. 304
3. __________ Job Set-up Subtask 12-13-80-861-058 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-80-941-059 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure. Subtask 12-13-80-010-073 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811.
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(3) Open the protective door of the AC/DC emergency power-center 740VU. Subtask 12-13-80-865-066 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-13-80-010-075 E. Get Access (1) Open the right aft fan cowl door (Ref. TASK 71-13-00-010-802): - FOR 4030EM1 416BR - FOR 4030EM2 426BR Subtask 12-13-80-040-056 F. Deactivation of the Thrust Reverser. WARNING : YOU MUST DEACTIVATE THE THRUST REVERSER DIRECTIONAL CONTROL _______ VALVE (DCV) BEFORE YOU WORK ON OR AROUND THE TRANSLATING COWL. IF YOU DO NOT DEACTIVATE THE DCV, YOU CAN CAUSE ACCIDENTAL THRUST REVERSER OPERATION AND INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT. (1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 7830-00-040-804).
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Subtask 12-13-80-010-074 G. Get Access (1) Put the adjustable access platform in position. (2) Open the thrust reverser lower left access door. - FOR 4030EM1 417EL - FOR 4030EM2 427EL 4. Procedure _________ (Ref. Fig. 304/TASK 12-13-80-991-006) Subtask 12-13-80-612-058 A. Do a Check and Service the Starter (with Pressure Fill Equipment) (1) Find the starter oil fill couplings attached to the bottom of the starter air duct towards the right side of the engine. NOTE : Make sure you do not use the Integrated Drive Generator (IDG) ____ oil fill connectors on the rear of the IDG. (2) Remove the coupling covers from the overflow drain quick disconnect coupling and the pressure fill quick disconnect coupling on the air starter duct bracket. (3) Put the end of the drain hose in the fluid drain container 5 USgal (19 l). (4) Connect the drain hose fitting to the overflow drain quick disconnect (larger) coupling on the air starter duct bracket. NOTE : Some oil can come out of the drain hose when you connect the ____ drain hose. (5) Connect the pressure fill hose from the pressure fill service unit to the pressure fill quick disconnect (smaller) coupling on the air starter duct bracket.
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Starter Oil Level Servicing - Pressure Fill Through Access Door Figure 304/TASK 12-13-80-991-006 R EFF : 001-049, 201-249, 251-252, 255-299, 12-13-80 Page 340 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
(6) Add oil as follows: CAUTION : MAKE SURE THAT YOU ATTACH THE DRAIN HOSE TO THE OVERFLOW _______ DRAIN QUICK DISCONNECT COUPLING BEFORE YOU TRY AND FILL THE STARTER. IF YOU DO NOT CONNECT THE DRAIN HOSE FIRST, YOU CAN PUT TOO MUCH PRESSURE INSIDE THE STARTER AND DAMAGE CAN OCCUR. (a) Use the pressure fill service unit and add the correct oil, lubricating, turbine engine (Material No. P03-001) until the oil comes out of the drain hose. (7) Remove the pressure hose from the coupling on the air starter bracket. (8) Install the coupling cover to the pressure fill quick disconnect coupling. (9) When the oil from the drain hose decreases to a drip, disconnect the drain hose from the overflow drain quick disconnect coupling on the air starter duct bracket. (10) Install the coupling cover to the overflow drain quick disconnect coupling. 5. Close-up ________ Subtask 12-13-80-410-072 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the lower left thrust reverser access door. - FOR 4030EM1 417EL - FOR 4030EM2 427EL Subtask 12-13-80-440-056 B. Make the thrust reverser serviceable (Ref. TASK 78-30-00-440-804).
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Subtask 12-13-80-865-067 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2 Subtask 12-13-80-410-071 D. Close Access (1) Close the right aft fan cowl door (Ref. TASK 71-13-00-410-802): - FOR 4030EM1 416BR - FOR 4030EM2 426BR (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Close the access door 811. (4) Remove the access platform(s). Subtask 12-13-80-862-056 E. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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ENGINE STARTING - SERVICING ___________________________ TASK 12-13-80-610-804 To Service the Pneumatic Starter Oil System WARNING : YOU MUST BE CAREFUL WHEN YOU DO WORK ON THE ENGINE PARTS AFTER THE _______ ENGINE IS SHUTDOWN. THE ENGINE PARTS CAN STAY HOT FOR ALMOST 1 HOUR. 1. __________________ Reason for the Job This procedure is applicable to engines with an Allied Signal or Hamilton Standard pneumatic starter. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R
No No No No
specific specific specific specific
circuit breaker(s) safety clip(s) adjustable access platform 1.22 m (4 ft.) access platform 2.5 m (8 ft. 2 in.) Torque Wrench : range 5.00 to 35.00 lbf.in (0.05 to 0.40 m.daN) Torque Wrench : range 36.00 to 220.00 lbf.in (0.40 to 2.60 m.daN)
No specific B. Consumable Materials
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
OMat 1011
Material No.
OMat 238
* engine oil (Ref. 70-30-00) * lockwire 0.028 to 0.031 in. (0.71 to 0.79 mm) dia (Ref. 70-30-00)
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C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------2 3
seal ring seal ring
80-11-41 60 -070 80-11-41 60 -070
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 70-02-01-910-801 70-12-04-910-804 70-51-00-910-802 71-13-00-010-805 71-13-00-410-805 80-11-41-000-803 80-11-41-400-803 12-13-80-991-005
Energize the Ground Service Network De-energize the Ground Service Network Identification, Lubrication and Fitting of Flexible Seal Rings Locking Techniques - Wire locking Torque Tightening Techniques Open the Fan Cowl Doors Close the Fan Cowl Doors Removal of the Pneumatic Starter (5000ES) Installation of the Pneumatic Starter (5000ES) Fig. 301
3. __________ Job Set-up Subtask 12-13-80-861-056 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-80-941-057 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure.
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Subtask 12-13-80-010-068 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU. Subtask 12-13-80-865-062 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-13-80-010-069 E. Get Access (1) Open the fan cowl doors: (Ref. TASK 71-13-00-010-805) - FOR 4030EM1 415AL, 416AR - FOR 4030EM2 425AL, 426AR (2) Put the adjustable access platform in position. Subtask 12-13-80-020-050 F. Get Access to the Pneumatic Starter (1) Remove the oil fill plug (1) and the oil level overflow plug (4) from the pneumatic starter. (Ref. Fig. 301/TASK 12-13-80-991-005) (2) Remove the lockwire from the oil fill plug (1) and the oil level overflow plug (4).
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Pneumatic Starter (Allied Signal) - Oil Fill Location Figure 301/TASK 12-13-80-991-005 EFF : 701-749, 12-13-80 Page 304 Config-2 Oct 01/00 SROS
(3) Remove the oil fill plug (1) and the oil level overflow plug (4). (4) Discard the seal rings (2) and (3). 4. Procedure _________ (Ref. Fig. 301/TASK 12-13-80-991-005) Subtask 12-13-80-612-056 A. Fill the Allied Signal Pneumatic Starter with clean engine oil: (Ref. Fig. 301/TASK 12-13-80-991-005) WARNING : YOU MUST NOT LET ENGINE OIL STAY ON YOUR SKIN. FLUSH THE OIL _______ FROM YOUR SKIN WITH WATER. THE OIL IS POISONOUS AND CAN BE ABSORBED INTO THE BODY. CAUTION : YOU MUST NOT LET ENGINE FUEL OR OIL FALL ON THE ENGINE. _______ UNWANTED FUEL OR OIL MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT-FREE CLOTH. THE FUEL OR OIL CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. CAUTION : YOU MUST USE THE SAME TYPE OF APPROVED OIL EACH TIME YOU FILL _______ THE PNEUNATIC STARTER WITH OIL. YOU MUST ONLY MIX APPROVED OILS IF IT BECOMES OPERATIONALLY NECESSARY. (1) Add clean engine oil (Material No. OMat 1011) to the pneumatic starter. (a) Continue to put oil in the pneumatic starter until oil starts to drip from the oil level overflow. (b) Wait until oil does not drip form the oil level overflow. (c) Use a clean cloth to remove oil from the external surface of the starter. (2) Install a new seal ring (3) on the oil level overflow plug (4) (Ref. TASK 70-02-01-910-801). (a) Lubricate the seal ring (3) with clean engine oil (Material No. OMat 1011). (3) Install the oil level overflow plug (4) to the pneumatic starter. (a) TORQUE the oil level overflow plug (4) to between 120 and 130 lbf.in (1.35 and 1.46 m.daN) (Ref. TASK 70-51-00-910-802)
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(4) Safety the oil level overflow plug (4) with lockwire 0.028 to 0.031 in. (0.71 to 0.79 mm) dia (Material No. OMat 238) (Ref. TASK 70-1204-910-804). (5) Install a new seal ring (2) to the oil fill plug (1) (Ref. TASK 7002-01-910-801). (a) Lubricate the seal ring (2) with clean engine oil (Material No. OMat 1011). (6) Install the oil fill plug (1) to the pneumatic starter. Subtask 12-13-80-612-059 B. Torque the oil fill plug. (1) TORQUE the oil fill plug (1) to between 20 and 35 lbf.in (0.22 and 0.39 m.daN) (Ref. TASK 70-51-00-910-802) Subtask 12-13-80-612-060 C. Safety the oil fill plug. (1) Safety the oil fill plug (1) with lockwire 0.028 to 0.031 in. (0.71 to 0.79 mm) dia (Material No. OMat 238). (Ref. TASK 70-12-04-910-804) (2) Look at the oil level sight glass; the oil level must be above the ADD mark. (3) If the oil level is not above the ADD mark on the oil level sight glass, replace the pneumatic starter (Ref. TASK 80-11-41-000-803) and (Ref. TASK 80-11-41-400-803). 5. Close-up ________ Subtask 12-13-80-865-063 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2
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Subtask 12-13-80-410-067 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Close the access door 811. (4) Close the fan cowl doors: (Ref. TASK 71-13-00-410-805) - FOR 4030EM1 415AL, 416AR - FOR 4030EM2 425AL, 426AR (5) Remove the access platform(s). Subtask 12-13-80-862-053 C. De-energize the ground service network (Ref. TASK 24-42-00-862-801)
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TASK 12-13-80-610-805 To Change the Oil in the Pneumatic Starter WARNING : YOU MUST BE CAREFUL WHEN YOU DO WORK ON THE ENGINE PARTS AFTER THE _______ ENGINE IS SHUTDOWN. THE ENGINE PARTS CAN STAY HOT FOR ALMOST 1 HOUR. 1. __________________ Reason for the Job This procedure is applicable to engines with Allied Signal Pneumatic Starter 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No
specific specific specific specific specific specific
circuit breaker(s) safety clip(s) lint-free cloth adjustable access platform 1.22 m (4 ft.) access platform 2.5 m (8 ft. 2 in.) container 5 l (1.3208 USgal) Torque Wrench : range 36.00 to 220.00 lbf.in (0.40 to 2.60 m.daN)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
OMat 1011
Material No.
OMat 238
* engine lubricating oil (synthetic) (Ref. 70-30-00) * lockwire 0.028 to 0.031 in. (0.71 to 0.79 mm) dia. (Ref. 70-30-00)
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C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------R R R
2 3 6
seal ring seal ring seal ring
80-11-41 60 -070 80-11-41 60 -070 80-11-41 60 -100
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 70-02-01-910-801 70-12-04-910-804 70-51-00-910-802 71-13-00-010-805 71-13-00-410-805 80-11-41-000-803 80-11-41-400-803 12-13-80-991-005
Energize the Ground Service Network De-energize the Ground Service Network Identification, Lubrication and Fitting of Flexible Seal Rings Locking Techniques - Wire locking Torque Tightening Techniques Open the Fan Cowl Doors Close the Fan Cowl Doors Removal of the Pneumatic Starter (5000ES) Installation of the Pneumatic Starter (5000ES) Fig. 301
3. __________ Job Set-up Subtask 12-13-80-861-060 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-13-80-941-061 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure.
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Subtask 12-13-80-010-079 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power center 740VU. Subtask 12-13-80-865-070 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-13-80-010-080 E. Get Access to the Pneumatic Starter (1) Open the fan cowl doors (Ref. TASK 71-13-00-010-805): - FOR 4030EM1 415AL, 416AR - FOR 4030EM2 425AL, 426AR (2) Put the adjustable access platform in position. 4. Procedure _________ (Ref. Fig. 301/TASK 12-13-80-991-005) Subtask 12-13-80-610-061 A. Change the Oil in the Allied Signal Pneumatic Starter WARNING : YOU MUST NOT LET ENGINE OIL STAY ON YOUR SKIN. FLUSH THE OIL _______ FROM YOUR SKIN WITH WATER. THE OIL IS POISONOUS AND CAN BE ABSORBED INTO THE BODY.
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CAUTION : YOU MUST NOT LET ENGINE FUEL OR OIL FALL ON THE ENGINE. _______ UNWANTED FUEL OR OIL MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT-FREE CLOTH. THE FUEL OR OIL CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. (1) Put a container in position to catch the oil that will come out of the starter. (2) Remove the lockwire that safeties the oil drain plug (5). (3) Remove the oil drain plug (5) and let unwanted oil drain into the container. (4) Remove and discard the seal ring (6). R
(5) Install a new seal ring (6) on the oil drain plug (5) (Ref. TASK 7002-01-910-801). (6) Install the oil drain plug (5) on the starter. TORQUE the plug to between 110 and 120 lbf.in (1.24 and 1.35 m.daN). (7) Safety the oil drain plug (5) with lockwire 0.028 to 0.031 in. (0.71 to 0.79 mm) dia. (Material No. OMat 238) (Ref. TASK 70-12-04-910804). (8) Remove the lockwire from the oil fill plug (1) and the oil level overflow plug (4). (9) Remove the oil fill plug (1) and the oil level overflow plug (4) from the starter. (10) Remove and discard the seal rings (2) and (3). (11) Put engine lubricating oil (synthetic) (Material No. OMat 1011) into the oil fill port of the starter: (a) Continue to put oil into the starter until the oil comes out from the overflow port. (b) Wait until the overflow stops. (c) Remove unwanted oil from the outside of the starter with a clean lint-free cloth.
R
(12) Install a new seal ring (3) on the oil level overflow plug (4) (Ref. TASK 70-02-01-910-801).
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(13) Install the oil level overflow plug (4) on the starter. TORQUE the plug to between 120 and 130 lbf.in (1.35 and 1.46 m.daN) (Ref. TASK 70-51-00-910-802). (14) Safety the oil level overflow plug (4) with lockwire 0.028 to 0.031 in. (0.71 to 0.79 mm) dia. (Material No. OMat 238) (Ref. TASK 70-1204-910-804). R
(15) Install a new seal ring (2) on the oil fill plug (1) (Ref. TASK 7002-01-910-801). (16) Install the oil fill plug (1) on the starter. TORQUE the plug to between 120 and 130 lbf.in (1.35 and 1.46 m.daN) (Ref. TASK 70-51-00910-802). (17) Safety the oil fill plug (1) with lockwire 0.028 to 0.031 in. (0.71 to 0.79 mm) dia. (Material No. OMat 238) (Ref. TASK 70-12-04-910804). Subtask 12-13-80-210-055 B. Do a Check of the Sight Glass (1) Look at the oil level sight glass on the starter. The oil level must be above the ADD mark on the right side of the sight glass. (2) If the oil level is not above the ADD mark, replace the pneumatic starter (Ref. TASK 80-11-41-000-803) and (Ref. TASK 80-11-41-400803). 5. Close-up ________ Subtask 12-13-80-865-071 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2
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Subtask 12-13-80-410-075 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Close the access door 811. (4) Close the fan cowl doors (Ref. TASK 71-13-00-410-805): - FOR 4030EM1 415AL, 416AR - FOR 4030EM2 425AL, 426AR (5) Remove the container. (6) Remove the access platform(s). Subtask 12-13-80-862-060 C. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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GAS - DESCRIPTION AND OPERATION _______________________________ 1. _______ General This section gives the instructions to charge the hydraulic power and components related to the landing gear. It includes the topics below: 12-14-29, P. Block 301 HYDRAULIC POWER 12-14-32, P. Block 301 LANDING GEAR
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HYDRAULIC POWER - SERVICING ___________________________ TASK 12-14-29-614-801 Fill the Green Power Accumulator (5151JM1) with Nitrogen 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific R
98F29103500000
access platform 2.5 m (8 ft. 2 in.) Torque Wrench : range 2.00 to 20.00 m.daN (15.00 to 150.00 lbf.ft) 1
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-801 29-10-00-200-801 12-14-29-991-001
Depressurize the Green Hydraulic System (Pressurized with the Hydraulic Ground Supply) Leak Check of Pressure on Hydraulic Power Accumulators (5151JM1,5151JM2,5151JM3) Fig. 301
3. __________ Job Set-up Subtask 12-14-29-864-050 A. Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801).
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Page 301 Jan 01/07
Subtask 12-14-29-010-050 B. Get Access (1) Put the access platform in position at the access door 197CB. (2) Open the Green ground service panel access door 197CB. 4. Procedure _________ (Ref. Fig. 301/TASK 12-14-29-991-001) Subtask 12-14-29-220-050 A. If the decrease in nitrogen pressure is more than 30 bar (435.1131 psi) (with respect to nominal pressure of accumulators) you must make sure that there are no leaks (Ref. TASK 29-10-00-200-801). Subtask 12-14-29-614-050 B. Fill the applicable accumulator with nitrogen. (1) Remove the blanking cap (2) from the charging valve (1). R
(2) Connect to the charging valve (1) the (98F29103500000) or a nitrogen bench capable of maxi pressure 150 bar (2175.5655 psi). (3) Loosen the charging valve nut (3). (4) Open the charging valve nut (3) slowly (turn to the OPEN direction) and fill the hydraulic power accumulator to the correct pressure for the ambient temperature.
R R R
NOTE : If you do this check immediately after aircraft landing, let ____ the pressure become stable for one hour to get a more accurate measurement (temperature compensation of the accumulator). NITROGEN PRESSURE
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Filling of the Green Power Accumulator Figure 301/TASK 12-14-29-991-001 EFF : ALL 12-14-29 SROS
Page 303 Apr 01/98
------------------------------------------------------------------------------| Temperature | Charging Pressure | |---------------------------|-------------------------------------------------| | deg.C | deg.F | bar | PSI | |-----------------------------------------------------------------------------| | -30 | -22 | 108 | 1566 | | -20 | - 4 | 112 | 1624 | | -10 | 14 | 116.5 | 1689 | | 0 | 32 | 121 | 1754 | | 10 | 50 | 125.5 | 1820 | | 20 | 68 | 130 | 1885 | | 30 | 86 | 134.5 | 1950 | | 40 | 104 | 139 | 2015 | | 50 | 112 | 143.5 | 2081 | | 60 | 140 | 148 | 2146 | ------------------------------------------------------------------------------(5) When the pressure is stable and correct, tighten the charging valve nut (3) (CLOSE position). (6) Make sure that the pressure shown on the pressure gage is correct. (7) Stop the supply and remove the nitrogen filling system from the charging valve (1). R R
(8) TORQUE the charging valve nut (3) to between 10.7 and 11.8 m.daN (78.90 and 87.02 lbf.ft).
R
(9) Install the blanking cap (2) on the charging valve. 5. Close-up ________ Subtask 12-14-29-410-050 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the Green ground service panel 197CB. (3) Remove the access platform(s).
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TASK 12-14-29-614-802 Fill the Blue Power Accumulator (5151JM2) with Nitrogen 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific R
98F29103500000
access platform 2.5 m (8 ft. 2 in.) Torque Wrench : range 2.00 to 20.00 m.daN (15.00 to 150.00 lbf.ft) 1
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-802 29-10-00-200-801 12-14-29-991-002
Depressurize the Blue Hydraulic System (Pressurized with the Hydraulic Ground Supply) Leak Check of Pressure on Hydraulic Power Accumulators (5151JM1,5151JM2,5151JM3) Fig. 302
3. __________ Job Set-up Subtask 12-14-29-864-051 A. Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802). Subtask 12-14-29-010-051 B. Get Access (1) Put the access platform in position at the access door 195BB. (2) Open the Blue ground service panel access door 195BB.
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4. Procedure _________ (Ref. Fig. 302/TASK 12-14-29-991-002) Subtask 12-14-29-220-051 A. If the decrease in nitrogen pressure is more than 30 bar (435.1131 psi) (with respect to nominal pressure of accumulators) you must make sure that there are no leaks (Ref. TASK 29-10-00-200-801). Subtask 12-14-29-614-051 B. Fill the applicable accumulator with nitrogen. (1) Remove the blanking cap (2) from the charging valve (1). R
(2) Connect to the charging valve (1) the (98F29103500000) or a nitrogen bench capable of maxi pressure 150 bar (2175.5655 psi). (3) Loosen the charging valve nut (3). (4) Open the charging valve nut (3) slowly (turn to the OPEN direction) and fill the hydraulic power accumulator to the correct pressure for the ambient temperature.
R R R
NOTE : If you do this check immediately after aircraft landing, let ____ the pressure become stable for one hour to get a more accurate measurement (temperature compensation of the accumulator). NITROGEN PRESSURE ------------------------------------------------------------------------------| Temperature | Charging Pressure | |---------------------------|-------------------------------------------------| | deg.C | deg.F | bar | PSI | |-----------------------------------------------------------------------------| | -30 | -22 | 108 | 1566 | | -20 | - 4 | 112 | 1624 | | -10 | 14 | 116.5 | 1689 | | 0 | 32 | 121 | 1754 | | 10 | 50 | 125.5 | 1820 | | 20 | 68 | 130 | 1885 | | 30 | 86 | 134.5 | 1950 | | 40 | 104 | 139 | 2015 | | 50 | 112 | 143.5 | 2081 | | 60 | 140 | 148 | 2146 | ------------------------------------------------------------------------------(5) When the pressure is stable and correct, tighten the charging valve nut (3) (CLOSE position).
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Filling of the Blue Power Accumulator Figure 302/TASK 12-14-29-991-002 EFF : ALL 12-14-29 SROS
Page 307 Apr 01/98
(6) Make sure that the pressure shown on the pressure gage is correct. (7) Stop the supply and remove the nitrogen filling system from the charging valve (1). R R
(8) TORQUE the charging valve nut (3) to between 10.7 and 11.8 m.daN (78.90 and 87.02 lbf.ft).
R
(9) Install the blanking cap (2) on the charging valve. 5. Close-up ________ Subtask 12-14-29-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the Blue ground service panel 195BB. (3) Remove the access platform(s).
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TASK 12-14-29-614-803 Fill the Yellow Power Accumulator (5151JM3) with Nitrogen 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific R
98F29103500000
access platform 2.5 m (8 ft. 2 in.) Torque Wrench : range 2.00 to 20.00 m.daN (15.00 to 150.00 lbf.ft) 1
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-803 29-10-00-200-801 12-14-29-991-003
Depressurize the Yellow Hydraulic System (Pressurized with the Hydraulic Ground Supply) Leak Check of Pressure on Hydraulic Power Accumulators (5151JM1,5151JM2,5151JM3) Fig. 303
3. __________ Job Set-up Subtask 12-14-29-864-052 A. Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803). Subtask 12-14-29-010-052 B. Get Access (1) Put the access platform in position at the access door 196BB. (2) Open the Yellow ground service panel access door 196BB.
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4. Procedure _________ (Ref. Fig. 303/TASK 12-14-29-991-003) Subtask 12-14-29-220-052 A. If the decrease in nitrogen pressure is more than 30 bar (435.1131 psi) (with respect to nominal pressure of accumulators) you must make sure that there are no leaks (Ref. TASK 29-10-00-200-801). Subtask 12-14-29-614-052 B. Fill the applicable accumulator with nitrogen. (1) Remove the blanking cap (2) from the charging valve (1). R
(2) Connect to the charging valve (1) the (98F29103500000) or a nitrogen bench capable of maxi pressure 150 bar (2175.5655 psi). (3) Loosen the charging valve nut (3). (4) Open the charging valve nut (3) slowly (turn to the OPEN direction) and fill the hydraulic power accumulator to the correct pressure for the ambient temperature.
R R R
NOTE : If you do this check immediately after aircraft landing, let ____ the pressure become stable for one hour to get a more accurate measurement (temperature compensation of the accumulator). NITROGEN PRESSURE ------------------------------------------------------------------------------| Temperature | Charging Pressure | |---------------------------|-------------------------------------------------| | deg.C | deg.F | bar | PSI | |-----------------------------------------------------------------------------| | -30 | -22 | 108 | 1566 | | -20 | - 4 | 112 | 1624 | | -10 | 14 | 116.5 | 1689 | | 0 | 32 | 121 | 1754 | | 10 | 50 | 125.5 | 1820 | | 20 | 68 | 130 | 1885 | | 30 | 86 | 134.5 | 1950 | | 40 | 104 | 139 | 2015 | | 50 | 112 | 143.5 | 2081 | | 60 | 140 | 148 | 2146 | ------------------------------------------------------------------------------(5) When the pressure is stable and correct, tighten the charging valve nut (3) (CLOSE position).
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Filling of the Yellow Power Accumulator Figure 303/TASK 12-14-29-991-003 EFF : ALL 12-14-29 SROS
Page 311 Apr 01/98
(6) Make sure that the pressure shown on the pressure gage is correct. (7) Stop the supply and remove the nitrogen filling system from the charging valve (1). R R
(8) TORQUE the charging valve nut (3) to between 10.7 and 11.8 m.daN (78.90 and 87.02 lbf.ft).
R
(9) Install the blanking cap (2) on the charging valve. 5. Close-up ________ Subtask 12-14-29-410-052 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the Yellow ground service panel 196BB. (3) Remove the access platform(s).
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Page 312 Jul 01/06
LANDING GEAR - SERVICING ________________________ TASK 12-14-32-614-801 Replenishment of the Tires WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED ON THE _______ LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. WARNING : LET THE BRAKES AND THE WHEELS BECOME COOL BEFORE YOU GO NEAR THE _______ LANDING GEAR. DO NOT APPLY A LIQUID OR GAS FIRE EXTINGUISHER DIRECTLY ON A HOT WHEEL OR BRAKE UNIT. THIS COULD CAUSE AN EXPLOSION. WARNING : USE ONLY DRY NITROGEN OR OTHER GASES TO INFLATE THE TIRES ON THE MAIN _______ GEAR WHEELS. THE OXYGEN IN THE GAS USED TO INFLATE THESE TIRES MUST NOT BE MORE THAN 5% (VOLUME). IF THE AIRCRAFT IS FAR FROM ITS BASE AND NO DRY NITROGEN IS AVAILABLE, YOU CAN USE AIR FOR THE SERVICING OF THE TIRES IF: - THE OXYGEN IN THE TIRES IS NOT MORE THAN 5% (VOLUME) OR - MAINTENANCE PERSONNEL REMOVE THE AIR FROM THE TIRES AND INFLATE THEM WITH DRY NITROGEN BEFORE 15 HOURS TIME SERVICE. A CHEMICAL REACTION BETWEEN THE OXYGEN IN THE TIRES AND GASES FROM THE INNER LINER CAN CAUSE A TIRE EXPLOSION. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R R R
No specific No specific No specific
1 ADAPTER - TIRE INFLATION/DEFLATION 1 CART - INFLATION, TIRE, NITROGEN 1 GAGE - PRESSURE, TIRE
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3. __________ Job Set-up Subtask 12-14-32-941-055 A. Preparation for Replenishment R
(1) Put the CART - INFLATION, TIRE, NITROGEN near the tire to be inflated. (2) Remove the tire-inflation valve cap.
R R
(3) Use a GAGE - PRESSURE, TIRE and a ADAPTER - TIRE INFLATION/DEFLATION to connect the inflation cart to the tire inflation valve. 4. Procedure _________ WARNING : DO NOT PUT COMPRESSED GAS IN CONTACT WITH YOUR SKIN. THE GAS CAN _______ GO THROUGH THE SKIN AND MAKE BUBBLES IN THE BLOOD. THIS CONDITION CAN KILL YOU. NOTE : AIRBUS recommends that when you inflate the tires, you use the ____ maximum normal pressure (given in the table). This is necessary to keep tire inflation to a minimum. NOTE : In the tables that follow the term loaded means with the aircraft ____ weight on the wheels. The term unloaded is when the applicable wheel is off the ground (jacked). Subtask 12-14-32-614-058-A A. Replenishment of the NLG Tires (1) Refer to the table to find the correct tire pressure. Inflate the tire with nitrogen. (2) If there is a large temperature decrease between the departure and the destination airports, the tire pressures given must be adjusted. If the temperature difference is more than 24 deg C lower, do this procedure: (a) Increase the given tire pressures 3.7% for each 10 deg C of temperature difference.
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EXAMPLE
Temperature at departure airport = 20 deg C Temperature at arrival airport = -10 deg C Temperature difference = 30 deg C Increase the tire pressure: 30/10 x 3.7% = 11.1% If the loaded tire pressure is 13.0 bar, increase the tire pressure: 13.0 bar +(13.0 bar x 11.1%) = 14.4 bar -------------------------------------------------------| TIRE DIMENSION | INFLATION PRESSURE | | AND TYPE |---------------------------------------| | | UNLOADED | LOADED | | | BAR (PSI) | BAR (PSI) | |----------------|-------------------|-------------------| | 1050 X 395R16 | 12.2 (177) normal | 12.7 (184) normal | | RADIAL | 12.8 (186) max | 13.3 (193) max | --------------------------------------------------------
Subtask 12-14-32-614-059 B. Replenishment of the MLG Tires (1) Refer to the table to find the correct tire pressure. Inflate the tire with nitrogen. (2) If there is a large temperature decrease between the departure and the destination airports, the tire pressures given must be adjusted. If the temperature difference is more than 24 deg C lower, do this procedure:
R R
(a) Increase the given tire pressures 3.7% for each 10 deg C of temperature difference. EXAMPLE
Temperature at departure airport = 20 deg C Temperature at arrival airport = -10 deg C Temperature difference = 30 deg C Increase the tire pressure: 30/10 x 3.7% = 11.1% If the loaded tire pressure is 13.0 bar, increase the tire pressure: 13.0 bar +(13.0 bar x 11.1%) = 14.4 bar
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-------------------------------------------------------| TIRE DIMENSION | INFLATION PRESSURE | | AND TYPE |---------------------------------------| | | UNLOADED | LOADED | | | BAR (PSI) | BAR (PSI) | |----------------|-------------------|-------------------| | 1400 X 530R23 | 13.6 (198) normal | 14.2 (206) normal | | RADIAL | | | | 54 X 21-23 | 14.3 (208) max | 14.9 (216) max | | BIAS | | | -------------------------------------------------------5. Close-up ________ Subtask 12-14-32-942-055 A. Removal of the Ground Support Equipment (1) Remove the inflation cart, pressure gage and adapter from the applicable tire. R R
(2) Remove the CART - INFLATION, TIRE, NITROGEN, GAGE - PRESSURE, TIRE and ADAPTER - TIRE INFLATION/DEFLATION from the applicable tire.
R
(3) Install the tire-inflation valve cap.
R
(4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
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TASK 12-14-32-614-802 Gas Replenishment of the MLG Shock Absorber WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED ON THE _______ LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. 1. __________________ Reason for the Job NOTE : You can complete this procedure with the aircraft on the ground or on ____ jacks. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No
specific specific specific specific specific specific specific specific
460007156
nitrogen source pressure gage 0 - 200 bar pressure gage 0 - 60 bar standard charging equipment thermometer warning notice access platform 3 m (9 ft. 10 in.) Torque Wrench : range 0.00 to 1.20 m.daN (0.00 to 9.00 lbf.ft) 1 ADAPTER, CHARGING - MLG
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B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 05-004B Material No. 19-010
USA MIL-L-25567 TYPE I OXYGEN LEAK DETECTOR (Ref. 20-31-00) USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-804 32-00-00-481-801
R R
32-12-00-010-801 32-12-00-410-801 12-14-32-991-001 12-14-32-991-031 12-14-32-991-002-A
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Installation of the Safety Devices on the Landing Gears Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Fig. 301 Fig. 302 Fig. 303
3. __________ Job Set-up Subtask 12-14-32-941-050 A. Safety Precautions (1) Put the warning notice in the cockpit to tell persons not to operate the landing gear controls. Subtask 12-14-32-860-050 B. Aircraft Maintenance Configuration (1) Make sure that the Green hydraulic system is depressurized (Ref. TASK 29-00-00-864-804). (2) Make sure that the safety devices are installed on the L/G (Ref. TASK 32-00-00-481-801).
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Subtask 12-14-32-010-054 C. Get Access (Ref. Fig. 301/TASK 12-14-32-991-001) (1) Open the applicable MLG door (Ref. TASK 32-12-00-010-801). (2) Put an access platform adjacent to the applicable MLG: - for the LH MLG at zone 731 - for the RH MLG at zone 741. (3) Remove and discard the lockwire from the bolts (5). (4) Remove the bolts (5), the washers (4), the bracket (3) and the panel (2). 4. Procedure _________ (Ref. Fig. 302/TASK 12-14-32-991-031, 303/TASK 12-14-32-991-002-A) Subtask 12-14-32-614-050 R
A. Gas Replenishment of the MLG Shock Absorber (Aircraft on the Ground) CAUTION : DO NOT INFLATE THE MLG SHOCK ABSORBER AT THE LOWER VALVE. IF _______ YOU USE THE LOWER VALVE HYDRAULIC FLUID WILL COME OUT. (1) Measure and write down the shock absorber extension (dimension H).
R
(2) Connect the nitrogen source to the standard charging equipment.
R
(3) Install the ADAPTER, CHARGING - MLG to the standard charging equipment. (4) Install the ADAPTER, CHARGING - MLG on the bleed/inflation valve (1). (5) Open the bleed/inflation valve (1). (6) Read and write down the pressure shown on the pressure gage 0 - 200 bar. (7) Close the bleed/inflation valve (1).
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MLG Bleed/Inflation Valve Figure 301/TASK 12-14-32-991-001 EFF : ALL 12-14-32 SROS
Page 308 Apr 01/98
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Shock Absorber Dimension H Figure 302/TASK 12-14-32-991-031
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MLG Shock Absorber Inflation Chart Figure 303/TASK 12-14-32-991-002-A12 (SHEET 1)
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MLG Shock Absorber Inflation Chart Figure 303/TASK 12-14-32-991-002-A22 (SHEET 2)
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(8) Do these steps: (a) Use a thermometer to measure and write down the surface temperature of the aluminium piston adjacent to the bleed inflation valve (1). (b) Use the inflation chart to find the correct pressure from the temperature and dimension H measurements you recorded. (9) If the pressure measured at step (6) is lower than the pressure got from the inflation chart, do this procedure: WARNING : DO NOT PUT COMPRESSED GAS IN CONTACT WITH YOUR SKIN. THE _______ GAS CAN GO THROUGH THE SKIN AND MAKE BUBBLES IN THE BLOOD. THIS CONDITION CAN KILL YOU. (a) Adjust the nitrogen source to give the necessary pressure. (b) Slowly open the bleed/inflation valve (1). (c) Inflate the shock absorber to the correct pressure shown on the inflation chart. (d) When the pressure is correct, close the bleed/inflation valve (1). If dimension H changes (before the correct pressure has been reached), measure dimension H again and do the steps from (8)(b) again with the new dimension H. (e) Close the charge valve on the nitrogen source and leave for a minimum of 10 minutes (to let the shock absorber stabilize). (f) Measure the pressure and dimension H again. (g) If the pressure has changed, do the steps (c) and (d) again. If the dimension H has changed, do the steps from (8)(b) again with the new dimension H. (h) Close the bleed/inflation valve (1). R R
(i) Stop the supply from the nitrogen source. Release the pressure and remove the nitrogen source from the standard charging equipment.
R
(j) Remove the standard charging equipment from the ADAPTER, CHARGING - MLG.
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(k) TORQUE the bleed/inflation valve (1) to between 0.60 and 0.8 m.daN (50 and 70 lbf.in). (l) Remove the ADAPTER, CHARGING - MLG from the bleed/inflation valve (1). CAUTION : DO NOT INSTALL A DUST CAP ON THE BLEED/INFLATION VALVE _______ OF THE MLG SHOCK ABSORBER. IF YOU DO, THERE IS A RISK THAT IT WILL FALL INTO THE SHOCK ABSORBER. 1 _
Do not install a dust cap on the bleed/inflation valve.
(m) Use SPECIAL MATERIALS (Material No. 05-004B) to do a leak test of the bleed/inflation valve (1). Leakage must not occur. (10) If the pressure measured at step (6) is higher than the pressure got from the inflation chart, do this procedure: (a) Slowly open the bleed/inflation valve (1). (b) Deflate the shock absorber to the correct pressure you got at step (8)(b) from the inflation chart. If the dimension H changes (before the correct pressure has been reached), measure the dimension H again. Do the steps from (8)(b) again with the new dimension H. (c) Close the charge valve on the nitrogen source and leave for a minimum of 10 minutes (to let the shock absorber stabilize). (d) Measure the pressure and the dimension H again. (e) If the pressure has changed, do the steps (b) and (c) again. If the dimension H has changed, do the steps from (8)(b) again. Use the new dimension H. (f) Close the bleed/inflation valve (1). R
(g) Remove the nitrogen source from the standard charging equipment.
R
(h) Remove the standard charging equipment from the ADAPTER, CHARGING - MLG. (i) TORQUE the bleed/inflation valve (1) to between 0.60 and 0.8 m.daN (50 and 70 lbf.in).
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(j) Remove the ADAPTER, CHARGING - MLG. CAUTION : DO NOT INSTALL A DUST CAP ON THE BLEED/INFLATION VALVE _______ OF THE MLG SHOCK ABSORBER. IF YOU DO, THERE IS A RISK THAT IT WILL FALL INTO THE SHOCK ABSORBER. 1 _
Do not install a dust cap on the bleed/inflation valve.
(k) Use the SPECIAL MATERIALS (Material No. 05-004B) to do a leak test of the bleed/inflation valve (1). Leakage must not occur. Subtask 12-14-32-614-051 B. Gas Replenishment of the MLG Shock Absorber (Aircraft on Jacks). WARNING : DO NOT PUT COMPRESSED GAS IN CONTACT WITH YOUR SKIN. THE GAS _______ CAN GO THROUGH THE SKIN AND MAKE BUBBLES IN THE BLOOD. THIS CONDITION CAN KILL YOU. CAUTION : DO NOT INFLATE THE MLG SHOCK ABSORBER AT THE LOWER VALVE. IF _______ YOU USE THE LOWER VALVE HYDRAULIC FLUID WILL COME OUT. (1) Make sure that the shock absorber is extended fully and the dimension H is between 773.5 mm (30.4527 in.) and 782.5 mm (30.8071 in.). (2) Do these steps: (a) Use a thermometer to measure and then write down the surface temperature of the aluminium piston adjacent to the bleed/inflation valve (1). (b) Look at the inflation chart and find the nearest fully extended inflation pressure (for the temperature you measured at step (a)). (3) Install the ADAPTER, CHARGING - MLG on the bleed/inflation valve (1). R
(4) Install the GEAR FILLING KIT-SHOCK ABSORBER or the standard charging equipment on the ADAPTER, CHARGING - MLG. (5) Set the nitrogen charge pressure to the inflation pressure you found at step (2)(b). Make sure the pressure control valve or the shut-off valve is closed. (6) Open the bleed/inflation valve (1) and read the pressure gage 0 - 60 bar.
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Page 315 Apr 01/03
(7) To get the correct shock absorber pressure you calculated at step (2)(b): - open the pressure control valve to inflate the shock absorber OR - open the bleed control valve to deflate the shock absorber. (8) Inflate or deflate the shock absorber to get the correct pressure you calculated at step (2). (9) Close the nitrogen charge valve. (10) After a period of 10 minutes (to let the shock absorber become stable), measure the pressure again. (11) If the pressure has changed, do the steps (6) thru (8) again. (12) Close the bleed/inflation valve (1). (13) Stop the nitrogen supply and remove the nitrogen source from the GEAR FILLING KIT-SHOCK ABSORBER or the standard charging equipment. (14) Remove the GEAR FILLING KIT-SHOCK ABSORBER or the standard charging equipment from the ADAPTER, CHARGING - MLG. (15) TORQUE the bleed/inflation valve (1) to between 0.60 and 0.8 m.daN (50 and 70 lbf.in). (16) Remove the ADAPTER, CHARGING - MLG. CAUTION : DO NOT INSTALL A DUST CAP ON THE BLEED/INFLATION VALVE OF _______ THE MLG SHOCK ABSORBER. IF YOU DO, THERE IS A RISK THAT IT WILL FALL INTO THE SHOCK ABSORBER. (a) Do not install a dust cap on the bleed/inflation valve. (17) Use the SPECIAL MATERIALS (Material No. 05-004B) to do a leak test of the Bleed/inflation valve (1). Leakage must not occur. 5. Close-up ________ Subtask 12-14-32-410-050 A. Close Access (1) Install the access panel (2) with the bracket (3), the washers (4) and the bolts (5). (a) TORQUE tighten the bolts (5) to 0.34 m.daN (30.08 lbf.in).
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(b) Safety the bolts (5) with MISCELLANEOUS (Material No. 19-010). (2) Remove the access platform(s). (3) Close the applicable MLG door (Ref. TASK 32-12-00-410-801). Subtask 12-14-32-942-050 B. Removal of Equipment (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
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TASK 12-14-32-614-804 Gas Replenishment of the NLG Shock Absorber WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED ON THE _______ LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. 1. __________________ Reason for the Job This task gives the procedure for gas replenishment when the aircraft is on the ground and when the aircraft is on jacks. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No No R
specific specific specific specific specific specific specific specific specific
U21891000
nitrogen source pressure gage 130 bar pressure gage 20 bar pressure gage 80 bar safety barriers standard charging equipment warning notices access platform 2.5 m (8 ft. 2 in.) Torque Wrench : range 0.00 to 1.20 m.daN (0.00 to 9.00 lbf.ft) 2 ADAPTOR - INFLATION
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B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 05-004B
USA MIL-L-25567 TYPE I OXYGEN LEAK DETECTOR (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-804 32-00-00-481-801 32-00-00-860-805 32-00-00-860-806 32-22-00-010-801 32-22-00-410-801 32-51-00-040-801 12-14-32-991-006 12-14-32-991-005 12-14-32-991-027 12-14-32-991-026 12-14-32-991-029
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Installation of the Safety Devices on the Landing Gears Ground Configuration after Flight Configuration Put the Aircraft in a Ground Configuration when it is Raised on Jacks Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance Deactivation of the Nose Wheel Steering Fig. 304 Fig. 305 Fig. 306 Fig. 307 Fig. 308
3. __________ Job Set-up Subtask 12-14-32-941-054 A. Safety Precautions (1) Put the warning notices in the cockpit to tell persons not to: - operate the landing gear controls - operate the nose wheel steering controls.
R
(2) Put the safety barriers in position.
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Subtask 12-14-32-860-054 B. Aircraft Maintenance Configuration NOTE : Do not install chocks to the NLG or the CLG during this procedure. ____ (1) Put the aircraft in: (a) Ground configuration after flight configuration, (Ref. TASK 3200-00-860-805). R R
(b) Aircraft in ground configuration when it is raised on jacks, (Ref. TASK 32-00-00-860-806). (2) Put the nose wheels in a central position. (3) Make sure that the green hydraulic system is depressurized, (Ref. TASK 29-00-00-864-804). (4) Deactivate the nose wheel steering NW/S, (Ref. TASK 32-51-00-040801). (5) Install the safety devices on the landing gear, (Ref. TASK 32-00-00481-801). Subtask 12-14-32-010-050 C. Get Access (1) Open the NLG doors (Ref. TASK 32-22-00-010-801). (2) Put the access platform adjacent to the NLG. 4. Procedure _________ (Ref. Fig. 304/TASK 12-14-32-991-006) Subtask 12-14-32-614-056
R
A. Gas Replenishment of the NLG Shock Absorber (Aircraft on the Ground) (Ref. Fig. 305/TASK 12-14-32-991-005) WARNING : DO NOT PUT COMPRESSED GAS IN CONTACT WITH YOUR SKIN. THE GAS _______ CAN GO THROUGH THE SKIN AND MAKE BUBBLES IN THE BLOOD. THIS CONDITION CAN KILL YOU.
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NLG - Pressure/Extension Graph 1 Figure 304/TASK 12-14-32-991-006
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Page 321 Apr 01/04
NLG Shock Absorber - Inflation Valves Figure 305/TASK 12-14-32-991-005
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(1) Remove the blanking caps (1) and (3) from the inflation valves (2) and (4). (2) Install the nitrogen source to the standard charging equipment. R R
(3) Install the standard charging equipment to supply each ADAPTOR INFLATION. Connect a pressure gage 130 bar to each of the charging valves (2) and (4).
R
(4) Install a ADAPTOR - INFLATION on the inflation valves (2) and (4). (5) Open the inflation valves (2) and (4). (6) Measure and write down the ambient temperature (temperature T1). (7) Read and write down the pressure at the inflation valve (2) (pressure P1) and at the inflation valve (4) (pressure P2).
R R
(8) If the pressure at P2 is less than the pressure at P1 plus 6.9 bar (100 psi): (a) Open the shut off valves X and Z. (b) Slowly pressurize the inflation valve (4) until the pressure at P2 is 6.9 bar (100 psi) more than the pressure at P1. NOTE : This makes sure that the floating piston goes against its ____ stop in the fully up position. (9) Measure and write down the shock absorber extension (dimension H). (10) Close the shut off valve Z and open the shut off valve Y. (a) Slowly add or remove nitrogen at the inflation valve (2) until the dimension H plus or minus 1 mm (0.04 in) agrees with the pressure P1 shown on the graph at ambient temperature T1. (Ref. Fig. 306/TASK 12-14-32-991-027) (11) Compare the pressure P1 and the pressure P2. If the pressure P2 is more than the pressure at P1, do paragraphs (13) thru (23). NOTE : If the pressure P2 is more than the pressure P1, this shows ____ that the floating piston has stayed against the stop in the fully up position. (12) If the pressure P2 is equal to or less than the pressure at P1, do paragraphs (5) thru (11) again.
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R
NLG - Pressure/Extension Graph ( C) Figure 306/TASK 12-14-32-991-027
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(13) Use the pressure P1 and T1 and find the position of P1 in relation to the Nominal pressure line on the graph. (Ref. Fig. 307/TASK 12-14-32-991-026) (14) If the measured pressure P1 is above the Nominal line shown on the graph, do this step: (a) Close the shut off valve Y and open the shut off valve Z. (b) Slowly remove nitrogen at the inflation valve (4) until the dimension H plus or minus 1 mm (0.04 in) agrees with the graph at pressure P1 and temperature T1. (Ref. Fig. 304/TASK 12-14-32-991-006) NOTE : The floating piston moves away from the stop. ____ (c) Compare the pressure P1 and P2. If the pressure P2 is the same as pressure P1, do paragraphs (16) to (23). (15) If the measured pressure P1 is equal to or below the Nominal line shown on the graph, do this step: (a) Slowly decrease the pressure at the inflation valve (4) until the pressure P2 agrees with the graph. (Ref. Fig. 307/TASK 12-14-32-991-026) NOTE : The floating piston stays against the stop. ____ (b) Compare the pressures P1 and P2. If the pressure P2 is more than the pressure P1 do the paragraphs (16) thru (23). (16) Close the inflation valves (2) and (4). (17) Stop the supply from the nitrogen source. Release the pressure and remove the nitrogen source from the standard charging equipment. R
(18) Remove the standard charging equipment from each ADAPTOR - INFLATION.
R
(19) Remove each ADAPTOR - INFLATION from the inflation valves (2) and (4). (20) TORQUE the inflation valves (2) and (4) to between 0.5 and 0.8 m.daN (44.24 and 70.79 lbf.in). (21) Use the SPECIAL MATERIALS (Material No. 05-004B) to do a leak test of the inflation valves (2) and (4). Leakage must not occur.
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NLG Shock Absorber - Pressure/Temperature Graph Figure 307/TASK 12-14-32-991-026
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(22) Install the blanking caps (1) and (3) on the inflation valves (2) and (4). (23) Close the NLG doors (Ref. TASK 32-22-00-410-801). Subtask 12-14-32-614-057 B. Gas Replenishment of the NLG Shock Absorber (Aircraft on Jacks) (Ref. Fig. 305/TASK 12-14-32-991-005, 308/TASK 12-14-32-991-029) (1) Make sure that the shock absorber is extended fully and the dimension H is between 408 and 416 mm (16.07 and 16.37 in). (2) Remove the blanking caps (1) and (3) from the inflation valves (2) and (4). R
(3) Install a ADAPTOR - INFLATION on each of the inflation valves (2) and (4).
R
(4) Install the GEAR FILLING KIT-SHOCK ABSORBER or the standard charging equipment to supply each ADAPTOR - INFLATION. Make sure that the pressure gage 20 bar connects to the charging valve (2) and the pressure gage 80 bar connects to the charging valve (4) (5) Measure and write down the ambient temperature. (6) Make sure that the shut-off valve Z is closed and open the inflation valve (4) with the ADAPTOR - INFLATION.
R
(7) Read and write down the pressure shown on the pressure gage for the inflation valve (4)(Pressure P2). (8) Compare the values with the values shown on the graph. (Ref. Fig. 307/TASK 12-14-32-991-026) (9) If the nitrogen pressure is not correct for the ambient temperature on the graph, do this procedure: WARNING : DO NOT PUT COMPRESSED GAS IN CONTACT WITH YOUR SKIN. THE _______ GAS CAN GO THROUGH THE SKIN AND MAKE BUBBLES IN THE BLOOD. THIS CONDITION CAN KILL YOU. (a) Open the shut-off valve X and Z and adjust the nitrogen-source supply pressure to the correct figure shown on the graph. (b) Close the shut-off valves X and Z and stop the supply from the nitrogen source.
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Pressure/Temperature Graph 2 Figure 308/TASK 12-14-32-991-029
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(10) Close the inflation valve (4). (11) Make sure that the shut-off valve Y is closed and open the inflation valve (2) with the ADAPTOR - INFLATION.
R
(12) Read and write down the pressure shown on the pressure gage for the inflation valve (2)(Pressure P1). (13) Compare the values with the values shown on the graph. (Ref. Fig. 308/TASK 12-14-32-991-029) (14) If the nitrogen pressure is not correct for the ambient temperature on the graph, do this procedure: WARNING : DO NOT PUT COMPRESSED GAS IN CONTACT WITH YOUR SKIN. THE _______ GAS CAN GO THROUGH THE SKIN AND MAKE BUBBLES IN THE BLOOD. THIS CONDITION CAN KILL YOU. (a) Open the shut-off valve X and Y and adjust the nitrogen-source supply pressure to the correct figure shown on the graph. (b) Close the shut-off valves X and Y and stop the supply from the nitrogen source. (15) Close the inflation valve (2). (16) Repeat steps (5) thru (15) and make sure that the pressures P1 and P2 are correct. R
(17) Remove the GEAR FILLING KIT-SHOCK ABSORBER or the standard charging equipment from each ADAPTOR - INFLATION.
R
(18) Remove the ADAPTOR - INFLATION from each inflation valve. (19) TORQUE the inflation valve (2) and (4) to between 0.5 and 0.8 m.daN (44.24 and 70.79 lbf.in). (20) Install the blanking caps (1) and (3) to the inflation valves (2) and (4). (21) Use the SPECIAL MATERIALS (Material No. 05-004B) to do a leak test of the inflation valves (2) and (4). Leakage must not occur. 5. Close-up ________ Subtask 12-14-32-942-054 A. Removal of the Ground Support Equipment (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
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TASK 12-14-32-614-807 Pressurization of the Brake Accumulator (5258GG, 5259GG, 5490GG, 5491GG, 5426GG, 5427GG) WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED ON THE _______ LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. WARNING : MAKE SURE THAT THE WHEEL CHOCKS ARE IN POSITION. MOVEMENTS OF THE _______ AIRCRAFT COULD BE DANGEROUS. 1. __________________ Reason for the Job NOTE : The Alternate Brake Return Accumulator is part of the Manifold ____ 5490GG(5491GG). 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R R
No No No No No
specific specific specific specific specific
accumulator filling system circuit breaker(s) safety clip(s) warning notice access platform 2.1 m (6 ft. 11 in.) Torque Wrench : range 0.00 to 1.20 m.daN (0.00 to 9.00 lbf.ft)
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B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-804 32-45-00-864-801 R R R R
12-14-32-991-007 12-14-32-991-012 12-14-32-991-014 12-14-32-991-020
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Release the Pressure from the Parking Brake System after Depressurization Fig. 309 Fig. 310 Fig. 311 Fig. 312
3. __________ Job Set-up Subtask 12-14-32-941-056 A. Safety Precautions WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. (1) Put the warning notice in the cockpit to tell persons not to pressurize the Blue or Green hydraulic systems. Subtask 12-14-32-860-055 B. Aircraft Maintenance Configuration (1) Put the wheel chocks in position. (2) On the panel 117VU, set the PARK BRK to the OFF position. (3) Make sure that the hydraulic systems are depressurized (Ref. TASK 2900-00-864-804). (4) Release the pressure from the Parking Brake system after depressurization (Ref. TASK 32-45-00-864-801).
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Subtask 12-14-32-010-052 C. Get Access (1) Put the access platform in the applicable position: FOR 5426GG, 5427GG at the zone 195 FOR 5258GG, 5259GG, 5490GG, 5491GG at the zone 731(741). Subtask 12-14-32-865-059 D. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU HYD PUMP G CTL 9JV U09 721VU HYD PUMP B CTL 9JC X12 722VU BSCU SYS 2 2GG U37 742VU BSCU SYS 1 1GG G62 4. Procedure _________ (Ref. Fig. 309/TASK 12-14-32-991-007) Subtask 12-14-32-614-061 R
A. Pressurize the Brake Return Accumulator (5258GG, 5259GG, 5490GG, 5491GG) (1) Remove the cap (1). (2) Install the accumulator filling system on the applicable charge valve. (3) Set the nitrogen supply pressure on the gage to 1 bar (14.5037 psi) more than the correct pressure for the related ambient temperature.
R R
CAUTION : MAKE SURE THAT YOU USE THE CORRECT PRESSURE CHART. THIS _______ PREVENTS DAMAGE TO THE HYDRAULIC SYSTEM COMPONENTS. (Ref. Fig. 310/TASK 12-14-32-991-012)
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Brake Accumulators - Location and Detail Figure 309/TASK 12-14-32-991-007
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Brake Return Accumulators - Pressure Graph Figure 310/TASK 12-14-32-991-012
EFF : ALL 12-14-32 SROS
Page 335 Jan 01/07
(4) Slowly open the control nut (2) on the charge valve. NOTE : When the charge valve is opened initially, the pressure will ____ decrease to approximately 1 bar (14.5 psi) less than the correct pressure. It will then slowly increase. (5) Close the control nut (2) when the needle on the accumulator pressure gage goes through the correct pressure. (6) TORQUE the control nut (2) to between 0.5 and 0.85 m.daN (44.24 and 75.22 lbf.in). (7) Stop the nitrogen supply. (8) Let the accumulator stay for approximately 10 minutes for its temperature to become stable. (9) Make sure that the accumulator gage needle is in the green sector. (10) Remove the accumulator filling system and check for leakage. (11) Install the cap (1). (12) TORQUE the cap (1) to between 0.1 and 0.12 m.daN (8.84 and 10.61 lbf.in). Subtask 12-14-32-614-067 R
B. Pressurize the Alternate Brake 6L Accumulators (5426GG, 5427GG) (1) Remove the cap (1). (2) Install the accumulator filling system on the applicable charge valve. (3) Set the supply pressure to the correct pressure for the related ambient temperature.
R R
CAUTION : MAKE SURE THAT YOU USE THE CORRECT PRESSURE CHART. THIS _______ PREVENTS DAMAGE TO THE HYDRAULIC SYSTEM COMPONENTS. (Ref. Fig. 311/TASK 12-14-32-991-014) (4) Open the control nut (2) and slowly pressurize the accumulator to the correct pressure for the related ambient temperature.
EFF : ALL 12-14-32 SROS
Page 336 Jul 01/06
R
Alternate Brake 6L Accumulators - Pressure Graph Figure 311/TASK 12-14-32-991-014
EFF : ALL 12-14-32 SROS
Page 337 Jul 01/06
(5) Let the filling system and accumulator pressure become equal and close the control nut (2). (Ref. Fig. 312/TASK 12-14-32-991-020) NOTE : The other accumulator will show a pressure increase. ____ This is an incorrect indication. (6) TORQUE the control nut (2) to between 0.5 and 0.85 m.daN (44.24 and 75.22 lbf.in). (7) Release the pressure from the Parking Brake System (Ref. TASK 32-4500-864-801). (8) Do the steps 1 thru 7 again for the other accumulator. NOTE : It is possible that you will need to do the steps 1 thru 7 ____ more than once for each accumulator, until a correct stable pressure shows. (9) Let the accumulator stay for approximately 10 minutes for its temperature to become stable. (10) Make sure that the accumulator gage shows the correct pressure. (11) Remove the accumulator filling system and check for leakage. (12) Install the cap (1). (13) TORQUE the cap (1) to between 0.1 and 0.12 m.daN (8.84 and 10.61 lbf.in). 5. Close-up ________ Subtask 12-14-32-865-060 A. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GG, 2GG, 9JC, 9JV. Subtask 12-14-32-942-056 B. Removal of Equipment (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 12-14-32 R SROS
Page 338 Jul 01/06
Alternate Park Brake Accumulators - Location and Detail Figure 312/TASK 12-14-32-991-020 EFF : ALL 12-14-32 R SROS
Page 339 Jul 01/06
TASK 12-14-32-614-811 Depressurization of the Brake Accumulator (5258GG, 5259GG, 5490GG, 5491GG, 5426GG and 5427GG) WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED ON THE _______ LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. WARNING : MAKE SURE THAT THE WHEEL CHOCKS ARE IN POSITION. MOVEMENTS OF THE _______ AIRCRAFT COULD BE DANGEROUS. 1. __________________ Reason for the Job NOTE : The Alternate Brake Return Accumulator is part of the Manifold ____ 5490GG(5491GG). 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific No specific No specific
circuit breaker(s) safety clip(s) warning notice access platform 2.1 m (6 ft. 11 in.)
EFF : ALL 12-14-32 SROS
Page 340 Jan 01/05
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-804 32-12-14-400-801 32-42-41-000-801 32-42-41-400-801 32-43-00-870-801 32-43-24-000-801 32-43-24-400-801 32-45-00-864-801 R R R
12-14-32-991-009 12-14-32-991-010 12-14-32-991-011 FOR FIN 5490GG, 5491GG 32-12-14-000-801
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Installation of the MLG Fixed Fairing Assembly Removal of the MLG Normal Brake Return Accumulator 5258GG(5259GG) Installation of the MLG Normal Brake Return Accumulator 5258GG(5259GG) Bleeding the Alternate Braking System at the Wheel Brakes Removal of the MLG Alternate Brake Return Accumulator Installation of the MLG Alternate Brake Return Accumulator Release the Pressure from the Parking Brake System after Depressurization Fig. 313 Fig. 314 Fig. 315 Removal of the MLG Fixed Fairing Assembly
3. __________ Job Set-up Subtask 12-14-32-941-057 A. Safety Precautions WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. (1) Put the warning notice in the cockpit to tell persons not to pressurize the hydraulic systems. Subtask 12-14-32-860-056 B. Aircraft Maintenance Configuration (1) Put the wheel chocks in position. (2) On the panel 117VU, set the PARK BRK to the OFF position.
EFF : ALL 12-14-32 SROS
Page 341 Apr 01/04
(3) Make sure that the hydraulic systems are depressurized (Ref. TASK 2900-00-864-804) (4) Make sure that the Park Brake accumulators are depressurized (Ref. TASK 32-45-00-864-801). Subtask 12-14-32-010-053 C. Get Access (1) Put the access platform in the applicable position: FOR 5426GG, 5427GG at the zone 195 FOR 5258GG, 5259GG, 5490GG, 5491GG at the zone 731(741). (2) FOR 5490GG, 5491GG remove the fixed fairing assembly (Ref. TASK 32-12-14-000-801). Subtask 12-14-32-865-061 D. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU HYD PUMP G CTL 9JV U09 721VU HYD PUMP B CTL 9JC X12 722VU BSCU SYS 2 2GG U37 742VU BSCU SYS 1 1GG G62 4. Procedure _________ Subtask 12-14-32-614-062 R
A. Depressurization of the Brake Accumulator (5258GG and 5259GG) (Ref. Fig. 313/TASK 12-14-32-991-009) (1) Remove the applicable return Brake accumulator (Ref. TASK 32-42-41000-801), but do not disconnect the hydraulic connectors. (2) Put the accumulator in the vertical position with the pressure gage (2) at the top.
EFF : ALL 12-14-32 SROS
Page 342 Apr 01/04
Brake Accumulators - Location and Detail Figure 313/TASK 12-14-32-991-009
R
EFF : ALL 12-14-32 SROS
Page 343 Apr 01/04
(3) Remove the cap (3). (4) Carefully loosen the control nut (1) and let the pressure decrease to zero on the pressure gage (2). (5) Close the control nut (1). (6) Install the cap (3). (7) Install the accumulator (Ref. TASK 32-42-41-400-801). Subtask 12-14-32-614-063 R
B. Depressurization of the Brake Accumulator (5490GG and 5491GG) (Ref. Fig. 314/TASK 12-14-32-991-010) (1) Remove the accumulator (Ref. TASK 32-43-24-000-801). (2) Hold the accumulator in the vertical position with the pressure gage (2) at the top. (3) Remove the cap (3). (4) Carefully loosen the control nut (1) and let the pressure decrease to zero on the pressure gage (2). NOTE : An amount of hydraulic fluid can come out with the nitrogen. ____ This is normal and further maintenance is not necessary. (5) Close the control nut (1). (6) Install the cap (3). (7) Install the accumulator (Ref. TASK 32-43-24-400-801). (8) Bleed the Blue hydraulic system (Ref. TASK 32-43-00-870-801). (9) Install the fixed fairing assembly (Ref. TASK 32-12-14-400-801). Subtask 12-14-32-614-064
R
C. Depressurization of the Park Brake Accumulator (5426GG, 5427GG) (Ref. Fig. 315/TASK 12-14-32-991-011) (1) Remove the cap (2). (2) Carefully loosen the control nut (3) and let the pressure decrease to zero on the pressure gage (1). (3) Close the control nut (3).
EFF : ALL 12-14-32 SROS
Page 344 Apr 01/04
Brake Accumulators - Location and Detail Figure 314/TASK 12-14-32-991-010
R
EFF : ALL 12-14-32 SROS
Page 345 Apr 01/04
Brake Accumulators - Location and Detail Figure 315/TASK 12-14-32-991-011
R
EFF : ALL 12-14-32 SROS
Page 346 Apr 01/04
(4) Install the cap (2). 5. Close-up ________ Subtask 12-14-32-942-057 A. Removal of Equipment (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 12-14-32 R SROS
Page 347 Jul 01/03
TASK 12-14-32-614-814 Depressurization of the Nose Wheel Steering Accumulator 5110GC WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED ON THE _______ LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No No No No No No
specific specific specific specific specific specific
bleed hose circuit breaker(s) safety clip(s) safety barriers warning notices container 2.0 l (0.5283 USgal) access platform 2.0 m (6 ft. 7 in.)
EFF : ALL 12-14-32 SROS
Page 348 Jan 01/05
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-14-32-614-812 29-00-00-864-801 29-14-00-614-801 R 32-51-00-040-801 12-14-32-991-015
Pressurization of the Nose Wheel Steering Accumulator 5110GC Depressurize the Green Hydraulic System (Pressurized with the Electric Pump) Depressurization of the Green Hydraulic Reservoir with Ground Equipment Deactivation of the Nose Wheel Steering Fig. 316
3. __________ Job Set-up Subtask 12-14-32-941-069 A. Safety Precautions (1) Put the safety barriers in position. (2) Put the warning notices in these positions: - on the ground services panel, to tell persons not to pressurize the Green hydraulic system - on the panel 245VU, to tell persons not to pressurize the Green hydraulic system. Subtask 12-14-32-860-062 B. Aircraft Maintenance Configuration (1) Deactivate the Nose Wheel Steering (Ref. TASK 32-51-00-040-801). (2) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (3) Depressurize the reservoir of the Green hydraulic system (Ref. TASK 29-14-00-614-801).
EFF : ALL 12-14-32 SROS
Page 349 Apr 01/05
Subtask 12-14-32-865-073 C. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------722VU BSCU SYS 2 2GG U37 742VU BSCU SYS 1 1GG G62 4. Procedure _________ Subtask 12-14-32-614-068 A. Depressurization of the Nose Wheel Steering Accumulator WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. R
(Ref. Fig. 316/TASK 12-14-32-991-015) (1) Put the access platform in position adjacent to the NWS hydraulic block. (2) Cut, remove and discard the lockwire from the cover (1). (3) Remove the cover (1) and the dustcap (2). (4) Slowly open the charge valve to release the pressure. (5) Close the charge valve and temporarily install the dustcap (2) and the cover (1). (6) To release the hydraulic pressure remaining in the Nose Wheel Steering System, do these steps: (a) Put a container below the bleed valve. (b) Remove the cap (3). (c) Put a bleed hose on the bleed valve. (d) Slowly loosen the bleed valve to release the hydraulic pressure. (e) When the flow of hydraulic fluid stops, tighten the bleed valve and remove the bleed hose.
EFF : ALL 12-14-32 SROS
Page 350 Apr 01/04
Nose Wheel Steering Accumulator - Location and Detail Figure 316/TASK 12-14-32-991-015
R
EFF : ALL 12-14-32 SROS
Page 351 Apr 01/04
(f) Install the cap (3) on the bleed valve. 5. Close-up ________ Subtask 12-14-32-860-061 A. Aircraft Maintenance Configuration (1) When the related maintenance operation is complete, pressurize the Nose Wheel Steering accumulator (Ref. TASK 12-14-32-614-812).
EFF : ALL 12-14-32 R SROS
Page 352 Jul 01/03
TASK 12-14-32-614-812 Pressurization of the Nose Wheel Steering Accumulator 5110GC WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED ON THE _______ LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No
specific specific specific specific specific specific specific
container pressure gage safety barriers thermometer warning notices Nitrogen Filling System access platform 2.0 m (6 ft. 7 in.)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------No specific
lockwire, corrosion resistant steel 0.8 mm (0.032 in.)
EFF : ALL 12-14-32 R SROS
Page 353 Apr 01/04
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-802 29-00-00-864-801 29-14-00-614-801 R 12-14-32-991-015
Fill the Green Hydraulic Reservoir with a Hand Pump Depressurize the Green Hydraulic System (Pressurized with the Hydraulic Ground Supply) Depressurization of the Green Hydraulic Reservoir with Ground Equipment Fig. 316
3. __________ Job Set-up Subtask 12-14-32-941-058 A. Safety Precautions (1) Put the safety barriers in position. (2) Put the warning notices in the cockpit and on the ground services panel to tell persons: - not to pressurize the Green hydraulic system - not to pressurize the Green hydraulic system reservoir. Subtask 12-14-32-860-059 B. Aircraft Maintenance Configuration (1) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (2) Depressurize the Green hydraulic system reservoir (Ref. TASK 29-1400-614-801). (3) Put the access platform in position at the NLG leg. Subtask 12-14-32-865-071 C. Get access to the avionics compartment. Then make sure that this(these) circuit breaker(s) is (are) open, safetied and tagged: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------722VU BSCU SYS 2 2GG U37 742VU BSCU SYS 1 1GG G62
EFF : ALL 12-14-32 SROS
Page 354 Apr 01/05
4. Procedure _________ Subtask 12-14-32-614-066 R
A. Pressurization of the NWS Accumulator with Nitrogen (Ref. Fig. 316/TASK 12-14-32-991-015) (1) Remove the cap (3) from the hydraulic bleed valve. (2) Put a container in position below the bleed valve. (3) Open the bleed valve. NOTE : The flow of hydraulic fluid from the bleed valve can stop and ____ start again as the accumulator is filled. (4) Remove and discard the lockwire from the cover (1). (5) Remove the cover (1) and the dust cap (2) from the charge valve. (6) Install the Nitrogen Filling System on the charge valve. (7) Slowly open the charge valve to pressurize the NWS accumulator to between 25 bar (362.5942 psi) and 40 bar (580.1508 psi). This will make sure that the piston in the accumulator is at the bottom. NOTE : The flow of hydraulic fluid from the bleed valve can stop and ____ start again as the accumulator is filled. (8) Close the charge valve. (9) Use a thermometer to measure the ambient temperature. (10) On the filling system, set the nitrogen pressure to the correct value for the ambient temperature (as shown in Table 1). Table 1
EFF : ALL 12-14-32 SROS
Page 355 Apr 01/04
------------------------------------------------------------------------------| Temperature | Charging Pressure | |---------------------------|-------------------------------------------------| | deg.C | deg.F | BAR | PSI | |-----------------------------------------------------------------------------| | -40 | -40 | 3.60 | 52.2 | | -30 | -22 | 3.75 | 54.4 | | -20 | - 4 | 3.90 | 56.6 | | -10 | 14 | 4.05 | 58.7 | | 0 | 32 | 4.20 | 60.9 | | 10 | 50 | 4.35 | 63.1 | | 20 | 68 | 4.50 | 65.1 | | 30 | 86 | 4.65 | 67.4 | | 40 | 104 | 4.75 | 68.8 | | 50 | 112 | 5.00 | 72.5 | | 60 | 140 | 5.20 | 75.4 | ------------------------------------------------------------------------------(11) Slowly open the charge valve and let the NWS accumulator pressure decrease to the correct value. (12) Close the charge valve. (13) Let the accumulator temperature become stable (approximately 10 minutes for a full pressurization from zero pressure). (14) Close the hydraulic bleed valve. (15) Remove the Nitrogen Filling System. (16) Use an applicable pressure gage to do a check of the gas pressure. If necessary pressurize the accumulator again. (17) Install the cap (3). (18) Install the dust cap (2) and the cover (1). R R
(19) TORQUE the cover (1) to between 0.15 m.daN (13.27 lbf.in) and 0.17 m.daN (15.04 lbf.in). (20) Safety the cover (1) with lockwire, corrosion resistant steel 0.8 mm (0.032 in.).
EFF : ALL 12-14-32 SROS
Page 356 Jan 01/06
5. Close-up ________ Subtask 12-14-32-611-050 A. Aircraft Maintenance Configuration (1) Make sure that the contents of the Green hydraulic reservoir is correct (Ref. TASK 12-12-29-611-802). R R R R
Subtask 12-14-32-865-072 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GG, 2GG Subtask 12-14-32-942-058
R
C. Removal of Equipment (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 12-14-32 SROS
Page 357 Jul 01/03
OXYGEN - SERVICING __________________ TASK 12-14-35-600-801 Servicing of the Oxygen Replenishing WARNING : KEEP ALL HYDROCARBONS (FUELS, LUBRICANTS, ETC.) AWAY FROM ALL SOURCES _______ OF OXYGEN. OXYGEN BECOMES EXPLOSIVE WHEN IT TOUCHES HYDROCARBONS. R
R R
WARNING : OBEY THESE SPECIAL PRECAUTIONS WHEN YOU DO THIS PROCEDURE: _______ - PREVENT ALL MAINTENANCE PROCEDURES NEARER THAN 5M (16.5 FT) TO THE WORKING AREA OF THE AIRCRAFT: - ALSO STOP ALL REFUELING, ALL REPAIRS ON FUEL AND HYDRAULIC SYSTEMS, ALL PROCEDURES THAT USE FLAMMABLE MATERIALS SUCH AS CLEANING AND DE-ICING MATERIALS. MAKE SURE THAT NO PERSONS CONNECT/DISCONNECT THE GROUND POWER CONNECTOR. - MAKE SURE THAT NO PERSONS SMOKE, AND THAT THERE ARE NO FLAMES, IN A RADIUS OF 15M (49.5 FT) OF THE REPLENISHING EQUIPMENT. USE ONLY TOOLS/GROUND SERVICING EQUIPMENT MADE SPECIALLY FOR OXYGEN SYSTEMS. - MAKE SURE THAT YOUR HANDS AND ALL THE TOOLS/GROUND SERVICING EQUIPMENT ARE CLEAN. THIS WILL PREVENT CONTAMINATION OF THE OXYGEN SYSTEM AND OF THE GROUND SERVICING EQUIPMENT. - CAREFULLY OBEY THE REPLENISHING INSTRUCTIONS ON THE AIRCRAFT PLACARDS. IF YOU DO NOT OBEY THESE INSTRUCTIONS, YOU CAN CAUSE A FIRE OR AN EXPLOSION. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No
specific specific specific specific
bonding cable circuit breaker(s) safety clip(s) warning notice access platform 2.5 m (8 ft. 2 in.)
EFF : ALL 12-14-35 SROS
Page 301 Oct 01/04
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-34-24-860-801 24-41-00-861-801 24-41-00-862-801 31-60-00-860-801 31-60-00-860-802 12-14-35-991-001 12-14-35-991-002
Aircraft Grounding for the Refuel/Defuel and Oxygen Servicing Operations Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A EIS Start Procedure EIS Stop Procedure Fig. 301 Fig. 302
3. __________ Job Set-up Subtask 12-14-35-861-050 R
A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). Subtask 12-14-35-010-050 B. Get Access (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the cover of the oxygen box. Subtask 12-14-35-941-050 C. Safety Precautions (Ref. Fig. 301/TASK 12-14-35-991-001) (1) Make sure that the overboard discharge indicator shows green. (2) Put a warning notice in position in the work area to tell persons that the oxygen filling operation is dangerous. (3) Make sure that the date of the test given on the cylinder is in the permitted time limit.
EFF : ALL 12-14-35 SROS
Page 302 Oct 01/04
Location of the Oxygen Filling Port Figure 301/TASK 12-14-35-991-001 EFF : ALL 12-14-35 R SROS
Page 303 Apr 01/00
(4) Make sure that the oxygen line end-fittings and the electrical connectors are in the correct condition. Subtask 12-14-35-865-050 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------742VU CREW OXY CTL 4HT L73 Subtask 12-14-35-860-050 E. Aircraft Maintenance Configuration (Ref. Fig. 302/TASK 12-14-35-991-002) (1) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00-860-801). (2) Do this step to electrically ground the oxygen ground-filling equipment: (a) Connect a bonding cable between the aircraft and the oxygen ground-filling equipment (Ref. TASK 12-34-24-860-801). 4. Procedure _________ Subtask 12-14-35-614-050 A. Servicing of the Oxygen Replenishing (Ref. Fig. 301/TASK 12-14-35-991-001) (1) Remove the blanking plug from the filling port 5769HT. R R
(2) Connect the filling assembly to the filling port 5769HT. (3) Measure the Outside Air Temperature (OAT) and the cockpit temperature with a thermometer. (4) Find the filling pressure. To do this, refer to the temperatures and the aircraft placards. (Ref. Fig. 302/TASK 12-14-35-991-002) (5) Slowly pressurize the system. Make sure that the filling pressure is correct on the pressure gage on the cylinder.
EFF : ALL 12-14-35 SROS
Page 304 Apr 01/02
Filling Pressure Figure 302/TASK 12-14-35-991-002 EFF : ALL 12-14-35 SROS
Page 305 Apr 01/98
Subtask 12-14-35-210-050 B. Test (1) Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 4HT (2) Make sure that the pressure value shown on the pressure gage is the same as the pressure indication on the DOOR page of the SD. 5. Close-up ________ Subtask 12-14-35-860-051 A. Put the Aircraft back to its Initial Configuration (1) Disconnect the filling assembly. (2) Put the blanking plug on the filling port. (3) Disconnect the bonding cable (Ref. TASK 12-34-24-860-801). (4) Make sure that the work area is clean and clear of tools and other items. (5) Do the EIS stop procedure (Ref. TASK 31-60-00-860-802). Subtask 12-14-35-410-050 B. Close Access R
(1) Close the cover of the oxygen box.
R
(2) Remove the warning notice(s).
R
(3) Close the access door 811.
R
(4) Remove the access platform(s). Subtask 12-14-35-862-050 C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
EFF : ALL 12-14-35 SROS
Page 306 Apr 01/02
WATER - DESCRIPTION AND OPERATION _________________________________ 1. _______ General This topic gives instructions for the servicing of the potable water system.
EFF : ALL 12-15-00 SROS
Page 1 Apr 01/98
POTABLE WATER - SERVICING _________________________ TASK 12-15-38-613-801 Fill the Potable Water System (Aircraft Electrical Power Available) WARNING : DO NOT DO WORK ON THE TOILET WASTE SYSTEM AND THE POTABLE WATER _______ SYSTEM AT THE SAME TIME. THIS WILL PREVENT CONTAMINATION OF THE POTABLE WATER SYSTEM. SUCH CONTAMINATION CAN BE DANGEROUS TO HEALTH. WARNING : BEFORE YOU DO WORK ON THE POTABLE WATER SYSTEM, CLEAN YOUR HANDS WITH _______ SOAP AND WATER. THIS WILL PREVENT INFECTION. (CONTAMINATION FROM TOILET WASTE IS DANGEROUS TO HEALTH). WARNING : MAKE SURE THAT THE EQUIPMENT YOU USE FOR THIS PROCEDURE IS CLEAN AND _______ APPROVED FOR THE POTABLE WATER SYSTEM. IF NOT IT CAN CAUSE CONTAMINATION OF THE POTABLE WATER SYSTEM. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
1 ACCESS PLATFORM 1M (3 FT) 1 CART - SERVICING, WATER, POTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-31-38-660-801 12-33-21-618-801 24-41-00-861-801 24-41-00-862-801 12-15-38-991-001-A
Cold Weather Maintenance Practices for Water/Waste Pre-conditioning through the Low-Pressure Ground Connection Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Fig. 301
EFF : ALL 12-15-38 R SROS
Page 301 Jul 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-15-38-991-003 12-15-38-991-002
Fig. 302 Fig. 303
3. __________ Job Set-up Subtask 12-15-38-861-051 A. Make sure that the Aircraft Electrical Circuits are energized (Ref. TASK 24-41-00-861-801). Subtask 12-15-38-865-053 B. Get access to the applicable 5000VE series panel(s). Then make sure that this(these) circuit breaker(s) is (are) closed.
R
------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------5005VE WATER SYSTEM QUANT IND 1MA E06 5005VE WATER SYSTEM DRAIN 1MP E05 Subtask 12-15-38-618-050 C. Preparation to Fill the Potable Water System (1) Obey the cold weather maintenance procedure (Ref. TASK 12-31-38-660801). (2) If the temperature in the aircraft is below 4 DEG.C (39.20 DEG.F) do the pre-conditioning procedure (Ref. TASK 12-33-21-618-801). Subtask 12-15-38-010-054 D. Get Access (1) Put the ACCESS PLATFORM 1M (3 FT) in position below the Potable-Water Service Panel (PWSP) at Zone 164. (2) Put the ACCESS PLATFORM 1M (3 FT) in position below the aft potable-water drain-panel at Zone 154.
EFF : ALL 12-15-38 SROS
Page 302 Jul 01/06
4. Procedure _________ Subtask 12-15-38-613-055 A. Fill the Potable Water System WARNING : MAKE SURE THAT THE EQUIPMENT YOU USE FOR THIS PROCEDURE IS _______ CLEAN AND APPROVED FOR THE POTABLE WATER SYSTEM. IF NOT IT CAN CAUSE CONTAMINATION OF THE POTABLE WATER SYSTEM. (1) Make sure that the PWSP access door 164AR is closed. (Ref. Fig. 301/TASK 12-15-38-991-001-A) NOTE : You can set the water quantity only at the FAP 120RH when the ____ PWSP access door 164AR is closed. (2) On the FAP 120RH set the necessary quantity of water. (Ref. Fig. 302/TASK 12-15-38-991-003) (a) Push the WATER hardkey. (b) Make sure that the amber NO WATER PRESELECT AVAIL message is not shown. (c) Push the necessary + and/or - softkeys to set the necessary quantity of water. NOTE : You can set 25%, 50%, 75% and 100%. The keys are only ____ activated, if the PWSP access door 164AR is closed. (3) Connect the potable-water service-vehicle. (Ref. Fig. 301/TASK 12-15-38-991-001-A) (a) Open the PWSP access door 164AR. NOTE : You must not do the filling procedure if the ATTENTION ____ STOP FILLING 38MA light is ON. (b) On the PWSP remove the cap 5252MB from the fill/drain nipple 26DV. (c) Connect the CART - SERVICING, WATER, POTABLE hose to the fill/drain nipple 26DV. (d) On the PWSP turn the control handle 5254MB from the NORMAL to the PULL TO FILL position. Then pull it out to the mechanical stop.
EFF : ALL 12-15-38 R SROS
Page 303 Jul 01/05
R
Potable-Water Service Panel Figure 301/TASK 12-15-38-991-001-A
EFF : ALL 12-15-38 SROS
Page 304 Jul 01/03
FAP Display Figure 302/TASK 12-15-38-991-003 EFF : ALL 12-15-38 R SROS
Page 305 Jul 01/98
(e) Make sure that the control light 3MP comes ON and the control light 38MA is OFF. (4) Fill the Potable Water Tanks CAUTION : DO NOT LET THE WATER PRESSURE BE MORE THAN THE SPECIFIED _______ VALUE. IF THE WATER PRESSURE IS TOO HIGH IT WILL CAUSE DAMAGE TO THE POTABLE WATER SYSTEM. NOTE : Stop immediately the fill procedure of the potable water tanks ____ if the control light ATTENTION STOP FILLING 38MA comes ON at the PWSP. (a) Operate the CART - SERVICING, WATER, POTABLE at a pressure of max. 125 psi (8.6184 bar) and fill the potable water tanks. NOTE : When the set value is reached, the control lights 5MA for ____ the FWD tank system and 15MA for the AFT tank system come ON. When the control light 5MA comes ON, the valve 22MA closes and the control light 3MP goes OFF. When the control light 15MA comes ON at first, the valve 37MA closes and the control light 38MA is not activated. In this case the valve 37MA opens again after the FWD tanks system has reached the set level. After the FWD and AFT tank systems have reached the set value, the valve 9MA closes and the control handle 5254MB turns automatically back to the NORMAL position. NOTE : To stop the fill procedure before the set quantity is ____ reached, you must turn the control handle 5254MB to the NORMAL position. (b) Stop the water flow at the CART - SERVICING, WATER, POTABLE. (5) Make sure that the actual quantity indication on the FAP and at PWSP is the same as the set quantity indication. (Ref. Fig. 301/TASK 12-15-38-991-001-A, 302/TASK 12-15-38-991-003) (6) Disconnect the potable-water service-vehicle. (Ref. Fig. 301/TASK 12-15-38-991-001-A) (a) Disconnect the CART - SERVICING, WATER, POTABLE hose from the fill/drain nipple 26DV at the PWSP. (b) Clean and dry the PWSP and the adjacent area.
EFF : ALL 12-15-38 R SROS
Page 306 Jul 01/05
(c) Visually examine the connections for leaks. NOTE : Leaks are not permitted. ____ (d) Install the cap 5252MB on the fill/drain nipple 26DV. (7) Clean and dry the aft potable-water drain-panel. (Ref. Fig. 303/TASK 12-15-38-991-002) (a) Open the aft potable-water drain-panel access door 154AR. (b) Clean and dry the aft potable-water drain-panel and the adjacent area. (c) Visually examine the connections for leaks. NOTE : Leaks are not permitted. ____ (d) Close the aft potable-water drain-panel access door 154AR. **ON A/C 001-049, Subtask 12-15-38-870-052 B. Bleed the Components (1) Galley Water-Heater NOTE : This procedure is the same for all the faucets of the galley ____ water-heaters. (a) Open the faucet of the galley water-heater. NOTE : This is only possible when the potable-water system is ____ pressurized and the shutoff valve of the galley is open. (b) Put an applicable container below the faucet to collect the water. NOTE : If you use the washbasin make sure that hoses are ____ connected to the drain masts (c) Close the faucet of the galley water-heater.
EFF : ALL 12-15-38 R SROS
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Aft Potable-Water Drain-Panel Figure 303/TASK 12-15-38-991-002 EFF : ALL 12-15-38 R SROS
Page 308 Jul 01/03
**ON A/C ALL 5. Close-up ________ Subtask 12-15-38-410-052 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access door 164AR and make sure that the access door 154AR is closed. (3) Make sure that the latches are correctly locked and that the doors make a continuous surface with the skin of the aircraft. (4) Remove the access platform(s). (5) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-15-38-862-051 B. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
EFF : ALL 12-15-38 R SROS
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TASK 12-15-38-613-802 Fill the Potable Water System (Aircraft Electrical Power not Available) 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No
specific specific specific specific
1 1 1 1
ACCESS PLATFORM 1M (3 FT) CART - SERVICING, WATER, POTABLE CONTAINER 10 L(2 1/2 USGAL) HOSE - DRAIN
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-31-38-660-801 12-33-21-618-801 12-15-38-991-001-A 12-15-38-991-002
Cold Weather Maintenance Practices for Water/Waste Pre-conditioning through the Low-Pressure Ground Connection Fig. 301 Fig. 303
3. __________ Job Set-up Subtask 12-15-38-865-054 A. Make sure that the electrical-power supply system is de-energized: Get access to the applicable 5000VE series panel(s). Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------5005VE WATER SYSTEM QUANT IND 1MA 17 C 5005VE WATER SYSTEM DRAIN 1MP 16 C
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Subtask 12-15-38-618-051 B. Preparation to Fill the Potable Water System (1) Obey the cold weather maintenance procedure (Ref. TASK 12-31-38-660801). (2) If the temperature in the aircraft is below 4 DEG.C (39.20 DEG.F) do the pre-conditioning procedure (Ref. TASK 12-33-21-618-801). Subtask 12-15-38-010-055 C. Get Access (1) Put the ACCESS PLATFORM 1M (3 FT) in position below the Potable-Water Service Panel (PWSP) at Zone 164. (2) Put the ACCESS PLATFORM 1M (3 FT) in position below the Aft Potable-Water Drain Panel (APWDP) at Zone 154. 4. Procedure _________ Subtask 12-15-38-613-056 A. Fill the Potable Water Tanks WARNING : MAKE SURE THAT THE EQUIPMENT YOU USE FOR THIS PROCEDURE IS _______ CLEAN AND APPROVED FOR THE POTABLE WATER SYSTEM. IF NOT IT CAN CAUSE CONTAMINATION OF THE POTABLE WATER SYSTEM. (1) On the APWDP: (Ref. Fig. 303/TASK 12-15-38-991-002) (a) Open the access door 154AR. (b) Connect a HOSE - DRAIN to the drain (overflow) nipple 5255MB connection on the APWDP. (c) Put a CONTAINER 10 L(2 1/2 USGAL) under the drain hose. (2) On the PWSP: (Ref. Fig. 301/TASK 12-15-38-991-001-A) (a) Open the access door 164AR. (b) Remove the cap assy 5252MB from the fill/drain nipple 26DV .
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(c) Connect the CART - SERVICING, WATER, POTABLE hose to the fill/drain nipple 26DV. (d) Connect a hose to the overflow nipple 28DV. (3) On the APWDP turn the FILL/DRAIN VALVE control handle to the OPEN position. (4) On the PWSP turn the control handle 5254MB to the PULL TO FILL position. Then pull it out to the mechanical stop. (5) Fill the potable water tanks. CAUTION : DO NOT LET THE WATER PRESSURE BE MORE THAN THE SPECIFIED _______ VALUE. IF THE WATER PRESSURE IS TOO HIGH IT WILL CAUSE DAMAGE TO THE POTABLE WATER SYSTEM. (a) Operate the potable-water service-vehicle at a pressure of 125 psi (8.6184 bar) and fill the potable water tanks. NOTE : When the tanks are full, water will flow from the overflow ____ nipple 28DV at the PWSP and drain (overflow) nipple 5255MB at the APWDP. (6) When water flows from: - the APWDP, turn the FILL/DRAIN VALVE control handle to the SHUT position, - the PWSP, push in the control handle 5254MB and turn it to the NORMAL position. (7) Stop the water flow at the potable-water service-vehicle. (8) On the PWSP: (a) Disconnect the hose from the fill/drain nipple 26DV. (b) Disconnect the overflow nipple 28DV. (c) Turn the control handle 5254MB to the PULL TO DRAIN position. Then pull it out to the mechanical stop. NOTE : Water will flow from the fill/drain nipple 26DV on the ____ PWSP. (d) After approximately 15 seconds, push in the control handle 5254MB and then turn to the NORMAL position.
EFF : ALL 12-15-38 R SROS
Page 312 Jul 01/05
(e) Install the cap assy 5252MB on the fill/drain nipple 26DV. (f) Clean and dry the PWSP and the adjacent area. (g) Visually examine the connections for leaks. NOTE : Leaks are not permitted. ____ (h) Make sure that the work area is clean and clear of tools and other items. (i) Close the PWSP access door 164AR. (9) On the APWDP (a) Disconnect the drain hose. (b) Remove the container. (c) Clean and dry the APWDP and the adjacent area. (d) Visually examine the connections for leaks. NOTE : Leaks are not permitted. ____ (e) Make sure that the work area is clean and clear of tools and other items. (f) Close the APWDP access door 154AR. **ON A/C 001-049, Subtask 12-15-38-870-053 B. Bleed the Components (1) Galley Water-Heater NOTE : This procedure is the same for all the faucets of the galley ____ water heaters. (a) Open the faucet of the galley water-heater. NOTE : This is only possible when the potable-water system is ____ pressurized and the shutoff valve of the galley is open.
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(b) Put an applicable container below the faucet to collect the water. NOTE : If you use the washbasin make sure that hoses are ____ connected to the drain masts (c) Close the faucet of the galley water-heater. **ON A/C ALL 5. Close-up ________ Subtask 12-15-38-865-055 A. Make sure that the system is energized: Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1MA, 1MP Subtask 12-15-38-410-053 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access doors 164AR and 154AR. (3) Make sure that the latches are correctly locked and that the access doors make a continuous surface with the skin of the aircraft. (4) Remove the access platform(s). (5) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL 12-15-38 R SROS
Page 314 Jul 01/05
TOILET SANITARY FLUID - DESCRIPTION AND OPERATION _________________________________________________ 1. _______ General This topic gives instructions for the servicing of the waste water system.
EFF : ALL 12-16-00 SROS
Page 1 Apr 01/98
LAVATORY ARTICLE - SERVICING ____________________________ TASK 12-16-25-613-801 Servicing of the Liquid Soap Dispenser 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
No specific
weak liquid soap
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 R
Energize the Ground Service Network De-energize the Ground Service Network
**ON A/C 001-049, 201-208, 251-252, 255-299, 401-449, 451-499, 12-16-25-991-001
Fig. 301
**ON A/C 209-249, 301-399, 701-749, 12-16-25-991-001-A
Fig. 301A
EFF : ALL 12-16-25 SROS
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**ON A/C ALL 3. __________ Job Set-up Subtask 12-16-25-861-050 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). 4. Procedure _________ Subtask 12-16-25-613-050 R
A. Servicing of the Soap Dispenser.
R R R R R
CAUTION : DO NOT USE INDUSTRIAL HAND CLEANERS, NATURAL SOAPS AND CLEANING _______ AGENTS THAT CONTAIN ABRASIVES, SOLVENTS OR A LARGE PROPORTION OF DISINFECTANT. THESE MATERIALS CAN CAUSE THE PUMP MECHANISM TO WEAR MORE QUICKLY.
R R R R
NOTE : The dispenser is applicable for normal liquid hand-cleaning ____ agents, soap creams and dish-washing agents for household use. We recommend that you use weak, biodegradable, fully synthetic agents.
R R R R
(1) Fill the Soap Dispenser **ON A/C 001-049, 201-208, 251-252, 255-299, 401-449, 451-499, (Ref. Fig. 301/TASK 12-16-25-991-001) **ON A/C 209-249, 301-399, 701-749, (Ref. Fig. 301A/TASK 12-16-25-991-001-A)
R
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Liquid Soap Dispenser Figure 301/TASK 12-16-25-991-001 R EFF : 001-049, 201-208, 251-252, 255-299, 12-16-25 401-449, 451-499, SROS
Page 303 Jul 01/05
Liquid Soap Dispenser Figure 301A/TASK 12-16-25-991-001-A R EFF : 209-249, 301-399, 701-749, 12-16-25 SROS
Page 304 Oct 01/00
**ON A/C ALL R R R
(a) Turn the cover (2) counterclockwise to release it from the shank (3) (refer to Step 1).
R R R
(b) Carefully lift and remove the cover (2) together with the spout (1) and the tube (4) from the shank (3) (refer to Step 2).
R R R
(c) Fill the soap dispenser with weak liquid soap through the shank (3) (refer to Step 3).
R R R
(d) Carefully put the cover (2) together with the spout (1) and the tube (4) on the shank (3).
R R R
(e) Turn the cover (2) clockwise until it is locked in position on the shank (3).
R
(f) Make sure that the work area is clean and clear of tools and other items. 5. Close-up ________ Subtask 12-16-25-862-050 A. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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TOILET SANITARY FLUID - SERVICING _________________________________ TASK 12-16-38-613-801 Servicing of the Toilet System WARNING : ALWAYS USE RUBBER GLOVES WHEN YOU DO WORK: _______ - ON THE TOILET WASTE SYSTEM, OR - ON PARTS THAT HAVE CONTAMINATION FROM THE WASTE SYSTEM. WHEN YOU COMPLETE THE WORK PROCEDURE, CLEAN YOUR HANDS WITH SOAP AND WATER. THIS WILL PREVENT INFECTION (TOILET WASTE IS DANGEROUS FOR HEALTH). WARNING : DO NOT DO WORK ON THE TOILET WASTE SYSTEM AND THE POTABLE WATER _______ SYSTEM AT THE SAME TIME. THIS WILL PREVENT CONTAMINATION OF THE POTABLE WATER SYSTEM. SUCH CONTAMINATION CAN BE DANGEROUS TO HEALTH. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific No specific
1 ACCESS PLATFORM 2M (6 FT) 4 CART - SERVICING, TOILET
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 14-001A Material No. 19-003
DEODORANT AIRCRAFT TOILET NON FORMALDE- HYDE BASE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
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C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-31-38-660-801 12-33-21-618-801 24-41-00-861-801 24-41-00-862-801 38-31-00-680-801 R
Cold Weather Maintenance Practices for Water/Waste Pre-conditioning through the Low-Pressure Ground Connection Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Draining of the Waste Holding Tanks
**ON A/C 001-049, 201-249, 251-252, 255-299, 12-16-38-991-001
Fig. 301
**ON A/C ALL R
Post SB
38-3040 For A/C 001-049,201-249,251-252,255-299,
12-16-38-991-001-B
Fig. 301A
**ON A/C ALL 3. __________ Job Set-up Subtask 12-16-38-861-050 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). Subtask 12-16-38-680-050 B. If the outside air temperature is as shown in the table drain the waste holding tanks (Ref. TASK 38-31-00-680-801). CAUTION : MAKE SURE THAT THE WATER TEMPERATURE IS NOT HIGHER THAN 60 _______ DEG.C (140.00 DEG.F), IF IT IS HIGHER, IT CAN CAUSE DAMAGE TO THE COMPONENT. Table 1 - Waste-Holding Tank Drain Configuration
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R R
----------------------------------------------------------------------------I Configuration I I I I---------------------------------------------------I Exposure I Waste tank I I Air I Cabin I Outside air I time I drain I IconditioningItemperatureI temperature I I I I------------I-----------I--------------------------I------------I------------I I I I Between 0 and -15 DEG.C I I Not I I ON I Above I 32 and 5 DEG.F I Any I required I I I 10DEG.C I--------------------------I------------I------------I I I I Below -15 DEG.C I I I I I 50DEG.F I 5 DEG.F I 1 h 15 min I I I------------I-----------I--------------------------I------------I I I I I Between 0 and -7 DEG.C I I I I I I 38 and 19.4 DEG.F I 1 h 30 min I Required I I I I--------------------------I------------I I I OFF I I Between -7 and -15 DEG.C I I I I I I 19.4 and 5 DEG.F I 0 h 45 min I I I I I--------------------------I------------I I I I I Below -15 DEG.C I I I I I I 5 DEG.F I any I I I-----------------------------------------------------------------------------I I If you have drained the waste holding tanks you must put 18l (4.755 USgal) I I of warm disinfectant at 30 DEG.C (86 DEG.F) in each waste holding tank I I 30 minutes before you start the engines. I ----------------------------------------------------------------------------Subtask 12-16-38-010-050 C. Get Access (1) Put an ACCESS PLATFORM 2M (6 FT) in position below the waste service panel. (2) Put the CART - SERVICING, TOILET in position. (3) Open the waste service panel door 171AL. 4. Procedure _________ **ON A/C 001-049, 201-249, 251-252, 255-299, (Ref. Fig. 301/TASK 12-16-38-991-001)
EFF : ALL 12-16-38 SROS
Page 303 Jan 01/07
Waste Service Panel Figure 301/TASK 12-16-38-991-001 R EFF : 001-049, 201-249, 251-252, 255-299, 12-16-38 SROS
Page 304 Jul 01/05
**ON A/C ALL R
Post SB
38-3040 For A/C 001-049,201-249,251-252,255-299,
(Ref. Fig. 301A/TASK 12-16-38-991-001-B) **ON A/C ALL WARNING : YOU MUST ALWAYS WEAR RUBBER GLOVES WHEN YOU DO THIS PROCEDURE TO _______ PREVENT INFECTION. Subtask 12-16-38-680-051 A. Draining of the System (1) Open the cap of the waste drain-line valve and the tank flush connections. (2) Connect the hose adapter and the 4-inch diameter drain hose of the CART - SERVICING, TOILET to the waste-tank drain connection. (3) Push the PUSH TO OPEN lever on the waste drain-line valve to the OPEN position. (4) Put the drain-valve control-lever to the OPEN position and let the waste drain. (5) Touch the drain hose and make sure that the waste has drained completely. Subtask 12-16-38-170-050 B. Flushing of the Waste Holding Tanks CAUTION : MAKE SURE THAT THE WATER TEMPERATURE IS NOT HIGHER THAN 60 _______ DEG.C (140.00 DEG.F), IF IT IS HIGHER, IT CAN CAUSE DAMAGE TO THE COMPONENT. (1) Connect the flush/fill hose (1-inch diameter) of the CART SERVICING, TOILET to a flush connection. (2) Operate the CART - SERVICING, TOILET. (a) Make sure that the water pressure is stable at 2.4 bar (35 psi) and the water flow rate is stable at 38.0 l (10.0 USgal) per minute.
EFF : ALL 12-16-38 SROS
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Waste Service Panel Figure 301A/TASK 12-16-38-991-001-B
R
R EFF : ALL 12-16-38 SROS
Page 306 Oct 01/03
(b) Flush the waste holding tank with 100 l (26.5 USgal) of water. (3) Do this procedure for each waste holding tank. (4) Put the drain-valve control-lever to the CLOSED position. (5) Disconnect the drain hose and the hose adapter. Subtask 12-16-38-618-050 C. Preparation to fill the Waste Holding Tanks with disinfectant (1) Obey the cold weather maintenance procedure (Ref. TASK 12-31-38-660801). (2) If the temperature in the aircraft is below 4 DEG.C (39.20 DEG.F) do the pre-conditioning procedure (Ref. TASK 12-33-21-618-801). Subtask 12-16-38-613-051 D. Disinfection of the Tanks R R R
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL _______ MATERIAL. THIS MATERIAL IS DANGEROUS. CAUTION : MAKE SURE THAT THE WATER TEMPERATURE IS NOT HIGHER THAN 60 _______ DEG.C (140.00 DEG.F), IF IT IS HIGHER, IT CAN CAUSE DAMAGE TO THE COMPONENT.
R (1) Use the CART - SERVICING, TOILET to fill each waste holding tank with 18 l (4.8 USgal) of disinfectant solution. NOTE : The disinfection solution is a 0.25% solution of DISINFECTANTS ____ (Material No. 14-001A) You must obey the instructions of the manufacturer fully for the correct solution, when other disinfection materials are used. NOTE : Some disinfectant will drain from the flush connections when ____ you disconnect the fill hose.
EFF : ALL 12-16-38 SROS
Page 307 Apr 01/05
(2) Make sure that there are no leaks from the toilet drain connections or the fill/rinse connections. NOTE : Leaks are not permitted. ____ (3) Close the cap of the waste drain-line valve. (4) Turn off the CART - SERVICING, TOILET and disconnect the flush/fill hose. (5) Close the caps of the tank flush connections. (6) Clean and dry the service panel area with a clean cloth MISCELLANEOUS (Material No. 19-003). 5. Close-up ________ Subtask 12-16-38-410-051 A. Close the Access door WARNING : AFTER YOU DO WORK ON THE TOILET WASTE SYSTEM, DO NOT DO _______ SERVICING OF THE POTABLE WATER SYSTEM. THIS WILL PREVENT CONTAMINATION OF THE POTABLE WATER SYSTEM. SUCH CONTAMINATION CAN BE DANGEROUS TO HEALTH. (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access door 171AL. NOTE : Make sure that the latches are correctly locked and that the ____ door makes a continuous surface with the skin of the aircraft. Subtask 12-16-38-862-050 B. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862801). Subtask 12-16-38-942-050 C. Removal of the Ground Support Equipment (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 12-16-38 R SROS
Page 308 Apr 01/05
RAIN REPELLENT - DESCRIPTION AND OPERATION __________________________________________ 1. General _______ This section gives the instructions related to fill the rain repellent can. It includes the topic below: 12-17-30/ P. Block 301 ICE AND RAIN PROTECTION
EFF : ALL 12-17-00 SROS
Page 1 Apr 01/98
ICE AND RAIN PROTECTION - SERVICING ___________________________________ TASK 12-17-30-200-801 Do a Check of Rain Repellent Fluid Can Assy For Correct Fluid Level and Pressure NOTE : If there is leakage of FORALKYL 2211, you can smell a pine odor. ____ 1. __________________ Reason for the Job R R
Self Explanatory 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------30-45-00-600-801 12-17-30-991-001-A
Servicing of the Rain-Repellent Fluid Can (5101DG) Fig. 301
3. __________ Job Set-up **ON A/C 002-049, 203-249, 301-399, 403-449, 451-499, 701-749, Subtask 12-17-30-869-050 A. Not applicable.
EFF : ALL 12-17-30 SROS
Page 301 Jul 01/06
**ON A/C ALL 4. Procedure _________ (Ref. Fig. 301/TASK 12-17-30-991-001-A) R
**ON A/C 001-001, 201-202, 251-252, 255-299, 401-402, Subtask 12-17-30-210-050 A. Inspection/Check of the Pressure Gage and Fluid Level (1) Pressure gage (a) Make sure that the pointer points to the green area (green band). (b) If the pointer points to the yellow area, replace the can (Ref. TASK 30-45-00-600-801). (2) Fluid level indication (a) Make sure that the fluid level indicator does not show the REFILL indication. (b) If you see the REFILL float, replace the can (Ref. TASK 30-45-00600-801). **ON A/C 002-049, 203-249, 301-399, 403-449, 451-499, 701-749, Subtask 12-17-30-210-050-A A. Inspection/Check of the Pressure Gage and Fluid Level (1) Pressure gage (a) Make sure that the pointer points to the green area (green band). (b) If the pointer points to the yellow area, replace the can (Ref. TASK 30-45-00-600-801). (2) Fluid level indication (a) Make sure that there is sufficient rain repellent fluid in the gage assy.
EFF : ALL 12-17-30 SROS
Page 302 Jul 01/05
Rain Repellent Fluid Gage Assy Figure 301/TASK 12-17-30-991-001-A EFF : ALL 12-17-30 R SROS
Page 303 Jan 01/03
(b) If you see the surface of the fluid, replace the can (Ref. TASK 30-45-00-600-801). R
**ON A/C ALL 5. Close-up ________
R
**ON A/C 002-049, 203-249, 301-399, 403-449, 451-499, 701-749, Subtask 12-17-30-869-051 A. Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 12-17-30 SROS
Page 304 Jan 01/03
SCHEDULED SERVICING - DESCRIPTION AND OPERATION _______________________________________________ 1. General _______ This section gives the instructions related to the servicing operations, for which a frequency is specified. It includes 12-21-00/P. 12-22-00/P. 12-24-00/P. 12-28-00/P.
the topics below: Block 301 CLEANING Block 301 LUBRICATION Block 301 DRAINAGE Block 301 USE OF MANUAL (MAGNETIC) FUEL QUANTITY INDICATORS
EFF : ALL 12-20-00 SROS
Page 1 Apr 01/98
CLEANING - DESCRIPTION AND OPERATION ____________________________________ 1. General _______ This section gives the instructions related to the aircraft external and internal cleaning. It includes the topics below: 12-21-11/P. Block 301 EXTERNAL CLEANING 12-21-12/P. Block 301 INTERNAL CLEANING
EFF : ALL 12-21-00 SROS
Page 1 Apr 01/98
EXTERNAL CLEANING - SERVICING _____________________________ TASK 12-21-11-615-802 External Cleaning WARNING : BE VERY CAREFUL IF YOU GO ON WET AIRCRAFT SURFACES. IF YOU SLIP, _______ THERE IS A RISK THAT YOU WILL FALL. WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A _______ FALL CAN KILL OR INJURE YOU. CAUTION : DO NOT USE HIGH-PRESSURE JETS OR VAPOR TO DO THE CLEANING PROCEDURE. _______ THIS TYPE OF EQUIPMENT CAN PUT WATER AND MOISTURE IN PARTS, AND CAN CAUSE DAMAGE TO EQUIPMENT, SPECIALLY TO: - ELECTRICAL EQUIPMENT SUCH AS HARNESSES, PROXIMITY SENSORS AND CONNECTORS (WITH SHORT CIRCUITS OR INCORRECT INDICATIONS AS A RESULT) - EQUIPMENT SUCH AS GEAR BOX SEALS, STEADY BEARINGS, ROTARY ACTUATORS AND UNIVERSAL JOINTS. R R
CAUTION : DURING THE ANTI-ICING/DE-ICING AND WASHING PROCEDURES, MAKE SURE THAT _______ THE HOT WATER OR HOT WATER/FLUID MIXTURES DO NOT CAUSE THE TEMPERATURE OF THE AIRCRAFT SKIN TO INCREASE TO MORE THAN +70⁰C. CAUTION : DO NOT USE A COMPRESSED AIR SUPPLY OF MORE THAN 10 PSI (0.70 BAR) _______ PRESSURE: - IF YOU USE A SPRAY GUN OR - WHEN YOU USE COMPRESSED AIR TO DRY THE CLEANED PARTS. AN IMPACT PRESSURE OF MORE THAN 10 PSI (0.70 BAR) WILL CAUSE DAMAGE TO THE PARTS.
R R R R R R R R R R R R R
WARNING : THERE IS A POSSIBLE HEALTH RISK TO PERSONNEL WHO DO MAINTENANCE TASKS _______ AFTER A BIRD STRIKE. THE SAFETY MEASURES THAT FOLLOW ARE RECOMMENDED: - USE DISPOSABLE GLOVES. - USE A DISPOSABLE COVERALL IF THERE IS A RISK OF BODY CONTACT WITH THE BIRD REMAINS. - DO NOT USE PRESSURIZED AIR OR WATER TO CLEAN THE PARTS WHICH WERE IN CONTACT WITH THE BIRD. - REMOVE THE BIRD REMAINS AND PUT THEM IN A PLASTIC BAG. - DO NOT TOUCH YOUR FACE, EYES, NOSE, ETC. WITH YOUR GLOVES. - REMOVE THE GLOVES AND THE DISPOSABLE COVERALL AND PUT THEM IN THE SAME PLASTIC BAG AS THE REMAINS. SEAL THE BAG. - DISCARD THE BAG AS YOU DO FOR USUAL GARBAGE. - CAREFULLY WASH YOUR HANDS WITH SOAP AND WATER.
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1. __________________ Reason for the Job R
NOTE : This task can contribute to fuel savings. ____
R
This task gives the procedure for: - external cleaning of the A/C, - cleaning of the windows, - cleaning of the landing gears and landing gear bays. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No No No No No
specific specific specific specific specific specific specific specific specific specific specific specific
1 1 6 1 2 1 1 1 1 1 1 1
BOOT - RUBBER BRUSH - BRISTLED, SOFT CHOCK - WHEEL CLEANING EQUIPMENT HEIGHT 17M (55FT) - MOBILE FILM - POLYETHYLENE GLOVES - RUBBER GOGGLES - PROTECTIVE OVERALL WITH HOOD - WATERPROOF SCRAPER - PLASTIC SPRAYING EQUIPMENT - LOW PRESSURE TAPE - ADHESIVE SPONGE
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 05-005
USA MIL-C-16173 GRADE II CORROSION PREVENTIVE (Ref. 20-31-00)
Material No. 05-027 Material No. 10-001 Material No. 11-001
RUST INHIBITOR(FOR CORROSION USE 15-004) (Ref. 20-31-00) USA AMS 1424 DE-ICING FLUID AEA/ISO TYPE I ISO 11075 (Ref. 20-31-00) USA MIL-D-16791 TYPE I DETERGENT (Ref. 20-31-00)
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 11-002 Material No. 11-026 Material No. 19-003
USA MIL-PRF-680 DRY CLEANING SOLVENT (VARSOL/WHITE SPIRIT) (Ref. 20-31-00) GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------09-10-00-584-802 09-10-00-584-808 10-11-00-555-814 12-22-32-600-817 12-22-32-600-819 12-31-12-660-801 12-34-24-860-802 24-41-00-861-801 24-41-00-861-801 24-41-00-862-801 32-11-00-100-801 32-12-00-010-801 32-12-00-410-801
Towing with the Nose Landing Gear from the Front Towing with Towbarless Tractor Aircraft Protection Equipment Lubrication of Main Landing Gear and Doors Lubrication of Nose Gear and Doors De-icing of the Aircraft Parked in an Open Area (Engines Stopped) Aircraft Grounding for the Maintenance Operations Energize the Aircraft Electrical Circuits from the External Power A Energize the Aircraft Electrical Circuits from the APU (APU Started with APU BAT) De-energize the Aircraft Electrical Circuits from the External Power A Cleaning of the Main Landing Gear Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance
R 32-21-00-100-801 32-22-00-010-801 32-22-00-410-801 56-10-00-100-801 56-10-00-100-802 56-21-15-100-801
Cleaning of the Nose Landing Gear Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance Cleaning of the Windshield (3DG1,3DG2). Cleaning of the Sliding (8DG1,8DG2) and the Fixed Windows (7DG1,7DG2). Cleaning of the Outer Surfaces of the Window Panes
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3. __________ Job Set-up Subtask 12-21-11-941-052 A. General (1) Quality of water for aircraft external cleaning (a) We recommend that you use potable water that has these qualities: - pH between 5 to 8.5 - Chloride level less than 100ppm. NOTE : Water that contains a high level of chloride and/or is ____ acidic-alkaline can cause corrosion. Treated water from city drainage can cause a risk of bacteriological contamination. Refer to the local regulations. (2) The persons that do the cleaning must put on BOOT - RUBBER, GLOVES RUBBER, GOGGLES - PROTECTIVE and OVERALL WITH HOOD - WATERPROOF. Subtask 12-21-11-860-052 B. Aircraft Maintenance Configuration (1) Tow the aircraft to the cleaning area (Ref. TASK 09-10-00-584-802) or (Ref. TASK 09-10-00-584-808). (2) Electrically ground the aircraft (Ref. TASK 12-34-24-860-802). (3) Put the CHOCK - WHEEL in position: (a) For the nose landing gear: - in front of and behind the wheels. (b) For the main landing gear: - in front of the FWD wheels and behind the AFT wheels. (4) Make sure that the slats, flaps, spoilers, ailerons and thrust reversers are retracted. (5) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801).
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(6) On the panel 225VU, push the DITCHING pushbutton switch to close: - the outflow valves 313HL and 315HL, - the underfloor extract valve 12HQ, - the overboard extract valve 13HQ. (7) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). (8) Electrically ground the aircraft (Ref. TASK 12-34-24-860-802). (9) Make sure that all landing gear doors, passenger/crew doors, cargo compartment doors, emergency exits, service panels and sliding windows are closed and that the engines are cold. (10) Install aircraft protection equipment (Ref. TASK 10-11-00-555-814). R R R R R R R R R R
WARNING : USE ONLY THE SPECIFIED TOOLS FOR THE PROTECTION OF THE _______ AIRCRAFT. DO NOT APPLY ADHESIVE TAPE ON THE PROBES, DUCTS, SENSORS (STATIC, PITOT, TAT, AOA). THE SPECIFIED TOOLS : - GIVE THE CORRECT PROTECTION TO THE AIRCRAFT EQUIPMENT, - ARE EASY TO SEE FROM THE GROUND. MAKE AN ENTRY IN THE AIRCRAFT LOG BOOK OR ATTACH A TAG ON THE CAPTAIN SIDE STICK TO TELL THE CREW THAT PROTECTION COVERS/DEVICES ARE INSTALLED. (11) Install a FILM - POLYETHYLENE or equivalent, on each landing gear wheel/brake. (12) Put TAPE - ADHESIVE on all remaining joints and openings where the cleaning products could fall and cause damage. Record the locations where you put the TAPE - ADHESIVE. Subtask 12-21-11-941-053 C. Job Set-up WARNING : CLEANING AGENT IS A HAZARDOUS MATERIAL WHICH CAN CAUSE INJURY _______ OR ILLNESS IF IT IS NOT CORRECTLY USED. REFER TO MANUFACTURERS SPECIFIC SAFETY AND HEALTH RECOMMENDATIONS BEFORE YOU USE THIS PRODUCT. CAREFULLY READ THE APPLICABLE MATERIAL SAFETY DATA SHEET AND OBEY ALL SAFETY AND HEALTH PRECAUTIONS. (1) Put CLEANING EQUIPMENT HEIGHT 17M (55FT) - MOBILE in position.
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(2) Prepare the cleaning equipment and the cleaning solution with CLEANING AGENTS (Material No. 11-001). Obey the manufacturer instructions. In very dirty areas, increase the concentration but obey the manufacturer instructions for use. If the temperature is less than or equal to 0 deg.C (32.00 deg.F) , use hot water between 38 deg.C (100.40 deg.F) and 43 deg.C (109.40 deg.F) with ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-001). Obey the manufacturer instructions. 4. Procedure _________ Subtask 12-21-11-615-053 A. Aircraft External Cleaning CAUTION : DO NOT USE A COMPRESSED AIR SUPPLY OF MORE THAN 10 PSI (0.70 _______ BAR) PRESSURE: - IF YOU USE A SPRAY GUN OR - WHEN YOU USE COMPRESSED AIR TO DRY THE CLEANED PARTS. AN IMPACT PRESSURE OF MORE THAN 10 PSI (0.70 BAR) WILL CAUSE DAMAGE TO THE PARTS. CAUTION : DO NOT USE STEAM AT MORE THAN THE SPECIFIED PRESSURE. BE _______ CAREFUL TO HOLD THE SPRAY GUN AT THE SPECIFIED DISTANCE AND ANGLE FROM THE SURFACE. IF YOU DO NOT OBEY THESE PRECAUTIONS, YOU CAN CAUSE DAMAGE TO THE SURFACE. (1) If the temperature is less than or equal to 0 deg.C (32.00 deg.F) do the de-icing of the aircraft (Ref. TASK 12-31-12-660-801). (2) Adjust the SPRAYING EQUIPMENT - LOW PRESSURE: - Adjust water, steam, cleaning solution and the temperature controls to the required settings. - Set the steam pressure to less than 10 psi (0.6894 bar), the steam pressure must not cause damage to materials. - Set the temperature so that the cleaning solution is not more than 50 deg.C (122.00 deg.F). (3) Hold the spray gun approximately 1 m (3.28 ft.) from the surface and inclined at approximately 45 degrees to the surface, never at 90 degrees. Move the spray head over the surface and be careful not to stay at one spot for more than 5 seconds. NOTE : If the weather temperature is hot, clean small areas so that ____ the cleaning solution does not become dry on the external skin.
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(4) Apply the cleaning solution from the bottom to the top of the aircraft (this prevents scratches and runs) in the sequence below: - lower forward fuselage from the leading edge of the wing to the nose of the aircraft. - lower aft fuselage from the wings to the leading edge of the horizontal stabilizer. - upper wing surface between the fuselage and the outboard engine pylon. - upper fuselage from the nose to the horizontal stabilizer. - lower center fuselage, engine nacelles and wing bottom skin. - tail cone, rudder, bottom and top skins of the horizontal stabilizer. NOTE : In the THS apron ____ the front to the If you point the anti-icing fluid compartment.
area, it is important to point the spray from rear. spray in the other direction (rear to front), can go into the rear fuselage non-pressurized
- wing top skin between the outboard engine pylon and the wing tips. (a) If there are signs of asphalt, remove them with a SPONGE lightly soaked with CLEANING AGENTS (Material No. 11-026) or CLEANING AGENTS (Material No. 11-002). (b) To remove mud or other unwanted material (insects,...), make it soft with water, and scrape it off with a SCRAPER - PLASTIC and a SPONGE soaked in water. Be very careful not to scratch the surface. If there are stains on the painted area, do not try to remove them. (5) Flushing of the aircraft CAUTION : MAKE SURE YOU FLUSH THE SURFACE SUFFICIENTLY TO REMOVE ALL _______ THE CLEANING SOLUTION. CLEANING SOLUTION THAT STAYS ON THE AIRCRAFT SURFACE CAN CAUSE CORROSION. (a) Let the cleaning solution have an effect, and after approximately 10 minutes, flush before it becomes dry. (b) Flush with hot water at 65 deg.C (149.00 deg.F) maximum to remove signs of cleaning solution. Do not use steam. (c) When you flush the wing and the horizontal stabilizer, always complete this step with the bottom skin.
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(d) If there is ice after the flushing operation, do the de-icing of the aircraft (Ref. TASK 12-31-12-660-801). (e) In the zones where access is not easy, use clean, dry compressed air that does not contain oil, to remove the remaining moisture. Subtask 12-21-11-615-054 B. Cleaning of the Windows (1) Clean the windshield (Ref. TASK 56-10-00-100-801). (2) Clean the sliding and the fixed windows (Ref. TASK 56-10-00-100-802). (3) Clean the outer surfaces of the window panes (Ref. TASK 56-21-15-100801). R R
Subtask 12-21-11-615-055-B C. Cleaning of the Landing Gear Bays and Landing Gears
R R R
CAUTION : MAKE SURE YOU FLUSH THE SURFACE SUFFICIENTLY TO REMOVE ALL THE _______ CLEANING SOLUTION. CLEANING SOLUTION THAT STAYS ON THE AIRCRAFT SURFACE CAN CAUSE CORROSION.
R R R
(1) Opening of the landing-gear doors: - open the nose landing-gear doors (Ref. TASK 32-22-00-010-801), - open the main landing-gear doors (Ref. TASK 32-12-00-010-801).
R R
(2) Make sure that the opening in the landing-gear bays are correctly closed.
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(3) Cleaning of the landing-gear bays
R R R
NOTE : As there are many components in the landing-gear bays that can ____ be easily damaged. We recommend that you clean the landing-gear bays only when you do maintenance procedures.
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(a) Make sure that each landing-gear wheel/brake has protection.
R R R
(b) Apply CLEANING AGENTS (Material No. 11-001) with a SPONGE only on the applicable parts of the landing-gear bays, and in the internal surfaces of the landing-gear doors.
R R R
(c) In the zones where access is not easy, apply CLEANING AGENTS (Material No. 11-001) with a BRUSH - BRISTLED, SOFT, to remove all signs of grease and oil.
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R R
(d) Flush the applicable parts of the landing-gear bays to remove all signs of cleaning solution.
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(e) In the zones where access is not easy, use clean, dry compressed air that does not contain oil, to remove the remaining moisture.
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(4) Cleaning of the landing-gears
R
(a) Cleaning of the Nose Landing-Gear (Ref. TASK 32-21-00-100-801).
R
(b) Cleaning of the Main Landing-Gear (Ref. TASK 32-11-00-100-801). Subtask 12-21-11-916-050 D. Corrosion Prevention (1) Remove SPECIAL MATERIALS (Material No. 05-005): - to all threads of studs on the bridge brackets, the washers and the nuts of the landing-gears. (2) Apply SPECIAL MATERIALS (Material No. 05-027): (a) On the painted surfaces of the landing-gears and the landing-gear bays. NOTE : The painted surfaces must be in the correct condition (no ____ damage, marks, scratches and/or signs of corrosion) before you apply the material. (3) Apply SPECIAL MATERIALS (Material No. 05-005): - to all threads of studs on the bridge brackets, the washers and the nuts of the landing-gears. Subtask 12-21-11-640-051 E. Lubrication (1) Lubricate the main landing gear and doors (Ref. TASK 12-22-32-600817). (2) Lubricate the nose gear and doors (Ref. TASK 12-22-32-600-819).
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Subtask 12-21-11-210-053 F. Visual Inspection (1) Make sure that the paint on the components is in the correct condition and that there are no signs of corrosion. (2) Make sure that the bond is correct and that none of the rubber sealant is missing. (3) Make sure that there is no unwanted material in the holes and threads. (4) Make sure that there is no hydraulic fluid on the hydraulic pipes. 5. Close-up ________ Subtask 12-21-11-860-053 A. Aircraft Maintenance Configuration (1) Remove the aircraft protective equipment (Ref. TASK 10-11-00-555814). (2) Remove all FILM - POLYETHYLENE. (3) Remove all signs of TAPE - ADHESIVE with a MISCELLANEOUS (Material No. 19-003) soaked in CLEANING AGENTS (Material No. 11-002). (4) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (5) On the panel 225 VU, release the DITCHING pushbutton switch to open: - the outflow valves 313HL and 315HL, - the underfloor extract valve 12HQ, - the overboard extract valve 13HQ. (a) Visually make sure that: - the outflow valves 313HL and 315HL are in the open position before you apply air on the aircraft and you start the air conditioning packs, - the avionics compartment ventilation operates correctly.
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Subtask 12-21-11-410-051 B. Put the aircraft back to its initial configuration (1) Remove the tag from the Captain side stick or write in the log book that the protection covers/devices are not installed. (2) Close the main landing-gear doors (Ref. TASK 32-12-00-410-801). (3) Close the nose landing-gear doors (Ref. TASK 32-22-00-410-801). (4) Remove the ground support and the maintenance equipment, the special and standard tools and all other items. (5) De-energize the aircraft electrical circuit (Ref. TASK 24-41-00-862801).
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INTERNAL CLEANING - SERVICING _____________________________ R
TASK 12-21-12-100-801
R
Cleaning of the Cockpit Display-Units
R
1. __________________ Reason for the Job
R
Self Explanatory
R R
2. ______________________ Job Set-up Information A. Referenced Information
R R R
------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R R R R R
22-82-12-100-801
R
3. __________ Job Set-up
R
Subtask 12-21-12-861-050
R R
24-42-00-861-801 24-42-00-862-801 31-63-22-100-801 12-21-12-991-008
A. Energize the ground service network (Ref. TASK 24-42-00-861-801)
R
4. Procedure _________
R
Subtask 12-21-12-160-050
R R
Cleaning of the Screen of the Multipurpose Control Display Unit (MCDU) (2CA1,2CA2,2CA3) Energize the Ground Service Network De-energize the Ground Service Network Cleaning of the Display Unit (DU) (1WK1,1WK2,2WK1,2WK2,3WK1,3WK2) Fig. 301
A. Cleaning of the Cockpit Display-Units (Ref. Fig. 301/TASK 12-21-12-991-008)
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(1) Clean the instrument panel display-units (DU) (Ref. TASK 31-63-22100-801).
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(2) Clean the multipurpose control display-unit(s) (MCDU) (Ref. TASK 2282-12-100-801).
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R R
Cockpit Display Units Figure 301/TASK 12-21-12-991-008
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(3) Make sure that the work area is clean and clear of tools and other items.
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5. Close-up ________
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Subtask 12-21-12-862-050
R R
A. De-energize the ground service network (Ref. TASK 24-42-00-862-801)
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TASK 12-21-12-100-802 R
Cleaning of the Cockpit Equipment/Furnishings 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R R R
No No No No
specific specific specific specific
vacuum cleaner 1 BRUSH - BRISTLED, FIBER, SOFT 1 BRUSH - BRISTLED, STIFF 1 CAP - PROTECTION
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------No specific Material No. 11-017 R R
Material No. 19-003
warm clean water USA AMS 1550 INTERIOR GENERAL PLASTIC CLEANER (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
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C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R
24-42-00-861-801 24-42-00-862-801 25-13-00-100-801 56-10-00-100-801 56-10-00-100-802
Energize the Ground Service Network De-energize the Ground Service Network Cleaning of Foam Plastic (Polyurethane) Parts Cleaning of the Windshield (3DG1,3DG2). Cleaning of the Sliding (8DG1,8DG2) and the Fixed Windows (7DG1,7DG2).
R R
CMM 25-11-XX 12-21-12-991-005
Fig. 302
3. __________ Job Set-up Subtask 12-21-12-861-057 A. Energize the ground service network (Ref. TASK 24-42-00-861-801) 4. Procedure _________ Subtask 12-21-12-160-054 R
A. Cleaning of the Cockpit Equipment/Furnishings (Ref. Fig. 302/TASK 12-21-12-991-005) WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL _______ MATERIALS ONLY WITH A GOOD FLOW OF AIR THROUGH THE WORK AREA. THESE MATERIALS ARE POISONOUS AND FLAMMABLE AND SKIN IRRITANTS. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
R R R R
(1) Clean the inner surface of the cockpit windows: (Ref. TASK 56-10-00-100-801) and (Ref. TASK 56-10-00-100-802).
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(2) Clean the foam plastic (polyurethane) parts (Ref. TASK 25-13-00-100801).
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Linings and furnishing - Cockpit Figure 302/TASK 12-21-12-991-005
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R R
(3) Clean the overhead panel, the glare shield, the main instrument panel, the lateral consoles and the center pedestal. (a) Put a CAP - PROTECTION on each electrical outlet. (b) Remove the loose dirt from the surfaces with a BRUSH - BRISTLED, FIBER, SOFT and a vacuum cleaner. CAUTION : USE ONLY THE SPECIFIED MATERIALS AND OBEY THE _______ INSTRUCTIONS FROM THE MANUFACTURERS. OTHER MATERIALS CAN CAUSE DAMAGE TO THE SURFACE PROTECTION OF THE COMPONENTS AND THE RELATED AREA. (c) Moisten a clean, lint-free cotton cloth MISCELLANEOUS (Material No. 19-003) with CLEANING AGENTS (Material No. 11-017) and apply it to the surface you will clean.
R R
NOTE : To prevent contamination of the cleaning agent, do not put ____ the cloth into the cleaning agent. (d) Moisten a clean, lint-free cotton cloth MISCELLANEOUS (Material No. 19-003) with warm clean water and lightly rub the surface you will clean. NOTE : Always make the cloth moist, not the part you will clean. ____ (e) Dry the surface with a clean, lint-free cotton cloth MISCELLANEOUS (Material No. 19-003). (4) Clean the Seats (a) Clean the seats as given in the (Ref. CMM 25-11-XX) of the seat manufacturer. (5) Clean the floor (a) Remove the loose dirt with a vacuum cleaner. NOTE : The following work steps are only applicable if ____ non-textile floor covering (NTF) is installed. (b) Apply CLEANING AGENTS (Material No. 11-017) to the surface with a BRUSH - BRISTLED, STIFF.
R R
NOTE : To prevent contamination of the cleaning agent, do not put ____ the brush into the cleaning agent.
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(c) Clean the surface with a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003) and warm clean water. (d) Dry the surface with a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003). (6) Remove the protection caps from the electrical outlets. (7) Make sure that the work area is clean and clear of tools and other items. 5. Close-up ________ Subtask 12-21-12-862-057 A. De-energize the ground service network (Ref. TASK 24-42-00-862-801)
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TASK 12-21-12-100-803 Cleaning of the Carpets and Non-Textile Floor (NTF) Covering 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No
specific specific specific specific specific
cloth medium fiber brush paper towels stiff fiber brush vacuum cleaner
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------No specific No specific Material No. 11-017 Material No. 11-018
warm clean water warm water USA AMS 1550 INTERIOR GENERAL PLASTIC CLEANER (Ref. 20-31-00) USA AMS 1630 CARPET AND FABRIC CLEANER (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801
Energize the Ground Service Network De-energize the Ground Service Network
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3. __________ Job Set-up Subtask 12-21-12-861-058 A. Energize the ground service network (Ref. TASK 24-42-00-861-801) 4. Procedure _________ Subtask 12-21-12-160-055 A. Cleaning of the Carpets and NTF Floor Covering WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL _______ MATERIALS ONLY WITH A GOOD FLOW OF AIR THROUGH THE WORK AREA. THESE MATERIALS ARE POISONOUS AND FLAMMABLE AND SKIN IRRITANTS. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. CAUTION : USE ONLY THE SPECIFIED MATERIALS AND OBEY THE INSTRUCTIONS FROM _______ THE MANUFACTURERS. OTHER MATERIALS CAN CAUSE DAMAGE TO THE SURFACE PROTECTION OF THE COMPONENTS AND THE RELATED AREA. (1) Clean the carpets. (a) Stain removal. 1 _
Soak the area of the stain with warm clean water.
2 _
Dry the area of the stain with paper towels.
3 _
Carefully apply CLEANING AGENTS (Material No. 11-018) to the area of the stain with a medium fiber brush.
4 _
Dry the area with paper towels.
5 _
Use a medium fiber brush to lift the carpet pile.
(b) Dirt removal. 1 _
Clean the area with a vacuum cleaner.
2 _
Use a medium fiber brush to lift the carpet pile.
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(2) Clean the NTF floor covering. (a) Remove the loose dirt from surface with a vacuum cleaner. (b) Apply CLEANING AGENTS (Material No. 11-017) to the surface with a stiff fiber brush. (c) Clean the surface with a cloth and a warm water. (d) Dry the surface with a cloth. 5. Close-up ________ Subtask 12-21-12-862-058 A. De-energize the ground service network (Ref. TASK 24-42-00-862-801)
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TASK 12-21-12-100-804 Cleaning of the Plastic Surfaces and Mirrors 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R R R
No specific No specific No specific
1 BRUSH - BRISTLED, FIBER, SOFT 1 CAP - PROTECTION 1 CHAMOIS LEATHER
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
No specific No specific Material No. 05-010 Material No. 11-017 Material No. 11-019
R R
Material No. 19-003
sponge warm clean water PLASTIC CLEANER (Ref. 20-31-00) USA AMS 1550 INTERIOR GENERAL PLASTIC CLEANER (Ref. 20-31-00) USA AMS 1535 CABIN WINDOW CLEANER (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
EFF : ALL 12-21-12 SROS
Page 312 Jul 01/06
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R
24-42-00-861-801 24-42-00-862-801 12-21-12-991-003
R
**ON A/C 301-399,
R
12-21-12-991-007
Energize the Ground Service Network De-energize the Ground Service Network Fig. 303
Fig. 304
**ON A/C ALL 3. __________ Job Set-up Subtask 12-21-12-861-059 A. Energize the ground service network (Ref. TASK 24-42-00-861-801) 4. Procedure _________ Subtask 12-21-12-160-056 A. Clean the Plastic Surfaces and Mirrors R R R
(Ref. Fig. 303/TASK 12-21-12-991-003) **ON A/C 301-399,
R
(Ref. Fig. 304/TASK 12-21-12-991-007)
EFF : ALL 12-21-12 SROS
Page 313 Apr 01/05
Component Location/Surface Finish Identification Figure 303/TASK 12-21-12-991-003- 12 (SHEET 1)
R
R EFF : ALL 12-21-12 SROS
Page 314 Apr 01/05
Component Location/Surface Finish Identification Figure 303/TASK 12-21-12-991-003- 22 (SHEET 2)
R
EFF : ALL 12-21-12 SROS
Page 315 Apr 01/05
Linings and furnishing - Lower Deck Cabin Figure 304/TASK 12-21-12-991-007
R
R EFF : 301-399, 12-21-12 SROS
Page 316 Apr 01/05
**ON A/C ALL WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL _______ MATERIALS ONLY WITH A GOOD FLOW OF AIR THROUGH THE WORK AREA. THESE MATERIALS ARE POISONOUS AND FLAMMABLE AND SKIN IRRITANTS. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. CAUTION : USE ONLY THE SPECIFIED MATERIALS AND OBEY THE INSTRUCTIONS FROM _______ THE MANUFACTURERS. OTHER MATERIALS CAN CAUSE DAMAGE TO THE SURFACE PROTECTION OF THE COMPONENTS AND THE RELATED AREA. NOTE : The water and equipment that you use for these procedures must be ____ clean and contain no particles that could damage the surfaces. (1) Cleaning of the plastic surfaces. R
(a) Put CAP - PROTECTION on the electrical outlets so that they do not get wet. (b) Remove the loose dirt from the surface with a BRUSH - BRISTLED, FIBER, SOFT.
R R R
(c) Apply CLEANING AGENTS (Material No. 11-017) to the dirty surface with a lint-free cotton cloth MISCELLANEOUS (Material No. 19003).
R
(d) Clean the surface with a sponge and warm clean water.
R R
(e) Dry the surface with a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003).
R
(f) Remove the protection caps from the electrical outlets. (2) Cleaning of the transparent plastic surfaces.
R
(a) Put CAP - PROTECTION on the electrical outlets so that they do not get wet.
R R R
(b) Clean the surface with a clean lint-free cotton cloth MISCELLANEOUS (Material No. 19-003) and warm clean water.
EFF : ALL 12-21-12 SROS
Page 317 Jul 01/06
R R
(c) Apply CLEANING AGENTS (Material No. 11-017) to the surface with a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003) .
R R
(d) Clean the surface with warm clean water and dry it with a CHAMOIS LEATHER . (e) If there is a stain:
R R R R R R R
- Apply SPECIAL MATERIALS (Material No. 05-010) to the surface with a lint-free cotton cloth MISCELLANEOUS (Material No. 19003). - Clean the surface with warm water and dry it with a chamois leather.
R
(f) Remove the protection caps from the electrical outlets. (3) Cleaning of the mirrors.
R
(a) Clean the surface with a sponge and warm clean water.
R R
(b) Apply CLEANING AGENTS (Material No. 11-019) to the surface with a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003).
R R
(c) Clean the surface with warm clean water and dry it with a CHAMOIS LEATHER. 5. Close-up ________ Subtask 12-21-12-862-059 A. De-energize the ground service network (Ref. TASK 24-42-00-862-801)
EFF : ALL 12-21-12 SROS
Page 318 Jul 01/06
TASK 12-21-12-100-805 Cleaning of the Curtains 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
paper towels
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 11-002 Material No. 11-018
USA MIL-PRF-680 DRY CLEANING SOLVENT (VARSOL/WHITE SPIRIT) (Ref. 20-31-00) USA AMS 1630 CARPET AND FABRIC CLEANER (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801
Energize the Ground Service Network De-energize the Ground Service Network
3. __________ Job Set-up Subtask 12-21-12-861-060 A. Energize the ground service network (Ref. TASK 24-42-00-861-801)
EFF : ALL 12-21-12 R SROS
Page 319 Jan 01/06
4. Procedure _________ Subtask 12-21-12-110-050 A. Cleaning of the Curtains WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL _______ MATERIALS ONLY WITH A GOOD FLOW OF AIR THROUGH THE WORK AREA. THESE MATERIALS ARE POISONOUS AND FLAMMABLE AND SKIN IRRITANTS. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. CAUTION : USE ONLY THE SPECIFIED MATERIALS AND OBEY THE INSTRUCTIONS FROM _______ THE MANUFACTURERS. OTHER MATERIALS CAN CAUSE DAMAGE TO THE SURFACE PROTECTION OF THE COMPONENTS AND THE RELATED AREA. (1) Stain removal. (a) Soak the area of the stain with CLEANING AGENTS (Material No. 11018). 1 _
Dry the wet area with paper towels.
(b) Dry clean. 1 _
Dry clean the area of the stain with a solution of CLEANING AGENTS (Material No. 11-018) and CLEANING AGENTS (Material No. 11-002).
5. Close-up ________ Subtask 12-21-12-862-060 A. De-energize the ground service network (Ref. TASK 24-42-00-862-801)
EFF : ALL 12-21-12 R SROS
Page 320 Jan 01/06
TASK 12-21-12-100-806 Cleaning of Light Alloy and Steel Components 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
cloth masking paper
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------No specific Material No. 11-016
warm clean water USA BOEING BAC 5000 BAC 5504 CLEANING SOLVENT (Ref. 20-31-00)
BAC 5750
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801
Energize the Ground Service Network De-energize the Ground Service Network
3. __________ Job Set-up Subtask 12-21-12-861-061 A. Energize the ground service network (Ref. TASK 24-42-00-861-801)
EFF : ALL 12-21-12 R SROS
Page 321 Jan 01/06
4. Procedure _________ Subtask 12-21-12-160-057 A. Cleaning of Light Alloy and Stainless Steel Components (1) Put masking paper on the electrical outlets so that they do not get wet. (a) Apply CLEANING AGENTS (Material No. 11-016) to the surface with a cloth. (b) Clean the surface with a cloth and warm clean water. (c) Dry the surface with a cloth. (d) Remove the masking paper from the electrical outlets. 5. Close-up ________ Subtask 12-21-12-862-061 A. De-energize the ground service network (Ref. TASK 24-42-00-862-801)
EFF : ALL 12-21-12 R SROS
Page 322 Jan 01/06
TASK 12-21-12-100-807 Cleaning of the Cargo Compartments 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
R
No No No No No No
specific specific specific specific specific specific
blanking caps BRUSH - NON METALLIC CONTAINER 100 L(25 USGAL) HOT AIR BLOWER OPERATING 40 DEG C (100 DEG F) SCRAPER - NON METALLIC VACUUM CLEANER
2 2 2 2 2
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R
No specific No specific Material No. 09-005 Material No. 11-001 Material No. 19-003
clean water Clean water USA MIL-S-81733 CLASS C CORROSION INHIBITIVE INTERFAY SEALANT (Ref. 20-31-00) USA MIL-D-16791 TYPE I DETERGENT (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
EFF : ALL 12-21-12 SROS
Page 323 Jan 01/07
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801
Energize the Ground Service Network De-energize the Ground Service Network
25-51-26-000-801 25-51-26-400-801 25-51-58-000-801
Removal of the Power Drive Units Installation of the Power Drive Units Removal of the Drain System in the FWD Cargo Compartment Removal of the Drain System in the AFT Cargo Compartment Installation of the Drain System in the FWD Cargo Compartment Installation of the Drain System in the AFT Cargo Compartment Visual Check of Drain Outlets for Evidence of Drainage System Obstruction and Clean as Necessary. Visual Check of Drain Outlets for Evidence of Drainage System Obstruction and Clean as Necessary. Aircraft Cleaning after a Fish Shipment Opening of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Removal of the Safety Support Equipment Closing of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Installation of the Safety Support Equipment
R
25-51-58-000-802 25-51-58-400-801 25-51-58-400-802 R R R R
25-52-00-210-802 25-53-00-210-804 51-78-00-615-803 52-30-00-010-801 52-30-00-080-801 52-30-00-410-801 52-30-00-480-801 3. __________ Job Set-up Subtask 12-21-12-861-063
A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-21-12-010-054 B. Get Access (1) If necessary, open the FWD and/or AFT cargo-compartment door (Ref. TASK 52-30-00-010-801). (2) Safety the cargo compartment door(s) (Ref. TASK 52-30-00-480-801).
EFF : ALL 12-21-12 SROS
Page 324 Jan 01/07
Subtask 12-21-12-865-057 C. Get access to the applicable 5000VE series panel(s). Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 14MY 5002VE FWD CARGO LOADING POWER RH1 5MY A13 5002VE FWD CARGO LOADING POWER LH1 3MY A10 5002VE FWD CARGO LOADING POWER RH2 4MY B13 5002VE FWD CARGO LOADING POWER LH2 2MY B10 5002VE FWD CARGO LOADING CTL 1MY C13 FOR 114MY **ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, 701-749, 5006VE 5006VE 5006VE 5006VE
AFT AFT AFT AFT
CLS / RH1-PWR CLS/LH1-POWER CLS / RH2-PWR CLS/LH2-POWER
105MY 103MY 104MY 102MY
A13 A10 B13 B10
101MY
C13
105MY 103MY 104MY 102MY
A13 A10 B13 B10
**ON A/C ALL 5006VE AFT CARGO LOADING CTL **ON A/C 301-399, 5006VE 5006VE 5006VE 5006VE
AFT AFT AFT AFT
CARGO CARGO CARGO CARGO
LOADING LOADING LOADING LOADING
POWER POWER POWER POWER
RH1 LH1 RH2 LH2
EFF : ALL 12-21-12 R SROS
Page 325 Jan 01/06
**ON A/C ALL 4. Procedure _________ Subtask 12-21-12-160-059 A. Dry Cleaning of the Cargo Compartment(s) WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL _______ MATERIALS ONLY WITH A GOOD FLOW OF AIR THROUGH THE WORK AREA. THESE MATERIALS ARE POISONOUS AND FLAMMABLE AND SKIN IRRITANTS. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. R
(1) Remove loose materials with a SCRAPER - NON METALLIC or a BRUSH - NON METALLIC and a VACUUM CLEANER.
R R
(2) Clean the area with CLEANING AGENTS (Material No. 11-001) and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003).
R
(3) Additional Special Cleaning after Seafood/Wet Cargo Shipment: NOTE : This procedure is only applicable if leakage from a shipping ____ container has been reported.
R R
(a) Make a cleaning solution of 0.5 % CLEANING AGENTS (Material No. 11-001) and Clean water: - Mix 5.0 g (0.17 oz) of CLEANING AGENTS (Material No. 11-001) with every 1 l (0.2641 USgal) of water. (b) Clean the area with the cleaning solution and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003). (c) Dry the area with a HOT AIR BLOWER OPERATING 40 DEG C (100 DEG F) .
R R
(4) If necessary clean the bilge area (Ref. TASK 51-78-00-615-803).
EFF : ALL 12-21-12 SROS
Page 326 Jan 01/07
Subtask 12-21-12-160-065 B. Wet Cleaning of the Cargo Compartment(s) WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL _______ MATERIALS ONLY WITH A GOOD FLOW OF AIR THROUGH THE WORK AREA. THESE MATERIALS ARE POISONOUS AND FLAMMABLE AND SKIN IRRITANTS. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. (1) Remove loose materials with a SCRAPER - NON METALLIC or a BRUSH - NON METALLIC and a VACUUM CLEANER.
R
(2) Remove the Power Drive Units (PDUs) (Ref. TASK 25-51-26-000-801). (3) Put blanking caps on the disconnected electrical connectors. (4) Apply SEALANT SEALANTS (Material No. 09-005) on all the mounting holes of the PDUs bonding points. R R R R R
(5) Do a check and clean as necessary the drain filters of the cargo loading system (CLS): - Forward cargo compartment (Ref. TASK 25-52-00-210-802), - Aft cargo compartment (Ref. TASK 25-53-00-210-804).
R
(6) Put a CONTAINER 100 L(25 USGAL) below the drain mast(s). (7) Clean the cargo compartment(s) as follows: CAUTION : MAKE SURE THAT YOU DO NOT PUT WATER DIRECTLY ON THE BALL _______ MATS AND THE FLOOR PANEL AREAS THAT HAVE POWER DRIVE UNITS. WATER ON THESE AREAS CAN CAUSE CORROSION AND ELECTRICAL MALFUNCTIONS IN THE CLS.
R R R R R R R R
(a) Flush hot max 60.0 deg.C (140.00 deg.F) clean water (or a cleaning solution of 0.5 % CLEANING AGENTS (Material No. 11-001) and water) with a maximum flow rate of 5 l/min: - On the floor panel area at the aft end of the forward compartment, - On the ball mat area of the aft compartment, - On the rigid corner sheets and the lower sidewall panels.
EFF : ALL 12-21-12 SROS
Page 327 Jan 01/07
R (b) Brush the floor panels to apply water flow to the roller track outer flanges. (c) Make sure that water flows freely through the drain masts. (8) Replace Drain System filters (Ref. TASK 25-51-58-000-801), (Ref. TASK 25-51-58-400-801), (Ref. TASK 25-51-58-000-802) and (Ref. TASK 25-5158-400-802), as necessary. R R
(9) Dry the compartment floor and the CLS with a HOT AIR BLOWER OPERATING 40 DEG C (100 DEG F) . (10) Install the PDUs (Ref. TASK 25-51-26-400-801). 5. Close-up ________ Subtask 12-21-12-865-058 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 14MY 1MY, 2MY, 3MY, 4MY, 5MY. FOR 114MY 101MY, 102MY, 103MY, 104MY, 105MY. Subtask 12-21-12-410-054 B. Close Access (1) Remove the safety support equipment from the cargo compartment doors (Ref. TASK 52-30-00-080-801). (2) Remove the access platform(s). (3) Close the cargo compartment door(s) (Ref. TASK 52-30-00-410-801). Subtask 12-21-12-862-063 C. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-21-12 SROS
Page 328 Jan 01/07
TASK 12-21-12-100-808 Cleaning of the Monitors and Display Screens in the Cabin 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
absorbent surgical cotton wadding sterile gauze pad
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 11-020 VISUAL DISPLAY UNIT ANTI-STATIC CLEANER (Ref. 20-31-00) C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801
Energize the Ground Service Network De-energize the Ground Service Network
3. __________ Job Set-up Subtask 12-21-12-861-062 A. Energize the ground service network (Ref. TASK 24-42-00-861-801).
EFF : ALL 12-21-12 R SROS
Page 329 Jan 01/06
4. Procedure _________ Subtask 12-21-12-160-058 A. Cleaning of the Monitors and Display Screens CAUTION : USE ONLY THE SPECIFIED MATERIALS AND OBEY THE INSTRUCTIONS FROM _______ THE MANUFACTURERS. OTHER MATERIALS CAN CAUSE DAMAGE TO THE SURFACE PROTECTION OF THE COMPONENTS AND THE RELATED AREA. (1) Get a absorbent surgical cotton wadding or a sterile gauze pad moist with CLEANING AGENTS (Material No. 11-020). Lightly rub one time the surface. (2) Get a new piece of wadding or gauze soaked with the anti-static cleaner. Rub the surface of the screen again and remove all the marks. NOTE : Use a new piece of wadding (or gauze) each time, because dust ____ on the wadding (or gauze) can cause scratches on the screen. Dry the screen with a clean wadding (or gauze). Rub the screen one time only with each new piece of wadding (or gauze). NOTE : Always make the pad moist, not the screen. ____ Rub the screen lightly. We recommend you mist the surface of the screen before you rub it with the wadding (or gauze). This prevents scratches. The more frequently you replace the wadding (or gauze) the faster and better is the cleaning. 5. Close-up ________ Subtask 12-21-12-862-062 A. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-21-12 R SROS
Page 330 Jan 01/06
TASK 12-21-12-100-809 Cleaning of the Plastic Wash Basin in the Lavatories 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 BRUSH - BRISTLED, FIBER, SOFT
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific No specific Material No. 05-008 Material No. 05-009 Material No. 19-003
abrasive general household cleaning agent mild soap solution sponge warm, clean water PLASTIC POLISHING COMPOUND (COARSE GRADE) (Ref. 20-31-00) USA PP-560 TYPE 1 PLASTIC POLISHING COMPOUND (FINE GRADE) (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 25-00-00-340-808 12-21-12-991-004
Energize the Ground Service Network De-energize the Ground Service Network Repair of the Lavatory Plastic Wash-Basin Fig. 305
EFF : ALL 12-21-12 R SROS
Page 331 Jan 01/06
3. __________ Job Set-up Subtask 12-21-12-861-064 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). 4. Procedure _________ Subtask 12-21-12-160-060 A. General Cleaning (Ref. Fig. 305/TASK 12-21-12-991-004) NOTE : The water and equipment that you use for these procedures must be ____ clean and contain no particles that could damage the surfaces. (1) Remove the loose dirt from the surface with a BRUSH - BRISTLED, FIBER, SOFT. (2) Apply a mild soap solution to the dirty surface with a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003). NOTE : If necessary, use more soap for a stronger solution. ____ (3) Rinse the surface with a sponge and warm, clean water. (4) Wipe the surface dry with a soft lint-free cotton cloth MISCELLANEOUS (Material No. 19-003) NOTE : Make sure that there is no abrasive material on the surface. ____ Abrasive materials can damage the surface. (5) If necessary, do Para. B. steps (1) thru (3). Subtask 12-21-12-160-061 B. Special Cleaning CAUTION : USE ONLY THE SPECIFIED MATERIALS AND OBEY THE INSTRUCTIONS FROM _______ THE MANUFACTURERS. OTHER MATERIALS CAN CAUSE DAMAGE TO THE SURFACE PROTECTION OF THE COMPONENTS AND THE RELATED AREA. NOTE : Removal of the Stain(s) made with: ____ - cigarette burns, - a felt pen, - a lipstick,
EFF : ALL 12-21-12 R SROS
Page 332 Jan 01/06
Linings and furnishing - Lavatory Figure 305/TASK 12-21-12-991-004 EFF : ALL 12-21-12 R SROS
Page 333 Jan 01/06
-
hair dye, hairspray, mascara, nail varnish, shoe polish.
(1) Apply an abrasive general household cleaning agent to the area of the stain(s) and wipe it with a moist cloth. NOTE : Do step (2) again, if necessary. ____ (2) Rinse the surface with a sponge and warm, clean water. (3) Wipe the surface dry with a soft lint-free cotton cloth MISCELLANEOUS (Material No. 19-003). NOTE : Make sure that there is no abrasive material on the surface. ____ Abrasive materials can damage the surface. (a) If necessary, do Para. C. steps (1) thru (3). Subtask 12-21-12-160-062 C. Intensive Cleaning (Polishing) CAUTION : USE ONLY THE SPECIFIED MATERIALS AND OBEY THE INSTRUCTIONS FROM _______ THE MANUFACTURERS. OTHER MATERIALS CAN CAUSE DAMAGE TO THE SURFACE PROTECTION OF THE COMPONENTS AND THE RELATED AREA. NOTE : Removal of the Stain(s) made with: ____ - cigarette burns, - a felt pen, - a lipstick, - hair dye, - hairspray, - mascara, - nail varnish, - shoe polish. (1) Apply SPECIAL MATERIALS (Material No. 05-008) to the area of the stain(s) and wipe it with a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003). (2) Apply SPECIAL MATERIALS (Material No. 05-009) to the area of the stain(s) and wipe it with a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003).
EFF : ALL 12-21-12 R SROS
Page 334 Jan 01/06
(3) Polish the surface with a soft lint-free cotton cloth MISCELLANEOUS (Material No. 19-003). NOTE : Make sure that there is no abrasive material on the surface. ____ Abrasive materials can damage the surface. Subtask 12-21-12-160-063 D. Removal of Scratches (1) Repair the surfaces that have scratches (Ref. TASK 25-00-00-340-808). 5. Close-up ________ Subtask 12-21-12-862-064 A. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-21-12 R SROS
Page 335 Jan 01/06
TASK 12-21-12-100-810 Cleaning of the Seat Covers 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
paper towel vacuum cleaner
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 11-002 Material No. 11-018
USA MIL-PRF-680 DRY CLEANING SOLVENT (VARSOL/WHITE SPIRIT) (Ref. 20-31-00) USA AMS 1630 CARPET AND FABRIC CLEANER (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 24-41-00-862-801
Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A
EFF : ALL 12-21-12 R SROS
Page 336 Apr 01/05
3. __________ Job Set-up Subtask 12-21-12-861-065 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). 4. Procedure _________ Subtask 12-21-12-110-051 A. Cleaning (1) Remove the loose dirt from the seats with a vacuum cleaner. (2) Removal of the Stains WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL _______ MATERIALS ONLY WITH A GOOD FLOW OF AIR THROUGH THE WORK AREA. THESE MATERIALS ARE POISONOUS AND FLAMMABLE AND SKIN IRRITANTS. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. WARNING : DO NOT GET THE COMPOUND ON YOUR SKIN. _______ IF YOU DO: - REMOVE IT IMMEDIATELY WITH A CLEAN CLOTH - WASH YOUR SKIN WITH SOAP AND RINSE WITH CLEAN WATER. CAUTION : USE ONLY THE SPECIFIED MATERIALS AND OBEY THE INSTRUCTIONS _______ FROM THE MANUFACTURERS. OTHER MATERIALS CAN CAUSE DAMAGE TO THE SURFACE PROTECTION OF THE COMPONENTS AND THE RELATED AREA. (a) Soak the area of the stain with CLEANING AGENTS (Material No. 11018). (b) Dry the wet area with a paper towel.
EFF : ALL 12-21-12 R SROS
Page 337 Apr 01/05
(3) Dry Clean (a) Dry clean the area of the stain with CLEANING AGENTS (Material No. 11-018) and CLEANING AGENTS (Material No. 11-002). (b) Dry the wet area with a paper towel. (4) Refer to the vendor documentation if necessary. 5. Close-up ________ Subtask 12-21-12-862-065 A. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
EFF : ALL 12-21-12 R SROS
Page 338 Apr 01/05
TASK 12-21-12-100-811 Cleaning of the Air Inlet Grids of Galleys and Lavatories 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------No specific No specific Material No. 11-017 Material No. 19-003
clean warm water sponge USA AMS 1550 INTERIOR GENERAL PLASTIC CLEANER (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------21-23-00-600-801 24-42-00-861-801 24-42-00-862-801 25-30-00-920-802 25-35-19-000-801 25-35-19-400-801
Replacement of the Lavatory Air-Extraction Filter Energize the Ground Service Network De-energize the Ground Service Network Discard the Galley Air-Extraction Filter-Element Removal of the Oven Installation of the Oven
3. __________ Job Set-up Subtask 12-21-12-861-067 A. Energize the ground service network (Ref. TASK 24-42-00-861-801)
EFF : ALL 12-21-12 R SROS
Page 339 Apr 01/05
4. Procedure _________ WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL MATERIALS _______ ONLY WITH A GOOD FLOW OF AIR THROUGH THE WORK AREA. THESE MATERIALS ARE POISONOUS AND FLAMMABLE AND SKIN IRRITANTS. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. CAUTION : USE ONLY THE SPECIFIED MATERIALS AND OBEY THE INSTRUCTIONS FROM _______ THE MANUFACTURERS. OTHER MATERIALS CAN CAUSE DAMAGE TO THE SURFACE PROTECTION OF THE COMPONENTS AND THE RELATED AREA. Subtask 12-21-12-160-066 A. Cleaning of the Ventilation Grids in the Galleys that have Ovens Installed. (1) Remove the oven(s) if necessary (Ref. TASK 25-35-19-000-801). (2) Apply CLEANING AGENTS (Material No. 11-017) to the grids. (3) Clean the grids with a sponge and clean warm water and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003). (4) Do a visual inspection of the component interface and/or the adjacent area. (5) If necessary replace the air filter pads (Ref. TASK 25-30-00-920802). (6) Install the oven(s) if removed (Ref. TASK 25-35-19-400-801). Subtask 12-21-12-160-067 B. Cleaning of the Ventilation Grids in the Lavatories (1) Apply CLEANING AGENTS (Material No. 11-017) to the grids. (2) Clean the grids with a sponge and clean warm water and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003). (3) Do a visual inspection of the component interface and/or the adjacent area.
EFF : ALL 12-21-12 R SROS
Page 340 Apr 01/05
(4) If necessary replace the air filter pads (Ref. TASK 21-23-00-600801). 5. Close-up ________ Subtask 12-21-12-862-067 A. De-energize the ground service network (Ref. TASK 24-42-00-862-801)
EFF : ALL 12-21-12 R SROS
Page 341 Apr 01/05
TASK 12-21-12-670-801 Disinfection of the Aircraft Equipment and Furnishing WARNING : ONLY PERSONS NECESSARY FOR THIS PROCEDURE ARE PERMITTED IN THE _______ AIRCRAFT DURING THE TASK. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific No specific
1 GUN - SPRAY 1 WARNING NOTICE
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------No specific Material No. 14-006B Material No. 19-003
clean water USA AMS 1452 DISINFECTANT LIQUID AIRCRAFT GENERAL PURPOSE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 52-30-00-010-801 52-30-00-410-801
Energize the Ground Service Network De-energize the Ground Service Network Opening of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Closing of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump
EFF : ALL 12-21-12 SROS
Page 342 Jan 01/06
3. __________ Job Set-up Subtask 12-21-12-861-051 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-21-12-010-051 B. Get Access (1) Get access to the cabin. (2) Open the FWD and AFT cargo-compartment doors (Ref. TASK 52-30-00-010801). (3) In the cockpit: - Open the floor panel (access hatch) 211FF. (4) Put the WARNING NOTICE in position to tell your personnel about the aircraft disinfection. **ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, Subtask 12-21-12-865-051 C. Get access to the avionics compartment and to the applicable 5000VE-series panel(s). Then open, safety and tag this (these) circuit breaker(s) : ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------715VU GALLEY AFT 12MC A54 715VU GALLEY FWD MID 23MC P56 **ON A/C 210-249, 715VU GALLEY FWD MID AFT 715VU GALLEY FWD MID AFT
112MC 223MC
C55 P57
R
EFF : ALL 12-21-12 SROS
Page 343 Jul 01/06
R
------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------**ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, 717VU GALLEY FWD MID
11MC
B51
717VU GALLEY FWD MID
111MC
C51
24MC
B60
223MC
P57
1MC 2MC
T10 S39 F06 F05 F04 F03 F02 F01 C07 C06 D16 D15
R R 718VU GALLEY AFT **ON A/C 001-049, 201-209, 251-252, 255-299, 401-449, 451-499, 718VU GALLEY FWD MID AFT **ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, 721VU GALLEY SYS 1 722VU GALLEY SYS 2 R R R R R R R R
5001VE 5001VE 5001VE 5001VE 5001VE 5001VE
RAZOR SOCKET RAZOR SOCKET VACUUM CLEANER VACUUM CLEANER VACUUM CLEANER VACUUM CLEANER
Z241 Z222 Z242 Z221
3MT 1MT 3ME 2ME 4ME 1ME
5005VE 5005VE 5005VE 5005VE
RAZOR SOCKET RAZOR SOCKET VACUUM CLEANER SOCKET Z272 VACUUM CLEANER SOCKET Z271
7MT 5MT 6ME 5ME
SOCKET SOCKET SOCKET SOCKET
EFF : 001-049, 201-249, 251-252, 255-299, 12-21-12 401-449, 451-499, SROS
Page 344 Jul 01/06
**ON A/C ALL 4. Procedure _________ WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL MATERIALS _______ ONLY WITH A GOOD FLOW OF AIR THROUGH THE WORK AREA. THESE MATERIALS ARE POISONOUS AND FLAMMABLE AND SKIN IRRITANTS. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL _______ MATERIAL. THIS MATERIAL IS DANGEROUS. R R
WARNING : DO NOT LET DISINFECTANTS GO ONTO FOODSTUFFS. DISINFECTANTS ARE _______ POISONOUS. DO NOT APPLY THEM AS A SPRAY DIRECTLY TO CARPETS OR COCKPIT INSTRUMENT PANELS. DISINFECTANTS CAN CAUSE DAMAGE TO FURNISHINGS AND EQUIPMENT. Subtask 12-21-12-615-050 A. Disinfection of the Aircraft Equipment and Furnishings (1) Cockpit Equipment and Furnishings: NOTE : Do NOT spray the disinfectant directly on cockpit panels. ____ (a) Carefully apply DISINFECTANTS (Material No. 14-006B) to all surfaces of the cockpit equipment and furnishings with a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003). (b) Clean and dry the cockpit equipment and furnishings with and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003). (2) Galleys: (a) Apply DISINFECTANTS (Material No. 14-006B) to the galleys and galley equipment with a GUN - SPRAY. (b) Clean and dry the galleys and the galley equipment with clean water and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003).
EFF : ALL 12-21-12 SROS
Page 345 Jan 01/07
(3) Lavatories: (a) Apply DISINFECTANTS (Material No. 14-006B) to all toilet seats and the lavatory equipment with a GUN - SPRAY. (b) Clean and dry the toilet seats and the lavatory equipment with clean water and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003). (4) Passenger Seating and Crew Rest Areas: (a) Apply DISINFECTANTS (Material No. 14-006B) to the cabin seats and the cabin equipment with a GUN - SPRAY. (b) Clean and dry the cabin equipment with clean water and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003). (5) Cargo Compartments: (a) Apply DISINFECTANTS (Material No. 14-006B) to the cargo compartments with a GUN - SPRAY. (b) Clean and dry the cargo compartments with clean water and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003). 5. Close-up ________ **ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, Subtask 12-21-12-865-052 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1MT, 3MT, 5MT, 7MT, 1ME, 2ME, 3ME, 4ME, 5ME, 6ME, 1MC, 11MC, 111MC, 2MC, 12MC, 112MC, 23MC, 223MC, 24MC
EFF : ALL 12-21-12 R SROS
Page 346 Jul 01/06
R
**ON A/C ALL Subtask 12-21-12-410-051 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the FWD and AFT cargo-compartment doors (Ref. TASK 52-30-00410-801). (3) Close the access hatch 211FF. (4) Remove the warning notice(s).
R R
(5) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-21-12-862-051 C. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
R
EFF : ALL 12-21-12 SROS
Page 347 Jan 01/06
TASK 12-21-12-670-802 Fumigation of the Aircraft Equipment and Furnishing WARNING : ONLY PERSONS NECESSARY FOR THIS PROCEDURE ARE PERMITTED IN THE _______ AIRCRAFT DURING THE TASK. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific
1 WARNING NOTICE
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 14-004 Material No. 19-003
INSECTICIDE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
12-21-12-100-801 12-21-12-100-802 12-21-12-100-804 12-21-12-100-806 12-21-12-100-808 12-33-21-618-801 24-42-00-861-801
Cleaning of the Cockpit Display-Units Cleaning of the Cockpit Equipment/Furnishings Cleaning of the Plastic Surfaces and Mirrors Cleaning of Light Alloy and Steel Components Cleaning of the Monitors and Display Screens in the Cabin Pre-conditioning through the Low-Pressure Ground Connection Energize the Ground Service Network
EFF : ALL 12-21-12 SROS
Page 348 Jan 01/06
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-862-801 52-10-00-010-801 52-10-00-410-801 52-30-00-010-801 52-30-00-410-801
De-energize the Ground Service Network Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door Opening of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Closing of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump
3. __________ Job Set-up Subtask 12-21-12-861-052 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). R R
Subtask 12-21-12-010-052-A B. Get Access
R
(1) Get access to the cabin through one of the passenger/crew doors.
R
NOTE : All other passenger/crew doors must be closed. ____
R R
(2) Open the forward and aft cargo-compartment doors (Ref. TASK 52-30-00010-801).
R R
(3) In the cockpit: - Open the floor panel (access hatch) 211FF.
R R
(4) If necessary remove the cushions and backrests of the cabin seats, the cockpit seats and the cabin attendants seats.
R R R
NOTE : We recommend that you remove all of the cushions and ____ backrests. The insecticide soaks into these materials and extends the ventilation time after fumigation.
R
(5) Open all of the stowages, the lavatory doors and the cockpit door.
R
(6) Remove the contents of the compartments of the galleys.
R
(7) Remove the galley equipment.
EFF : ALL 12-21-12 SROS
Page 349 Jan 01/06
R R
(8) Put the WARNING NOTICE in position to tell your personnel about the aircraft fumigation.
R R R R R R R R R R R R R R R R R R R
NOTE : Fumigation is required for these compartment volumes: ____ -----------------------------------------------------------------------------| | Aircraft Model | | Compartment |-----------------------------------------------------------| | A330/A340-200 | A330/A340-300| A340-500 | A340-600 | -----------------------------------------------------------------------------| Cockpit | 12 m3 | 12 m3 | 12 m3 | 12 m3 | | | (424 ft.3) | (424 ft.3) | (424 ft.3) | (424 ft.3) | -----------------------------------------------------------------------------| Cabin | 317 m3 | 346 m3 | 370 m3 | 420 m3 | | (SEE NOTE) | (11195 ft.3) | (12219 ft.3) | (13066 ft.3) | (14832 ft.3)| -----------------------------------------------------------------------------| Forward Cargo | 92 m3 | 107 m3 | 110.7 m3 | 144 m3 | | | (3249 ft.3) | (3779 ft.3) | (3909 ft.3) | (5085 ft.3) | -----------------------------------------------------------------------------| Aft and Bulk | 94 m3 | 108,4 m3 | 124 m3 | 129 m3 | | Cargo (basic, | (3320 ft.3) | (3828 ft.3) | (3850 ft.3 ) | (4414 ft.3) | | no options) | | | | | ------------------------------------------------------------------------------
R R R
NOTE : Cabin volumes are calculated with the compartment furnishings ____ installed. 109 m3 (3849.299 ft.3)
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, Subtask 12-21-12-865-053
R R R
C. Get access to the avionics compartment and to the applicable 5000VE-series panel(s). Then open, safety and tag this (these) circuit breaker(s) : ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION -------------------------------------------------------------------------------
R 715VU GALLEY AFT 715VU GALLEY FWD MID R
12MC 23MC
A54 P56
112MC
C55
**ON A/C 210-249, 715VU GALLEY FWD MID AFT
EFF : ALL 12-21-12 SROS
Page 350 Jan 01/06
------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------715VU GALLEY FWD MID AFT 223MC P57 R R
**ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, 717VU GALLEY FWD MID
11MC
B51
717VU GALLEY FWD MID
111MC
C51
24MC
B60
223MC
P57
1MC 2MC
T10 S39 F06 F05 F04 F03 F02 F01 C07 C06 D16 D15
R R 718VU GALLEY AFT **ON A/C 001-049, 201-209, 251-252, 255-299, 401-449, 451-499, 718VU GALLEY FWD MID AFT **ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, 721VU GALLEY SYS 1 722VU GALLEY SYS 2 R R R R R R R R
5001VE 5001VE 5001VE 5001VE 5001VE 5001VE
RAZOR SOCKET RAZOR SOCKET VACUUM CLEANER VACUUM CLEANER VACUUM CLEANER VACUUM CLEANER
Z241 Z222 Z242 Z221
3MT 1MT 3ME 2ME 4ME 1ME
5005VE 5005VE 5005VE 5005VE
RAZOR SOCKET RAZOR SOCKET VACUUM CLEANER SOCKET Z272 VACUUM CLEANER SOCKET Z271
7MT 5MT 6ME 5ME
SOCKET SOCKET SOCKET SOCKET
EFF : 001-049, 201-249, 251-252, 255-299, 12-21-12 401-449, 451-499, SROS
Page 351 Jul 01/06
**ON A/C 301-399, 701-749, Subtask 12-21-12-865-062 D. Get access to the avionics compartment and to the applicable 5000VE-series panel(s). Then open, safety and tag this (these) circuit breaker(s) : ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------R 710VU GALLEY FWD MID AFT
223MC
P57
715VU GALLEY FWD MID AFT
112MC
C55
12MC 11MC 111MC 23MC 24MC 1MC 2MC 3ME 2ME 4ME 1LQ 1ME 6ME 5ME
A54 B51 C51 P56 B60 T10 S39 F04 F03 F02 F01 F01 D16 D15
11LQ
D08
11LQ
D08
R R
R R R R R R R
717VU 717VU 717VU 717VU 718VU 721VU 722VU 5001VE 5001VE 5001VE 5001VE 5001VE 5005VE 5005VE
GALLEY AFT GALLEY FWD MID GALLEY FWD MID GALLEY FWD MID GALLEY AFT GALLEY SYS 1 GALLEY SYS 2 VACUUM CLEANER SOCKET Z241 VACUUM CLEANER SOCKET Z222 VACUUM CLEANER SOCKET Z242 LAV FWD&MID DOOR 2 LIGHT VACUUM CLEANER SOCKET Z221 VACUUM CLEANER SOCKET Z272 VACUUM CLEANER SOCKET Z271
R
**ON A/C 301-399,
R
5005VE LIGHT LAV AFT & LOWER
R
**ON A/C 701-749,
R
5005VE LIGHT LAV AFT & MID
R EFF : 301-399, 701-749, 12-21-12 SROS
Page 352 Jul 01/06
**ON A/C ALL 4. Procedure _________ Subtask 12-21-12-615-051 A. Fumigation of the Aircraft WARNING : ONLY PERSONS NECESSARY FOR THIS PROCEDURE ARE PERMITTED IN THE _______ AIRCRAFT DURING THE TASK. WARNING : USE THE CORRECT BREATHING EQUIPMENT. THE GAS IS POISONOUS. _______ WARNING : ALWAYS PUT ON RUBBER GLOVES, GOGGLES AND PROTECTIVE CLOTHES TO _______ PREVENT INFECTION WHEN YOU DO THIS WORK. WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL _______ MATERIAL. THIS MATERIAL IS DANGEROUS. R R
WARNING : DO NOT LET DISINFECTANTS GO ONTO FOODSTUFFS. DISINFECTANTS ARE _______ POISONOUS. DO NOT APPLY THEM AS A SPRAY DIRECTLY TO CARPETS OR COCKPIT INSTRUMENT PANELS. DISINFECTANTS CAN CAUSE DAMAGE TO FURNISHINGS AND EQUIPMENT. (1) Fumigate the Cockpit and the Cabin Area (a) Apply DISINFECTANTS (Material No. 14-004) or equivalent to the: - Floor area of the cockpit - Floor of the galleys and the lavatories - Floor adjacent to the galleys and lavatories - Cabin area. (b) Dry all wet surfaces and covers immediately with a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003). (c) Close the forward passenger/crew door (Ref. TASK 52-10-00-410801). (2) Fumigate the Cargo Compartments (a) Apply DISINFECTANTS (Material No. 14-004) or equivalent to the cargo compartments. (b) Close the forward and aft cargo-compartment doors (Ref. TASK 5230-00-410-801).
EFF : ALL 12-21-12 SROS
Page 353 Jan 01/07
(c) Keep the aircraft doors closed for 45 minutes. (3) Do the ground air pre-conditioning for 1 hour to remove the insecticide from the cabin and cockpit (Ref. TASK 12-33-21-618-801). (4) Open all of the passenger/crew doors (Ref. TASK 52-10-00-010-801) and the forward and aft cargo-compartment doors (Ref. TASK 52-30-00-010801). (5) Let all doors stay open for 5 hours before you go into the aircraft. (6) Clean all the surfaces of the cockpit and the cabin: - The cockpit display units (Ref. TASK 12-21-12-100-801) - The cockpit equipment and furnishings (Ref. TASK 12-21-12-100-802) - The plastic surfaces and mirrors (Ref. TASK 12-21-12-100-804) - The light alloy and steel components (Ref. TASK 12-21-12-100-806) - The monitors and display screens in the cabin (Ref. TASK 12-21-12-100-808). 5. Close-up ________ Subtask 12-21-12-865-054 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1MT, 3MT, 5MT, 7MT, 1ME, 2ME, 3ME, 4ME, 5ME, 6ME, 1MC, 11MC, 111MC, 2MC, 12MC, 112MC, 23MC, 223MC, 24MC **ON A/C 301-399, 701-749, Subtask 12-21-12-865-063 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1LQ, 11LQ, 1ME, 2ME, 3ME, 4ME, 5ME, 6ME, 1MC, 11MC, 111MC, 2MC, 12MC, 112MC, 23MC, 223MC, 24MC
EFF : ALL 12-21-12 R SROS
Page 354 Jul 01/06
**ON A/C ALL Subtask 12-21-12-410-052 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the forward and aft cargo-compartment doors (Ref. TASK 52-3000-410-801). (3) Close the access hatch 211FF. (4) Remove the warning notice(s). (5) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-21-12-862-052 D. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-21-12 R SROS
Page 355 Jul 01/06
TASK 12-21-12-670-804 R
Fumigation of the Fuselage Pressurized Areas with Carbon-Dioxide (CO2 Gas) 1. __________________ Reason for the Job Refer to the SIL 12-007 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific No specific No specific No specific No specific No specific No specific FOR FIN 8DG2 No specific FOR FIN 315HL No specific
1 3 1 2 1 1 2
CHARGING EQUIPMENT - GAS, STANDARD DETECTOR ACT8800 - GRAS HOSE - RUBBER LOCALLY MANUFACTURED - ADAPTER SAFETY BARRIER SUPPLY LINE - GAS, PRESSURIZED WARNING NOTICE
1 ACCESS PLATFORM 5M (16 FT) 1 ACCESS PLATFORM 2M (6 FT)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------No specific Material No. 08-074
cable ties MASKING TAPE (Ref. 20-31-00)
Material No. 14-009 C02 GAS (Ref. 20-31-00)
EFF : ALL 12-21-12 SROS
Page 356 Jan 01/06
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------08-21-00-200-801 12-33-21-618-801
R
21-31-00-710-802 24-42-00-861-801 24-42-00-862-801 25-25-11-000-801 25-25-11-400-801 52-10-00-010-801 52-10-00-410-801 52-30-00-010-801 52-30-00-010-803 52-30-00-410-801
R R
52-30-00-410-803 53-00-00-991-013 AMM AMM
Quick Leveling Procedures Pre-conditioning through the Low-Pressure Ground Connection Operational Test of the Manual Mode Energize the Ground Service Network De-energize the Ground Service Network Removal of a Filler Panel Installation of a Filler Panel Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door Opening of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Opening of the BULK Cargo-Compartment Door Closing of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Closing of the BULK Cargo-Compartment Door Piston Drain Valves of the Lower Fuselage and Bilge Area
30-71-00 52-41-00
R AMM 56-12-00 SIL 12-007 12-21-12-991-009 12-21-12-991-001
Fig. 306 Fig. 307
R 3. __________ Job Set-up Subtask 12-21-12-941-050 A. Safety Precautions WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL _______ MATERIAL. THIS MATERIAL IS DANGEROUS. (1) Make sure that there is sufficient airflow around the aircraft. (2) Do this task on the apron.
EFF : ALL 12-21-12 SROS
Page 357 Jan 01/06
(3) If you do the task in the hangar: (a) Open the doors of the hangar. R
(b) Put SAFETY BARRIER in position to keep all persons out of the work area. (c) Put the WARNING NOTICE in position to tell your personnel about the aircraft fumigation.
R R
(d) If you do the task in a hangar which has under-floor areas, make sure that they are sealed.
R
NOTE : This carbon-dioxide gas (CO2 gas) is heavier than air. ____ Subtask 12-21-12-010-055 B. Get Access
R R
(1) Put the access platforms in position. (a) FOR 8DG2 - Put the ACCESS PLATFORM 5M (16 FT) in position at the sliding window 8DG2.
R R
(b) FOR 315HL - Put the ACCESS PLATFORM 2M (6 FT) in position at the outflow valve 315HL.
R
(2) In the cockpit: (a) Open the sliding window 8DG2 (Ref. AMM 56-12-00).
R
(3) In the forward utility area of the cabin: (a) Remove the filler-panels of the center service-channel as necessary to get access to the area above the ceiling (Ref. TASK 25-25-11-000-801).
EFF : ALL 12-21-12 SROS
Page 358 Jan 01/06
Subtask 12-21-12-480-050 C. Installation of the Equipment (Ref. SIL 12-007) (1) Install the sliding window adapter. (Ref. Fig. 306/TASK 12-21-12-991-009) (a) Put the LOCALLY MANUFACTURED - ADAPTER (1) in position in the cockpit window frame and attach it with the screws and the wing nuts. R R
(b) Put the HOSE - RUBBER, min. dia. 150 mm (6.0 in.), (2) through the opening in the center service channel.
R R
(c) Put the upper end of the hose (2) in the highest position in the fuselage and attach it with cable ties. (d) Connect the lower end of the hose (2) to the window adapter. (2) Install the air-outflow valve-adapter. (Ref. Fig. 307/TASK 12-21-12-991-001)
R R
(a) Put the LOCALLY MANUFACTURED - ADAPTER (1) in position on the outflow valve 315HL and attach it with the hooks and the wing nuts. (b) Connect the SUPPLY LINE - GAS, PRESSURIZED of the DISINFECTANTS (Material No. 14-009) CHARGING EQUIPMENT - GAS, STANDARD to the adapter (1). Subtask 12-21-12-869-050 D. Aircraft Maintenance Configuration (1) Close the air outflow valve 313HL (Ref. TASK 21-31-00-710-802). (2) Make sure that the attitude of the aircraft is level or nose-up (Ref. TASK 08-21-00-200-801). (3) Close the passenger/crew door(s) (Ref. TASK 52-10-00-410-801).
R
(4) Close the forward and aft cargo-compartment doors (Ref. TASK 52-3000-410-801). (5) Make sure that the avionics compartment access door Z811 is closed (Ref. AMM 52-41-00).
EFF : ALL 12-21-12 SROS
Page 359 Jan 01/06
Adapter Cockpit Sliding-Window Figure 306/TASK 12-21-12-991-009 EFF : ALL 12-21-12 R SROS
Page 360 Jan 01/06
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Adapter Aft Air-Outflow Valve Figure 307/TASK 12-21-12-991-001
EFF : ALL 12-21-12 SROS
Page 361 Jan 01/06
(6) Make sure that the BULK cargo compartment door is closed (Ref. TASK 52-30-00-410-803). (7) Close the outlet of all: - Fuselage drain valves (Ref. TASK 53-00-00-991-013) and - Waste-water drain masts (Ref. AMM 30-71-00)
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with BONDING AND ADHESIVE COMPOUNDS (Material No. 08-074). 4. Procedure _________ Subtask 12-21-12-614-050 A. Fumigation of the Aircraft (Ref. SIL 12-007) WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL _______ MATERIAL. THIS MATERIAL IS DANGEROUS. WARNING : DO NOT BREATHE THE GAS. CARBON DIOXIDE IS POISONOUS AND CAN _______ KILL YOU. R
WARNING : USE THE CORRECT BREATHING EQUIPMENT. THE GAS IS POISONOUS. _______ WARNING : BEFORE YOU START THE FUMIGATION PROCEDURE, MAKE SURE THAT NO _______ PERSONS ARE IN THE AIRCRAFT. THE FUMIGATION GAS CAN CAUSE DEATH. WARNING : DO NOT OPEN THE DOORS DURING THE PROCEDURE. POISONOUS GAS IS _______ INSIDE THE AIRCRAFT. (1) Put a WARNING NOTICE in position at all doors to tell your personnel not to open them. (2) Operate the gas charging equipment to fill the pressurized area of the fuselage with DISINFECTANTS (Material No. 14-009) (carbon-dioxide). (a) Refer to the following table for the required quantity of CO2 gas.
EFF : ALL 12-21-12 SROS
Page 362 Jan 01/06
-----------------------------------------------------------------------------| | Aircraft Model | -----------------------------------------------------------------------------| | A330/A340-200 | A330/A340-300 | A340-500 | A340-600 | -----------------------------------------------------------------------------| Quantity of | | | | | | CO2 gas | 2300kg | 2500kg | 2700kg | 3000kg | | (carbon-dioxide) | | | | | | | | | | | -----------------------------------------------------------------------------(3) Stop the gas charging equipment when the DETECTOR ACT8800 - GRAS shows that CO2 (carbon-dioxide) flows out of the outlet hose (2). (Ref. Fig. 306/TASK 12-21-12-991-009)
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(4) Keep all doors closed for 12 hours. Subtask 12-21-12-010-056 B. Opening of all Pressure Sealed Doors WARNING : STOP THE OPENING PROCEDURE IF THE RED WARNING LIGHT FLASHES. _______ RESIDUAL PRESSURE COULD CAUSE THE DOOR TO OPEN WITH A SUDDEN FORCE AND INJURE PERSONS AND/OR DAMAGE THE AIRCRAFT. WARNING : DO NOT BREATHE THE GAS. CARBON DIOXIDE IS POISONOUS AND CAN _______ KILL YOU. R
WARNING : USE THE CORRECT BREATHING EQUIPMENT. THE GAS IS POISONOUS. _______ (1) Make sure that there is sufficient airflow around the aircraft.
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(2) Open the forward and aft cargo compartment doors (Ref. TASK 52-30-00010-801). (3) Open the avionics compartment access door Z811 (Ref. AMM 52-41-00). (4) Open the BULK cargo-compartment door (Ref. TASK 52-30-00-010-803). (5) Open all the passenger/crew doors (Ref. TASK 52-10-00-010-801). (6) Open the air-outflow valve 313HL (Ref. TASK 21-31-00-710-802).
EFF : ALL 12-21-12 SROS
Page 363 Jan 01/06
Subtask 12-21-12-080-050 C. Removal of the Equipment (Ref. Fig. 306/TASK 12-21-12-991-009, 307/TASK 12-21-12-991-001) (1) Disconnect the gas charging equipment from the air-outflow valve adapter (1). (2) Remove the outlet tube (2) and the adapters (1). R R R R R
(3) Remove the masking tape (Mat. No. 08-074) from the outlet of the: - waste-water drain masts (Ref. AMM 30-71-00) and - all fuselage drain valves (Ref. TASK 53-00-00-991-013). Subtask 12-21-12-861-066 D. Energize the ground service network (Ref. TASK 24-42-00-861-801) Subtask 12-21-12-618-050 E. Removal of the Remaining CO2 (Carbon-Dioxide) WARNING : DO NOT BREATHE THE GAS. CARBON DIOXIDE IS POISONOUS AND CAN _______ KILL YOU.
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WARNING : USE THE CORRECT BREATHING EQUIPMENT. THE GAS IS POISONOUS. _______ (1) Do the ground air pre-conditioning for a minimum of 30 min to remove the remaining CO2 from all areas (Ref. TASK 12-33-21-618-801). (2) Do a check of the CO2 concentration. (a) Use a DETECTOR ACT8800 - GRAS and examine the aircraft for remaining CO2. (b) Make sure that there is less than 5% Vol. CO2 concentration 0.2 m (0.65 ft.) above the cabin floor level.
EFF : ALL 12-21-12 SROS
Page 364 Jan 01/06
5. Close-up ________ Subtask 12-21-12-410-055 A. Close Access (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items. (2) Remove the warning notice(s). (3) Install the filler-panels of the center service channel in the forward cabin utility area (Ref. TASK 25-25-11-400-801). (4) Close the cockpit sliding window 8DG2 (Ref. AMM 56-12-00). (5) Close all pressure sealed doors. R R
(a) Close the forward and aft cargo compartment doors (Ref. TASK 5230-00-410-801).
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(b) Close the avionics compartment access door (Ref. AMM 52-41-00).
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(c) Close the bulk cargo compartment door (Ref. TASK 52-30-00-410803).
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(d) Close the passenger/crew door(s) (Ref. TASK 52-10-00-410-801). (6) If you did the task in a hangar with under-floor areas: WARNING : DO NOT BREATHE THE GAS. CARBON DIOXIDE IS POISONOUS AND CAN _______ KILL YOU. WARNING : USE THE CORRECT BREATHING EQUIPMENT. THE GAS IS POISONOUS. _______ (a) Carefully open the sealed areas of the hangar and do a check for remaining CO2 concentration with a DETECTOR ACT8800 - GRAS. (b) Make sure that there is less than 5% Vol. CO2 concentration 0.2 m (0.65 ft.) above the floor of the under floor areas of the hangar. Subtask 12-21-12-862-066 B. De-energize the ground service network (Ref. TASK 24-42-00-862-801)
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Page 365 Jan 01/07
INTENTIONALLY BLANK
R 12-21-12 SROS
Page 366 Jan 01/07
TASK 12-21-12-670-805 Special Precautions to Apply Insecticide Agent in Auxiliary Area Compartments and Cargo Compartments, during Turn-Around 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 WARNING NOTICE
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 14-010 INSECTICIDE A/C CABIN (IN FLIGHT) (Ref. 20-31-00) Material No. 14-010A Material No. 14-010B
INSECTICIDE,A/C CABIN (IN FLIGHT) (Ref. 20-31-00) USA AMS 1450 INSECTICIDE,AIRCRAFT (Ref. 20-31-00)
3. __________ Job Set-up Subtask 12-21-12-941-051 A. Preparation (1) Put a WARNING NOTICE in position in the cockpit to tell the flight crew that: - The procedure to apply insecticides in compartments that have smoke detectors is in progress. - Smoke warning(s) caused from the insecticide agent can occur.
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4. Procedure _________ Subtask 12-21-12-670-050 R R
A. Application of the Insecticide Agent
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(1) Apply the insecticide agent: - DISINFECTANTS (Material No. 14-010) or - DISINFECTANTS (Material No. 14-010A) or - DISINFECTANTS (Material No. 14-010B) to the auxiliary area compartments and the cargo compartments as necessary. Subtask 12-21-12-210-050 B. Visual Inspection (1) If a smoke warning occurs during the procedure: (a) Do a visual inspection of the related compartment to make sure that there is no smoke. (b) If the insecticide agent caused the warning: - The warning will stop automatically after 3 minutes. Subtask 12-21-12-865-059 C. Put the Aircraft back to its Initial Configuration (1) If a smoke warning has occurred: (a) Start the ventilation controller 280HN again to get the normal ventilation of the affected compartment(s). - In the cockpit on the overhead RESET panel 262VU: pull the C/Bs - VENT CONT LANE 1 and - VENT CONT LANE 2 at the same time for a minimum of 5 seconds but less than 10 seconds.
EFF : ALL 12-21-12 SROS
Page 368 Jan 01/06
NOTE : The CBs must be closed in less than 10 seconds to avoid ____ the automatic shut-down of the IFE system. **ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, Subtask 12-21-12-710-050 D. Test of the Ventilation of the Auxiliary Areas (Crew-Rest) Compartment(s). (1) In the related crew-rest compartment(s): - Make sure that the ventilation and heating system operates correctly. **ON A/C ALL 5. Close-up ________ Subtask 12-21-12-942-055 A. Close Access (1) Remove the warning notice(s).
EFF : ALL 12-21-12 SROS
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DUST REMOVAL - CLEANING/PAINTING ________________________________ TASK 12-21-13-100-801 Dust Removal 1. __________________ Reason for the Job To remove the dust from the avionics compartment and from the center pedestal 100VU in the cockpit. R
NOTE : This task can contribute to fuel savings. ____ 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
soft brush vacuum cleaner access platform 2.5 m (8 ft. 2 in.)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 19-003
USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
EFF : ALL 12-21-13 SROS
Page 701 Jan 01/07
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------21-28-34-000-801 21-28-34-400-801 21-31-34-000-801 21-31-34-400-801
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21-53-34-000-801 21-53-34-400-801 21-63-34-000-801 21-63-34-400-801 22-82-12-000-801 22-82-12-400-801 22-83-34-000-802 22-83-34-400-802 23-11-33-000-801 23-11-33-400-801 23-12-33-000-801 23-12-33-400-801 23-24-34-000-801 23-24-34-400-801 23-51-12-000-801 23-51-12-400-801 23-51-34-000-801 23-51-34-400-801 23-73-34-000-801 23-73-34-400-801 23-81-13-000-801 23-81-13-400-801 24-41-34-000-801 24-41-34-400-801 24-42-00-861-801 24-42-00-862-801 26-16-34-000-801 26-16-34-400-801
Removal of the Ventilation Controller (280HN) Installation of the Ventilation Controller (280HN) Removal of the Cabin Pressure Controller (311HL,312HL) Installation of the Cabin Pressure Controller (311HL,312HL) Removal of the Pack Controller (531HH, 532HH) Installation of the Pack Controller (531HH, 532HH) Removal of the Zone Controller (630HK) Installation of the Zone Controller (630HK) Removal of the MCDU (2CA1,2CA2,2CA3) Installation of the MCDU (2CA1,2CA2,2CA3) Removal of the FMGEC (1CA1,1CA2) Installation of the FMGEC (1CA1,1CA2) Removal of the HF Transceiver (1RE1) Installation of the HF Transceiver (1RE1) Removal of the VHF Transceiver (1RC1,1RC2,1RC3) Installation of the VHF Transceiver (1RC1,1RC2,1RC3) Removal of the ACARS Management Unit (or ACARS Communications Management Unit (1RB1) Installation of the ACARS Management Unit (or ACARS Communications Management Unit (1RB1) Removal of the Audio Control Panel Installation of the Audio Control Panel Removal of the Audio Management Unit (1RN) Installation of the Audio Management Unit (1RN) Removal of the CIDS Director (101RH,102RH) Installation of the CIDS Director (101RH,102RH) Removal of the Radio Management Panel (1RG1,1RG2,1RG3) Installation of the Radio Management Panel (1RG1,1RG2,1RG3) Removal of the Ground Power Control Unit (GPCU) (1XG) Installation of the Ground Power Control Unit (GPCU) (1XG) Energize the Ground Service Network De-energize the Ground Service Network Removal of the Smoke Detection Control-Unit (SDCU) (20WH) Installation of the Smoke Detection Control-Unit (SDCU) (20WH)
EFF : ALL 12-21-13 SROS
Page 702 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------27-51-34-000-801 27-51-34-400-801 27-92-14-000-801 27-92-14-400-801 27-93-34-000-801 27-93-34-400-801 27-94-34-000-801 27-94-34-400-801 27-95-34-000-801 27-95-34-400-801 28-51-34-000-801 28-51-34-400-801 29-11-34-000-801 29-11-34-400-801 31-33-34-000-801 31-33-34-400-803 31-33-52-000-801 31-33-52-400-801 31-36-34-000-801 31-36-34-400-801 31-36-52-000-801 31-36-52-400-801 31-53-34-000-801 31-53-34-400-801 31-55-34-000-801 31-55-34-400-801 31-62-34-000-801 31-62-34-400-801 32-31-71-000-801 32-31-71-400-801
Removal of the Slat and Flap Control Computer (SFCC) (21CV,22CV) Installation of the Slat and Flap Control Computer (SFCC) (21CV,22CV) Removal of the Speedbrake Control-Lever Assy (20CE) Installation of the Speedbrake Control-Lever Assy (20CE) Removal of the Flight Control Primary Computer (FCPC) (2CE1,2CE2,2CE3) Installation of the Flight Control Primary Computer (FCPC) (2CE1,2CE2,2CE3) Removal of the Flight Control Secondary Computer (FCSC) (3CE1,3CE2) Installation of the Flight Control Secondary Computer (FCSC) (3CE1,3CE2) Removal of the Flight Control Data Concentrator (FCDC) (1CE1,1CE2) Installation of the Flight Control Data Concentrator (FCDC) (1CE1,1CE2) Removal of the Fuel Control and Monitoring Computer (FCMC) (5QM1,5QM2) Installation of the Fuel Control and Monitoring Computer (FCMC) (5QM1,5QM2) Removal of the HSMU (1JG) Installation of the HSMU (1JG) Removal of the FDIU (2TU) Installation of the FDIU (2TU) Removal of the Quick Access Recorder (QAR)(3TU) Installation of the Quick Access Recorder (QAR)(3TU) Removal of the Data Management Unit (DMU)(1TV) Installation of the Data Management Unit (DMU)(1TV) Removal of the Digital ACMS Recorder (DAR)(2TV) Installation of the Digital ACMS Recorder (DAR)(2TV) Removal of the FWC (1WW1,1WW2) Installation of the FWC (1WW1,1WW2) Removal of the SDAC (1WV1,1WV2) Installation of the SDAC (1WV1,1WV2) Removal of the Display Management Computer (DMC)(1WT1, 1WT2, 1WT3) Installation of the Display Management Computer (DMC)(1WT1, 1WT2, 1WT3) Removal of the LGCIU (5GA1,5GA2) Installation of the LGCIU (5GA1,5GA2)
EFF : ALL 12-21-13 R SROS
Page 703 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-42-34-000-801 32-42-34-400-801 32-49-34-000-801 32-49-34-400-801 34-12-34-000-801 34-12-34-400-801 R R R
34-36-31-000-801 34-36-31-000-802 34-36-31-400-801 34-36-31-400-802 34-41-12-000-801 34-41-12-400-801 34-41-33-000-801 34-41-33-400-801 34-43-34-000-801 34-43-34-400-801 34-48-34-000-801 34-48-34-400-801 34-51-33-000-801 34-51-33-400-801 34-52-12-000-801 34-52-12-400-801 34-52-33-000-801 34-52-33-400-801 34-53-31-000-801 34-53-31-400-801 34-55-31-000-801 34-55-31-400-801 36-11-34-000-801 36-11-34-400-801 45-13-34-000-801 45-13-34-400-801
Removal of the BSCU (3GG) Installation of the BSCU (3GG) Removal of the TPIC (2GV) Installation of the TPIC (2GV) Removal of the Air Data/Inertial Reference Unit (ADIRU) (1FP1, 1FP2, 1FP3) Installation of the Air Data/Inertial Reference Unit (ADIRU) (1FP1, 1FP2, 1FP3) Removal of the ILS Receiver (1RT1,1RT2) Removal of the Multi Mode Receiver (40RT1, 40RT2) Installation of the ILS Receiver (1RT1,1RT2) Installation of the Multi Mode Receiver (40RT1, 40RT2) Removal of the Weather Radar Control Unit (3SQ) Installation of the Weather Radar Control Unit (3SQ) Removal of the Weather Radar Transceiver (1SQ1, 1SQ2) Installation of the Weather Radar Transceiver (1SQ1, 1SQ2) Removal of the TCAS Computer (1SG) Installation of the TCAS Computer (1SG) Removal of the Ground Proximity Warning Computer (GPWC) (1WZ) Installation of the Ground Proximity Warning Computer (GPWC) (1WZ) Removal of the DME Interrogator (1SD1, 1SD2) Installation of the DME Interrogator (1SD1, 1SD2) Removal of the ATC/TCAS Control Unit (2SH) Installation of the ATC/TCAS Control Unit (2SH) Removal of the ATC/Mode S Transponder (1SH1, 1SH2) Installation of the ATC/Mode S Transponder (1SH1, 1SH2) Removal of the ADF Receiver (1RP1, 1RP2) Installation of the ADF Receiver (1RP1, 1RP2) Removal of the VOR/MKR Receiver (1RS1, 1RS2) Installation of the VOR/MKR Receiver (1RS1, 1RS2) Removal of the Bleed Monitoring Computer (BMC) (1HA1, 1HA2, 1HA3, 1HA4) Installation of the Bleed Monitoring Computer (BMC) (1HA1, 1HA2, 1HA3, 1HA4) Removal of the Central Maintenance Computer (CMC) (1TM1,1TM2) Installation of the Central Maintenance Computer (CMC) (1TM1,1TM2)
EFF : ALL 12-21-13 SROS
Page 704 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R
45-41-22-000-801 45-41-22-400-801 46-21-34-000-801 46-21-34-400-801 52-71-34-000-801 52-71-34-400-801 73-25-34-000-801
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73-25-34-000-802 73-25-34-000-803 73-25-34-000-804 73-25-34-000-805 73-25-34-400-801
R R R R R R
73-25-34-400-802 73-25-34-400-803 73-25-34-400-804 12-21-13-991-001 12-21-13-991-002
Removal of the Printer (2TP) Installation of the Printer (2TP) Removal of the Air Traffic Service Unit (ATSU) (1TX1) Installation of the Air Traffic Service Unit (ATSU) (1TX1) Removal of the Proximity Switch Control Unit (5MJ). Installation of the Proximity Switch Control Unit (5MJ). Removal of the EIVMU (Engine Interface Vibration Monitoring Unit) (1KS1,1KS2,1KS3,1KS4) Removal of the EIVMU (Engine Interface Vibration Monitoring Unit) (1KS1,1KS2) Removal of the EIVMU (Engine Interface Vibration Monitoring Unit) (1KS1,1KS2). Removal of the EIVMU (Engine Interface and Vibration Monitoring Unit) (1KS1, 1KS2) Removal of the EIVMU (Engine Interface and Vibration Monitoring Unit) (1KS1,1KS2,1KS3,1KS4) Installation of the EIVMU (Engine Interface Vibration Monitoring Unit) (1KS1,1KS2,1KS3,1KS4) Installation of the EIVMU (Engine Interface Vibration Monitoring Unit) (1KS1,1KS2) Installation of the EIVMU (Engine Interface Vibration Monitoring Unit). (1KS1,1KS2). Installation of the EIVMU (Engine Interface and Vibration Monitoring Unit) (1KS1, 1KS2) Fig. 701 Fig. 702
3. __________ Job Set-up Subtask 12-21-13-861-050 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-21-13-010-050 B. Get Access (1) Put the access platform in position at the access door 811. (2) Open the access door 811.
EFF : ALL 12-21-13 SROS
Page 705 Jan 01/07
(3) Removal of the units from the cockpit. (Ref. Fig. 701/TASK 12-21-13-991-001) (a) On the center pedestal 100VU: - remove the MCDU (2CA1, 2CA2, 2CA3) (Ref. TASK 22-82-12-000801), - remove the radio management panel (1RG1, 1RG2) (Ref. TASK 2381-13-000-801), - remove the audio control panel (2RN1, 2RN2) (Ref. TASK 23-5112-000-801), - remove the weather radar control unit (3SQ) (Ref. TASK 34-4112-000-801), - remove the ATC/TCAS control unit (2SH) (Ref. TASK 34-52-12-000801), - remove the speedbrake control-lever assy (20CE) (Ref. TASK 2792-14-000-801), - remove the printer (2TP) (Ref. TASK 45-41-22-000-801). - remove the air traffic service unit (1TX1) (Ref. TASK 46-21-34000-801).
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(4) Removal of the computers from the avionics compartment. (Ref. Fig. 702/TASK 12-21-13-991-002) (a) On the shelf - remove the - remove the 000-801), - remove the - remove the - remove the 801), - remove the 801), - remove the
811VU: HF transceiver (1RE1) (Ref. TASK 23-11-33-000-801), ATC/Mode S transponder (1SH1) (Ref. TASK 34-52-33-
(b) On the shelf - remove the - remove the 801), - remove the - remove the 801), - remove the 801), - remove the 000-801), - remove the
812VU: ADF receiver (1RP2) (Ref. TASK 34-53-31-000-801), audio management unit (1RN) (Ref. TASK 23-51-34-000-
TCAS computer (1SG) (Ref. TASK 34-43-34-000-801), VHF transceiver (1RC1) (Ref. TASK 23-12-33-000-801), DME interrogator (1SD1) (Ref. TASK 34-51-33-000VOR/MKR receiver (1RS1) (Ref. TASK 34-55-31-000ADF receiver (1RP1) (Ref. TASK 34-53-31-000-801).
VHF transceiver (1RC2) (Ref. TASK 23-12-33-000-801), DME interrogator (1SD2) (Ref. TASK 34-51-33-000VOR/MKR receiver (1RS2) (Ref. TASK 34-55-31-000ATC/Mode S transponder (1SH2) (Ref. TASK 34-52-33HF transceiver (1RE2) (Ref. TASK 23-11-33-000-801).
EFF : ALL 12-21-13 SROS
Page 706 Jan 01/07
Location of Units in the Cockpit (Center Pedestal 100VU) Figure 701/TASK 12-21-13-991-001 EFF : ALL 12-21-13 R SROS
Page 707 Jan 01/07
Location of Shelves and Computers in the Avionics Compartment Figure 702/TASK 12-21-13-991-002 EFF : ALL 12-21-13 R SROS
Page 708 Jan 01/07
(c) On the shelf - remove the - remove the 000-801), - remove the
821VU: VHF transceiver (1RC3) (Ref. TASK 23-12-33-000-801), ACARS management unit (1RB1) (Ref. TASK 23-24-34CIDS director (101RH) (Ref. TASK 23-73-34-000-801).
(d) On the shelf 822VU: - remove the CIDS director (102RH) (Ref. TASK 23-73-34-000-801). (e) On the shelf 831VU: - remove the EIVMU (Engine Interface Vibration Monitoring Unit (1KS1) (Ref. TASK 73-25-34-000-801) , (Ref. TASK 73-25-34-000802), (Ref. TASK 73-25-34-000-803), (Ref. TASK 73-25-34-000804), - remove the Fuel Control and Monitoring Computer (FCMC) (5QM1) (Ref. TASK 28-51-34-000-801), - remove the Display Management Computer (DMC) (1WT1) (Ref. TASK 31-62-34-000-801), - remove the FWC (1WW1) (Ref. TASK 31-53-34-000-801), - remove the SDAC (1WV1) (Ref. TASK 31-55-34-000-801).
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(f) On the shelf 832VU: - remove the EIVMU (Engine Interface Vibration Monitoring Unit) (1KS2) (Ref. TASK 73-25-34-000-801) , (Ref. TASK 73-25-34-000802), (Ref. TASK 73-25-34-000-803), (Ref. TASK 73-25-34-000804), (Ref. TASK 73-25-34-000-805), - remove the Fuel Control and Monitoring Computer (FCMC) (5QM2) (Ref. TASK 28-51-34-000-801), - remove the Display Management Computer (DMC) (1WT2) (Ref. TASK 31-62-34-000-801), - remove the FWC (1WW2) (Ref. TASK 31-53-34-000-801), - remove the SDAC (1WV2) (Ref. TASK 31-55-34-000-801).
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(g) On the shelf 841VU: - remove the FMGEC (1CA1) (Ref. TASK 22-83-34-000-802), - remove the Slat and Flap Control Computer (SFCC) (21CV) (Ref. TASK 27-51-34-000-801), - remove the Display Management Computer (DMC) (1WT3) (Ref. TASK 31-62-34-000-801), - remove the HSMU (1JG) (Ref. TASK 29-11-34-000-801), - remove the Flight Control Data Concentrator (FCDC) (1CE1) (Ref. TASK 27-95-34-000-801), - remove the Flight Control Primary Computer (FCPC) (2CE3) (Ref. TASK 27-93-34-000-801).
EFF : ALL 12-21-13 SROS
Page 709 Jan 01/07
(h) On the shelf - remove the - remove the (Ref. TASK - remove the (Ref. TASK - remove the (Ref. TASK - remove the (Ref. TASK
842VU: FMGEC (1CA2) (Ref. TASK 22-83-34-000-802), Slat and Flap Control Computer (SFCC) (22CV) 27-51-34-000-801), Flight Control Data Concentrator (FCDC) (1CE2) 27-95-34-000-801), Flight Control Secondary Computer (FCSC) (3CE2) 27-94-34-000-801), Flight Control Primary Computer (FCPC) (2CE2) 27-93-34-000-801).
(i) On the shelf 851VU: - remove the Ground Proximity Warning Computer (GPWC) (1WZ) (Ref. TASK 34-48-34-000-801), - remove the zone controller (630HK) (Ref. TASK 21-63-34-000801), - remove the cabin pressure controller (311HL) (Ref. TASK 21-3134-000-801), - remove the pack controller (531HH) (Ref. TASK 21-53-34-000801), - remove the Bleed Monitoring Computer (BMC) (1HA1) (Ref. TASK 36-11-34-000-801), - remove the BSCU (3GG) (Ref. TASK 32-42-34-000-801), - remove the LGCIU (5GA1) (Ref. TASK 32-31-71-000-801). (j) On the shelf 852VU: - remove the ventilation controller (280HN) (Ref. TASK 21-28-34000-801), - remove the cabin pressure controller (312HL) (Ref. TASK 21-3134-000-801), - remove the Bleed Monitoring Computer (BMC) (1HA2) (Ref. TASK 36-11-34-000-801), - remove the pack controller (532HH) (Ref. TASK 21-53-34-000801), - remove the Ground Power Control Unit (GPCU) (1XG) (Ref. TASK 24-41-34-000-801), - remove the TPIC (2GV) (Ref. TASK 32-49-34-000-801), - remove the Smoke Detection Control-Unit (SDCU) (20WH) (Ref. TASK 26-16-34-000-801), - remove the LGCIU (5GA2) (Ref. TASK 32-31-71-000-801). (k) On the shelf 861VU: - remove the Central Maintenance Computer (CMC) (1TM1) (Ref. TASK 45-13-34-000-801).
EFF : ALL 12-21-13 R SROS
Page 710 Jan 01/07
(l) On the shelf 862VU: - remove the proximity switch control unit (5MJ) (Ref. TASK 5271-34-000-801), - remove the FDIU (2TU) (Ref. TASK 31-33-34-000-801), - Remove the Quick Access Recorder (QAR) (3TU) (Ref. TASK 31-3352-000-801), - remove the Digital ACMS Recorder (DAR) (2TV) (Ref. TASK 31-3652-000-801), - remove the Data Management Unit (DMU) (1TV) (Ref. TASK 31-3634-000-801), - remove the Central Maintenance Computer (CMC) (1TM2) (Ref. TASK 45-13-34-000-801), (m) On the shelf 872VU: - remove the Air Data/Inertial Reference Unit (ADIRU) (1FP1, 1FP2) (Ref. TASK 34-12-34-000-801). (n) Remove the Air Data/Inertial Reference Unit (ADIRU) (1FP3) (Ref. TASK 34-12-34-000-801). (o) On the mounting tray 5SQ: - remove the weather radar transceiver (1SQ1, 1SQ2) (Ref. TASK 34-41-33-000-801). (p) On the shelf - remove the (Ref. TASK - remove the (Ref. TASK - remove the (Ref. TASK - remove the (Ref. TASK
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915VU: ILS receiver (1RT1) (Ref. TASK 34-36-31-000-801), 34-36-31-000-802). Flight Control Secondary Computer (FCSC) (3CE1) 27-94-34-000-801), Flight Control Primary Computer (FCPC) (2CE1) 27-93-34-000-801), ILS receiver (1RT2) (Ref. TASK 34-36-31-000-801), 34-36-31-000-802).
(q) On the shelves 811VU, 812VU, 821VU, 822VU, 831VU, 832VU, 841VU, 842VU, 851VU, 852VU, 861VU, 862VU, 915VU: (Ref. Fig. 702/TASK 12-21-13-991-002) - remove the rack assy.
EFF : ALL 12-21-13 SROS
Page 711 Jan 01/07
4. Procedure _________ (Ref. Fig. 701/TASK 12-21-13-991-001, 702/TASK 12-21-13-991-002) Subtask 12-21-13-160-050 A. Cleaning of the Avionics Compartment and of the Cockpit (1) Use a vacuum cleaner and a soft brush or a MISCELLANEOUS (Material No. 19-003) and clean: (a) the area where the units and computers were installed, (b) the area of the rack assy. (c) all the faces of the removed units and computers, (d) the avionics compartment, (e) the ducts, (f) the shelves. NOTE : Keep the vacuum cleaner out of the avionics compartment to ____ prevent new dust contamination in the avionics compartment. 5. Close-up ________ Subtask 12-21-13-410-050 A. Close Access (1) Installation of the units in the cockpit. (Ref. Fig. 701/TASK 12-21-13-991-001) NOTE : For computers with loadable software, software loading is not ____ necessary if you install the computer removed for access. (a) On the center pedestal 100VU: - install the MCDU (2CA1, 2CA2, 2CA3) (Ref. TASK 22-82-12-400801), - install the radio management panel (1RG1, 1RG2) (Ref. TASK 2381-13-400-801), - install the audio control panel (2RN1, 2RN2) (Ref. TASK 23-5112-400-801),
EFF : ALL 12-21-13 R SROS
Page 712 Jan 01/07
- install the weather radar control unit (3SQ) (Ref. TASK 34-4112-400-801), - install the ATC/TCAS control unit (2SH) (Ref. TASK 34-52-12400-801), - install the speedbrake control lever assy (20CE) (Ref. TASK 2792-14-400-801), - install the printer (2TP) (Ref. TASK 45-41-22-400-801), (Ref. TASK 46-21-34-400-801).
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(2) Installation of the computers in the avionics compartment. (Ref. Fig. 702/TASK 12-21-13-991-002) NOTE : For computers with loadable software, software loading is not ____ necessary if you install the computer removed for access. (a) On the shelves 811VU, 812VU, 821VU, 822VU, 831VU, 832VU, 841VU, 842VU, 851VU, 852VU, 861VU, 862VU, 915VU: (Ref. Fig. 702/TASK 12-21-13-991-002) - install the rack assy. (b) On the shelf 811VU: - install the HF transceiver (1RE1) (Ref. TASK 23-11-33-400-801), - install the ATC/Mode S transponder (1SH1) (Ref. TASK 34-52-33400-801), - install the TCAS computer (1SG) (Ref. TASK 34-43-34-400-801), - install the VHF transceiver (1RC1) (Ref. TASK 23-12-33-400801), - install the DME interrogator (1SD1) (Ref. TASK 34-51-33-400801), - install the VOR/MKR receiver (1RS1) (Ref. TASK 34-55-31-400801), - install the ADF receiver (1RP1) (Ref. TASK 34-53-31-400-801). (c) On the shelf 812VU: - install the ADF receiver (1RP2) (Ref. TASK 34-53-31-400-801), - install the audio management unit (1RN) (Ref. TASK 23-51-34400-801), - install the VHF transceiver (1RC2) (Ref. TASK 23-12-33-400801), - install the DME interrogator (1SD2) (Ref. TASK 34-51-33-400801), - install the VOR/MKR receiver (1RS2) (Ref. TASK 34-55-31-400801), - install the ATC/Mode S transponder (1SH2) (Ref. TASK 34-52-33400-801), - install the HF transceiver (1RE2) (Ref. TASK 23-11-33-400-801).
EFF : ALL 12-21-13 SROS
Page 713 Jan 01/07
(d) On the shelf 821VU: - install the VHF transceiver (1RC3) (Ref. TASK 23-12-33-400801), - install the ACARS management unit (1RB1) (Ref. TASK 23-24-34400-801), - install the CIDS director (101RH) (Ref. TASK 23-73-34-400-801). (e) On the shelf 822VU: - install the CIDS director (102RH) (Ref. TASK 23-73-34-400-801). (f) On the shelf 831VU: - install the EIVMU (Engine Interface Vibration Monitoring Unit) (1KS1) (Ref. TASK 73-25-34-400-801) , (Ref. TASK 73-25-34-400802), (Ref. TASK 73-25-34-400-803), (Ref. TASK 73-25-34-400804), - install the Fuel Control and Monitoring Computer (FCMC) (5QM1) (Ref. TASK 28-51-34-400-801), - install the Display Management Computer (DMC) (1WT1) (Ref. TASK 31-62-34-400-801), - install the FWC (1WW1) (Ref. TASK 31-53-34-400-801), - install the SDAC (1WV1) (Ref. TASK 31-55-34-400-801).
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(g) On the shelf 832VU: - install the EIVMU (Engine Interface Vibration Monitoring Unit) (1KS2) (Ref. TASK 73-25-34-400-801) , (Ref. TASK 73-25-34-400802), (Ref. TASK 73-25-34-400-803), (Ref. TASK 73-25-34-400804), - install the Fuel Control and Monitoring Computer (FCMC) (5QM2) (Ref. TASK 28-51-34-400-801), - install the Display Management Computer (DMC) (1WT2) (Ref. TASK 31-62-34-400-801), - install the FWC (1WW2) (Ref. TASK 31-53-34-400-801), - install the SDAC (1WV2) (Ref. TASK 31-55-34-400-801).
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(h) On the shelf 841VU: - install the FMGEC (1CA1) (Ref. TASK 22-83-34-400-802), - install the Slat and Flap Control Computer (SFCC) (21CV) (Ref. TASK 27-51-34-400-801), - install the Display Management Computer (DMC) (1WT3) (Ref. TASK 31-62-34-400-801), - install the HSMU (1JG) (Ref. TASK 29-11-34-400-801), - install the Flight Control Data Concentrator (FCDC) (1CE1) (Ref. TASK 27-95-34-400-801), - install the Flight Control Primary Computer (FCPC) (2CE3) (Ref. TASK 27-93-34-400-801).
EFF : ALL 12-21-13 SROS
Page 714 Jan 01/07
(i) On the shelf 842VU: - install the FMGEC (1CA2) (Ref. TASK 22-83-34-400-802), - install the Slat and Flap Control Computer (SFCC) (22CV) (Ref. TASK 27-51-34-400-801), - install the Flight Control Data Concentrator (FCDC) (1CE2) (Ref. TASK 27-95-34-400-801), - install the Flight Control Secondary Computer (FCSC) (3CE2) (Ref. TASK 27-94-34-400-801), - install the Flight Control Primary Computer (FCPC) (2CE2) (Ref. TASK 27-93-34-400-801). (j) On the shelf 851VU: - install the Ground Proximity Warning Computer (GPWC) (1WZ) (Ref. TASK 34-48-34-400-801), - install the zone controller (630HK) (Ref. TASK 21-63-34-400801), - install the cabin pressure controller (311HL) (Ref. TASK 21-3134-400-801), - install the pack controller (531HH) (Ref. TASK 21-53-34-400801), - install the Bleed Monitoring Computer (BMC) (1HA1) (Ref. TASK 36-11-34-400-801), - install the BSCU (3GG) (Ref. TASK 32-42-34-400-801), - install the LGCIU (5GA1) (Ref. TASK 32-31-71-400-801). (k) On the shelf 852VU: - install the ventilation controller (280HN) (Ref. TASK 21-28-34400-801), - install the cabin pressure controller (312HL) (Ref. TASK 21-3134-400-801), - install the Bleed Monitoring Computer (BMC) (1HA2) (Ref. TASK 36-11-34-400-801), - install the pack controller (532HH) (Ref. TASK 21-53-34-400801), - install the Ground Power Control Unit (GPCU) (1XG) (Ref. TASK 24-41-34-400-801), - install the TPIC (2GV) (Ref. TASK 32-49-34-400-801), - install the Smoke Detection Control-Unit (SDCU) (20WH) (Ref. TASK 26-16-34-400-801), - install the LGCIU (5GA2) (Ref. TASK 32-31-71-400-801). (l) On the shelf 861VU: - install the Central Maintenance Computer (CMC) (1TM1) (Ref. TASK 45-13-34-400-801).
EFF : ALL 12-21-13 R SROS
Page 715 Jan 01/07
(m) On the shelf 862VU: - install the proximity switch control unit (5MJ) (Ref. TASK 5271-34-400-801), - install the FDIU (2TU) (Ref. TASK 31-33-34-400-803), - install the Quick Access Recorder (QAR) (3TU) (Ref. TASK 31-3352-400-801), - install the Digital ACMS Recorder (DAR) (2TV) (Ref. TASK 31-3652-400-801), - install the Data Management Unit (DMU) (1TV) (Ref. TASK 31-3634-400-801), - install the Central Maintenance Computer (CMC) (1TM2) (Ref. TASK 45-13-34-400-801), (n) On the shelf 872VU: - install the Air Data/Inertial Reference Unit (ADIRU) (1FP1, 1FP2) (Ref. TASK 34-12-34-400-801). (o) Install the Air Data/Inertial Reference Unit (ADIRU) (1FP3) (Ref. TASK 34-12-34-400-801). (p) On the mounting tray 5SQ: - install the weather radar transceiver (1SQ1, 1SQ2) (Ref. TASK 34-41-33-400-801). (q) On the shelf 915VU: - install the ILS receiver (1RT1) (Ref. TASK 34-36-31-400-801), (Ref. TASK 34-36-31-400-802). - install the Flight Control Secondary Computer (FCSC) (3CE1) (Ref. TASK 27-94-34-400-801), - install the Flight Control Primary Computer (FCPC) (2CE1) (Ref. TASK 27-93-34-400-801), - install the ILS receiver (1RT2) (Ref. TASK 34-36-31-400-801).
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(3) Make sure that the work area is clean and clear of tools and other items. (4) Close the access door 811. (5) Remove the access platform(s). Subtask 12-21-13-862-050 B. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-21-13 SROS
Page 716 Jan 01/07
TASK 12-21-13-100-802 Cleaning of Relay Box VU Panel Grids 1. __________________ Reason for the Job Refer to the MPD TASK: 212600-07 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 12-21-13-991-003
Energize the Ground Service Network De-energize the Ground Service Network Fig. 703
3. __________ Job Set-up Subtask 12-21-13-860-050 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). (2) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the access door 811. (3) Open the access door 811.
EFF : ALL 12-21-13 R SROS
Page 717 Jan 01/07
4. Procedure _________ (Ref. Fig. 703/TASK 12-21-13-991-003) Subtask 12-21-13-140-050 A. Cleaning of the Grids of the Relay Boxes NOTE : In the avionics compartment, use a vacuum cleaner and a soft brush ____ to clean the equipments. Keep the vacuum cleaner out of the avionics compartment to prevent dust contamination. (1) Clean the grids of the left relay box 751VU (a) Clean the left and right external grids. (b) Clean the bottom external grid. (c) Open the door of the relay box. (d) Clean the left and right internal grids. (e) Clean the bottom internal grid. (f) Close the door of the relay box. (2) Clean the grids of the right relay box 752VU (a) Clean the left and right external grids. (b) Clean the bottom external grid. (c) Open the door of the relay box. (d) Clean the left and right internal grids. (e) Clean the bottom internal grid. (f) Close the door of the relay box.
EFF : ALL 12-21-13 R SROS
Page 718 Jan 01/07
Location of Relay Boxes in the Avionics Compartment Figure 703/TASK 12-21-13-991-003 EFF : ALL 12-21-13 R SROS
Page 719 Jan 01/07
5. Close-up ________ Subtask 12-21-13-860-051 A. Put the Aircraft back to its Initial Configuration (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access door 811. (3) Remove the access platform(s). (4) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-21-13 SROS
Page 720 Jan 01/07
LUBRICATION - DESCRIPTION AND OPERATION _______________________________________ 1. _______ General This section gives the instructions related to the lubrication of the flight controls, the landing gear, the doors, the fuselage, the rudder and sliding windows. It includes the topics below: 12-22-27/P. Block 301 FLIGHT CONTROLS 12-22-32/P. Block 301 LANDING GEAR 12-22-52/P. Block 301 DOORS 12-22-53/P. Block 301 FUSELAGE 12-22-55/P. Block 301 STABILIZERS 12-22-56/P. Block 301 WINDOWS A. Lubrication Point Symbols: Each type of lubrication point is identified by a symbol. (Ref. Fig. 001)
EFF : ALL 12-22-00 SROS
Page 1 Apr 01/98
Lubrication Point Symbols Figure 001 EFF : ALL 12-22-00 SROS
Page 2 Apr 01/98
FLIGHT CONTROLS - SERVICING ___________________________ TASK 12-22-27-640-801 Lubricate the Trimmable Horizontal Stabilizer (THS) Actuator Ball Screw Nut WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. 1. __________________ Reason for the Job Refer to the MPD TASK: 274400-09 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No No No No No
specific specific specific specific specific
circuit breaker(s) safety clip(s) ACCESS PLATFORM 5M (16 FT) CONTAINER 1 L (1/4 USGAL) GUN - GREASE WARNING NOTICE
1 1 1 1
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 04-004 Material No. 19-003
USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
EFF : ALL 12-22-27 SROS
Page 301 Jan 01/05
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 27-40-00-866-801 29-00-00-863-802 29-00-00-863-803 29-00-00-864-802 29-00-00-864-803 29-00-00-864-804 R
ESPM 20-55-10 ESPM 20-55-20 12-22-27-991-001-A
Energize the Ground Service Network De-energize the Ground Service Network Operation of the THS Actuator Pressurize the Blue Hydraulic System with the Electric Pump Pressurize the Yellow Hydraulic System with the Electric Pump Depressurize the Blue Hydraulic System (Pressurized with the Electric Pump) Depressurize the Yellow Hydraulic System (Pressurized with the Electric Pump) Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Fig. 301
3. __________ Job Set-up Subtask 12-22-27-860-054 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). (2) Make sure that the hydraulic systems are depressurized (Ref. TASK 29-00-00-864-804).
EFF : ALL 12-22-27 SROS
Page 302 Apr 01/05
Subtask 12-22-27-865-050 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU FCPC3 STBY COM 7CE6 R20 721VU FCPC3 STBY MON 7CE5 R19 722VU FCPC 3 7CE3 V42 722VU FCPC 2 NORM 7CE2 V41 722VU FCPC 3 7CE4 V38 742VU FCPC 1 NORM 7CE1 C69 742VU FCPC 1 STBY 11CE K69 Subtask 12-22-27-010-050 C. Get Access (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the THS. (2) Put the ACCESS PLATFORM 5M (16 FT) below the access door 312AR, open the access door 312AR and set the LIGHT switch 4LJ to ON. (3) Make sure that the temperature of the ball screw nut is above 1 DEG.C (33.80 DEG.F). 4. Procedure _________ (Ref. Fig. 301/TASK 12-22-27-991-001-A) Subtask 12-22-27-640-063 A. Lubricate the THS-Actuator Ball Screw-Nut CAUTION : DO NOT MIX LITHIUM-COMPLEX THICKENED GREASE WITH CLAY_______ THICKENED GREASE. IF YOU MIX THESE GREASES, YOU CAN CAUSE DAMAGE TO THE BALL NUT OF THE THS ACTUATOR. R R
(1) Clean the vent hole area, the grease nipple and the THS-actuator ball screw-nut.To do this, use a clean lint-free cloth MISCELLANEOUS (Material No. 19-003). (2) Use a non-metallic device and make sure that the vent hole is clear.
EFF : ALL 12-22-27 SROS
Page 303 Jul 01/06
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Trimmable Horizontal Stabilizer (THS) Actuator Figure 301/TASK 12-22-27-991-001-A
EFF : ALL 12-22-27 SROS
Page 304 Jan 01/04
(3) Use a GUN - GREASE (MIL-PRF-23827) and apply the new COMMON GREASE (Material No. 04-004) through the grease nipple of the THS-actuator ball screw-nut. Do this until the grease comes out of the nut vent hole. It is usual that some grease comes out of the upper/lower nut seal. (4) Make sure that no grease comes out of the transfer tubes. If grease comes out of the transfer tubes, speak to Airbus.
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(5) Put a CONTAINER 1 L (1/4 USGAL) in position below the vent hole. (6) Use a GUN - GREASE (MIL-PRF-23827) and again apply the new COMMON GREASE (Material No. 04-004) through the grease nipple of the THS-actuator ball screw-nut. Do this until 150 cm3 (9.15 in.3) of the grease comes out of the nut vent hole. (7) Remove the unwanted grease from the grease nipple and the top and bottom of the nut. To do this, use a clean lint-free cloth MISCELLANEOUS (Material No. 19-003). (8) Pressurize the Blue or the Yellow hydraulic system (Ref. TASK 29-0000-863-802) or (Ref. TASK 29-00-00-863-803). (9) Operate the THS R R R
CAUTION : MAKE SURE THAT YOU REMOVE THE GREASING TOOL BEFORE YOU _______ OPERATE THE THS ACTUATOR. THE GREASING TOOL CAN CAUSE DAMAGE TO THE THS ACTUATOR. (a) Move the THS to the 14⁰UP stop position and then back to the neutral position (Ref. TASK 27-40-00-866-801). (10) Depressurize the Blue or the Yellow hydraulic system (Ref. TASK 2900-00-864-802) or (Ref. TASK 29-00-00-864-803) and make sure that the hydraulic system is depressurized (Ref. TASK 29-00-00-864-804). (11) Clean the THS-actuator ball screw-nut around the transfer tubes with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003). (12) Use a GUN - GREASE (MIL-PRF-23827) and again apply the new COMMON GREASE (Material No. 04-004) through the grease nipple of the THS-actuator ball screw-nut. Do this until the grease comes continuously out of the nut vent hole. (13) Make sure that no grease comes out of the transfer tubes. If grease comes out of the transfer tubes, contact Airbus. (14) Put a CONTAINER 1 L (1/4 USGAL) in position below the vent hole.
EFF : ALL 12-22-27 SROS
Page 305 Jan 01/07
(15) Use a GUN - GREASE and again apply the new COMMON GREASE (Material No. 04-004) through the grease nipple of the THS-actuator ball screw-nut. Do this until 150 cm3 (9.15 in.3) of the grease comes out of the nut vent hole. (16) Clean the vent hole area, the grease nipple and the THS-actuator ball screw-nut. To do this, use a clean lint-free cloth MISCELLANEOUS (Material No. 19-003). (a) If you find contamination of the electrical cables, you must clean them (Ref. ESPM 20-55-10) and (Ref. ESPM 20-55-20). (17) Make sure that the ball in the grease nipple closes correctly the grease nipple. 5. Close-up ________ Subtask 12-22-27-865-051 A. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 7CE1, 7CE2, 7CE3, 7CE4, 7CE5, 7CE6, 11CE. Subtask 12-22-27-410-050 B. Close Access R R R
CAUTION : MAKE SURE THAT YOU REMOVE THE GREASING TOOL BEFORE YOU OPERATE _______ THE THS ACTUATOR. THE GREASING TOOL CAN CAUSE DAMAGE TO THE THS ACTUATOR. (1) Make sure that the work area is clean and clear of tools and other items. (2) Set the LIGHT switch 4LJ to OFF and close the access door 312AR. (3) Remove the access platform(s). (4) Remove the warning notice(s). (5) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-22-27-860-055 C. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-22-27 SROS
Page 306 Jan 01/07
TASK 12-22-27-640-802 Lubricate the Trimmable Horizontal Stabilizer (THS) Mechanical Control Chains R R
WARNING : KEEP ALL HYDROCARBONS (FUELS, LUBRICANTS, ETC.) AWAY FROM ALL SOURCES _______ OF OXYGEN. OXYGEN BECOMES EXPLOSIVE WHEN IT TOUCHES HYDROCARBONS. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Refer to the MPD TASK: 274100-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific No specific 98F27401000000
1 1 1 1
circuit breaker(s) safety clip(s) ACCESS PLATFORM 3M (10 FT) BRUSH - BRISTLED WARNING NOTICE PITCH TRIM CONTROL LOCKING
EFF : ALL 12-22-27 SROS
Page 307 Jul 01/06
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 04-004 Material No. 05-002 Material No. 05-005 Material No. 11-002 R R
Material No. 19-003
USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00) USA MIL-C-16173 GRADE II CORROSION PREVENTIVE (Ref. 20-31-00) USA MIL-PRF-680 DRY CLEANING SOLVENT (VARSOL/WHITE SPIRIT) (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------1
cotter pins
27-41-04 03 -110
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 27-40-00-866-801 29-00-00-864-804 12-22-27-991-002
Energize the Ground Service Network De-energize the Ground Service Network Operation of the THS Actuator Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Fig. 302
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INTENTIONALLY BLANK
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INTENTIONALLY BLANK
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Page 310 Apr 01/03
3. __________ Job Set-up Subtask 12-22-27-860-056 A. Aircraft Maintenance Configuration (1) Make sure that the pitch-trim control wheels on the panel 125VU are in the 0 position (Ref. TASK 27-40-00-866-801). (2) Install the PITCH TRIM CONTROL LOCKING (98F27401000000) on the pitch-trim control wheels. (3) Put the WARNING NOTICE in position on the panel 125VU to tell persons not to operate the pitch-trim controls. (4) Energize the ground service network (Ref. TASK 24-42-00-861-801). (5) Make sure that the hydraulic systems are depressurized (Ref. TASK 29-00-00-864-804). Subtask 12-22-27-865-052 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU FCPC3 STBY COM 7CE6 R20 721VU FCPC3 STBY MON 7CE5 R19 722VU FCPC 3 7CE3 V42 722VU FCPC 2 NORM 7CE2 V41 722VU FCPC 3 7CE4 V38 742VU FCPC 1 NORM 7CE1 C69 742VU FCPC 1 STBY 11CE K69 Subtask 12-22-27-010-051 C. Get Access (Ref. Fig. 302/TASK 12-22-27-991-002) (1) Put the ACCESS PLATFORM 3M (10 FT) below the access door 312AR and open the access door 312AR and set the LIGHT switch 4LJ to ON. (2) Remove the screws (8), the washers (7), release the quick-release fasteners (6) and remove the protective cover (9).
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Control Chain Figure 302/TASK 12-22-27-991-002- 12 (SHEET 1) EFF : ALL 12-22-27 R SROS
Page 312 Jan 01/02
Control Chain Figure 302/TASK 12-22-27-991-002- 22 (SHEET 2) EFF : ALL 12-22-27 R SROS
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(3) Remove and discard the cotter pins (1), remove the nuts (2), the washers (3), the bolts (4) and the chain cover (5). 4. Procedure _________ (Ref. Fig. 302/TASK 12-22-27-991-002) Subtask 12-22-27-640-051 A. Lubrication of the THS Mechanical Control Chains R R R
WARNING : KEEP ALL HYDROCARBONS (FUELS, LUBRICANTS, ETC.) AWAY FROM ALL _______ SOURCES OF OXYGEN. OXYGEN BECOMES EXPLOSIVE WHEN IT TOUCHES HYDROCARBONS. WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Clean the forward and the aft chain with CLEANING AGENTS (Material No. 11-002) and a BRUSH - BRISTLED.
R R
(2) Use a BRUSH - BRISTLED to apply a thin layer of the COMMON GREASE (Material No. 04-004) to the chains.
R
(3) Do not apply too much grease to the chains.
R R R
(a) If you apply too much grease to the chains: - Use a clean lint-free cloth MISCELLANEOUS (Material No. 19-003) to remove the unwanted grease from the chains.
R R
(4) Make sure that the grease does not fall into the area of the electronic and/or oxygen equipment. 5. Close-up ________ Subtask 12-22-27-410-058 A. Close Access (Ref. Fig. 302/TASK 12-22-27-991-002) (1) Install the chain cover (5). (a) Apply the SPECIAL MATERIALS (Material No. 05-002) to the interface of the chain cover (5), to the bolts (4) and the nuts (2).
EFF : ALL 12-22-27 SROS
Page 314 Jul 01/06
(b) Install the chain cover (5), the bolts (4), the washers (3), the nuts (2) and safety the nuts (2) with the new cotter pins (1). (c) Apply the SPECIAL MATERIALS (Material No. 05-005) to the bolts (4) and the nuts (2). (2) Install the protective cover (9), tighten the quick-release fasteners (6) and install the washers (7) and the screws (8). Subtask 12-22-27-865-053 B. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 7CE1, 7CE2, 7CE3, 7CE4, 7CE5, 7CE6, 11CE. Subtask 12-22-27-410-051 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Set the LIGHT switch 4LJ to OFF and close the access door 312AR. (3) Remove the access platform(s). (4) Remove the warning notice(s). (5) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-22-27-860-057 D. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801). (2) Remove the PITCH TRIM CONTROL LOCKING from the pitch-trim control wheels.
EFF : ALL 12-22-27 R SROS
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TASK 12-22-27-640-803 R
Lubrication of Flap Track/Carriage (1-5) Roller Bearings WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Refer to the MPD TASK: 275400-04 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific 98D27803000000 98F29208217000
circuit breaker(s) safety clip(s) 1 WARNING NOTICE 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER 1 SAFETY PIN - RAT
EFF : ALL 12-22-27 SROS
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B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R
Material No. 04-004 Material No. 19-003
USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 27-50-00-866-801 27-50-00-866-802 29-24-00-081-801 29-24-00-481-801 32-12-00-010-801 32-12-00-410-801 12-22-27-991-003
Energize the Ground Service Network De-energize the Ground Service Network Extension of the Flaps on the Ground Retraction of the Flaps on the Ground Removal of the RAT Safety Pin Installation of the RAT Safety Pin Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Fig. 303
3. __________ Job Set-up Subtask 12-22-27-860-050 A. Aircraft Maintenance Configuration (1) Fully extend the flaps (Ref. TASK 27-50-00-866-801). (2) Put the WARNING NOTICE in position on panel 114VU to tell persons not to operate the flap/slat controls. (3) Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER on the flap/slat control lever on panel 114VU. (4) Energize the ground service network (Ref. TASK 24-42-00-861-801).
EFF : ALL 12-22-27 SROS
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Subtask 12-22-27-865-054 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM 10CV X14 722VU SFCC 2 FLAP 2CV T43 742VU SFCC 1 FLAP 1CV L61 Subtask 12-22-27-010-052 C. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Install the SAFETY PIN - RAT (Ref. TASK 29-24-00-481-801). 4. Procedure _________ (Ref. Fig. 303/TASK 12-22-27-991-003) Subtask 12-22-27-640-052 A. Lubrication of the Flap Track/Carriage Roller Bearings WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Clean the grease nipples with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003). R R R
(2) Apply the COMMON GREASE (Material No. 04-004) to the flap-track/carriage roller bearings through the the grease nipples until the new grease comes out from the fittings. (3) Remove the unwanted grease from the greasing points.
EFF : ALL 12-22-27 SROS
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5. Close-up ________ Subtask 12-22-27-865-055 A. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1CV, 2CV, 10CV Subtask 12-22-27-410-052 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the MLG doors (Ref. TASK 32-12-00-410-801). (3) Remove the SAFETY PIN - RAT (Ref. TASK 29-24-00-081-801). (4) Remove the access platform(s). Subtask 12-22-27-860-051 C. Put the Aircraft back to its Initial Configuration (1) Remove the warning notice(s). (2) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever on panel 114VU. (3) Retract the flaps (Ref. TASK 27-50-00-866-802). (4) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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R
Flap Track Rollers Figure 303/TASK 12-22-27-991-003- 12 (SHEET 1)
EFF : ALL 12-22-27 SROS
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R
Flap Track Rollers Figure 303/TASK 12-22-27-991-003- 22 (SHEET 2)
EFF : ALL 12-22-27 SROS
Page 321 Jul 01/04
TASK 12-22-27-640-804 R
Lubrication of all Slat Track Roller Bearings, Pinion Bearings, Rack and Pinion Teeth and Slat Track 2 and 3 Lever Bearings WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Refer to the MPD TASK: 278000-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific 98D27803000000
circuit breaker(s) safety clip(s) 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 WARNING NOTICE 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
EFF : ALL 12-22-27 SROS
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B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 04-022 Material No. 19-003
USA MIL-PRF-81322 SYNTHE.HYDROCARBON GREASE HIGH PRESSURE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 27-50-00-866-801 27-50-00-866-802 27-80-00-866-801 27-80-00-866-802 57-41-37-000-801 57-41-37-400-801 57-42-37-000-801 57-42-37-400-801 12-22-27-991-004
Energize the Ground Service Network De-energize the Ground Service Network Extension of the Flaps on the Ground Retraction of the Flaps on the Ground Extension of the Slats on the Ground Retraction of the Slats on the Ground Removal of the Access Panels and Covers Installation of the Access Panels and Covers Removal of the Access Panels and Covers Installation of the Access Panels and Covers Fig. 304
3. __________ Job Set-up Subtask 12-22-27-860-052 A. Aircraft Maintenance Configuration (1) Fully extend the flaps (Ref. TASK 27-50-00-866-801). (2) Fully extend the slats (Ref. TASK 27-80-00-866-801). (3) Put the WARNING NOTICE in position on panel 114VU to tell persons not to operate the flap/slat controls. (4) Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER on the flap/slat control lever on panel 114VU. (5) Energize the ground service network (Ref. TASK 24-42-00-861-801).
EFF : ALL 12-22-27 SROS
Page 323 Jan 01/06
Subtask 12-22-27-865-056 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM AVAIL 10CW X13 722VU SFCC 2 SLAT 2CW V40 742VU SFCC 1 SLAT 1CW L62 Subtask 12-22-27-010-064 C. Get Access (1) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position. (2) Remove the access panels (Ref. TASK 57-41-37-000-801) 57-42-37-000-801): - in the Zone 521: 521BB, 521CB, 521GB, 521JB, - in the Zone 522: 522CB, 522TB, 522GB, 522HB, 522JB, 522RB, - in the Zone 523: 523CB, 523EB, 523GB, 523JB, 523LB, - in the Zone 621: 621BB, 621CB, 621GB, 621JB, - in the Zone 622: 622CB, 622TB, 622GB, 622HB, 622JB, 622RB, - in the Zone 623: 623CB, 623EB, 623GB, 623JB, 623LB,
and (Ref. TASK 522LB, 522NB, 523NB, 622LB, 622NB, 623NB.
4. Procedure _________ (Ref. Fig. 304/TASK 12-22-27-991-004) Subtask 12-22-27-640-053 A. Lubrication of all the Slat Track Roller Bearings, the Pinion Bearings, the Rack and Pinion Teeth, including the Slat Track 2 and 3 Lever Bearings WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Clean the grease nipples with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003).
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Slat Track Rollers and Pinions Figure 304/TASK 12-22-27-991-004
EFF : ALL 12-22-27 SROS
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INTENTIONALLY BLANK
R 12-22-27 SROS
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(2) Apply COMMON GREASE (Material No. 04-022) to: - the slat track roller bearings, - the pinion bearings, - the rack and pinion teeth and - the slat track 2 and track 3 lever bearings through the grease nipples until the new grease comes out. (3) Remove the unwanted grease from the greasing points. 5. Close-up ________ Subtask 12-22-27-410-054 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access 57-42-37-400-801): - in the Zone 521: - in the Zone 522: 522RB, - in the Zone 523: - in the Zone 621: - in the Zone 622: 622RB, - in the Zone 623:
panels (Ref. TASK 57-41-37-400-801) and (Ref. TASK 521BB, 521CB, 521GB, 521JB, 522CB, 522TB, 522GB, 522HB, 522JB, 522LB, 522NB, 523CB, 523EB, 523GB, 523JB, 523LB, 523NB, 621BB, 621CB, 621GB, 621JB, 622CB, 622TB, 622GB, 622HB, 622JB, 622LB, 622NB, 623CB, 623EB, 623GB, 623JB, 623LB, 623NB.
Subtask 12-22-27-865-057 B. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1CW, 2CW, 10CW Subtask 12-22-27-860-053 C. Put the Aircraft back to its Initial Configuration (1) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever on panel 114VU. (2) Retract the slats (Ref. TASK 27-80-00-866-802). R
(3) Retract the flaps (Ref. TASK 27-50-00-866-802).
R
(4) Remove the warning notice(s).
EFF : ALL 12-22-27 SROS
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R
(5) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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TASK 12-22-27-640-805 Lubrication of all Spoiler Linkage Bearings fitted with Grease Nipples WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Refer to the MPD TASK: 276400-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific No specific 98D27603002001 98D27803000000
circuit breaker(s) safety clip(s) 1 WARNING NOTICE 1 SPOILER MAINTENANCE KEY 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
EFF : ALL 12-22-27 SROS
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B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R
Material No. 04-004 Material No. 19-003
USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 27-50-00-866-801 27-50-00-866-802 27-60-00-866-801 27-60-00-866-802 27-64-00-710-801 29-00-00-864-804 12-22-27-991-005
Energize the Ground Service Network De-energize the Ground Service Network Extension of the Flaps on the Ground Retraction of the Flaps on the Ground Extension of the Spoilers for Maintenance Retraction of the Spoilers after Maintenance Operational Test of the Spoilers Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Fig. 305
3. __________ Job Set-up Subtask 12-22-27-860-058 A. Aircraft Maintenance Configuration (1) Extend the flaps (Ref. TASK 27-50-00-866-801). (2) Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER on the slat/flap control lever on the panel 114VU. (3) Make sure that the aircraft hydraulic systems are depressurized (Ref. TASK 29-00-00-864-804). (4) Energize the ground service network (Ref. TASK 24-42-00-861-801).
EFF : ALL 12-22-27 SROS
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(5) Put the WARNING NOTICE in position in the cockpit to tell persons not to operate the flight controls. Subtask 12-22-27-865-058 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU FCPC3 STBY COM 7CE6 R20 721VU FCPC3 STBY MON 7CE5 R19 722VU FCDC 2 6CE2 T42 722VU FCSC 2 10CE2 T39 722VU FCPC 3 7CE3 V42 722VU FCPC 2 NORM 7CE2 V41 722VU FCPC 3 7CE4 V38 742VU FCSC 1 NORM 10CE1 C70 742VU FCPC 1 NORM 7CE1 C69 742VU FCSC 1 STBY 9CE G77 742VU FCPC 1 STBY 11CE K69 742VU FCDC 1 6CE1 L76 Subtask 12-22-27-860-067 C. Aircraft Maintenance Configuration (1) Extend the spoilers (Ref. TASK 27-60-00-866-801). R
(2) Install the SPOILER MAINTENANCE KEY (98D27603002001). 4. Procedure _________ (Ref. Fig. 305/TASK 12-22-27-991-005) Subtask 12-22-27-640-054 A. Lubrication of all Spoiler Linkage Bearings fitted with Grease Nipples WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Clean the grease nipples with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003).
EFF : ALL 12-22-27 SROS
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R
Spoiler Hinge Bearings Figure 305/TASK 12-22-27-991-005
EFF : ALL 12-22-27 SROS
Page 332 Jul 01/04
R R
(2) Apply the COMMON GREASE (Material No. 04-004) to the spoiler hinge bearings through the grease nipples until the new grease comes out. (3) Remove the unwanted grease from the greasing points. 5. Close-up ________ Subtask 12-22-27-860-059 A. Put the Aircraft back to its Initial Configuration (1) Remove the SPOILER MAINTENANCE KEY (98D27603002001). (2) Retract the spoilers (Ref. TASK 27-60-00-866-802). (3) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the slat/flap control lever on the panel 114VU. (4) Retract the flaps (Ref. TASK 27-50-00-866-802). (5) Remove the warning notice(s). Subtask 12-22-27-865-059 B. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CE1, 6CE2, 7CE1, 7CE2, 7CE3, 7CE4, 7CE5, 7CE6, 9CE, 10CE1, 10CE2, 11CE. Subtask 12-22-27-710-050 C. Do the operational test of the spoilers (Ref. TASK 27-64-00-710-801). Subtask 12-22-27-860-062 D. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-22-27 SROS
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TASK 12-22-27-640-806 Lubrication of Flap Steady Bearings WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Refer to the MPD TASK: 275400-08 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific No specific No specific 98D27803000000
circuit breaker(s) safety clip(s) 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 WARNING NOTICE 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
EFF : ALL 12-22-27 SROS
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B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 04-022 Material No. 04-024 Material No. 19-003
USA MIL-PRF-81322 SYNTHE.HYDROCARBON GREASE HIGH PRESSURE (Ref. 20-31-00) AIB AIMS 09-06-001 SYNTHETIC GREASE FOR FLAP & SLAT MECHANISM (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 27-50-00-866-801 27-50-00-866-802 27-80-00-866-801 27-80-00-866-802 12-22-27-991-006-A
Energize the Ground Service Network De-energize the Ground Service Network Extension of the Flaps on the Ground Retraction of the Flaps on the Ground Extension of the Slats on the Ground Retraction of the Slats on the Ground Fig. 306
3. __________ Job Set-up Subtask 12-22-27-860-060 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). (2) Fully extend the flaps (Ref. TASK 27-50-00-866-801). (3) Fully extend the slats (Ref. TASK 27-80-00-866-801). (4) Put the WARNING NOTICE in position on panel 114VU to tell persons not to operate the flap/slat controls. (5) Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER on the flap/slat control lever on panel 114VU.
EFF : ALL 12-22-27 SROS
Page 335 Jan 01/06
Subtask 12-22-27-865-060 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM 10CV X14 722VU SFCC 2 FLAP 2CV T43 742VU SFCC 1 FLAP 1CV L61 Subtask 12-22-27-010-060 C. Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position. 4. Procedure _________ (Ref. Fig. 306/TASK 12-22-27-991-006-A) Subtask 12-22-27-640-055 A. Lubrication of the Flap Steady Bearings WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Clean the grease nipples with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003). (2) Apply COMMON GREASE (Material No. 04-022) or COMMON GREASE (Material No. 04-024) to the steady bearings through the grease nipples until the new grease comes out. (3) Remove the unwanted grease from the greasing points. 5. Close-up ________ Subtask 12-22-27-865-061 A. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1CV, 2CV, 10CV.
EFF : ALL 12-22-27 R SROS
Page 336 Oct 01/03
Flap/Slat Steady Bearings Figure 306/TASK 12-22-27-991-006-A EFF : ALL 12-22-27 R SROS
Page 337 Oct 01/03
Subtask 12-22-27-860-061 B. Put the Aircraft back to its Initial Configuration (1) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever on panel 114VU. R
(2) Retract the slats (Ref. TASK 27-80-00-866-802).
R
(3) Retract the flaps (Ref. TASK 27-50-00-866-802). Subtask 12-22-27-410-055 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Remove the warning notice(s). (3) Remove the access platform(s). (4) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-22-27-860-063 D. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-22-27 SROS
Page 338 Apr 01/04
TASK 12-22-27-640-807 Lubrication of the Aileron Hinge Bearings WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Refer to the MPD TASK: 271400-04 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific No specific No specific 98F27108438000
circuit breaker(s) safety clip(s) 1 ACCESS PLATFORM 5M (16 FT) 1 WARNING NOTICE 4 DISTANCE COLLAR - AILERON
EFF : ALL 12-22-27 SROS
Page 339 Jan 01/05
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 04-022 Material No. 19-003
USA MIL-PRF-81322 SYNTHE.HYDROCARBON GREASE HIGH PRESSURE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 29-00-00-864-804 12-22-27-991-007
Energize the Ground Service Network De-energize the Ground Service Network Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Fig. 307
3. __________ Job Set-up Subtask 12-22-27-860-064 A. Aircraft Maintenance Configuration (1) Make sure that the aircraft hydraulic systems are depressurized (Ref. TASK 29-00-00-864-804). (2) Energize the ground service network (Ref. TASK 24-42-00-861-801). (3) Put the WARNING NOTICE in position in the cockpit to tell persons not to operate the flight controls.
EFF : ALL 12-22-27 SROS
Page 340 Jan 01/06
Subtask 12-22-27-865-062 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------722VU FCDC 2 6CE2 T42 722VU FCSC 2 10CE2 T39 722VU FCPC 3 7CE3 V42 722VU FCPC 2 NORM 7CE2 V41 722VU FCPC 3 7CE4 V38 742VU FCSC 1 NORM 10CE1 C70 742VU FCPC 1 NORM 7CE1 C69 742VU FCSC 1 STBY 9CE G77 742VU FCPC 1 STBY 11CE K69 742VU FCDC 1 6CE1 L76 Subtask 12-22-27-010-063 C. Get Access R R
(1) Put the ACCESS PLATFORM 5M (16 FT) in position below the inboard aileron. (2) Remove the applicable access panels: - For the left inboard aileron, access panels 575AB, 575BB, 591AB, 591BB, 591CB, 591DB, 575AT. - For the right inboard aileron, access panels 675AB, 675BB, 691AB, 691BB, 691CB, 691DB, 675AT. - For the left outboard aileron, access panels 575CB, 575DB, 592AB, 592BB, 592CB, 592DB, 575BT. - For the right outboard aileron, access panels 675CB, 675DB, 692AB, 692BB, 692CB, 692DB, 675BT.
R R R R
(3) Move the trailing edge of the inboard and outboard ailerons up and install the DISTANCE COLLAR - AILERON (98F27108438000) on the aileron servo controls.
R R
EFF : ALL 12-22-27 SROS
Page 341 Oct 01/04
4. Procedure _________ (Ref. Fig. 307/TASK 12-22-27-991-007) Subtask 12-22-27-640-056 A. Lubrication of all Aileron Hinge Bearings WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Clean the grease nipples with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003). (2) Apply COMMON GREASE (Material No. 04-022) to the aileron hinge bearings through the grease nipples until the new grease comes out. (3) Remove the unwanted grease from the greasing points. 5. Close-up ________ Subtask 12-22-27-410-059 A. Close Access R R
(1) Remove the DISTANCE COLLAR - AILERON (98F27108438000) from the aileron servo controls. (2) Install the applicable access panels: - For the left inboard aileron, access panels 575AB, 575BB, 591AB, 591BB, 591CB, 591DB, 575AT. - For the right inboard aileron, access panels 675AB, 675BB, 691AB, 691BB, 691CB, 691DB, 675AT. - For the left outboard aileron, access panels 575CB, 575DB, 592AB, 592BB, 592CB, 592DB, 575BT. - For the right outboard aileron, access panels 675CB, 675DB, 692AB, 692BB, 692CB, 692DB, 675BT.
R R R R
Subtask 12-22-27-865-063 B. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CE1, 6CE2, 7CE1, 7CE2, 7CE3, 7CE4, 9CE, 10CE1, 10CE2, 11CE.
EFF : ALL 12-22-27 SROS
Page 342 Oct 01/04
Aileron Hinge Bearings Figure 307/TASK 12-22-27-991-007 EFF : ALL 12-22-27 R SROS
Page 343 Oct 01/03
Subtask 12-22-27-410-056 C. Close Access (1) Remove the warning notice(s). (2) Remove the access platform(s). (3) Remove the ground support and maintenance equipment, the special and standard tools and all other items. Subtask 12-22-27-860-065 D. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-22-27 R SROS
Page 344 Oct 01/03
TASK 12-22-27-640-808 Lubrication of Slat Rotary Actuator Type A (Track 2-3) WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Refer to the MPD TASK: 278000-05 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific 98D27803000000
circuit breaker(s) safety clip(s) 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 WARNING NOTICE 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
EFF : ALL 12-22-27 R SROS
Page 345 Jan 01/07
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R
Material No. 04-004 Material No. 04-022 Material No. 04-024 Material No. 19-003
USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) USA MIL-PRF-81322 SYNTHE.HYDROCARBON GREASE HIGH PRESSURE (Ref. 20-31-00) AIB AIMS 09-06-001 SYNTHETIC GREASE FOR FLAP & SLAT MECHANISM (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R
24-42-00-861-801 24-42-00-862-801 27-80-00-866-801 27-80-00-866-802 57-41-37-000-801 57-41-37-400-801 57-42-37-000-801 57-42-37-400-801 SIL 12-008
Energize the Ground Service Network De-energize the Ground Service Network Extension of the Slats on the Ground Retraction of the Slats on the Ground Removal of the Access Panels and Covers Installation of the Access Panels and Covers Removal of the Access Panels and Covers Installation of the Access Panels and Covers (for corrective action)
**ON A/C ALL Post SB Post SB
27-3077 For A/C 401-449, 27-3100 For A/C ALL
12-22-27-991-008
Fig. 308
EFF : ALL 12-22-27 SROS
Page 346 Jan 01/07
**ON A/C ALL 3. __________ Job Set-up R
**ON A/C ALL
R
Post SB
27-3100 For A/C ALL
Subtask 12-22-27-860-066 A. Aircraft Maintenance Configuration (1) Fully extend the slats (Ref. TASK 27-80-00-866-801). (2) Put the WARNING NOTICE in position on panel 114VU to tell persons not to operate the flap/slat controls. (3) Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER on the flap/slat control lever on panel 114VU. (4) Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-22-27-865-064 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM AVAIL 10CW X13 722VU SFCC 2 SLAT 2CW V40 742VU SFCC 1 SLAT 1CW L62 R R
Subtask 12-22-27-010-066-A C. Get Access
R
(1) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position.
R R R R
(2) Remove the access panels (Ref. TASK 57-41-37-000-801) and (Ref. TASK 57-42-37-000-801): - in the Zone 521: 521DB, 521GB, - in the Zone 621: 621DB, 621GB,
EFF : ALL 12-22-27 SROS
Page 347 Jan 01/06
**ON A/C ALL 4. Procedure _________ **ON A/C ALL Post SB Post SB
27-3077 For A/C 401-449, 27-3100 For A/C ALL
(Ref. Fig. 308/TASK 12-22-27-991-008) Subtask 12-22-27-640-057-A A. Lubrication of the Slat Rotary Actuators Type A R (1) Lubrication of the Slat Rotary Actuators (Type A) on Slat Track 2 and 3 PN: 954A0000-03, 954A0000-04, 954B0000-02, 954C0000-01 and subsequent versions
R R R R R
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE _______ THIS/THESE MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES.
R R R R R R R R R R R R R R R
CAUTION : WHEN YOU DO A MAINTENANCE TASK THAT USES COMMON GREASE, _______ OBEY THESE PRECAUTIONS: - IF POSSIBLE, USE ONLY GREASES OF THE SAME SPECIFICATION TYPE (IT IS PERMITTED TO USE DIFFERENT BRANDS IF THE SPECIFICATION TYPE IS THE SAME). WE SPECIALLY RECOMMEND THAT YOU DO NOT MIX GREASES THAT HAVE CLAY THICKENERS WITH GREASES THAT HAVE LITHIUM THICKENERS. SUCH A MIXTURE CAN CHANGE THE LUBRICATION PROPERTIES OF THE GREASE. - IF YOU CANNOT OBEY THESE PRECAUTIONS AND YOU USE GREASES OF DIFFERENT TYPES (SPECIALLY THOSE WITH CLAY THICKENERS AND LITHIUM THICKENERS), DECREASE THE SERVICING INTERVALS (BY HALF, FOR EXAMPLE) SPECIFIED IN THE MAINTENANCE PLANNING DOCUMENT. DO THIS FOR APPROXIMATELY THREE OR FOUR SERVICES (REFER TO YOUR IN-SERVICE DATA TO FIND THE NUMBER OF SERVICES BEST ADAPTED TO AIRCRAFT). NOTE : It is not permitted to apply grease again to the slat rotary ____ actuators (Type A) PN: 954A0000-01, 954A0000-02, 954B0000-01. (a) Clean the grease nipple (1) of the rotary actuator with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003).
EFF : ALL 12-22-27 SROS
Page 348 Jan 01/07
R R
Slat Rotary Actuator Type A Figure 308/TASK 12-22-27-991-008
R EFF : ALL 12-22-27 SROS
Page 349 Jan 01/06
R R R R
(b) Apply the COMMON GREASE (Material No. 04-022), or the COMMON GREASE (Material No. 04-024), or the COMMON GREASE (Material No. 04-004) to the grease nipple (1). For the correct type of grease to use, refer to the the SIL (Ref. SIL 12-008). (c) Make sure that the new grease comes out of the actuator vent valve (2). (d) Remove the unwanted grease from the grease nipple (1) and the actuator vent valve (2). **ON A/C ALL 5. Close-up ________ **ON A/C ALL Post SB
27-3100 For A/C ALL
Subtask 12-22-27-410-057-A A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels (Ref. TASK 57-41-37-400-801) and (Ref. TASK 57-42-37-400-801): - in the Zone 521: 521DB, 521GB, - in the Zone 621: 621DB, 621GB, Subtask 12-22-27-865-065 B. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1CW, 2CW, 10CW. Subtask 12-22-27-860-068 C. Put the Aircraft back to its Initial Configuration (1) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever on panel 114VU. (2) Retract the slats (Ref. TASK 27-80-00-866-802).
EFF : ALL 12-22-27 SROS
Page 350 Jan 01/07
(3) Remove the access platform(s). (4) Remove the warning notice(s). (5) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-22-27 R SROS
Page 351 Jan 01/07
**ON A/C ALL TASK 12-22-27-640-815 Lubrication of Slat Rotary Actuator Type B (Track 5-16) WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Refer to the MPD TASK: 278000-07 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No
specific specific specific specific
98D27803000000 98F20008247000
circuit breaker(s) safety clip(s) 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 WARNING NOTICE Torque Wrench : range 0.00 to 1.20 m.daN (0.00 to 9.00 lbf.ft) 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER 1 QUANTITY LIMITER - REGREASING
EFF : ALL 12-22-27 R SROS
Page 352 Jan 01/07
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R
Material No. 04-004 Material No. 04-022 Material No. 04-024
USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) USA MIL-PRF-81322 SYNTHE.HYDROCARBON GREASE HIGH PRESSURE (Ref. 20-31-00) AIB AIMS 09-06-001 SYNTHETIC GREASE FOR FLAP & SLAT MECHANISM (Ref. 20-31-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------3
O-ring
27-84-49 01 -020
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R
24-42-00-861-801 24-42-00-862-801 27-80-00-866-801 27-80-00-866-802 57-41-37-000-801 57-41-37-400-801 57-42-37-000-801 57-42-37-400-801 SIL 12-008
Energize the Ground Service Network De-energize the Ground Service Network Extension of the Slats on the Ground Retraction of the Slats on the Ground Removal of the Access Panels and Covers Installation of the Access Panels and Covers Removal of the Access Panels and Covers Installation of the Access Panels and Covers (for corrective action)
**ON A/C 001-001, 201-205, 251-252, 255-299, 401-449, 12-22-27-991-013-A
Fig. 309
EFF : ALL 12-22-27 SROS
Page 353 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------**ON A/C 002-049, 206-249, 301-399, 401-449, 451-499, 701-749, Post SB
27-3077 For A/C 401-449,
12-22-27-991-013
Fig. 309A
**ON A/C ALL 3. __________ Job Set-up Subtask 12-22-27-860-080 A. Aircraft Maintenance Configuration (1) Fully extend the slats (Ref. TASK 27-80-00-866-801). (2) Put the WARNING NOTICE in position on panel 114VU to tell persons not to operate the flap/slat controls. (3) Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER on the flap/slat control lever on panel 114VU. (4) Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-22-27-865-078 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM AVAIL 10CW X13 722VU SFCC 2 SLAT 2CW V40 742VU SFCC 1 SLAT 1CW L62
EFF : ALL 12-22-27 R SROS
Page 354 Jan 01/07
Subtask 12-22-27-010-075 C. Get Access (1) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position. (2) Remove the access panels (Ref. TASK 57-41-37-000-801) 57-42-37-000-801): - In the Zone 522: 522CB, 522TB, 522JB, 522LB, 522NB, - In the Zone 523: 523CB, 523EB, 523GB, 523JB, 523LB, - In the Zone 622: 622CB, 622TB, 622JB, 622LB, 622NB, - In the Zone 623: 623CB, 623EB, 623GB, 623JB, 623LB,
R R R R
and (Ref. TASK 522RB 523NB 622RB 623NB.
4. Procedure _________ **ON A/C 001-001, 201-205, 251-252, 255-299, 401-449, (Ref. Fig. 309/TASK 12-22-27-991-013-A) **ON A/C 002-049, 206-249, 301-399, 401-449, 451-499, 701-749, Post SB
27-3077 For A/C 401-449,
(Ref. Fig. 309A/TASK 12-22-27-991-013) **ON A/C 001-001, 201-205, 251-252, 255-299, 401-449, Subtask 12-22-27-640-064-A R
A. Lubrication of all Slat Rotary Actuators (Type B) Track 5 thru 16 WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES.
R EFF : ALL 12-22-27 SROS
Page 355 Jan 01/07
Slat Rotary Actuator Type B Figure 309/TASK 12-22-27-991-013-A R EFF : 001-001, 201-205, 251-252, 255-299, 12-22-27 401-449, SROS
Page 356 Jan 01/07
Slat Rotary Actuator Type B Figure 309A/TASK 12-22-27-991-013 R EFF : 002-049, 206-249, 301-399, 401-449, 12-22-27 451-499, 701-749, SROS
Page 357 Jan 01/07
R R R R R R R R R R R R R R R
CAUTION : WHEN YOU DO A MAINTENANCE TASK THAT USES COMMON GREASE, OBEY _______ THESE PRECAUTIONS: - IF POSSIBLE, USE ONLY GREASES OF THE SAME SPECIFICATION TYPE (IT IS PERMITTED TO USE DIFFERENT BRANDS IF THE SPECIFICATION TYPE IS THE SAME). WE SPECIALLY RECOMMEND THAT YOU DO NOT MIX GREASES THAT HAVE CLAY THICKENERS WITH GREASES THAT HAVE LITHIUM THICKENERS. SUCH A MIXTURE CAN CHANGE THE LUBRICATION PROPERTIES OF THE GREASE. - IF YOU CANNOT OBEY THESE PRECAUTIONS AND YOU USE GREASES OF DIFFERENT TYPES (SPECIALLY THOSE WITH CLAY THICKENERS AND LITHIUM THICKENERS), DECREASE THE SERVICING INTERVALS (BY HALF, FOR EXAMPLE) SPECIFIED IN THE MAINTENANCE PLANNING DOCUMENT. DO THIS FOR APPROXIMATELY THREE OR FOUR SERVICES (REFER TO YOUR IN-SERVICE DATA TO FIND THE NUMBER OF SERVICES BEST ADAPTED TO AIRCRAFT).
R R R R
(1) Fill the QUANTITY LIMITER - REGREASING with the COMMON GREASE (Material No. 04-022), or the COMMON GREASE (Material No. 04-024), or the COMMON GREASE (Material No. 04-004). For the correct type of grease to use, refer to the SIL (Ref. SIL 12-008).
R R
NOTE : Step 1 is only applicable when you fill the quantity limiter ____ (5) and the hose (1) for the first time.
R R R
(a) Remove the hose (1) from the quantity limiter (5). Connect the grease gun to the quantity limiter on the same side as the piston. (b) Operate the grease gun until the piston of the quantity limiter (5) is at the opposite end of the chamber.
R R
(c) Make sure that the chamber of the quantity limiter (5) is full with grease.
R R
(d) Remove the grease gun from the quantity limiter (5). Install it on the opposite side and connect the hose (1) to the quantity limiter (5). (e) Operate the grease gun until the piston of the quantity limiter (5) is at the opposite end of the chamber.
R R
(f) Make sure that the chamber of the quantity limiter (5) is full with grease.
R
(g) Make sure that the new grease comes out of the adapter (4). If not, do the steps (a) thru (f) again as necessary.
R EFF : 001-001, 201-205, 251-252, 255-299, 12-22-27 401-449, SROS
Page 358 Jan 01/07
(h) Interchange the grease gun and the hose (1) at the quantity limiter (5). R R
NOTE : The hose (1), the quantity limiter (5) and the adapter (4) ____ are part of the QUANTITY LIMITER - REGREASING (98F20008247000). (2) Lubricate the Slat Rotary Actuator
R R
(a) Remove the plug (2) and the O-ring (3) from the rotary actuator and install the adapter (4) on the rotary actuator. (b) Operate the grease gun until the piston of the quantity limiter (5) is at the opposite end of the chamber. (c) Remove the adapter (4) of the QUANTITY LIMITER - REGREASING from the rotary actuator. (d) Remove the O-ring (3) from the plug (2) and install the new Oring (3) on the plug (2). (e) Install the plug (2) on the rotary actuator. (f) TORQUE the plug (2) to between 0.4 and 0.6 m.daN (35.39 and 53.09 lbf.in). (g) Interchange the grease gun and the hose (1) at the quantity limiter (5).
R R
(h) Make sure that the chamber of the quantity limiter (5) is full with grease.
R
(i) Repeat the steps (a) thru (h) for each rotary actuator. **ON A/C 002-049, 206-249, 301-399, 451-499, 701-749, Subtask 12-22-27-640-064
R
A. Lubrication of all Slat Rotary Actuators (Type B) Track 5 thru 16 WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-22-27 301-399, 401-449, 451-499, 701-749, SROS
Page 359 Jan 01/07
R R R R R R R R R R R R R R R
CAUTION : WHEN YOU DO A MAINTENANCE TASK THAT USES COMMON GREASE, OBEY _______ THESE PRECAUTIONS: - IF POSSIBLE, USE ONLY GREASES OF THE SAME SPECIFICATION TYPE (IT IS PERMITTED TO USE DIFFERENT BRANDS IF THE SPECIFICATION TYPE IS THE SAME). WE SPECIALLY RECOMMEND THAT YOU DO NOT MIX GREASES THAT HAVE CLAY THICKENERS WITH GREASES THAT HAVE LITHIUM THICKENERS. SUCH A MIXTURE CAN CHANGE THE LUBRICATION PROPERTIES OF THE GREASE. - IF YOU CANNOT OBEY THESE PRECAUTIONS AND YOU USE GREASES OF DIFFERENT TYPES (SPECIALLY THOSE WITH CLAY THICKENERS AND LITHIUM THICKENERS), DECREASE THE SERVICING INTERVALS (BY HALF, FOR EXAMPLE) SPECIFIED IN THE MAINTENANCE PLANNING DOCUMENT. DO THIS FOR APPROXIMATELY THREE OR FOUR SERVICES (REFER TO YOUR IN-SERVICE DATA TO FIND THE NUMBER OF SERVICES BEST ADAPTED TO AIRCRAFT).
R R R R
(1) Fill the quantity limiter (3) with the COMMON GREASE (Material No. 04-022), or the COMMON GREASE (Material No. 04-024), or the COMMON GREASE (Material No. 04-004). For the correct type of grease to use, refer to the SIL (Ref. SIL 12-008). NOTE : The step 1 is only applicable when you fill the quantity ____ limiter (3) and the hose (4) for the first time.
R R
NOTE : The hose (4), the quantity limiter (3) and the adapter (2) are ____ part of the QUANTITY LIMITER - REGREASING. (a) Remove the hose (4) from the quantity limiter (3). Connect the grease gun to the quantity limiter (3) on the same side as the piston. (b) Operate the grease gun until the piston of the quantity limiter (3) is at the opposite end of the chamber. (c) Make sure that the chamber of the quantity limiter (3) is full with grease. (d) Remove the grease gun from the quantity limiter (3). (e) Install the grease gun on the opposite side and connect the hose (4) to the quantity limiter (3). (f) Operate the grease gun until the piston of the quantity limiter (3) is at the opposite end of the chamber. (g) Make sure that the chamber of the quantity limiter (3) is full with grease.
R EFF : 002-049, 206-249, 301-399, 451-499, 12-22-27 701-749, SROS
Page 360 Jan 01/07
(h) Make sure that the new grease comes out of the adapter (2). If not, do the steps (a) thru (g) again as necessary.
R
(i) Interchange the grease gun and the hose (4) at the quantity limiter (3). (2) Lubricate the Slat Rotary Actuator (a) Remove the plug (1) from the rotary actuator and install the adapter (2) on the rotary actuator. (b) Operate the grease gun until the piston of the quantity limiter (3) is at the opposite end of the chamber. (c) Remove the adapter (2) from the rotary actuator. (d) Install the plug (1) on the rotary actuator. (e) TORQUE the plug (1) to between 0.4 and 0.6 m.daN (35.39 and 53.09 lbf.in). (f) Interchange the grease gun and the hose (4) at the quantity limiter (3). (g) Make sure that the chamber of the quantity limiter (3) is full with grease. R
(h) Do the steps (a) thru (g) again for each rotary actuator. **ON A/C 001-001, 201-205, 251-252, 255-299, Post SB
27-3100 For A/C 001-001,201-205,251-252,255-299,
Subtask 12-22-27-640-064-C R
A. Lubrication of all Slat Rotary Actuators (Type B) Track 5 thru 16 WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-22-27 301-399, 451-499, 701-749, SROS
Page 361 Jan 01/07
R R R R R R R R R R R R R R R
CAUTION : WHEN YOU DO A MAINTENANCE TASK THAT USES COMMON GREASE, OBEY _______ THESE PRECAUTIONS: - IF POSSIBLE, USE ONLY GREASES OF THE SAME SPECIFICATION TYPE (IT IS PERMITTED TO USE DIFFERENT BRANDS IF THE SPECIFICATION TYPE IS THE SAME). WE SPECIALLY RECOMMEND THAT YOU DO NOT MIX GREASES THAT HAVE CLAY THICKENERS WITH GREASES THAT HAVE LITHIUM THICKENERS. SUCH A MIXTURE CAN CHANGE THE LUBRICATION PROPERTIES OF THE GREASE. - IF YOU CANNOT OBEY THESE PRECAUTIONS AND YOU USE GREASES OF DIFFERENT TYPES (SPECIALLY THOSE WITH CLAY THICKENERS AND LITHIUM THICKENERS), DECREASE THE SERVICING INTERVALS (BY HALF, FOR EXAMPLE) SPECIFIED IN THE MAINTENANCE PLANNING DOCUMENT. DO THIS FOR APPROXIMATELY THREE OR FOUR SERVICES (REFER TO YOUR IN-SERVICE DATA TO FIND THE NUMBER OF SERVICES BEST ADAPTED TO AIRCRAFT).
R R R R
(1) Fill the quantity limiter (5) with the COMMON GREASE (Material No. 04-022) or the COMMON GREASE (Material No. 04-024), or the COMMON GREASE (Material No. 04-004). For the correct type of grease to use, refer to the SIL (Ref. SIL 12-008).
R R
NOTE : Step 1 is only applicable when you fill the quantity limiter ____ (5) and the hose (1) for the first time.
R R
NOTE : The hose (1), the quantity limiter (5) and the adapter (4) are ____ part of the QUANTITY LIMITER - REGREASING. (a) Remove the hose (1) from the quantity limiter (5). Connect the grease gun to the quantity limiter (5) on the same side as the piston. (b) Operate the grease gun until the piston of the quantity limiter (5) is at the opposite end of the chamber. (c) Make sure that the chamber of the quantity limiter (5) is full with grease. (d) Remove the grease gun from the quantity limiter (5). (e) Install the grease gun on the opposite side and connect the hose (1) to the quantity limiter (5). (f) Operate the grease gun until the piston of the quantity limiter (5) is at the opposite end of the chamber. (g) Make sure that the chamber of the quantity limiter (5) is full with grease.
R EFF : 001-001, 201-205, 251-252, 255-299, 12-22-27 SROS
Page 362 Jan 01/07
(h) Make sure that the new grease comes out of the adapter (4). If not, do the steps (a) thru (g) again as necessary.
R
(i) Interchange the grease gun and the hose (1) at the quantity limiter (5). (2) Lubricate the Slat Rotary Actuator R R
(a) Remove the plug (2) and the O-ring (3) from the rotary actuator and install the adapter (4) on the rotary actuator. (b) Operate the grease gun until the piston of the quantity limiter (6) is at the opposite end of the chamber. (c) Remove the adapter (4) of the QUANTITY LIMITER - REGREASING from the rotary actuator. (d) Remove the O-ring (3) from the plug (2) and install the new Oring (3) on the plug (2). (e) Install the plug (2) on the rotary actuator. (f) TORQUE the plug (2) to between 0.4 and 0.6 m.daN (35.39 and 53.09 lbf.in). (g) Interchange the grease gun and the hose (1) at the quantity limiter (5). (h) Make sure that the chamber of the quantity limiter (5) is full with grease.
R
(i) Do the steps (a) thru (h) again for each rotary actuator. **ON A/C 002-049, 206-249, 301-399, 401-449, 451-499, 701-749, Post SB Post SB
27-3077 For A/C 401-449, 27-3100 For A/C 002-049,206-249,301-399,401-449,451-499,701-749,
Subtask 12-22-27-640-064-B R
A. Lubrication of all Slat Rotary Actuators (Type B) Track 5 thru 16 WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-22-27 301-399, 401-449, 451-499, 701-749, SROS
Page 363 Jan 01/07
R R R R R R R R R R R R R R R
CAUTION : WHEN YOU DO A MAINTENANCE TASK THAT USES COMMON GREASE, OBEY _______ THESE PRECAUTIONS: - IF POSSIBLE, USE ONLY GREASES OF THE SAME SPECIFICATION TYPE (IT IS PERMITTED TO USE DIFFERENT BRANDS IF THE SPECIFICATION TYPE IS THE SAME). WE SPECIALLY RECOMMEND THAT YOU DO NOT MIX GREASES THAT HAVE CLAY THICKENERS WITH GREASES THAT HAVE LITHIUM THICKENERS. SUCH A MIXTURE CAN CHANGE THE LUBRICATION PROPERTIES OF THE GREASE. - IF YOU CANNOT OBEY THESE PRECAUTIONS AND YOU USE GREASES OF DIFFERENT TYPES (SPECIALLY THOSE WITH CLAY THICKENERS AND LITHIUM THICKENERS), DECREASE THE SERVICING INTERVALS (BY HALF, FOR EXAMPLE) SPECIFIED IN THE MAINTENANCE PLANNING DOCUMENT. DO THIS FOR APPROXIMATELY THREE OR FOUR SERVICES (REFER TO YOUR IN-SERVICE DATA TO FIND THE NUMBER OF SERVICES BEST ADAPTED TO AIRCRAFT).
R R R R
(1) Fill the quantity limiter (3) with the COMMON GREASE (Material No. 04-022), or the COMMON GREASE (Material No. 04-024), or the COMMON GREASE (Material No. 04-004). For the correct type of grease to use, refer to the SIL (Ref. SIL 12-008).
R R
NOTE : Step 1 is only applicable when you fill the quantity limiter ____ (3) and the hose (4) for the first time.
R R
NOTE : The hose (4), the quantity limiter (3) and the adapter (2) are ____ part of the QUANTITY LIMITER - REGREASING. (a) Remove the hose (4) from the quantity limiter (3). Connect the grease gun to the quantity limiter (3) on the same side as the piston. (b) Operate the grease gun until the piston of the quantity limiter (3) is at the opposite end of the chamber. (c) Make sure that the chamber of the quantity limiter (3) is full with grease. (d) Remove the grease gun from the quantity limiter (3). (e) Install the grease gun on the opposite side and connect the hose (4) to the quantity limiter (3). (f) Operate the grease gun until the piston of the quantity limiter (3) is at the opposite end of the chamber. (g) Make sure that the chamber of the quantity limiter (3) is full with grease.
R EFF : 002-049, 206-249, 301-399, 401-449, 12-22-27 451-499, 701-749, SROS
Page 364 Jan 01/07
(h) Make sure that the new grease comes out of the adapter (2). If not, do the steps (a) thru (g) again as necessary.
R
(i) Interchange the grease gun and the hose (4) at the quantity limiter (3). (2) Lubricate the Slat Rotary Actuator (a) Remove the plug (1) from the rotary actuator and install the adapter (2) on the rotary actuator. (b) Operate the grease gun until the piston of the quantity limiter (3) is at the opposite end of the chamber. (c) Remove the adapter (2) of the QUANTITY LIMITER - REGREASING from the rotary actuator. (d) Install the plug (1) on the rotary actuator. (e) TORQUE the plug (1) to between 0.4 and 0.6 m.daN (35.39 and 53.09 lbf.in). (f) Interchange the grease gun and the hose (4) at the quantity limiter (3). (g) Make sure that the chamber of the quantity limiter (3) is full with grease. R
(h) Do the steps (a) thru (g) again for each rotary actuator. **ON A/C ALL 5. Close-up ________ Subtask 12-22-27-410-068 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access 57-42-37-400-801): - In the Zone 522: - In the Zone 523: - In the Zone 622:
R R R
panels (Ref. TASK 57-41-37-400-801) and (Ref. TASK 522CB, 522TB, 522JB, 522LB, 522NB, 522RB 523CB, 523EB, 523GB, 523JB, 523LB, 523NB 622CB, 622TB, 622JB, 622LB, 622NB, 622RB
EFF : ALL 12-22-27 SROS
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R
- In the Zone 623: 623CB, 623EB, 623GB, 623JB, 623LB, 623NB. Subtask 12-22-27-865-079 B. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1CW, 2CW, 10CW. Subtask 12-22-27-860-081 C. Put the Aircraft back to its Initial Configuration (1) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever on panel 114VU. (2) Retract the slats (Ref. TASK 27-80-00-866-802). (3) Remove the access platform(s). (4) Remove the warning notice(s). (5) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-22-27 SROS
Page 366 Jan 01/07
TASK 12-22-27-640-810 Lubrication of Rudder Servo-Control Roller-Bearings (Rudder Side) WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Refer to the MPD TASK: 272400-06 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific 98F27207514000
circuit breaker(s) safety clip(s) warning notice(s) 1 ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE 1 PIN - RIGGING
EFF : ALL 12-22-27 R SROS
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B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 04-004 Material No. 19-003
USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 27-21-00-840-801 29-00-00-863-801 29-00-00-863-802 29-00-00-863-803 29-00-00-864-801 29-00-00-864-802 29-00-00-864-803 55-33-13-000-801 55-33-13-400-801 12-22-27-991-010
Energize the Aircraft Electrical Circuits from the External Power A Removal/Installation of the Control Rod on the Rudder Mechanical control Pressurize the Green Hydraulic System with the Electric Pump Pressurize the Blue Hydraulic System with the Electric Pump Pressurize the Yellow Hydraulic System with the Electric Pump Depressurize the Green Hydraulic System (Pressurized with the Electric Pump) Depressurize the Blue Hydraulic System (Pressurized with the Electric Pump) Depressurize the Yellow Hydraulic System (Pressurized with the Electric Pump) Removal of the Vertical-Stabilizer Trailing-Edge Access-Panels Installation of the Vertical-Stabilizer Trailing-Edge Access-Panels Fig. 310
EFF : ALL 12-22-27 R SROS
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3. __________ Job Set-up Subtask 12-22-27-869-050 A. To do this task outside the hangar during wind gusts, refer to the removal/installation of the control rod on the rudder mechanical control (Ref. TASK 27-21-00-840-801). Refer again to the above mentioned task to install the control rod at the end of this procedure. Subtask 12-22-27-010-069 B. Get Access (1) Put the ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE in position at the rudder leading-edge. (2) Remove the trailing-edge access-panels 325NL (Ref. TASK 55-33-13-000801). Subtask 12-22-27-860-071 C. Aircraft Maintenance Configuration (Ref. Fig. 310/TASK 12-22-27-991-010) (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) On the FLT CTL section of the overhead panel 241VU, make sure that the PRIM 1 and SEC 1 pushbutton switches are pushed (the OFF and FAULT legends of these pushbutton switches are off). (3) On the FLT CTL section of the overhead panel 212VU, make sure that the PRIM 2, PRIM 3 and SEC 2 pushbutton switches are pushed (the OFF and FAULT legends of these pushbutton switches are off). (4) Pressurize the aircraft hydraulic systems (Ref. TASK 29-00-00-863-801), (Ref. TASK 29-00-00-863-802) and (Ref. TASK 29-00-00-863-803). (5) Put the rudder pedals in the neutral position. (6) Make sure that the RUD TRIM control switch on the panel 115VU is set to the neutral position. (7) Make sure that the RUD TRIM indicator on the panel 115VU shows 0.
EFF : ALL 12-22-27 R SROS
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Rudder Servo Control Figure 310/TASK 12-22-27-991-010 EFF : ALL 12-22-27 R SROS
Page 370 Jan 01/07
(8) Install the PIN - RIGGING (98F27207514000) A in the bellcrank assembly of the servo control actuator 5002CY3. (9) Depressurize the aircraft hydraulic systems (Ref. TASK 29-00-00-864-801), (Ref. TASK 29-00-00-864-802) and (Ref. TASK 29-00-00-864-803). (10) Put the warning notice(s) in position in the cockpit to tell persons: - not to operate the flight controls, - not to pressurize the aircraft hydraulic systems. Subtask 12-22-27-865-076 D. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU FCPC3 STBY COM 7CE6 R20 721VU FCPC3 STBY MON 7CE5 R19 722VU FCDC 2 6CE2 T42 722VU FCSC 2 10CE2 T39 722VU FCPC 3 7CE3 V42 722VU FCPC 2 NORM 7CE2 V41 722VU FCPC 3 7CE4 V38 742VU FCSC 1 NORM 10CE1 C70 742VU FCPC 1 NORM 7CE1 C69 742VU FCSC 1 STBY 9CE G77 742VU FCPC 1 STBY 11CE K69 742VU FCDC 1 6CE1 L76 4. Procedure _________ (Ref. Fig. 310/TASK 12-22-27-991-010) Subtask 12-22-27-640-059 A. Lubrication of the Rudder Servo-Control Tailstock Roller-Bearings (Rudder Side) WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Clean the grease nipples with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003).
EFF : ALL 12-22-27 R SROS
Page 371 Jan 01/07
(2) Apply COMMON GREASE (Material No. 04-004) to the roller bearings through the grease nipples until the new grease comes out. (3) Remove the unwanted grease from the greasing points. 5. Close-up ________ Subtask 12-22-27-865-077 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CE1, 6CE2, 7CE1, 7CE2, 7CE3, 7CE4, 7CE5, 7CE6, 9CE, 10CE1, 10CE2, 11CE. Subtask 12-22-27-860-072 B. Put the Aircraft back to its Initial Configuration (1) Pressurize the Green hydraulic system (Ref. TASK 29-00-00-863-801). (2) On the FLT CTL section of the overhead panel 241VU, make sure that the PRIM 1 and SEC 1 pushbutton switches are pushed (the OFF and FAULT legends of these pushbutton switches are off). (3) Remove the PIN - RIGGING (98F27207514000) A from the bellcrank assembly of the servo control actuator 5002CY3. (4) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (5) Make sure that the work area is clean and clear of tools and other items. Subtask 12-22-27-410-063 C. Close Access (1) Install the trailing-edge access-panel 325NL (Ref. TASK 55-33-13-400801). (2) Remove the access platform(s). (3) Remove the warning notice(s).
EFF : ALL 12-22-27 R SROS
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TASK 12-22-27-640-811 Lubrication of the Aileron Actuator Roller Bearings WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Refer to the MPD TASK: 271400-05 NOTE : This Task is applicable only for aileron actuators which have ____ installed grease nipples at the actuator eye-end. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific 98D27903500000
circuit breaker(s) safety clip(s) 1 ACCESS PLATFORM 5M (16 FT) 1 WARNING NOTICE 2 PIN-SIDE STICK LOCKING
EFF : ALL 12-22-27 R SROS
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B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 04-004 Material No. 19-003
USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-804 12-22-27-991-011
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Fig. 311
3. __________ Job Set-up Subtask 12-22-27-860-073 A. Aircraft Maintenance Configuration (1) Make sure that the aircraft hydraulic systems are depressurized (Ref. TASK 29-00-00-864-804). (2) Put the WARNING NOTICE in position to tell persons: - not to pressurize the hydraulic systems, - not to pressurize the hydraulic reservoirs. (3) Install the PIN-SIDE STICK LOCKING in the capt and F/O side stick. (4) Put a warning notice in the cockpit to tell persons not to operate the flight controls.
EFF : ALL 12-22-27 R SROS
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Subtask 12-22-27-865-070 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU FCPC3 STBY COM 7CE6 R20 721VU FCPC3 STBY MON 7CE5 R19 722VU FCDC 2 6CE2 T42 722VU FCSC 2 10CE2 T39 722VU FCPC 3 7CE3 V42 722VU FCPC 2 NORM 7CE2 V41 722VU FCPC 3 7CE4 V38 742VU FCSC 1 NORM 10CE1 C70 742VU FCPC 1 NORM 7CE1 C69 742VU FCSC 1 STBY 9CE G77 742VU FCPC 1 STBY 11CE K69 742VU FCDC 1 6CE1 L76 Subtask 12-22-27-010-071 C. Get Access (1) Put the ACCESS PLATFORM 5M (16 FT) in position below the applicable aileron. (2) Remove the applicable access panels: - FOR 7CS1, 8CS1 remove 575AB, - FOR 7CS2, 8CS2 remove 675AB, - FOR 9CS1, 10CS1 remove 575CB, - FOR 9CS2, 10CS2 remove 675CB.
EFF : ALL 12-22-27 R SROS
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4. Procedure _________ (Ref. Fig. 311/TASK 12-22-27-991-011) Subtask 12-22-27-640-060 A. Lubrication of the Aileron Servo-Control Roller-Bearings WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Clean the grease nipples with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003). (2) Apply COMMON GREASE (Material No. 04-004) with maximum 10 Lbs/min. to the roller bearings through the grease nipples until the new grease comes out. (3) Remove the unwanted grease from the greasing points. 5. Close-up ________ Subtask 12-22-27-410-064 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the applicable access panels: - FOR 7CS1, 8CS1 install 575AB, - FOR 7CS2, 8CS2 install 675AB, - FOR 9CS1, 10CS1 install 575CB, - FOR 9CS2, 10CS2 install 675CB. (3) Remove the access platform(s). Subtask 12-22-27-865-071 B. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CE1, 6CE2, 7CE1, 7CE2, 7CE3, 7CE4, 7CE5, 7CE6, 9CE, 10CE1, 10CE2, 11CE.
EFF : ALL 12-22-27 R SROS
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ASC Roller Bearings Figure 311/TASK 12-22-27-991-011 EFF : ALL 12-22-27 R SROS
Page 377 Jan 01/07
Subtask 12-22-27-860-074 C. Remove the PIN-SIDE STICK LOCKING from the capt and F/O side stick.
EFF : ALL 12-22-27 R SROS
Page 378 Jan 01/07
TASK 12-22-27-640-813 Lubrication of Slat Steady Bearings WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Refer to the MPD TASK: 278000-06 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific 98D27803000000
circuit breaker(s) safety clip(s) 1 ACCESS PLATFORM 2M (6 FT) 1 WARNING NOTICE 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
EFF : ALL 12-22-27 R SROS
Page 379 Jan 01/07
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 04-022 Material No. 04-024 Material No. 19-003
USA MIL-PRF-81322 SYNTHE.HYDROCARBON GREASE HIGH PRESSURE (Ref. 20-31-00) AIB AIMS 09-06-001 SYNTHETIC GREASE FOR FLAP & SLAT MECHANISM (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 27-80-00-866-801 27-80-00-866-802 53-35-13-000-802 53-35-13-400-802 57-41-37-000-801 57-41-37-400-801 57-42-37-000-801 57-42-37-400-801 12-22-27-991-006-A
Energize the Ground Service Network De-energize the Ground Service Network Extension of the Slats on the Ground Retraction of the Slats on the Ground Removal of the Belly Fairing Access Panels Installation of the Belly Fairing Access Panels Removal of the Access Panels and Covers Installation of the Access Panels and Covers Removal of the Access Panels and Covers Installation of the Access Panels and Covers Fig. 306
3. __________ Job Set-up Subtask 12-22-27-860-075 A. Aircraft Maintenance Configuration (1) Fully extend the slats (Ref. TASK 27-80-00-866-801). (2) Put the WARNING NOTICE in position on panel 114VU to tell persons not to operate the flap/slat controls. (3) Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER on the flap/slat control lever on panel 114VU.
EFF : ALL 12-22-27 R SROS
Page 380 Jan 01/07
(4) Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-22-27-865-072 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM AVAIL 10CW X13 722VU SFCC 2 SLAT 2CW V40 742VU SFCC 1 SLAT 1CW L62 Subtask 12-22-27-010-073-A C. Get Access (1) Put the ACCESS PLATFORM 2M (6 FT) in position. (2) Remove the applicable access panels (Ref. TASK 53-35-13-000-802), (Ref. TASK 57-41-37-000-801) or (Ref. TASK 57-42-37-000-801): - FOR 5003CW, 5005CW remove 193DB, - FOR 5017CW remove 521BB, - FOR 5023CW remove 522AB, - FOR 5025CW remove 522BB, - FOR 5031CW remove 522HB, - FOR 5066CW remove 523CB, - FOR 5077CW remove 621BB, - FOR 5083CW remove 622AB, - FOR 5085CW remove 622BB, - FOR 5091CW remove 622HB, - FOR 5126CW remove 623CB.
EFF : ALL 12-22-27 R SROS
Page 381 Jan 01/07
4. Procedure _________ (Ref. Fig. 306/TASK 12-22-27-991-006-A) Subtask 12-22-27-640-061 A. Lubrication of the Slat Steady Bearings WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Clean the grease nipples with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003). (2) Apply COMMON GREASE (Material No. 04-022) or COMMON GREASE (Material No. 04-024) to the steady bearings through the grease nipples until the new grease comes out. (3) Remove the unwanted grease from the greasing points. 5. Close-up ________ Subtask 12-22-27-865-073 A. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1CW, 2CW, 10CW. Subtask 12-22-27-860-076 B. Put the Aircraft back to its Initial Configuration (1) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever on panel 114VU. (2) Retract the slats (Ref. TASK 27-80-00-866-802). (3) Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER on the flap/slat control lever on panel 114VU.
EFF : ALL 12-22-27 R SROS
Page 382 Jan 01/07
Subtask 12-22-27-410-066-A C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panel (Ref. TASK 53-35-13-400-802), (Ref. TASK 5741-37-400-801) or (Ref. TASK 57-42-37-400-801): - FOR 5003CW, 5005CW install 193DB, - FOR 5017CW install 521BB, - FOR 5023CW install 522AB, - FOR 5025CW install 522BB, - FOR 5031CW install 522HB, - FOR 5066CW install 523CB, - FOR 5077CW install 621BB, - FOR 5083CW install 622AB, - FOR 5085CW install 622BB, - FOR 5091CW install 622HB, - FOR 5126CW install 623CB. (3) Remove the warning notice(s). (4) Remove the access platform(s). (5) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL 12-22-27 R SROS
Page 383 Jan 01/07
Subtask 12-22-27-860-077 D. Put the Aircraft back to its Initial Configuration (1) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever on panel 114VU. (2) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-22-27 R SROS
Page 384 Jan 01/07
TASK 12-22-27-640-814 Lubrication of the Elevator Actuator Roller Bearings WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN _______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : - FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 TO 15 MINUTES. - GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. 1. __________________ Reason for the Job Refer to the MPD TASK: 273400-06 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific 98D27903500000
circuit breaker(s) safety clip(s) 1 ACCESS PLATFORM 6M (20 FT) 1 WARNING NOTICE 2 PIN-SIDE STICK LOCKING
EFF : ALL 12-22-27 R SROS
Page 385 Jan 01/07
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 04-004 Material No. 19-003
USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-804 55-13-11-000-801 55-13-11-400-801
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Removal of the Trailing-Edge Access Panels Installation of the Trailing-Edge Access Panels
**ON A/C ALL Post SB
27-3076 For A/C 001-049,201-210,251-252,255-299,301-399,401-449, 451-499,701-749,
12-22-27-991-012
Fig. 312
EFF : ALL 12-22-27 R SROS
Page 386 Jan 01/07
**ON A/C ALL 3. __________ Job Set-up **ON A/C ALL Post SB
27-3076 For A/C 001-049,201-210,251-252,255-299,301-399,401-449, 451-499,701-749,
Subtask 12-22-27-860-078 A. Aircraft Maintenance Configuration (1) Make sure that the aircraft hydraulic systems are depressurized (Ref. TASK 29-00-00-864-804). (2) Put the WARNING NOTICE in position to tell persons: - not to pressurize the hydraulic systems, - not to pressurize the hydraulic reservoirs. (3) Install the PIN-SIDE STICK LOCKING in the capt and F/O side stick. (4) Put a warning notice in the cockpit to tell persons not to operate the flight controls. Subtask 12-22-27-865-074 B. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU FCPC3 STBY COM 7CE6 R20 721VU FCPC3 STBY MON 7CE5 R19 722VU FCDC 2 6CE2 T42 722VU FCSC 2 10CE2 T39 722VU FCPC 3 7CE3 V42 722VU FCPC 2 NORM 7CE2 V41 722VU FCPC 3 7CE4 V38 742VU FCSC 1 NORM 10CE1 C70 742VU FCPC 1 NORM 7CE1 C69 742VU FCSC 1 STBY 9CE G77 742VU FCPC 1 STBY 11CE K69 742VU FCDC 1 6CE1 L76
EFF : ALL 12-22-27 R SROS
Page 387 Jan 01/07
Subtask 12-22-27-010-074 C. Get Access (1) Put the ACCESS PLATFORM 6M (20 FT) in position and open the trailing-edge access panels 334CB, 344CB (Ref. TASK 55-13-11-000801). **ON A/C ALL 4. Procedure _________ **ON A/C ALL Post SB
27-3076 For A/C 001-049,201-210,251-252,255-299,301-399,401-449, 451-499,701-749,
(Ref. Fig. 312/TASK 12-22-27-991-012) Subtask 12-22-27-640-062 A. Lubrication of the Elevator Servo-Control Roller-Bearings WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE _______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES. (1) Clean the grease nipples with a clean lint-free cloth MISCELLANEOUS (Material No. 19-003). (2) Apply COMMON GREASE (Material No. 04-004) with maximum 10 Lbs/min. to the roller bearings through the grease nipples until the new grease comes out. (3) Remove the unwanted grease from the greasing points.
EFF : ALL 12-22-27 SROS
Page 388 Jan 01/07
Elevator Actuator Roller-Bearings Figure 312/TASK 12-22-27-991-012 EFF : ALL 12-22-27 SROS
Page 389 Jan 01/07
**ON A/C ALL 5. Close-up ________ **ON A/C ALL Post SB
27-3076 For A/C 001-049,201-210,251-252,255-299,301-399,401-449, 451-499,701-749,
Subtask 12-22-27-410-067 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the trailing-edge access panel 334CB, 344CB (Ref. TASK 55-1311-400-801). (3) Remove the PIN-SIDE STICK LOCKING from the capt and F/O side stick. (4) Remove all the fixtures, tools, test and support equipment used during this procedure. Subtask 12-22-27-865-075 B. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CE1, 6CE2, 7CE1, 7CE2, 7CE3, 7CE4, 7CE5, 7CE6, 9CE, 10CE1, 10CE2, 11CE.
EFF : ALL 12-22-27 SROS
Page 390 Jan 01/07
LANDING GEAR - SERVICING ________________________ TASK 12-22-32-600-817 Lubrication of Main Landing Gear and Doors WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED ON THE _______ LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. R R R R R R R R R
WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL MATERIALS _______ ONLY WITH A GOOD FLOW OF AIR THROUGH THE WORK AREA. THESE MATERIALS ARE POISONOUS AND FLAMMABLE AND SKIN IRRITANTS. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. 1. __________________ Reason for the Job
R R
Refer to the MPD TASK: 321000-03 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No
specific specific specific specific
circuit breaker(s) safety clip(s) 1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE 1 LUBRICATING EQUIPMENT 1 WARNING NOTICE
EFF : ALL 12-22-32 SROS
Page 301 Jul 01/06
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 04-022 Material No. 05-047
USA MIL-PRF-81322 SYNTHE.HYDROCARBON GREASE HIGH PRESSURE (Ref. 20-31-00) C Z-11.904 ANTI COR. COMPOUND(HIGH TEMP.SILICONE SEALANT) (Ref. 20-31-00)
Material No. 11-024 Material No. 11-026 Material No. 19-003 Material No. 19-010
CLEANING AGENT, ALKALINE-WATERBASED. (Ref. 20-31-00) GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00) USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------1 1
O-ring O-ring
32-11-11 73 -070 32-11-11 73 -070A
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-801 R R R
32-00-00-860-804 32-00-00-860-805 32-12-00-010-801 32-12-00-410-801 12-22-32-991-037
Depressurize the Green Hydraulic System (Pressurized with the Electric Pump) Flight Configuration Precautions Ground Configuration after Flight Configuration Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Fig. 301
EFF : ALL 12-22-32 SROS
Page 302 Jul 01/06
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
**ON A/C 001-049, 201-210, 251-252, 255-299, 301-399, 401-449, 451-499,
R
12-22-32-991-005
R
**ON A/C ALL
R R R
Post SB
R
12-22-32-991-005-B
R
**ON A/C ALL
R R R
12-22-32-991-038 12-22-32-991-041 12-22-32-991-042
R
**ON A/C ALL
R
Post SB
R
12-22-32-991-042-A
R
**ON A/C ALL
R R
12-22-32-991-043 12-22-32-991-013
Post SB
Fig. 302
32-3125 For A/C 001-049,201-210,251-252,255-299,301-399,401-449, 451-499, 32-3141 For A/C ALL Fig. 302A
Fig. 303 Fig. 304 Fig. 305
32-3138 For A/C ALL Fig. 305A
Fig. 306 Fig. 307
3. __________ Job Set-up Subtask 12-22-32-941-067 A. Safety Precautions R (1) In the cockpit, on the panel 312VU: - make sure that the landing gear lever (6GA) is in the DOWN position - put a WARNING NOTICE in the cockpit to tell persons not to operate the landing gear lever.
EFF : ALL 12-22-32 SROS
Page 303 Jul 01/06
Subtask 12-22-32-860-078 B. Aircraft Maintenance Configuration (1) Make sure that the Green hydraulic system is depressurized (Ref. TASK 29-00-00-864-801). R R
(2) Do the flight configuration precautions (Ref. TASK 32-00-00-860-804). Subtask 12-22-32-865-068
R
C. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU HYD PUMP G CTL 9JV U09 722VU LGCIU 2 2GA U38 742VU LGCIU 1 1GA L63
R R R
Subtask 12-22-32-010-071 D. Get Access (Ref. Fig. 301/TASK 12-22-32-991-037)
R R
(1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position adjacent to the applicable MLG leg.
R
(2) Open the MLG doors (Ref. TASK 32-12-00-010-801).
R
(3) Remove and discard the lockwire from the bolts (5).
R
(4) Remove the bolts (5) and the washers (4).
R
(5) Remove the bracket (3) and the cover (2).
R
(6) Remove and discard the O-ring (1).
R
(7) Cut, remove and discard the lockwire from the bolts (6).
R
(8) Remove the bolts (6) and the cover (7).
R EFF : ALL 12-22-32 SROS
Page 304 Jul 01/06
R R
MLG-Greasing Point Access Figure 301/TASK 12-22-32-991-037
R EFF : ALL 12-22-32 SROS
Page 305 Jul 01/06
Subtask 12-22-32-110-054 E. Preparation of Equipment (1) Make sure that the LUBRICATING EQUIPMENT is in the correct condition before you use it. (2) Operate the LUBRICATING EQUIPMENT to make sure that the lines and adaptors are full of new lubricant. R R R
(3) Clean the greasers with the clean cloth MISCELLANEOUS (Material No. 19-003) and CLEANING AGENTS (Material No. 11-026). 4. Procedure _________
R R
**ON A/C 001-049, 201-210, 251-252, 255-299, 301-399, 401-449, 451-499, (Ref. Fig. 302/TASK 12-22-32-991-005)
R
**ON A/C ALL
R R R
Post SB
R R R
Post SB
32-3125 For A/C 001-049,201-210,251-252,255-299,301-399,401-449, 451-499, 32-3141 For A/C ALL
(Ref. Fig. 302A/TASK 12-22-32-991-005-B) **ON A/C ALL (Ref. Fig. 303/TASK 12-22-32-991-038, 304/TASK 12-22-32-991-041, 305/TASK 12-22-32-991-042)
R
**ON A/C ALL
R
Post SB
R R R
32-3138 For A/C ALL
(Ref. Fig. 305A/TASK 12-22-32-991-042-A) **ON A/C ALL (Ref. Fig. 306/TASK 12-22-32-991-043, 307/TASK 12-22-32-991-013)
R EFF : ALL 12-22-32 SROS
Page 306 Jul 01/06
R R
Shortening Mechanism - Lubrication Points Figure 302/TASK 12-22-32-991-005
EFF : 001-049, 201-210, 251-252, 255-299, 12-22-32 301-399, 401-449, 451-499, SROS
Page 307 Jul 01/06
R R
Shortening Mechanism - Lubrication Points Figure 302A/TASK 12-22-32-991-005-B
EFF : ALL 12-22-32 SROS
Page 308 Jul 01/06
INTENTIONALLY BLANK
R 12-22-32 SROS
Page 309 Jul 01/06
R R
MLG - Shortening Mechanism - Lubrication Points Figure 303/TASK 12-22-32-991-038- 12 (SHEET 1)
EFF : ALL 12-22-32 SROS
Page 310 Jul 01/06
R R
MLG - Shortening Mechanism - Lubrication Points Figure 303/TASK 12-22-32-991-038- 22 (SHEET 2)
EFF : ALL 12-22-32 SROS
Page 311 Jul 01/06
R
MLG Lubrication Points Location Figure 304/TASK 12-22-32-991-041- 16 (SHEET 1)
EFF : ALL 12-22-32 SROS
Page 312 Jan 01/07
R
MLG Lubrication Points Location Figure 304/TASK 12-22-32-991-041- 26 (SHEET 2)
EFF : ALL 12-22-32 SROS
Page 313 Jan 01/07
R
MLG Lubrication Points Location Figure 304/TASK 12-22-32-991-041- 36 (SHEET 3)
EFF : ALL 12-22-32 SROS
Page 314 Jan 01/07
R
MLG Lubrication Points Location Figure 304/TASK 12-22-32-991-041- 46 (SHEET 4)
EFF : ALL 12-22-32 SROS
Page 315 Jan 01/07
R
MLG Lubrication Points Location Figure 304/TASK 12-22-32-991-041- 56 (SHEET 5)
EFF : ALL 12-22-32 SROS
Page 316 Jan 01/07
R
MLG Lubrication Points Location Figure 304/TASK 12-22-32-991-041- 66 (SHEET 6)
EFF : ALL 12-22-32 SROS
Page 317 Jan 01/07
R R
MLG Greaser location Figure 305/TASK 12-22-32-991-042
EFF : ALL 12-22-32 SROS
Page 318 Jul 01/06
R R
MLG Greaser location Figure 305A/TASK 12-22-32-991-042-A
EFF : ALL 12-22-32 SROS
Page 319 Jul 01/06
R R
MLG Lubrication Points Location Figure 306/TASK 12-22-32-991-043
EFF : ALL 12-22-32 SROS
Page 320 Jul 01/06
INTENTIONALLY BLANK
R 12-22-32 SROS
Page 321 Jul 01/06
R
MLG Uplock, Door Uplock Units and Pins - Lubrication Points Figure 307/TASK 12-22-32-991-013- 12 (SHEET 1)
EFF : ALL 12-22-32 SROS
Page 322 Jan 01/07
R
MLG Uplock, Door Uplock Units and Pins - Lubrication Points Figure 307/TASK 12-22-32-991-013- 22 (SHEET 2)
EFF : ALL 12-22-32 SROS
Page 323 Jan 01/07
**ON A/C 001-049, 201-210, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 12-22-32-640-084 A. Lubrication of the MLG Shortening Mechanism -------------------------------------------------------------------| SHORTENING MECHANISM | |--------------------------------------------------------------------| | No.| Component/Location |Total| Position of Greasers | |----|--------------------|-----|------------------------------------| | 1 | Pintle Pin | 3 | 3 on the pin. | | | Connection | | | | | View A | | | |----|--------------------|-----|------------------------------------| | 2 | Adjustable Link | 3 | 2 on the body of the link | | | View B | | (Lubricate only one). | | | | | 1 on the adjustable links | | | | | spherical bearing eye-end and | | | | | bellcrank interface. | |----|--------------------|-----|------------------------------------| | 3 | Bellcrank | 3 | 2 on the bellcrank lever. | | | View C | | 1 on the bellcrank link bearing/ | | | | | bellcrank bearing joint. | |----|--------------------|-----|------------------------------------| | 4 | Bellcrank | 1 | 1 on the pivot pin. | |----|--------------------|-----|------------------------------------| | 5 | Link Sub-Assy | 2 | 2 on the link body. | | | View D | | | |----|--------------------|-----|------------------------------------| | 6 | Upper Link Pin | 4 | 2 on each end of the pivot pin | | | View E | | (Lubricate only one greaser on | | | | | each end of the pin). | |----|--------------------|-----|------------------------------------| | 7 | Upper Link | 4 | 4 on the link body | | | View E | | (Access through change over | | | | | valve access hole) | |----|--------------------|-----|------------------------------------| | 8 | Lower Link | 4 | 4 on the link body. | | | View E | | (Access through change over | | | | | valve access hole) | |----|--------------------|-----|------------------------------------| | 9 | Shock Absorber | 6 | 2 on each lug on the top surface | | | View F | | (Lubricate only one greaser on | | | | | each lug). | | | | | (Access through change over |
R R R
R R R R R R R R R R R R R R R R R R R R
R EFF : 001-049, 201-210, 251-252, 255-299, 12-22-32 301-399, 401-449, 451-499, SROS
Page 324 Jul 01/06
-------------------------------------------------------------------| SHORTENING MECHANISM | |--------------------------------------------------------------------| | No.| Component/Location |Total| Position of Greasers | |----|--------------------|-----|------------------------------------| | | | | valve access hole). | --------------------------------------------------------------------
R
(1) Lubricate the greasers with COMMON GREASE (Material No. 04-022) until the new grease comes out. Use the table above, to find the greasers. NOTE : The grease gun pressure must be less than 3000 psi (200 bar). ____ (2) Remove the unwanted grease. R R
(3) Clean the greasers with a clean cloth MISCELLANEOUS (Material No. 19003) and CLEANING AGENTS (Material No. 11-026). **ON A/C ALL Post SB
32-3125 For A/C 001-049,201-210,251-252,255-299,301-399,401-449, 451-499,
Subtask 12-22-32-640-084-A A. Lubrication of the MLG Shortening Mechanism -------------------------------------------------------------------| SHORTENING MECHANISM | |--------------------------------------------------------------------| | No.| Component/Location |Total| Position of Greasers | |----|--------------------|-----|------------------------------------| | 1 | Pintle Pin | 3 | 3 on the pin. | | | Connection | | | | | View A | | | |----|--------------------|-----|------------------------------------| | 2 | Adjustable Link | 3 | 2 on the body of the link | | | View B | | (Lubricate only one). | | | | | 1 on the adjustable links | | | | | spherical bearing eye-end and | | | | | bellcrank interface. | |----|--------------------|-----|------------------------------------| | 3 | Bellcrank | 4 | 2 on the bellcrank lever. | | | View C | | 1 on the bellcrank link bearing/ | | | | | bellcrank bearing joint. | | | | | 1 on the inboard bush in the main | | | | | fitting for the bellcrank. |
R R R
R R
EFF : ALL 12-22-32 SROS
Page 325 Jul 01/06
-------------------------------------------------------------------| SHORTENING MECHANISM | |--------------------------------------------------------------------| | No.| Component/Location |Total| Position of Greasers | |----|--------------------|-----|------------------------------------| |----|--------------------|-----|------------------------------------| | 4 | Bellcrank | 1 | 1 on the pivot pin. | |----|--------------------|-----|------------------------------------| | 5 | Link Sub-Assy | 2 | 2 on the link body. | | | View D | | | |----|--------------------|-----|------------------------------------| | 6 | Upper Link Pin | 4 | 2 on each end of the pivot pin | | | | | (Lubricate only one greaser on | | | | | each end of the pin). | |----|--------------------|-----|------------------------------------| | 7 | Upper Link | 4 | 4 on the link body. | | | View E | | (Access through change over | | | | | valve access hole). | | | | | | |----|--------------------|-----|------------------------------------| | 8 | Lower Link | 4 | 4 on the link body. | | | View E | | (Access through change over | | | | | valve access hole). | |----|--------------------|-----|------------------------------------| | 9 | Shock Absorber | 6 | 2 on each lug on the top surface | | | View F | | (Lubricate only one greaser on| | | | | | each lug). | | | | | (Access through change over | | | | | valve access hole). | --------------------------------------------------------------------
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(1) Lubricate the greasers with COMMON GREASE (Material No. 04-022) until the new grease comes out. Use the table above, to find the greasers. NOTE : The grease gun pressure must be less than 3000 psi (200 bar). ____ (2) Remove the unwanted grease. R R
(3) Clean the greasers with a clean cloth MISCELLANEOUS (Material No. 19003) and CLEANING AGENTS (Material No. 11-026).
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Page 326 Jul 01/06
R
**ON A/C ALL
R R R
Post SB
R
Subtask 12-22-32-640-084-B
R
Post SB
32-3125 For A/C 001-049,201-210,251-252,255-299,301-399,401-449, 451-499, 32-3141 For A/C ALL
A. Lubrication of the MLG Shortening Mechanism
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-------------------------------------------------------------------| SHORTENING MECHANISM | |--------------------------------------------------------------------| | No.| Component/Location |Total| Position of Greasers | |----|--------------------|-----|------------------------------------| | 1 | Pintle Pin | 3 | 3 on the pin. | | | Connection | | | | | View A | | | |----|--------------------|-----|------------------------------------| | 2 | Adjustable Link | 3 | 2 on the body of the link | | | View B | | (Lubricate only one). | | | | | 1 on the adjustable links | | | | | spherical bearing eye-end and | | | | | bellcrank interface. | |----|--------------------|-----|------------------------------------| | 3 | Bellcrank | 4 | 2 on the bellcrank body. | | | View C | | 1 on the bellcrank link bearing/ | | | | | bellcrank bearing joint. | | | | | 1 on the inboard bush in the main | | | | | fitting for the bellcrank. | |----|--------------------|-----|------------------------------------| | 4 | Bellcrank | 1 | 1 on the pivot pin. | |----|--------------------|-----|------------------------------------| | 5 | Link Sub-Assy | 2 | 2 on the link body. | | | View D | | | |----|--------------------|-----|------------------------------------| | 6 | Upper Link Pin | 4 | 2 on each end of the pivot pin | | | | | (Lubricate only one greaser on | | | | | each end of the pin). | |----|--------------------|-----|------------------------------------| | 7 | Upper Link | 4 | 4 on the link body | | | View E | | (Access through change over | | | | | valve access hole). | |----|--------------------|-----|------------------------------------| | 8 | Lower Link | 4 | 4 on the link body | | | View E | | (Access through change over. | | | | | valve access hole). |
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-------------------------------------------------------------------| SHORTENING MECHANISM | |--------------------------------------------------------------------| | No.| Component/Location |Total| Position of Greasers | |----|--------------------|-----|------------------------------------| |----|--------------------|-----|------------------------------------| | 9 | Shock Absorber | 6 | 2 on each lug on the top surface | | | View F | | (Lubricate only one greaser on | | | | | each lug) | | | | | (Access through change over. | | | | | valve access hole). | --------------------------------------------------------------------(1) Lubricate the greasers with COMMON GREASE (Material No. 04-022) until the new grease comes out. Use the table above, to find the greasers. NOTE : The grease gun pressure must be less than 3000 psi (200 bar). ____ (2) Remove the unwanted grease. (3) Clean the greasers with a clean cloth MISCELLANEOUS (Material No. 19003) and CLEANING AGENTS (Material No. 11-026). **ON A/C ALL Subtask 12-22-32-640-085-B R
B. Lubrication of Main Gear -------------------------------------------------------------------| No.| Component/Location|Total| Position of Greasers | |----|-------------------|-----|-------------------------------------| | 10 | Rear Pintle | 10 | | |10A | View A | | 3 on the pintle pin greaser insert. | |10B | View A | | 2 on the eccentric pin. | |10C | View A | | 3 on the turnbuckle link upper pin. | |10D | View A | | 2 on the main fitting bearing. | |----|-------------------|-----|-------------------------------------| | 11 | Forward Pintle | 8 | | |11A | View B | | 4 on the fwd bearing (only the 2 | | | | | inboard greasers need to be | | | | | lubricated). | |11B | View B | | 3 on the pin greaser insert. | |11C | View B | | 1 on the strut/actuator bracket. | |----|-------------------|-----|-------------------------------------| | 12 | Intermediate Link | 9 | |
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-------------------------------------------------------------------| No.| Component/Location|Total| Position of Greasers | |----|-------------------|-----|-------------------------------------| |12A | View C | | 1 on the retraction link. | |12B | View C | | 3 on the retraction link/retraction | | | | | bracket attachment pin. | |12C | View C,M | | 3 on the attachment pin at the rear | | | | | spar/retraction link. | |12D | View C | | 2 on the retraction link fitting | | | | | bearing. | |----|-------------------|-----|-------------------------------------| | 13 | Retraction | 7 | | | | Actuator | | | |13A | View D | | 2 on the actuator ram eye end/ | | | | | retraction link attachment pin. | |13B | View D | | 1 on the actuator ram eye end. | |13C | View D | | 1 on the actuator cylinder eye end. | |13D | View D | | 3 on the actuator cylinder/main leg | | | | | attachment pin. | |----|-------------------|-----|-------------------------------------| | 14 | Lock Stay/Actuator| 28 | | |14A | View E | | 2 on the upper attachment pin. | |14B | View E | | 3 on the upper lock stay connector | | | | | link. | |14C | View E | | 1 on the upper lock stay eye end. | |14D | View E | | 1 on the upper lock stay eye end. | |14E | View E,N | | 8 on the lower lock stay. | |14F | View E | | 4 on the link pivot. | |14G | View E | | 2 on the connecting link. | |14H | View E | | 1 on the actuator ram eye end. | |14I | View E | | 4 on the actuator cylinder eye end. | |14J | View W | | 2 on the link pivot bracket. | |----|-------------------|-----|-------------------------------------| | 15 | Side Stay Assembly| 27 | | |15A | View F,V | | 4 on the bearings of the side stay | | | | | fitting on the rear spar. | |15B | View F | | 2 on the lower cardan lubrication | | | | | spool. | |15C | View F | | 2 on the upper side stay at the | | | | | lock stay attachment pin. | |15D | View F,R | | 8 1 at each end of the springs. | |15E | View F,R | | 1 on the actuator attachment bracket| |15F | View F,P | | 8 4 on the upper and lower cardan | | | | | attachment pins. | |15G | View F,Q | | 2 on the upper and lower lock stay | | | | | connection pin. | |----|-------------------|-----|-------------------------------------|
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-------------------------------------------------------------------| No.| Component/Location|Total| Position of Greasers | |----|-------------------|-----|-------------------------------------| | 16 | Articulation Link | 22 | | | | Pitch Trimmer | | | |16A | View G | | 3 on the pitch trimmer/pivot link | | | | | attachment pin. | |16B | View G,S | | 1 on the pitch trimmer eye end. | |16C | View G | | 3 on the pivot pin/lower. | | | | | articulation link attachment pin. | |16D | View G | | 2 on the lower articulation link. | |16E | View G | | 3 on the lower articulation link/ | | | | | bogie attachment pin. | |16F | View G | | 4 2 on each end of the pitch trimmer| | | | | /main leg attachment pin. | |16G | View G | | 6 3 on each upper articulation link/| | | | | main leg attachment pin. | |----|-------------------|-----|-------------------------------------| | 17 | Shock Strut/ | 36 | | | | Bogie Beam | | | |17A | View H,U | | 2 on the shock strut/bogie beam | | | | | attachment. | |17A | View H,U | | 2 on the shock strut/brake rod | | | | | attachment. | |17B | View H | | 8 2 on each brake unit. | |17C | View H | | 2 on the bogie beam at the shock | | | | | strut /bogie beam attachment. | |17D | View H | | 2 on the lower torque link. | |17D | View H | | 2 on the lower torque link sleeve. | |17E | View H | | 2 on the torque link apex pin. | |17F | View H | | 2 on the upper torque link. | |17F | View H | | 2 on the upper torque link/main leg | | | | | attachment lugs. | |17G | View H,T | |12 3 on each brake rod. | R -------------------------------------------------------------------(1) Lubricate the greasers with COMMON GREASE (Material No. 04-022) until the new grease comes out. Use the table above, to find the greasers. NOTE : The grease pressure must be less than 3000 psi (207 bar). ____ (2) Remove the unwanted grease. (3) Clean the greasers with a clean cloth MISCELLANEOUS (Material No. 19003) and CLEANING AGENTS (Material No. 11-026).
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**ON A/C ALL Post SB
32-3138 For A/C ALL
Subtask 12-22-32-640-085-C R
B. Lubrication of Main Gear -------------------------------------------------------------------| No.| Component/Location|Total| Position of Greasers | |----|-------------------|-----|-------------------------------------| | 10 | Rear Pintle | 10 | | |10A | View A | | 3 on the pintle pin greaser insert. | |10B | View A | | 2 on the eccentric pin. | |10C | View A | | 3 on the turnbuckle link upper pin. | |10D | View A | | 2 on the main fitting bearing. | |----|-------------------|-----|-------------------------------------| | 11 | Forward Pintle | 8 | | |11A | View B | | 4 on the fwd bearing (only the 2 | | | | | inboard greasers need to be | | | | | lubricated). | |11B | View B | | 3 on the pin greaser insert. | |11C | View B | | 1 on the strut/actuator bracket. | |----|-------------------|-----|-------------------------------------| | 12 | Intermediate Link | 9 | | |12A | View C | | 1 on the retraction link. | |12B | View C | | 3 on the retraction link/retraction | | | | | bracket attachment pin. | |12C | View C,M | | 3 on the attachment pin at the rear | | | | | spar/retraction link. | |12D | View C | | 2 on the retraction link fitting | | | | | bearing. | |----|-------------------|-----|-------------------------------------| | 13 | Retraction | 7 | | | | Actuator | | | |13A | View D | | 2 on the actuator ram eye end/ | | | | | retraction link attachment pin. | |13B | View D | | 1 on the actuator ram eye end. | |13C | View D | | 1 on the actuator cylinder eye end. | |13D | View D | | 3 on the actuator cylinder/main leg | | | | | attachment pin. | |----|-------------------|-----|-------------------------------------| | 14 | Lock Stay/Actuator| 28 | | |14A | View E | | 2 on the upper attachment pin. | |14B | View E | | 3 on the upper lock stay connector | | | | | link. | |14C | View E | | 1 on the upper lock stay eye end. |
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-------------------------------------------------------------------| No.| Component/Location|Total| Position of Greasers | |----|-------------------|-----|-------------------------------------| |14D | View E | | 1 on the upper lock stay eye end. | |14E | View E,N | | 8 on the lower lock stay. | |14F | View E | | 4 on the link pivot. | |14G | View E | | 2 on the connecting link. | |14H | View E | | 1 on the actuator ram eye end. | |14I | View E | | 4 on the actuator cylinder eye end. | |14J | View W | | 2 on the link pivot bracket. | |----|-------------------|-----|-------------------------------------| | 15 | Side Stay Assembly| 27 | | |15A | View F,V | | 4 on the bearings of the side stay | | | | | fitting on the rear spar. | |15B | View F | | 2 on the lower cardan lubrication | | | | | spool. | |15C | View F | | 2 on the upper side stay at the | | | | | lock stay attachment pin. | |15D | View F,R | | 8 1 at each end of the springs. | |15E | View F,R | | 1 on the actuator attachment bracket| |15F | View F,P | | 8 4 on the upper and lower cardan | | | | | attachment pins. | |15G | View F,Q | | 2 on the upper and lower lock stay | | | | | connection pin. | |----|-------------------|-----|-------------------------------------| | 16 | Articulation Link | 22 | | | | Pitch Trimmer | | | |16A | View G | | 3 on the pitch trimmer/pivot link | | | | | attachment pin. | |16B | View G,S | | 1 on the pitch trimmer eye end. | |16C | View G | | 3 on the pivot pin/lower | | | | | articulation link attachment pin. | |16D | View G | | 2 on the lower articulation link. | |16E | View G | | 3 on the lower articulation link/ | | | | | bogie attachment pin. | |16F | View G | | 4 2 on each end of the pitch trimmer| | | | | /main leg attachment pin. | |16G | View G | | 6 3 on each upper articulation link/| | | | | main leg attachment pin. | |----|-------------------|-----|-------------------------------------| | 17 | Shock Strut/ | 44 | | | | Bogie Beam | | | |17B | View H,U | | 2 on the shock strut/bogie beam | | | | | attachment. | |17A | View H,U | | 2 on the shock strut/brake rod | | | | | attachment. | |17B | View H | |16 4 on each brake unit. |
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-------------------------------------------------------------------| No.| Component/Location|Total| Position of Greasers | |----|-------------------|-----|-------------------------------------| |17C | View H | | 2 on the bogie beam at the shock | | | | | strut /bogie beam attachment. | |17D | View H | | 2 on the lower torque link. | |17D | View H | | 2 on the lower torque link sleeve. | |17E | View H | | 2 on the torque link apex pin. | |17F | View H | | 2 on the upper torque link. | |17F | View H | | 2 on the upper torque link/main leg | | | | | attachment lugs. | |17G | View H,T | |12 3 on each brake rod. | R -------------------------------------------------------------------(1) Lubricate the greasers with COMMON GREASE (Material No. 04-022) until the new grease comes out. Use the table above, to find the greasers. NOTE : The grease pressure must be less than 3000 psi (207 bar). ____ (2) Remove the unwanted grease. (3) Clean the greasers with a clean cloth MISCELLANEOUS (Material No. 19003) and CLEANING AGENTS (Material No. 11-026). **ON A/C ALL Subtask 12-22-32-640-086 R R
C. Lubrication of the MLG Uplock, the Door Uplock Unit, the Door Hinges and Actuator -------------------------------------------------------------------| No.| Component/Location|Total| Position of Greasers | |----|-------------------|-----|-------------------------------------| | 18 | Main Door | 5 | | |18A | Actuator | | 2 1 on the upper and lower eye end. | | | | | NOTE: Do not apply grease to the | | | | | attachment bolt greasers. | |18B | Hinges | | 3 1 on each door hinge bolt. | |----|-------------------|-----|-------------------------------------| | 19 | MLG Uplock | 4 | | |19A | View A | | 2 on each side of the casing. | |----|-------------------|-----|-------------------------------------| | 20 | MLG Door Uplock | 4 | | |20A | View B | | 2 on each side of the casing. |
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-------------------------------------------------------------------| No.| Component/Location|Total| Position of Greasers | |----|-------------------|-----|-------------------------------------| |----|-------------------|-----|-------------------------------------| | 21 | Door Uplock Roller| 1 | | |21A | View D | | 1 on the roller attachment pin. | --------------------------------------------------------------------
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(1) Lubricate the greasers with COMMON GREASE (Material No. 04-022) until the new grease comes out of the vent holes. Use the table above to find the greasers (which are identified by a red washer): NOTE : The grease pressure must be less than 3000 psi (200 bar). ____ (2) Remove the unwanted grease. (3) Clean the greasers with a clean cloth MISCELLANEOUS (Material No. 19003) and CLEANING AGENTS (Material No. 11-026). (4) Apply a layer of COMMON GREASE (Material No. 04-022) by hand to the surface of the: - gear uplock roller (22) - door uplock roller (23). (5) Remove the unwanted grease. 5. Close-up ________ Subtask 12-22-32-410-068 A. Close Access (1) Install the new O-ring (1) on the cover (2). (2) Hold the cover (2) and the bracket (3) in position. (3) Install the washers (4) and the bolts (5). (4) Safety the bolts (5) with MISCELLANEOUS (Material No. 19-010). (5) Install the cover (7). (6) Install the bolts (6). (7) Safety the bolts (6) with MISCELLANEOUS (Material No. 19-010).
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(8) Use a clean cloth MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-024) to clean the interface of the cover (7) and the heads of the bolts (6). (9) Apply a continuous bead of SPECIAL MATERIALS (Material No. 05-047) on the interface of the cover (7) and a layer on the heads of the bolts (6). (10) Remove the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE. (11) Close the MLG doors (Ref. TASK 32-12-00-410-801). Subtask 12-22-32-865-069 B. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GA, 2GA, 9JV. Subtask 12-22-32-860-089 C. Aircraft Maintenance Configuration (1) Put the aircraft back to the correct (ground) condition (Ref. TASK 32-00-00-860-805). (2) Put the Aircraft back to its Initial Configuration Subtask 12-22-32-942-067 D. Removal of Equipment (1) Remove the access platform(s). (2) Remove the warning notice(s). (3) Remove all the fixtures, tools, test and support equipment used during this procedure.
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TASK 12-22-32-600-819 Lubrication of Nose Gear and Doors WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING : MAKE SURE THAT THE GROUND SAFETY LOCKS ARE CORRECTLY INSTALLED ON THE _______ NOSE GEAR AND DOORS. THIS PREVENTS UNWANTED MOVEMENT OF THE NLG AND NLG DOORS. WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL MATERIALS _______ ONLY WITH A GOOD FLOW OF AIR THROUGH THE WORK AREA. THESE MATERIALS ARE POISONOUS AND FLAMMABLE AND SKIN IRRITANTS. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. 1. __________________ Reason for the Job Refer to the MPD TASK: 322000-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific D23304000
circuit breaker(s) safety clip(s) 1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE 4 WARNING NOTICE 1 GROUNDLOCK PIN - NLG
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B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 04-022
USA MIL-PRF-81322 SYNTHE.HYDROCARBON GREASE HIGH PRESSURE (Ref. 20-31-00)
Material No. 11-026
GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
R Material No. 19-003
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-801 32-00-00-481-801 32-22-00-010-801 32-22-00-410-801 32-51-00-040-801 32-51-00-440-801 32-51-00-720-801 32-51-00-720-801 R R R
12-22-32-991-002 12-22-32-991-014 12-22-32-991-010
R
**ON A/C ALL
R
Post SB
R
12-22-32-991-010-A
R
**ON A/C ALL
R
12-22-32-991-036
Depressurize the Green Hydraulic System (Pressurized with the Electric Pump) Installation of the Safety Devices on the Landing Gears Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance Deactivation of the Nose Wheel Steering Reactivation of the Nose Wheel Steering Functional Test of the Nose Wheel Steering (NWS) with the Handwheel(s) Functional Test of the Nose Wheel Steering (NWS) with the Handwheel(s) (CMS Procedure) Fig. 308 Fig. 309 Fig. 310
32-3192 For A/C ALL Fig. 310A
Fig. 311
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3. __________ Job Set-up Subtask 12-22-32-941-066 A. Safety Precautions (1) Put the WARNING NOTICE on the steering handwheels and the rudder pedals to tell persons not to operate the nose wheel steering (NWS). (2) Install the GROUNDLOCK PIN - NLG (D23304000) in the NLG Lock Stay (Ref. TASK 32-00-00-481-801). (3) On the panel 312VU: - make sure that the landing gear lever (6GA) is in the DOWN position - put the WARNING NOTICE to tell persons not to operate the landing gear. Subtask 12-22-32-860-076 B. Aircraft Maintenance Configuration (1) Deactivate the (NWS) (Ref. TASK 32-51-00-040-801). (2) Make sure that the Green hydraulic system is depressurized (Ref. TASK 29-00-00-864-801). Subtask 12-22-32-865-066 C. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------722VU BSCU SYS 2 2GG U37 742VU BSCU SYS 1 1GG G62 Subtask 12-22-32-010-069 D. Get Access (1) Open the NLG doors (Ref. TASK 32-22-00-010-801). (2) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE adjacent to the NLG leg.
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Subtask 12-22-32-840-051 E. Preparation of the Lubrication Equipment (1) Make sure that the lubrication equipment is serviceable before you fill it. (2) Operate the lubrication equipment to make sure that the lines and the adaptors are full of new lubricant. (3) Clean the greasers with a cloth MISCELLANEOUS (Material No. 19-003) and CLEANING AGENTS (Material No. 11-026). 4. Procedure _________ Subtask 12-22-32-640-078 R
A. Lubrication of the Nose Gear (Ref. Fig. 308/TASK 12-22-32-991-002) -------------------------------------------------------------------| NOSE LANDING GEAR | |--------------------------------------------------------------------| | No.| Component/Location |Total| Position of Greasers | |----|--------------------|-----|------------------------------------| | 1 | Attachment Points | 7 | 2 on the structure at the trunnion | | | to A/C Structure | | bearings (1 each side). | | | | | 5 on the dragstay trunnion pin | | | | | (3 on one side, 2 on the other). | |----|--------------------|-----|------------------------------------| | 2 | Retraction | 7 | 1 on the actuator cylinder eye end.| | | Actuator | | 1 on the attachment pin to the leg.| | | | | 3 on the structure pin. | | | | | 2 on the actuator rod eye-end | |----|--------------------|-----|------------------------------------| | 3 | Upper Leg | 6 | 4 on the top of the trunnion pin | | | | | housing (2 each side). | | | | | 2 on the end of the trunnion pins | | | | | (1 each side). | |----|--------------------|-----|------------------------------------| | 4 | Downlock Actuator | 3 | 2 on the actuator lugs on the leg. | | | Attachment | | 1 on the actuator/locklink | | | | | attachment pin. | |----|--------------------|-----|------------------------------------| | 5 | Torque Links and | 13 | 2 on the lugs at the connection of |
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NLG - Lubrication Points Figure 308/TASK 12-22-32-991-002- 18 (SHEET 1)
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NLG - Lubrication Points Figure 308/TASK 12-22-32-991-002- 28 (SHEET 2)
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NLG - Lubrication Points Figure 308/TASK 12-22-32-991-002- 38 (SHEET 3)
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NLG - Lubrication Points Figure 308/TASK 12-22-32-991-002- 48 (SHEET 4)
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NLG - Lubrication Points Figure 308/TASK 12-22-32-991-002- 58 (SHEET 5)
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NLG - Lubrication Points Figure 308/TASK 12-22-32-991-002- 68 (SHEET 6)
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NLG - Lubrication Points Figure 308/TASK 12-22-32-991-002- 78 (SHEET 7)
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NLG - Lubrication Points Figure 308/TASK 12-22-32-991-002- 88 (SHEET 8)
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-------------------------------------------------------------------| NOSE LANDING GEAR | |--------------------------------------------------------------------| | No.| Component/Location |Total| Position of Greasers | |----|--------------------|-----|------------------------------------| | | Shock Absorber | | the upper torque link to the leg.| | | | | 3 on the upper torque link. | | | | | 4 on the lower torque link. | | | | | 2 on the lugs at the connection | | | | | of the lower torque link to the | | | | | shock absorber piston. | | | | | 2 on the lower bearing of the shock| | | | | absorber cylinder. | |----|--------------------|-----|------------------------------------| | 6 | Steering Actuators | 12 | 1 on each rod end of the steering | | | and Leg Flanges | | actuator. | | | | | 2 on the upper flange. | | | | | 4 on the steering actuator | | | | | attachment pins (2 each side). | | | | | 4 on the lower flange. | |----|--------------------|-----|------------------------------------| | 7 | Lock Links | 4 | 2 on the fork end. | | | | | 1 at the central pin. | | | | | 1 at the leg attachment pin. | |----|--------------------|-----|------------------------------------| | 8 | Drag Stay | 14 | 4 on the fork end of the upper | | | | | stay. | | | | | 3 on the leg attachment pin. | | | | | 2 on the dragstay/trunnion | | | | | attachment pin. | | | | | 3 on the lower stay. | | | | | 2 on apex pin. | --------------------------------------------------------------------
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R R R R R
(1) Lubricate the greasers with COMMON GREASE (Material No. 04-022) until the new grease comes out. Use the tables above, to find the greasers: NOTE : The grease pressure must be less than 3000 psi (206 bar). ____ (2) Remove the unwanted grease. R R
(3) Clean the greasers with a clean cloth MISCELLANEOUS (Material No. 19003) and CLEANING AGENTS (Material No. 11-026).
EFF : ALL 12-22-32 SROS
Page 348 Jul 01/06
Subtask 12-22-32-640-079 B. Lubrication of NLG Doors (Ref. Fig. 309/TASK 12-22-32-991-014) -------------------------------------------------------------------| NLG DOORS | |--------------------------------------------------------------------| | No.| Component/Location |Total| Position of Greasers | |----|--------------------|-----|------------------------------------| | 9 | Bracket | 2 | 1 on each bracket (in bay) | | | | | NOTE : Do not apply grease to the | | | | | attachment bolt greasers. | |----|--------------------|-----|------------------------------------| | 10 | Door Actuator | 2 | 1 on each eye-end (in bay). | |----|--------------------|-----|------------------------------------| | 11 | Door Actuator | 2 | 1 on each eye-end (on door). | |----|--------------------|-----|------------------------------------| | 12 | Forward Door Hinge | 2 | 1 on each bracket (on door). | | | | | - NOTE: Do not apply grease to | | | | | attachment bolt greaser. | |----|--------------------|-----|------------------------------------| | 13 | Forward Door Hinge | 2 | 1 on each door bracket (in bay) | |-------------------------|-----|------------------------------------| | 14 | Rear Door Strut | 4 | 1 on pivot assembly. | | | | | 1 on fitting assembly. | | | | | 2 on strut. | --------------------------------------------------------------------
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(1) lubricate the greasers with COMMON GREASE (Material No. 04-022) until the new grease comes out. Use the tables above to find the greasers. NOTE : The grease pressure must be less than 3000 psi (206 bar). ____ (2) Remove the unwanted grease. (3) Clean the greasers with a clean cloth MISCELLANEOUS (Material No. 19003) and CLEANING AGENTS (Material No. 11-026).
EFF : ALL 12-22-32 SROS
Page 349 Jan 01/07
NLG Doors - Lubrication Points Figure 309/TASK 12-22-32-991-014- 12 (SHEET 1)
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EFF : ALL 12-22-32 SROS
Page 350 Jul 01/06
NLG Doors - Lubrication Points Figure 309/TASK 12-22-32-991-014- 22 (SHEET 2)
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EFF : ALL 12-22-32 SROS
Page 351 Jul 01/06
Subtask 12-22-32-640-080 R R
C. Lubrication of Nose Landing Gear Rotating Sleeve (Ref. Fig. 310/TASK 12-22-32-991-010) -------------------------------------------------------------------| NWS ROTATING SLEEVE | |--------------------------------------------------------------------| | No.| Component/Location |Total| Position of Greasers | |----|--------------------|-----|------------------------------------| | 15 | NWS Rotating | 2 | 2 on the front face of | | | Sleeve | | the rotating sleeve. | --------------------------------------------------------------------
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(1) Clean the greasers with a clean cloth MISCELLANEOUS (Material No. 19003) and CLEANING AGENTS (Material No. 11-026).
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(2) Use the table above to find the location of the greasers: NOTE : The grease pressure must be less than 3000 psi (206.8427 bar). ____
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(3) Lubricate the rotating sleeve through the greasers with COMMON GREASE (Material No. 04-022) until new grease comes out. NOTE : A large amount of grease can come out of the lower part of the ____ rotating sleeve before grease comes out of the top witness holes.
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(4) Remove the unwanted grease.
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(5) Do a test of the nose wheel steering to distribute the grease in the rotating sleeve, (Ref. TASK 32-51-00-720-801) or (Ref. TASK 32-51-00720-801).
EFF : ALL 12-22-32 SROS
Page 352 Jul 01/06
NLG - Nose Wheel Steering - Rotating Sleeve - Lubrication Points Figure 310/TASK 12-22-32-991-010
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EFF : ALL 12-22-32 SROS
Page 353 Jul 01/06
R
**ON A/C ALL
R
Post SB
R
Subtask 12-22-32-640-080-A
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32-3192 For A/C ALL
C. Lubrication of Nose Landing Gear Rotating Sleeve (Ref. Fig. 310A/TASK 12-22-32-991-010-A)
R R R R R R R
-------------------------------------------------------------------| NWS ROTATING SLEEVE | |--------------------------------------------------------------------| | No.| Component/Location |Total| Position of Greasers | |----|--------------------|-----|------------------------------------| | 15 | NWS Rotating Sleeve| 4 | 4 on the rotating sleeve. | --------------------------------------------------------------------
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(1) Clean the greasers with a clean cloth MISCELLANEOUS (Material No. 19003) and CLEANING AGENTS (Material No. 11-026).
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(2) Use the table above to find the location of the greasers:
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NOTE : The grease pressure must be less than 3000 psi (206.8427 bar). ____
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(3) Lubricate the rotating sleeve through the greasers with COMMON GREASE (Material No. 04-022) until new grease comes out.
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NOTE : A large amount of grease can come out of the lower part of the ____ rotating sleeve before grease comes out of the top witness holes.
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(4) Remove the unwanted grease.
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(5) Do a test of the nose wheel steering to distribute the grease in the rotating sleeve, (Ref. TASK 32-51-00-720-801) or (Ref. TASK 32-51-00720-801).
EFF : ALL 12-22-32 SROS
Page 354 Jul 01/06
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NLG - Nose Wheel Steering - Rotating Sleeve - Lubrication Points Figure 310A/TASK 12-22-32-991-010-A
EFF : ALL 12-22-32 SROS
Page 355 Jul 01/06
**ON A/C ALL Subtask 12-22-32-640-081 D. Lubrication of all Gear Up-Locks, Door Up-Lock Units and Pins (Ref. Fig. 311/TASK 12-22-32-991-036) R
------------------------------------------------------------------| NLG UPLOCK, DOOR UPLOCK | | ------------------------------------------------------------------| | No.| Component/Location |Total| Position of Greasers | |----|--------------------|-----|-----------------------------------| | 16 | NLG Uplock | 4 | 2 on each side of the casing. | |----|--------------------|-----|-----------------------------------| | 19 | NLG Door Uplock | 2 | 1 on each door. | | | Fitting | | | |----|--------------------|-----|-----------------------------------| | 20 | NLG Door Uplock | 4 | 4 on the casing. | -------------------------------------------------------------------
R R R R R R R R R R
(1) Lubricate the greasers with COMMON GREASE (Material No. 04-022) until the new grease comes out of the vent holes. Use the table above to find the greasers (identified by a red washer): NOTE : The grease pressure must be less than 3000 psi (200 bar). ____ NOTE : Look at work step (4) for the parts on which you apply grease ____ with your hand. (2) Remove the unwanted grease. (3) Clean the greasers with a cloth MISCELLANEOUS (Material No. 19-003) and CLEANING AGENTS (Material No. 11-026). (4) Apply (by hand) COMMON GREASE (Material No. 04-022) to the external surface of: - the apex pin of the drag stay (17) - the NLG door uplock fitting (18) on each door. (5) Remove the unwanted grease.
EFF : ALL 12-22-32 SROS
Page 356 Jan 01/07
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NLG Uplock, Door Uplock Units and Pins - Lubrication Points Figure 311/TASK 12-22-32-991-036
EFF : ALL 12-22-32 SROS
Page 357 Jul 01/06
5. Close-up ________ Subtask 12-22-32-865-067 A. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GG, 2GG. Subtask 12-22-32-410-067 B. Close Access (1) Remove the adjustable access platform. (2) Close the NLG doors (Ref. TASK 32-22-00-410-801). Subtask 12-22-32-860-077 C. Reactivate the NWS (Ref. TASK 32-51-00-440-801). Subtask 12-22-32-942-066 D. Removal of Equipment (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 12-22-32 R SROS
Page 358 Jul 01/06
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TASK 12-22-32-640-801
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Lubrication of MLG Bogie Pivot Pin
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WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS.
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1. __________________ Reason for the Job
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Refer to the MPD TASK: 321000-04 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment
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------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
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No specific No specific
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1 LUBRICATING EQUIPMENT 1 WARNING NOTICE
B. Consumable Materials
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------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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Material No. 04-022 Material No. 11-026 Material No. 19-003
USA MIL-PRF-81322 SYNTHE.HYDROCARBON GREASE HIGH PRESSURE (Ref. 20-31-00) GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
EFF : ALL 12-22-32 SROS
Page 359 Jul 01/06
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-801 R
12-22-32-991-040
Depressurize the Green Hydraulic System (Pressurized with the Electric Pump) Fig. 312
3. __________ Job Set-up Subtask 12-22-32-941-072 A. Safety Precautions (1) In the cockpit, on the panel 312VU: - make sure that the landing gear lever (6GA) is in the DOWN position - put a WARNING NOTICE in the cockpit to tell persons not to operate the landing gear lever. (2) Make sure that the Green hydraulic system is depressurized (Ref. TASK 29-00-00-864-801). Subtask 12-22-32-110-056 B. Preparation of Equipment (1) Make sure that the LUBRICATING EQUIPMENT is in the correct condition before you use it. (2) Operate the LUBRICATING EQUIPMENT to make sure that the lines and adaptors are full of new lubricant. (3) Application of the cleaning agents: WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL _______ MATERIALS ONLY WITH A GOOD FLOW OF AIR THROUGH THE WORK AREA. THESE MATERIALS ARE POISONOUS AND FLAMMABLE AND SKIN IRRITANTS. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
EFF : ALL 12-22-32 SROS
Page 360 Jan 01/07
(a) Clean the greasers with a clean MISCELLANEOUS (Material No. 19003) and CLEANING AGENTS (Material No. 11-026). 4. Procedure _________ R
(Ref. Fig. 312/TASK 12-22-32-991-040) Subtask 12-22-32-640-104 A. Lubrication of MLG Bogie Pivot Pin ------------------------------------------------------------------| MLG BOGIE PIVOT PIN | |-------------------------------------------------------------------| | No.| Component/Location |Total| Position of Greasers | |----|--------------------|-----|-----------------------------------| | 1 | Bogie Beam | 2 | 1 each side at pivot point | |----|--------------------|-----|-----------------------------------| | 2 | Pivot Pin | 2 | 1 below each end of pivot pin | ------------------------------------------------------------------(1) Lubricate the greasers with COMMON GREASE (Material No. 04-022) until the new grease comes out. Use the table above to find the greasers. NOTE : The grease gun pressure must be less than 3000 psi (200 bar). ____ (2) Remove the unwanted grease. (3) Application of cleaning agents: WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL _______ MATERIALS ONLY WITH A GOOD FLOW OF AIR THROUGH THE WORK AREA. THESE MATERIALS ARE POISONOUS AND FLAMMABLE AND SKIN IRRITANTS. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. (a) Clean the greasers with the clean MISCELLANEOUS (Material No. 19003) and CLEANING AGENTS (Material No. 11-026). (4) Remove any unwanted grease that has come out from the joints.
EFF : ALL 12-22-32 SROS
Page 361 Jan 01/07
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MLG Bogie Pivot Pin - Lubrication Points Figure 312/TASK 12-22-32-991-040
EFF : ALL 12-22-32 SROS
Page 362 Jan 01/07
5. Close-up ________ Subtask 12-22-32-942-072 A. Removal of Equipment (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 12-22-32 R SROS
Page 363 Jan 01/07
R R R
CLG - Gear Uplock and Door Uplock Units and Pins and Door hinges - Lubrication Points Figure 313/TASK 12-22-32-991-008- 12 (SHEET 1) EFF : ALL Page 364 Jan 01/07 SROS
12-22-32
R R R
CLG - Gear Uplock and Door Uplock Units and Pins and Door hinges - Lubrication Points Figure 313/TASK 12-22-32-991-008- 22 (SHEET 2) EFF : ALL Page 365 Jan 01/07 SROS
12-22-32
DOORS - SERVICING _________________ TASK 12-22-52-600-801 Lubrication of the FWD Cargo-Compartment Door Hinge Arm Bearings, Locking Mechanism, Latching Mechanism and Interlock Mechanism 1. __________________ Reason for the Job Refer to the MPD TASK: 523100-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific No specific No specific No specific 98F52308279000
adjustable access platform brush circuit breaker(s) safety clip(s) grease gun lint-free cloth oil can 1 BAR - R/I ACTUATOR
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 03-001 Material No. 04-004
USA MIL-PRF-7870 MINERAL OIL (LOW TEMP) (Ref. 20-31-00) USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00)
EFF : ALL 12-22-52 SROS
Page 301 Jan 01/05
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------52-30-00-010-801 52-30-00-080-801 52-30-00-410-801 52-30-00-480-801 R R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 701-749, 12-22-52-991-001
R
Opening of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Removal of the Safety Support Equipment Closing of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Installation of the Safety Support Equipment
Fig. 301
**ON A/C 001-001, 201-202, 251-252, 401-449, 12-22-52-991-002
Fig. 302
**ON A/C 002-049, 203-249, 255-299, 301-399, 451-499, 701-749, 12-22-52-991-002-A R
Fig. 302A
**ON A/C 001-001, 201-202, 251-252, 401-449, 12-22-52-991-003
Fig. 303
**ON A/C 002-049, 203-249, 255-299, 301-399, 451-499, 701-749, 12-22-52-991-003-A R
Fig. 303A
**ON A/C 001-001, 201-202, 251-252, 401-449, 12-22-52-991-004
Fig. 304
**ON A/C 002-049, 203-249, 255-299, 301-399, 451-499, 701-749, 12-22-52-991-004-A
Fig. 304A
EFF : ALL 12-22-52 SROS
Page 302 Jul 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-22-52-991-010 R
Fig. 305
**ON A/C 001-001, 201-202, 251-252, 401-449, 12-22-52-991-016 12-22-52-991-017 12-22-52-991-018 12-22-52-991-019
Fig. Fig. Fig. Fig.
306 307 308 309
**ON A/C ALL 3. __________ Job Set-up Subtask 12-22-52-010-050 A. Get Access (1) Put the adjustable access platform in position below the closed FWD cargo-compartment door (referred to as cargo door). (2) Remove the access panels 132AR, 132BR, 132CR, 132DR, 132ER, 132FR, 132GR, 132HR, 132JR, 132KR, 132LR from the fuselage above the cargo door to get access to the door hinge arms. (3) Remove the access panels 821AR, 821BR, 821CR, 821DR from the cargo door to get access to the different door mechanism. (4) Open the cargo door to the vertical position (Ref. TASK 52-30-00-010801) and safety it with the BAR - R/I ACTUATOR (98F52308279000) (Ref. TASK 52-30-00-480-801). Subtask 12-22-52-865-050 B. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------5002VE CARGO DOOR CTL 1MJ A02
EFF : ALL 12-22-52 SROS
Page 303 Jul 01/05
4. Procedure _________ R
**ON A/C 001-001, 201-202, 251-252, 401-449, Subtask 12-22-52-640-050 A. Lubrication (Ref. Fig. 301/TASK 12-22-52-991-001, 302/TASK 12-22-52-991-002, 303/TASK 12-22-52-991-003, 304/TASK 12-22-52-991-004) NOTE : This procedure is applicable for door serial No. 1001 to 1252. ____ (1) Lubricate the door hinges (1) with COMMON GREASE (Material No. 04004). Use a grease gun. (2) Lubricate the door eccentric bushes (2) and the eccentric bolts with COMMON GREASE (Material No. 04-004). Use a grease gun and a brush. (3) Lubricate the door handle mechanism (3) and the handle flap mechanism (4) with OILS (Material No. 03-001), COMMON GREASE (Material No. 04004). Use a grease gun, an oil can and a brush. (4) Lubricate the door locking shaft (6), the interlock mechanism and the door latching shaft (5) with OILS (Material No. 03-001). Use an oil can. (5) Lubricate the door hook attachment bolts (7) and (8) with COMMON GREASE (Material No. 04-004). Use a grease gun. (6) Lubricate the universal joints (9) with OILS (Material No. 03-001). Use an oil can. (7) Lubricate the spring unit (10) and the link assembly (11) with OILS (Material No. 03-001). Use an oil can. (8) Remove the unwanted lubricant with a lint-free cloth.
EFF : ALL 12-22-52 SROS
Page 304 Jul 01/05
FWD Cargo-Compartment Door - Lubrication of Door Hinges and Lock Fittings Figure 301/TASK 12-22-52-991-001 R EFF : ALL 12-22-52 SROS
Page 305 Jul 01/99
Cargo-Compartment Doors - Lubrication - Door Serial No. 1001 to 1252 Figure 302/TASK 12-22-52-991-002 R EFF : 001-001, 201-202, 251-252, 401-449, 12-22-52 SROS
Page 306 Jul 01/05
INTENTIONALLY BLANK
R 12-22-52 SROS
Page 307 Jul 01/99
FWD Cargo-Compartment Door - Lubrication of Latching Mechanism Figure 302A/TASK 12-22-52-991-002-A12 (SHEET 1) R EFF : 002-049, 203-249, 255-299, 301-399, 12-22-52 451-499, 701-749, SROS
Page 308 Apr 01/04
FWD Cargo-Compartment Door - Lubrication of Latching Mechanism Figure 302A/TASK 12-22-52-991-002-A22 (SHEET 2) R EFF : 002-049, 203-249, 255-299, 301-399, 12-22-52 451-499, 701-749, SROS
Page 309 Apr 01/04
Cargo Compartment Doors - Lubrication - Door Serial No. 1001 to 1252 Figure 303/TASK 12-22-52-991-003 R EFF : 001-001, 201-202, 251-252, 401-449, 12-22-52 SROS
Page 310 Jul 01/05
INTENTIONALLY BLANK
R 12-22-52 SROS
Page 311 Jul 01/99
FWD Cargo-Compartment Door - Lubrication of Locking Mechanism Figure 303A/TASK 12-22-52-991-003-A12 (SHEET 1) R EFF : 002-049, 203-249, 255-299, 301-399, 12-22-52 451-499, 701-749, SROS
Page 312 Apr 01/04
FWD Cargo-Compartment Door - Lubrication of Locking Mechanism Figure 303A/TASK 12-22-52-991-003-A22 (SHEET 2) R EFF : 002-049, 203-249, 255-299, 301-399, 12-22-52 451-499, 701-749, SROS
Page 313 Apr 01/04
Cargo Compartment Doors - Lubrication - Door Serial No. 1001 to 1252 Figure 304/TASK 12-22-52-991-004 R EFF : 001-001, 201-202, 251-252, 401-449, 12-22-52 SROS
Page 314 Jul 01/05
R
**ON A/C 002-049, 203-249, 255-299, 301-399, 451-499, 701-749, Subtask 12-22-52-640-050-A A. Lubrication of the FWD Cargo Door NOTE : Use a grease gun, an oil can or a brush as required for the ____ lubrication procedure. (1) Lubricate the door hinge arms and the latch fittings as follows: (Ref. Fig. 301/TASK 12-22-52-991-001) (a) Lubricate the hinge bolt (1) with COMMON GREASE (Material No. 04004). (b) Lubricate the eccentric bushes (2) and the eccentric bolts (3) with COMMON GREASE (Material No. 04-004). (2) Lubricate the latching mechanism as follows: (Ref. Fig. 302A/TASK 12-22-52-991-002-A) (a) Lubricate the handle bolt (5), the hook bolt (9) and the bellcrank bolt (10) with COMMON GREASE (Material No. 04-004). (b) Apply COMMON GREASE (Material No. 04-004) to the mating surface of the catch hook (7). (c) Lubricate the push button (4) and the catch hook linkage (6) of the latching handle with OILS (Material No. 03-001). (d) Lubricate the cardan joints (11) of the torque tube assy with OILS (Material No. 03-001). (e) Lubricate the bearings of the latching shaft (8) with OILS (Material No. 03-001). (3) Lubricate the locking mechanism as follows: (Ref. Fig. 303A/TASK 12-22-52-991-003-A) (a) Lubricate the bearings of the locking handle (15) with OILS (Material No. 03-001). (b) Lubricate the bearings of the double lever shaft (12) with OILS (Material No. 03-001).
R EFF : 002-049, 203-249, 255-299, 301-399, 12-22-52 451-499, 701-749, SROS
Page 315 Apr 01/04
(c) Lubricate the bearings of the bellcrank shaft (14) with OILS (Material No. 03-001). (d) Lubricate the bearings of the rear locking shaft (17) and the joint fork assemblies (17) with OILS (Material No. 03-001). (e) Lubricate the universal joint bearings of the locking shafts (18) with OILS (Material No. 03-001). (f) Lubricate the upper and lower pins of the gas spring (13) with OILS (Material No. 03-001). (4) Lubricate the switch mechanism as follows: (Ref. Fig. 304A/TASK 12-22-52-991-004-A) (a) Lubricate the bearings of the support lever shaft (21) with OILS (Material No. 03-001). (b) Lubricate the upper and lower pins of the gas spring (22) with OILS (Material No. 03-001). (c) Lubricate the spring of the target lever (23) with OILS (Material No. 03-001). (5) Lubricate the interlock mechanism as follows: (Ref. Fig. 305/TASK 12-22-52-991-010) (a) Lubricate the mating surface of the integrated stop (27) (part of the fuselage latch fitting) with COMMON GREASE (Material No. 04004). (b) Lubricate the mating surface of the interlock lever (28) with OILS (Material No. 03-001). (c) Lubricate the bearings of the interlock shaft (29) with OILS (Material No. 03-001). (6) Remove the unwanted lubricant with a lint-free cloth.
R EFF : 002-049, 203-249, 255-299, 301-399, 12-22-52 451-499, 701-749, SROS
Page 316 Apr 01/04
FWD Cargo-Compartment Door - Lubrication of Switch Mechanism Figure 304A/TASK 12-22-52-991-004-A R EFF : 002-049, 203-249, 255-299, 301-399, 12-22-52 451-499, 701-749, SROS
Page 317 Apr 01/04
Lubrication of Interlock Mechanism Figure 305/TASK 12-22-52-991-010 R EFF : 002-049, 203-249, 255-299, 301-399, 12-22-52 451-499, 701-749, SROS
Page 318 Apr 01/04
R
**ON A/C 001-001, 201-202, 251-252, 401-449, Subtask 12-22-52-640-058 B. Lubrication of the FWD Cargo Door NOTE : This procedure is applicable for door serial No. 1253 and ____ subsequent. NOTE : Use a grease gun, an oil can or a brush as required for the ____ lubrication procedure. (1) Lubricate the door hinge arms and the latch fittings as follows: (Ref. Fig. 301/TASK 12-22-52-991-001) (a) Lubricate the hinge bolt (1) with COMMON GREASE (Material No. 04004). (b) Lubricate the eccentric bushes (2) and the eccentric bolts (3) with COMMON GREASE (Material No. 04-004). (2) Lubricate the latching mechanism as follows: (Ref. Fig. 306/TASK 12-22-52-991-016) (a) Lubricate the handle bolt (5), the hook bolt (9) and the bellcrank bolt (10) with COMMON GREASE (Material No. 04-004). (b) Apply COMMON GREASE (Material No. 04-004) to the mating surface of the catch hook (7). (c) Lubricate the push button (4) and the catch hook linkage (6) of the latching handle with OILS (Material No. 03-001). (d) Lubricate the cardan joints (11) of the torque tube assy with OILS (Material No. 03-001). (e) Lubricate the bearings of the latching shaft (8) with OILS (Material No. 03-001). (3) Lubricate the locking mechanism as follows: (Ref. Fig. 307/TASK 12-22-52-991-017) (a) Lubricate the bearings of the locking handle (15) with OILS (Material No. 03-001).
R EFF : 001-001, 201-202, 251-252, 401-449, 12-22-52 SROS
Page 319 Jul 01/05
Cargo Compartment Doors - Lubrication - Door Serial No. 1253 and subsequent Figure 306/TASK 12-22-52-991-016- 12 (SHEET 1) R EFF : 001-001, 201-202, 251-252, 401-449, 12-22-52 SROS
Page 320 Jul 01/05
Cargo Compartment Doors - Lubrication - Door Serial No. 1253 and subsequent Figure 306/TASK 12-22-52-991-016- 22 (SHEET 2) R EFF : 001-001, 201-202, 251-252, 401-449, 12-22-52 SROS
Page 321 Jul 01/05
Cargo Compartment Doors - Lubrication - Door Serial No. 1253 and subsequent Figure 307/TASK 12-22-52-991-017- 12 (SHEET 1) R EFF : 001-001, 201-202, 251-252, 401-449, 12-22-52 SROS
Page 322 Jul 01/05
Cargo Compartment Doors - Lubrication - Door Serial No. 1253 and subsequent Figure 307/TASK 12-22-52-991-017- 22 (SHEET 2) R EFF : 001-001, 201-202, 251-252, 401-449, 12-22-52 SROS
Page 323 Jul 01/05
(b) Lubricate the bearings of the double lever shaft (12) with OILS (Material No. 03-001). (c) Lubricate the bearings of the bellcrank shaft (14) with OILS (Material No. 03-001). (d) Lubricate the bearings of the rear locking shaft (17) and the joint fork assemblies (17) with OILS (Material No. 03-001). (e) Lubricate the universal joint bearings of the locking shafts (18) with OILS (Material No. 03-001). (f) Lubricate the upper and lower pins of the gas spring (13) with OILS (Material No. 03-001). (4) Lubricate the switch mechanism as follows: (Ref. Fig. 308/TASK 12-22-52-991-018) (a) Lubricate the bearings of the support lever shaft (21) with OILS (Material No. 03-001). (b) Lubricate the upper and lower pins of the gas spring (22) with OILS (Material No. 03-001). (c) Lubricate the bearings of the target lever (23) with OILS (Material No. 03-001). (5) Lubricate the interlock mechanism as follows: (Ref. Fig. 309/TASK 12-22-52-991-019) (a) Lubricate the mating surface of the integrated stop (27) (part of the fuselage stop fitting) with COMMON GREASE (Material No. 04004). (b) Lubricate the mating surface of the interlock lever (28) with OILS (Material No. 03-001). (c) Lubricate the bearings of the interlock shaft (29) with OILS (Material No. 03-001). (6) Remove the unwanted lubricant with a lint-free cloth.
R EFF : 001-001, 201-202, 251-252, 401-449, 12-22-52 SROS
Page 324 Jul 01/05
Cargo Compartment Doors - Lubrication - Door Serial No. 1253 and subsequent Figure 308/TASK 12-22-52-991-018 R EFF : 001-001, 201-202, 251-252, 401-449, 12-22-52 SROS
Page 325 Jul 01/05
FWD Cargo-Compartment Door Lubrication of Interlock Mechanism - Door Serial No. 1253 and subsequent Figure 309/TASK 12-22-52-991-019 R EFF : 001-001, 201-202, 251-252, 401-449, Page 326 Jul 01/05 SROS
12-22-52
**ON A/C ALL 5. Close-up ________ Subtask 12-22-52-410-050 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels 821AR, 821BR, 821CR, 821DR on the cargo door. (3) Remove the BAR - R/I ACTUATOR (Ref. TASK 52-30-00-080-801) and close the cargo door (Ref. TASK 52-30-00-410-801). (4) Install the access panels 132AR, 132BR, 132CR, 132DR, 132ER, 132FR, 132GR, 132HR, 132JR, 132KR, 132LR on the fuselage above the cargo door. (5) Remove the access platform(s).
EFF : ALL 12-22-52 R SROS
Page 327 Oct 01/99
TASK 12-22-52-600-802 R
Lubrication of the Telescopic Arm and Exterior Control Handle 1. __________________ Reason for the Job Refer to the MPD TASK: 521121-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
brush grease gun lint-free cloth
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 04-004 Material No. 04-017
USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) USA A-A-59173 SILICONE GREASE (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------52-10-00-010-801 52-10-00-410-801 12-22-52-991-005 12-22-52-991-006
Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door Fig. 310 Fig. 311
EFF : ALL 12-22-52 SROS
Page 328 Jul 01/06
3. __________ Job Set-up Subtask 12-22-52-010-051 A. Get Access (1) Open the passenger crew exit doors (Ref. TASK 52-10-00-010-801). 4. Procedure _________ R
(Ref. Fig. 310/TASK 12-22-52-991-005, 311/TASK 12-22-52-991-006) Subtask 12-22-52-640-051 A. Lubricating (1) Lubricate the door damper connection linkage (12) with COMMON GREASE (Material No. 04-004). Use a grease gun. (2) Lubricate the external door operating handle mechanism (13) with COMMON GREASE (Material No. 04-017). Use a brush. (3) Remove the unwanted lubricant with a lint-free cloth. 5. Close-up ________ Subtask 12-22-52-410-051 A. Close Access (1) Close the passenger crew exit doors (Ref. TASK 52-10-00-410-801). Subtask 12-22-52-942-051 B. Close Up (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL 12-22-52 SROS
Page 329 Oct 01/99
Doors - Lubrication Figure 310/TASK 12-22-52-991-005
R
EFF : ALL 12-22-52 SROS
Page 330 Oct 01/99
Doors - Lubrication Figure 311/TASK 12-22-52-991-006
R
EFF : ALL 12-22-52 SROS
Page 331 Oct 01/99
TASK 12-22-52-600-807 R
Lubrication of the Telescopic Arm and Exterior Control Handle 1. __________________ Reason for the Job Refer to the MPD TASK: 522200-03 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
brush grease gun lint-free cloth
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 04-004 Material No. 04-017
USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) USA A-A-59173 SILICONE GREASE (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------52-20-00-010-801 52-20-00-410-801 12-22-52-991-005 12-22-52-991-006
Opening of the Emergency Exit Door Closing of the Emergency Exit Door Fig. 310 Fig. 311
EFF : ALL 12-22-52 SROS
Page 332 Jul 01/06
3. __________ Job Set-up Subtask 12-22-52-010-056 A. Get Access (1) Open the emergency exit doors (Ref. TASK 52-20-00-010-801). 4. Procedure _________ Subtask 12-22-52-640-056 R
A. Lubricating (Ref. Fig. 310/TASK 12-22-52-991-005, 311/TASK 12-22-52-991-006) (1) Lubricate the door damper connection linkage (12) with COMMON GREASE (Material No. 04-004). Use a grease gun. (2) Lubricate the external door operating handle mechanism (13) with COMMON GREASE (Material No. 04-017). Use a brush. (3) Remove unwanted lubricant with a lint-free cloth. 5. Close-up ________ Subtask 12-22-52-410-056 A. Close Access (1) Close the emergency exit doors (Ref. TASK 52-20-00-410-801). Subtask 12-22-52-942-056 B. Close Up (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL 12-22-52 SROS
Page 333 Oct 01/99
TASK 12-22-52-600-803 Lubrication of the BULK Cargo-Compartment Door 1. __________________ Reason for the Job Refer to the MPD TASK: 523300-03 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
lint-free cloth
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 03-001 Material No. 04-004
USA MIL-PRF-7870 MINERAL OIL (LOW TEMP) (Ref. 20-31-00) USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------52-30-00-010-803 52-30-00-410-803 52-33-15-000-801 52-33-15-400-801 12-22-52-991-007
Opening of the BULK Cargo-Compartment Door Closing of the BULK Cargo-Compartment Door Removal of the Protection Lining Installation of the Protection Lining Fig. 312
EFF : ALL 12-22-52 SROS
Page 334 Jan 01/05
R
3. __________ Job Set-up
R
Subtask 12-22-52-010-052
R
A. Get Access
R R R
(1) Open the BULK cargo-compartment door (referred to as BULK door) (Ref. TASK 52-30-00-010-803) sufficiently to get access to the barrel lock assembly.
R R
(2) Safety the not fully opened BULK door with an applicable support device.
R R
(3) Remove the protection lining from the BULK door (Ref. TASK 52-33-15000-801).
R R R R
4. Procedure _________ (Ref. Fig. 312/TASK 12-22-52-991-007) Subtask 12-22-52-640-052 A. Lubrication
R
(1) Lubricate the universal joint (61) with OILS (Material No. 03-001).
R
(2) Lubricate the barrel lock (62) with OILS (Material No. 03-001).
R
(3) Lubricate the latch rod (63) with OILS (Material No. 03-001).
R
(4) Lubricate the catch assembly (64) with OILS (Material No. 03-001).
R
(5) Lubricate the handle rod (65) with OILS (Material No. 03-001).
R
(6) Lubricate the handle shaft (66) as follows:
R R
(a) Push the push button of the outer handle, so that the handle comes free of its recess.
R R
(b) Lubricate the handle shaft (66) with COMMON GREASE (Material No. 04-004).
R R
(c) Move the handle several times in and out to make sure that the shaft is sufficiently lubricated.
R
(7) Remove the unwanted grease and oil with a lint-free cloth.
EFF : ALL 12-22-52 SROS
Page 335 Apr 01/03
R R
BULK Cargo-Compartment Door - Lubrication Figure 312/TASK 12-22-52-991-007
EFF : ALL 12-22-52 SROS
Page 336 Apr 01/03
R
5. Close-up ________
R
Subtask 12-22-52-410-052
R
A. Close Access
R R
(1) Make sure that the work area is clean and clear of tools and other items.
R R
(2) Install the protection lining on the BULK door (Ref. TASK 52-33-15400-801).
R
(3) Make sure that the support device is removed.
R
(4) Close the BULK door (Ref. TASK 52-30-00-410-803).
R R
Subtask 12-22-52-942-052 B. Close-up
R R
(1) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL 12-22-52 SROS
Page 337 Apr 01/03
TASK 12-22-52-600-808 Lubrication of the AFT Cargo-Compartment Door Hinge Arm Bearings, Locking, Latching and Interlock Mechanism 1. __________________ Reason for the Job Refer to the MPD TASK: 523200-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific No specific No specific No specific 98F52308279000
adjustable access platform brush circuit breaker(s) safety clip(s) grease gun lint-free cloth oil can 1 BAR - R/I ACTUATOR
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 03-001 Material No. 04-004
USA MIL-PRF-7870 MINERAL OIL (LOW TEMP) (Ref. 20-31-00) USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00)
EFF : ALL 12-22-52 SROS
Page 338 Jan 01/05
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------52-30-00-010-801 52-30-00-080-801 52-30-00-410-801 52-30-00-480-801 R
**ON A/C 001-001, 201-202, 251-252, 401-449, 12-22-52-991-002 12-22-52-991-003 12-22-52-991-004
R R
Opening of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Removal of the Safety Support Equipment Closing of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Installation of the Safety Support Equipment
Fig. 302 Fig. 303 Fig. 304
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 701-749, 12-22-52-991-011
Fig. 313
**ON A/C 002-049, 203-249, 255-299, 301-399, 451-499, 701-749, 12-22-52-991-012 12-22-52-991-013 12-22-52-991-014 12-22-52-991-015 R
Fig. Fig. Fig. Fig.
314 315 316 317
**ON A/C 001-001, 201-202, 251-252, 401-449, 12-22-52-991-020 12-22-52-991-021 12-22-52-991-022 12-22-52-991-023
Fig. Fig. Fig. Fig.
318 319 320 321
EFF : ALL 12-22-52 SROS
Page 339 Jul 01/05
**ON A/C ALL 3. __________ Job Set-up Subtask 12-22-52-010-057 A. Get Access (1) Put the adjustable access platform in position below the closed AFT cargo-compartment door (referred to as cargo door). (2) Remove the access panels 152AR, 152BR, 152CR, 152DR, 152ER, 152FR, 152GR, 152HR, 152JR, 152KR, 152LR from the fuselage above the cargo door to get access to the door hinge arms. (3) Open the cargo door to the vertical position (Ref. TASK 52-30-00-010801) and safety it with the BAR - R/I ACTUATOR (98F52308279000) (Ref. TASK 52-30-00-480-801). (4) Remove the access panels 822AR, 822BR, 822CR, 822DR from the cargo door to get access to the different door mechanism. Subtask 12-22-52-865-053 B. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------5002VE CARGO DOOR CTL 1MJ A02 4. Procedure _________ R
**ON A/C 001-001, 201-202, 251-252, 401-449, Subtask 12-22-52-640-057 A. Lubrication (Ref. Fig. 302/TASK 12-22-52-991-002, 303/TASK 12-22-52-991-003, 304/TASK 12-22-52-991-004, 313/TASK 12-22-52-991-011) NOTE : This procedure is applicable for door serial No. 1001 to 1252. ____ (1) Lubricate the door hinges (31) with COMMON GREASE (Material No. 04004). Use a grease gun.
EFF : ALL 12-22-52 SROS
Page 340 Jul 01/05
AFT Cargo-Compartment Door Lubrication of Hinge Arms and Lock Fittings Figure 313/TASK 12-22-52-991-011
R
R EFF : ALL 12-22-52 SROS
Page 341 Apr 01/03
(2) Lubricate the door eccentric bushes (32) and the eccentric bolts (33) with COMMON GREASE (Material No. 04-004). Use a grease gun and a brush. (3) Lubricate the door handle mechanism (3) and the handle flap mechanism (4) with OILS (Material No. 03-001), COMMON GREASE (Material No. 04004). Use a grease gun, an oil can and a brush. (4) Lubricate the door locking schaft (6), the interlock mechanism and the door latching schaft (5) with OILS (Material No. 03-001). Use an oil can. (5) Lubricate the door hook attachment bolts (7) and (8) with COMMON GREASE (Material No. 04-004). Use a grease gun. (6) Lubricate the universal joints (9) with OILS (Material No. 03-001). Use an oil can. (7) Lubricate the spring unit (10) and the link assembly (11) with OILS (Material No. 03-001). Use an oil can. (8) Remove the unwanted lubricant with a lint-free cloth. **ON A/C 002-049, 203-249, 255-299, 301-399, 451-499, 701-749, Subtask 12-22-52-640-057-A A. Lubrication of the AFT Cargo Door NOTE : Use a grease gun, an oil can or a brush as required for the ____ lubrication procedure. (1) Lubricate the door hinge arms and the latch fittings as follows: (Ref. Fig. 313/TASK 12-22-52-991-011) (a) Lubricate the hinge bolt (31) with COMMON GREASE (Material No. 04-004). (b) Lubricate the eccentric bushes (32) and the eccentric bolts (33) with COMMON GREASE (Material No. 04-004). (2) Lubricate the latching mechanism as follows: (Ref. Fig. 314/TASK 12-22-52-991-012) (a) Lubricate the handle bolt (35), the hook bolt (39) and the bellcrank bolt (40) with COMMON GREASE (Material No. 04-004).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-22-52 301-399, 401-449, 451-499, 701-749, SROS
Page 342 Jul 01/05
(b) Apply COMMON GREASE (Material No. 04-004) to the mating surface of the catch hook (37). (c) Lubricate the push button (34) and the catch hook linkage (36) of the latching handle with OILS (Material No. 03-001). (d) Lubricate the cardan joints (41) of the torque tube assy with OILS (Material No. 03-001). (e) Lubricate the bearings of the latching shaft (38) with OILS (Material No. 03-001). (3) Lubricate the locking mechanism as follows: (Ref. Fig. 315/TASK 12-22-52-991-013) (a) Lubricate the bearings of the locking handle (45) with OILS (Material No. 03-001). (b) Lubricate the bearings of the double lever shaft (42) with OILS (Material No. 03-001). (c) Lubricate the bearings of the bellcrank shaft (44) with OILS (Material No. 03-001). R R
(d) Lubricate the bearings of the joint fork assemblies (47) with OILS (Material No. 03-001). (e) Lubricate the universal joints bearings of the locking shafts (48) with OILS (Material No. 03-001). (f) Lubricate the upper and lower pins of the gas spring (43) with OILS (Material No. 03-001). (4) Lubricate the switch mechanism as follows: (Ref. Fig. 316/TASK 12-22-52-991-014) (a) Lubricate the bearings of the support lever shaft (51) with OILS (Material No. 03-001). (b) Lubricate the upper and lower pins of the gas spring (53) with OILS (Material No. 03-001). (c) Lubricate the spring of the target lever (52) with OILS (Material No. 03-001).
EFF : 002-049, 203-249, 255-299, 301-399, 12-22-52 451-499, 701-749, SROS
Page 343 Jul 01/06
AFT Cargo-Compartment Door - Lubrication of Latching Mechanism Figure 314/TASK 12-22-52-991-012- 12 (SHEET 1) R EFF : 002-049, 203-249, 255-299, 301-399, 12-22-52 451-499, 701-749, SROS
Page 344 Apr 01/04
AFT Cargo-Compartment Door - Lubrication of Latching Mechanism Figure 314/TASK 12-22-52-991-012- 22 (SHEET 2) R EFF : 002-049, 203-249, 255-299, 301-399, 12-22-52 451-499, 701-749, SROS
Page 345 Apr 01/04
AFT Cargo-Compartment Door - Lubrication of Locking Mechanism Figure 315/TASK 12-22-52-991-013- 12 (SHEET 1) R EFF : 002-049, 203-249, 255-299, 301-399, 12-22-52 451-499, 701-749, SROS
Page 346 Apr 01/04
AFT Cargo-Compartment Door - Lubrication of Locking Mechanism Figure 315/TASK 12-22-52-991-013- 22 (SHEET 2) R EFF : 002-049, 203-249, 255-299, 301-399, 12-22-52 451-499, 701-749, SROS
Page 347 Apr 01/04
AFT Cargo-Compartment Door - Lubrication of Switch Mechanism Figure 316/TASK 12-22-52-991-014 R EFF : 002-049, 203-249, 255-299, 301-399, 12-22-52 451-499, 701-749, SROS
Page 348 Apr 01/04
(5) Lubricate the interlock mechanism as follows: (Ref. Fig. 317/TASK 12-22-52-991-015) (a) Lubricate the mating surface of the integrated stop (57) (part of the fuselage latch fitting ) with COMMON GREASE (Material No. 04004). (b) Lubricate the mating surface of the interlock lever (56) with OILS (Material No. 03-001). (c) Lubricate the bearings of the interlock shaft (58) with OILS (Material No. 03-001). (6) Remove the unwanted lubricant with a lint-free cloth. R
**ON A/C 001-001, 201-202, 251-252, 401-449, Subtask 12-22-52-640-059 B. Lubrication of the AFT Cargo Door NOTE : This procedure is applicable for door serial No. 1253 and ____ subsequent. NOTE : Use a grease gun, an oil can or a brush as required for the ____ lubrication procedure. (1) Lubricate the door hinge arms and the latch fittings as follows: (Ref. Fig. 313/TASK 12-22-52-991-011) (a) Lubricate the hinge bolt (31) with COMMON GREASE (Material No. 04-004). (b) Lubricate the eccentric bushes (32) and the eccentric bolts (33) with COMMON GREASE (Material No. 04-004). (2) Lubricate the latching mechanism as follows: (Ref. Fig. 318/TASK 12-22-52-991-020) (a) Lubricate the handle bolt (35), the hook bolt (39) and the bellcrank bolt (40) with COMMON GREASE (Material No. 04-004). (b) Apply COMMON GREASE (Material No. 04-004) to the mating surface of the catch hook (37).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-22-52 301-399, 401-449, 451-499, 701-749, SROS
Page 349 Jul 01/05
AFT Cargo-Compartment Door - Lubrication of Interlock Mechanism Figure 317/TASK 12-22-52-991-015 R EFF : 002-049, 203-249, 255-299, 301-399, 12-22-52 451-499, 701-749, SROS
Page 350 Apr 01/04
INTENTIONALLY BLANK
R 12-22-52 SROS
Page 351 Apr 01/03
AFT Cargo-Compartment Door - Lubrication Latching Mechanism - Door Serial No. 1253 and subsequent Figure 318/TASK 12-22-52-991-020- 12 (SHEET 1) R EFF : 001-001, 201-202, 251-252, 401-449, Page 352 Jul 01/05 SROS
12-22-52
AFT Cargo-Compartment Door - Lubrication Latching Mechanism - Door Serial No. 1253 and subsequent Figure 318/TASK 12-22-52-991-020- 22 (SHEET 2) R EFF : 001-001, 201-202, 251-252, 401-449, Page 353 Jul 01/05 SROS
12-22-52
(c) Lubricate the push button (34) and the catch hook linkage (36) of the latching handle with OILS (Material No. 03-001). (d) Lubricate the cardan joints (41) of the torque tube assy with OILS (Material No. 03-001). (e) Lubricate the bearings of the latching shaft (38) with OILS (Material No. 03-001). (3) Lubricate the locking mechanism as follows: (Ref. Fig. 319/TASK 12-22-52-991-021) (a) Lubricate the bearings of the locking handle (45) with OILS (Material No. 03-001). (b) Lubricate the bearings of the bellcrank shaft (44) with OILS (Material No. 03-001). (c) Lubricate the bearings of the double lever shaft (42) with OILS (Material No. 03-001). (d) Lubricate the bearings of the joint fork asssemblies (47) with OILS (Material No. 03-001). (e) Lubricate the universal joints bearings of the locking shafts (48) with OILS (Material No. 03-001). (f) Lubricate the upper and lower pins of the gas spring (43) with OILS (Material No. 03-001). (4) Lubricate the switch mechanism as follows: (Ref. Fig. 320/TASK 12-22-52-991-022) (a) Lubricate the bearings of the support lever shaft (51) with OILS (Material No. 03-001). (b) Lubricate the upper and lower pins of the gas spring (53) with OILS (Material No. 03-001). (c) Lubricate the spring of the target lever (52) with OILS (Material No. 03-001). (5) Lubricate the interlock mechanism as follows: (Ref. Fig. 321/TASK 12-22-52-991-023) (a) Lubricate the mating surface of the integrated stop (57) (part of the fuselage latch fitting) with OILS (Material No. 03-001).
R EFF : 001-001, 201-202, 251-252, 401-449, 12-22-52 SROS
Page 354 Jul 01/05
(b) Lubricate the mating surface of the interlock lever (56) with OILS (Material No. 03-001). (c) Lubricate the bearings of the interlock shaft (58) with OILS (Material No. 03-001). (6) Remove the unwanted lubricant with a lint-free cloth. **ON A/C ALL 5. Close-up ________ Subtask 12-22-52-410-057 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels 822AR, 822BR, 822CR, 822DR on the cargo door. (3) Remove the BAR - R/I ACTUATOR (Ref. TASK 52-30-00-080-801) and close the cargo door (Ref. TASK 52-30-00-410-801). (4) Install the access panels 152AR, 152BR, 152CR, 152DR, 152ER, 152FR, 152GR, 152HR, 152JR, 152KR, 152LR on the fuselage above the cargo door. (5) Remove the access platform(s).
R EFF : ALL 12-22-52 SROS
Page 355 Apr 01/03
AFT Cargo-Compartment Door - Lubrication of Locking Mechanism - Door Serial No. 1253 and subsequent Figure 319/TASK 12-22-52-991-021- 12 (SHEET 1) R EFF : 001-001, 201-202, 251-252, 401-449, Page 356 Jul 01/05 SROS
12-22-52
AFT Cargo-Compartment Door - Lubrication of Locking Mechanism - Door Serial No. 1253 and subsequent Figure 319/TASK 12-22-52-991-021- 22 (SHEET 2) R EFF : 001-001, 201-202, 251-252, 401-449, Page 357 Jul 01/05 SROS
12-22-52
AFT Cargo-Compartment Door - Lubrication of Switch Mechanisn - Door Serial No. 1253 and subsequent Figure 320/TASK 12-22-52-991-022 R EFF : 001-001, 201-202, 251-252, 401-449, Page 358 Jul 01/05 SROS
12-22-52
AFT Cargo-Compartment Door - Lubrication of Interlock Mechanism - Door Serial No. 1253 and subsequent Figure 321/TASK 12-22-52-991-023 R EFF : 001-001, 201-202, 251-252, 401-449, Page 359 Jul 01/05 SROS
12-22-52
TASK 12-22-52-600-809 Lubrication of the Slider Mechanism on all Pax/Crew and Emergency Exit Doors 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 04-004 R R
USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00)
Material No. 04-017A Material No. 15-004
SILICONE GREASE (Ref. 20-31-00) USA MIL-C-16173 GRADE 3 CORROSION PREVENTIVE COMPOUND (Ref. 20-31-00)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 25-62-41-000-801 25-62-41-400-801 52-10-00-010-801 52-10-00-860-801 52-10-00-860-802 52-20-00-010-801 52-20-00-860-801 52-20-00-860-802 CMM 521216 12-22-52-991-024
Energize the Ground Service Network De-energize the Ground Service Network Removal of the Escape Facilities Installation of the Escape Facilities Opening of the Passenger/Crew Door Special Precautions before Work on the Passenger/Crew Door Special Precautions after Work on the Passenger/Crew Door Opening of the Emergency Exit Door Special Precautions before Work on the Emergency Exit Door Special Precautions after Work on the Emergency Exit Door (for corrective action) Fig. 322
EFF : ALL 12-22-52 SROS
Page 360 Jul 01/05
3. __________ Job Set-up Subtask 12-22-52-861-050 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-22-52-010-058 B. Get Access WARNING : DO NOT OPEN THE PASSENGER/CREW DOORS WHILE THE RED WARNING _______ LIGHT FLASHES, IF THE RED WARNING LIGHT FLASHES, REMAINING PRESSURE COULD CAUSE DOOR TO OPEN SUDDENLY AND COULD: - KILL OR CAUSE SERIOUS INJURY TO PERSONS - CAUSE DAMAGE TO THE AIRCRAFT. CAUTION : DO NOT APPLY TEMPORARY PROTECTION ON THE OXYGEN SYSTEMS. _______ MAKE SURE THAT THE TEMPORARY PROTECTION DOES NOT GET : - ON COMPOSITE PARTS, CONTROL CABLES, PULLEYS, TEFLON BEARINGS, - ON LUBRICATED SURFACES, - IN DRAIN VALVES OR OTHER ORIFICES. TEMPORARY PROTECTION ON OR IN THESE PARTS CAN CAUSE DAMAGE. CAUTION : DO NOT OPEN THE DOOR IF THE WIND SPEED IS MORE THAN 40 KNOTS TO _______ PREVENT DAMAGE TO THE DOOR OR TO THE AIRCRAFT STRUCTURE. IF THE AIRCRAFT IS PUT INTO THE WIND THE MAXIMUM WIND SPEED CAN BE 50 KNOTS. R R
(1) Open the applicable passenger/crew door (Ref. TASK 52-10-00-010-801) or the emergency exit door (Ref. TASK 52-20-00-010-801).
R R
(2) Do the special precautions before you start work on the applicable door (Ref. TASK 52-10-00-860-801) or (Ref. TASK 52-20-00-860-801).
R R
(3) If necessary, remove the escape facilities (Ref. TASK 25-62-41-000801).
EFF : ALL 12-22-52 SROS
Page 361 Apr 01/05
4. Procedure _________ Subtask 12-22-52-640-060 A. Lubrication of the Slider Mechanism (Ref. Fig. 322/TASK 12-22-52-991-024) WARNING : MAKE SURE THE PERCUSSION LEVER OF THE DOOR DAMPER CYLINDER IS _______ IN THE DISARMED POSITION WITH THE SAFETY PIN INSTALLED. TO MAKE SURE THAT THE DOOR DOES NOT OPEN SUDDENLY. IF THE DOOR OPENS SUDDENLY IT CAN CAUSE INJURY AND OR DAMAGE. R R
(1) Close the applicable door and make sure that slide control handle stays in the DISARMED position. (2) Clean the component interface and/or the adjacent area.
R R
(3) Apply a layer of the COMMON GREASE (Material No. 04-004) to the mating surfaces of the sliders and the girt bar.
R R
NOTE : It is permitted to apply the COMMON GREASE (Material No. 04____ 017A) as an alternative to the COMMON GREASE (Material No. 04004). (4) Make sure that the applicable door is correctly closed and the slide control handle is in the ARMED position.
R
(5) Apply a layer of the STORAGE PRESERVATION (Material No. 15-004) as a spray to the spring guide and the pawl. (6) Operate the pawl to make sure that the slider mechanism operates correctly. (7) If the slider mechanism does not operate correctly, replace or repair the slider. (Ref. CMM 521216). 5. Close-up ________ Subtask 12-22-52-410-058 A. Close Access (1) Do the special precautions after work on the applicable door (Ref. TASK 52-10-00-860-802) or (Ref. TASK 52-20-00-860-802). (2) If necessary, install the escape facilities (Ref. TASK 25-62-41-400801).
EFF : ALL 12-22-52 SROS
Page 362 Jul 01/05
R
Lubrication of Slider Mechanism Figure 322/TASK 12-22-52-991-024
EFF : ALL 12-22-52 SROS
Page 363 Apr 01/05
R R
(3) Remove all the fixtures, tools, test and support equipment used during this procedure. Subtask 12-22-52-862-050 B. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-22-52 SROS
Page 364 Apr 01/05
FUSELAGE - SERVICING ____________________ TASK 12-22-53-600-801 Lubrication of the THS Hinge Line Bearings WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. 1. __________________ Reason for the Job Refer to the MPD TASK: 551600-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No
specific specific specific specific
circuit breaker(s) safety clip(s) warning notices access platform 6.0 m (19 ft. 8 in.) 1 GUN - GREASE
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R
Material No. 04-004 Material No. 19-003
USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
EFF : ALL 12-22-53 SROS
Page 301 Jul 01/04
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-804 R 12-22-53-991-001
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Fig. 301
3. __________ Job Set-up Subtask 12-22-53-864-050 A. Make sure that the Blue, Green and Yellow hydraulic systems are depressurized (Ref. TASK 29-00-00-864-804). Subtask 12-22-53-865-050 B. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------742VU FCPC 1 NORM 7CE1 C69 Subtask 12-22-53-941-050 C. Get Access (1) Put warning notices in position in the cockpit to tell persons: - not to pressurize the hydraulic systems, - not to operate the flight controls. (2) Put the access platform in position at the access door 313AL. (3) Open and safety the access door 313AL.
EFF : ALL 12-22-53 SROS
Page 302 Apr 01/03
4. ___________________ Servicing Procedure (Ref. Fig. 301/TASK 12-22-53-991-001) Subtask 12-22-53-640-050 A. Lubrication of the THS Hinge Line Bearings (1) Clean the grease nipples with a lint-free cotton cloth, MISCELLANEOUS (Material No. 19-003). (2) Do a check of the grease nipples for good condition. R
(3) Lubricate the bearings with the COMMON GREASE (Material No. 04-004) through the grease nipples with a GUN - GREASE. (4) Make sure that the new grease comes out of the bearings. (5) Remove the unwanted grease with a lint-free cotton cloth, MISCELLANEOUS (Material No. 19-003). 5. Close-up ________ Subtask 12-22-53-410-050 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access door 313AL. (3) Remove the access platform(s). (4) Remove the warning notice(s). Subtask 12-22-53-865-051 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 7CE1.
EFF : ALL 12-22-53 SROS
Page 303 Jul 01/04
R
Lubrication Points of the THS Bearings Figure 301/TASK 12-22-53-991-001
EFF : ALL 12-22-53 SROS
Page 304 Jul 01/04
TASK 12-22-53-600-802 Lubrication of the THS Upper and Lower Frame Attachment Bearings WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. 1. __________________ Reason for the Job Refer to the MPD TASK: 551600-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No
specific specific specific specific
circuit breaker(s) safety clip(s) 1 ACCESS PLATFORM 6M (20 FT) 1 GUN - GREASE 1 WARNING NOTICE
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R
Material No. 04-004 Material No. 19-003
USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
EFF : ALL 12-22-53 SROS
Page 305 Jul 01/04
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-804 R
12-22-53-991-002
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Fig. 302
3. __________ Job Set-up Subtask 12-22-53-864-051 A. Make sure that the Blue, Green and Yellow hydraulic systems are depressurized (Ref. TASK 29-00-00-864-804). Subtask 12-22-53-865-052 B. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------742VU FCPC 1 NORM 7CE1 C69 Subtask 12-22-53-941-051 C. Get Access (1) Put a WARNING NOTICE in position in the cockpit to tell persons: - not to pressurize the hydraulic systems, - not to operate the flight controls. (2) Put the ACCESS PLATFORM 6M (20 FT) in position at the access door 313AL. (3) Open and safety the access door 313AL.
EFF : ALL 12-22-53 SROS
Page 306 Jan 01/04
4. Procedure _________ (Ref. Fig. 302/TASK 12-22-53-991-002) Subtask 12-22-53-640-051 A. Lubrication of the THS Upper and Lower Frame Attachment Bearings R
(1) Clean the grease nipples with a clean cloth MISCELLANEOUS (Material No. 19-003). (2) Do a check of the grease nipples for good condition.
R R R
(3) Lubricate the bearings with the COMMON GREASE (Material No. 04-004) through the grease nipples with a GUN - GREASE.
R
(4) Make sure that the new grease comes out of the bearings.
R
(5) Remove the unwanted grease with a clean cloth MISCELLANEOUS (Material No. 19-003). 5. Close-up ________ Subtask 12-22-53-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access door 313AL. (3) Remove the access platform(s). (4) Remove the warning notice(s). Subtask 12-22-53-865-053 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 7CE1.
EFF : ALL 12-22-53 SROS
Page 307 Jul 01/04
R
Lubrication Points of the THS Bearings Figure 302/TASK 12-22-53-991-002
EFF : ALL 12-22-53 SROS
Page 308 Jul 01/04
STABILIZERS - SERVICING _______________________ TASK 12-22-55-600-802 Lubrication of the Rudder Bearing No. 6 1. __________________ Reason for the Job Refer to the MPD TASK: 272400-07 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
circuit breaker(s) safety clip(s)
R R
No specific No specific No specific
warning notices access platform 17.5 m (57 ft. 5 in.) 1 GUN - GREASE
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R R R
Material No. 04-004 Material No. 19-003
USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-00-00-864-804 55-33-13-000-801 55-33-13-400-801 12-22-55-991-002
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Removal of the Vertical-Stabilizer Trailing-Edge Access-Panels Installation of the Vertical-Stabilizer Trailing-Edge Access-Panels Fig. 301
EFF : ALL 12-22-55 SROS
Page 301 Jul 01/04
3. __________ Job Set-up Subtask 12-22-55-864-051 A. Make sure that the Blue, Green and Yellow hydraulic systems are depressurized (Ref. TASK 29-00-00-864-804). Subtask 12-22-55-865-052 B. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------742VU FCPC 1 NORM 7CE1 C69 Subtask 12-22-55-941-051 C. Get Access (1) Put warning notices in position in the cockpit to tell persons: - not to pressurize the hydraulic systems, - not to operate the flight controls. (2) Put the access platform in position at the vertical stabilizer. (3) Open and safety the access panel (Ref. TASK 55-33-13-000-801) 325PL. 4. Procedure _________ (Ref. Fig. 301/TASK 12-22-55-991-002) Subtask 12-22-55-640-051 A. Lubrication of the Rudder Hinge Bearing No. 6 R R
(1) Clean the grease nipple with a lint-free cotton cloth, MISCELLANEOUS (Material No. 19-003).
R R R
(2) Lubricate with the COMMON GREASE (Material No. 04-004) through the grease nipple with a GUN - GREASE.
R
(3) Make sure that the new grease comes out of the bearing.
R R
(4) Remove the unwanted grease with a lint-free cotton cloth, MISCELLANEOUS (Material No. 19-003).
EFF : ALL 12-22-55 SROS
Page 302 Jul 01/04
R R
Rudder Hinge Bearing No. 6 Figure 301/TASK 12-22-55-991-002
EFF : ALL 12-22-55 SROS
Page 303 Jul 01/00
5. Close-up ________ Subtask 12-22-55-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access panel 325PL (Ref. TASK 55-33-13-400-801). (3) Remove the ground support and maintenance equipment, the special and standard tools and all other items. (4) Remove the access platform(s). (5) Remove the warning notice(s). Subtask 12-22-55-865-053 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 7CE1.
EFF : ALL 12-22-55 R SROS
Page 304 Jul 01/00
WINDOWS - SERVICING ___________________ TASK 12-22-56-600-801 Servicing of the Sliding Windows 1. __________________ Reason for the Job This subject gives the procedure to clean and lubricate the mechanism of the sliding windows. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
brush clean and dry cloth
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 05-001 R
Material No. 11-003
USA SAE-AS8660 INSULATING AND SEALING GREASE SILICONE (Ref. 20-31-00) USA ASTM D 740 METHYL-ETHYL-KETONE (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-22-56-991-001
Fig. 301
EFF : ALL 12-22-56 SROS
Page 301 Oct 01/04
3. __________ Job Set-up Subtask 12-22-56-941-050 A. Get Access (1) Open the right and left sliding window. 4. Procedure _________ (Ref. Fig. 301/TASK 12-22-56-991-001) Subtask 12-22-56-615-050 A. Cleaning of the Rail and of the Locking System (1) Clean the rail and the locking system with a brush soaked in CLEANING AGENTS (Material No. 11-003). (2) Make dry with a clean and dry cloth. Subtask 12-22-56-640-050 B. Lubrication of the Rail and of the Locking System (Ref. Fig. 301/TASK 12-22-56-991-001) (1) Apply SPECIAL MATERIALS (Material No. 05-001) internally to the rails and to all the locking system. (2) Remove all the unwanted material from the rails. 5. Close-up ________ Subtask 12-22-56-942-050 A. Get Access (1) Close the right and the left sliding window. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 12-22-56 SROS
Page 302 Apr 01/98
Lubrication of the Sliding Windows Figure 301/TASK 12-22-56-991-001 EFF : ALL 12-22-56 SROS
Page 303 Apr 01/98
DRAINAGE - DESCRIPTION AND OPERATION ____________________________________ 1. _______ General This section gives the instructions to drain the air data system. It includes the topics below: 12-24-34, P. Block 301 AIR DATA
EFF : ALL 12-24-00 SROS
Page 1 Apr 01/98
HYDRAULIC POWER - SERVICING ___________________________ TASK 12-24-29-600-801 Servicing of the Leakage Recovery Tank (5230JM001, 5230JM002, 5230JM003) 1. __________________ Reason for the Job Refer to the MPD TASK: 291700-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
access platform 1.98 m (6 ft. 6 in.) container 5 l (1.3208 USgal)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-14-00-614-801 R 29-14-00-614-802 R 29-14-00-614-803 R 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 12-24-29-991-001
Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Depressurization of the Green Hydraulic Reservoir with Ground Equipment Depressurization of the Blue Hydraulic Reservoir with Ground Equipment Depressurization of the Yellow Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Fig. 301
EFF : ALL 12-24-29 SROS
Page 301 Jul 01/06
3. __________ Job Set-up Subtask 12-24-29-860-050 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801)
R
(2) Make sure that the hydraulic systems are depressurized and put them in the maintenance configuration. (Ref. TASK 29-00-00-864-804). (3) Depressurize the related hydraulic reservoir Depressurize the reservoir of the Green hydraulic system (Ref. TASK 29-14-00-614-801) Depressurize the reservoir of the Blue hydraulic system (Ref. TASK 29-14-00-614-802) Depressurize the reservoir of the Yellow hydraulic system (Ref. TASK 29-14-00-614-803) Subtask 12-24-29-010-050 B. Get Access (Ref. TASK 32-12-00-010-801) FOR 5230JM001 Open the right MLG door. FOR 5230JM002, 5230JM003 Open the left MLG door. (1) Put a access platform in position below the applicable tank. FOR 5230JM001 In zone 148. FOR 5230JM002 In zone 147. FOR 5230JM003 In zone 195
EFF : ALL 12-24-29 SROS
Page 302 Apr 01/04
4. Procedure _________ (Ref. Fig. 301/TASK 12-24-29-991-001) Subtask 12-24-29-020-050 A. Removal of the Leakage Recovery Tank (1) Disconnect the pipe (1). R
(2) Remove the tank (3) from its support (4). Subtask 12-24-29-680-050 B. Drain all the fluid from the tank. Put the hydraulic fluid into a container. 5. Close-up ________ Subtask 12-24-29-420-050 A. Installation of the Leakage Recovery tank. (1) Clean the component interface and/or the adjacent area. (2) Do a visual inspection of the component interface and/or the adjacent area. (3) Install the tank (3) on its support (4). (4) Hold the tank (3) and tighten the clamp (2). (5) Connect the pipe (1) to the tank. Subtask 12-24-29-860-051 B. Put the Aircraft back to its Initial Configuration (1) Pressurize the reservoirs of the Green, Blue and Yellow hydraulic system (Ref. TASK 29-14-00-614-804) (2) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
EFF : ALL 12-24-29 SROS
Page 303 Apr 01/04
R
Leakage Recovery Tank Figure 301/TASK 12-24-29-991-001
EFF : ALL 12-24-29 SROS
Page 304 Oct 01/01
Subtask 12-24-29-410-050 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Remove the access platform(s). R
(3) Close the applicable MLG door (Ref. TASK 32-12-00-410-801). FOR 5230JM001 Close the right MLG door. FOR 5230JM002, 5230JM003 Close the left MLG door.
R
EFF : ALL 12-24-29 SROS
Page 305 Jul 01/06
AIR DATA SYSTEM - SERVICING ___________________________ TASK 12-24-34-600-801 Draining of the Standby Static Pressure-Lines 1. __________________ Reason for the Job Remove water from the standby static pressure-lines. 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-24-34-991-001
Fig. 301
3. __________ Job Set-up Subtask 12-24-34-010-050 A. Find the static drain 133AL. 4. Procedure _________ (Ref. Fig. 301/TASK 12-24-34-991-001) Subtask 12-24-34-680-050 A. On the static drain 133AL push the drain valve (1) until the water in the standby static pressure-lines is eliminated. 5. Close-up ________ Subtask 12-24-34-410-050 A. Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 12-24-34 SROS
Page 301 Apr 01/98
Draining of the Standby Static Pressure-Lines Figure 301/TASK 12-24-34-991-001 EFF : ALL 12-24-34 SROS
Page 302 Apr 01/98
POTABLE WATER SYSTEM - MAINTENANCE PRACTICES ____________________________________________ TASK 12-24-38-680-801 Draining of the Potable Water System (with Electrical Power) WARNING : DO NOT DO WORK ON THE TOILET WASTE SYSTEM AND THE POTABLE WATER _______ SYSTEM AT THE SAME TIME. THIS WILL PREVENT CONTAMINATION OF THE POTABLE WATER SYSTEM. SUCH CONTAMINATION CAN BE DANGEROUS TO HEALTH. WARNING : BEFORE YOU DO WORK ON THE POTABLE WATER SYSTEM, CLEAN YOUR HANDS WITH _______ SOAP AND WATER. THIS WILL PREVENT INFECTION. (CONTAMINATION FROM TOILET WASTE IS DANGEROUS TO HEALTH). WARNING : MAKE SURE THAT THE EQUIPMENT YOU USE FOR THIS PROCEDURE IS CLEAN AND _______ APPROVED FOR THE POTABLE WATER SYSTEM. IF NOT IT CAN CAUSE CONTAMINATION OF THE POTABLE WATER SYSTEM. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R R R R R
No No No No
specific specific specific specific
1 1 1 1
ACCESS PLATFORM 1M (3 FT) ACCESS PLATFORM 2M (6 FT) CONTAINER 10 L(2 1/2 USGAL) HOSE - DRAIN
B. Consumable Materials
R R R
------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R
Material No. 19-003
USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
EFF : ALL 12-24-38 SROS
Page 201 Oct 01/01
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801
Energize the Ground Service Network De-energize the Ground Service Network
**ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, 701-749, 12-24-38-991-001-A
Fig. 201
**ON A/C 301-399, 12-24-38-991-001-B
Fig. 201A
**ON A/C ALL 3. __________ Job Set-up Subtask 12-24-38-861-050 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-24-38-865-050 B. Get access to the applicable 5000VE series panel(s). Then make sure that this(these) circuit breaker(s) is (are) closed.
R
------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------5005VE WATER SYSTEM QUANT IND 1MA E06 5005VE WATER SYSTEM DRAIN 1MP E05
EFF : ALL 12-24-38 SROS
Page 202 Jul 01/06
**ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, 701-749, Subtask 12-24-38-941-050 C. Put an ACCESS PLATFORM 1M (3 FT) in position at Zone 133, an ACCESS PLATFORM 1M (3 FT) in position at Zone 154 and an ACCESS PLATFORM 1M (3 FT) in position at Zone 164. Subtask 12-24-38-860-050 D. Aircraft Maintenance Configuration (1) Make sure that the potable water shutoff-valves in all lavatories are open. (2) Make sure that the potable water shutoff-valves in all wet galleys are open. Subtask 12-24-38-010-051 E. Get Access (1) Open the access doors 133BL, 154AR, 164AR. **ON A/C 301-399, Subtask 12-24-38-941-050-A C. Put an ACCESS PLATFORM 1M (3 FT) in position at Zone 133, an ACCESS PLATFORM 1M (3 FT) in position at Zone 153, an ACCESS PLATFORM 1M (3 FT) in position at Zone 154 and an ACCESS PLATFORM 2M (6 FT) in position at Zone 164. Subtask 12-24-38-860-050-A D. Aircraft Maintenance Configuration (1) Make sure that the potable water shutoff-valves in all lavatories are open. (2) Make sure that the potable water shutoff-valves in all wet galleys are open. (3) Make sure that the potable water shutoff-valve 5005MB is open.
EFF : 001-049, 201-249, 251-252, 255-299, 12-24-38 301-399, 401-449, 451-499, 701-749, R SROS
Page 203 Jan 01/06
Subtask 12-24-38-010-051-A E. Get Access (1) Open the access doors 133BL, 154AR, 164AR, 197JB. **ON A/C ALL 4. Procedure _________ **ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, 701-749, Subtask 12-24-38-680-050-A A. Drain the System (Ref. Fig. 201/TASK 12-24-38-991-001-A) (1) Connect the HOSE - DRAIN to: - the fill/drain nipple 26DV on the potable water service-panel, - the nipple assy 140DW on the FWD potable-water drain-panel, - the nipple assemblies 5255MB and 1400DW on the AFT potable-water drain-panel.
R R
(2) Turn the fill/drain control handle 5254MB on the potable-water service-panel to the DRAIN position. Then pull it out to the mechanical stop. NOTE : The drain-valve control lights 3MP and 6MP come on. ____ NOTE : Water drains from: ____ - the fill/drain nipple 26DV on the potable-water service-panel, - the nipple assy 140DW on the FWD potable-water drain-panel. NOTE : Operate all water faucets in the galleys and in the ____ lavatories, the coffee makers and the water heaters to drain them. NOTE : When the water level in the FWD potable water-tank is 5%: ____ - the control light 10MP comes on, - water will drain from the nipple assy 5255MB on the AFT potable-water drain-panel.
EFF : ALL 12-24-38 SROS
Page 204 Jul 01/06
(3) Close the drain valves. CAUTION : MAKE SURE THAT THE DRAIN VALVES STAY OPEN AFTER YOU DRAIN _______ THE SYSTEM. THIS PREVENTS DAMAGE TO THE SYSTEM IN FREEZING CONDITIONS. (a) If the outside temperature is less than 0 deg.C (32.00 deg.F) do not close the drain valves. (4) When the system is drained, push in the fill/drain control handle 5254MB on the potable water service-panel and turn it to the NORMAL position. NOTE : The drain-valve control lights 3MP, 6MP and 10MP go off. ____ (5) Disconnect the drain hoses from the drain ports. (6) Clean and dry the panels with a clean cloth MISCELLANEOUS (Material No. 19-003). (7) Install the cap on the fill/drain nipple 26DV of the potable water service-panel. **ON A/C 301-399, Subtask 12-24-38-680-050-B A. Drain the System (Ref. Fig. 201A/TASK 12-24-38-991-001-B) (1) Connect the HOSE - DRAIN to: - The fill/drain nipple 26DV on the potable-water service-panel, - The nipple assemblies 5255MB and 1400DW on the AFT potable-water drain-panel, - The nipple assy 141DW on the LD LAV potable-water drain-panel, - The nipple assy 140DW on the FWD potable-water drain-panel.
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(2) Turn the fill/drain control handle 5254MB on the potable-water service-panel to the DRAIN position. Then pull it out to the mechanical stop. NOTE : The drain-valve control lights 3MP, 14MP and 6MP come on. ____ NOTE : Water drains from: ____ - The fill/drain nipple 26DV on the potable-water service-panel,
EFF : 001-049, 201-249, 251-252, 255-299, 12-24-38 301-399, 401-449, 451-499, 701-749, SROS
Page 205 Jul 01/06
Potable Water Service Panels Figure 201/TASK 12-24-38-991-001-A13 (SHEET 1) R EFF : 001-049, 201-249, 251-252, 255-299, 12-24-38 401-449, 451-499, 701-749, SROS
Page 206 Jan 01/06
Potable Water Service Panels Figure 201/TASK 12-24-38-991-001-A23 (SHEET 2) R EFF : 001-049, 201-249, 251-252, 255-299, 12-24-38 401-449, 451-499, 701-749, SROS
Page 207 Jan 01/06
Potable Water Service Panels Figure 201/TASK 12-24-38-991-001-A33 (SHEET 3) R EFF : 001-049, 201-249, 251-252, 255-299, 12-24-38 401-449, 451-499, 701-749, SROS
Page 208 Jan 01/06
INTENTIONALLY BLANK
R 12-24-38 SROS
Page 209 Jan 01/06
Potable Water Service Panel Figure 201A/TASK 12-24-38-991-001-B14 (SHEET 1) R EFF : 301-399, 12-24-38 SROS
Page 210 Jan 01/06
Potable Water Service Panel Figure 201A/TASK 12-24-38-991-001-B24 (SHEET 2) R EFF : 301-399, 12-24-38 SROS
Page 211 Jan 01/06
Potable Water Service Panel Figure 201A/TASK 12-24-38-991-001-B34 (SHEET 3) R EFF : 301-399, 12-24-38 SROS
Page 212 Jan 01/06
Potable Water Service Panel Figure 201A/TASK 12-24-38-991-001-B44 (SHEET 4) R EFF : 301-399, 12-24-38 SROS
Page 213 Jan 01/06
- The nipple assy 141DW on the LD LAV potable water system, - The nipple assy 5250MB on the FWD potable-water drain-panel. NOTE : Operate all water faucets in the galleys and in the ____ lavatories, the coffee makers and the water heaters to drain them. NOTE : When the water level in the FWD potable water-tank is 5%: ____ - the control light 10MP comes on, - water will drain from the nipple assy 5255MB on the AFT potable-water drain-panel. (3) Close the drain valves. CAUTION : MAKE SURE THAT THE DRAIN VALVES STAY OPEN AFTER YOU DRAIN _______ THE SYSTEM. THIS PREVENTS DAMAGE TO THE SYSTEM IN FREEZING CONDITIONS. (a) If the outside temperature is less than 0 deg.C (32.00 deg.F) do not close the drain valves. (4) When the system is drained, push in the fill/drain control handle 5254MB on the potable water service-panel and turn it to the NORMAL position. NOTE : The drain-valve control lights 3MP, 6MP, 14MP and 10MP go off. ____ (5) Disconnect the drain hoses from the drain ports. (6) Clean and dry the panels with a clean cloth MISCELLANEOUS (Material No. 19-003). (7) Install the cap on the fill/drain nipple 26DV of the potable-water service-panel. **ON A/C 001-049, Subtask 12-24-38-680-052 B. Drain the Components WARNING : MAKE SURE THAT THE POTABLE WATER SYSTEM IS DEPRESSURIZED. A _______ PRESSURIZED SYSTEM CAN CAUSE INJURY TO PERSONS WHEN THEY DO WORK ON IT.
R EFF : 001-049, 301-399, 12-24-38 SROS
Page 214 Jan 01/06
(1) Galley Water-Heater NOTE : This procedure is the same for all the faucets of the galley ____ water heaters. (a) On the galley water-heater set the ON/OFF switch (2) to the OFF position. (b) Make sure that the water is not hot. (c) Put an applicable CONTAINER 10 L(2 1/2 USGAL) below the OPEN TO DRAIN connection (1) to collect the water. (d) On the galley water-heater open the OPEN TO DRAIN connection (1). (e) Let the water drain into the applicable container. (f) Close the OPEN TO DRAIN connection (1). NOTE : The connection has to be tight. Leaks are not permitted. ____ **ON A/C ALL 5. Close-up ________ **ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, 701-749, Subtask 12-24-38-410-050 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access doors 133BL, 154AR, 164AR. NOTE : Make sure that the latches are correctly locked and that the ____ door makes a continuous surface with the skin of the aircraft. NOTE : In freezing conditions, when the drain valves are opened ____ manually, you cannot close the access panels. (3) Remove the access platform(s).
R EFF : ALL 12-24-38 SROS
Page 215 Jan 01/06
**ON A/C 301-399, Subtask 12-24-38-410-050-A A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access doors 133BL, 154AR, 164AR, 197JB. NOTE : Make sure that the latches are correctly locked and that the ____ door makes a continuous surface with the skin of the aircraft. NOTE : In freezing conditions, when the drain valves are opened ____ manually, you cannot close the access panels. (3) Remove the access platform(s). **ON A/C ALL Subtask 12-24-38-862-050 B. De-energize the ground service network (Ref. TASK 24-42-00-862-801). Subtask 12-24-38-942-050 C. Remove the ground support and maintenance equipment, the special and standard tools and all other items.
R EFF : ALL 12-24-38 SROS
Page 216 Jan 01/06
TASK 12-24-38-680-802 Draining of the Potable Water System (without Electrical Power) 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
1 ACCESS PLATFORM 1M (3 FT) 1 CONTAINER 10 L(2 1/2 USGAL) 5 HOSE - DRAIN
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 19-003
USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
3. __________ Job Set-up **ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, 701-749, Subtask 12-24-38-941-051 A. Put an ACCESS PLATFORM 1M (3 FT) in position at Zone 133, an ACCESS PLATFORM 1M (3 FT) in position at Zone 154 and an ACCESS PLATFORM 1M (3 FT) in position at Zone 164.
R EFF : ALL 12-24-38 SROS
Page 217 Jan 01/06
Subtask 12-24-38-860-051 B. Aircraft Maintenance Configuration (1) Make sure that the potable water shut-off valves in all lavatories are open. (2) Make sure that the potable water shut-off valves in all wet galleys are open. Subtask 12-24-38-010-052 C. Get Access (1) Open the access doors 133BL, 154AR, 164AR. **ON A/C 301-399, Subtask 12-24-38-941-051-A A. Put an ACCESS PLATFORM 1M (3 FT) in position at Zone 133, an ACCESS PLATFORM 1M (3 FT) in position at Zone 153, an ACCESS PLATFORM 1M (3 FT) in position at Zone 154 and an ACCESS PLATFORM 1M (3 FT) in position at Zone 164. Subtask 12-24-38-860-051-A B. Aircraft Maintenance Configuration (1) Make sure that the potable water shut-off valves in all lavatories are open. (2) Make sure that the potable water shut-off valves in all wet galleys are open. (3) Make sure that the potable water shut-off valve 5005MB is open. Subtask 12-24-38-010-052-A C. Get Access (1) Open the access doors 133BL, 154AR, 164AR, 197JB.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-24-38 301-399, 401-449, 451-499, 701-749, SROS
Page 218 Jan 01/06
**ON A/C ALL 4. Procedure _________ **ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, 701-749, Subtask 12-24-38-680-051 A. Drain the System (1) Connect the HOSE - DRAIN to: - the fill/drain port on the potable water service-panel, - the drain ports on the aft potable-water drain-panel, - the drain port on the forward potable-water drain-panel. (2) Turn the fill/drain control handle 5254MB on the potable water service-panel to the DRAIN position. Then pull it out to the mechanical stop. (3) Turn the fill/drain control handle 5258MB on the aft potable-water drain-panel to the OPEN position. (4) Turn the filling line drain-handle 5259MB on the aft potable-water drain-panel to the OPEN position. (5) Turn the drain control handle on the forward potable-water drain-panel to the OPEN position. NOTE : Water will drain from: ____ - the fill/drain port on the potable water service-panel, - the filling-line drain port on the aft potable-water drain-panel, - the drain port on the forward potable-water drain-panel. (6) When the system is drained: CAUTION : MAKE SURE THAT THE DRAIN VALVES STAY OPEN AFTER YOU DRAIN _______ THE SYSTEM. THIS PREVENTS DAMAGE TO THE SYSTEM IN FREEZING CONDITIONS. - turn the control handles on the aft and forward potable-water drain-panels to the SHUT position, - push the control handle 5254MB on the potable water service-panel in and turn it to the NORMAL position.
R EFF : ALL 12-24-38 SROS
Page 219 Jan 01/06
(7) Disconnect the drain hoses from the drain ports. (8) Clean and dry the panels with a clean cloth MISCELLANEOUS (Material No. 19-003). (9) Install the cap on the fill/drain port of the service panel. **ON A/C 301-399, Subtask 12-24-38-680-051-A A. Drain the System (1) Connect the HOSE - DRAIN to: - The fill/drain port on the potable-water service-panel, - The drain ports on the AFT potable-water drain-panel, - The drain ports on the LD LAV potable-water drain-panel, - The drain port on the FWD potable-water drain-panel. (2) Turn the fill/drain control handle 5254MB on the potable-water service-panel to the DRAIN position. Then pull it out to the mechanical stop. (3) Turn the fill/drain control handle 5258MB on the AFT potable-water drain-panel to the OPEN position. (4) Turn the filling line drain-handle 5259MB on the AFT potable-water drain-panel to the OPEN position. (5) Turn the drain control handle on the LD LAV potable-water drain-panel to the OPEN position. (6) Turn the drain control handle on the FWD potable-water drain-panel to the OPEN position. NOTE : Water will drain from: ____ - The fill/drain port on the potable-water service-panel, - The filling-line drain port on the AFT potable-water drain-panel, - The drain port on the LD LAV potable-water drain-panel. - The drain port on the FWD potable-water drain-panel.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-24-38 301-399, 401-449, 451-499, 701-749, SROS
Page 220 Jan 01/06
(7) When the system is drained: CAUTION : MAKE SURE THAT THE DRAIN VALVES STAY OPEN AFTER YOU DRAIN _______ THE SYSTEM. THIS PREVENTS DAMAGE TO THE SYSTEM IN FREEZING CONDITIONS. - Turn the control handles on the AFT, LD LAV and FWD potable-water drain-panels to the SHUT position, - Push the control handle 5254MB on the potable water service-panel in and turn it to the NORMAL position. (8) Disconnect the drain hoses from the drain ports. (9) Clean and dry the panels with a clean cloth MISCELLANEOUS (Material No. 19-003). (10) Install the cap on the fill/drain port of the service panel. **ON A/C 001-049, Subtask 12-24-38-680-053 B. Drain the Components WARNING : MAKE SURE THAT THE POTABLE WATER SYSTEM IS DEPRESSURIZED. A _______ PRESSURIZED SYSTEM CAN CAUSE INJURY TO PERSONS WHEN THEY DO WORK ON IT. (1) Galley Water-Heater NOTE : This procedure is the same for all the faucets of the galley ____ water-heaters. (a) Make sure that the water is not hot. (b) Put an applicable container below the OPEN TO DRAIN connection (1) to collect the water. (c) On the galley water-heater open the OPEN TO DRAIN connection (1). (d) Let the water drain into the CONTAINER 10 L(2 1/2 USGAL). (e) Close the OPEN TO DRAIN connection (1). NOTE : The connection has to be tight. Leaks are not permitted. ____
R EFF : 001-049, 301-399, 12-24-38 SROS
Page 221 Jan 01/06
**ON A/C ALL 5. Close-up ________ **ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, 701-749, Subtask 12-24-38-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access doors 133BL, 154AR, 164AR. NOTE : Make sure that the latches are correctly locked and that the ____ door makes a continuous surface with the skin of the aircraft. NOTE : In freezing conditions, when the drain valves are opened ____ manually, you cannot close the access panels. (3) Remove the access platform(s). (4) Remove the ground support and maintenance equipment, the special and standard tools and all other items. **ON A/C 301-399, Subtask 12-24-38-410-051-A A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access doors 133BL, 154AR, 164AR, 197JB. NOTE : Make sure that the latches are correctly locked and that the ____ door makes a continuous surface with the skin of the aircraft. NOTE : In freezing conditions, when the drain valves are opened ____ manually, you cannot close the access panels. (3) Remove the access platform(s).
R EFF : ALL 12-24-38 SROS
Page 222 Jan 01/06
(4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : 301-399, 12-24-38 R SROS
Page 223 Jan 01/06
USE OF MANUAL MAGNETIC FUEL QUANTITY INDICATORS - DESCRIPTION AND OPERATION ___________________________________________________________________________ 1. General _______ The Manual Magnetic Indicators (MMIs) can be used to find the quantity of fuel in the tanks when the aircraft is on the ground. There are no MMIs in the trim tank. Thus this procedure cannot be used to calculate the quantity of fuel in the trim tank. Electrical power is not required to operate the MMIs. Before the MMIs are used it is necessary to read the indication on the aircraft attitude monitor (5000QT). Then, to find the quantity of fuel in the tanks it is necessary to use conversion tables and this data: - the MMI indications - the aircraft attitude-monitor indication - the specific gravity of the fuel. For the description and operation of the MMIs refer to 28-43-00. For the use of the MMIs refer to 12-11-28. R
**ON A/C 251-252, 701-749,
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Post SB
28-3078 For A/C 251-252,701-749,
1. General _______ The Manual Magnetic Indicators (MMIs) can be used to find the quantity of fuel in the tanks when the aircraft is on the ground. There are no MMIs in the trim tank. Thus this procedure cannot be used to calculate the quantity of fuel in the trim tank. Electrical power is not required to operate the MMIs. To find the quantity of fuel in the tanks it is necessary to use conversion tables and this data: - the MMI indications - the specific gravity of the fuel. For the description and operation of the MMIs refer to 28-43-00. For the use of the MMIs refer to 12-11-28.
EFF : ALL 12-28-00 SROS
Page 1 Jul 01/06
UNSCHEDULED SERVICING - DESCRIPTION AND OPERATION _________________________________________________ 1. General _______ This section gives the instructions related to the servicing operations for which no frequency is specified. It includes 12-31-00/P. 12-32-00/P. 12-33-00/P. 12-36-00/P.
the topics below: Block 001 AIRCRAFT PROTECTION Block 001 SAMPLING FOR ANALYSIS Block 001 PRE-CONDITIONING Block 001 SYSTEM LINE FLUSHING
EFF : ALL 12-30-00 SROS
Page 1 Apr 01/98
COLD WEATHER MAINTENANCE - AIRCRAFT PROTECTION - DESCRIPTION AND OPERATION __________________________________________________________________________ 1. General _______ A. Safe operation of aircraft in cold weather conditions raises specific problems. Aircraft downtime and delays in flight schedules caused by cold weather problems can be minimized by a program of preventive cold weather servicing. R R
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B. Procedures for cold weather servicing during cold weather must be developed by the operator. This servicing must meet their specific requirements based on: - their cold weather experience - the available equipment and materials - the climatic conditions existing at their bases C. This topic contains information to assist the operator in defining, developing, and implementing cold weather preventive maintenance procedures that will minimize aircraft downtime and improve the safe operating level of the aircraft in adverse climatic conditions. These procedures are: - 12-31-11,P. Block 201 ANTI-ICING PROTECTION - 12-31-12,P. Block 201 ICE AND SNOW REMOVAL. - 12-31-21,P. Block 201 AIR CONDITIONING. - 12-31-24,P. Block 201 ELECTRICAL POWER. - 12-31-25,P. Block 201 EQUIPMENT/FURNISHINGS. - 12-31-27,P. Block 201 FLIGHT CONTROLS. - 12-31-28,P. Block 201 FUEL. - 12-31-31,P. Block 201 INDICATING/RECORDING SYSTEMS AND NAVIGATION. - 12-31-32,P. Block 201 LANDING GEAR. - 12-31-35,P. Block 201 DEICING/ANTI-ICING OXYGEN SYSTEM. - 12-31-38,P. Block 201 WATER/WASTE. - 12-31-49,P. Block 201 AUXILIARY POWER UNIT. - 12-31-51,P. Block 201 STRUCTURE. - 12-31-52,P. Block 201 DOORS. - 12-31-71,P. Block 201 POWER PLANT. D. Cold Soak Definition The aircraft is in cold soak configuration when : - it is parked in cold weather (Outside Air Temperature (OAT) lower than 0 deg.C (32.00 deg.F)) and - there is no supply of power to the aircraft (no air conditioning).
EFF : ALL 12-31-00 SROS
Page 1 Oct 01/04
2. __________________________________ De-icing and Anti-icing Guidelines A. De-Icing and Anti-Icing Glossary (1) De-icing is a procedure to remove frost, ice, snow and slush from the aircraft surfaces. R R R R R R
(2) De-icing fluids are normally applied heated. Typical de-icing fluids are: - Heated water, - Newtonian fluids (ISO or SAE or AEA Type I), - Mixtures of water and Type I fluid, - Non-Newtonian fluid (ISO or SAE or AEA Type II or Type IV), - Mixtures of water and Type II or Type IV fluid.
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(3) Follow manufacturers guidelines to increase the temperature of de-icing and anti-icing fluids. De-icing and anti-icing fluids are not heated in tanks too many times or for long periods because: - the quantity of water in the fluids will decrease and - there will be a possible degradation of the fluid performance. For Type I fluids, water loss can cause unwanted aerodynamic effects. For Type II and Type IV fluids, thermal exposure and/or water loss can decrease fluid viscosity which causes lower holdover times. One or more of the conditions that follow can decrease fluid performance: - not much fluid used - trucks that do not operate with heating system on for extended periods of time, - high temperatures in fluid tanks, - high temperatures in water tanks which directly touch the fluid tanks (no insulation between tanks).
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(4) Anti-icing is a precautionary procedure which provides protection against the formation of frost or ice and snow accumulations on the treated surfaces of the aircraft for a limited period of time, the holdover time.
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(5) Anti-icing fluids are normally applied cold directly onto clean aircraft surfaces. Typical anti-icing fluids are: - Newtonian fluids (ISO or SAE or AEA type I), - Mixtures of water and Type I fluid, - Non-Newtonian fluids (ISO or SAE or AEA Type II or Type IV), - Mixtures of water and Type II or Type IV fluid.
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(6) Non-Newtonian Fluids (Type II or Type IV) have a viscosity that reduces with increased air flow over the fluid.
EFF : ALL 12-31-00 SROS
Page 2 Oct 01/04
(7) Newtonian Fluids (Type I) have a low viscosity that only changes with temperature. (8) Holdover time is the estimated time during which anti-icing fluids will prevent the formation of frost or ice and snow accumulations on the protected surfaces of the aircraft. The holdover time starts at the beginning of the anti-icing treatment. (9) De-/Anti-icing is a combination of the de-icing and the anti-icing procedures and is performed in one or two steps. (10) One step De-/Anti-icing is carried out with an anti-icing fluid, normally heated. The aircraft is de-iced and the fluid that remains on the aircraft gives limited anti-ice protection. (11) Two step De-icing/Anti-Icing, as inferred, comprises two completely separate steps : The first step is to de-ice the aircraft (remove frost, ice, slush and snow accumulations), then to immediately follow this with an anti-icing procedure. B. An aircraft performance certification is based upon that aircraft having an uncontaminated or clean structure. (1) Ice, snow and frost or combinations of them will disturb the airflow, affecting lift and drag. It also increases the aircraft weight. (2) The aircraft, and especially its surfaces that provide lift and stability, must be aerodynamically clean. If they are not, safe operation is not possible. (3) If the fuel temperature is below freezing point and the aircraft is subject to precipitation, clear ice may form on the wings (wing tank area), even if the outside temperature is as high as 15 deg.C (59.00 deg.F). (4) An aircraft that is ready for flight must not have ice, snow, slush or frost adhering to its critical flight surfaces (Wings, vertical and horizontal stabilizers and rudder). Thin hoarfrost is permitted on the upper surface of the fuselage. NOTE : Thin hoarfrost is usually a white crystalline deposit which ____ usually develops equally on external surfaces on cold nights without clouds; it is sufficiently thin that surface features (lines or markings) can be seen below it. NOTE : A frost layer less than 3 mm (1/8 in.) on the underside of the ____ wing, in the area of fuel tanks, is permitted without effect on take off performance if it is caused by cold fuel (low fuel temperature, OAT above freezing and high humidity). This note is not applicable in THS underside.
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EFF : ALL 12-31-00 SROS
Page 3 Jan 01/07
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(5) A contamination check of the aircraft must include all parts of the aircraft. You must do this visual inspection from a position which gives a clear view of all surfaces. Because collected clear ice is not always easily seen, we recommend that you inspect critical surfaces (wings, vertical and horizontal stabilizers and rudder) with your hands. (6) Weather conditions determine when the aircraft de-/anti-icing must be carried out. (7) During checks on the ground, electrical or mechanical ice-detectors must not replace physical checks. (8) If the aircraft arrives at the gate with the flaps/slats in a position other than fully retracted, you must inspect these flaps/slats, and if necessary de-ice before retraction.
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C. De-icing and/or Anti-icing Equipment and Materials (1) Type I Fluids Type I fluids are normally used for aircraft de-icing and have only a limited effect when used for anti-icing purposes. Type I fluids are normally used for aircraft de-icing. These fluids contain at least 80 % by volume of either : - Monoethylene-glycol - Diethylene-glycol - Monopropylene-glycol - or a mixture of these glycols. The other 20% comprise inhibitors to restrict corrosion and increase the flash-point together with water and wetting agents. These fluids show a low viscosity which only changes with temperatures. The freezing point of a water/glycol mixture will vary with the amount of water contained in the fluid. It must be noted that the lowest freezing point of concentrated TYPE I fluid will be approximately -10 deg.C (+14.00 deg.F) whereas the lowest temperature protection will be found with a mixture of 60%/40% TYPE I fluid to water mixture whose freezing point will be below -50 deg.C (-58.00 deg.F) Also due to the lower viscosity, it flows off the wing more easily. Therefore a 50/50 mixture of TYPE I fluids to water is normally used. R
(2) Type II or Type IV fluids contain at least 50% by volume of either : - Monoethylene-glycol - Diethylene-glycol - Monopropylene-glycol - or a mixture of these glycols. The other 50% comprise :
EFF : ALL 12-31-00 SROS
Page 4 Oct 01/04
- inhibitors to restrict corrosion and increase the flash-point - water and wetting agents to allow the fluid to form a uniform film over the aircraft surfaces - thickening agents to enable the fluid to adhere to the aircraft surfaces for longer periods. Type II or Type IV fluids have a longer holdover time than type I fluid. (3) Fluid dilution Type I, Type II and Type IV fluids can be diluted with water. This may be done if due to weather conditions there are no requirements for a long conservation time or the higher freezing points are sufficient for the climatic conditions present.
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(4) Holdover times Holdover times are the estimated times that the applied anti-icing fluid will prevent the formation of frost, ice and the accumulation of snow on the protected surfaces of an aircraft. When applying the first step de/anti-icing process, the holdover time is from the start of the de/anti-icing application and when applying the second step de/anti-icing process, the holdover time is from the start of the anti-icing application. The holdover times given are for general information only. The indicated time of protection may be shortened: - in severe weather - in high winds and jet blasts - by the age and condition of the fluid - by the method of application
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(5) The anti-icing code It is important that the flight crew get clear and precise information from persons who have carried out any de-/anti-icing procedures. In order to improve the quality of communication between the de-/anti-icing team and the flight crew, it is recommended that an anti-icing code be used. This will enable the flight crew to assess the Holdover Time. This code must contain the following information : - Type of Fluid - Percentage of fluid to water (for type II and Type IV fluids only) - Time de-/anti-icing application began (preferably local time) - Complete name of the anti-icing fluid (so called brand-name) for Type II and Type IV fluids only (optional).
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NOTE : The time referred to in the anti-icing codes must be the ____ starting time of the anti-icing procedure. Two examples of anti-icing codes are given below :
EFF : ALL 12-31-00 SROS
Page 5 Oct 01/04
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AEA Type II/ 75/ 16.43 local XXXXX ----------- --- ----------- ----| | | | | | | | | | | | | | | |__ Complete name of fluid | | | | | |__________ Local Time of start of the application | | | |____________________ % of fluid/water by vol: 75% fluid/25% water | Type of fluid used ISO Type I/ 06.30 UTC ---------- --------| | | | | - Universal coordinated Time of start of the application | ------ Type of fluid used (6) Equipment (a) Mobile equipment Truck mounted de-icing/anti-icing equipment must ideally be compatible for the application of Type I, Type II and Type IV fluids. Therefore the pump must be of the cavity or diaphragm type. Older types of centrifugal pumps cause degradation of fluids and their viscosity is reduced. (b) Static facilities Purpose-built de-icing/anti-icing facilities, available at some airports, consist of spray nozzles mounted on a gantry. The gantry moves at a predetermined speed over the aircraft or the aircraft moves under the gantry. The rate of fluid application can be computer-controlled, giving consistent and fast fluid application.
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(c) Protective clothing The usual precautions generally taken with chemicals must be applied when using de-icing/anti-icing fluids. This includes wearing protective clothing, protective glasses and the application of suitable skin ointment on exposed skin.
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EFF : ALL 12-31-00 SROS
Page 6 Oct 01/04
ANTI-ICING PROTECTION - MAINTENANCE PRACTICES _____________________________________________ TASK 12-31-11-660-801 Anti-Icing Protection R
CAUTION : DO NOT APPLY ANTI-ICING/DE-ICING FLUID IN: _______ - THE AIR INTAKES AND EXHAUST OF THE ENGINES OR APU - THE AIR OUTLET OF THE OUTFLOW VALVES - ALL OTHER AIR INTAKES OR OUTLETS.
R R R
CAUTION : BEFORE YOU DO THE ANTI-ICING/DE-ICING PROCEDURE, ALWAYS PUT _______ PROTECTION (SHEET MATERIAL) ON THE BRAKE UNITS. ANTI-ICING/DE-ICING FLUID CAN CAUSE CORROSION. CAUTION : DO NOT POINT HIGH-PRESSURE JETS: _______ - AT EQUIPMENT SUCH AS GEAR BOX SEALS, STEADY BEARINGS, ROTARY ACTUATORS AND UNIVERSAL JOINTS, - AT ELECTRICAL COMPONENTS SUCH AS HARNESSES, PROXIMITY SENSORS AND CONNECTORS. THE IMPACT PRESSURE OF THE JETS MUST NOT BE MORE THAN 5 PSI (0.35 BAR). FOR FAIRINGS, THE IMPACT PRESSURE OF THE JETS MUST NOT BE MORE THAN 1.5 PSI (0.1 BAR). HIGH PRESSURE JETS CAN PUSH LIQUIDS INTO BEARINGS, JOINTS, BRAKES, ELECTRICAL CONNECTORS AND OTHER SEALED COMPONENTS. LIQUIDS THAT GET INTO THESE AREAS CAN CAUSE CORROSION, FREEZE DURING AIRCRAFT FLIGHT, REMOVE NECESSARY LUBRICANTS OR START INCORRECT ELECTRICAL FUNCTIONS. CAUTION : DO NOT USE JET EXHAUST TO REMOVE SNOW OR ICE FROM THE AIRFRAME. _______ THE HIGH PRESSURE AND HIGH TEMPERATURE OF JET EXHAUST CAN CAUSE DAMAGE TO THE AIRCRAFT.
R R
CAUTION : DURING THE ANTI-ICING/DE-ICING AND WASHING PROCEDURES, MAKE SURE THAT _______ THE HOT WATER OR HOT WATER/FLUID MIXTURES DO NOT CAUSE THE TEMPERATURE OF THE AIRCRAFT SKIN TO INCREASE TO MORE THAN +70⁰C. 1. __________________ Reason for the Job NOTE : These guidelines were prepared with the Association of European ____ Airlines (AEA) recommendations: Recommendations for anti-icing of aircraft on ground. NOTE : The operators must use the procedures applicable to their individual ____ operating procedures and requirements. NOTE : The data given in the tables in this procedure are guidelines only. ____
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Page 201 Jan 01/07
The user can use these guidelines and his experience and knowledge of the local weather conditions to help him make the decision. The user must make the decision about the applicable protection procedures. The time of protection will be shorter in very bad weather conditions. High wind speeds and jet blast can cause damage to the protective film. If these conditions occur, the time of protection will be much shorter. The time of protection can also be much shorter if the wind temperature is lower than the OAT. Because conditions are not always the same, a pre-take-off inspection is necessary when you use the times given in the tables.
R R
The procedures prevent the formation of ice in some areas (wings, vertical and horizontal stabilizers, rudder) and make the removal of snow from the aircraft easier. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R R
No specific No specific
warning notice 1 DE-ICING/ANTI-ICING EQUIPMENT - 17 M (55 FT) SPRAYING HEIGHT
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 10-001 Material No. 10-003 Material No. 10-004
USA AMS 1424 DE-ICING FLUID AEA/ISO TYPE I ISO 11075 (Ref. 20-31-00) USA AMS 1428 ANTI/DE-ICING FLUID AEA/ISO TYPE II ISO 11078 (Ref. 20-31-00) USA AMS 1428 ANTI ICE/DE ICINGFLUID TYPE IV (Ref. 20-31-00)
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C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
10-11-00-555-814 24-41-00-861-801 24-41-00-862-801 12-31-11-991-002 12-31-11-991-003
Aircraft Protection Equipment Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Fig. 201 Fig. 202
3. __________ Job Set-up Subtask 12-31-11-660-051 A. Recommendations (1) An aircraft that is prepared for flight must not have ice, snow, slush or frost on its critical flight surfaces (wings, vertical and horizontal stabilizers, rudder). (2) A contamination check of the aircraft must include all parts of the aircraft. You must do this visual inspection from a position which gives a clear view of all surfaces. Because you cannot always easily see collected transparent ice, we recommend that you do an inspection of critical surfaces (wings, vertical and horizontal stabilizers, rudder) with your hands. R R
(3) Do the aircraft anti-icing/de-icing if weather conditions make it necessary. (4) When you do a check on the ground, electrical or mechanical ice-detectors must not replace manual checks. (5) If the aircraft comes to the gate with the flaps/slats in a position other than fully retracted: - you must do an inspection of these flaps/slats, - you must de-ice before retraction, if necessary.
R R R
(6) Application limits: Do not apply a new layer of anti-icing fluid directly on a layer applied before. If you must apply new anti-icing protection before the subsequent flight, you must:
EFF : ALL 12-31-11 SROS
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- first, do the de-icing of the aircraft with a hot fluid solution, - then, apply the anti-icing protection on the clean aircraft. Subtask 12-31-11-660-052 B. Different Types of Anti-Icing Fluids (Ref. Fig. 201/TASK 12-31-11-991-002, 202/TASK 12-31-11-991-003) R R R R
CAUTION : DO NOT MAKE THE ANTI-ICING/DE-ICING FLUID IN TANKS HOT TOO MANY _______ TIMES OR FOR LONG PERIODS. IF YOU DO, THE QUANTITY OF WATER IN THE FLUID WILL DECREASE AND THERE WILL BE A POSSIBLE DEGRADATION OF THE FLUID PERFORMANCE.
R R R
You usually apply anti-icing/de-icing fluid cold directly on clean aircraft surfaces. Typical anti-icing/de-icing fluids are: - Newtonian fluids (ISO or SAE or AEA Type I). - Mixtures of water and Type I fluid. - Non-Newtonian fluids (ISO or SAE or AEA Type II or Type IV). - Mixtures of water and Type II or Type IV fluid. Obey manufacturers guidelines to increase the temperature of anti-icing/de-icing fluid. For Type I fluids, water loss may cause unwanted aerodynamic effects. For Type II and Type IV fluids, thermal exposure and/or water loss may decrease fluid viscosity which causes lower holdover times. One or more of the conditions that follow can decrease fluid performance: - not much fluid used, - trucks that do not operate with heating system on for extended periods of time, - high temperatures in fluid tanks, - high temperatures in water tanks which directly touch the fluid tanks (no insulation between tanks).
R R
(1) Type I fluid (a) The primary function of this fluid is to prevent refreezing when no precipitation conditions occur. (b) Newtonian fluids (Type I) have a low viscosity that only changes with temperature. (2) Type II or Type IV fluid (a) The primary function of these fluids is to prevent refreezing when precipitation occurs.
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R
Guidelines for the Application of Fluid/Water Mixtures (Minimum Concentrations) as a Function of OAT Figure 201/TASK 12-31-11-991-002 EFF : ALL Page 205 Oct 01/04 SROS
12-31-11
R R R
Guidelines for Holdover Times Possible for Fluid Mixtures as a Function of Weather Conditions and OAT Figure 202/TASK 12-31-11-991-003- 12 (SHEET 1) EFF : ALL Page 206 Oct 01/04 SROS
12-31-11
R R R
Guidelines for Holdover Times Possible for Fluid Mixtures as a Function of Weather Conditions and OAT Figure 202/TASK 12-31-11-991-003- 22 (SHEET 2) EFF : ALL Page 207 Oct 01/04 SROS
12-31-11
(b) Non-newtonian fluids (Type II or Type IV) have a viscosity that decreases with increased airflow over the fluids. Subtask 12-31-11-555-050 C. Aircraft Maintenance Configuration R R
(1) Install the aircraft protection equipment (Ref. TASK 10-11-00-555814).
R
(2) Make sure that the APU bleed and the aircraft engine bleeds are stopped.
R
(3) Energize the ground service network (Ref. TASK 24-41-00-861-801).
R R
(4) Make sure that the flaps, the slats, the spoilers, the speed brakes and the thrust reversers are retracted.
R R R R
(5) On the center pedestal, set the pitch-trim control wheel to two degrees NOSE DN. This will drain and prevent accumulation of fluid in the THS.
R
(6) On the panel 212VU: - Make sure that the EXTRACT pushbutton switch is pushed (FAULT and OVRD legend off).
R
(7) On the panel 225VU: - Release the APU BLEED pushbutton switch (the ON legend goes off). - Release the ENG BLEED 1, ENG BLEED 2, ENG BLEED 3 and ENG BLEED 4 pushbutton switches (the OFF legends come on). - Lift the guard of the DITCHING pushbutton switch and push the pushbutton switch.
R
(8) Put a warning notice to tell persons to remove snow from their shoes and clothes before they go into the aircraft. This is very important in the cargo compartments. If there is ice or snow on the latches, this can cause defective operation of the cargo loading system. Subtask 12-31-11-210-050 D. Visual Inspection (1) Make sure that the two sliding windows are closed.
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4. Procedure _________ Subtask 12-31-11-941-050 R
A. Put the DE-ICING/ANTI-ICING EQUIPMENT - 17 M (55 FT) SPRAYING HEIGHT in position. NOTE : To use the mobile equipment on the ramp, it has a storage tank for ____ the anti-icing/de-icing fluid. Do not mix other fluids with the anti-icing/de-icing fluid. Use the fluid at the recommended concentration for the temperature to get a correct protection.
R R R
Subtask 12-31-11-660-050 R
B. Aircraft Anti-Icing
R
CAUTION : DO NOT APPLY ANTI-ICING/DE-ICING FLUID (MATERIAL NO. 10-001), _______ (MATERIAL NO. 10-003) OR (MATERIAL NO. 10-004) ON THE COCKPIT OR CABIN WINDOWS. IT CAN CAUSE CRACKS ON THE WINDOW. THE FLUID CAN ALSO GO INTO THE WINDOW SEAL. YOU MUST CLOSE ALL DOORS AND WINDOWS TO PREVENT: - CONTAMINATION OF GALLEY FLOOR AREAS WITH FLUID, - CONTAMINATION OF UPHOLSTERY. (1) Apply ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-001) or ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-003) or ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-004) on all aircraft surfaces. Do not apply fluid directly on: - the APU air intake, - the engine air intake and the exhaust, - the underfloor extract and the overboard extract valves, - the air intakes and the outlets, - the landing gear doors, - the pitot probes, - the static probes, - the AOA sensors.
R R R
(2) Do not put too much anti-icing/de-icing fluid in the rudder, elevator and aileron servo-control areas. Use sufficient fluid to remove the ice and the snow.
R R R
NOTE : In the THS apron area, it is important to point the spray from ____ the front to the rear. If you point the spray in the other direction (rear to front), anti-icing/de-icing fluid can go into the rear fuselage non-pressurized compartment.
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R (3) To prevent the flow of fluid on the cockpit windows, remove the remaining ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-001), ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-003) or ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-004) from the forward areas. You can clean the surface with clear water and a soft cloth. (4) If you find ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-001), ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-003) or ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-004) on the cockpit or cabin windows, clean the window with clear water and a soft cloth. NOTE : Do not use the wipers to clean the fluid on the windows. ____ NOTE : If you use ANTI-ICING AND DE-ICING MATERIALS (Material No. 10____ 003), make sure that there is no remaining fluid on the cockpit windows. Be specially careful of windows with wipers. 5. Close-up ________ Subtask 12-31-11-554-050 A. Removal of the Protections (1) Remove the protections and clean them with water to remove the remaining anti-icing/de-icing fluid.
R
Subtask 12-31-11-942-050 B. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-41-00-862-801). R
(2) Remove the mobile equipment. (3) Make sure that the work area is clean and clear of tools and other items.
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ICE AND SNOW REMOVAL - MAINTENANCE PRACTICES ____________________________________________ TASK 12-31-12-660-801 De-icing of the Aircraft Parked in an Open Area (Engines Stopped) R
CAUTION : DO NOT APPLY ANTI-ICING/DE-ICING FLUID IN: _______ - THE AIR INTAKES AND EXHAUST OF THE ENGINES OR APU - THE AIR OUTLET OF THE OUTFLOW VALVES - ALL OTHER AIR INTAKES OR OUTLETS.
R R R
CAUTION : BEFORE YOU DO THE ANTI-ICING/DE-ICING PROCEDURE, ALWAYS PUT _______ PROTECTION (SHEET MATERIAL) ON THE BRAKE UNITS. ANTI-ICING/DE-ICING FLUID CAN CAUSE CORROSION. CAUTION : DO NOT POINT HIGH-PRESSURE JETS: _______ - AT EQUIPMENT SUCH AS GEAR BOX SEALS, STEADY BEARINGS, ROTARY ACTUATORS AND UNIVERSAL JOINTS, - AT ELECTRICAL COMPONENTS SUCH AS HARNESSES, PROXIMITY SENSORS AND CONNECTORS. THE IMPACT PRESSURE OF THE JETS MUST NOT BE MORE THAN 5 PSI (0.35 BAR). FOR FAIRINGS, THE IMPACT PRESSURE OF THE JETS MUST NOT BE MORE THAN 1.5 PSI (0.1 BAR). HIGH PRESSURE JETS CAN PUSH LIQUIDS INTO BEARINGS, JOINTS, BRAKES, ELECTRICAL CONNECTORS AND OTHER SEALED COMPONENTS. LIQUIDS THAT GET INTO THESE AREAS CAN CAUSE CORROSION, FREEZE DURING AIRCRAFT FLIGHT, REMOVE NECESSARY LUBRICANTS OR START INCORRECT ELECTRICAL FUNCTIONS.
R R
CAUTION : DURING THE ANTI-ICING/DE-ICING AND WASHING PROCEDURES, MAKE SURE THAT _______ THE HOT WATER OR HOT WATER/FLUID MIXTURES DO NOT CAUSE THE TEMPERATURE OF THE AIRCRAFT SKIN TO INCREASE TO MORE THAN +70⁰C. CAUTION : DO NOT USE JET EXHAUST TO REMOVE SNOW OR ICE FROM THE AIRFRAME. _______ THE HIGH PRESSURE AND HIGH TEMPERATURE OF JET EXHAUST CAN CAUSE DAMAGE TO THE AIRCRAFT. 1. __________________ Reason for the Job NOTE : These guidelines have been prepared using the Association of European ____ Airlines (AEA) anti-icing code: Recommendations for the de-icing of aircraft on ground. NOTE : The operators must use the procedures applicable to their individual ____ operating methods and requirements. NOTE : The data given in the tables in this procedure are guidelines only. ____
EFF : ALL 12-31-12 SROS
Page 201 Jan 01/07
The user can use these guidelines and his experience and knowledge of the local weather conditions to help him make the decision. It is the responsibility of the user to make the decision about the applicable methods of protection. The time of protection will be shorter in very bad weather conditions. High wind speeds and jet blast can cause damage to the protective film. If these conditions occur, the time of protection will be much shorter. The time of protection can also be much shorter if the wing temperature is lower than the OAT. Because conditions are not always the same, the pre-take-off inspection is necessary when you use the times given in the tables. The procedures show how to remove ice and snow from some areas of the aircraft when the engines are stopped. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R
No No No No
specific specific specific specific
broom soft brush warning notice 1 DE-ICING/ANTI-ICING EQUIPMENT - 17 M (55 FT) SPRAYING HEIGHT
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 03-001 Material No. 10-001 Material No. 10-003 Material No. 10-004
USA MIL-PRF-7870 MINERAL OIL (LOW TEMP) (Ref. 20-31-00) USA AMS 1424 DE-ICING FLUID AEA/ISO TYPE I ISO 11075 (Ref. 20-31-00) USA AMS 1428 ANTI/DE-ICING FLUID AEA/ISO TYPE II ISO 11078 (Ref. 20-31-00) USA AMS 1428 ANTI ICE/DE ICINGFLUID TYPE IV (Ref. 20-31-00)
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C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 24-41-00-862-801 12-31-12-991-002 12-31-12-991-003
Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Fig. 201 Fig. 202
3. __________ Job Set-up Subtask 12-31-12-660-055 A. Different Types of Anti-Icing Fluids. (Ref. Fig. 201/TASK 12-31-12-991-002, 202/TASK 12-31-12-991-003) R R R R
CAUTION : DO NOT MAKE THE ANTI-ICING/DE-ICING FLUID IN TANKS HOT TOO MANY _______ TIMES OR FOR LONG PERIODS. IF YOU DO, THE QUANTITY OF WATER IN THE FLUID WILL DECREASE AND THERE WILL BE A POSSIBLE DEGRADATION OF THE FLUID PERFORMANCE. You usually apply anti-icing fluids cold directly onto clean aircraft surfaces. Typical anti-icing fluids are: - Newtonian fluids (ISO or SAE or AEA Type I), - Mixtures of water and Type I fluid, - Non-Newtonian fluids (ISO or SAE or AEA Type II or Type IV), - Mixtures of water and Type II or Type IV fluid. Follow manufacturers guidelines to increase the temperature of de-icing and anti-icing fluids. For Type I fluids, water loss may cause unwanted aerodynamic effects. For Type II or Type IV fluids, thermal exposure and/or water loss may decrease fluid viscosity which causes lower holdover times. One or more of the conditions that follow can decrease fluid performance: - not much fluid used, - trucks that do not operate with heating system on for extended periods of time, - high temperatures in fluid tanks, - high temperatures in water tanks which directly touch the fluid tanks (no insulation between tanks).
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R
Guidelines for the Application of Fluid/Water Mixtures (Minimum Concentrations) as a Function of OAT Figure 201/TASK 12-31-12-991-002 EFF : ALL Page 204 Oct 01/04 SROS
12-31-12
INTENTIONALLY BLANK
R 12-31-12 SROS
Page 205 Oct 01/04
R R R
Guideline for Possible Holdover Times for Fluid Mixtures as a Function of Weather Conditions and OAT Figure 202/TASK 12-31-12-991-003- 12 (SHEET 1) EFF : ALL Page 206 Oct 01/04 SROS
12-31-12
R R R
Guideline for Possible Holdover Times for Fluid Mixtures as a Function of Weather Conditions and OAT Figure 202/TASK 12-31-12-991-003- 22 (SHEET 2) EFF : ALL Page 207 Oct 01/04 SROS
12-31-12
(1) Type I fluid (a) The primary function of this fluid is to prevent refreezing when no precipitation conditions occur. (b) Newtonian fluids (Type I) have a low viscosity that only changes with temperature. (2) Type II or Type IV fluid (a) The primary function of these fluids is to prevent refreezing even when precipitation occurs. (b) Non-newtonian fluids (Type II or Type IV) have a viscosity that decreases with increased airflow over the fluids. Subtask 12-31-12-941-050 B. Safety Precautions (1) Put a warning notice in position to tell persons to remove the snow from their shoes before they go into the aircraft. This is very important specially in the cargo compartment, because the snow can damage the cargo loading system. R Subtask 12-31-12-869-050-A C. Aircraft Maintenance Configuration CAUTION : BEFORE YOU PUSH THE DITCHING PUSHBUTTON SWITCH, MAKE SURE THAT _______ THERE IS NO SUPPLY OF AIR TO THE AIRCRAFT THROUGH THE LOW PRESSURE CONNECTION. IF THERE IS A SUPPLY OF AIR, YOU CAN CAUSE UNWANTED PRESSURIZATION OF THE AIRCRAFT. (1) Energize the ground service network (Ref. TASK 24-41-00-861-801). (2) Make sure that the APU bleed and aircraft engine are stopped. R R R
(3) On the center pedestal, set the pitch-trim control wheel to two degrees NOSE DN. This will drain and prevent accumulation of fluid in the THS.
R
(4) On the panel 212VU: - Make sure that the EXTRACT pushbutton switch is pushed (FAULT and OVRD legend off).
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Page 208 Jul 01/06
(5) On the panel 225VU: - Release the APU BLEED pushbutton switch (the ON legend goes off). - release the ENG BLEED 1, ENG BLEED 2 pushbutton switches (the OFF legend comes on). - Lift the guard of the DITCHING pushbutton switch and push the pushbutton switch (the ON legend comes on). 4. Procedure _________ Subtask 12-31-12-660-050 A. Remove the snow. (1) If the layer of snow is too thick, remove most of the snow with a broom. Use a broom with soft bristles so that you do not damage the aircraft skin. R
(2) Put the DE-ICING/ANTI-ICING EQUIPMENT - 17 M (55 FT) SPRAYING HEIGHT in position.
R R
NOTE : To use the mobile equipment on the ramp, it has a storage tank ____ for the anti-icing fluid. Do not mix other fluids with the anti-icing fluid. Use it at the ambient temperature. (3) Prepare the de-icing compound. For this, obey the instructions of the supplier. Do not mix the de-icing compound with other fluids and use it at ambient temperature. (4) Apply the ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-001) or ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-003) or ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-004) on the aircraft skin with the spray gun of the deicing equipment. Do not apply fluid directly on: - the APU air intake and the exhaust nozzles, - the air-conditioning pack inlets, - the engine cowls, air intake and exhaust nozzle, - the forward outflow valve 313HL, - the aft outflow valve 315HL, - the avionics-ventilation underfloor extract valve 12HQ, - the avionics-ventilation overboard extract valve 13HQ, - the landing gear doors and fairings, - the brake system and wheels of the landing gear, - the battery venturi, - the pitot probes, - the temperature sensors,
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- the ice detection probes, - the static probes, - the AOA sensors. (5) Do not put too much de-icing fluid in the rudder, elevator and aileron servo-control areas. Use sufficient fluid to remove the ice and the snow. NOTE : In the THS apron area, it is important to point the spray from ____ the front to the rear. If you point the spray in the other direction (rear to front), de-icing fluid can go into the rear fuselage non-pressurized compartment. (6) Remove the snow with a soft brush from: - the engine air intake and exhaust nozzle, - the APU exhaust nozzle, - the landing gear, - the outlets of the outflow and extract valves, - the landing-gear braking system, - the inlets and outlets of the air-conditioning system. (7) Make sure that there is no ice, frost or snow in the engine air intake, all the air inlets and outlets, and the engine fan blades. This includes the rear side of the engine fan blades. R
(8) Landing gear
R R R
CAUTION : REMOVE ICE AND SNOW TO PREVENT INGRESS OF CONTAMINANTS INTO _______ BRAKES AND WHEELS. PUT COVERS ON TO PREVENT FURTHER INGRESS OF CONTAMINANTS.
R R
Remove collected ice or snow on the landing gear with a reg or a soft brush. Subtask 12-31-12-640-050 B. Lubrication (1) If the control handle of the cargo compartment doors stays blocked, lubricate the handle and the latch with OILS (Material No. 03-001)
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5. Close-up ________ Subtask 12-31-12-942-050 A. Put the Aircraft back to its Initial Configuration (1) On the panel 25 VU, release the DITCHING pushbutton switch (the ON legend is off). (2) Visually make sure that the outflow valves 313HL and 315HL are in the OPEN position before: - you supply air to the aircraft, - you start the air conditioning packs. (3) De-energize the ground service network (Ref. TASK 24-41-00-862-801). (4) Remove the access platform(s). (5) Remove the warning notice(s). (6) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
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TASK 12-31-12-660-802 De-icing of the Aircraft Parked in an Open Area (Engines Running) WARNING : WEAR A SAFETY HARNESS WHEN YOU DE-ICE THE FORWARD FUSELAGE WITH THE _______ ENGINES AT IDLE. THE SUCTION AND EXHAUST OF THE ENGINES CAN BE DANGEROUS. R
CAUTION : DO NOT APPLY ANTI-ICING/DE-ICING FLUID IN: _______ - THE AIR INTAKES AND EXHAUST OF THE ENGINES OR APU - THE AIR OUTLET OF THE OUTFLOW VALVES - ALL OTHER AIR INTAKES OR OUTLETS.
R R R
CAUTION : BEFORE YOU DO THE ANTI-ICING/DE-ICING PROCEDURE, ALWAYS PUT _______ PROTECTION (SHEET MATERIAL) ON THE BRAKE UNITS. ANTI-ICING/DE-ICING FLUID CAN CAUSE CORROSION. CAUTION : DO NOT POINT HIGH-PRESSURE JETS: _______ - AT EQUIPMENT SUCH AS GEAR BOX SEALS, STEADY BEARINGS, ROTARY ACTUATORS AND UNIVERSAL JOINTS, - AT ELECTRICAL COMPONENTS SUCH AS HARNESSES, PROXIMITY SENSORS AND CONNECTORS. THE IMPACT PRESSURE OF THE JETS MUST NOT BE MORE THAN 5 PSI (0.35 BAR). FOR FAIRINGS, THE IMPACT PRESSURE OF THE JETS MUST NOT BE MORE THAN 1.5 PSI (0.1 BAR). HIGH PRESSURE JETS CAN PUSH LIQUIDS INTO BEARINGS, JOINTS, BRAKES, ELECTRICAL CONNECTORS AND OTHER SEALED COMPONENTS. LIQUIDS THAT GET INTO THESE AREAS CAN CAUSE CORROSION, FREEZE DURING AIRCRAFT FLIGHT, REMOVE NECESSARY LUBRICANTS OR START INCORRECT ELECTRICAL FUNCTIONS. CAUTION : DO NOT USE JET EXHAUST TO REMOVE SNOW OR ICE FROM THE AIRFRAME. _______ THE HIGH PRESSURE AND HIGH TEMPERATURE OF JET EXHAUST CAN CAUSE DAMAGE TO THE AIRCRAFT.
R R
CAUTION : DURING THE ANTI-ICING/DE-ICING AND WASHING PROCEDURES, MAKE SURE THAT _______ THE HOT WATER OR HOT WATER/FLUID MIXTURES DO NOT CAUSE THE TEMPERATURE OF THE AIRCRAFT SKIN TO INCREASE TO MORE THAN +70⁰C. 1. __________________ Reason for the Job To de-ice the aircraft before passengers go into it. The flight crew is in the aircraft .
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2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
warning notice
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 10-001 Material No. 10-003 Material No. 10-004
USA AMS 1424 DE-ICING FLUID AEA/ISO TYPE I ISO 11075 (Ref. 20-31-00) USA AMS 1428 ANTI/DE-ICING FLUID AEA/ISO TYPE II ISO 11078 (Ref. 20-31-00) USA AMS 1428 ANTI ICE/DE ICINGFLUID TYPE IV (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-31-12-991-002 12-31-12-991-003
Fig. 201 Fig. 202
3. __________ Job Set-up Subtask 12-31-12-660-056 A. Different Types of Anti-Icing Fluids. (Ref. Fig. 201/TASK 12-31-12-991-002, 202/TASK 12-31-12-991-003) R R R R
CAUTION : DO NOT MAKE THE ANTI-ICING/DE-ICING FLUID IN TANKS HOT TOO MANY _______ TIMES OR FOR LONG PERIODS. IF YOU DO, THE QUANTITY OF WATER IN THE FLUID WILL DECREASE AND THERE WILL BE A POSSIBLE DEGRADATION OF THE FLUID PERFORMANCE.
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R R R R R R R R R R R R R R R R R R R
You usually apply anti-icing fluids cold directly onto clean aircraft surfaces. Typical anti-icing fluids are: - Newtonian fluids (ISO or SAE or AEA Type I), - Mixtures of water and Type I fluid, - Non-Newtonian fluids (ISO or SAE or AEA Type II or Type IV), - Mixtures of water and Type II or Type IV fluid. Follow manufacturers guidelines to increase the temperature of de-icing and anti-icing fluids. For Type I fluids, water loss may cause unwanted aerodynamic effects. For Type II or Type IV fluids, thermal exposure and/or water loss may decrease fluid viscosity which causes lower holdover times. One or more of the conditions that follow can decrease fluid performance: - not much fluid used, - trucks that do not operate with heating system on for extended periods of time, - high temperatures in fluid tanks, - high temperatures in water tanks which directly touch the fluid tanks (no insulation between tanks).
R
(1) Type I fluid
R R
(a) The primary function of this fluid is to prevent refreezing when no precipitation conditions occur.
R R
(b) Newtonian fluids (Type I) have a low viscosity that only changes with temperature.
R
(2) Type II or Type IV fluid
R R
(a) The primary function of these fluids is to prevent refreezing even when precipitation occurs.
R R
(b) Non-newtonian fluids (Type II or Type IV) have a viscosity that decreases with increased airflow over the fluids.
R
Subtask 12-31-12-941-051
R
B. Safety Precautions
R R R R
(1) Put a warning notice in position to tell persons to remove the snow from their shoes before they go into the aircraft. This is very important specially in the cargo compartment, because the snow can damage the cargo loading system.
EFF : ALL 12-31-12 SROS
Page 214 Jul 01/06
Subtask 12-31-12-860-051 R
C. Aircraft Maintenance Configuration (1) Make sure that the engine throttle control-levers are at IDLE position.
R R R
(2) On the center pedestal, set the pitch-trim control wheel to two degrees NOSE DN. This will drain and prevent accumulation of fluid in the THS.
R
(3) On the panel 117VU. - Make sure that the PARKING BRAKE selector switch is set to ON.
R
(4) On the panel 212VU: - Make sure that the EXTRACT pushbutton switch is pushed (FAULT and OVRD legends OFF).
R
(5) On the panel 225VU: - release the APU BLEED pushbutton switch (the ON legend goes off) - release the ENG BLEED 1 and ENG BLEED 2 pushbutton switches (the OFF legends come on) - release the PACK 1 and PACK 2 pushbutton switches (the OFF legends come on). - lift the guard of the DITCHING pushbutton switch and push the pushbutton switch (the ON legend comes on).
R
(6) Make sure that the landing gear doors, the passenger/crew doors, the cargo compartment doors and the sliding windows are closed.
R
(7) Make sure that the ground support and maintenance equipment are removed. 4. Procedure _________ Subtask 12-31-12-660-051 A. De-icing of the Aircraft
R R R
(1) Prepare the de-icing compound. For this, obey the instructions of the supplier. Do not mix the de-icing compound with the other fluids and use it at the ambient temperature.
EFF : ALL 12-31-12 SROS
Page 215 Jul 01/06
R R R R R R R R R R R R R R R R R R R R
(2) Apply the ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-001) or ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-003) or ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-004) on the aircraft skin with the spray gun of the de-icing equipment. Do not apply fluid directly on: - the APU air intake and the exhaust nozzles, - the air-conditioning pack inlets, - the engine cowls, air intake and exhaust nozzles, - the forward outflow valve 313HL, - the aft outflow valve 315HL, - the avionics-ventilation underfloor extract valve 12HQ, - the avionics-ventilation overboard extract valve 13HQ, - the landing gear doors and fairings, - the brake system and the wheels of the landing gear, - the battery venturi, - the pitot probes, - the temperature sensors, - the ice detection probes, - the static probes, - the AOA sensors.
R R R R R
NOTE : In the THS apron area, it is important to point the spray from ____ the front to the rear. If you point the spray in the other direction (rear to front), de-icing fluid can go into the rear fuselage non-pressurized compartment.
R Subtask 12-31-12-210-050 B. Visual Inspection (1) Make sure that after you complete the de-icing procedure, there is no more snow or ice in these areas: - the engine air intakes and exhaust nozzles, - the engine fan blades (this includes the rear side of the engine fan blades), - the APU air intake and exhaust nozzle, - the flight control surfaces: slats, flaps, ailerons, spoilers, elevator, rudder, - the forward outflow valve 313HL, - the aft outflow valve 315HL, - the avionics-ventilation underfloor extract-valve 12HQ, - the avionics-ventilation overboard extract-valve 13HQ, - the pitot probes, - the static ports,
EFF : ALL 12-31-12 SROS
Page 216 Jul 01/06
- the battery venturi, - the temperature sensors. 5. Close-up ________ Subtask 12-31-12-860-052 A. Aircraft Maintenance Configuration (1) On the panel 225VU: - release the DITCHING pushbutton switch (the ON legend is off). NOTE : Visually make sure that the outflow valves 313HL and 315HL are ____ in the OPEN position before you supply air to the aircraft. - push the PACK 1 and PACK 2 pushbutton switches (the OFF legends go off). - push the ENG BLEED 1 and ENG BLEED 2 pushbutton switches (the OFF legends go off) Subtask 12-31-12-942-051 B. Put the Aircraft back to its Initial Configuration (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL 12-31-12 SROS
Page 217 Jul 01/06
TASK 12-31-12-660-803 De-icing of the Aircraft after Landing with Snow on the Runways 1. __________________ Reason for the Job NOTE : The guidelines have been prepared using the Association of European ____ Airlines (AEA) recommendations : Recommendations for the de-icing of aircraft on ground. NOTE : The operators should use the procedures applicable to their ____ individual operating methods and requirements. To remove the snow and ice from some areas of the aircraft. 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R
10-11-00-555-807 32-00-00-481-801
Parking Procedure in Flight-ready Condition (Parking of not more than 15 Days) Installation of the Safety Devices on the Landing Gears
3. __________ Job Set-up Subtask 12-31-12-491-050 A. Safety Precautions (1) Install the safety devices on the landing gear (Ref. TASK 32-00-00481-801).
EFF : ALL 12-31-12 SROS
Page 218 Jul 01/06
4. Procedure _________ Subtask 12-31-12-660-054 A. Removal of the Snow and Ice from the Aircraft (1) Remove all signs of snow and ice from: - the wing leading edges, - the flap and slat mechanisms, - the flap and slat tracks, - the landing gear (wheels and brake system), - the engine air intakes, - the engine fan blades (this includes the rear side of the engine fan blades).
R R
Subtask 12-31-12-860-053 B. If you think that snow will fall, put the aircraft in this configuration. R R
(1) Put the aircraft in the parking configuration (Ref. TASK 10-11-00555-807). (2) Make sure that you close all: - access doors and panels, - landing gear doors, - passenger doors and exits, - cargo compartment doors, - sliding windows. (3) Make sure that: - the flaps, slats, spoilers, airbrakes and thrust reverser doors are retracted - the trimmable horizontal stabilizer is in the neutral position. 5. Close-up ________ Subtask 12-31-12-942-052 A. Put the Aircraft back to its Initial Configuration (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL 12-31-12 SROS
Page 219 Jul 01/06
COLD WEATHER MAINTENANCE - AIR CONDITIONING - MAINTENANCE PRACTICES ___________________________________________________________________ TASK 12-31-21-660-801 Cold Weather Maintenance Practices for the Air Conditioning 1. __________________ Reason for the Job This procedure gives the cold weather maintenance practices for the air conditioning. 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-31-31-660-801 12-31-38-660-801 12-31-49-660-801 R R R R R
12-33-21-618-801 12-33-21-618-801 12-33-21-618-801
Cold Weather Maintenance Practices for Indicating/Recording and Navigation Systems Cold Weather Maintenance Practices for Water/Waste Cold Weather Maintenance Practices for the Auxiliary Power Unit Pre-conditioning through the Low-Pressure Ground Connection Pre-conditioning through the High-Pressure Ground Connection Pre-conditioning with the APU
3. __________ Job Set-up Subtask 12-31-21-660-050 A. General (1) To know if ground conditioning is necessary, refer to tables 1 and 2 in the cold weather practices for the water/waste system (Ref. TASK 12-31-38-660-801).
EFF : ALL 12-31-21 SROS
Page 201 Oct 01/01
(2) Avionics Bay Temperature CAUTION : DO NOT ENERGIZE THE AIRCRAFT ELECTRICAL NETWORK IF: _______ - THE TEMPERATURE IN THE AVIONICS COMPARTMENT IS EQUAL TO OR LESS THAN -40⁰C (-40.00⁰F), AND - THE CIRCUIT BREAKERS FOR THE COMPUTERS IN THE AVIONICS COMPARTMENT ARE CLOSED. BEFORE YOU ENERGIZE THE ELECTRICAL CIRCUITS IN THESE TEMPERATURES, YOU MUST OPEN THE CIRCUIT BREAKERS. IF THE CIRCUIT BREAKERS STAY CLOSED, PERMANENT DAMAGE CAN OCCUR TO THE COMPUTERS. NOTE : The temperature factor for operation of those computers ____ located in the aircraft avionics bay is the avionics bay temperature. You must measure the temperature in the avionics bay with a suitable temperature measuring device. (3) If the temperature in the aircraft avionics bay is between -40 deg.C (-40.00 deg.F) and -15 deg.C (+5.00 deg.F): - do not energize the aircraft electrical circuits before the related computer systems circuit breakers are opened. 4. Procedure _________ Subtask 12-31-21-660-051 A. Pre-conditioning Recommendations (1) If the avionics bay temperature is equal to or less than -40 deg.C (40.00 deg.F) you must do the pre-conditioning through the LP ground connector (Ref. TASK 12-33-21-618-801). (2) If the avionics bay temperature is between -15 deg.C (+5.00 deg.F) and -40 deg.C (-40.00 deg.F) you must do the pre-conditioning through: (a) The LP ground connector (Ref. TASK 12-33-21-618-801) or, (b) The HP ground connector (Ref. TASK 12-33-21-618-801). NOTE : When you do the pre-conditioning through the HP ground ____ connector: - it is possible to operate the avionics bay computers in this temperature range but incorrect operation of the computers can occur (Ref. TASK 12-31-31-660-801). - this may cause the pre-conditioning to stop.
EFF : ALL 12-31-21 R SROS
Page 202 Oct 01/01
- this can be because of the temperature conditions and not necessarily through a technical malfunction. (3) If the avionics bay temperature is above -15 deg.C (+5.00 deg.F) you must do the pre-conditioning: (a) Through the LP ground connector (Ref. TASK 12-33-21-618-801) or, (b) Through the HP ground connector (Ref. TASK 12-33-21-618-801) or (c) With the APU (Ref. TASK 12-33-21-618-801) and (Ref. TASK 12-3149-660-801). 5. Close-up ________ Subtask 12-31-21-941-050 A. Not applicable.
EFF : ALL 12-31-21 SROS
Page 203 Apr 01/98
COLD WEATHER MAINTENANCE - ELECTRICAL POWER - MAINTENANCE PRACTICES ___________________________________________________________________ TASK 12-31-24-660-801 Cold Weather Maintenances for Electrical Power 1. __________________ Reason for the Job R R
This procedure gives the cold weather maintenances practices for the batteries when the aircraft is in cold soak configuration. 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-38-51-000-801 24-38-52-000-801
Removal of the Battery (2PB1, 2PB2) Removal of the Battery 3 (2PB3)
3. __________ Job Set-up Subtask 12-31-24-941-050 R
A. Not applicable. 4. Procedure _________ Subtask 12-31-24-660-050 A. General In very low temperatures, the chemical reaction of the electrolyte is slower and the performance of the batteries decreases : - the quantity of high current the batteries can supply decreases, - the time necessary to charge the batteries increases. This procedure gives you instructions that keep the batteries serviceable. NOTE : The values specified in this procedure are only applicable if the ____ aircraft doors stay closed during the cold soak.
EFF : ALL 12-31-24 SROS
Page 201 Jan 01/07
Subtask 12-31-24-660-051 B. Battery Cold Weather Maintenance Practices (1) The batteries can stay on the aircraft during the cold soak if : - the OAT stays higher than -15 deg.C (+5.00 deg.F), - the OAT is approximately -15 deg.C (+5.00 deg.F) for not more than 12 hours, - the OAT is between -15 deg.C (+5.00 deg.F) and -30 deg.C (-22.00 deg.F) for not more than 6 hours. However, you must remove the battery if the temperature has been below -15 deg.C (+5.00 deg.F) for more than 12 hours. (2) You must remove the batteries (2PB1, 2PB2 and 2PB3) if the OAT is lower than -30 deg.C (-22.00 deg.F) during the cold soak (Ref. TASK 24-38-51-000-801) (Ref. TASK 24-38-52-000-801). NOTE : We recommend that you use a ground power unit to start the APU ____ if the OAT was lower than -15 deg.C (+5.00 deg.F) during the cold soak.
EFF : ALL 12-31-24 SROS
Page 202 Apr 01/98
COLD WEATHER MAINTENANCE - EQUIPMENT/FURNISHINGS - MAINTENANCE PRACTICES ________________________________________________________________________ TASK 12-31-25-660-801 Cold Weather Maintenance Practices for Equipment/Furnishings WARNING : DO NOT OPEN OR GO NEAR PRESSURE-SEALED DOORS WHEN THE AIRCRAFT IS _______ PRESSURIZED. A PRESSURE-SEALED DOOR THAT OPENS WHEN THE AIRCRAFT IS PRESSURIZED: - WILL CAUSE EXPLOSIVE DECOMPRESSION. - CAN KILL OR CAUSE INJURY TO PERSONS AND/OR CAUSE DAMAGE TO THE AIRCRAFT/EQUIPMENT. CAUTION : BEFORE YOU SUPPLY AIR FROM AN EXTERNAL SOURCE OF THE APU, MAKE _______ CERTAIN THAT : -AT LEAST ONE COCKPIT WINDOW OR CABIN DOOR IS OPEN AND THAT IT REMAINS OPEN DURING SERVICING. -IF THE AIRCRAFT IS PARKED OUTSIDE AND IS NOT PROTECTED FROM THE RAIN ONE MAINTENANCE DOOR OR AVIONICS COMPARTMENT ACCESS DOOR IS OPEN AND THAT IT REMAINS OPEN DURING SERVICING. 1. __________________ Reason for the Job R
These procedures give the cold weather maintenance practices for the equipment/furnishings. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
2 WARNING NOTICE
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R Material No. 15-005A
AIB TN 10138 TYPE I GRADE 2 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
EFF : ALL 12-31-25 SROS
Page 201 Apr 01/02
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R R R R R R
12-31-38-660-801 53-00-00-000-802 53-00-00-000-803 53-00-00-400-802 53-00-00-400-803
Cold Weather Maintenance Practices for Water/Waste Removal of the Floor Panels in the FWD Cargo-Compartment Removal of the Floor Panels in the AFT Cargo-Compartment Installation of the Floor Panels in the FWD Cargo-Compartment Installation of the Floor Panels in the AFT Cargo-Compartment
3. __________ Job Set-up Subtask 12-31-25-941-050 A. Not applicable. 4. Procedure _________ Subtask 12-31-25-660-050 A. Cargo Compartment - Door Sill Latch (1) Remove floor covering (Ref. TASK 53-00-00-000-802) (Ref. TASK 53-0000-000-803). (2) Make sure that area is clean and clear. (3) Apply a STORAGE PRESERVATION (Material No. 15-005A) to latch mechanisms. (4) Install floor covering (Ref. TASK 53-00-00-400-802) (Ref. TASK 53-0000-400-803).
EFF : ALL 12-31-25 SROS
Page 202 Jan 01/01
Subtask 12-31-25-660-051 B. Cabin Escape Facilities (1) Girt Bar (a) If the aircraft is parked and not heated: - Make sure that all snow and/or slush is removed from the door exit area, before you close the doors of the aircraft. (b) Clean dirt from the floor fittings and the sliders. Do a check every 350 flight hours or more frequently as necessary. R R
(2) Do not apply grease to the cleaned area. Subtask 12-31-25-660-052 C. Escape slides (1) If the aircraft is exposed to temperature changes (from cold to warm), the pressure gages of the escape slides can give NO GO indication for a short time because the green temperature compensator cursor in the gage reacts to temperature changes faster than the gas expansion in the bottle. (2) NO GO indications may occur for short periods under the following circumstances : - if the cabin door is open in cold condition when the aircraft in being prepared or while passengers are embarking. - when the aircraft is heated for flight preparation after. (3) After closing of the doors and when the aircraft temperature becomes stable, the NO GO indication is no longer present. Subtask 12-31-25-660-053 D. Galley Equipment (1) You must drain all the galley equipment which contains water, such as coffee makers and water boilers. (2) You must operate the taps several times to make sure that the supply lines are empty (Ref. TASK 12-31-38-660-801). (3) If the conditions to drain all the galley equipment cannot be carried out, the heating recommendations should be used as follows :
EFF : ALL 12-31-25 SROS
Page 203 Apr 01/05
---------------------------------------------------------------------------| OUTSIDE AIR |EXTERNAL HEAT | APU | SUPERVISOR | DRAINING OF | | TEMPERATURE | SOURCE | | | WATER SYSTEM | |--------------|--------------|--------------|--------------|--------------| | 0 deg.C | 1 HOUR | | | | | (32 deg.F) | | | | | | to | EVERY | NO | NO | NO | | -5 deg.C | | | | | | (23 deg.F) | 4 HOURS | | | | |--------------|--------------|--------------|--------------|--------------| | -5 deg.C | 2 HOURS | | | | | (23 deg.F) | | | | | | to | EVERY | NO | NO | NO | | -10 deg.C | | | | | | (14 deg.F) | 4 HOURS | | | | |--------------|--------------|--------------|--------------|--------------| | -10 deg.C | | | | | | (14 deg.F) | | | | | | to | CONTINUOUS | NO | NO | NO | | -15 deg.C | | | | | | (5 deg.F) | | | | | |--------------|--------------|--------------|--------------|--------------| | BELOW | | AS | | | | -15 deg.C | CONTINUOUS | REQUIRED | YES | YES | | (5 deg.F) | | | | | ---------------------------------------------------------------------------Subtask 12-31-25-620-050 E. First Aid Kits (1) Remove the first aid kits from the aircraft if the cabin temperature is below -10 deg.C (+14.00 deg.F). R R
(2) To avoid damage to the kit equipment keep the kits in a place with a temperature between min. 1 deg.C (33.80 deg.F) and 40 deg.C (104.00 deg.F) max.
R
(3) Put a WARNING NOTICE in position to tell personnel that the first aid kits are removed.
EFF : ALL 12-31-25 SROS
Page 204 Apr 01/05
R
**ON A/C 001-049, 201-202, 251-252, 255-299, 401-449, 451-499, 701-749, Subtask 12-31-25-620-051 F. Doctors Kit (7610MX) (1) Remove the doctors kits from the aircraft if the cabin temperature is less than 1 deg.C (33.80 deg.F). NOTE : To avoid damage to the kit equipment keep the kits in a place ____ with a temperature between min. 1 deg.C (33.80 deg.F) and 40 deg.C (104.00 deg.F) max. (2) Put a WARNING NOTICE in position to tell personnel that the doctors kits are removed.
R EFF : 001-049, 201-202, 251-252, 255-299, 12-31-25 401-449, 451-499, 701-749, SROS
Page 205 Jul 01/05
COLD WEATHER MAINTENANCE - FLIGHT CONTROLS - MAINTENANCE PRACTICES __________________________________________________________________ TASK 12-31-27-660-801 Cold Weather Maintenance Procedures for Flight Controls WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. 1. __________________ Reason for the Job This procedure gives the instructions to lubricate the flight controls in cold weather conditions. 2. ______________________ Job Set-up Information A. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 10-001 Material No. 10-003 Material No. 10-004
USA AMS 1424 DE-ICING FLUID AEA/ISO TYPE I ISO 11075 (Ref. 20-31-00) USA AMS 1428 ANTI/DE-ICING FLUID AEA/ISO TYPE II ISO 11078 (Ref. 20-31-00) USA AMS 1428 ANTI ICE/DE ICINGFLUID TYPE IV (Ref. 20-31-00)
EFF : ALL 12-31-27 R SROS
Page 201 Jan 01/07
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-22-27-640-803 12-22-27-640-804 12-22-27-640-806 12-31-11-660-801
Lubrication of Flap Track/Carriage (1-5) Roller Bearings Lubrication of all Slat Track Roller Bearings, Pinion Bearings, Rack and Pinion Teeth and Slat Track 2 and 3 Lever Bearings Lubrication of Flap Steady Bearings Anti-Icing Protection
3. __________ Job Set-up Subtask 12-31-27-941-050 A. Not applicable. 4. Procedure _________ Subtask 12-31-27-660-050 A. Check of the Flight Controls (1) Make sure that ice and/or snow is not forced into the areas between the flight control surfaces during the deicing procedures. (2) Remove any ice from : - the wing leading edge - the slats - the flaps - the spoilers - the ailerons (3) You must retract the wing flaps and slats during periods of snowfall and icing conditions. If it is necessary to operate these controls, make sure that they are clear of accumulation before retraction. R R R R
(4) If an aircraft arrives with the slats and flaps in a position other than fully retracted during a period of ice or snow conditions, those slats and flaps which are extended must be inspected for ice and snow accumulation before retracting.
EFF : ALL 12-31-27 SROS
Page 202 Jan 01/07
(5) All control surfaces must have no ice, snow or frost. After the deicing operation, do a check of the associated hinges, tracks, actuators and servo controls for trapped moisture that can freeze. Apply anti-icing fluid for protection ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-001), ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-003) or ANTI-ICING AND DE-ICING MATERIALS (Material No. 10-004) (Ref. TASK 12-31-11-660-801) (6) Do a check of the leading edge area of the spoilers, the flaps for ice, snow and frost. (7) Final checks after aircraft deicing on flap/slat areas : the applicable areas must have no snow and ice as well as water accumulation. During snowfall, freezing rain and drifting snow it is possible that snow and melting ice go into slots, drainage openings, hinges and operating linkage and will freeze again. You must do the check of these areas with special attention when an aircraft has been parked outside for a long period under the above conditions. Subtask 12-31-27-660-051 B. Lubrication of the Flaps and Slats (1) Do the applicable flap/slat lubrication tasks (Ref. TASK 12-22-27640-803) (Ref. TASK 12-22-27-640-804) (Ref. TASK 12-22-27-640-806) (2) The winter preparation program should include the flap and slat lubrication. NOTE : In climates where the atmosphere is both particularly cold and ____ humid (mist/fog) use your experience to reduce the lubrication task intervals during winter operations. NOTE : In extreme climates and low ambient temperatures it may be ____ difficult to lubricate the flap and slat systems correctly. If hangar space is not available then it is recommended to do the lubrication tasks at a station where the appropriate facilities are available or where the ambient temperature is above 0 deg.C (32.00 deg.F).
R R R
(3) Increases in grease stiffness may occur if water present within a lubricant forms discrete lumps of ice, the associated increases in system friction may then result in torque limiter operation. (4) When you do the lubrication tasks take care to ensure that all the old grease is removed in order to reduce the risk of an increase in grease stiffness.
EFF : ALL 12-31-27 SROS
Page 203 Jan 01/07
COLD WEATHER MAINTENANCE - FUEL - MAINTENANCE PRACTICES _______________________________________________________ TASK 12-31-28-660-801 Cold Weather Maintenance Practices for the Fuel System WARNING : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND DAMAGE. _______ WARNING : MAKE SURE THE AREA AROUND THE AIRCRAFT IS SAFE BEFORE YOU START A _______ REFUEL/DEFUEL PROCEDURE. IN THIS SAFE AREA, DO NOT LET PERSONS: - SMOKE - MAKE SPARKS OR FIRE - USE ANY EQUIPMENT WHICH IS NOT APPROVED FOR THE TASK. AIRCRAFT FUEL IS FLAMMABLE. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
hot air blower safety barriers surface contact thermometer
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-32-28-281-803 R R
12-32-28-281-810 28-00-00-610-801
Operate Water Drain Valves to Drain Accumulated Water from Trim Tank and Trim Vent Surge Tank Operate Water Drain Valves to Drain Accumulated Water from Center, Inner, Outer and Wing Vent Surge Tanks Fuel Safety Procedures
EFF : ALL 12-31-28 SROS
Page 201 Apr 01/05
3. __________ Job Set-up Subtask 12-31-28-869-050 A. General Information This procedure gives the cold weather maintenance practices for the fuel system when an aircraft is operated or stored in conditions with ground temperatures of between 0 deg.C (32 deg.F) and -54 deg.C (-67 deg.F). The fuel storage and handling conditions can have an important effect on the amount of water in solution with the fuel. In unsatisfactory conditions, each 3785 liters (1000 USgal) of fuel can contain up to 0.76 l (0.2 USgal) of water. Water can get into the tanks in different ways: - the fuel supplied to the aircraft contains water - the air in the tank contains moisture (water) - during descent large quantities of moist air can enter the tank - fuel which is open to dampness or wet atmospheric conditions will contain larger quantities of water than fuel stored in sealed containers. In cold conditions, much of this water can come out of solution and fall to the bottom of the tank. It then collects at the lowest parts of the tank and can form ice. The formation of ice (and the presence of water) in the fuel tanks can have an effect on the accuracy and/or performance of the quantity indication system. It can also cause engine or corrosion related problems. Approved anti-ice additive can be added, in the correct proportions, to the fuel which is supplied to the aircraft. This can prevent water in the fuel from freezing and let it be drained from a tank with a fuel temperature below 0 deg.C (32 deg.F). The ice in the fuel tank can be melted through these procedures: - ambient air heat in a hangar - a refuel with warm fuel - warm air heat from a blower, until the temperature of the whole of the bottom skin is 1 deg.C (34 deg.F). This procedure is usually done in a hangar, but can be used outside if a hangar is not available - a combination of these methods. NOTE : Ice can form on the inside of the fuel tank close to ____ drain valve. When you drain fuel from the tank for a analysis check, fuel flows over the ice and collects can cause incorrect analysis results. The procedure that follows should remove most of the from the fuel tank.
the water water water. This water/ice
EFF : ALL 12-31-28 SROS
Page 202 Apr 01/98
You must do the water drain procedure regularly to make sure that all the water is drained from the tank low points. Subtask 12-31-28-941-050 B. Safety Precautions WARNING : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND _______ DAMAGE. (1) You must obey the safety procedures when you do work on the fuel system (Ref. TASK 28-00-00-610-801). (2) Put the safety barriers in position. 4. Procedure _________ R R
Subtask 12-31-28-660-050-A A. Water Draining of the Tanks
R R
CAUTION : DO NOT USE FORCE TO OPEN THE WATER DRAIN VALVES. THIS PREVENTS _______ DAMAGE TO THE VALVES.
R R
(1) If a water drain does not open with the usual pressure, find the cause. The valve could be frozen because of the low temperature.
R
(2) Water draining of the tanks (aircraft in a hangar)
R
(a) If possible, refuel the aircraft with warm fuel.
R R
(b) Use a surface contact thermometer to measure the temperature of the bottom skin of the tank to be drained.
R R R
(c) If necessary, use an approved hot air blower to warm the bottom skin of the tank to be drained. Make sure the temperature of the bottom skin does not increase to more than 50 deg.C (122 deg.F).
R R R
NOTE : The temperature of all the bottom skin should be 1 deg.C ____ (34 deg.F) or more measured one minute after the removal of the hot air blower.
R R R
(d) Drain accumulated water (Ref. TASK 12-32-28-281-810) 30 minutes after the aircraft has been refuelled (and before the bottom skin temperature decreases below 0 deg.C (32 deg.F)).
EFF : ALL 12-31-28 SROS
Page 203 Apr 01/05
R R R R
NOTE : When you do the water drain procedure, it can be necessary ____ to drain large quantities of fuel to get a satisfactory HYDROKIT test result (Ref. TASK 12-32-28-281-810) and (Ref. TASK 12-32-28-281-803).
R
(3) Water draining of the tanks (aircraft outside)
R R R R
CAUTION : MAKE SURE THAT THE TEMPERATURE OF THE AIR FROM THE HOT AIR _______ BLOWER IS NOT MORE THAN 50 DEG.C (122 DEG.F). IF THE TEMPERATURE IS MORE THAN 50 DEG.C (122 DEG.F) YOU CAN CAUSE DAMAGE TO THE AIRCRAFT.
R
(a) If possible, refuel the aircraft with warm fuel.
R R
(b) Use a surface contact thermometer to measure the temperature of the bottom skin of the tank to be drained.
R R R R
NOTE : To do the procedure the temperature near to the drain ____ valves should be 1 deg.C (34 deg.F) or more. It is possible that not all of the ice will be melted, thus the drain procedure will not be fully successful.
R R R
(c) Use an approved hot air blower to warm the bottom skin of the tank to be drained. Make sure the temperature of the bottom skin does not increase to more than 50 deg.C (122 deg.F).
R R R
NOTE : The temperature of the bottom skin near to the drain valve ____ should be 1 deg.C (34 deg.F) or more measured one minute after the removal of the hot air blower.
R R R R
(d) Drain the accumulated water (Ref. TASK 12-32-28-281-810) 30 minutes after the aircraft has been refuelled (and before the bottom skin temperature near to the drain valves decreases below 0 deg.C (32 deg.F)).
R R R R
NOTE : When you do the water drain procedure, it can be necessary ____ to drain large quantities of fuel to get a satisfactory HYDROKIT test result (Ref. TASK 12-32-28-281-810) and (Ref. TASK 12-32-28-281-803).
EFF : ALL 12-31-28 SROS
Page 204 Apr 01/05
Subtask 12-31-28-660-051 R
B. Anti-Icing Additives (1) If you think that the fuel temperature will be less than 0 deg.C (32 deg.F) (and if it is not possible to warm the aircraft in a hangar) you can put anti-icing additives in the fuel. This makes sure that the water in the fuel does not freeze. When you add anti-icing additives to the fuel, the concentration must not be more than 0.15% by volume. You must also make sure that the additive is fully mixed with the fuel.
R R R R R
NOTE : Refer to the engine manufacturer data for approved fuel ____ additives. 5. Close-up ________ Subtask 12-31-28-942-050 A. Removal of Equipment (1) Remove the safety barriers. (2) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL 12-31-28 SROS
Page 205 Oct 01/99
______________________________________________________________________ COLD WEATHER MAINTENANCE - INDICATING/RECORDING SYSTEMS AND NAVIGATION MAINTENANCE PRACTICES _____________________ TASK 12-31-31-660-801 Cold Weather Maintenance Practices for Indicating/Recording and Navigation Systems 1. __________________ Reason for the Job This procedure gives the cold weather maintenance practices for indicating/recording and navigation systems. 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-31-21-660-801
Cold Weather Maintenance Practices for the Air Conditioning
3. __________ Job Set-up Subtask 12-31-31-941-050 A. Not applicable. 4. Procedure _________ Subtask 12-31-31-660-050 A. General (1) When the Outside Air Temperature (OAT) is very low, cold (temperature lower than -15 deg.C (+5.00 deg.F)) in the avionics compartment can cause incorrect operation of the computers. NOTE : This is only due to the cold weather conditions and not to a ____ technical malfunction.
EFF : ALL 12-31-31 SROS
Page 201 Apr 01/98
Subtask 12-31-31-660-051 B. Recommendations (1) Make sure that the computers are at a temperature equal to or higher than -15 deg.C (+5.00 deg.F) for correct operation. NOTE : If you energize the computers at very low temperatures the ____ following can occur. If the temperature is : - equal to or lower than -40 deg.C (-40.00 deg.F), you can cause permanent damage to the computers. - between -40 deg.C (-40.00 deg.F) and -15 deg.C (+5.00 deg.F), the computers can operate but normal operation can stop momentarily. - equal to or higher than -15 deg.C (+5.00 deg.F), the computers operate normally. (a) Preconditioning It is recommended to use the pre-conditioning procedure to increase the temperature in the avionics compartment (Ref. TASK 12-31-21-660-801). (b) Energization of the computers If the temperature is higher than -40 deg.C (-40.00 deg.F), you can energize the computers to increase the temperature to -15 deg.C (+5.00 deg.F). The time necessary to increase the temperature will change with the OAT, the humidity and the time since the avionics compartment ventilation stopped.
EFF : ALL 12-31-31 SROS
Page 202 Apr 01/98
COLD WEATHER MAINTENANCE - LANDING GEAR - MAINTENANCE PRACTICES _______________________________________________________________ TASK 12-31-32-660-801 Cold Weather Maintenance Practices for the Landing Gear 1. __________________ Reason for the Job This procedure gives the cold weather maintenance practices for the tires and precautions for towing. 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-41-00-220-801
Check Tire Pressures
3. __________ Job Set-up Subtask 12-31-32-941-050 A. Not applicable. 4. Procedure _________ Subtask 12-31-32-660-050 A. General (1) When there is a decrease in the ambient temperature, the tire pressures also decrease. A 3 deg.C (5.4 deg.F) change in temperature causes a 1 percent change in tire pressure. R R
NOTE : The tires wear faster if the pressure in the tires are low. ____ Low tire pressure can increase the risk of tire failure.
EFF : ALL 12-31-32 SROS
Page 201 Jul 01/02
Subtask 12-31-32-660-051 B. Recommendations (1) Tire pressure check (a) When the aircraft is parked in cold weather conditions (cold soak) for more than one hour, do a check of the tire pressure (Ref. TASK 32-41-00-220-801). R R R
(b) You must use dry nitrogen to correct the tire pressure. Moisture in air can change to ice in the valve, which causes a permanent leak. However, if dry nitrogen is not available at outstations, air can be used with the limitations that follow: - the total content of oxygen is less than 5% volume - the tire inflation valve does not leak after inflation - the air does not stay in the tire for more than 15 hours. You must service the tire with dry nitrogen at the end of this time.
R R
(c) If a tire is inflated with air, you must record this in the maintenance log. (2) Towing precautions Be careful during aircraft towing operations in cold weather conditions. Do not make small-radius turns which can cause too much load on the sidewalls of the tires.
EFF : ALL 12-31-32 SROS
Page 202 Jul 01/02
R
TASK 12-31-32-916-801
R
Cold Weather Protection for the Landing Gear Axles
R R R R R R R
WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS.
R R R
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED ON THE _______ LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR.
R
1. __________________ Reason for the Job
R R R R
To give more corrosion protection to the landing gear axles when de-icing fluids are used during cold weather. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment
R R R
------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R R
No specific No specific No specific
R
Aerospec Protect 1 SPATULA - NON METALLIC AR WARNING NOTICE
B. Consumable Materials
R R R
------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R R R R R
Material No. 08-074 Material No. 11-002 Material No. 19-003
MASKING TAPE (Ref. 20-31-00) USA MIL-PRF-680 DRY CLEANING SOLVENT (VARSOL/WHITE SPIRIT) (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
EFF : ALL 12-31-32 SROS
Page 203 Jan 01/07
R
C. Referenced Information
R R R
------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R R R R R R R
32-00-00-481-801
R
3. __________ Job Set-up
R
Subtask 12-31-32-941-051
R
A. Safety Precautions
32-41-14-000-801 32-41-14-400-801 12-31-32-991-001
Installation of the Safety Devices on the Landing Gears Removal of the MLG Axle Sleeve (6560GG,6561GG,6562GG,6563GG,6564GG,6565GG, 6566GG,6567GG) Installation of the MLG Axle Sleeve (6560GG,6561GG,6562GG,6563GG,6564GG, 6565GG,6566GG,6567GG) Fig. 201
R R
(1) Make sure that the safety devices are installed on the landing gear (Ref. TASK 32-00-00-481-801).
R R
(2) On the panel 312VU make sure the landing gear is in the down position.
R R R R
(3) Put a WARNING NOTICE: - on the applicable MLG ground-opening handle to tell persons not to operate the handle - on the panel 312VU to tell persons not to operate the landing gear.
R R
Subtask 12-31-32-010-050 B. Get Access
R R
(1) Remove the applicable MLG axle sleeve(s) (Ref. TASK 32-41-14-000801).
EFF : ALL 12-31-32 SROS
Page 204 Jan 01/07
R R R R
4. Procedure _________ (Ref. Fig. 201/TASK 12-31-32-991-001) Subtask 12-31-32-916-050 A. Application of Corrosion Protection on the Landing Gear Axles
R R R R R R R R R
WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL _______ MATERIALS ONLY WITH A GOOD FLOW OF AIR THROUGH THE WORK AREA. THESE MATERIALS ARE POISONOUS AND FLAMMABLE AND SKIN IRRITANTS. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
R R R R R
CAUTION : MAKE SURE THAT THE CLEANING AGENTS OR SOLVENTS DO NOT GET IN OR _______ ON : - COMPONENT PARTS - PROTECTIVE COVERS - ELECTRICAL WIRING AND CONNECTORS.
R R R
(1) Use a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-002) to clean the landing gear axle to remove the used Aerospec Protect.
R R
(2) Do a visual inspection to make sure that the axle is serviceable and there is no corrosion.
R R
NOTE : If you find corrosion refer to AIRBUS for the repair ____ procedure.
R R
(3) Apply BONDING AND ADHESIVE COMPOUNDS (Material No. 08-074) to the area of the axle that is not applicable.
R R
(4) Refer to the manufacturers instructions to apply a thin, smooth layer of Aerospec Protect on the axle.
R R R R
NOTE : During application of the Aerospec Protect you must: ____ - keep the aerosol container vertical. - make sure you have applied the aerosol spray over the full applicable area.
EFF : ALL 12-31-32 SROS
Page 205 Jan 01/07
R R
Cold Weather Protection for the Landing Gear Axles - Location and Details Figure 201/TASK 12-31-32-991-001
EFF : ALL 12-31-32 SROS
Page 206 Jan 01/07
R R
(5) Wait for a minimum of 1 minute drying time, do steps (4) to (5) until you get a satisfactory layer of Aerospec Protect.
R R
NOTE : Refer to the manufactures instructions for drying times. These ____ can change with local conditions.
R R
(6) Remove the BONDING AND ADHESIVE COMPOUNDS (Material No. 08-074) from the axle.
R R
(7) Use a SPATULA - NON METALLIC to make the edges of the Aerospec Protect smooth.
R R
(8) Use a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-002) to remove unwanted Aerospec Protect.
R R
Subtask 12-31-32-410-050 B. Close Access
R R
NOTE : Make sure you do not damage the corrosion protection you have ____ applied to the axle.
R
(1) Install the applicable axle sleeve(s) (Ref. TASK 32-41-14-400-801).
R
5. Close-up ________
R
Subtask 12-31-32-942-050
R
A. Removal of Equipment
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 12-31-32 SROS
Page 207 Jan 01/07
COLD WEATHER MAINTENANCE - OXYGEN - MAINTENANCE PRACTICES _________________________________________________________ TASK 12-31-35-660-801 Cold Weather Maintenance - Oxygen System 1. __________________ Reason for the Job This procedure gives the cold weather maintenance practices for the oxygen system. 2. ______________________ Job Set-up Information A. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 05-004
USA MIL-PRF-25567 TYPE I OXYGEN LEAK DETECTOR (Ref. 20-31-00)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R
12-14-35-600-801 12-33-21-618-801 35-11-41-000-801 35-11-41-400-801
Servicing of the Oxygen Replenishing Pre-conditioning through the Low-Pressure Ground Connection Removal of the Oxygen Cylinder/Valve Assy Installation of the Oxygen Cylinder/Valve Assy
3. __________ Job Set-up Subtask 12-31-35-941-050 A. Not applicable.
EFF : ALL 12-31-35 SROS
Page 201 Jul 01/06
4. Procedure _________ Subtask 12-31-35-660-050 A. Installation of Oxygen Cylinder(s). (Ref. TASK 35-11-41-000-801) (Ref. TASK 35-11-41-400-801) NOTE : When you replace oxygen cylinder(s), you must mandatorily obey the ____ Removal/Installation procedure for oxygen cylinder(s). (1) If you replace the oxygen cylinder(s) of the crew oxygen system when the ambient temperature is -20 deg.C (-4.00 deg.F) or less : - make sure that the temperature in the oxygen cylinder compartment is more than -20 deg.C (-4.00 deg.F). If this temperature is -20 deg.C (-4.00 deg.F) or less, the SPECIAL MATERIALS (Material No. 05-004) used to do the leak test will freeze. (2) It is recommended to replace the cylinder after a flight but before the compartment temperature is -20 deg.C (-4.00 deg.F). Or you can do this task while you pre-condition the aircraft on the ground. (Ref. TASK 12-33-21-618-801) Subtask 12-31-35-660-051 B. Replenishment of Oxygen Cylinder(s). (Ref. TASK 12-14-35-600-801) NOTE : When you fill oxygen cylinder(s), you must mandatorily obey the ____ replenishment procedure for oxygen cylinder(s). (1) The maximum charging pressure of the cylinder changes with the ambient temperature. Be careful that the pressure at which you pressurize the cylinder is not more than the maximum charging pressure.
R R
(2) It is recommended to fill the cylinder before the temperature in the oxygen cylinder compartment is -20 deg.C (-4.00 deg.F) but only after : - the aircraft network is de-energized, - the aircraft and equipment are bonded to ground.
EFF : ALL 12-31-35 SROS
Page 202 Jan 01/07
COLD WEATHER MAINTENANCE - WATER/ WASTE - MAINTENANCE PRACTICES _______________________________________________________________ TASK 12-31-38-660-801 Cold Weather Maintenance Practices for Water/Waste CAUTION : MAKE SURE THAT THE TEMPERATURE OF THE AIR FROM THE HOT AIR BLOWER IS _______ NOT MORE THAN 50 DEG.C (122 DEG.F). IF THE TEMPERATURE IS MORE THAN 50 DEG.C (122 DEG.F) YOU CAN CAUSE DAMAGE TO THE AIRCRAFT. CAUTION : BEFORE YOU SUPPLY AIR FROM AN EXTERNAL SOURCE OF THE APU, MAKE _______ CERTAIN THAT : -AT LEAST ONE COCKPIT WINDOW OR CABIN DOOR IS OPEN AND THAT IT REMAINS OPEN DURING SERVICING. -IF THE AIRCRAFT IS PARKED OUTSIDE AND IS NOT PROTECTED FROM THE RAIN ONE MAINTENANCE DOOR OR AVIONICS COMPARTMENT ACCESS DOOR IS OPEN AND THAT IT REMAINS OPEN DURING SERVICING. R R R R
CAUTION : IN FREEZING CONDITIONS, MAKE SURE THAT SERVICE PANELS OR CAPS ARE NOT _______ FROZEN BEFORE YOU TRY TO OPEN THEM. IF THE SERVICE PANELS OR CAPS ARE FROZEN, YOU MUST APPLY HOT AIR TO DE-ICE THEM FIRST. IF YOU TRY TO OPEN THEM WHEN THEY ARE FROZEN, YOU CAN CAUSE DAMAGE TO THEM. 1. __________________ Reason for the Job To prevent damage to the water/waste system by ice when the aircraft is not supplied with power or other sources of hot air. NOTE : Although an aircraft is resistant to very low ambient temperatures, ____ the cabin air conditioning (and WIPU system) keep the pipes (and water systems sufficiently warm to prevent them) from freezing. However, when the aircraft is not energized or stays on the ground at sub-zero temperatures, you must do additional procedures to prevent damage to the systems by ice.
R 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 CART - SERVICING, TOILET
EFF : ALL 12-31-38 SROS
Page 201 Jan 01/07
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 14-001A DEODORANT AIRCRAFT TOILET NON FORMALDE- HYDE BASE (Ref. 20-31-00) C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-15-38-613-801 12-24-38-680-801 12-33-21-618-801 38-10-00-614-801 38-10-00-614-803 38-31-00-680-801
Fill the Potable Water System (Aircraft Electrical Power Available) Draining of the Potable Water System (with Electrical Power) Pre-conditioning through the Low-Pressure Ground Connection Pressurization of the Potable Water System Release of the Pressure from the Potable Water System Draining of the Waste Holding Tanks
3. __________ Job Set-up Subtask 12-31-38-941-050 A. There is no special job set-up for this task. 4. Procedure _________ Subtask 12-31-38-660-050 A. Pre-Flight (First Flight of the Day) (1) After draining of the water/waste system due to low ambient temperatures you must obey the steps that follow. (2) Make sure that all drain valves are closed.
EFF : ALL 12-31-38 R SROS
Page 202 Jul 01/06
(3) Potable Water System (a) Fill the potable water system (Ref. TASK 12-15-38-613-801) with warm potable water of 30 deg.C (86.00 deg.F) not earlier than 30 minutes before the engine start. (b) Pressurize the potable water system (Ref. TASK 38-10-00-614-801) and examine the fill/drain valve for leaks. (c) Remove excessive water from around the service panel before you close it. (4) Waste System (a) Pre-charge the waste holding tanks not earlier than 30 minutes before the engine start: - Use a CART - SERVICING, TOILET to fill each waste holding tank with 18 l (4.8 USgal) of DISINFECTANTS (Material No. 14-001A). (b) Remove excessive liquid from around the service panel before you close it. R
**ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499, 701-749, Subtask 12-31-38-660-051 B. Post Flight (Last Flight of the Day but not Transit Stops) (Ref. TASK 3831-00-680-801) (Ref. TASK 12-24-38-680-801) (1) General (a) Do the servicing of the potable water system and waste water tanks as soon as possible after a flight. (b) Read tables 1 and 2 (draining of the water and waste system) to find if it is necessary to drain the water and waste from the system. (c) After draining of the system and parking of the aircraft at temperatures below 0 deg.C (32.00 deg.F): - Let the drain valves and the service panels stay open to let remaining fluid to flow out. - Do not install the caps on the drain and the fill/drain nipples.
EFF : ALL 12-31-38 SROS
Page 203 Jul 01/05
NOTE : If you install the caps, the remaining fluid can freeze ____ immediately behind the drain and fill/drain caps and will cause: - Damage to the piping system - The system to become unserviceable - Delay at the next servicing. ------------------------------------------------------------------------------| TABLE 1 | |-----------------------------------------------------------------------------| | CONFIGURATION | | WATER | -------------------------------------------------|COLD SOAK TIME| AND | | AIR | CABIN | OUTSIDE AIR | (HOURS:MIN) | WASTE | | CONDITIONING | TEMPERATURE | TEMPERATURE | | TANKS DRAIN | |--------------|-------------|-------------------|--------------|-------------| | | | BETWEEN | | NOT | | | | 0 AND -15 deg.C | ANY | REQUIRED | | | ABOVE | (32 AND 5 deg.F) | | | | ON | 10 deg.C |-------------------|--------------|-------------| | | (50 deg.F) | BELOW | | | | | | -15 deg.C | 1:15 | | | | | (5 deg.F) | | | |--------------|-------------|-------------------|--------------| | | | | BETWEEN | | | | | | 0 AND -7 deg.C | 1:30 | | | | |(32 AND 19.4 deg.F)| | | | | |-------------------|--------------| | | OFF | | BETWEEN | | REQUIRED | | | | -7 AND -15 deg.C | 0:30 | | | | | (19.4 AND 5 deg.F)| | | | | |-------------------|--------------| | | | | BELOW | | | | | | -15 deg.C | ANY | | | | | (5 deg.F) | | | ------------------------------------------------------------------------------(2) Potable water system CAUTION : DO NOT OPEN THE ELECTRICAL DRAIN VALVES FOR LONGER THAN _______ NECESSARY IF YOU USE THE APU OR ENGINE(S) TO PRESSURIZE THE SYSTEM. IF THE VALVES STAY OPEN TOO LONG, THE HOT BLEED AIR CAN CAUSE DAMAGE TO THE TANK QUANTITY TRANSMITTER. (a) If you park the aircraft at very low temperature: - Drain the water from the potable water system, - Remove the remaining water from the potable water system, as stated below:
R EFF : 001-049, 201-249, 251-252, 255-299, 12-31-38 401-449, 451-499, 701-749, SROS
Page 204 Jul 01/05
1 _
Drain the potable water system (Ref. TASK 12-24-38-680-801).
2 _
Close all the lavatory and galley manual shutoff valves.
3 _
Close all the potable-water drain and fill drain valves.
4 _
Pressurize the potable water system (Ref. TASK 38-10-00-614801).
5 _
To remove the remaining water from the potable water system do the procedure as follows: NOTE : This procedure is the same for all lavatories and ____ galleys which have potable water supplied equipment (as there are water heater, coffeemaker and water faucet). a _
Open one related manual shutoff valve of one lavatory or galley.
b _
Operate the faucet (HOT and COLD).
c _
Make sure that air but no water comes out of the faucet.
d _
Flush the toilet as often as necessary until you are sure that air but no water comes out of the toilet rinse valve.
e _
Close the related manual shutoff valve.
f _
Do the whole procedure for all lavatories and galleys which have potable-water supplied equipment.
6 _
Open all drain valves of the potable water system and release the pressure from the potable water system (Ref. TASK 38-1000-614-803).
7 _
Open the manual shutoff valves in all lavatories or galleys.
(b) If you cannot drain the potable water system: - Do the pre-conditioning of the aircraft (Ref. TASK 12-33-21618-801) as follows:
R EFF : 001-049, 201-249, 251-252, 255-299, 12-31-38 401-449, 451-499, 701-749, SROS
Page 205 Jul 01/05
---------------------------------------------------------------------------| TABLE 2 | |--------------------------------------------------------------------------| | OUTSIDE AIR |EXTERNAL HEAT | APU | SUPERVISOR | DRAINING OF | | TEMPERATURE | SOURCE | | | WATER SYSTEM | |--------------|--------------|--------------|--------------|--------------| | 0 deg.C | 1 HOUR | | | | | (32 deg.F) | | | | | | to | EVERY | NO | NO | NO | | -5 deg.C | | | | | | (23 deg.F) | 4 HOURS | | | | |--------------|--------------|--------------|--------------|--------------| | -5 deg.C | 2 HOURS | | | | | (23 deg.F) | | | | | | to | EVERY | NO | NO | NO | | -10 deg.C | | | | | | (14 deg.F) | 4 HOURS | | | | |--------------|--------------|--------------|--------------|--------------| | -10 deg.C | | | | | | (14 deg.F) | | | | | | to | CONTINUOUS | NO | NO | NO | | -15 deg.C | | | | | | (5 deg.F) | | | | | |--------------|--------------|--------------|--------------|--------------| | BELOW | | AS | | | | -15 deg.C | CONTINUOUS | REQUIRED | YES | YES | | (5 deg.F) | | | | | ---------------------------------------------------------------------------**ON A/C 301-399, Subtask 12-31-38-660-051-A B. Post Flight (Last Flight of the Day but not Transit Stops) (Ref. TASK 3831-00-680-801) (Ref. TASK 12-24-38-680-801) (1) General (a) Push the auto-flush pushbutton on the 5001VE panel. (This starts two flush cycles in the LD-LAVs to prevent waste deposit build up or freezing in the waste pipes). (b) Do the servicing of the potable water system and waste water tanks as soon as possible after a flight.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-31-38 301-399, 401-449, 451-499, 701-749, SROS
Page 206 Jul 01/05
(c) Read tables 1 and 2 (draining of the water and waste system) to find if it is necessary to drain the water and waste from the system. R R R R R R
(d) After draining of the system and parking of the aircraft at temperatures below 0 deg.C (32.00 deg.F): - Let the drain valves and the service panels stay open to let remaining fluid to flow out. - Do not install the caps on the drain and the fill/drain nipples.
R R R R R R R
NOTE : If you install the caps, the remaining fluid can freeze ____ immediately behind the drain and fill/drain caps and will cause: - Damage to the piping system - The system to become unserviceable - Delay at the next servicing. ------------------------------------------------------------------------------| TABLE 1 | |-----------------------------------------------------------------------------| | CONFIGURATION | | WATER | -------------------------------------------------|COLD SOAK TIME| AND | | AIR | CABIN | OUTSIDE AIR | (HOURS:MIN) | WASTE | | CONDITIONING | TEMPERATURE | TEMPERATURE | | TANKS DRAIN | |--------------|-------------|-------------------|--------------|-------------| | | | BETWEEN | | NOT | | | | 0 AND -15 deg.C | ANY | REQUIRED | | | ABOVE | (32 AND 5 deg.F) | | | | ON | 10 deg.C |-------------------|--------------|-------------| | | (50 deg.F) | BELOW | | | | | | -15 deg.C | 1:15 | | | | | (5 deg.F) | | | |--------------|-------------|-------------------|--------------| | | | | BETWEEN | | | | | | 0 AND -7 deg.C | 1:30 | | | | |(32 AND 19.4 deg.F)| | | | | |-------------------|--------------| | | OFF | | BETWEEN | | REQUIRED | | | | -7 AND -15 deg.C | 0:30 | | | | | (19.4 AND 5 deg.F)| | | | | |-------------------|--------------| | | | | BELOW | | | | | | -15 deg.C | ANY | | | | | (5 deg.F) | | | -------------------------------------------------------------------------------
EFF : 301-399, 12-31-38 SROS
Page 207 Jul 01/04
(2) Potable water system CAUTION : DO NOT OPEN THE ELECTRICAL DRAIN VALVES FOR LONGER THAN _______ NECESSARY IF YOU USE THE APU OR ENGINE(S) TO PRESSURIZE THE SYSTEM. IF THE VALVES STAY OPEN TOO LONG, THE HOT BLEED AIR CAN CAUSE DAMAGE TO THE TANK QUANTITY TRANSMITTER. (a) If you park the aircraft at very low temperature: - Drain the water from the potable water system, - Remove the remaining water from the potable water system, as stated below: 1 _
Drain the potable water system (Ref. TASK 12-24-38-680-801).
2 _
Close all the lavatory and galley manual shutoff valves.
3 _
Close all the potable-water drain and fill drain valves.
4 _
Pressurize the potable water system (Ref. TASK 38-10-00-614801).
5 _
To remove the remaining water from the potable water system do the procedure as follows: NOTE : This procedure is the same for all lavatories and ____ galleys which have potable water supplied equipment (as there are water heater, coffeemaker and water faucet). a _
Open one related manual shutoff valve of one lavatory or galley.
b _
Operate the faucet (HOT and COLD).
c _
Make sure that air but no water comes out of the faucet.
d _
Flush the toilet as often as necessary until you are sure that air but no water comes out of the toilet rinse valve.
e _
Close the related manual shutoff valve.
f _
Do the whole procedure for all lavatories and galleys which have potable-water supplied equipment.
EFF : 301-399, 12-31-38 R SROS
Page 208 Jul 01/04
R R R
6 _
Open all drain valves of the potable water system and release the pressure from the potable water system (Ref. TASK 38-1000-614-803).
R
7 _
Open the manual shutoff valves in all galleys and lavatories.
(b) If you cannot drain the potable water system: - Do the pre-conditioning of the aircraft (Ref. TASK 12-33-21618-801) as follows: ---------------------------------------------------------------------------| TABLE 2 | |--------------------------------------------------------------------------| | OUTSIDE AIR |EXTERNAL HEAT | APU | SUPERVISOR | DRAINING OF | | TEMPERATURE | SOURCE | | | WATER SYSTEM | |--------------|--------------|--------------|--------------|--------------| | 0 deg.C | 1 HOUR | | | | | (32 deg.F) | | | | | | to | EVERY | NO | NO | NO | | -5 deg.C | | | | | | (23 deg.F) | 4 HOURS | | | | |--------------|--------------|--------------|--------------|--------------| | -5 deg.C | 2 HOURS | | | | | (23 deg.F) | | | | | | to | EVERY | NO | NO | NO | | -10 deg.C | | | | | | (14 deg.F) | 4 HOURS | | | | |--------------|--------------|--------------|--------------|--------------| | -10 deg.C | | | | | | (14 deg.F) | | | | | | to | CONTINUOUS | NO | NO | NO | | -15 deg.C | | | | | | (5 deg.F) | | | | | |--------------|--------------|--------------|--------------|--------------| | BELOW | | AS | | | | -15 deg.C | CONTINUOUS | REQUIRED | YES | YES | | (5 deg.F) | | | | | ----------------------------------------------------------------------------
EFF : 301-399, 12-31-38 SROS
Page 209 Jul 01/03
COLD WEATHER MAINTENANCE - AIRBORNE AUXILIARY POWER - MAINTENANCE PRACTICES ___________________________________________________________________________ TASK 12-31-49-660-801 Cold Weather Maintenance Practices for the Auxiliary Power Unit 1. __________________ Reason for the Job This procedure gives the cold weather maintenance practices for the Auxiliary Power Unit (APU) when the aircraft is in a cold soak condition. 2. ______________________ Job Set-up Information A. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
Material No. 03-003
USA MIL-PRF-7808 LUBRICATING OIL TURBINE SYNTHETIC BASE (Ref. 20-31-00)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-31-24-660-801 12-33-21-618-801 12-33-21-618-801 12-33-21-618-801 24-41-00-861-801 49-00-00-860-801 49-00-00-860-801 49-00-00-860-802 49-61-34-000-801 49-61-34-400-801 49-91-00-600-801
Cold Weather Maintenances for Electrical Power Ground Air Pre-conditioning through the Low-Pressure Ground Connection Ground Air Pre-conditioning through the High-Pressure Ground Connection Ground Air Pre-conditioning with the APU Energize the Aircraft Electrical Circuits from the External Power A Start of the APU with Power Supply from the APU Battery Start of the APU with External Power Supply Shutdown of the APU with Power Supply from the APU Battery Removal of the ECB (59KD) Installation of the ECB (59KD) Oil Change
EFF : ALL 12-31-49 SROS
Page 201 Apr 01/99
3. __________ Job Set-up Subtask 12-31-49-941-050 A. Not applicable. 4. Procedure _________ Subtask 12-31-49-660-050 A. Electronic Control Box 59KD (ECB 59KD) (1) If the Outside Air Temperature (OAT) is/will be lower than -40 deg.C (-40.00 deg.F) and the aircraft is not pre-conditioned (heated) alternatively: - through the LP ground connection (Ref. TASK 12-33-21-618-801), - the HP ground connection (Ref. TASK 12-33-21-618-801), or - with the APU (Ref. TASK 12-33-21-618-801). (a) Remove the ECB 59KD from the aircraft (Ref. TASK 49-61-34-000801). (b) Keep the ECB 59KD in a dry storage at a temperature of between 15 deg.C (59.00 deg.F) and 35 deg.C (95.00 deg.F). Subtask 12-31-49-660-051 B. Auxiliary Power Unit (APU) NOTE : DO NOT MIX OILS OF DIFFERENT BRANDS OR TYPES| ____ NOTE : It is recommended to use type 1 oils OILS (Material No. 03-003) ____ for APU operation in cold weather conditions. (1) Oil type. (a) If necessary, do an oil change to type 1 OILS (Material No. 03003) (Ref. TASK 49-91-00-600-801). (2) Electrical power (Ref. TASK 12-31-24-660-801). (a) If external power is available. 1 _
Energize the aircraft electrical circuits from the external power (Ref. TASK 24-41-00-861-801).
EFF : ALL 12-31-49 SROS
Page 202 Apr 01/98
2 _
On the APU section on the overhead panel 215VU, make sure that the APU MASTER SW pushbutton switch is set to OFF (the ON legend is off). NOTE : The APU oil heater increases the temperature of the oil ____ in the APU gearbox oil reservoir during cold soak condition.
(b) If no external power is available. 1 _
It is recommended to start the APU every three hours and operate it for one hour (Ref. TASK 49-00-00-860-801) (Ref. TASK 49-00-00-860-802) if the Outside Air Temperature (OAT) is lower than -30 deg.C (-22.00 deg.F). NOTE : These values are only applicable if all the access ____ doors are closed.
Subtask 12-31-49-660-052 C. APU Starting after a Cold Soak Condition (1) ECB 59KD. NOTE : Do not operate the ECB 59KD for more than 30 minutes at -40 ____ deg.C (-40.00 deg.F) or lower. (a) If the ECB was on the aircraft during the cold soak, make sure that the temperature of the ECB is higher than -40 deg.C (-40.00 deg.F). If the temperature of the ECB is lower than -40 deg.C (-40.00 deg.F), use a pre-conditioning procedure to increase the temperature of the ECB to a minimum of -40 deg.C (-40.00 deg.F) (Ref. TASK 12-33-21-618-801) or (Ref. TASK 12-33-21-618-801). (b) If the ECB was removed from the aircraft and kept at a temperature of between 15 deg.C (59.00 deg.F) and 35 deg.C (95.00 deg.F), install the ECB (Ref. TASK 49-61-34-400-801). (2) Electrical Power. (a) For the cold weather maintenance - electrical power (Ref. TASK 12-31-24-660-801). (b) Start and operate the APU (Ref. TASK 49-00-00-860-801).
EFF : ALL 12-31-49 SROS
Page 203 Apr 01/98
Subtask 12-31-49-660-053 D. Turn-Around Time For turn-around in cold weather conditions, when it is not pratical to remove equipment, it is recommended to keep the APU in operation. In this configuration : - the temperature in the cabin will not decrease, - no specific cold weather maintenance practices are necessary for the APU system.
EFF : ALL 12-31-49 SROS
Page 204 Apr 01/98
COLD WEATHER MAINTENANCE - STRUCTURE - MAINTENANCE PRACTICES ____________________________________________________________ TASK 12-31-51-660-801 Cold Weather Maintenance Practices for the Structure. 1. __________________ Reason for the Job This procedure gives the cold weather maintenance practices for the structure. 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------53-00-00-000-803 53-00-00-200-803 53-00-00-400-803
Removal of the Floor Panels in the AFT Cargo Compartment Visual Check of the Piston Drain Valves in the Lower Fuselage Shell (from Outside) and in the FWD and AFT Cargo Compartment Doors Installation of the Floor Panels in the AFT Cargo Compartment
3. __________ Job Set-up Subtask 12-31-51-941-050 A. Not applicable. 4. Procedure _________ Subtask 12-31-51-660-050 A. General (1) At the start of each winter, make sure that the drain valves in the lower fuselage are clean and operate correctly. (Ref. TASK 53-00-00200-803)
EFF : ALL 12-31-51 SROS
Page 201 Apr 01/98
(2) Ice can collect in the lower fuselage areas especially when the aircraft flies from warm, humid climates to cold climates. In some conditions, the ice can collect during more than one flight. NOTE : Water/ice in the lower fuselage can cause failure of the radio ____ altimeter. (3) When you do a check for ice in the lower fuselage, look for ice in the aft area before you look in the forward area. Ice usually collects more easily in the aft area than in the forward area. Water evaporation is faster in the forward area because of the warnm air from the avionics compartment. Subtask 12-31-51-660-051 B. Check for Ice (1) Remove a floor panel from the forward end of the aft cargo compartment. (Ref. TASK 53-00-00-000-803) (2) Look for ice in the lower fuselage. (3) If you find ice below the aft cargo compartment, look for ice below the forward cargo compartment. (4) Install the floor panel (Ref. TASK 53-00-00-400-803). (5) Frequency of check You must adapt the frequency of the check to the climatic conditions in whichthe aircraft operates. In the worst condition one check per week should be sufficient initially. Subtask 12-31-51-660-052 C. Removal of Ice (1) Warm hangar The recommended procedure is to put the aircraft in a warm hangar with cargo bay doors open. This will cause all the ice in the aircraft to melt and the water will flow out through the drain valves.
EFF : ALL 12-31-51 SROS
Page 202 Apr 01/98
(2) Hot air blower CAUTION : MAKE SURE THAT THE TEMPERATURE OF THE AIR FROM THE HOT AIR _______ BLOWER IS NOT MORE THAN 50 DEG.C (122 DEG.F). IF THE TEMPERATURE IS MORE THAN 50 DEG.C (122 DEG.F) YOU CAN CAUSE DAMAGE TO THE AIRCRAFT. You can use a hot air blower if the aircraft is parked in an open area. (3) Frequency of ice removal You must adapt the frequency of ice removal to the climatic conditions in which the aircraft operates. In the worst conditions, one overnight stop a week is usually sufficient for ice removal. (4) The procedure used to remove ice from the lower fuselage must be monitored to make sure that all water drains are working and that all the ice is removed.
EFF : ALL 12-31-51 SROS
Page 203 Apr 01/98
COLD WEATHER MAINTENANCE - DOORS - MAINTENANCE PRACTICES ________________________________________________________ TASK 12-31-52-660-801 Cold Weather Maintenance Procedures for the Doors System 1. __________________ Reason for the Job This procedure gives the cold weather maintenance practices for the doors system. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 HOT AIR BLOWER OPERATING 40 DEG C (100 DEG F)
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 04-011 R
Material No. 04-017 Material No. 05-001 Material No. 11-004 Material No. 15-005A Material No. 19-003
USA MIL-G-4343 SILICONE GREASE PNEUMATIC SYST AND SEALS (Ref. 20-31-00) USA A-A-59173 SILICONE GREASE (Ref. 20-31-00) USA SAE-AS8660 INSULATING AND SEALING GREASE SILICONE (Ref. 20-31-00) USA MIL-T-81533 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (Ref. 20-31-00) AIB TN 10138 TYPE I GRADE 2 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
EFF : ALL 12-31-52 SROS
Page 201 Oct 01/04
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R
12-22-52-600-809 52-10-00-860-801 52-10-00-860-802 52-20-00-860-801 52-20-00-860-802 52-30-00-010-801 52-30-00-010-803 52-30-00-410-801 52-30-00-410-803 52-30-00-480-801 52-31-15-000-801 52-31-15-400-801 52-32-15-000-801 52-32-15-400-801 52-33-15-000-801 52-33-15-400-801
Lubrication of the Slider Mechanism on all Pax/Crew and Emergency Exit Doors Special Precautions before Work on the Passenger/Crew Door Special Precautions after Work on the Passenger/Crew Door Special Precautions before Work on the Emergency Exit Door Special Precautions after Work on the Emergency Exit Door Opening of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Opening of the BULK Cargo-Compartment Door Closing of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Closing of the BULK Cargo-Compartment Door Installation of the Safety Support Equipment Removal of the Protection Linings Installation of the Protection Linings Removal of the Protection Linings Installation of the Protection Linings Removal of the Protection Lining Installation of the Protection Lining
3. __________ Job Set-up Subtask 12-31-52-941-050 A. Get Access (1) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the applicable passenger/crew door, emergency exit door, cargo door, fuselage service panel or fuselage access door. (2) Do the related special precautions, then open the applicable passenger/crew door (Ref. TASK 52-10-00-860-801). (3) Do the related special precautions, then open the applicable emergency exit door (Ref. TASK 52-20-00-860-801).
EFF : ALL 12-31-52 SROS
Page 202 Jan 01/06
(4) Open the FWD and/or AFT cargo-compartment door (Ref. TASK 52-30-00010-801) and install the related actuator safety lock(s) (Ref. TASK 52-30-00-480-801). (5) Remove the protection linings from the FWD and/or AFT cargo-compartment door (Ref. TASK 52-31-15-000-801) and (Ref. TASK 52-32-15-000-801). (6) Open the BULK cargo-compartment door (Ref. TASK 52-30-00-010-803). (7) Remove the protection linings from the BULK cargo-compartment door (Ref. TASK 52-33-15-000-801). (8) Remove/open the applicable fuselage service panel(s) and/or access door(s). 4. Procedure _________ Subtask 12-31-52-660-055 A. Winter Preparation (1) Winter preparation of the passenger crew doors and the emergency exits. (a) Make sure that the pressure seal drains and the drain holes of the passenger/crew doors and the emergency exits are clear and not blocked. R R
(b) Make sure that the slider mechanism is correctly lubricated (Ref. TASK 12-22-52-600-809).
R R R
(c) Use a lint-free cotton cloth, MISCELLANEOUS (Material No. 19003), and the CLEANING AGENTS (Material No. 11-004) to clean these components of the passenger/crew doors and the emergency exits: - the door guide rollers, the roller fittings and the upper and lower door guide fittings - the pressure seals and their contact areas on the fuselage.
R R
(d) Apply the silicone grease, COMMON GREASE (Material No. 04-017), to the door guide rollers, the roller fittings and the upper and lower guide fittings.
R R
(e) Apply the silicone grease, SPECIAL MATERIALS (Material No. 05001), to the pressure seals and to their contact areas on the fuselage.
EFF : ALL 12-31-52 SROS
Page 203 Jan 01/06
R R
(f) Apply the temporary protective compound, STORAGE PRESERVATION (Material No. 15-005A), to these areas of the passenger/crew doors and the emergency exits: - the inner surfaces and the structure - the exterior control handle assemblies. (2) Winter preparation of the FWD, AFT and BULK cargo-compartment doors. (a) Make sure that the pressure seal drains of the cargo-compartment doors are clear and not blocked.
R R R
(b) Use a lint-free cotton cloth, MISCELLANEOUS (Material No. 19003), and the CLEANING AGENTS (Material No. 11-004) to clean these components of the applicable cargo-compartment doors: - the pressure seals and their contact areas on the fuselage - the external operating handles - the door hinges and the guide fittings - the internal mechanisms of the lock shafts, the operating handles and the latch assemblies.
R R R
(c) Apply the silicone grease, SPECIAL MATERIALS (Material No. 05001), and the silicone grease, COMMON GREASE (Material No. 04011) to the pressure seals.
R R
(d) Apply the temporary protective compound, STORAGE PRESERVATION (Material No. 15-005A), to the external control handles and the shafts.
R R
(e) Lubricate the door hinges and guide fittings. Apply the temporary protective compound, STORAGE PRESERVATION (Material No. 15-005A), to the latch assemblies and the latch spools. (f) Lubricate the internal operating mechanisms of the doors (lock shafts, operating handles and latch assemblies).
R R R
(g) Apply the temporary protective compound, STORAGE PRESERVATION (Material No. 15-005A), as a spray, to the lower internal bays of the doors. Subtask 12-31-52-660-050 B. Passenger/Crew Doors and Emergency Exit Doors (Before Flight) (1) Remove all the snow and slush from the subsequent areas before you close a passenger/crew door or an emergency exit door: - the door pressure seal - the seal contact area on the fuselage.
EFF : ALL 12-31-52 SROS
Page 204 Jan 01/06
Subtask 12-31-52-660-051 C. FWD, AFT and BULK Cargo-Compartment Doors (Before Flight) CAUTION : MAKE SURE THAT THE TEMPERATURE OF THE AIR FROM THE HOT AIR _______ BLOWER IS NOT MORE THAN 50 DEG.C (122 DEG.F). IF THE TEMPERATURE IS MORE THAN 50 DEG.C (122 DEG.F) YOU CAN CAUSE DAMAGE TO THE AIRCRAFT. (1) Remove as much snow and/or water as possible from the cargo pallets before you install them in the aircraft. NOTE : Large quantities of melting snow and water can cause the ____ cargo-compartment doors to freeze in their closed positions. (2) Do not open the cargo-compartment doors until immediately before you install the cargo pallets. (3) Close the cargo-compartment doors immediately after the installation of the cargo pallets is complete. (4) If the aircraft is parked in a hangar, open the cargo-compartment doors to their vertical positions. NOTE : This procedure will help to remove the moisture from the inner ____ surfaces of the doors. R
(5) Use a HOT AIR BLOWER OPERATING 40 DEG C (100 DEG F) to remove the ice from doors or panels that are frozen in their closed positions. Do not use hard or sharp tools to remove the ice. Subtask 12-31-52-660-052 D. Passenger/Crew Doors and Emergency Exits (After Flight) (1) Aircraft not parked in a hangar (a) Remove the snow and/or slush from the subsequent areas before you close the passenger/crew doors and/or the emergency exits: - the door pressure seals - the door contact areas on the fuselage. (b) Use a lint-free cotton cloth, MISCELLANEOUS (Material No. 19-003) and the CLEANING AGENTS (Material No. 11-004) to clean the pressure seals of the passenger/crew doors and the emergency exits.
EFF : ALL 12-31-52 SROS
Page 205 Apr 01/04
(c) Apply the silicone grease, SPECIAL MATERIALS (Material No. 05001) to the pressure seals of the passenger/crew doors and the emergency exits. (d) Make sure that the pressure seal drains and the drain holes of the passenger/crew doors and the emergency exits are clear and not blocked. (2) Aircraft parked in a hangar (a) Open the passenger/crew doors and the emergency exits. NOTE : This procedure will help to remove the moisture from the ____ inner surfaces of the doors. Subtask 12-31-52-660-053 E. FWD, AFT and BULK Cargo-Compartment Doors (After Flight) (1) Remove the snow and/or slush from the subsequent areas before you close the cargo-compartment doors: - the door pressure seals - the door contact areas on the fuselage. (2) If the aircraft flies from an airport where the ambient temperature is more than 0 deg.C (32.00 deg.F) to an airport where the ambient temperature is less than 0 deg.C (32.00 deg.F), you must: (a) Apply the temporary protective compound, STORAGE PRESERVATION (Material No. 15-005A) as a spray, to the subsequent areas of the cargo-compartment doors: - the operating mechanisms - the inner surfaces of the lower areas of the cargo doors. NOTE : This procedure will keep the effects of freezing ____ condensation to a minimum at cold airports. (3) Maintenance NOTE : The frequency of the subsequent procedure may be increased as ____ required by the operating environment. (a) Make sure that the pressure seal drains of the cargo-compartment doors are clear and not blocked.
EFF : ALL 12-31-52 R SROS
Page 206 Oct 01/02
(b) Use a lint-free cotton cloth, MISCELLANEOUS (Material No. 19-003) and the CLEANING AGENTS (Material No. 11-004) to clean these components of the applicable cargo-compartment doors: - the pressure seals and their contact areas on the fuselage R - the external operating handles - the door hinges and the guide fittings.
R
(c) Apply the silicone grease, SPECIAL MATERIALS (Material No. 05001) and the silicone grease, COMMON GREASE (Material No. 04-011) to the pressure seals. R R R R
(d) Apply the temporary protective compound, STORAGE PRESERVATION (Material No. 15-005A) to the external control handles and the shafts.
R
(e) Lubricate the door hinges and the guide fittings. Apply the temporary protective compound, STORAGE PRESERVATION (Material No. 15-005A) to the latch assemblies and the latch spools. Subtask 12-31-52-660-054 F. Service Panels (1) Apply the temporary protective compound, STORAGE PRESERVATION (Material No. 15-005A) as a spray, to the hinges and latch mechanisms of the fuselage service panels and doors. 5. Close-up ________ Subtask 12-31-52-942-050 A. Put the aircraft back to its operational configuration. (1) Make sure that the work area is clean and clear of tools and other items. (2) Do the related special precautions, then close the applicable passenger/crew doors (Ref. TASK 52-10-00-860-802). (3) Do the related special precautions, then close the applicable emergency exit doors (Ref. TASK 52-20-00-860-802). (4) Install the protection linings on the FWD and/or AFT cargo-compartment door (Ref. TASK 52-31-15-400-801) and (Ref. TASK 52-32-15-400-801).
EFF : ALL 12-31-52 SROS
Page 207 Oct 01/02
(5) Remove the actuator safety lock(s) and close the FWD and/or AFT cargo-compartment door (Ref. TASK 52-30-00-410-801). (6) Install the protection linings on the BULK cargo-compartment door (Ref. TASK 52-33-15-400-801). (7) Close the BULK cargo-compartment door (Ref. TASK 52-30-00-410-803). (8) Close/Install the applicable fuselage service panel(s) and/or access door(s). (9) Remove the access platform(s).
EFF : ALL 12-31-52 R SROS
Page 208 Oct 01/02
COLD WEATHER MAINTENANCE - POWER PLANT - MAINTENANCE PRACTICES ______________________________________________________________ TASK 12-31-71-660-801 Cold Weather Maintenance Practices of Engines 1. __________________ Reason for the Job This procedure gives the cold weather maintenance practices for the engines. 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------71-00-00-660-801 71-00-00-660-802 71-00-00-860-844
Prepare the Engine After Shutdown in Cold Weather. Prepare the Engine Before Starting in Cold Weather Power Plant Operation During Cold Weather
3. __________ Job Set-up Subtask 12-31-71-941-050 A. Not applicable. 4. Procedure _________ R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 12-31-71-660-050-A A. General (1) Prepare the engine in cold weather conditions (Ref. TASK 71-00-00660-802) and (Ref. TASK 71-00-00-660-801).
EFF : ALL 12-31-71 SROS
Page 201 Jul 01/05
R
**ON A/C 701-749,
R
Subtask 12-31-71-660-050-B
R
A. General
R R
(1) Do the power plant operation during cold weather (Ref. TASK 71-00-00860-844).
EFF : 701-749, 12-31-71 SROS
Page 202 Oct 01/03
SAMPLING FOR ANALYSIS - DESCRIPTION AND OPERATION _________________________________________________ R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 1. General _______ This section gives the instructions related to the different fluid samplings which may be done for an analysis. It includes the topics below: 12-23-24/P. Block 301 INTEGRATED DRIVE GENERATOR OIL 12-32-28/P. Block 301 FUEL 12-32-29/P. Block 301 HYDRAULIC FLUID 12-32-49/P Block 301 APU 12-32-79/P. Block 301 ENGINE OIL **ON A/C 701-749, 1. General _______ This section gives the instructions related to the different fluid samplings which may be done for an analysis. It includes the topics below: 12-23-24/P. Block 301 INTEGRATED DRIVE GENERATOR OIL 12-32-28/P. Block 301 FUEL 12-32-29/P. Block 301 HYDRAULIC FLUID 12-32-49/P Block 301 APU
EFF : ALL 12-32-00 SROS
Page 1 Jul 01/05
INTEGRATED DRIVE GENERATOR OIL - SERVICING __________________________________________ TASK 12-32-24-281-803 Sampling of the IDG Oil for Analysis WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE COMPONENTS IMMEDIATELY AFTER _______ THE ENGINE IS SHUTDOWN. THE ENGINE COMPONENTS CAN STAY HOT FOR UP TO ONE HOUR. WARNING : WEAR GOGGLES, INSULATED GLOVES AND OTHER PROTECTIVE CLOTHES. _______ HOT OIL CAN BURN YOUR EYES AND SKIN. IF OIL TOUCHES YOUR EYES OR SKIN, GET MEDICAL AID. 1. __________________ Reason for the Job To find the cause of the oil contamination (skydrol, fuel, water, chlorine, oil, degradation and other causes). NOTE : The best location and time to get an oil sample is at the case drain ____ after operation of the engine, when the IDG oil is at the operating temperature (80 deg. C (176 deg. F)). 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No
specific specific specific specific specific
DH13PM
circuit breaker(s) safety clip(s) container 5.7 l (1.5 USgal) transparent bottle 1 l (0.26 USgal) access platform 2.5 m (8 ft. 2 in.) Torque Wrench : range 36.00 to 220.00 lbf.in (0.40 to 2.60 m.daN) 1 TANK - ENGINE OIL FILLING UP
R EFF : 001-049, 201-249, 251-252, 255-299, 12-32-24 Page 301 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
P05-289
Material No. 03-002
* lockwire 0.032 in. (0.80 mm) dia. (Ref. 70-30-00) GB DEF-STAN 91-101 LUBRICATING OIL TURBINE ENGINE SYNT BASE (Ref. 20-31-00)
C. Expendable Parts ------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ------------------------------------------------------------------------------2
O-ring
24-21-51 42A-060
D. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-13-24-610-801 24-42-00-861-801 24-42-00-862-801 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801 78-30-00-040-804 78-30-00-410-801 78-30-00-440-804 12-32-24-991-004
IDG Servicing - Filling of the IDG with Oil or Addition of Oil after a Level Check Energize the Ground Service Network De-energize the Ground Service Network Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Deactivation of the Thrust Reverser for Maintenance Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Reactivation of the Thrust Reverser after Maintenance Fig. 301
R EFF : 001-049, 201-249, 251-252, 255-299, 12-32-24 Page 302 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
3. __________ Job Set-up Subtask 12-32-24-861-052 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-32-24-941-052 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure. Subtask 12-32-24-010-054 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU. Subtask 12-32-24-865-054 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-32-24-010-055 E. Get Access (1) Open the aft fan cowl doors (Ref. TASK 71-13-00-010-802): - FOR 4030EM1 415BL, 416BR, - FOR 4030EM2 425BL, 426BR.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-32-24 Page 303 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
Subtask 12-32-24-040-050 F. Deactivation of the Thrust Reverser WARNING : YOU MUST DEACTIVATE THE THRUST REVERSER DIRECTIONAL CONTROL _______ VALVE (DCV) BEFORE YOU WORK ON OR AROUND THE TRANSLATING COWL. IF YOU DO NOT DEACTIVATE THE DCV, YOU CAN CAUSE ACCIDENTAL THRUST REVERSER OPERATION AND INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT. (1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 7830-00-040-804). Subtask 12-32-24-010-058 G. Get Access (1) Open the thrust reverser cowl doors (Ref. TASK 78-30-00-010-801): FOR 4030EM1 417AL, 418AR, FOR 4030EM2 427AL, 428AR. 4. Procedure _________ (Ref. Fig. 301/TASK 12-32-24-991-004) Subtask 12-32-24-864-052 A. Depressurization of the IDG Case WARNING : POINT THE OVERFLOW DRAIN HOSE INTO A CONTAINER WHEN YOU CONNECT _______ THE HOSE TO THE OVERFLOW DRAIN VALVE. THIS WILL PREVENT BURNS FROM THE HOT OIL SPRAY. HOT OIL CAN CAUSE BURNS TO EYES AND SKIN. CAUTION : DO NOT USE DEVICES OTHER THAN THE APPROVED OVERFLOW DRAIN-HOSE _______ FITTING. HARD METAL OBJECTS SUCH AS SCREWDRIVERS CAN CAUSE DAMAGE TO THE OVERFLOW DRAIN-VALVE SEAT. (1) Put a container 5.7 l (1.5 USgal) below the IDG. (2) Remove the dust cap (4) from the overflow drain valve (8). (3) Put the end of the overflow drain hose (7) of the TANK - ENGINE OIL FILLING UP (DH13PM) in the container (6).
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IDG Oil Sampling for Analysis Figure 301/TASK 12-32-24-991-004 R EFF : 001-049, 201-249, 251-252, 255-299, 12-32-24 Page 305 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
(4) Do this step to depressurize the IDG case: (a) Connect the overflow drain hose (7) of the TANK - ENGINE OIL FILLING UP (DH13PM) to the overflow drain valve (8). NOTE : Some oil can come out of the overflow drain hose (7) of ____ the TANK - ENGINE OIL FILLING UP (DH13PM) when you connect it. Subtask 12-32-24-281-054 B. Oil Sampling WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. _______ CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU. NOTE : Make sure that the oil is not too hot. ____ (1) Cut and remove the lockwire from the case drain plug (1). (2) Loosen the case drain plug (1). (3) Put a transparent bottle 1 l (0.26 USgal) below the case drain port (3). NOTE : The transparent bottle (5) must be clean and sterilized. ____ (4) Slowly remove the case drain plug (1) until oil flows out of the case drain port (3). (5) Fill the transparent bottle (5) with approximately 20 ml (0.0053 USgal) of oil. (6) Seal the case drain port (3). (7) Remove the O-ring (2) from the case drain plug (1) and discard it. Subtask 12-32-24-640-052 C. Lubricate the new O-ring (2) with OILS (Material No. 03-002).
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Subtask 12-32-24-420-052 D. Installation of the Case Drain Plug (1) Install the new O-ring (2) on the case drain plug (1). (2) Install the case drain plug (1) in the case drain port (3). (3) TORQUE the case drain plug (1) to between 55 and 75 lbf.in (0.62 and 0.84 m.daN). (4) Safety the case drain plug (1) with lockwire 0.032 in. (0.80 mm) dia. (Material No. P05-289). Subtask 12-32-24-281-055 E. Oil Sample Bottle (1) Send the oil sample bottle to laboratory immediately with these data: (a) Oil sampling date. (b) Type and brand of oil used. (c) Operating time since last oil sampling. (d) IDG total operating time. (e) Identification of the IDG (Serial Number). NOTE : If you do not do the analysis immediately, seal the ____ bottle. Subtask 12-32-24-020-052 F. Removal of the Overflow Drain Hose (1) Disconnect the overflow drain hose (7) of the TANK - ENGINE OIL FILLING UP (DH13PM) from the overflow drain valve (8). (2) Install the dust cap (4) on the overflow drain valve (8). Subtask 12-32-24-612-052 G. Fill the IDG with oil or add oil to the IDG after a level check (Ref. TASK 12-13-24-610-801).
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5. Close-up ________ Subtask 12-32-24-410-054 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the thrust reverser cowl doors (Ref. TASK 78-30-00-410-801): - FOR 4030EM1 417AL, 418AR, - FOR 4030EM2 427AL, 428AR. Subtask 12-32-24-440-050 B. Make the thrust reverser serviceable after maintenance (Ref. TASK 78-3000-440-804). Subtask 12-32-24-865-055 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2 Subtask 12-32-24-410-052 D. Close Access (1) Close the protective door of the AC/DC emergency power center 740VU. (2) Close the access door 811. (3) Remove the access platform(s). (4) Close the aft fan cowl doors (Ref. TASK 71-13-00-410-802): - FOR 4030EM1 415BL, 416BR, - FOR 4030EM2 425BL, 426BR.
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Subtask 12-32-24-862-052 E. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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INTEGRATED DRIVE GENERATOR OIL - SERVICING __________________________________________ TASK 12-32-24-281-804 Sampling of the IDG Oil for Analysis WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE COMPONENTS IMMEDIATELY AFTER _______ THE ENGINE IS SHUTDOWN. THE ENGINE COMPONENTS CAN STAY HOT FOR UP TO ONE HOUR. WARNING : WEAR GOGGLES, INSULATED GLOVES AND OTHER PROTECTIVE CLOTHES. _______ HOT OIL CAN BURN YOUR EYES AND SKIN. IF OIL TOUCHES YOUR EYES OR SKIN, GET MEDICAL AID. 1. __________________ Reason for the Job To find the cause of the oil contamination (skydrol, fuel, water, chlorine, oil, degradation and other causes). R R R
NOTE : The best location and time to get an oil sample is at the case drain ____ after operation of the engine, when the IDG oil is at the operating temperature (80 deg.C (176 deg.F)). 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No
specific specific specific specific specific
DH13PM
circuit breaker(s) safety clip(s) container 5.7 l (1.5 USgal) transparent bottle 1 l (0.26 USgal) access platform 2.5 m (8 ft. 2 in.) Torque Wrench : range 36.00 to 220.00 lbf.in (0.40 to 2.60 m.daN) 1 TANK - ENGINE OIL FILLING UP
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B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No.
OMAT 238
Material No. 03-002
* lockwire 0.028 to 0.031 in.(0.71 to 0.79 mm) dia. (Ref. 70-30-00) GB DEF-STAN 91-101 LUBRICATING OIL TURBINE ENGINE SYNT BASE (Ref. 20-31-00)
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C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-13-24-612-808 24-42-00-861-801 24-42-00-862-801 71-13-00-010-805 71-13-00-410-805 78-31-00-040-805 78-31-00-440-805 12-32-24-991-002
IDG Servicing - Filling of the IDG with Oil or Addition of Oil after Level Check Energize the Ground Service Network De-energize the Ground Service Network Open the Fan Cowl Doors Close the Fan Cowl Doors Deactivation of the Thrust Reverser for Maintenance Activation of the Thrust Reverser after Maintenance Fig. 301
3. __________ Job Set-up Subtask 12-32-24-861-053 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-32-24-941-053 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure.
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Subtask 12-32-24-010-056 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU. Subtask 12-32-24-865-056 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-32-24-010-057 E. Get Access (1) Open the fan cowl doors (Ref. TASK 71-13-00-010-805): - FOR 4030EM1 415AL, 416AR, - FOR 4030EM2 425AL, 426AR. Subtask 12-32-24-040-053 F. Deactivation of the Thrust Reverser WARNING : YOU MUST DEACTIVATE THE THRUST REVERSER BEFORE YOU DO WORK ON _______ OR AROUND IT. IF YOU DO NOT, THE THRUST REVERSER CAN OPERATE ACCIDENTALLY AND CAUSE INJURY AND/OR DAMAGE. (1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 7831-00-040-805).
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4. Procedure _________ (Ref. Fig. 301/TASK 12-32-24-991-002) Subtask 12-32-24-864-053 A. Depressurization of the IDG Case WARNING : POINT THE OVERFLOW DRAIN HOSE INTO A CONTAINER WHEN YOU CONNECT _______ THE HOSE TO THE OVERFLOW DRAIN VALVE. THIS WILL PREVENT BURNS FROM THE HOT OIL SPRAY. HOT OIL CAN CAUSE BURNS TO EYES AND SKIN. CAUTION : DO NOT USE DEVICES OTHER THAN THE APPROVED OVERFLOW DRAIN-HOSE _______ FITTING. HARD METAL OBJECTS SUCH AS SCREWDRIVERS CAN CAUSE DAMAGE TO THE OVERFLOW DRAIN-VALVE SEAT. (1) Put a container 5.7 l (1.5 USgal) below the IDG. (2) Remove the dust cap (4) from the overflow drain valve (2). (3) Put the end of the overflow drain hose (8) of the TANK - ENGINE OIL FILLING UP (DH13PM) in the container (7). (4) Do this step to depressurize the IDG case: (a) Connect the overflow drain hose (8) of the TANK - ENGINE OIL FILLING UP (DH13PM) to the overflow drain valve (2). NOTE : Some oil can come out of the overflow drain hose (8) of ____ the TANK - ENGINE OIL FILLING UP (DH13PM) when you connect it. Subtask 12-32-24-281-056 B. Oil Sampling WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. _______ CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU. NOTE : Make sure that the oil is not too hot. ____ (1) Cut and remove the lockwire from the case drain plug (6). (2) Loosen the case drain plug (6).
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IDG Oil Sampling for Analysis Figure 301/TASK 12-32-24-991-002 EFF : 701-749, 12-32-24 Page 305 Config-2 Oct 01/00 SROS
(3) Put a transparent bottle 1 l (0.26 USgal) below the case drain port (1). NOTE : The transparent bottle (3) must be clean and sterilized. ____ (4) Slowly remove the case drain plug (6) until oil flows out of the case drain port (1). (5) Fill the transparent bottle (3) with approximately 20 ml (0.0053 USgal) of oil. (6) Seal the case drain port (1). (7) Remove the O-ring (5) from the case drain plug (6) and discard it. Subtask 12-32-24-640-053 C. Lubricate the new O-ring (5) with OILS (Material No. 03-002). Subtask 12-32-24-420-053 D. Installation of the Case Drain Plug (1) Install the new O-ring (5) on the case drain plug (6). (2) Install the case drain plug (6) in the case drain port (1). (3) TORQUE the case drain plug (6) to between 55 and 75 lbf.in (0.62 and 0.84 m.daN). (4) Safety the case drain plug (6) with lockwire 0.028 to 0.031 in.(0.71 to 0.79 mm) dia. (Material No. OMAT 238). Subtask 12-32-24-281-057 E. Oil Sample Bottle (1) Send the oil sample bottle to laboratory immediately with these data: (a) Oil sampling date. (b) Type and brand of oil used. (c) Operating time since last oil sampling. (d) IDG total operating time.
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(e) Identification of the IDG (Serial Number). NOTE : If you do not do the analysis immediately, seal the ____ bottle. Subtask 12-32-24-020-053 F. Removal of the Overflow Drain Hose (1) Disconnect the overflow drain hose (8) of the TANK - ENGINE OIL FILLING UP (DH13PM) from the overflow drain valve (2). (2) Install the dust cap (4) on the overflow drain valve (2). Subtask 12-32-24-612-053 G. Fill the IDG with oil or add oil to the IDG after a level check (Ref. TASK 12-13-24-612-808). 5. Close-up ________ Subtask 12-32-24-440-053 A. Make the thrust reverser serviceable after maintenance (Ref. TASK 78-3100-440-805). Subtask 12-32-24-865-057 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2 Subtask 12-32-24-410-053 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Close the access door 811. (4) Remove the access platform(s).
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(5) Close the fan cowl doors (Ref. TASK 71-13-00-410-805): - FOR 4030EM1 415AL, 416AR, - FOR 4030EM2 425AL, 426AR. Subtask 12-32-24-862-053 D. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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FUEL - SERVICING ________________ TASK 12-32-28-281-810 Operate Water Drain Valves to Drain Accumulated Water from Center, Inner, Outer and Wing Vent Surge Tanks WARNING : DO NOT GET AIRCRAFT FUEL: _______ - IN YOUR MOUTH - IN YOUR EYES - ON YOUR SKIN FOR A LONG TIME. WARNING : DO NOT GET YOUR CLOTHES SOAKED WITH FUEL. _______ AIRCRAFT FUEL IS POISONOUS AND CAN GO THROUGH YOUR SKIN INTO YOUR BODY. IF YOU ARE CONTAMINATED WASH WITH CLEAN WATER AND IF NECESSARY GET MEDICAL HELP. WARNING : MAKE SURE THAT YOU HAVE THE CORRECT FIRE FIGHTING EQUIPMENT _______ AVAILABLE. R R
CAUTION : ALWAYS USE THE CORRECT TOOL TO OPEN THE WATER DRAIN VALVE. THIS CAN _______ PREVENT DAMAGE TO THE SEALS. 1. __________________ Reason for the Job Refer to the MPD TASK: 281100-10 NOTE : If you operate the water drains more frequently than the MPD ____ interval, you can prevent these long-term problems: - decreased precision of the fuel quantity indications - the risk of corrosion from microbiological contamination. NOTE : You must operate the water drains more frequently if you find a high ____ water content when you do this procedure. NOTE : The conditions to operate the water drains are best when the fuel ____ temperature is more than 5 deg.C. NOTE : If possible, do the water drain procedure before you refuel. If you ____ refuel the aircraft before you do this procedure, the water and the fuel will mix. Because of this, you must wait one hour for the separation of the water and the fuel before you can drain the water from the tank.
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NOTE : For the gravity procedure AIRBUS recommends that there must be more ____ than 10% content of fuel in each tank. If you have less than 10%
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content of fuel, then the indirect water drain valves will have a decreased flow. It is recommended that you use the suction procedure when you have less than 10% content of fuel. R
NOTE : This task can contribute to fuel savings. ____ 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific No specific No specific 97A28002117002 98A28104000000
hose hydrokit suction pump transparent glass container 1 l (0.2641 USgal) container 10 l (2.6416 USgal) 1 PURGING TOOL 1 PURGER, WATER DRAIN
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-31-28-660-801 12-32-28-281-812 28-00-00-610-801 12-32-28-991-001-A 12-32-28-991-003-A
Cold Weather Maintenance Practices for the Fuel System Sample Fuel for Microbiological Contamination Analysis Fuel Safety Procedures Fig. 301 Fig. 302
3. __________ Job Set-up Subtask 12-32-28-941-061 A. Safety Precautions WARNING : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND _______ DAMAGE. (1) Obey the fuel safety procedures (Ref. TASK 28-00-00-610-801).
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R R R R
(2) If the fuel temperature is less than , -5 deg.C (+23.00 deg.F) water in the fuel tanks and/or water drain valves may be frozen). To keep the flight turnaround times, do the cold weather maintenance practices for the fuel system (Ref. TASK 12-31-28-660-801). 4. Procedure _________ (Ref. Fig. 301/TASK 12-32-28-991-001-A, 302/TASK 12-32-28-991-003-A) Subtask 12-32-28-680-062 A. Operate Water Drain Valves to Drain Accumulated Water from Center, Inner, Outer and Wing Vent Surge Tanks WARNING : MAKE SURE THE AREA AROUND THE AIRCRAFT IS SAFE BEFORE YOU START _______ A REFUEL/DEFUEL PROCEDURE. IN THIS SAFE AREA, DO NOT LET PERSONS: - SMOKE - MAKE SPARKS OR FIRE - USE ANY EQUIPMENT WHICH IS NOT APPROVED FOR THE TASK. AIRCRAFT FUEL IS FLAMMABLE. NOTE : During this procedure you must continue to operate all the drain ____ valves until no more water comes out. NOTE : AIRBUS recommends that you do a test for microbial contamination, ____ in not more than 10 days, if: - the sample you drain from the tank has a strong sulphide smell - you can see objects in the sample (Ref. TASK 12-32-28-281-812). (1) Gravity procedure
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(a) Push the center of the applicable water drain valve with the PURGER, WATER DRAIN. Drain approximately 1.0 l (0.2641 USgal) of fuel (as a sample) from the drain valve.
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(b) Remove the PURGER, WATER DRAIN from the drain valve. (c) Examine the drain valve for leaks. (d) Do this procedure at all of the water drain valves.
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Water Drain Valves - Location Figure 301/TASK 12-32-28-991-001-A
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Water Drain Valves - Location For Suction Procedure Figure 302/TASK 12-32-28-991-003-A
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(2) Suction procedure (a) On the PURGING TOOL, disconnect the funnel from the bottle. (b) Attach one end of the hose to the funnel and attach the other end of the hose to the suction pump. NOTE : The illustration shows a typical suction pump with an air ____ drill power source. The suction pump used must be a type approved for use on a fuel system and the applicable safety precautions must be taken. (c) Put the outlet of the suction pump into the container and start the suction pump. (d) Push the center of the applicable water drain valve with the funnel. Drain approximately 1.0 l (0.2641 USgal) of fuel (as a sample) from the drain valve. (e) Remove the funnel from the drain valve. (f) Examine the drain valve for leaks. (g) Do this procedure at all of the water drain valves. (h) Connect the funnel to the PURGING TOOL (97A28002117002). Subtask 12-32-28-281-059 B. Fuel/Water Sampling (1) Put the fuel sample into a transparent glass container. If you do not do the analysis immediately, seal the container. Subtask 12-32-28-750-060 R
C. Water Contamination Test (1) Let the sample become stable. (a) If the sample moves into two layers, it contains water. Continue to drain from the water drain valve until it has no water. (b) If the sample stays in one layer, it can be all fuel or all water. To find if the sample is fuel or water, do the test that follows.
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WARNING : DO THE TEST ONLY IN AN APPROVED AREA. _______ (c) Do this test: ------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------R R R
1. If you have a hydrokit available, refer to the manufacturers instructions and test the sample.
- If the powder stays white, the sample is fuel and the test is complete. or
R R R R R R R
- If the white powder changes color, refer to the color indicator comparison card. If the sample is water, you must do the test until all of the water is removed from the tank. (the powder does not change color). 2. If you do not have a hydrokit available, add water to the sample
- If the sample moves into two layers, the sample taken is all fuel and the test is complete. or - If the sample stays in one layer, the sample is water. Continue to take samples and test until all the water has been removed.
NOTE : You can use the same procedure to do an analysis on a ____ sample from a fuel tanker. Remove the sample from the supply connector of the fuel tanker. 5. Close-up ________ Subtask 12-32-28-942-061 A. Removal of Equipment (1) Make sure that the work area is clean and clear of tools and other items. NOTE : To discard the samples, refer to the local regulations. ____
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TASK 12-32-28-281-803 Operate Water Drain Valves to Drain Accumulated Water from Trim Tank and Trim Vent Surge Tank WARNING : DO NOT GET AIRCRAFT FUEL: _______ - IN YOUR MOUTH - IN YOUR EYES - ON YOUR SKIN FOR A LONG TIME. WARNING : DO NOT GET YOUR CLOTHES SOAKED WITH FUEL. _______ AIRCRAFT FUEL IS POISONOUS AND CAN GO THROUGH YOUR SKIN INTO YOUR BODY. IF YOU ARE CONTAMINATED WASH WITH CLEAN WATER AND IF NECESSARY GET MEDICAL HELP. WARNING : MAKE SURE THAT YOU HAVE THE CORRECT FIRE FIGHTING EQUIPMENT _______ AVAILABLE. WARNING : MONITOR THE MOVEMENT OF FUEL VERY CAREFULLY DURING THE GROUND FUEL _______ TRANSFER. MOVEMENT OF FUEL TO THE TRIM TANK CAN CAUSE THE AIRCRAFT TO OVERBALANCE. CAUTION : ALWAYS USE THE CORRECT TOOL TO OPEN THE WATER DRAIN VALVE. THIS CAN _______ PREVENT DAMAGE TO THE SEALS. 1. __________________ Reason for the Job Refer to the MPD TASK: 281100-02 NOTE : If possible, do the water drain procedure before you refuel. If you ____ refuel the aircraft before you do this procedure, the water and the fuel will mix. Because of this, you must wait one hour for the separation of the water and the fuel before you can drain the water from the tank. NOTE : For the gravity procedure there must be more than 1000 kg (2205 lb) ____ fuel in the trim tank. R
NOTE : This task can contribute to fuel savings. ____
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2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
R R R R
No specific No specific No specific No specific No specific No specific No specific 98A28104000000 98A28104031000
1 1 1 1 1
hot-air blower hydrokit suction pump transparent glass container 1 l (0.2641 USgal) ACCESS PLATFORM 8M (26 FT) - ADJUSTABLE CONTAINER 10 L(2 1/2 USGAL) HOSE - FUEL RESISTANT PURGER, WATER DRAIN PURGER - WATER DRAIN
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-32-28-281-812 27-40-00-866-801 28-00-00-610-801 28-25-00-869-802 12-32-28-991-009
Sample Fuel for Microbiological Contamination Analysis Operation of the THS Actuator Fuel Safety Procedures Ground Fuel Transfer To The Trim Tank Fig. 303
3. __________ Job Set-up (Ref. Fig. 303/TASK 12-32-28-991-009) Subtask 12-32-28-941-052 A. Safety Precautions WARNING : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND _______ DAMAGE. R
(1) Obey the fuel safety procedures (Ref. TASK 28-00-00-610-801).
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(2) Put an ACCESS PLATFORM 8M (26 FT) - ADJUSTABLE in position below the applicable water drain valve.
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Trim Tank and Trim Vent Surge Tank - Location for Suction and Gravity Procedure Figure 303/TASK 12-32-28-991-009
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(3) If the fuel temperature is less than -5 deg.C (+23.00 deg.F) (and/or the water drain valves are frozen), to keep the flight turnaround times, either: - use an approved hot-air blower to warm the drain valve area or - wait until one hour after the refuel procedure.
R R
Subtask 12-32-28-860-052 B. Aircraft Maintenance Configuration (1) Put the THS to the 4 degree position (Ref. TASK 27-40-00-866-801). NOTE : The maximum angle for draining water from the THS is 5 ____ degrees. On level ground the aircraft has a 1 degree nose down attitude. 4. Procedure _________ Subtask 12-32-28-680-056 A. Operate Water Drain Valves to Drain Accumulated Water from Trim Tank and Trim Vent Surge Tank WARNING : MAKE SURE THE AREA AROUND THE AIRCRAFT IS SAFE BEFORE YOU START _______ A REFUEL/DEFUEL PROCEDURE. IN THIS SAFE AREA, DO NOT LET PERSONS: - SMOKE - MAKE SPARKS OR FIRE - USE ANY EQUIPMENT WHICH IS NOT APPROVED FOR THE TASK. AIRCRAFT FUEL IS FLAMMABLE. NOTE : Before you can do a gravity water drain procedure at the trim ____ tank, it must contain a minimum fuel level of 1000 kg (2205 lb). This makes sure that the level of fuel is sufficient to force the fuel or water up to the remote drain valve. If the fuel level is 1000 kg (2205 lb) or more: - do the gravity procedure. If the fuel level is less than 1000 kg (2205 lb): - do the suction procedure or, - do a fuel ground transfer (Ref. TASK 28-25-00-869-802) so that the fuel level is 1000 kg (2205 lb) or more and do the gravity procedure. If you do the fuel ground transfer, you must wait a minimum of one hour before you operate the water drain valves.
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NOTE : During this procedure you must continue to operate all the drain ____ valves until only fuel comes out. NOTE : AIRBUS recommends that you do a test for microbial contamination, ____ in not more than 10 days, if: - the sample you drain from the tank has a strong sulphide smell - you can see objects in the sample (Ref. TASK 12-32-28-281-812). (1) Gravity procedure R
(a) Push the center of the applicable water drain valve with the PURGER, WATER DRAIN (98A28104000000). Drain approximately 1.0 l (0.2641 USgal) of fuel (as a sample) from the drain valve.
R
(b) Remove the PURGER, WATER DRAIN from the drain valve and examine the drain valve for leaks. (c) Do this procedure at all of the water drain valves (5105QS1, 5105QS2 and 5106QS) in the Trim Tank and Trim Vent Surge Tank. (2) Suction procedure NOTE : It is possible for FIN 5105QS1 and 5105QS2 that you cannot get ____ a satisfactory seal between the standard tool and the trim tank surface to use the suction method.
R R
(a) On the PURGER - WATER DRAIN (98A28104031000), disconnect the HOSE - FUEL RESISTANT from the bottle.
R R R
(b) Connect the end of the HOSE - FUEL RESISTANT to the inlet of the suction pump. NOTE : The illustration shows a typical suction pump with an air ____ drill power source. You must use a fuel approved type of suction pump for use on a fuel system and the applicable safety precautions must be taken.
R R
(c) Put the outlet of the suction pump into the CONTAINER 10 L(2 1/2 USGAL) and start the suction pump.
R R
(d) Push the center of the applicable water drain valve with the PURGER - WATER DRAIN. Drain approximately 1.0 l (0.2641 USgal) of fuel (as a sample) from the drain valve.
R R
(e) Remove the PURGER - WATER DRAIN from the drain valve and examine the drain valve for leaks.
EFF : ALL 12-32-28 SROS
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(f) Do this procedure at all of the water drain valves. R
(g) Connect the hose removed at step (a), to the bottle. Subtask 12-32-28-281-052 B. Fuel/Water Sampling (1) Put the fuel sample into a transparent glass container. If you do not do the analysis immediately, seal the container. Subtask 12-32-28-750-054 C. Water Contamination Test
R
(1) Let the sample become stable. (a) If the sample moves into two layers, it contains water. Continue to drain from the water drain valve until only fuel comes out. (b) If the sample stays in one layer, it can be all fuel or all water. To identify if the sample is fuel or water, do the test that follows. WARNING : DO THE TEST ONLY IN AN APPROVED AREA. _______ (c) Do this test: ------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------1. If you have a hydrokit available, refer to the manufacturers instructions and test the sample.
- If the powder stays white, the sample is fuel and the test is complete. or - If the white powder changes color, refer to the color indicator comparison card. If the sample is water, you must do the test until all of the water is removed from the tank (the powder does not change color).
R R
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------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------2. If you do not have a hydrokit - If the sample moves into two layers, available, add water to the the sample taken is all fuel and the sample test is complete. or - If the sample stays in one layer, the sample is water. Continue to collect samples. Do the test until all the water is removed.
R R 5. Close-up ________ Subtask 12-32-28-942-053 A. Removal of Equipment
(1) Make sure that the work area is clean and clear of tools and other items. (2) Remove the access platform(s). NOTE : To discard the samples, refer to the local regulations. ____
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Page 314 Jan 01/07
TASK 12-32-28-281-804 Draining of the Fuel/Air Separator WARNING : DO NOT GET AIRCRAFT FUEL: _______ - IN YOUR MOUTH - IN YOUR EYES - ON YOUR SKIN FOR A LONG TIME. WARNING : DO NOT GET YOUR CLOTHES SOAKED WITH FUEL. _______ AIRCRAFT FUEL IS POISONOUS AND CAN GO THROUGH YOUR SKIN INTO YOUR BODY. IF YOU ARE CONTAMINATED WASH WITH CLEAN WATER AND IF NECESSARY GET MEDICAL HELP. WARNING : MAKE SURE THAT YOU HAVE THE CORRECT FIRE FIGHTING EQUIPMENT _______ AVAILABLE. 1. __________________ Reason for the Job To drain the fuel/air separator for maintenance purposes. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific 98A28007570000
warning notices container 25 l (6.6042 USgal) access platform 5.0 m (16 ft. 5 in.) 1 ADAPTER - VENT AND DRAIN VALVE, APU
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B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 24-41-00-862-801
R
28-00-00-610-801 28-25-00-650-802 28-51-00-710-801 12-32-28-991-002
Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Fuel Safety Procedures Suction Defuel Procedure FCMS Fuel Valves Test Fig. 304
3. __________ Job Set-up Subtask 12-32-28-941-053 A. Safety Precautions WARNING : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND _______ DAMAGE. (1) Obey the fuel safety procedures (Ref. TASK 28-00-00-610-801). (2) Put the warning notices - on the panel 215VU to - on the panel 245VU to - on the panel 990VU to aircraft.
in these positions: tell persons not to operate the APU tell persons not to operate the fuel system tell persons not to refuel/defuel the
Subtask 12-32-28-860-050 B. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED _______ BEFORE YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT. UNWANTED ELECTRICAL POWER CAN BE DANGEROUS. (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861801). (2) Suction defuel the trim tank (Ref. TASK 28-25-00-650-802). (3) On the MCDU, get access to the FCMS VALVES TEST page (Ref. TASK 2851-00-710-801).
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(4) On the FCMS Valves Test page, put the the trim tank inlet valve (705QN valve L) to the OPEN position. NOTE : This makes sure that a vacuum will not prevent the drain ____ procedure. Subtask 12-32-28-010-050 C. Get Access (1) Put the access platform in position below the access panel 311AL. (2) Open the access panel 311AL. Subtask 12-32-28-491-050 D. Not applicable 4. Procedure _________ R
(Ref. Fig. 304/TASK 12-32-28-991-002) Subtask 12-32-28-680-055 A. Draining of the Fuel/Air Separator Procedure (1) Put the container in position on the access platform. (2) Put the end of the hose (3) into the container. (3) Remove the blanking cap (4) from the drain valve (1). (4) Connect the ADAPTER - VENT AND DRAIN VALVE, APU (98A28007570000) (2) to the drain valve (1). (5) Drain all of the fuel out of the fuel/air separator. (6) Remove the ADAPTER - VENT AND DRAIN VALVE, APU (98A28007570000) (2) from the drain valve (1). (7) Connect the blanking cap (4) to the drain valve (1). 5. Close-up ________ Subtask 12-32-28-091-050 A. Not applicable
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Fuel/Air Separator Water Drain - Location Figure 304/TASK 12-32-28-991-002
R
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Subtask 12-32-28-410-050 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access panel 311AL. Subtask 12-32-28-860-051 C. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED _______ BEFORE YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT. UNWANTED ELECTRICAL POWER CAN BE DANGEROUS. (1) On the MCDU, get access to the FCMS VALVES TEST page (Ref. TASK 2851-00-710-801). (2) On the FCMS Valves Test page, put the the trim tank inlet valve (705QN valve L) to the SHUT position. (3) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). Subtask 12-32-28-942-052 D. Removal of Equipment (1) Remove the access platform(s). (2) Remove the warning notice(s). NOTE : To discard the fuel, refer to the local regulations. ____
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TASK 12-32-28-281-807 Operate the Drain Valve of the Fuel/Air Separator to Drain any Accumulated Water WARNING : DO NOT GET AIRCRAFT FUEL: _______ - IN YOUR MOUTH - IN YOUR EYES - ON YOUR SKIN FOR A LONG TIME. WARNING : DO NOT GET YOUR CLOTHES SOAKED WITH FUEL. _______ AIRCRAFT FUEL IS POISONOUS AND CAN GO THROUGH YOUR SKIN INTO YOUR BODY. IF YOU ARE CONTAMINATED WASH WITH CLEAN WATER AND IF NECESSARY GET MEDICAL HELP. WARNING : MAKE SURE THAT YOU HAVE THE CORRECT FIRE FIGHTING EQUIPMENT _______ AVAILABLE. 1. __________________ Reason for the Job Refer to the MPD TASK: 282200-07 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific No specific No specific 98A28007570000
hydrokit warning notices transparent glass container 1 l (0.2641 USgal) container 25 l (6.6042 USgal) access platform 5.5 m (18 ft. 1 in.) 1 ADAPTER - VENT AND DRAIN VALVE, APU
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B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-32-28-281-803 12-32-28-680-801 12-32-28-680-802 24-41-00-861-801 24-41-00-862-801 28-00-00-610-801 28-22-43-000-802 28-22-43-400-802 28-51-00-740-803 51-78-00-615-805 R
12-32-28-991-002
Operate Water Drain Valves to Drain Accumulated Water from Trim Tank and Trim Vent Surge Tank Heating of Fuel/Air Separator - Warm Fuel Procedure Heating of Fuel/Air Separator - Hot Air Procedure Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Fuel Safety Procedures Removal of the Drain Valve (5216QA) Installation of the Drain Valve (5216QA) Interrogation of the FCMS Input Parameters Pages Aircraft Cleaning after a Fuel Leakage (for corrective action) Fig. 304
3. __________ Job Set-up Subtask 12-32-28-941-058 A. Safety Precautions WARNING : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND _______ DAMAGE. (1) Obey the fuel safety procedures (Ref. TASK 28-00-00-610-801). (2) Put the warning notices - on the panel 215VU to - on the panel 245VU to - on the panel 990VU to aircraft.
in these positions: tell persons not to operate the APU tell persons not to operate the fuel system tell persons not to refuel/defuel the
Subtask 12-32-28-860-057 B. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED _______ BEFORE YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT. UNWANTED ELECTRICAL POWER CAN BE DANGEROUS.
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(1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) On the MCDU, get access to page 10 of the FCMS input parameters page (Ref. TASK 28-51-00-740-803). (3) On the panel 215VU, push (in) the APU MASTER SW P/BSW. Make sure that the ON light comes on. (4) On the MCDU, make sure that the fwd APU fuel pump is in operation. Subtask 12-32-28-010-054 C. Get Access (1) Put the access platform in position below the access panel 311AL. (2) Open the access panel 311AL. 4. Procedure _________ R
(Ref. Fig. 304/TASK 12-32-28-991-002) Subtask 12-32-28-680-059 A. Operate the Drain Valve of the Fuel/Air Separator to Drain any Accumulated Water (1) Do a fuel leak check around the area of the drain valve. There must be no leaks. If there are signs of a leak, replace the seal (Ref. TASK 28-22-43-000-802) and (Ref. TASK 28-22-43-400-802). (2) Put the container in position. (3) Remove the cap (4) from the drain valve (1). (4) It is possible that water in the fuel/air separator has changed to ice. If there is ice in the fuel/air separator, do the heating of the fuel/air separator procedure (Ref. TASK 12-32-28-680-801) or (Ref. TASK 12-32-28-680-802). (5) On the ADAPTER - VENT AND DRAIN VALVE, APU (98A28007570000) (2), put the end of the hose (3) into the container. (6) Connect the ADAPTER - VENT AND DRAIN VALVE, APU (98A28007570000) (2) to the drain valve (1).
EFF : ALL 12-32-28 SROS
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(7) Drain between 8 l (2.0 USgal) and 10 l (2.5 USgal) of fuel from the fuel/air separator. (8) Remove the ADAPTER - VENT AND DRAIN VALVE, APU (98A28007570000) (2) from the drain valve (1). Subtask 12-32-28-790-051 B. Leak Check (1) Do a fuel leak check around the area of the drain valve. Leakage is not allowed. If there are signs of a leak, replace the seal (Ref. TASK 28-22-43-000-802) and (Ref. TASK 28-22-43-400-802). (2) Install the cap (4) on the drain valve (1). (3) If there was an internal spillage during the procedure, you must do the aircraft cleaning after a fuel leakage procedure (Ref. TASK 5178-00-615-805). Subtask 12-32-28-281-056 C. Fuel/Water Sampling (1) Put the fuel sample into a transparent glass container. If you do not do the analysis immediately, seal the container. NOTE : The test must be done before the next flight. ____ Subtask 12-32-28-750-057 D. Water Contamination Test (1) Let the sample become stable. (a) If the sample moves into two layers, it contains water. Continue to drain from the water drain valve until it has no water. (b) If the sample stays in one layer, it can be all fuel or all water. To find if the sample is fuel or water, do the test that follows. WARNING : DO THE TEST ONLY IN AN APPROVED AREA. _______
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INTENTIONALLY BLANK
R 12-32-28 SROS
Page 324 Jul 01/05
(c) Do this test: ------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------1. If you have a hydrokit available, put the contents into the sample
- If the powder stays white, the sample is fuel and the test is complete. or - If the white powder changes color to purple, the sample is water. Continue to take samples and test until all the water has been removed.
2. If you do not have a hydrokit available, add water to the sample
- If the sample moves into two layers, the sample taken is all fuel and the test is complete. or - If the sample stays in one layer, the sample is water. Continue to take samples and test until all the water has been removed.
3. Measure the amount of water taken from the fuel/air separator.
- If the amount of water is 0.5 l or more, do a water drain check of the trim tank (Ref. TASK 12-32-28-281803).
5. Close-up ________ Subtask 12-32-28-410-054 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access panel 311AL.
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Subtask 12-32-28-860-058 B. Aircraft Maintenance Configuration (1) On the panel 215VU, release (out) the APU MASTER SW. Make sure that the ON light goes off. (2) On the MCDU, push the line key adjacent to the RETURN indication until the MCDU Menu page comes into view. (3) On the MCDU, set the BRT knob to OFF. (4) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). Subtask 12-32-28-942-058 C. Removal of Equipment (1) Remove the access platform(s). (2) Remove the warning notice(s). NOTE : To discard the fuel, refer to the local regulations. ____
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TASK 12-32-28-680-801 Heating of Fuel/Air Separator - Warm Fuel Procedure 1. __________________ Reason for the Job To melt ice that has formed in the fuel/air separator and has blocked the drain point. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
warning notices
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-32-28-281-805 24-41-00-861-801 24-41-00-862-801 28-00-00-610-801 28-25-00-869-802 31-60-00-860-801
Draining of the Fuel/Air Separator to Remove Accumulated Water Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Fuel Safety Procedures Ground Fuel Transfer To The Trim Tank EIS Start Procedure
3. __________ Job Set-up Subtask 12-32-28-941-056 A. Safety Precautions WARNING : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND _______ DAMAGE. (1) Obey the fuel safety procedures (Ref. TASK 28-00-00-610-801).
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(2) Put the warning notices - on the panel 215VU to - on the panel 245VU to - on the panel 990VU to aircraft.
in these positions: tell persons not to operate the APU tell persons not to operate the fuel system tell persons not to refuel/defuel the
Subtask 12-32-28-860-055 B. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED _______ BEFORE YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT. UNWANTED ELECTRICAL POWER CAN BE DANGEROUS. (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Do the EIS start procedure (Ref. TASK 31-60-00-860-801). (3) On the ECAM control panel, push the FUEL icon switch. 4. Procedure _________ Subtask 12-32-28-880-050 A. Heating of the Fuel/Air Separator - Warm Fuel Procedure WARNING : MONITOR THE MOVEMENT OF FUEL VERY CAREFULLY DURING THE GROUND _______ FUEL TRANSFER. MOVEMENT OF FUEL TO THE TRIM TANK CAN CAUSE THE AIRCRAFT TO OVERBALANCE. (1) Do a fuel ground transfer of 1000 kg (2200 lb) minimum to the trim tank (Ref. TASK 28-25-00-869-802). (2) Wait for 30 minutes. (3) Try to do the draining of the fuel/air separator procedure (Ref. TASK 12-32-28-281-805). If the drain is successful, the heating procedure is complete. (4) If the draining of the fuel/air separator is not successful, continue the heating procedure.
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(5) Do a forward transfer (a) On the FUEL panel 245VU, push (in) the T TANK MODE switch. (b) On the ECAM System Display, monitor the transfer of fuel from the trim tank. (c) When the trim-tank fuel quantity is 300 kg (600 lb) less, release (out) the T TANK MODE switch. (6) Wait for 30 minutes. (7) Try to do the draining of the fuel/air separator procedure (Ref. TASK 12-32-28-281-805). If the drain is successful, the heating procedure is complete. (8) If the draining of the fuel/air separator is not successful, do the heating procedure again. Continue to do the heating procedure until the ice has melted. 5. Close-up ________ Subtask 12-32-28-860-056 A. Aircraft Maintenance Configuration (1) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). Subtask 12-32-28-942-056 B. Removal of Equipment (1) Remove the warning notice(s).
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TASK 12-32-28-680-802 Heating of Fuel/Air Separator - Hot Air Procedure 1. __________________ Reason for the Job To melt ice that has formed in the fuel/air separator and has blocked the drain point. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
hot air blower warning notices access platform 5.0 m (16 ft. 5 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-32-28-281-805 27-40-00-866-801 28-00-00-610-801
Draining of the Fuel/Air Separator to Remove Accumulated Water Operation of the THS Actuator Fuel Safety Procedures
3. __________ Job Set-up Subtask 12-32-28-941-057 A. Safety Precautions WARNING : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND _______ DAMAGE. (1) Obey the fuel safety procedures (Ref. TASK 28-00-00-610-801).
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(2) Put the warning notices in these positions: - in the cockpit to tell persons not to operate the THS - on the panel 215VU to tell persons not to operate the APU - on the panel 245VU to tell persons not to operate the fuel system - on the panel 990VU to tell persons not to refuel/defuel the aircraft. Subtask 12-32-28-860-059 B. Aircraft Maintenance Configuration (1) Put the THS to the 0 degree position (Ref. TASK 27-40-00-866-801). Subtask 12-32-28-010-053 C. Get Access (1) Put the access platform in position below the access door 312AR. (2) Open the access door 312AR. R 4. Procedure _________ Subtask 12-32-28-880-051 A. Heating of the Fuel/Air Separator - Hot Air Procedure CAUTION: MAKE SURE THAT THE TEMPERATURE OF THE HOT AIR DOES NOT EXCEED 70 DEG C. THIS PREVENTS DAMAGE TO THE VALVE AND STRUCTURE. (1) Use a pipe from a hot air blower to blow hot air onto the water drain valve area of the fuel/air separator. (2) Keep the hot air on the area of the valve for 30 minutes. (3) Try to do the draining of the fuel/air separator procedure (Ref. TASK 12-32-28-281-805). If the drain is successful, the heating procedure is complete. (4) If the draining of the fuel/air separator is not successful, repeat the heating procedure. (5) Try to do the draining of the fuel/air separator procedure (Ref. TASK 12-32-28-281-805). If the drain is successful, the heating procedure is complete.
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(6) If the draining of the fuel/air separator is not successful, do the heating procedure again. Continue to do the heating procedure until the ice has melted. 5. Close-up ________ Subtask 12-32-28-091-053 A. Removal of the Safety Locks (1) Remove the MECHANICAL INPUT - RIGGING PIN from the mechanical input of the THS actuator. Subtask 12-32-28-410-053 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access door 312AR. Subtask 12-32-28-942-057 C. Removal of Equipment (1) Remove the access platform(s). (2) Remove the warning notice(s).
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TASK 12-32-28-281-812 R
Sample Fuel for Microbiological Contamination Analysis WARNING : DO NOT GET AIRCRAFT FUEL: _______ - IN YOUR MOUTH - IN YOUR EYES - ON YOUR SKIN FOR A LONG TIME. WARNING : DO NOT GET YOUR CLOTHES SOAKED WITH FUEL. _______ AIRCRAFT FUEL IS POISONOUS AND CAN GO THROUGH YOUR SKIN INTO YOUR BODY. IF YOU ARE CONTAMINATED WASH WITH CLEAN WATER AND IF NECESSARY GET MEDICAL HELP. WARNING : MAKE SURE THAT YOU HAVE THE CORRECT FIRE FIGHTING EQUIPMENT _______ AVAILABLE. 1. __________________ Reason for the Job
R
Refer to the MPD TASK: 281100-15 This procedure lets you do a test of the sample locally or you can send it to a laboratory. Refer to Service Information Letter (SIL 28-079) for more information about microbiological contamination in fuel tanks. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific No specific
transparent fuel resistant plastic container(s) 1 MICROBMONITOR 2 TEST KIT ECHA MICROBIOLOGY UK (CAGE CODE 0HZY6) 1 FUELSTAT RESINAE TEST KIT CONIDIA BIOSCIENCE UK (CAGE CODE KE385) 1 HY-LITE JET A1 FUEL TEST KIT MERCK KGAA, GERMANY (CAGE CODE D2186)
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B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-32-28-281-801 12-32-28-281-803 12-32-28-281-807 28-00-00-610-801 28-11-00-600-814 28-11-00-600-815 28-11-00-600-818 28-11-00-600-819
R
28-11-00-600-822 12-32-28-991-008 12-32-28-991-010
Operate Water Drain Valves to Drain Accumulated Water from Center, Inner, Outer and Wing Vent Surge Tanks Operate Water Drain Valves to Drain Accumulated Water from Trim Tank and Trim Vent Surge Tank Operate the Drain Valve of the Fuel/Air Separator to Drain any Accumulated Water Fuel Safety Procedures BIOBOR Biocidal Shock Treatment - With Fuel Mixed with Biocide BIOBOR Biocidal Shock Treatment - When Fuel Mixed with Biocide is not Available (Metered Injection Rig Method) KATHON Biocidal Shock Treatment - With Fuel Mixed with Biocide KATHON Biocidal Shock Treatment - When Fuel Mixed with Biocide is not Available (Metered Injection Rig Method) Removal of The Microbiological Particles Fig. 305 Fig. 306
3. __________ Job Set-up R
(Ref. Fig. 305/TASK 12-32-28-991-008, 306/TASK 12-32-28-991-010) Subtask 12-32-28-941-063 A. Safety Precautions WARNING : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND _______ DAMAGE. (1) Obey the fuel safety procedures (Ref. TASK 28-00-00-610-801).
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R
Maintenance Plan Flowchart - Microbiological Contamination Figure 305/TASK 12-32-28-991-008
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R
Microbiological Contamination Test Kits - Comparison Table Figure 306/TASK 12-32-28-991-010- 12 (SHEET 1)
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R
Microbiological Contamination Test Kits - Comparison Table Figure 306/TASK 12-32-28-991-010- 22 (SHEET 2)
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4. Procedure _________ Subtask 12-32-28-281-061 A. Sample Fuel for Microbiological Contamination Analysis NOTE : If moderate or heavy microbiological contamination is found in the ____ samples: - all the fuel tanks may have microbiological contamination - a biocidal shock treatment must be applied to all of the fuel tanks (Ref. TASK 28-11-00-600-814) or (Ref. TASK 28-11-00-600815) or (Ref. TASK 28-11-00-600-818) or (Ref. TASK 28-11-00-600819). (1) Drain a fuel and water sample from each fuel tank (Ref. TASK 12-3228-281-801) and (Ref. TASK 12-32-28-281-803). You must use a different sample container for each fuel tank. NOTE : Do not put additives in the samples to show the water ____ contents. NOTE : Before you collect the samples, read the manufacturers ____ instructions in the test kit. Make sure you use a sample container that is specified and that it is clean and dry before use. An incorrect, dirty sample container can give an unwanted effect to the results. (2) Put the sample(s) into a transparent fuel resistant plastic container(s) with a minimum capacity of 1.0 l (0.2641 USgal) and: - seal the container(s) - make sure you can see free water and fuel in the sample(s) (for the MICROBMONITOR2 kit or the FUELSTAT RESINAE kit). (3) Identify each sample with a label that shows: - the aircraft number - the time and the date of the sample - the fuel tank the sample came from - all additives you know about.
R
(4) Keep the sealed sample containers in a cool protected area. NOTE : After the test samples are collected, microbial contamination ____ in the sample could multiply or die. It is recommended that the samples are tested before 6 hours but no later than 24 hours. AIRBUS recommends that the samples are tested in no more than 6 hours.
EFF : ALL 12-32-28 SROS
Page 338 Jan 01/07
NOTE : Choose one microbial test kit for the complete procedure. Do ____ not compare results between the microbial detection kits. They use different methods to give results. If you need help, ask the kit manufacturer. Subtask 12-32-28-281-065 B. Not applicable Subtask 12-32-28-281-067 C. Not applicable Subtask 12-32-28-281-068 D. Fuel/Air Separator (1) Drain a fuel sample from the fuel/air separator (Ref. TASK 12-32-28281-807). Subtask 12-32-28-281-062 R
E. Sample Test - MICROBMONITOR2 Test Kit Procedure (1) Do one of the steps that follow: (a) Use the MICROBMONITOR 2 TEST KIT ECHA MICROBIOLOGY UK (CAGE CODE 0HZY6) (and the manufacturers instructions) to do a test on the WATER and FUEL samples, or (b) Send the WATER and FUEL samples to an approved laboratory. (2) Do a check of the results: NOTE : If you do only one test, it can give an incorrect indication ____ of the condition of the fuel tanks. If a test shows contamination, (moderate or heavy) do the test again, (in not more than 10 days) before you remove the aircraft from service. Use the same test kit for the second test. (a) Negligible contamination 1 _
R R R
The contamination is negligible if: - the WATER sample contents has 1000 CFU/milli liter (Colony Forming Units) or less - the FUEL sample contents has 4000 CFU/liter or less.
EFF : ALL 12-32-28 SROS
Page 339 Jan 01/06
2 _
Continue to monitor the fuel tanks at the scheduled inspection interval. This procedure is now complete.
(b) Moderate contamination 1 _
The contamination is moderate if: - the WATER sample contents has between 1000 and 10000 CFU/milli liter - the FUEL sample contents has between 4000 and 20000 CFU/liter.
2 _
Use the same method and do the sample test again in not more than 10 days after the first test.
3 _
If the contamination has not changed from moderate: - do the BIOBOR or KATHON biocidal shock treatment (moderate contamination procedure) to all of the fuel tanks, (Ref. TASK 28-11-00-600-814) or (Ref. TASK 28-11-00-600-815) or (Ref. TASK 28-11-00-600-818) or (Ref. TASK 28-11-00-600819).
R R R R
(c) Heavy contamination 1 _
The contamination is heavy if: - the WATER sample contents is more than 10000 CFU/milli liter - the FUEL sample contents is more than 20000 CFU/liter.
2 _
Use the same method and do the sample test again in not more than 10 days after the first test.
3 _
If the contamination has not changed from heavy: - do the BIOBOR or KATHON biocidal shock treatment (heavy contamination procedure) to all of the fuel tanks (Ref. TASK 28-11-00-600-814) or (Ref. TASK 28-11-00-600-815) or (Ref. TASK 28-11-00-600-818) or (Ref. TASK 28-11-00-600819).
R R
R R R
NOTE : When you do the heavy contamination procedure, you will ____ need to enter the applicable fuel tanks to remove the contamination (Ref. TASK 28-11-00-600-822). The MICROBMONITOR2 Test Kit Procedure is now complete go to para. 5.(Close-up).
EFF : ALL 12-32-28 SROS
Page 340 Jan 01/06
Subtask 12-32-28-281-064 F. Sample Test - FUELSTAT RESINAE Test Kit Procedure NOTE : The FUELSTAT RESINAE test kit shows the most frequent type of ____ contamination you can find in fuel tanks (Hormoconis Resinae). Other types of contamination will not be shown. (1) Do one of the steps that follow: (a) Use the FUELSTAT RESINAE TEST KIT CONIDIA BIOSCIENCE UK (CAGE CODE KE385) (and the manufacturers instructions) to do a test on the WATER and FUEL samples, or (b) Send the WATER and FUEL samples to an approved laboratory. (2) Do a check of the results: NOTE : If you do only one test, it can give an incorrect indication ____ of the condition of the fuel tanks. If a test shows contamination, (moderate or heavy) do the test again, (in not more than 10 days) before you remove the aircraft from service. Use the same test kit to do the second test. (a) Negligible contamination 1 _
The contamination is negligible if the indication lines (on the test kit) show a negative result.
2 _
Continue to monitor the fuel tanks at the scheduled inspection interval. This procedure is now complete.
(b) Moderate contamination 1 _
The contamination is moderate if the indication lines (on the test kit) show a low positive result. Use the same method and do the sample test again in not more than 10 days after the first test.
EFF : ALL 12-32-28 R SROS
Page 341 Jan 01/07
2 _
If the contamination has not changed from moderate: - do the BIOBOR or KATHON biocidal shock treatment (moderate contamination procedure) to all of the fuel tanks, (Ref. TASK 28-11-00-600-814) or (Ref. TASK 28-11-00-600-815) or (Ref. TASK 28-11-00-600-818) or (Ref. TASK 28-11-00-600819).
(c) Heavy contamination 1 _
The contamination is heavy if the indication lines (on the test kit) show a high positive result.
2 _
Use the same method and do the sample test again in not more than 10 days after the first test. If the contamination has not changed from heavy: - do a BIOBOR or KATHON biocidal shock treatment (heavy contamination procedure) to all of the fuel tanks (Ref. TASK 28-11-00-600-814) or (Ref. TASK 28-11-00-600-815) or (Ref. TASK 28-11-00-600-818) or (Ref. TASK 28-11-00-600819). NOTE : When you do the heavy contamination procedure, you will ____ need to enter the applicable fuel tanks to remove the contamination (Ref. TASK 28-11-00-600-822). The FUELSTAT RESINAE Test Kit Procedure is now complete go to para.5.(Close-up).
Subtask 12-32-28-281-069 R
G. Sample Test - HY-LiTE Jet A1 Fuel Test Kit Procedure NOTE : The manufacturers recommend you only use a fuel resistant ____ transparent plastic sample container. Glass containers will give an unwanted effect to the operation of the test kit. If possible, do the test in a clean area. (1) Do one of the steps that follow: (a) Use the HY-LITE JET A1 FUEL TEST KIT MERCK KGAA, GERMANY (CAGE CODE D2186) (and the manufacturers instructions) to do a test on the WATER and FUEL samples, or (b) Send the WATER and FUEL samples to an approved laboratory.
EFF : ALL 12-32-28 SROS
Page 342 Jan 01/07
(2) Do a check of the results: NOTE : If you do only one test, it can give an incorrect indication ____ of the condition of the fuel tanks. If a test shows contamination, (moderate or heavy) do the test again, (in not more than 10 days) before you remove the aircraft from service. Use the same test kit to do the second test. (a) Negligible contamination 1 _
The contamination is negligible if: - the WATER/FUEL sample contents has 1000 RLU/liter (Relative Light Units) or less.
2 _
Continue to monitor the fuel tanks at the scheduled inspection interval. This procedure is now complete.
R R
(b) Moderate contamination 1 _
The contamination is moderate if: - the WATER/FUEL sample contents has between 1000 and 5000 RLU/liter
2 _
Use the same method and do the sample test again in not more than 10 days after the first test.
3 _
If the contamination has not changed from moderate: - do the BIOBOR or KATHON biocidal shock treatment (moderate contamination procedure) to all of the fuel tanks, (Ref. TASK 28-11-00-600-814) or (Ref. TASK 28-11-00-600-815) or (Ref. TASK 28-11-00-600-818) or (Ref. TASK 28-11-00-600819).
R R
(c) Heavy contamination 1 _
The contamination is heavy if: - the WATER/FUEL sample contents is more than 5000 RLU/liter
2 _
Use the same method and do the sample test again in not more than 10 days after the first test.
R
EFF : ALL 12-32-28 SROS
Page 343 Jan 01/07
3 _
If the contamination has not changed from heavy: - do the BIOBOR or KATHON biocidal shock treatment (heavy contamination procedure) to all of the fuel tanks (Ref. TASK 28-11-00-600-814) or (Ref. TASK 28-11-00-600-815) or (Ref. TASK 28-11-00-600-818) or (Ref. TASK 28-11-00-600819). NOTE : When you do the heavy contamination procedure, you will ____ need to enter the applicable fuel tanks to remove the contamination (Ref. TASK 28-11-00-600-822).
5. Close-up ________ Subtask 12-32-28-942-063 A. Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 12-32-28 R SROS
Page 344 Jan 01/07
HYDRAULIC FLUID - SERVICING ___________________________ TASK 12-32-29-281-801 Sampling for Analysis WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE _______ CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM. MOVEMENT OF THE FLIGHT CONTROL SURFACES CAN BE DANGEROUS AND/OR CAUSE DAMAGE. WARNING : MAKE SURE THAT THE CONTROLS AGREE WITH THE POSITION OF THE ITEMS THEY _______ OPERATE BEFORE YOU PRESSURIZE A HYDRAULIC SYSTEM. UNWANTED MOVEMENT OF HYDRAULICALLY OPERATED ITEMS CAN BE DANGEROUS AND/OR CAUSE DAMAGE. WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL MATERIALS _______ ONLY WITH A GOOD FLOW OF AIR THROUGH THE WORK AREA. THESE MATERIALS ARE POISONOUS AND FLAMMABLE AND SKIN IRRITANTS. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. 1. __________________ Reason for the Job Refer to the MPD TASK: 291000-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R R R
No specific No specific No specific No specific HSPA181-380J
warning notices glass sample bottle 0.2 l (0.0528 USgal) plastic sample bottle exclusively made from poly-ethylene 0.2 l (0.0528 USgal) container 1.0 l (0.2641 USgal) 1 HYDRAULIC PURIFIER
EFF : ALL 12-32-29 SROS
Page 301 Jan 01/07
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R Material No. 19-017
USA AMS 5687 LOCKWIRE 1.25 MM (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-801 12-12-29-611-802 12-12-29-611-803 12-12-29-611-804 12-12-29-611-805 12-12-29-611-806 12-36-29-611-801 12-36-29-611-801 12-36-29-611-802 12-36-29-611-802 12-36-29-611-803 12-36-29-611-803 12-36-29-611-804 12-36-29-611-805 12-36-29-611-806
Fill the Green Hydraulic Reservoir with a Hydraulic Service Cart Fill the Green Hydraulic Reservoir with a Hand Pump Fill the Blue Hydraulic Reservoir with a Hydraulic Service Cart Fill the Blue Hydraulic Reservoir with a Hand Pump Fill the Yellow Hydraulic Reservoir with a Hydraulic Service Cart Fill the Yellow Hydraulic Reservoir with a Hand Pump Replacement of the Hydraulic Fluid of the Green Hydraulic System with a Fluid Replacement and Recovery Bench Replacement of the Hydraulic Fluid of the Green Hydraulic System with a Fluid Replacement and Recovery Bench Replacement of the Hydraulic Fluid of the Blue Hydraulic System with a Fluid Replacement and Recovery Bench Replacement of the Hydraulic Fluid of the Blue Hydraulic System with a Fluid Replacement and Recovery Bench Replacement of the Hydraulic Fluid of the Yellow Hydraulic System with a Fluid Replacement and Recovery Bench Replacement of the Hydraulic Fluid of the Yellow Hydraulic System with a Fluid Replacement and Recovery Bench Reclaim the Fluid in the Green Hydraulic System Reclaim the Fluid in the Blue Hydraulic System Reclaim the Fluid in the Yellow Hydraulic System
EFF : ALL 12-32-29 SROS
Page 302 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-36-29-611-807 R R R R
12-36-29-611-808 12-36-29-611-809 12-36-29-615-801 12-36-29-615-802 12-36-29-615-803 29-00-00-863-801 29-00-00-863-802 29-00-00-863-803 29-00-00-864-801 29-00-00-864-802 29-00-00-864-803
R R
29-00-00-910-805 32-12-00-010-801 32-12-00-410-801 SIL 29-081 12-32-29-991-001
Replacement of the Hydraulic Fluid of the Green Hydraulic System with the Green Electric Pump Replacement of the Hydraulic Fluid of the Blue Hydraulic System with the Blue Electric Pump Replacement of the Hydraulic Fluid of the Yellow Hydraulic System with the Yellow Electric Pump Clean the Fluid in the Green Hydraulic System (with the Pall Purifier) Clean the Fluid in the Blue Hydraulic System (with the Pall Purifier) Clean the Fluid in the Yellow Hydraulic System (with the Pall Purifier) Pressurize the Green Hydraulic System with the Ground Hydraulic Supply Pressurize the Blue Hydraulic System with the Ground Hydraulic Supply Pressurize the Yellow Hydraulic System with the Ground Hydraulic Supply Depressurize the Green Hydraulic System (Pressurized with the Hydraulic Ground Supply) Depressurize the Blue Hydraulic System (Pressurized with the Hydraulic Ground Supply) Depressurize the Yellow Hydraulic System (Pressurized with the Hydraulic Ground Supply) Safety Procedures of the Hydraulic System Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Fig. 301
3. __________ Job Set-up R
Subtask 12-32-29-941-050
R
A. Safety Precautions
R
(1) Obey the hydraulic safety procedures (Ref. TASK 29-00-00-910-805).
R R R
(2) Put the warning notices in position to tell persons not to move: - the flight controls, - the lever of the landing gear selector.
EFF : ALL 12-32-29 SROS
Page 303 Jan 01/06
Subtask 12-32-29-010-050 B. Get Access (1) For Green or Blue hydraulic system: - Open the left MLG door (Ref. TASK 32-12-00-010-801). (2) For Yellow hydraulic system: - Open the right MLG door (Ref. TASK 32-12-00-010-801). Subtask 12-32-29-864-050 R
C. Pressurize the concerned hydraulic systems - for Green hydraulic system (Ref. TASK 29-00-00-863-801), - for Blue hydraulic system (Ref. TASK 29-00-00-863-802), - for Yellow hydraulic system (Ref. TASK 29-00-00-863-803). 4. Procedure _________ (Ref. Fig. 301/TASK 12-32-29-991-001) Subtask 12-32-29-680-050
R
A. Flush the sampling valve (1) Remove and discard WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. _______ CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU. (a) Remove and discard the lockwire from the applicable sampling valve: - for the Green hydraulic system, sampling valve 5123JM1 - for the Blue hydraulic system, sampling valve 5123JM2 - for the Yellow hydraulic system, sampling valve 5123JM3. (2) Remove the cap (3) from sampling valve (1).
R R
(3) Put the container below the sampling valve.
R
(4) Put the notch in the head of the cap (3) below the head of the needle valve (2).
R
(5) Move the cap (3) to pull the needle valve (2) down and drain 0.2 l (0.0528 USgal) into the container.
EFF : ALL 12-32-29 SROS
Page 304 Jan 01/07
R
(6) Remove the cap (3) from the needle valve (2).
R R
(7) Discard the hydraulic fluid (refer to the local regulations).
R R
NOTE : You must flush the sampling valve before you remove each ____ sample. Subtask 12-32-29-281-050
R
B. Remove a sample from the sampling valve
R R
(1) Put the clean glass sample bottle or plastic sample bottle exclusively made from poly-ethylene below the sampling valve (1). (2) Put the notch in the head of the cap (3) below the head of the needle valve (2). (3) Move the cap (3) to pull the needle valve (2) down and drain 0.2 l (0.0528 US gal) into the sample bottle.
R
(4) Remove the cap (3) from the needle valve (2). R
(5) Seal the sample bottle.
R R
(6) Put a tag on the sample bottle with the aircraft registration, the system identification, the date and time. (7) Send the sample bottle to the analysis laboratory. (8) Depressurize the concerned hydraulic systems: - for Green hydraulic system (Ref. TASK 29-00-00-864-801), - for Blue hydraulic system (Ref. TASK 29-00-00-864-802), - for Yellow hydraulic system (Ref. TASK 29-00-00-864-803).
R R
(9) Install the cap (3) on the sampling valve (1). R
(10) Safety the cap with MISCELLANEOUS (Material No. 19-017).
EFF : ALL 12-32-29 SROS
Page 305 Jan 01/07
Sampling Valve - Location Figure 301/TASK 12-32-29-991-001- 12 (SHEET 1) EFF : ALL 12-32-29 SROS
Page 306 Apr 01/98
Sampling Valve - Location Figure 301/TASK 12-32-29-991-001- 22 (SHEET 2) EFF : ALL 12-32-29 SROS
Page 307 Apr 01/98
Subtask 12-32-29-281-051 C. Admissible Particle Contamination of Hydraulic Fluid R R R R R R R
(1) For correct operation of hydraulic equipment, the hydraulic fluid must be clean. The number of particles contained in 100 cubic-centimeters (6 cu.in.) must not be more than the class 9 requirements of NSA 307110 specifications. The hydraulic fluid used for replenishing, topping up etc, hydraulic systems (cart reservoirs) must agree with the requirements of class 7 of the NSA 307110 specifications (initial state).
R R
(2) Reference list of maximum limits of class 7 and class 9 of NSA 307110 specification: -----------------------------------------------------------------------------NUMBER OF PARTICLES -----------------------------------------------------------------------------Particle size Class 7 Class 9 -----------------------------------------------------------------------------5 to 15 micron 32000 128000 15 to 25 micron 5700 22800 25 to 50 micron 1012 4050 50 to 100 micron 180 720 > 100 micron 32 128
R R R R
(3) If a sample analysis shows a contamination rate higher of one or more of the class 9 values:
R R
(a) Stop the hydraulic tests,
R R R R R R R
(b) clean the hydraulic fluid (Ref. TASK 12-36-29-615-801), (Ref. TASK 12-36-29-615-802) and (Ref. TASK 12-36-29-615-803). - or reclaim it with the hydraulic ground power cart (Ref. TASK 12-36-29-611-804), (Ref. TASK 12-36-29-611-805) and (Ref. TASK 12-36-29-611-806). - or change it (Ref. TASK 12-36-29-611-807), (Ref. TASK 12-36-29611-808) and (Ref. TASK 12-36-29-611-809).
EFF : ALL 12-32-29 SROS
Page 308 Jan 01/06
R R R R R
NOTE : It is possible that Airbus will give you approval for ____ aircraft dispatch, if the contamination rate is more than the given limits (please see SIL 29-081) depending on the level of contamination and given if only one system is contaminated. **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 12-32-29-281-052
R
D. Chemical analysis
R R
(1) Chemical analysis must be to NSA307110 Limit Characteristics of fluid in operation.
R R
(2) If the values of the chemical analysis are not in the limits given in the table below, do the following corrective actions:
R R R R R R R
(a) If the water or chlorine content of the fluid sample are equal or more than the values given above: - Clean the hydraulic fluid with the HYDRAULIC PURIFIER (HSPA181380J) (Ref. TASK 12-36-29-615-801), (Ref. TASK 12-36-29-615802) and (Ref. TASK 12-36-29-615-803), - or change the hydraulic fluid (Ref. TASK 12-36-29-611-801), (Ref. TASK 12-36-29-611-802) and (Ref. TASK 12-36-29-611-803).
R R R R
(b) If the acidity, density, viscosity or conductivity of the fluid sample are out of the permitted values given above: - Change the hydraulic fluid (Ref. TASK 12-36-29-611-807), (Ref. TASK 12-36-29-611-808) and (Ref. TASK 12-36-29-611-809).
R R R R R R
(3) Airbus has defined additional time limited authorizations to prevent aircraft operational impact in case of Chemical Contamination (Ref. SIL 29-081). Airbus considers the aircraft can stay in service during the additional time frames, waiting for corrective action and new results avaibility.
EFF : ALL 12-32-29 SROS
Page 309 Jan 01/06
------------------------------------------------------------------------------| NSA 307110 Requirements Additional Temporary | | Authorization | ------------------------------------------------------------------------------|Hydraulic |In Service |Corrective | Tolerance | Allowed Time | |Fluid |Limits |Action | | Frames | |Parameters | |Application | (see NOTE 1) | (see NOTE 2) | ------------------------------------------------------------------------------Acid Number
R R R
1.5mg KOH/g max
immediately
1.5 to 2.5mg KOH/g max
7 calendar days
Density 970 to 1066 at 23 +/- 3 deg kg/m3
immediately
Not Applicable
600 FH
Water Content
0.50% max
immediately
0.5% to 1% 1% to 1.5%
600 FH 7calendar days
Viscosity at 38 deg.C
6 to 12.5 CST
immediately
5.5 to 6 CST
10 calendar days or 150 FH
Chlorine Content
200 ppm max
immediately
200 to 300 ppm
10 calendar days or 150 FH
Electrical conductivity
0.30 immediately microSiemens.c minimum
lower than 0.30 600 FH microSiemens.cm min
NOTE : 1: Tolerance represent the level of contaminations allowed for ____ a limited time duration (see associated allowed time frame). NOTE : 2: Allowed Time Frames is an additional time the aircraft can ____ stay into service. It is the period from the discovery of the contamination to new results availability (including corrective action, new sample removal and new analysis).
EFF : 001-049, 201-249, 251-252, 255-299, 12-32-29 301-399, 401-449, 451-499, SROS
Page 310 Jul 01/06
**ON A/C 701-749, Subtask 12-32-29-281-052-A R
D. Chemical analysis
R R
(1) Chemical analysis must be to NSA307110 Limit Characteristics of fluid in operation.
R R
(2) If the values of the chemical analysis are not in the limits given in the table below, do the following corrective actions:
R R R R R R R
(a) If the water or chlorine content of the fluid sample are equal or more than the values given above: - Clean the hydraulic fluid with the HYDRAULIC PURIFIER (HSPA181380J) (Ref. TASK 12-36-29-615-801), (Ref. TASK 12-36-29-615802) and (Ref. TASK 12-36-29-615-803), - or change the hydraulic fluid (Ref. TASK 12-36-29-611-801), (Ref. TASK 12-36-29-611-802) and (Ref. TASK 12-36-29-611-803).
R R R R R
(b) If the acidity, density, viscosity or conductivity of the fluid sample are out of the permitted values given above: - Change the hydraulic fluid (Ref. TASK 12-36-29-611-807), (Ref. TASK 12-36-29-611-808) and (Ref. TASK 12-36-29-611-809). |end
R R R R R R
(3) Airbus has defined additional time limited authorizations to prevent aircraft operational impact in case of Chemical Contamination (Ref. SIL 29-081). Airbus considers the aircraft can stay in service during the additional time frames, waiting for corrective action and new results avaibility.
R EFF : 701-749, 12-32-29 SROS
Page 311 Jan 01/06
------------------------------------------------------------------------------| NSA 307110 Requirements Additional Temporary | | Authorization | ------------------------------------------------------------------------------|Hydraulic |In Service |Corrective | Tolerance | Allowed Time | |Fluid |Limits |Action | | Frames | |Parameters | |Application | (see NOTE 1) | (see NOTE 2) | ------------------------------------------------------------------------------Acid Number
R R R
1.5mg KOH/g max
immediately
1.5 to 2.5mg KOH/g max
7 calendar days
Density 970 to 1066 at 23 +/- 3 deg kg/m3
immediately
Not Applicable
600 FH
Water Content
0.50% max
immediately
0.5% to 1% 1% to 1.5%
600 FH 7calendar days
Viscosity at 38 deg.C
6 to 12.5 CST
immediately
5.5 to 6 CST
10 calendar days or 150 FH
Chlorine Content
200 ppm max
immediately
200 to 300 ppm
10 calendar days or 150 FH
Electrical conductivity
0.30 immediately microSiemens.c minimum
lower than 0.30 600 FH microSiemens.cm min
NOTE : 1: Tolerance represent the level of contaminations allowed for ____ a limited time duration (see associated allowed time frame). NOTE : 2: Allowed Time Frames is an additional time the aircraft can ____ stay into service. It is the period from the discovery of the contamination to new results availability (including corrective action, new sample removal and new analysis).
EFF : 701-749, 12-32-29 SROS
Page 312 Jul 01/06
**ON A/C ALL 5. Close-up ________ Subtask 12-32-29-611-050 A. Make sure that the fluid level in the hydraulic reservoir is correct. If necessary, fill the concerned reservoir: - for green reservoir (Ref. TASK 12-12-29-611-801) or (Ref. TASK 12-1229-611-802). - for blue reservoir (Ref. TASK 12-12-29-611-803) or (Ref. TASK 12-12-29611-804). - for yellow reservoir (Ref. TASK 12-12-29-611-805) or (Ref. TASK 12-1229-611-806). Subtask 12-32-29-410-050 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the MLG doors (Ref. TASK 32-12-00-410-801).
EFF : ALL 12-32-29 SROS
Page 313 Jan 01/06
APU - SERVICING _______________ TASK 12-32-49-281-801 Oil Sampling for Analysis WARNING : DO NOT TOUCH THE APU UNTIL IT IS SUFFICIENTLY COOL TO PREVENT BURNS _______ WHEN YOU DO THE MAINTENANCE TASK(S). 1. __________________ Reason for the Job R R
To find the causes of oil contamination (fuel, oil degradation and other causes).
R R
NOTE : You must get the sample 15 to 30 minutes after APU shutdown and ____ before you add oil to the tank. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No
specific specific specific specific specific specific
circuit breaker(s) safety clip(s) clean and lint-free cloth plastic bottle warning notice access platform 2.5 m (8 ft. 2 in.) access platform 7.2 m (23 ft. 7 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-13-49-612-801 24-42-00-861-801 24-42-00-862-801 29-00-00-864-804 12-32-49-991-001
Gravity Servicing of the APU Oil Reservoir Energize the Ground Service Network De-energize the Ground Service Network Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action. Fig. 301
EFF : ALL 12-32-49 SROS
Page 301 Oct 01/00
3. __________ Job Set-up Subtask 12-32-49-860-050 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). (2) Make sure that the hydraulic systems are depressurized (Ref. TASK 29-00-00-864-804). (3) Put the warning notice in position on the panel 215VU to tell persons not to start the APU. Subtask 12-32-49-010-050 B. Get Access to the Avionics Compartment (1) Put the access platform in position below the access door 811. (2) Open the access door 811. Subtask 12-32-49-865-050 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU APU FIRE SQUIB B 2WF P09 721VU APU FIRE VLV CTL 4WF P07 742VU APU START CTL 1KA C72 742VU APU FIRE SQUIB A 1WF J72 742VU APU FIRE VLV CTL 3WF J71 Subtask 12-32-49-010-051 D. Get Access (1) Put the access platform in position below the APU compartment. (2) Open the APU access door 315AL and and safety it in the open position. (3) Set the LIGHT SW 3LJ to the ON position.
EFF : ALL 12-32-49 SROS
Page 302 Jul 01/00
4. Procedure _________ (Ref. Fig. 301/TASK 12-32-49-991-001) Subtask 12-32-49-281-050 A. Get a sample CAUTION : MAKE SURE THAT THE SCUPPER OF THE OIL TANK IS CLEAN TO PREVENT _______ CONTAMINATION OF THE TANK DURING THE SERVICING OPERATION. CAUTION : USE A NEW AND VERY CLEAN PLASTIC BOTTLE WITH A NEW SCREW TOP _______ AND A NEW PLASTIC TUBE. DO NOT USE THESE ITEMS AGAIN. (1) Clean the oil tank scupper. - Clean the oil tank scupper with a clean and lint-free cloth, before you remove the oil filler cap. (2) Open the oil tank WARNING : REMOVE THE OIL TANK FILLER CAP AT LEAST 5 MINUTES AFTER _______ ENGINE SHUTDOWN TO LET TANK PRESSURE DECREASE. OTHERWISE, PRESSURIZED HOT OIL FROM THE TANK COULD CAUSE BURNS. R R R R
(a) Squeeze the plastic bottle (2) and put the free end of the tube into the oil through the filling port (3).
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(b) Release the pressure on the bottle to remove the oil sample by suction.
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(3) Tag the oil sample with these data: - APU total operating time. - Operating time since the last oil sampling. - Date of sample. - Identification of the APU (Serial Number). - Type and brand of the oil used.
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(4) Send the sample for chemical or spectrometric analysis to the laboratory as soon as possible.
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(5) Do a check of the oil level and fill the oil tank if necessary (Ref. TASK 12-13-49-612-801).
EFF : ALL 12-32-49 SROS
Page 303 Oct 01/00
Oil Sampling for Analysis Figure 301/TASK 12-32-49-991-001 EFF : ALL 12-32-49 SROS
Page 304 Jul 01/00
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(6) Close the oil tank. 5. Close-up ________ Subtask 12-32-49-410-050 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Set the LIGHT SW 3LJ to the OFF position. (3) Close the APU access door 315AL. (4) Remove the access platform(s). Subtask 12-32-49-865-051 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1KA, 1WF, 2WF, 3WF, 4WF Subtask 12-32-49-410-051 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the access door 811. (3) Remove the access platform(s). Subtask 12-32-49-860-051 D. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801) (2) Remove the warning notice(s). (3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL 12-32-49 SROS
Page 305 Oct 01/00
ENGINE OIL - SERVICING ______________________ TASK 12-32-79-281-803 Sampling of the Engine Oil. WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE AFTER THE ENGINE IS SHUTDOWN. _______ THE ENGINE CAN STAY HOT FOR A LONG TIME AFTER THE ENGINE IS SHUTDOWN. WARNING : USE PROTECTIVE CLOTHING WHEN YOU USE ENGINE OIL. OIL CAN CAUSE SKIN _______ IRRITATION. CAUTION : DO NOT OPERATE THE ENGINE WITHOUT SUFFICIENT OIL. THIS WILL CAUSE A _______ POSSIBLE INFLIGHT SHUTDOWN AND POSSIBLE DAMAGE TO THE ENGINE. CAUTION : DO NOT LET ENGINE FUEL OR OIL FALL ON THE ENGINE. YOU MUST _______ IMMEDIATELY REMOVE UNWANTED FUEL OR OIL WITH A CLOTH. THE FUEL OR OIL CAN CAUSE DAMAGE TO SOME ENGINE PARTS. 1. __________________ Reason for the Job To get a sample of engine oil to: - determine if there is fuel in the engine oil system - get warning information on the oil lube wetted parts. To determine fuel content in the oil, the recommended detection methods are: - a flash point test and - a viscosity test. If you find fuel in the oil, the suspect cause is the fuel/oil cooler located on the engine core at approximately the 9 oclock position. To get warning information for wear of oil lube wetted mechanical parts before failure, the recommended detection method is: - Spectrometric Oil Analysis Procedure (SOAP). This method is the analysis of submicroparticles suspended in oil using a direct spectrometer with automatic concentration computation.
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2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No
specific specific specific specific specific
circuit breaker(s) safety clip(s) squeeze plastic bottle 0.02 l (0.0052 USgal) adjustable access platform 1.22 m (4 ft.) access platform 2.5 m (8 ft. 2 in.) plastic hose 20 in. (0.5079 m)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-13-79-610-806 24-42-00-861-801 24-42-00-862-801
Servicing of the Engine Oil System Energize the Ground Service Network De-energize the Ground Service Network
3. __________ Job Set-up Subtask 12-32-79-861-052 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-32-79-941-053 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure and not more than 30 minutes before you do this procedure. Subtask 12-32-79-010-057 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-32-79 Page 302 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
(3) Open the protective door of the AC/DC emergency power-center 740VU. Subtask 12-32-79-865-054 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-32-79-010-058 E. Get Access (1) Put the adjustable access platform in position. (2) Open the upper left thrust reverser access door: - FOR 4030EM1 417DL - FOR 4030EM2 427DL 4. Procedure _________ Subtask 12-32-79-210-050 A. Get the Oil Sample NOTE : You must take the oil sample 30 minutes or less after the engine ____ shutdown. NOTE : Do not replenish the oil until after you take the sample. ____ NOTE : Sampling equipment must be sterile have no chemical action on oil ____ and fuel. (1) Remove the oil tank cap. (2) Put the plastic hose into the oil tank until the hose touches the bottom.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-32-79 Page 303 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
(3) Pull the hose out approximately 0.5 in. (12.6999 mm) from the bottom. (4) Using a siphon or a squeeze plastic bottle, take the oil sample from the tank. (5) Take 0.150 l (0.0396 USgal) for fuel contamination detection. (6) Take 0.015 l (0.0039 USgal) SOAP inspection. (7) Remove and discard the plastic hose. NOTE : It is important to use a new hose with each oil sample to make ____ sure of an accurate sample. (8) Install the bottle cap. (9) Install the oil tank cap as follows: (a) With the handle at open, align and install the cap to the filler neck. (b) Push down on the cap and turn the handle clockwise to close. (c) Push the handle into the cap to lock the cap. (d) Make sure that the cap is installed equally and completely. Subtask 12-32-79-610-050 B. Service the Engine Oil System (Ref. TASK 12-13-79-610-806) NOTE : Write the amount of oil that you added. ____ Subtask 12-32-79-410-056 C. Close the thrust reverser access door: FOR 4030EM1 417DL FOR 4030EM2 427DL
R EFF : 001-049, 201-249, 251-252, 255-299, 12-32-79 Page 304 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
Subtask 12-32-79-800-050 D. Miscellaneous (1) Write the information which follows on the label: (a) A/C registration number. (b) Engine serial number. (c) Date of sampling. (d) Engine hours. (e) Oil added since last sample. (2) Send the sample to the laboratory as fast as possible so that the sample is usable and the analysis is accurate. Subtask 12-32-79-210-051 E. Oil Contamination by Fuel (Acceptable Limits) NOTE : The laboratory will analyze the sample by one or all of the ____ following methods. (1) Flash Point Method Method
Acceptable Limits
ASTM D92-57
340 deg.F
(171 deg.C)
or higher SETA Flash
340 deg.F
(171 deg.C)
or higher (2) Viscosity Method Method ASTM D445
Acceptable Limits
35 percent increase from actual measured new oil viscosity at 100 deg.F (37.8 deg.C)
R EFF : 001-049, 201-249, 251-252, 255-299, 12-32-79 Page 305 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
5. Close-up ________ Subtask 12-32-79-865-055 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2 Subtask 12-32-79-410-057 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Close the access door 811. (4) Remove the access platform(s). Subtask 12-32-79-862-052 C. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-32-79 Page 306 301-399, 401-449, 451-499, Config-1 Jul 01/05 SROS
ENGINE OIL - SERVICING ______________________ TASK 12-32-79-280-801 Get a Sample of Engine Oil for Analysis 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No
specific specific specific specific specific
circuit breaker(s) safety clip(s) container - oil resistant 0.5 litres (0.132 USgal) syringe - oil 0.25 litre (0.066 USgal) adjustable access platform 1.22 m (4 ft.) access platform 2.5 m (8 ft. 2 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801
Energize the Ground Service Network De-energize the Ground Service Network
3. __________ Job Set-up Subtask 12-32-79-861-053 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-32-79-941-054 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure.
EFF : 701-749, 12-32-79 Page 301 Config-2 Apr 01/02 SROS
Subtask 12-32-79-010-059 C. Get Access to the Avionics Compartment (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the protective door of the AC/DC emergency power-center 740VU. Subtask 12-32-79-865-056 D. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-32-79-010-060 E. Get Access (1) Put the adjustable access platform in the correct position at the right side of the engine. (2) Open the access panel on the right fan cowl door: - FOR 4030EM1 416CR - FOR 4030EM2 426CR 4. Procedure _________ WARNING : YOU MUST NOT LET ENGINE OIL STAY ON YOUR SKIN. FLUSH THE OIL FROM _______ YOUR SKIN WITH WATER. THE OIL IS POISONOUS AND CAN BE ABSORBED INTO THE BODY.
EFF : 701-749, 12-32-79 Page 302 Config-2 Apr 01/02 SROS
Subtask 12-32-79-680-050 A. Get a sample of engine oil: (1) Remove the oil filler cap. (2) Use a clean syringe - oil 0.25 litre (0.066 USgal) to get approximately 0,25 litres (0.066 USgal) of oil from the engine oil tank. (3) Put the oil sample into a clean container - oil resistant 0.5 litres (0.132 USgal). Seal and identify the sample. (4) Install the oil filler cap. Subtask 12-32-79-280-050 B. Send the sample to a laboratory for analysis. The permitted levels of contamination by volume are as follows: (1) Fuel - aviation kerosine and diesel - 0.5 percent (2) Hydraulic oil - mineral and phosphate - 0.3 percent (3) Synthetic oil which is not approved - 10.0 percent (4) Mineral oil - 2.0 percent. 5. Close-up ________ Subtask 12-32-79-865-057 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2 Subtask 12-32-79-410-058 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the protective door of the AC/DC emergency power center 740VU.
EFF : 701-749, 12-32-79 Page 303 Config-2 Apr 01/02 SROS
(3) Close the access door 811. (4) Close the access panel on the right fan cowl door: - FOR 4030EM1 416CR - FOR 4030EM2 426CR (5) Remove the access platform(s). Subtask 12-32-79-862-053 C. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : 701-749, 12-32-79 Page 304 Config-2 Apr 01/02 SROS
PRE-CONDITIONING - DESCRIPTION AND OPERATION ____________________________________________ 1. _______ General You can pre-condition the aircraft on the ground with: - a ground air-supply unit through the Low Pressure (LP) ground connectors, - a ground air-supply unit through the High Pressure (HP) ground connectors, - the APU bleed air supply. For the pre-conditioning you have to open the air outflow valves 313HL and 315HL to permit an overpressure in the cabin. 2. __________________ System Description
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A. Pre-conditioning with the Low Pressure (LP) Ground Connector You can connect a ground air-supply unit to the LP ground connections for ventilation of the aircraft. It is not necessary to operate the air conditioning packs. There are two LP ground connectors installed on the bottom of the belly fairing (access door 191EB). Through these connectors you supply the air from a ground air-supply unit to the cabin air distribution and regulation system (Ref. 21-21-00).
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B. Pre-conditioning with the High Pressure (HP) Ground Connector You can connect a ground air-supply unit to the HP ground connections for ventilation of the aircraft. You have to operate the air conditioning packs for this condition. There are two HP ground connectors installed on the bottom of the belly fairing (access door 193GB). Through these connectors you supply the compressed air from a ground air-supply unit to the crossbleed duct. The air flows from the crossbleed duct to the air conditioning packs. From the air conditioning packs the air flows to the cabin air distribution and regulation system (Ref. 21-21-00).
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C. Pre-conditioning with the APU Bleed Air Supply The APU air system supplies bleed air to the aircraft pneumatic system (Ref. 36-12-00). You have to operate the air conditioning packs for this condition. The APU load compressor supplies the APU bleed air. When the APU bleed valve is in the opened position: - the Pressure Regulating Valves (PRV) close and thus shut off the engine bleed-air supply, - the APU supplies bleed air through the APU bleed air duct to the crossbleed duct. Then the air flows from the crossbleed duct to the air conditioning packs. From the air conditioning packs the air flows to the cabin air distribution and regulation system (Ref. 21-21-00).
EFF : ALL 12-33-00 SROS
Page 1 Jul 01/06
GROUND AIR PRE-CONDITIONING - MAINTENANCE PRACTICES ___________________________________________________ TASK 12-33-21-618-801 Pre-conditioning through the Low-Pressure Ground Connection WARNING : MAKE SURE THAT THE FWD AVIONICS ACCESS DOOR 811 IS OPEN WITH A _______ WARNING PLACARD ATTACHED TO IT. THE WARNING NOTICE MUST TELL PERSONS NOT TO CLOSE THE DOOR. THIS PREVENTS ACCIDENTAL PRESSURIZATION OF THE AIRCRAFT. CAUTION : DO NOT USE CONDITIONED AIR FROM THE PACKS AT THE SAME TIME AS AIR _______ FROM THE LOW-PRESSURE GROUND UNITS. THIS CAN CAUSE DAMAGE TO THE CHECK VALVES. R R R R
CAUTION : MAKE SURE THAT THE GROUND AIR-SUPPLY UNIT IS NOT TOO NEAR THE _______ AIRCRAFT AND THAT THE ENGINE EXHAUST PIPE OF THE GROUND AIR- SUPPLY UNIT POINTS AWAY FROM THE AIRCRAFT. HEAT FROM THIS UNIT AND FROM THE EXHAUST CAN CAUSE DAMAGE TO THE AIRCRAFT STRUCTURE. 1. __________________ Reason for the Job NOTE : There are alternative methods for the pre-conditioning. This task ____ gives one of the methods. For the other methods refer to the relevant tasks in this page block. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
ground air-supply unit(s) warning notice access platform 2.5 m (8 ft. 2 in.)
EFF : ALL 12-33-21 SROS
Page 201 Jan 01/03
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 12-33-21-991-001 12-33-21-991-002
Energize the Ground Service Network De-energize the Ground Service Network Fig. 201 Fig. 202
3. __________ Job Set-up (Ref. Fig. 201/TASK 12-33-21-991-001) Subtask 12-33-21-861-050 A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 12-33-21-010-051 B. Get Access (1) Open the access door 191EB. (2) Connect the ground air-supply unit(s) to the aircraft LP connector(s). (3) Put the access platform in position below the access door 811. (4) Open the access door 811. (5) Install a warning notice on the access door 811 to tell persons not to close the access door 811.
EFF : ALL 12-33-21 R SROS
Page 202 Jan 01/03
LP and HP Ground Connectors Figure 201/TASK 12-33-21-991-001 EFF : ALL 12-33-21 SROS
Page 203 Apr 01/98
4. Procedure _________ (Ref. Fig. 202/TASK 12-33-21-991-002) Subtask 12-33-21-618-050 A. Pre-conditioning through the LP Ground Connector(s) (1) On the panel 212VU, make sure that the CAB FANS pushbutton switch is in the on position (the OFF legend is off). (2) Start the ground air-supply unit(s) and - the airflow is max. 3.2 kg/sec (423.3 - the supplied air pressure is not more - the supplied air temperature does not deg.F).
make sure that: lb/min), than 65 mbar (0.94 psi), go above 70 deg.C (158.00
(3) Set the necessary output air temperature on the ground air-supply unit(s). Subtask 12-33-21-618-055 B. When the pre-conditioning is no longer necessary, stop the ground air-supply unit(s). 5. Close-up ________ Subtask 12-33-21-410-051 A. Close Access (1) Disconnect and remove the ground air-supply unit(s) from the aircraft LP connector(s). (2) Make sure that the work area is clean and clear of tools and other items. (3) Close the access door 191EB. (4) Close the access door 811. (5) Remove the warning notice(s). (6) Remove the access platform(s). (7) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL 12-33-21 R SROS
Page 204 Jan 01/03
Cockpit Panels 212VU and 225VU Figure 202/TASK 12-33-21-991-002 EFF : ALL 12-33-21 R SROS
Page 205 Jan 01/03
Subtask 12-33-21-862-050 B. De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 12-33-21 R SROS
Page 206 Jan 01/03
TASK 12-33-21-618-801- 01 Pre-conditioning through the High-Pressure Ground Connection WARNING : MAKE SURE THAT THE FWD AVIONICS ACCESS DOOR 811 IS OPEN WITH A _______ WARNING PLACARD ATTACHED TO IT. THE WARNING NOTICE MUST TELL PERSONS NOT TO CLOSE THE DOOR. THIS PREVENTS ACCIDENTAL PRESSURIZATION OF THE AIRCRAFT. CAUTION : MAKE SURE THAT THE GROUND-AIR SUPPLY IF FREE FROM OIL CONTAMINATION. _______ OIL CONTAMINATION CAN CAUSE THE SMELL OF OIL IN THE CABIN AND MAKE THE AIR-CONDITIONING PACKS UNSERVICEABLE. R R R R
CAUTION : MAKE SURE THAT THE GROUND AIR-SUPPLY UNIT IS NOT TOO NEAR THE _______ AIRCRAFT AND THAT THE ENGINE EXHAUST PIPE OF THE GROUND AIR- SUPPLY UNIT POINTS AWAY FROM THE AIRCRAFT. HEAT FROM THIS UNIT AND FROM THE EXHAUST CAN CAUSE DAMAGE TO THE AIRCRAFT STRUCTURE. 1. __________________ Reason for the Job NOTE : There are alternative methods for the pre-conditioning. This task ____ gives one of the methods. For the other methods refer to the relevant tasks in this page block. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
ground air-supply unit warning notice access platform 2.5 m (8 ft. 2 in.)
EFF : ALL 12-33-21 SROS
Page 207 Jan 01/03
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 24-41-00-862-801
Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A EIS Start Procedure EIS Stop Procedure Fig. 201 Fig. 202
31-60-00-860-801 31-60-00-860-802 12-33-21-991-001 12-33-21-991-002 3. __________ Job Set-up
(Ref. Fig. 202/TASK 12-33-21-991-002) Subtask 12-33-21-865-052 A. Make sure that this(these) circuit breaker(s) is(are) closed:
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------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------715VU L RECIRC FAN 1HG1 B54 721VU LAV+GALY EXTC FAN 1HU A02 721VU PACK 1 L1 115VAC 1HH1 F02 721VU PACK 1 L2 115VAC 3HH1 K04 721VU CAB PRESS MAN 3HL P11 721VU ZONE CTL SYS 1 1HK1 R08 721VU PACK 1 L2 28VDC 4HH1 R07 721VU PACK 1 L1 28VDC 2HH1 T08 **ON A/C 401-449, 451-499, 721VU EXTC FAN AFT CARGO
8HN
E02
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 722VU EXTC FAN FWD CARGO
11HN
EFF : ALL 12-33-21 SROS
A34
Page 208 Jan 01/06
------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------**ON A/C ALL 722VU 722VU 722VU 722VU 722VU 722VU 722VU 722VU 722VU 725VU 742VU 742VU 742VU 742VU 742VU 742VU
EXTC FAN BULK CRG PACK 2 L2 115VAC PACK 2 L1 115VAC AIR XBLEED AUTO CPC 2 CARGO VENT CTL L1 ZONE CTL SYS 2 PACK 2 L2 28VDC PACK 2 L1 28VDC R RECIRC FAN RAM AIR PACK 1 FLOW CTL CPC 1 AIR XBLEED MAN PACK 2 FLOW CTL CARGO VENT CTL L2
5HN 3HH2 1HH2 1HV 2HL 2HN 1HK2 4HH2 2HH2 1HG2 1HZ 1HB1 1HL 2HV 1HB2 1HN
A37 E44 H48 R45 U44 U43 U42 U41 U40 B23 A68 A67 A66 C75 F80 L72
Subtask 12-33-21-860-054 B. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00-860-801). (3) On the ECAM control panel, push the BLEED key (on the SD, the BLEED page comes into view). (4) On the panel 225VU make sure that: - the PACK 1 and PACK 2 pushbutton switches are in the on position (the FAULT legends are on and the OFF legends are off), - the COCKPIT and the CABIN temperature selectors are at the 12 oclock position, - the HOT AIR 1 and the HOT AIR 2 pushbutton switches are in the on position (the OFF legends are off). (5) On the panel 225VU, set the the crossbleed valve selector-switch to OPEN.
EFF : ALL 12-33-21 R SROS
Page 209 Jan 01/03
(6) On the panel 212VU, make sure that the CAB FANS pushbutton switch is in the on position (the OFF legend is off). Subtask 12-33-21-010-052 C. Get Access (Ref. Fig. 201/TASK 12-33-21-991-001) (1) Open the access door 193GB. (2) Connect the ground air-supply unit to the aircraft HP connectors 7300HA and 7302HA. (3) Put the access platform in position below the access door 811. (4) Open the access door 811. (5) Install a warning notice on the access door 811 to tell persons not to close the access door 811. 4. Procedure _________ (Ref. Fig. 202/TASK 12-33-21-991-002) Subtask 12-33-21-618-056 A. Pre-conditioning through the HP Ground Connector (1) Start the ground air-supply unit and make sure that: - the airflow is max. 3.2 kg/sec (423.3 lb/min), - the supplied air pressure is not more than 3.5 bar (50.7631 psi), - the supplied air temperature does not go above 260 deg.C (500.00 deg.F). NOTE : On the panel 225VU, the PACK 1 and PACK 2 FAULT legends go off ____ when the flow control valves open. (2) On the AIR BLEED page of the System Display, make sure that the pack discharge-temperature indication is normal (green). Subtask 12-33-21-618-057 B. When the pre-conditioning is no longer necessary stop the ground air-supply unit.
EFF : ALL 12-33-21 R SROS
Page 210 Jan 01/03
5. Close-up ________ Subtask 12-33-21-860-055 A. Put the Aircraft back to its Initial Configuration (1) On the panel 225VU, set the crossbleed valve selector-switch to AUTO. (2) Do the EIS stop procedure (Ref. TASK 31-60-00-860-802). (3) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). Subtask 12-33-21-410-052 B. Close Access (1) Disconnect and remove the ground air-supply unit from the HP connectors 7300HA and 7302HA. (2) Make sure that the work area is clean and clear of tools and other items. (3) Close the access door 193GB. (4) Close the access door 811. (5) Remove the warning notice(s). (6) Remove the access platform(s). (7) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL 12-33-21 R SROS
Page 211 Jan 01/03
TASK 12-33-21-618-801- 02 Pre-conditioning with the APU WARNING : MAKE SURE THAT THE FWD AVIONICS ACCESS DOOR 811 IS OPEN WITH A _______ WARNING PLACARD ATTACHED TO IT. THE WARNING NOTICE MUST TELL PERSONS NOT TO CLOSE THE DOOR. THIS PREVENTS ACCIDENTAL PRESSURIZATION OF THE AIRCRAFT. 1. __________________ Reason for the Job NOTE : There are alternative methods for the pre-conditioning. This task ____ gives one of the methods. For the other methods refer to the relevant tasks in this page block. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
warning notice access platform 2.5 m (8 ft. 2 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 24-41-00-862-801 31-60-00-860-801 31-60-00-860-802 49-00-00-860-801 49-00-00-860-802 12-33-21-991-002
Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A EIS Start Procedure EIS Stop Procedure Start of the APU with External Power Supply Shutdown of the APU with Power Supply from the APU Battery Fig. 202
EFF : ALL 12-33-21 R SROS
Page 212 Jan 01/03
3. __________ Job Set-up (Ref. Fig. 202/TASK 12-33-21-991-002) Subtask 12-33-21-865-053 A. Make sure that this(these) circuit breaker(s) is(are) closed:
R
------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------715VU L RECIRC FAN 1HG1 B54 721VU LAV+GALY EXTC FAN 1HU A02 721VU PACK 1 L1 115VAC 1HH1 F02 721VU PACK 1 L2 115VAC 3HH1 K04 721VU CAB PRESS MAN 3HL P11 721VU ZONE CTL SYS 1 1HK1 R08 721VU PACK 1 L2 28VDC 4HH1 R07 721VU PACK 1 L1 28VDC 2HH1 T08 **ON A/C 401-449, 451-499, 721VU EXTC FAN AFT CARGO
8HN
E02
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 722VU EXTC FAN FWD CARGO
11HN
A34
**ON A/C ALL 722VU 722VU 722VU 722VU 722VU 722VU 722VU 722VU 722VU 725VU 742VU 742VU 742VU 742VU
EXTC FAN BULK CRG PACK 2 L2 115VAC PACK 2 L1 115VAC AIR XBLEED AUTO CPC 2 CARGO VENT CTL L1 ZONE CTL SYS 2 PACK 2 L2 28VDC PACK 2 L1 28VDC R RECIRC FAN RAM AIR PACK 1 FLOW CTL CPC 1 AIR XBLEED MAN
5HN 3HH2 1HH2 1HV 2HL 2HN 1HK2 4HH2 2HH2 1HG2 1HZ 1HB1 1HL 2HV
EFF : ALL 12-33-21 SROS
A37 E44 H48 R45 U44 U43 U42 U41 U40 B23 A68 A67 A66 C75
Page 213 Jan 01/06
------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------742VU PACK 2 FLOW CTL 1HB2 F80 742VU CARGO VENT CTL L2 1HN L72 Subtask 12-33-21-860-056 B. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00-860-801). (3) On the ECAM control panel, push the BLEED key (on the SD, the BLEED page comes into view). (4) On the panel 225VU make sure that: - the PACK 1 and PACK 2 pushbutton switches are in the on position (the FAULT legends are on and the OFF legends are off), - the COCKPIT and the CABIN temperature selectors are at the 12 oclock position, - the HOT AIR 1 and the HOT AIR 2 pushbutton switches are in the on position (the OFF legends are off). (5) On the panel 225VU, set the crossbleed valve selector-switch to OPEN. (6) On the panel 212VU, make sure that the CAB FANS switch is in the on position (the OFF legend is off). Subtask 12-33-21-010-053 C. Safety Precautions (1) Put the access platform in position below the access door 811. (2) Open the access door 811. (3) Install a warning notice on the access door 811 to tell persons not to close the access door 811.
EFF : ALL 12-33-21 R SROS
Page 214 Jan 01/04
4. Procedure _________ (Ref. Fig. 202/TASK 12-33-21-991-002) Subtask 12-33-21-618-058 A. Pre-conditioning with the APU (1) Start the APU (Ref. TASK 49-00-00-860-801). NOTE : On the panel 225VU, the PACK 1 and PACK 2 FAULT legends go off ____ when the flow control valves open. (2) On the panel 225VU push the APU BLEED pushbutton switch to the on position (the ON legend comes on). (3) On the AIR BLEED page of the System Display, make sure that the pack discharge temperature-indication is normal (green). Subtask 12-33-21-618-059 B. When the pre-conditioning is no longer necessary: (1) On the panel 225VU push the APU BLEED pushbutton switch to the off position (the ON legend goes off). (2) Stop the APU (Ref. TASK 49-00-00-860-802). 5. Close-up ________ Subtask 12-33-21-860-057 A. Put the Aircraft back to its Initial Configuration (1) On the panel 225VU, set the crossbleed valve selector-switch to AUTO. (2) Do the EIS stop procedure (Ref. TASK 31-60-00-860-802). (3) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801)
EFF : ALL 12-33-21 R SROS
Page 215 Jan 01/03
Subtask 12-33-21-410-053 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Remove the warning notice(s). (3) Close the access door 811. (4) Remove the access platform(s). (5) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL 12-33-21 SROS
Page 216 Jan 01/03
GROUNDING POINTS - DESCRIPTION AND OPERATION ____________________________________________ 1. General _______ This section gives the instructions to ground the aircraft for the refuel/defuel operations or for the maintenance operations. In the other conditions, the electrostatic discharge of the aircraft is made through the tires. It includes the topic below: 12-34-24/P. Block 201.
EFF : ALL 12-34-00 SROS
Page 1 Apr 01/98
AIRCRAFT GROUNDING - MAINTENANCE PRACTICES __________________________________________ TASK 12-34-24-860-801-A Aircraft Grounding for the Refuel/Defuel and Oxygen Servicing Operations WARNING : DO NOT WEAR A HEADSET OR TOUCH CABLES/LINES CONNECTED TO THE AIRCRAFT _______ WHEN THERE IS A RISK OF LIGHTNING. LIGHTNING IS DANGEROUS. 1. __________________ Reason for the Job To electrostatically balance the aircraft during the refuel/defuel and oxygen servicing operations. NOTE : Bonding is essential, grounding is recommended. ____ 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
bonding cable ground cable
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-34-24-991-001 12-34-24-991-002
Fig. 201 Fig. 202
3. __________ Job Set-up Subtask 12-34-24-210-052 A. Safety Precautions R R
(1) Make sure that the fuel tanker or oxygen ground filling equipment is grounded.
EFF : ALL 12-34-24 SROS
Page 201 Jan 01/07
4. Procedure _________ Subtask 12-34-24-480-052 A. Connection of the Ground Cables WARNING : ALWAYS CONNECT THE GROUND CABLE TO THE PARKING GROUND POINT _______ BEFORE YOU CONNECT IT TO THE AIRCRAFT. DO NOT ATTACH THE CABLE TO THE AIRCRAFT FIRST (THERE IS A RISK OF ELECTRIC SHOCK). NOTE : For the satisfactory removal of an electrical charge from the ____ aircraft: - the aircraft ground cable must have a section of 22 mm2 (0.0033 in2) or more. - the total electrical resistance of the cable between the parking ground point and the grounding point of the landing gear must not be more than 500 milliohms. - the resistance between the end connector on the ground cable and the nearest adjacent metal part of the landing gear must not be more than 10 milliohms. (1) Connect a ground cable to the grounding point on one of the MLG legs or on the NLG leg, (Ref. Fig. 201/TASK 12-34-24-991-001) R R
(2) Connect a bonding cable between the fuel tanker or the oxygen ground filling equipment and a grounding point on one of the MLG legs or the NLG leg, (Ref. Fig. 201/TASK 12-34-24-991-001) or connect a bonding cable between the fuel tanker and the grounding point on the upper wing surface (Ref. Fig. 202/TASK 12-34-24-991-002) The aircraft wheels must be on ground. 5. Close-up ________ Subtask 12-34-24-080-052 A. Disconnect the ground and bonding cables. (1) After the refuel/defuel or oxygen servicing operation, disconnect all the grounding and bonding cables.
EFF : ALL 12-34-24 SROS
Page 202 Jan 01/07
Location of the Grounding Points on the NLG and MLG Figure 201/TASK 12-34-24-991-001 EFF : ALL 12-34-24 SROS
Page 203 Apr 01/98
Grounding Point on the Wing Upper Surface Figure 202/TASK 12-34-24-991-002 EFF : ALL 12-34-24 SROS
Page 204 Apr 01/98
TASK 12-34-24-860-802 Aircraft Grounding for the Maintenance Operations WARNING : DO NOT WEAR A HEADSET OR TOUCH CABLES/LINES CONNECTED TO THE AIRCRAFT _______ WHEN THERE IS A RISK OF LIGHTNING. LIGHTNING IS DANGEROUS. 1. __________________ Reason for the Job R
To electrostatically balance the aircraft during the maintenance operations. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
ground cable
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-34-24-991-001 12-34-24-991-002
Fig. 201 Fig. 202
3. __________ Job Set-up Subtask 12-34-24-869-051 A. Not applicable. 4. Procedure _________ Subtask 12-34-24-210-051 A. Safety Precautions R
(1) Make sure that the access platform or the step ladder are grounded.
EFF : ALL 12-34-24 SROS
Page 205 Jan 01/07
Subtask 12-34-24-480-051 B. Connection of the Ground Cables WARNING : ALWAYS CONNECT THE GROUND CABLE TO THE PARKING GROUND POINT _______ BEFORE YOU CONNECT IT TO THE AIRCRAFT. DO NOT ATTACH THE CABLE TO THE AIRCRAFT FIRST (THERE IS A RISK OF ELECTRIC SHOCK). NOTE : For the satisfactory removal of an electrical charge from the ____ aircraft: - the aircraft ground cable must have a section of 22 mm2 (0.0033 in2) or more (for copper only). - the total electrical resistance of the cable between the parking ground point and the grounding point on the landing gear must not be more than 500 milliohms. - the resistance between the end connector on the ground cable and the nearest adjacent metal part of the landing gear must not be more than 10 milliohms.
R R
R R
(1) We recommend to connect the parking or the hangar ground cable to the aircraft grounding point on one of the MLG legs or on the NLG leg, (Ref. Fig. 201/TASK 12-34-24-991-001) The aircraft wheels must be on ground. NOTE : If the aircraft is on jacks for retraction and extension ____ checks of the landing gear, connect the parking or the hangar ground cable: - to the aircraft grounding point on the wings, (Ref. Fig. 202/TASK 12-34-24-991-002)
R R R
(2) We recommend to connect the ground cable of the step ladder or the access platform to the aircraft grounding point on one of the MLG legs or the NLG leg. The aircraft wheels must be on ground. NOTE : If the aircraft is on jacks for retraction and extension ____ checks of the landing gear, connect the parking or the hangar ground cable: - to the aircraft grounding point on the wings, (Ref. Fig. 202/TASK 12-34-24-991-002)
EFF : ALL 12-34-24 SROS
Page 206 Jan 01/07
5. Close-up ________ Subtask 12-34-24-080-051 A. Disconnect the ground cables. (1) After the maintenance operation, disconnect all the grounding cables.
EFF : ALL 12-34-24 SROS
Page 207 Jan 01/07
SYSTEM LINE FLUSHING - DESCRIPTION AND OPERATION ________________________________________________ 1. General _______ This section gives the instructions related to the flushing of a system line to remove all foreign matters from the fluid and from the system line. The fluid may be used again only if its characteristics obey the applicable specifications. It includes the topics below: 12-36-29/P. Block 301 HYDRAULIC POWER
EFF : ALL 12-36-00 SROS
Page 1 Apr 01/98
HYDRAULIC POWER - SERVICING ___________________________ R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, TASK 12-36-29-170-801 Flushing of the Case-Drain line of the Green Hydraulic System WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job To flush the Green hydraulic system after a failure of the engine pump. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No No No
specific specific specific specific specific specific specific specific specific specific
adaptor adjustable access platform blanking plug circuit breaker(s) safety clip(s) hydraulic power cart strap warning notice access platform 2.5 m (8 ft. 2 in.) container 20 l (5.2833 USgal) access platform 3 m (9 ft. 10 in.)
EFF : ALL 12-36-29 SROS
Page 301 Jul 01/05
------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific 98F12303000000
container 5 l (1.3208 USgal) Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft) 1 HYDRAULIC CONNECTORS
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-801 12-12-29-611-802 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-10-00-611-801 29-11-43-600-802 29-11-44-600-801 29-14-00-614-801 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 78-30-00-040-804 78-30-00-440-804 12-36-29-991-032 12-36-29-991-013 FOR FIN 4030EM1 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801
Fill the Green Hydraulic Reservoir with a Hydraulic Service Cart Fill the Green Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Drainage of the Green Hydraulic Reservoir Servicing of the (Forward) Engine-Pump Case-Drain Filter Element 5013JM1 Servicing of the Green Reservoir LP-Filter (5011JM1) Depressurization of the Green Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Deactivation of the Thrust Reverser for Maintenance Reactivation of the Thrust Reverser after Maintenance Fig. 301 Fig. 302 Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS)
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 302 Jul 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------78-30-00-410-801 FOR FIN 4030EM2 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801 78-30-00-410-801
Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Opening of (5120EA) Closing of (5120EA) Opening of 4130KS) Closing of 4130KS)
the Aft Fan Cowl Doors (5110EA) and the Aft Fan Cowl Doors (5110EA) and the Thrust Reverser Cowl Doors (4120KS to the Thrust Reverser Cowl Doors (4120KS to
3. __________ Job Set-up Subtask 12-36-29-860-062 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Make sure that the Green hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-804). (3) Depressurize the reservoir of the Green hydraulic system (Ref. TASK 29-14-00-614-801). (4) Drain the Green hydraulic reservoir (Ref. TASK 29-10-00-611-801). Subtask 12-36-29-941-062 B. Safety Precautions (1) Make sure that the engine 1(2), shutdown occurred not less than 5 minutes before you do this procedure. (2) On the panel 225VU, make sure that the APU BLEED pushbutton switch is released (ON legend off) and install a warning notice to tell persons not to use it.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 303 Jul 01/05
(3) Put a warning notice in position to tell persons not to pressurize the hydraulic system: - on the HYD/FUEL control panel 245VU in the cockpit, - on the Green hydraulic system, access door 197CB. (4) On the panel 125VU: - make sure that the ENG MASTER switches for the two engines are in the OFF position, - put a warning notice to tell persons not to supply power to the EEC. (5) On the panel 285VU: - make sure that the ON legend of the related ENG FADEC GND PWR pushbutton switch is off, - put a warning notice to tell persons not to supply power to the FADEC system. (6) Put a container below the Green hydraulic engine pump and below the case drain filter. Subtask 12-36-29-865-076 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU HYD PUMP G CTL 9JV U09 721VU HYD PUMP G ENG 1 14JG2 X11 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 721VU HYD PUMP G CTL 9JV U09 722VU FADEC B ENG 2 13KS2 K49 722VU HYD PUMP G ENG 2 14JG1 X45 742VU FADEC A ENG 2 12KS2 Q74
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 304 Jul 01/05
Subtask 12-36-29-010-075 D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Open the fan cowl doors FOR 4030EM1 Open the door 415BL (Ref. TASK 71-13-00-010-802). FOR 4030EM2 Open the door 425BL (Ref. TASK 71-13-00-010-802). Subtask 12-36-29-040-062 E. Make the thrust reverser unserviceable for maintenance (Ref. TASK 78-3000-040-804). Subtask 12-36-29-010-132 F. Get Access (1) Open the right thrust-reverser door: FOR 4030EM1 Open the door 417AL (Ref. TASK 78-30-00-010-801). FOR 4030EM2 Open the door 427AL (Ref. TASK 78-30-00-010-801). (2) Put the access platform in position. (3) Put a container under the applicable hose. Subtask 12-36-29-010-076 G. Get access to the avionics compartment. (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the door of the AC/DC emergency power-center 740VU. (4) Put the adjustable access platform in position.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 305 Jul 01/05
4. Procedure _________ Subtask 12-36-29-860-086 A. Preparation before the flushing of the Case-Drain line (Ref. Fig. 301/TASK 12-36-29-991-032) CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE ON THE GROUND HYDRAULIC CART _______ IS SET TO A MINIMUM OF 7 BARS (101.53 PSI). CAUTION : BE CAREFUL WHEN YOU DISCONNECT THE RETURN LINE FROM THE _______ RESERVOIR. THE HYDRAULIC FLUID IN THE LINE WILL FLOW OUT. (1) Remove the two clamps (2) from the return line (1). (2) Disconnect the return line (1) from the reservoir and from the filter (5011JM1). (3) Remove the return line (1) between the reservoir and from the filter (5011JM1). (4) Put blanking plug to the reseroir. (5) Connect the return hose of the hydraulic power cart to the filter (5011JM1) with the hydraulic power cart/return line interface (98F12303000100) of the HYDRAULIC CONNECTORS (98F12303000000). (6) Attach the return of the hydraulic power cart to the aircraft structure with a strap. (7) Disconnect the case drain line from the engine pump. (8) Put a blanking plug to the case drain. (9) Connect the pressure hose of the hydraulic power cart to the case drain line with the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000). Subtask 12-36-29-170-062 B. Flushing of the Case-Drain Line (Ref. Fig. 302/TASK 12-36-29-991-013) adaptor. (1) Operate the hydraulic power cart for 2mn at 20 bars. (2) Stop the hydraulic power cart.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 306 Jul 01/05
(3) Replace the hydraulic filters, case drain and LP: - the two case drain filters 5013JM1 (Ref. TASK 29-11-43-600-802), - the LP filter 5011JM1 (Ref. TASK 29-11-44-600-801). Subtask 12-36-29-420-062 C. Connection of the Hydraulic Line (1) Remove the strap which attach the return hose of the hydraulic power cart to the aircraft structure. (2) Remove the blanking plug from the reservoir. (3) Remove the hydraulic power cart/return line interface (98F12303000100) of the HYDRAULIC CONNECTORS (98F12303000000) from the filter (5011JM1) and from the hydraulic power cart. (4) Connect the return line (1) to the reservoir and to the filter (5011JM1). (5) Install the two clamps (2) on the return line (1). (6) Remove the blanking plug from the case drain. (7) Remove the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000) from the case drain line and from the hydraulic power cart. (8) Connect the case drain line to the engine pump. (9) TORQUE the case drain line to between 2.43 and 3.16 m.daN (17.92 and 23.30 lbf.ft). Subtask 12-36-29-865-077 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 4030EM1 9JV, 14JG2, 12KS1, 13KS1 FOR 4030EM2 9JV, 14JG1, 12KS2, 13KS2 Subtask 12-36-29-611-062 E. Fill the Green hydraulic reservoir (Ref. TASK 12-12-29-611-801) or (Ref. TASK 12-12-29-611-802).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 307 Jul 01/05
Hydraulic Connections Figure 301/TASK 12-36-29-991-032- 12 (SHEET 1) R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 308 Jul 01/05
Hydraulic Connections Figure 301/TASK 12-36-29-991-032- 22 (SHEET 2) R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 309 Jul 01/05
Flushing of the Case-Drain Line of the Green Hydraulic System Figure 302/TASK 12-36-29-991-013 R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 310 Jul 01/05
Subtask 12-36-29-863-062 F. Pressurize the Green hydraulic reservoir (Ref. TASK 29-14-00-614-804). Subtask 12-36-29-410-131 G. Close the right thrust reverser : - FOR 4030EM1 close the door 417AL (Ref. TASK 78-30-00-410-801) - FOR 4030EM2 close the door 427AL (Ref. TASK 78-30-00-410-801) Subtask 12-36-29-440-062 H. Make sure that the thrust reverser is serviceable after maintenance (Ref. TASK 78-30-00-440-804). Subtask 12-36-29-410-074 J. Close the fan cowl doors FOR 4030EM1 - close the door 415BL (Ref. TASK 71-13-00-410-802) FOR 4030EM2 - close the door 425BL (Ref. TASK 71-13-00-410-802). Subtask 12-36-29-281-062 K. Sampling (1) Perform a fluid sampling for particular contamination (Ref. TASK 1232-29-281-801). (2) Perform in daily check, the check of the clogging indicators, of the case drain filters 5013JM1, HP filters 5111JM101, 5111JM102, LP filter 5011JM1. Do this operation again until the clogging indicator stay in. 5. Close-up ________ Subtask 12-36-29-410-075 A. Close Access (1) Close the door of the AC/DC emergency power-center 740VU. (2) Close the access door 811.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 311 Jul 01/05
(3) Remove the access platform(s). (4) Close the MLG doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-942-062 B. Remove the safety devices (1) Remove the warning notice(s). Subtask 12-36-29-862-062 C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 312 Jul 01/05
**ON A/C 701-749, TASK 12-36-29-170-801-A Flushing of the Case-Drain line of the Green Hydraulic System WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job To flush the Green hydraulic system after a failure of the engine pump. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No No
specific specific specific specific specific specific specific specific specific
98F12303000000
adjustable access platform blanking plug circuit breaker(s) safety clip(s) hydraulic power cart strap warning notice access platform 2.5 m (8 ft. 2 in.) container 5 l (1.3208 USgal) Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft) 1 HYDRAULIC CONNECTORS
R EFF : 701-749, 12-36-29 SROS
Page 313 Apr 01/02
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-801 12-12-29-611-802 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-10-00-611-801 29-11-43-600-807 29-11-44-600-801 29-14-00-614-801 R 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 12-36-29-991-033 12-36-29-991-019 FOR FIN 4030EM1 71-13-00-010-805 71-13-00-410-805 FOR FIN 4030EM2 71-13-00-010-805 71-13-00-410-805
Fill the Green Hydraulic Reservoir with a Hydraulic Service Cart Fill the Green Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Drainage of the Green Hydraulic Reservoir Servicing of the Engine-Pump Case Drain Filter (5013JM1) Servicing of the Green Reservoir LP-Filter (5011JM1) Depressurization of the Green Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Fig. 303 Fig. 304 Open the Fan Cowl Doors Close the Fan Cowl Doors Open the Fan Cowl Doors Close the Fan Cowl Doors
3. __________ Job Set-up Subtask 12-36-29-860-068 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Make sure that the Green hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-804).
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(3) Depressurize the reservoir of the Green hydraulic system (Ref. TASK 29-14-00-614-801). (4) Drain the Green hydraulic reservoir (Ref. TASK 29-10-00-611-801). Subtask 12-36-29-941-068 B. Safety Precautions (1) Make sure that the engine 1(2), shutdown occurred not less than 5 minutes before you do this procedure. (2) On the panel 225VU, make sure that the APU BLEED pushbutton switch is released (ON legend off) and install a warning notice to tell persons not to use it. (3) Put a warning notice in position to tell persons not to pressurize the hydraulic system: - on the HYD/FUEL control panel 245VU in the cockpit, - on the Green hydraulic system, access door 197CB. (4) On the panel 125VU: - make sure that the ENG MASTER switches for the two engines are in the OFF position, - put a warning notice to tell persons not to supply power to the EEC. (5) On the panel 285VU: - make sure that the ON legend of the related ENG FADEC GND PWR pushbutton switch is off, - put a warning notice to tell persons not to supply power to the FADEC system. (6) Put a container below the Green hydraulic engine pump and below the case drain filter.
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Subtask 12-36-29-865-088 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU HYD PUMP G CTL 9JV U09 722VU FADEC B ENG 1 13KS1 D44 742VU HYD PUMP G ENG 1 14JG2 E67 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 721VU HYD PUMP G CTL 9JV U09 722VU FADEC B ENG 2 13KS2 K49 722VU HYD PUMP G ENG 2 14JG1 X45 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-36-29-010-087 D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Open the fan cowl doors FOR 4030EM1 Open the door 416AR (Ref. TASK 71-13-00-010-805) FOR 4030EM2 Open the door 426AR (Ref. TASK 71-13-00-010-805). Subtask 12-36-29-010-088 E. Get access to the avionics compartment. (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the door of the AC/DC emergency power-center 740VU. (4) Put the adjustable access platform in position.
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4. Procedure _________ Subtask 12-36-29-860-092 A. Preparation before the flushing of the Case-Drain line (Ref. Fig. 303/TASK 12-36-29-991-033) R R
CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE ON THE GROUND HYDRAULIC CART _______ IS SET TO A MINIMUM OF 7 BARS (101.53 PSI). CAUTION : BE CAREFUL WHEN YOU DISCONNECT THE RETURN LINE FROM THE _______ RESERVOIR. THE HYDRAULIC FLUID IN THE LINE WILL FLOW OUT. (1) Remove the two clamps (2) from the return line (1). (2) Disconnect the return line (1) from the reservoir and from the filter (5011JM1). (3) Remove the return line (1) between the reservoir and the filter (5011JM1). (4) Put blanking plug to the reservoir. (5) Connect the return hose of the hydraulic power cart to the filter (5011JM1) with the hydraulic power cart/return line interface (98F12303000100) of the HYDRAULIC CONNECTORS (98F12303000000). (6) Attach the return hose of the hydraulic power cart to the aircraft structure with a strap. (7) Disconnect the case drain line from the engine pump. (8) Put a blanking plug to the case drain. (9) Connect the pressure hose of the hydraulic power cart to the case drain line with the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000). Subtask 12-36-29-170-068 B. Flushing of the Case-Drain Line (Ref. Fig. 304/TASK 12-36-29-991-019) (1) Operate the hydraulic power cart for 2mn at 20 bars. (2) Stop the hydraulic power cart.
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Hydraulic Connections Figure 303/TASK 12-36-29-991-033- 12 (SHEET 1) EFF : 701-749, 12-36-29 R SROS
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Hydraulic Connections Figure 303/TASK 12-36-29-991-033- 22 (SHEET 2) R EFF : 701-749, 12-36-29 SROS
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Flushing of the Case-Drain Line of the Green Hydraulic system Figure 304/TASK 12-36-29-991-019 EFF : 701-749, 12-36-29 R SROS
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INTENTIONALLY BLANK
R 12-36-29 SROS
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INTENTIONALLY BLANK
R 12-36-29 SROS
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(3) Replace the hydraulic filters, case drain and LP: - the two case drain filters 5013JM1 (Ref. TASK 29-11-43-600-807), - the LP filter 5011JM1 (Ref. TASK 29-11-44-600-801). Subtask 12-36-29-420-068 C. Connection of the Hydraulic Line (1) Remove the strap which attach the return hose of the hydraulic power cart to the aircraft structure. (2) Remove the blanking plug from the reservoir. (3) Remove the hydraulic power cart/return line interface (98F12303000100) of the HYDRAULIC CONNECTORS (98F12303000000) from the filter (5011JM) and from the hydraulic power cart. (4) Connect the return line (1) to the resevoir and to the filter (5011JM1). (5) Install the two clamps (2) on the return line (1). (6) Remove the blanking plug from the case drain. (7) Remove the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000) from the case drain line and from the hydraulic power cart. (8) Connect the case drain line to the engine pump. (9) TORQUE the case drain line to between 2.43 and 3.16 m.daN (17.92 and 23.30 lbf.ft). Subtask 12-36-29-865-089 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 4030EM1 9JV, 14JG2, 12KS1, 13KS1 FOR 4030EM2 9JV, 14JG1, 12KS2, 13KS2 Subtask 12-36-29-611-068 E. Fill the Green hydraulic reservoir (Ref. TASK 12-12-29-611-801) or (Ref. TASK 12-12-29-611-802).
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Subtask 12-36-29-863-068 F. Pressurize the Green hydraulic reservoir (Ref. TASK 29-14-00-614-804). Subtask 12-36-29-410-086 G. Close the fan cowl doors FOR 4030EM1 - close the door 416AR (Ref. TASK 71-13-00-410-805) FOR 4030EM2 - close the door 426AR (Ref. TASK 71-13-00-410-805). Subtask 12-36-29-281-068 H. Sampling (1) Perform a fluid sampling for particular contamination (Ref. TASK 1232-29-281-801). (2) Perform in daily check, the check of the clogging indicators, of the case drain filters 5013JM1, HP filters 5111JM101, 5111JM102, LP filter 5011JM1. Do this operation again until the clogging indicator stay in. 5. Close-up ________ Subtask 12-36-29-410-087 A. Close Access (1) Close the door of the AC/DC emergency power-center 740VU. (2) Close the access door 811. (3) Remove the access platform(s). (4) Close the MLG doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-942-068 B. Remove the safety devices (1) Remove the warning notice(s).
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Subtask 12-36-29-862-068 C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
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R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, TASK 12-36-29-170-802 Flushing of the HP line of the Green Hydraulic System WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job To flush the Green hydraulic system after a failure of the engine pump. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No No No
specific specific specific specific specific specific specific specific specific specific
adjustable access platform blanking plugs circuit breaker(s) safety clip(s) hydraulic power cart warning notice access platform 2.5 m (8 ft. 2 in.) container 20 l (5.2833 USgal) access platform 3 m (9 ft. 10 in.) container 5 l (1.3208 USgal) Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft)
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------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific 98F12303000000
Torque Wrench : range 1.00 to 10.00 m.daN (8.00 to 75.00 lbf.ft) Torque Wrench : range 2.00 to 20.00 m.daN (15.00 to 150.00 lbf.ft) 1 HYDRAULIC CONNECTORS
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-801 12-12-29-611-802 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-11-45-600-801 29-14-00-614-801 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 78-30-00-040-804 78-30-00-440-804
Fill the Green Hydraulic Reservoir with a Hydraulic Service Cart Fill the Green Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Servicing of the Green HP Filter (5111JM101,5111JM102) Depressurization of the Green Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Deactivation of the Thrust Reverser for Maintenance Reactivation of the Thrust Reverser after Maintenance
R 12-36-29-991-035 12-36-29-991-014 FOR FIN 4030EM1 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801
Fig. 305 Fig. 306 Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS)
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------78-30-00-410-801 FOR FIN 4030EM2 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801 78-30-00-410-801
Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Opening of (5120EA) Closing of (5120EA) Opening of 4130KS) Closing of 4130KS)
the Aft Fan Cowl Doors (5110EA) and the Aft Fan Cowl Doors (5110EA) and the Thrust Reverser Cowl Doors (4120KS to the Thrust Reverser Cowl Doors (4120KS to
3. __________ Job Set-up Subtask 12-36-29-860-063 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Make sure that the Green hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-804). (3) Depressurize the reservoir of the Green hydraulic system (Ref. TASK 29-14-00-614-801). Subtask 12-36-29-941-063 B. Safety Precautions (1) Make sure that the engine 1(2), shutdown occurred not less than 5 minutes before you do this procedure. (2) On the panel 225VU, make sure that the APU BLEED pushbutton switch is released (ON legend off) and install a warning notice to tell persons not to use it. (3) Put a warning notice in position to tell persons not to pressurize the hydraulic system: - on the HYD/FUEL control panel 245VU in the cockpit, - on the Green hydraulic system, access door 197CB.
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(4) On the panel 125VU: - make sure that the ENG MASTER switches for the two engines are in the OFF position, - put a warning notice to tell persons not to supply power to the EEC. (5) On the panel 285VU: - make sure that the ON legend of the related ENG FADEC GND PWR pushbutton switch is off, - put a warning notice to tell persons not to supply power to the FADEC system. (6) Put a container below the Green hydraulic engine pump and below the case drain filter. Subtask 12-36-29-865-078 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU HYD PUMP G CTL 9JV U09 721VU HYD PUMP G ENG 1 14JG2 X11 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 721VU HYD PUMP G CTL 9JV U09 722VU FADEC B ENG 2 13KS2 K49 722VU HYD PUMP G ENG 2 14JG1 X45 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-36-29-010-077 D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Open the fan cowl doors FOR 4030EM1 Open the door 415BL (Ref. TASK 71-13-00-010-802). FOR 4030EM2 Open the door 425BL (Ref. TASK 71-13-00-010-802).
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Subtask 12-36-29-040-063 E. Make the thrust reverser unserviceable for maintenance (Ref. TASK 78-3000-040-804). Subtask 12-36-29-010-133 F. Get Access (1) Open the right thrust-reverser door: FOR 4030EM1 Open the door 417AL (Ref. TASK 78-30-00-010-801). FOR 4030EM2 Open the door 427AL (Ref. TASK 78-30-00-010-801). (2) Put the access platform in position. (3) Put a container under the applicable hose. Subtask 12-36-29-010-078 G. Get access to the avionics compartment. (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the door of the AC/DC emergency power-center 740VU. (4) Put the adjustable access platform in position. 4. Procedure _________ Subtask 12-36-29-860-087 A. Preparation before the flushing of the HP line (Ref. Fig. 305/TASK 12-36-29-991-035) CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE ON THE GROUND HYDRAULIC CART _______ IS SET TO A MINIMUM OF 7 BARS (101.53 PSI). (1) Disconnect the case drain line from the engine pump. (2) Disconnect the pressure line from the engine pump. (3) Disconnect the case drain line from the case drain filter.
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Hydraulic Connections Figure 305/TASK 12-36-29-991-035 R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 331 Jul 01/05
(4) Connect the pressure line and the case drain line together with the engine pump case drain/engine pump pressure connection (98F12303000104) of the HYDRAULIC CONNECTORS (98F12303000000). (5) Connect the pressure hose of the hydraulic power cart to the case drain line with the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000). (6) Connect the return hose of the hydraulic power cart to the interface (98F12303000106) of the HYDRAULIC CONNECTORS (98F12303000000). (7) Connect the free end of the interface to the delivery ground connector 5131JM1. (8) Put blanking plugs on the disconnected line ends. (9) Close the leak measurement valve. - on the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/GREEN pushbutton switch (the OFF legend comes on). Subtask 12-36-29-170-063 B. Flushing of the HP Line (Ref. Fig. 306/TASK 12-36-29-991-014) (1) Operate the hydraulic power cart for 2mn at 20 bars. (2) Stop the hydraulic power cart. (3) Open the leak measurement valve: - on the HYD section of the maintenance panel 285VU, push the LEAK MEASUREMENT VALVES/GREEN pushbutton switch (the OFF legend goes off). R R
(4) Replace the HP filters 5111JM101 and 5111JM102 (Ref. TASK 29-11-45600-801).
R
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Flushing of the HP Line of the Green Hydraulic System Figure 306/TASK 12-36-29-991-014 R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
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Subtask 12-36-29-420-063 C. Connection of the Hydraulic Line (1) Remove the blanking plugs from the disconnected line ends. (2) Remove the engine pump case drain/engine pump pressure connection (98F12303000104) of the HYDRAULIC CONNECTORS (98F12303000000) from the pressure line and from the case drain line. (3) Remove the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000) from the case drain line and from the hydraulic power cart. (4) Connect the pressure line to the engine pump. (5) TORQUE the pressure line to between 12.88 and 14.24 m.daN (94.98 and 105.01 lbf.ft). (6) Connect the case drain line to the engine pump. (7) TORQUE the case drain line to between 2.43 and 3.16 m.daN (17.92 and 23.30 lbf.ft). (8) Connect the pump case drain hose to the case drain. (9) TORQUE the case drain hose to between 5.31 and 6.21 m.daN (39.15 and 45.79 lbf.ft). Subtask 12-36-29-865-079 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 4030EM1 9JV, 14JG2, 12KS1, 13KS1 FOR 4030EM2 9JV, 9JV, 14JG1, 12KS2, 13KS2 Subtask 12-36-29-611-063 E. Fill the Green hydraulic reservoir (Ref. TASK 12-12-29-611-801) or (Ref. TASK 12-12-29-611-802). Subtask 12-36-29-863-063 F. Pressurize the Green hydraulic reservoir (Ref. TASK 29-14-00-614-804).
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Subtask 12-36-29-410-132 G. Close the right thrust reverser : - FOR 4030EM1 close the door 417AL (Ref. TASK 78-30-00-410-801) - FOR 4030EM2 close the door 427AL (Ref. TASK 78-30-00-410-801) Subtask 12-36-29-440-063 H. Make sure that the thrust reverser is serviceable after maintenance (Ref. TASK 78-30-00-440-804). Subtask 12-36-29-410-076 J. Close the fan cowl doors FOR 4030EM1 - close the door 415BL (Ref. TASK 71-13-00-410-802) FOR 4030EM2 - close the door 425BL (Ref. TASK 71-13-00-410-802). Subtask 12-36-29-281-063 K. Sampling (1) Perform a fluid sampling for particular contamination (Ref. TASK 1232-29-281-801). R R
(2) Perform in daily check of the clogging indicators of the HP filters 5111JM101 and 5111JM102. Do this operation again until the clogging indicator stay in. 5. Close-up ________ Subtask 12-36-29-410-077 A. Close Access (1) Close the door of the AC/DC emergency power-center 740VU. (2) Close the access door 811. (3) Remove the access platform(s). (4) Close the MLG doors (Ref. TASK 32-12-00-410-801).
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Subtask 12-36-29-942-063 B. Remove the safety devices (1) Remove the warning notice(s). Subtask 12-36-29-862-063 C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
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**ON A/C 701-749, TASK 12-36-29-170-802-A Flushing of the HP line of the Green Hydraulic System WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job To flush the Green Hydraulic System after a failure of the engine pump. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No
specific specific specific specific specific specific specific specific
No specific 98F12303000000
adjustable access platform blanking plugs circuit breaker(s) safety clip(s) hydraulic power cart warning notice access platform 2.5 m (8 ft. 2 in.) container 5 l (1.3208 USgal) Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft) Torque Wrench : range 2.00 to 20.00 m.daN (15.00 to 150.00 lbf.ft) 1 HYDRAULIC CONNECTORS
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B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-801 12-12-29-611-802 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-11-45-600-801 29-14-00-614-801 R 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 78-31-41-000-803 12-36-29-991-036 12-36-29-991-020 FOR FIN 4030EM1 71-13-00-010-805 71-13-00-410-805 FOR FIN 4030EM2 71-13-00-010-805 71-13-00-410-805
Fill the Green Hydraulic Reservoir with a Hydraulic Service Cart Fill the Green Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Servicing of the Green HP Filter (5111JM101,5111JM102) Depressurization of the Green Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Removal of the Isolation Control Unit (4117KS) Fig. 307 Fig. 308 Open the Fan Cowl Doors Close the Fan Cowl Doors Open the Fan Cowl Doors Close the Fan Cowl Doors
3. __________ Job Set-up Subtask 12-36-29-860-069 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Make sure that the Green hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-804).
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(3) Depressurize the reservoir of the Green hydraulic system (Ref. TASK 29-14-00-614-801). Subtask 12-36-29-941-069 B. Safety Precautions (1) Make sure that the engine 1(2), shutdown occurred not less than 5 minutes before you do this procedure. (2) On the panel 225VU, make sure that the APU BLEED pushbutton switch is released (ON legend off) and install a warning notice to tell persons not to use it. (3) Put a warning notice in position to tell persons not to pressurize the hydraulic system: - on the HYD/FUEL control panel 245VU in the cockpit, - on the Green hydraulic system, access door 197CB. (4) On the panel 125VU: - make sure that the ENG MASTER switches for the two engines are in the OFF position, - put a warning notice to tell persons not to supply power to the ECU. (5) On the panel 285VU: - make sure that the ON legend of the related ENG FADEC GND PWR pushbutton switch is off, - put a warning notice to tell persons not to supply power to the FADEC system. (6) Put a container below the Green hydraulic engine pump and below the case drain filter.
EFF : 701-749, 12-36-29 R SROS
Page 339 Apr 01/01
Subtask 12-36-29-865-091 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU HYD PUMP G CTL 9JV U09 722VU FADEC B ENG 1 13KS1 D44 742VU HYD PUMP G ENG 1 14JG2 E67 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 721VU HYD PUMP G CTL 9JV U09 722VU FADEC B ENG 2 13KS2 K49 722VU HYD PUMP G ENG 2 14JG1 X45 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-36-29-010-089 D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Open the fan cowl doors FOR 4030EM1 Open the door 416AR (Ref. TASK 71-13-00-010-805) FOR 4030EM2 Open the door 426AR (Ref. TASK 71-13-00-010-805). Subtask 12-36-29-010-098 E. Get access to the avionics compartment. (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the door of the AC/DC emergency power-center 740VU. (4) Put the adjustable access platform in position.
EFF : 701-749, 12-36-29 R SROS
Page 340 Apr 01/01
4. Procedure _________ Subtask 12-36-29-860-093 A. Preparation before the flushing of the HP line (Ref. Fig. 307/TASK 12-36-29-991-036) R R
CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE ON THE GROUND HYDRAULIC CART _______ IS SET TO A MINIMUM OF 7 BARS (101.53 PSI). (1) Disconnect the case drain line from the engine pump. (2) Disconnect the pressure line from the engine pump. (3) Disconnect the case drain line from the case drain filter. (4) Connect the pressure line and the case drain line together with the engine pump case drain/engine pump pressure connection (98F12303000104) of the HYDRAULIC CONNECTORS (98F12303000000). (5) Connect the pressure hose of the hydraulic power cart to the case drain line with the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000). (6) Connect the return hose of the hydraulic power cart to the interface (98F12303000106) of the HYDRAULIC CONNECTORS (98F12303000000). (7) Connect the free end of the interface to the delivery ground connector 5131JM1. (8) Put blanking plugs on the disconnected line ends. (9) Close the leak measurement valve. - on the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/GREEN pushbutton switch (the OFF legend comes on). Subtask 12-36-29-170-069 B. Flushing of the HP Line (Ref. Fig. 308/TASK 12-36-29-991-020) (1) Operate the hydraulic power cart for 2mn at 20 bars. (2) Stop the hydraulic power cart.
EFF : 701-749, 12-36-29 SROS
Page 341 Oct 01/04
Hydraulic Connections Figure 307/TASK 12-36-29-991-036 EFF : 701-749, 12-36-29 R SROS
Page 342 Apr 01/01
Flushing of the HP Line of the Green Hydraulic System Figure 308/TASK 12-36-29-991-020 EFF : 701-749, 12-36-29 R SROS
Page 343 Apr 01/01
(3) Open the leak measurement valve: - on the HYD section of the maintenance panel 285VU, push the LEAK MEASUREMENT VALVES/GREEN pushbutton switch (the OFF legend goes off). (4) Replace the hydraulic filters, HP and filter element: - replace the HP filters 5111JM101, 5111JM102 (Ref. TASK 29-11-45600-801), - replace the filter element located on the Isolation Control Unit 4117KS (Ref. TASK 78-31-41-000-803). Subtask 12-36-29-420-069 C. Connection of the Hydraulic Line (1) Remove the blanking plugs from the disconnected line ends. (2) Remove the engine pump case drain/engine pump pressure connection (98F12303000104) of the HYDRAULIC CONNECTORS (98F12303000000) from the pressure line and from the case drain line. (3) Remove the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000) from the case drain line and from the hydraulic power cart. (4) Connect the pressure line to the engine pump. (5) TORQUE the pressure line to between 12.88 and 14.24 m.daN (94.98 and 105.01 lbf.ft). (6) Connect the case drain line to the engine pump. (7) Connect the pump case drain hose to the case drain. (8) TORQUE the case drain line to between 2.43 and 3.16 m.daN (17.92 and 23.30 lbf.ft). Subtask 12-36-29-865-092 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 4030EM1 9JV, 14JG2, 12KS1, 13KS1 FOR 4030EM2 9JV, 14JG1, 12KS2, 13KS2
EFF : 701-749, 12-36-29 R SROS
Page 344 Apr 01/01
Subtask 12-36-29-611-069 E. Fill the Green hydraulic reservoir (Ref. TASK 12-12-29-611-801) or (Ref. TASK 12-12-29-611-802). Subtask 12-36-29-863-069 F. Pressurize the Green hydraulic reservoir (Ref. TASK 29-14-00-614-804). Subtask 12-36-29-410-088 G. Close the fan cowl doors FOR 4030EM1 - close the door 416AR (Ref. TASK 71-13-00-410-805) FOR 4030EM2 - close the door 426AR (Ref. TASK 71-13-00-410-805). Subtask 12-36-29-281-069 H. Sampling (1) Perform a fluid sampling for particular contamination (Ref. TASK 1232-29-281-801). (2) Perform in daily check, the check of the clogging indicators of the HP filters 5111JM101, 5111JM102 and the filter element located on the Isolation Control Unit 4117KS. Do this operation again until the clogging indicator stay in. 5. Close-up ________ Subtask 12-36-29-410-089 A. Close Access (1) Close the door of the AC/DC emergency power-center 740VU. (2) Close the access door 811. (3) Remove the access platform(s). (4) Close the MLG doors (Ref. TASK 32-12-00-410-801).
R EFF : 701-749, 12-36-29 SROS
Page 345 Apr 01/01
Subtask 12-36-29-942-069 B. Remove the safety devices (1) Remove the warning notice(s). Subtask 12-36-29-862-069 C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 701-749, 12-36-29 SROS
Page 346 Apr 01/01
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, TASK 12-36-29-170-803 Flushing of the Case-Drain line of the Blue Hydraulic System WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job To flush the Blue hydraulic system after a failure of the engine pump. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No No
specific specific specific specific specific specific specific specific specific
98F12303000000
adjustable access platform blanking plug circuit breaker(s) safety clip(s) hydraulic power cart strap warning notice access platform 2.5 m (8 ft. 2 in.) container 5 l (1.3208 USgal) Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft) 1 HYDRAULIC CONNECTORS
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 347 Jul 01/05
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-803 12-12-29-611-804 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-10-00-611-802 29-11-43-600-804 29-12-44-600-801 29-12-45-600-801 29-14-00-614-802 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 78-30-00-040-804 78-30-00-440-804 12-36-29-991-038 12-36-29-991-015 FOR FIN 4030EM1 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801 78-30-00-410-801
Fill the Blue Hydraulic Reservoir with a Hydraulic Service Cart Fill the Blue Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Drainage of the Blue Hydraulic Reservoir Servicing of the (Aft) Engine-Pump Case-Drain Filter Element 5013JM2 Servicing of the Blue Reservoir LP-Filter (5011JM2) Servicing of the Blue HP Filter (5111JM2) Depressurization of the Blue Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Deactivation of the Thrust Reverser for Maintenance Reactivation of the Thrust Reverser after Maintenance Fig. 309 Fig. 310 Opening of (5120EA) Closing of (5120EA) Opening of 4130KS) Closing of 4130KS)
the Aft Fan Cowl Doors (5110EA) and the Aft Fan Cowl Doors (5110EA) and the Thrust Reverser Cowl Doors (4120KS to the Thrust Reverser Cowl Doors (4120KS to
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 348 Jul 01/05
3. __________ Job Set-up Subtask 12-36-29-860-064 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Make sure that the Blue hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-804). (3) Depressurize the reservoir of the Blue hydraulic system (Ref. TASK 29-14-00-614-802). (4) Drain the Blue hydraulic reservoir (Ref. TASK 29-10-00-611-802). Subtask 12-36-29-941-064 B. Safety Precautions (1) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure. (2) On the panel 225VU, make sure that the APU BLEED pushbutton switch is released (ON legend off) and install a warning notice to tell persons not to use it. (3) Put a warning notice in position to tell persons not to pressurize the hydraulic system: - on the HYD/FUEL control panel 245VU in the cockpit, - on the Blue hydraulic system, access door 196BB. (4) On the panel 125VU: - make sure that the ENG MASTER switches for the two engines are in the OFF position, - put a warning notice to tell persons not to supply power to the EEC. (5) On the panel 285VU: - make sure that the ON legend of the related ENG FADEC GND PWR pushbutton switch is off, - put a warning notice to tell persons not to supply power to the FADEC system.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 349 Jul 01/05
(6) Put a container below the Blue hydraulic engine pump and below the case drain filter. Subtask 12-36-29-865-080 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU HYD PUMP B ENG 1 11JB U08 721VU HYD PUMP B CTL 9JC X12 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 Subtask 12-36-29-010-079 D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Open the fan cowl doors: FOR 4030EM1 Open the door 415BL (Ref. TASK 71-13-00-010-802) Subtask 12-36-29-040-064 E. Make the thrust reverser unserviceable for maintenance (Ref. TASK 78-3000-040-804). Subtask 12-36-29-010-134 F. Get Access (1) Open the right thrust-reverser door: FOR 4030EM1 Open the door 417AL (Ref. TASK 78-30-00-010-801). Subtask 12-36-29-010-080 G. Get access to the avionics compartment. (1) Put the access platform in position at the access door 811. (2) Open the access door 811.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 350 Jul 01/05
(3) Open the door of the AC/DC emergency power-center 740VU. (4) Put the adjustable access platform in position. 4. Procedure _________ Subtask 12-36-29-860-088 A. Preparation before the flushing of the Case-Drain line (Ref. Fig. 309/TASK 12-36-29-991-038) CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE ON THE GROUND HYDRAULIC CART _______ IS SET TO A MINIMUM OF 7 BARS (101.53 PSI). CAUTION : BE CAREFUL WHEN YOU DISCONNECT THE RETURN LINE FROM THE _______ RESERVOIR. THE HYDRAULIC FLUID IN THE LINE WILL FLOW OUT. (1) Disconnect and remove the return line from the reservoir and from the filter (5011JM2). (2) Put a blanking plug on the reservoir. (3) Connect the return hose of the hydraulic power cart to the filter (5011JM2) with the hydraulic power cart/return line interface (98F12303000100) of the HYDRAULIC CONNECTORS (98F12303000000). (4) Attach the return hose of the hydraulic power cart to the aicraft structure with a strap. (5) Disconnect the case drain line from the engine pump. (6) Put a blanking plug to the case drain. (7) Connect the pressure hose of the hydraulic power cart to the case drain line with the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000). Subtask 12-36-29-170-064 B. Flushing of the Case-Drain Line (Ref. Fig. 310/TASK 12-36-29-991-015) (1) Operate the hydraulic power cart for 2mn at 20 bars. (2) Stop the hydraulic power cart.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 351 Jul 01/05
Hydraulic connections Figure 309/TASK 12-36-29-991-038- 12 (SHEET 1) R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 352 Jul 01/05
Hydraulic connections Figure 309/TASK 12-36-29-991-038- 22 (SHEET 2) R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 353 Jul 01/05
Flushing of the Case-Drain Line of the Blue Hydraulic System Figure 310/TASK 12-36-29-991-015 R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 354 Jul 01/05
(3) Replace the hydraulic filters, case drain and LP: - the case drain filter 5013JM2 (Ref. TASK 29-11-43-600-804), - the LP filter 5011JM2 (Ref. TASK 29-12-44-600-801), - the HP filter 5111JM2 (Ref. TASK 29-12-45-600-801). Subtask 12-36-29-420-064 C. Connection of the Hydraulic Line (1) Remove the strap which attach the return hose of the hydraulic power cart to the structure. (2) Remove the blanking plug from the reservoir. (3) Remove the hydraulic power cart/return line interface (98F12303000100) of the HYDRAULIC CONNECTORS (98F12303000000) from the filter (5011JM2) and from the hydraulic power cart. (4) Connect the return line to the reservoir and to the filter (5011JM2). (5) Remove the blanking plug from the case drain. (6) Remove the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000) from the case drain line and from the hydraulic power cart. (7) Connect the case drain line to the engine pump. (8) TORQUE the case drain line to between 2.43 and 3.16 m.daN (17.92 and 23.30 lbf.ft). Subtask 12-36-29-865-081 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 4030EM1 9JC, 11JB, 12KS1, 13KS1 Subtask 12-36-29-611-064 E. Fill the Blue hydraulic reservoir (Ref. TASK 12-12-29-611-803) or (Ref. TASK 12-12-29-611-804). Subtask 12-36-29-863-064 F. Pressurize the Blue hydraulic reservoir (Ref. TASK 29-14-00-614-804).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 355 Jul 01/05
Subtask 12-36-29-410-133 G. Close the right thrust reverser : - FOR 4030EM1 close the door 417AL (Ref. TASK 78-30-00-410-801) Subtask 12-36-29-440-064 H. Make sure that the thrust reverser is serviceable after maintenance (Ref. TASK 78-30-00-440-804). Subtask 12-36-29-410-078 J. Close the fan cowl doors. FOR 4030EM1 - close the door 415BL (Ref. TASK 71-13-00-410-802). Subtask 12-36-29-281-064 K. Sampling (1) Perform a fluid sampling for particular contamination (Ref. TASK 1232-29-281-801). (2) Perform in daily check, the check of the clogging indicators, of the case drain filter 5013JM2, HP filter 5111JM2, LP filter 5011JM2. Do this operation again until the clogging indicator stay in. 5. Close-up ________ Subtask 12-36-29-410-079 A. Close Access (1) Close the door of the AC/DC emergency power-center 740VU. (2) Close the access door 811. (3) Remove the access platform(s). (4) Close the MLG doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-942-064 B. Remove the safety devices. (1) Remove the warning notice(s).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 356 Jul 01/05
Subtask 12-36-29-862-064 C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 357 Jul 01/05
**ON A/C 701-749, TASK 12-36-29-170-803-A Flushing of the Case-Drain line of the Blue Hydraulic System WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job To flush the Blue hydraulic system after a failure of the engine pump. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No No
specific specific specific specific specific specific specific specific specific
98F12303000000
adjustable access platform blanking plug circuit breaker(s) safety clip(s) hydraulic power cart strap warning notice access platform 2.5 m (8 ft. 2 in.) container 5 l (1.3208 USgal) Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft) 1 HYDRAULIC CONNECTORS
EFF : 701-749, 12-36-29 R SROS
Page 358 Apr 01/01
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-803 12-12-29-611-804 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-10-00-611-802 29-11-43-600-809 29-12-44-600-801 29-12-45-600-801 29-14-00-614-802 R 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 12-36-29-991-039 12-36-29-991-021 FOR FIN 4030EM1 71-13-00-010-805 71-13-00-410-805
Fill the Blue Hydraulic Reservoir with a Hydraulic Service Cart Fill the Blue Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Drainage of the Blue Hydraulic Reservoir Servicing of the Engine Pump Case Drain Filter (5013JM2) Servicing of the Blue Reservoir LP-Filter (5011JM2) Servicing of the Blue HP Filter (5111JM2) Depressurization of the Blue Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Fig. 311 Fig. 312 Open the Fan Cowl Doors Close the Fan Cowl Doors
3. __________ Job Set-up Subtask 12-36-29-860-070 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Make sure that the Blue hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-804).
EFF : 701-749, 12-36-29 SROS
Page 359 Apr 01/05
(3) Depressurize the reservoir of the Blue hydraulic system (Ref. TASK 29-14-00-614-802). (4) Drain the Blue hydraulic reservoir (Ref. TASK 29-10-00-611-802). Subtask 12-36-29-941-070 B. Safety Precautions (1) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure. (2) On the panel 225VU, make sure that the APU BLEED pushbutton switch is released (ON legend off) and install a warning notice to tell persons not to use it. (3) Put a warning notice in position to tell persons not to pressurize the hydraulic system: - on the HYD/FUEL control panel 245VU in the cockpit, - on the Blue hydraulic system, access door 196BB. (4) On the panel 125VU: - make sure that the ENG MASTER switches for the two engines are in the OFF position, - put a warning notice to tell persons not to supply power to the ECU. (5) On the panel 285VU: - make sure that the ON legend of the related ENG FADEC GND PWR pushbutton switch is off, - put a warning notice to tell persons not to supply power to the FADEC system. (6) Put a container below the Blue hydraulic engine pump and below the case drain filter.
EFF : 701-749, 12-36-29 R SROS
Page 360 Apr 01/01
Subtask 12-36-29-865-093 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU HYD PUMP B ENG 1 11JB U08 721VU HYD PUMP B CTL 9JC X12 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 Subtask 12-36-29-010-090 D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Open the fan cowl door FOR 4030EM1 Open the door 416AR (Ref. TASK 71-13-00-010-805) Subtask 12-36-29-010-091 E. Get access to the avionics compartment. (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the door of the AC/DC emergency power-center 740VU. (4) Put the adjustable access platform in position. 4. Procedure _________ Subtask 12-36-29-860-094 A. Preparation before the flushing of the Case-Drain line (Ref. Fig. 311/TASK 12-36-29-991-039) R R
CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE ON THE GROUND HYDRAULIC CART _______ IS SET TO A MINIMUM OF 7 BARS (101.53 PSI). CAUTION : BE CAREFUL WHEN YOU DISCONNECT THE RETURN LINE FROM THE _______ RESERVOIR. THE HYDRAULIC FLUID IN THE LINE WILL FLOW OUT.
EFF : 701-749, 12-36-29 SROS
Page 361 Oct 01/04
Hydraulic Connections Figure 311/TASK 12-36-29-991-039- 12 (SHEET 1) EFF : 701-749, 12-36-29 R SROS
Page 362 Apr 01/01
Hydraulic Connections Figure 311/TASK 12-36-29-991-039- 22 (SHEET 2) EFF : 701-749, 12-36-29 R SROS
Page 363 Apr 01/01
(1) Disconnect and remove the return line from the reservoir and from the filter (5011JM2). (2) Put a blanking plug on the reservoir. (3) Connect the return hose of the hydraulic power cart to the filter (5011JM2) with the hydraulic power cart/return line interface (98F12303000100) of the HYDRAULIC CONNECTORS (98F12303000000). (4) Attach the return hose of the hydraulic power cart to the aircraft structure with a strap. (5) Disconnect the case drain line from the engine pump. (6) Put a blanking plug to the case drain. (7) Connect the pressure hose of the hydraulic power cart to the case drain line with the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000). Subtask 12-36-29-170-070 B. Flushing of the Case-Drain Line (Ref. Fig. 312/TASK 12-36-29-991-021) (1) Operate the hydraulic power cart for 2mn at 20 bars. (2) Stop the hydraulic power cart. (3) Replace the hydraulic filters, case drain and LP: - the case drain filter 5013JM2 (Ref. TASK 29-11-43-600-809), - the LP filter 5011JM2 (Ref. TASK 29-12-44-600-801), - the HP filter 5111JM2 (Ref. TASK 29-12-45-600-801). Subtask 12-36-29-420-070 C. Connection of the Hydraulic Line (1) Remove the strap which attach the return hose of the hydraulic power cart to the aircraft structure. (2) Remove the blanking plug from the reservoir. (3) Remove the hydraulic power cart/return line interface (98F12303000100) of the HYDRAULIC CONNECTORS (98F12303000000) from the filter (5011JM2) and from the hydraulic power cart.
EFF : 701-749, 12-36-29 R SROS
Page 364 Apr 01/01
Flushing of the Case-Drain line of the Blue Hydraulic System Figure 312/TASK 12-36-29-991-021 EFF : 701-749, 12-36-29 R SROS
Page 365 Apr 01/01
(4) Connect the return line to the reservoir and to the filter (5011JM2). (5) Remove the blanking plug from the case drain. (6) Remove the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000) from the case drain line and from the hydraulic power cart. (7) Connect the case drain line to the engine pump. (8) TORQUE the case drain line to between 2.43 and 3.16 m.daN (17.92 and 23.30 lbf.ft). Subtask 12-36-29-865-094 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 4030EM1 9JC, 11JB, 12KS1, 13KS1 Subtask 12-36-29-611-070 E. Fill the Blue hydraulic reservoir (Ref. TASK 12-12-29-611-803) or (Ref. TASK 12-12-29-611-804). Subtask 12-36-29-863-070 F. Pressurize the Blue hydraulic reservoir (Ref. TASK 29-14-00-614-804). Subtask 12-36-29-410-090 G. Close the fan cowl doors. FOR 4030EM1 - close the door 416AR (Ref. TASK 71-13-00-410-805). Subtask 12-36-29-281-070 H. Sampling (1) Perform a fluid sampling for particular contamination (Ref. TASK 1232-29-281-801). (2) Perform in daily check, the check of the clogging indicators, of the case drain filter 5013JM2, HP filter 5111JM2, LP filter 5011JM2. Do this operation again until the clogging indicator stay in.
R EFF : 701-749, 12-36-29 SROS
Page 366 Apr 01/01
5. Close-up ________ Subtask 12-36-29-410-091 A. Close Access (1) Close the door of the AC/DC emergency power-center 740VU. (2) Close the access door 811. (3) Remove the access platform(s). (4) Close the MLG doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-942-070 B. Remove the safety devices. (1) Remove the warning notice(s). Subtask 12-36-29-862-070 C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 701-749, 12-36-29 SROS
Page 367 Apr 01/01
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, TASK 12-36-29-170-804 Flushing of the HP line of the Blue Hydraulic System WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job To flush the Blue hydraulic system after a failure of the engine pump. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No
specific specific specific specific specific specific specific specific
No specific
adjustable access platform blanking plugs circuit breaker(s) safety clip(s) hydraulic power cart warning notice access platform 2.5 m (8 ft. 2 in.) container 5 l (1.3208 USgal) Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft) Torque Wrench : range 1.00 to 10.00 m.daN (8.00 to 75.00 lbf.ft)
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 368 Jul 01/05
------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific 98F12303000000
Torque Wrench : range 2.00 to 20.00 m.daN (15.00 to 150.00 lbf.ft) 1 HYDRAULIC CONNECTORS
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-803 12-12-29-611-804 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-12-45-600-801 29-14-00-614-802 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 78-30-00-040-804 78-30-00-440-804 78-31-11-000-801 12-36-29-991-041 12-36-29-991-016 FOR FIN 4030EM1 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801 78-30-00-410-801
Fill the Blue Hydraulic Reservoir with a Hydraulic Service Cart Fill the Blue Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Servicing of the Blue HP Filter (5111JM2) Depressurization of the Blue Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Deactivation of the Thrust Reverser for Maintenance Reactivation of the Thrust Reverser after Maintenance Removal of the Hydraulic Filter Element Fig. 313 Fig. 314 Opening of (5120EA) Closing of (5120EA) Opening of 4130KS) Closing of 4130KS)
the Aft Fan Cowl Doors (5110EA) and the Aft Fan Cowl Doors (5110EA) and the Thrust Reverser Cowl Doors (4120KS to the Thrust Reverser Cowl Doors (4120KS to
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 369 Jul 01/05
3. __________ Job Set-up Subtask 12-36-29-860-065 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Make sure that the Blue hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-804). (3) Depressurize the reservoir of the Blue hydraulic system (Ref. TASK 29-14-00-614-802). Subtask 12-36-29-941-065 B. Safety Precautions (1) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure. (2) On the panel 225VU, make sure that the APU BLEED pushbutton switch is released (ON legend off) and install a warning notice to tell persons not to use it. (3) Put a warning notice in position to tell persons not to pressurize the hydraulic system: - on the HYD/FUEL control panel 245VU in the cockpit, - on the Blue hydraulic system, access door 196BB. (4) On the panel 125VU: - make sure that the ENG MASTER switches for the two engines are in the OFF position, - put a warning notice to tell persons not to supply power to the EEC. (5) On the panel 285VU: - make sure that the ON legend of the related ENG FADEC GND PWR pushbutton switch is off, - put a warning notice to tell persons not to supply power to the FADEC system. (6) Put a container below the Blue hydraulic engine pump and below the case drain filter.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 370 Jul 01/05
Subtask 12-36-29-865-082 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU HYD PUMP B ENG 1 11JB U08 721VU HYD PUMP B CTL 9JC X12 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 Subtask 12-36-29-010-081 D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Open the fan cowl doors: FOR 4030EM1 Open the door 415BL (Ref. TASK 71-13-00-010-802) Subtask 12-36-29-040-065 E. Make the thrust reverser unserviceable for maintenance (Ref. TASK 78-3000-040-804). Subtask 12-36-29-010-135 F. Get Access (1) Open the right thrust-reverser door: FOR 4030EM1 Open the door 417AL (Ref. TASK 78-30-00-010-801). Subtask 12-36-29-010-082 G. Get access to the avionics compartment. (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the door of the AC/DC emergency power-center 740VU. (4) Put the adjustable access platform in position.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 371 Jul 01/05
4. Procedure _________ Subtask 12-36-29-860-089 A. Preparation before the flushing of the HP line (Ref. Fig. 313/TASK 12-36-29-991-041) CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE ON THE GROUND HYDRAULIC CART _______ IS SET TO A MINIMUM OF 7 BARS (101.53 PSI). (1) Disconnect the case drain line from the engine pump. (2) Disconnect the pressure line from the engine pump. (3) Disconnect the case drain line from the case drain filter. (4) Connect the pressure line and the case drain line together with the engine pump case drain/engine pump pressure connection (98F12303000104) of the HYDRAULIC CONNECTORS (98F12303000000). (5) Connect the pressure hose of the hydraulic power cart to the case drain line with the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000). (6) Connect the return hose of the hydraulic power cart to the interface (98F12303000106) of the HYDRAULIC CONNECTORS (98F12303000000). (7) Connect the free end of the interface to the delivery ground connector 5131JM2. (8) Put blanking plugs on the disconnected line ends. (9) Close the leak measurement valve. - on the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/BLUE pushbutton switch (the OFF legend comes on). Subtask 12-36-29-170-065 B. Flushing of the HP Line (Ref. Fig. 314/TASK 12-36-29-991-016) (1) Operate the hydraulic power cart for 2mn at 20 bars. (2) Stop the hydraulic power cart.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 372 Jul 01/05
Hydraulic Connections Figure 313/TASK 12-36-29-991-041 R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 373 Jul 01/05
Flushing of the HP Line of the Blue Hydraulic System Figure 314/TASK 12-36-29-991-016 R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 374 Jul 01/05
(3) Open the leak measurement valve: - on the HYD section of the maintenance panel 285VU, push the LEAK MEASUREMENT VALVES/BLUE pushbutton switch (the OFF legend goes off). (4) Replace the hydraulic filters, HP and HCU: - replace the HP filter 5111JM2 (Ref. TASK 29-12-45-600-801), - replace the HCU filter 5000EG2 (Ref. TASK 78-31-11-000-801). Subtask 12-36-29-420-065 C. Connection of the Hydraulic Line (1) Remove the blanking plugs from the disconnected line ends. (2) Remove the engine pump case drain/engine pump pressure connection (98F12303000104) of the HYDRAULIC CONNECTORS (98F12303000000) from the pressure line and from the case drain line. (3) Remove the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000) from the case drain line and from the hydraulic power cart. (4) Connect the pressure line to the engine pump. (5) TORQUE the pressure line to between 12.88 and 14.24 m.daN (94.98 and 105.01 lbf.ft). (6) Connect the case drain line to the engine pump. (7) TORQUE the case drain line to between 2.43 and 3.16 m.daN (17.92 and 23.30 lbf.ft). (8) Connect the pump case drain hose to the case drain. (9) TORQUE the case drain hose to between 5.31 and 6.21 m.daN (39.15 and 45.79 lbf.ft). Subtask 12-36-29-865-083 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 4030EM1 9JC, 11JB, 12KS1, 13KS1
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 375 Jul 01/05
Subtask 12-36-29-611-065 E. Fill the Blue hydraulic reservoir (Ref. TASK 12-12-29-611-803) or (Ref. TASK 12-12-29-611-804). Subtask 12-36-29-863-065 F. Pressurize the Blue hydraulic reservoir (Ref. TASK 29-14-00-614-804). Subtask 12-36-29-410-134 G. Close the right thrust reverser : - FOR 4030EM1 close the door 417AL (Ref. TASK 78-30-00-410-801) Subtask 12-36-29-440-065 H. Make sure that the thrust reverser is serviceable after maintenance (Ref. TASK 78-30-00-440-804). Subtask 12-36-29-410-080 J. Close the fan cowl doors. FOR 4030EM1 - close the door 415BL (Ref. TASK 71-13-00-410-802) Subtask 12-36-29-281-065 K. Sampling (1) Perform a fluid sampling for particular contamination (Ref. TASK 1232-29-281-801). (2) Perform in daily check, the check of the clogging indicators of the HP filter 5111JM2 and the HCU filter 5000EG2. Do this operation again until the clogging indicator stay in. 5. Close-up ________ Subtask 12-36-29-410-081 A. Close Access (1) Close the door of the AC/DC emergency power-center 740VU. (2) Close the access door 811.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 376 Jul 01/05
(3) Remove the access platform(s). (4) Close the MLG doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-942-065 B. Remove the safety devices. (1) Remove the warning notice(s). Subtask 12-36-29-862-065 C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 377 Jul 01/05
**ON A/C 701-749, TASK 12-36-29-170-804-A Flushing of the HP line of the Blue Hydraulic System WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job To flush the Blue hydraulic system after a failure of the engine pump. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No
specific specific specific specific specific specific specific specific
No specific 98F12303000000
adjustable access platform blanking plugs circuit breaker(s) safety clip(s) hydraulic power cart warning notice access platform 2.5 m (8 ft. 2 in.) container 5 l (1.3208 USgal) Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft) Torque Wrench : range 2.00 to 20.00 m.daN (15.00 to 150.00 lbf.ft) 1 HYDRAULIC CONNECTORS
EFF : 701-749, 12-36-29 R SROS
Page 378 Apr 01/01
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-803 12-12-29-611-804 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-12-45-600-801 29-14-00-614-802 R 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 78-31-41-000-803 12-36-29-991-042 12-36-29-991-022 FOR FIN 4030EM1 71-13-00-010-805 71-13-00-410-805
Fill the Blue Hydraulic Reservoir with a Hydraulic Service Cart Fill the Blue Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Servicing of the Blue HP Filter (5111JM2) Depressurization of the Blue Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Removal of the Isolation Control Unit (4117KS) Fig. 315 Fig. 316 Open the Fan Cowl Doors Close the Fan Cowl Doors
3. __________ Job Set-up Subtask 12-36-29-860-071 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Make sure that the Blue hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-804). (3) Depressurize the reservoir of the Blue hydraulic system (Ref. TASK 29-14-00-614-802).
EFF : 701-749, 12-36-29 SROS
Page 379 Apr 01/05
Subtask 12-36-29-941-071 B. Safety Precautions (1) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure. (2) On the panel 225VU, make sure that the APU BLEED pushbutton switch is released (ON legend off) and install a warning notice to tell persons not to use it. (3) Put a warning notice in position to tell persons not to pressurize the hydraulic system: - on the HYD/FUEL control panel 245VU in the cockpit, - on the Blue hydraulic system, access door 196BB. (4) On the panel 125VU: - make sure that the ENG MASTER switches for the two engines are in the OFF position, - put a warning notice to tell persons not to supply power to the ECU. (5) On the panel 285VU: - make sure that the ON legend of the related ENG FADEC GND PWR pushbutton switch is off, - put a warning notice to tell persons not to supply power to the FADEC system. (6) Put a container below the Blue hydraulic engine pump and below the case drain filter. Subtask 12-36-29-865-095 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU HYD PUMP B ENG 1 11JB U08 721VU HYD PUMP B CTL 9JC X12 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73
EFF : 701-749, 12-36-29 R SROS
Page 380 Apr 01/01
Subtask 12-36-29-010-092 D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Open the fan cowl doors: FOR 4030EM1 Open the door 416AR (Ref. TASK 71-13-00-010-805) Subtask 12-36-29-010-093 E. Get access to the avionics compartment. (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the door of the AC/DC emergency power-center 740VU. (4) Put the adjustable access platform in position. 4. Procedure _________ Subtask 12-36-29-860-095 A. Preparation before the flushing of the HP line (Ref. Fig. 315/TASK 12-36-29-991-042) R R
CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE ON THE GROUND HYDRAULIC CART _______ IS SET TO A MINIMUM OF 7 BARS (101.53 PSI). (1) Disconnect the case drain line from the engine pump. (2) Disconnect the pressure line from the engine pump. (3) Disconnect the case drain line from the case drain filter. (4) Connect the pressure line and the case drain line together with the engine pump case drain/engine pump pressure connection (98F12303000104) of the HYDRAULIC CONNECTORS (98F12303000000). (5) Connect the pressure hose of the hydraulic power cart to the case drain line with the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000).
EFF : 701-749, 12-36-29 SROS
Page 381 Oct 01/04
Hydraulic Connections Figure 315/TASK 12-36-29-991-042 EFF : 701-749, 12-36-29 R SROS
Page 382 Apr 01/01
(6) Connect the return hose of the hydraulic power cart to the interface (98F12303000106) of the HYDRAULIC CONNECTORS (98F12303000000). (7) Connect the free end of the interface to the delivery ground connector 5131JM2. (8) Put blanking plugs on the disconnected line ends. (9) Close the leak measurement valve. - on the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/BLUE pushbutton switch (the OFF legend comes on). Subtask 12-36-29-170-071 B. Flushing of the HP Line (Ref. Fig. 316/TASK 12-36-29-991-022) (1) Operate the hydraulic power cart for 2mn at 20 bars. (2) Stop the hydraulic power cart. (3) Open the leak measurement valve: - on the HYD section of the maintenance panel 285VU, push the LEAK MEASUREMENT VALVES/BLUE pushbutton switch (the OFF legend goes off). (4) Replace the hydraulic filters, HP and filter element: - replace the HP filter 5111JM2 (Ref. TASK 29-12-45-600-801), - remove the filter element located on the Isolation Control Unit 4117KS (Ref. TASK 78-31-41-000-803). Subtask 12-36-29-420-071 C. Connection of the Hydraulic Line (1) Remove the blanking plugs from the disconnected line ends. (2) Remove the engine pump case drain/engine pump pressure connection (98F12303000104) of the HYDRAULIC CONNECTORS (98F12303000000) from the pressure line and from the case drain line. (3) Remove the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000) from the case drain line and from the hydraulic power cart. (4) Connect the pressure line to the engine pump.
EFF : 701-749, 12-36-29 R SROS
Page 383 Apr 01/01
Flushing of the HP Line of the Blue Hydraulic System Figure 316/TASK 12-36-29-991-022 EFF : 701-749, 12-36-29 R SROS
Page 384 Apr 01/01
(5) TORQUE the pressure line to between 12.88 and 14.24 m.daN (94.98 and 105.01 lbf.ft). (6) Connect the case drain line to the engine pump. (7) Connect the pump case drain hose to the case drain. (8) TORQUE the case drain line to between 2.43 and 3.16 m.daN (17.92 and 23.30 lbf.ft). Subtask 12-36-29-865-096 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 4030EM1 9JC, 11JB, 12KS1, 13KS1 Subtask 12-36-29-611-071 E. Fill the Blue hydraulic reservoir (Ref. TASK 12-12-29-611-803) or (Ref. TASK 12-12-29-611-804). Subtask 12-36-29-863-071 F. Pressurize the Blue hydraulic reservoir (Ref. TASK 29-14-00-614-804). Subtask 12-36-29-410-092 G. Close the fan cowl doors. FOR 4030EM1 - close the door 416AR (Ref. TASK 71-13-00-410-805) Subtask 12-36-29-281-071 H. Sampling (1) Perform a fluid sampling for particular contamination (Ref. TASK 1232-29-281-801). (2) Perform in daily check, the check of the clogging indicators of the HP filter 5111JM2 and the filter element located on the Isolation Control Unit 4117KS. Do this operation again until the clogging indicator stay in.
R EFF : 701-749, 12-36-29 SROS
Page 385 Apr 01/01
5. Close-up ________ Subtask 12-36-29-410-093 A. Close Access (1) Close the door of the AC/DC emergency power-center 740VU. (2) Close the access door 811. (3) Remove the access platform(s). (4) Close the MLG doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-942-071 B. Remove the safety devices. (1) Remove the warning notice(s). Subtask 12-36-29-862-071 C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 701-749, 12-36-29 SROS
Page 386 Apr 01/01
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, TASK 12-36-29-170-805 Flushing of the Case-Drain line of the Yellow Hydraulic System WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job To flush the Yellow hydraulic system after a failure of the engine pump. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No No
specific specific specific specific specific specific specific specific specific
98F12303000000
adjustable access platform blanking plug circuit breaker(s) safety clip(s) hydraulic power cart strap warning notice access platform 2.5 m (8 ft. 2 in.) container 5 l (1.3208 USgal) Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft) 1 HYDRAULIC CONNECTORS
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 387 Jul 01/05
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-805 12-12-29-611-806 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-10-00-611-803 29-11-43-600-804 29-13-44-600-801 29-14-00-614-803 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 78-30-00-040-804 78-30-00-440-804 12-36-29-991-044 12-36-29-991-017 FOR FIN 4030EM2 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801 78-30-00-410-801
Fill the Yellow Hydraulic Reservoir with a Hydraulic Service Cart Fill the Yellow Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Drainage of the Yellow Hydraulic Reservoir Servicing of the (Aft) Engine-Pump Case-Drain Filter Element 5013JM2 Servicing of the Yellow Reservoir LP-Filter (5011JM3) Depressurization of the Yellow Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Deactivation of the Thrust Reverser for Maintenance Reactivation of the Thrust Reverser after Maintenance Fig. 317 Fig. 318 Opening of (5120EA) Closing of (5120EA) Opening of 4130KS) Closing of 4130KS)
the Aft Fan Cowl Doors (5110EA) and the Aft Fan Cowl Doors (5110EA) and the Thrust Reverser Cowl Doors (4120KS to the Thrust Reverser Cowl Doors (4120KS to
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 388 Jul 01/05
3. __________ Job Set-up Subtask 12-36-29-860-066 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Make sure that the Yellow hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-804). (3) Depressurize the reservoir of the Yellow hydraulic system (Ref. TASK 29-14-00-614-803). (4) Drain the Yellow hydraulic reservoir (Ref. TASK 29-10-00-611-803). Subtask 12-36-29-941-066 B. Safety Precautions (1) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure. (2) On the panel 225VU, make sure that the APU BLEED pushbutton switch is released (ON legend off) and install a warning notice to tell persons not to use it. (3) Put a warning notice in position to tell persons not to pressurize the hydraulic system: - on the HYD/FUEL control panel 245VU in the cockpit, - on the Yellow hydraulic system, access door 196BB. (4) On the panel 125VU: - make sure that the ENG MASTER switches for the two engines are in the OFF position, - put a warning notice to tell persons not to supply power to the EEC. (5) On the panel 285VU: - make sure that the ON legend of the related ENG FADEC GND PWR pushbutton switch is off, - put a warning notice to tell persons not to supply power to the FADEC system.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 389 Jul 01/05
(6) Put a container below the Yellow hydraulic engine pump and below the case drain filter. Subtask 12-36-29-865-084 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 722VU HYD PUMP Y CTL 9JJ R36 722VU HYD PUMP Y ENG 2 12JY T46 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-36-29-010-083 D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Open the fan cowl doors: FOR 4030EM2 Open the door 425BL (Ref. TASK 71-13-00-010-802) Subtask 12-36-29-040-066 E. Make the thrust reverser unserviceable for maintenance (Ref. TASK 78-3000-040-804). Subtask 12-36-29-010-136 F. Get Access (1) Open the right thrust-reverser door: FOR 4030EM2 Open the door 427AL (Ref. TASK 78-30-00-010-801). Subtask 12-36-29-010-084 G. Get access to the avionics compartment. (1) Put the access platform in position at the access door 811. (2) Open the access door 811.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 390 Jul 01/05
(3) Open the door of the AC/DC emergency power-center 740VU. (4) Put the adjustable access platform in position. 4. Procedure _________ Subtask 12-36-29-860-090 A. Preparation before the flushing of the Case-Drain line (Ref. Fig. 317/TASK 12-36-29-991-044) CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE ON THE GROUND HYDRAULIC CART _______ IS SET TO A MINIMUM OF 7 BARS (101.53 PSI). CAUTION : BE CAREFUL WHEN YOU DISCONNECT THE RETURN LINE FROM THE _______ RESERVOIR. THE HYDRAULIC FLUID IN THE LINE WILL FLOW OUT. (1) Disconnect and remove the return line from the reservoir and from the filter (5011JM3). (2) Put a blanking plug on the reservoir. (3) Connect the return hose of the hydraulic power cart to the filter (5011JM3) with the hydraulic power cart/return line interface (98F12303000100) of the HYDRAULIC CONNECTORS (98F12303000000). (4) Attach the return hose of the hydraulic power cart to the aircraft structure with a strap. (5) Disconnect the case drain line from the engine pump. (6) Put a blanking plug to the case drain. (7) Connect the pressure hose of the hydraulic power cart to the case drain line with the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000). Subtask 12-36-29-170-066 B. Flushing of the Case-Drain Line (Ref. Fig. 318/TASK 12-36-29-991-017) (1) Operate the hydraulic power cart for 2mn at 20 bars. (2) Stop the hydraulic power cart.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 391 Jul 01/05
Hydraulic Connections Figure 317/TASK 12-36-29-991-044- 12 (SHEET 1) R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 392 Jul 01/05
Hydraulic Connections Figure 317/TASK 12-36-29-991-044- 22 (SHEET 2) R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 393 Jul 01/05
Flushing of the Case-Drain Line of the Yellow Hydraulic System Figure 318/TASK 12-36-29-991-017 R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 394 Jul 01/05
(3) Replace the hydraulic filters, case drain and LP: - the case drain filter 5013JM2 (Ref. TASK 29-11-43-600-804), - the LP filter 5011JM3 (Ref. TASK 29-13-44-600-801). Subtask 12-36-29-420-066 C. Connection of the Hydraulic Line (1) Remove the strap which attach the return hose of the hydraulic power cart to the aircraft structure. (2) Remove the blanking plug from the reservoir. (3) Remove the hydraulic power cart/return line interface (98F12303000100) of the HYDRAULIC CONNECTORS (98F12303000000) from the filter (5011JM3) and from the hydraulic power cart. (4) Connect the return line to the reservoir and to the filter (5011JM3). (5) Remove the blanking plug from the case drain. (6) Remove the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000) from the case drain line and from the hydraulic power cart. (7) Connect the case drain line to the engine pump. (8) TORQUE the case drain line to between 2.43 and 3.16 m.daN (17.92 and 23.30 lbf.ft). Subtask 12-36-29-865-085 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 4030EM2 9JJ, 12JY, 12KS2, 13KS2 Subtask 12-36-29-611-066 E. Fill the Yellow hydraulic reservoir (Ref. TASK 12-12-29-611-805) or (Ref. TASK 12-12-29-611-806). Subtask 12-36-29-863-066 F. Pressurize the Yellow hydraulic reservoir (Ref. TASK 29-14-00-614-804).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 395 Jul 01/05
Subtask 12-36-29-410-135 G. Close the right thrust reverser : - FOR 4030EM2 close the door 427AL (Ref. TASK 78-30-00-410-801) Subtask 12-36-29-440-066 H. Make sure that the thrust reverser is serviceable after maintenance (Ref. TASK 78-30-00-440-804). Subtask 12-36-29-410-082 J. Close the fan cowl doors. FOR 4030EM2 - close the door 425BL (Ref. TASK 71-13-00-410-802). Subtask 12-36-29-281-066 K. Sampling (1) Perform a fluid sampling for particular contamination (Ref. TASK 1232-29-281-801). (2) Perform in daily check, the check of the clogging indicators, of the case drain filter 5013JM2, HP filter 5111JM3, LP filter 5011JM3. Do this operation again until the clogging indicator stay in. 5. Close-up ________ Subtask 12-36-29-410-083 A. Close Access (1) Close the door of the AC/DC emergency power-center 740VU. (2) Close the access door 811. (3) Remove the access platform(s). (4) Close the MLG doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-942-066 B. Remove the safety devices. (1) Remove the warning notice(s).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 396 Jul 01/05
Subtask 12-36-29-862-066 C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page 397 Jul 01/05
**ON A/C 701-749, TASK 12-36-29-170-805-A Flushing of the Case-Drain line of the Yellow Hydraulic System WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job To flush the Yellow hydraulic system after a failure of the engine pump. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No No
specific specific specific specific specific specific specific specific specific
98F12303000000
adjustable access platform blanking plug circuit breaker(s) safety clip(s) hydraulic power cart strap warning notice access platform 2.5 m (8 ft. 2 in.) container 5 l (1.3208 USgal) Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft) 1 HYDRAULIC CONNECTORS
EFF : 701-749, 12-36-29 R SROS
Page 398 Apr 01/01
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-805 12-12-29-611-806 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-10-00-611-803 29-11-43-600-809 29-13-44-600-801 29-14-00-614-803 R 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 12-36-29-991-045 12-36-29-991-023 FOR FIN 4030EM2 71-13-00-010-805 71-13-00-410-805
Fill the Yellow Hydraulic Reservoir with a Hydraulic Service Cart Fill the Yellow Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Drainage of the Yellow Hydraulic Reservoir Servicing of the Engine Pump Case Drain Filter (5013JM2) Servicing of the Yellow Reservoir LP-Filter (5011JM3) Depressurization of the Yellow Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Fig. 319 Fig. 320 Open the Fan Cowl Doors Close the Fan Cowl Doors
3. __________ Job Set-up Subtask 12-36-29-860-072 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Make sure that the Yellow hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-804). (3) Depressurize the reservoir of the Yellow hydraulic system (Ref. TASK 29-14-00-614-803).
EFF : 701-749, 12-36-29 SROS
Page 399 Apr 01/05
(4) Drain the Yellow hydraulic reservoir (Ref. TASK 29-10-00-611-803). Subtask 12-36-29-941-072 B. Safety Precautions (1) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure. (2) On the panel 225VU, make sure that the APU BLEED pushbutton switch is released (ON legend off) and install a warning notice to tell persons not to use it. (3) Put a warning notice in position to tell persons not to pressurize the hydraulic system: - on the HYD/FUEL control panel 245VU in the cockpit, - on the Yellow hydraulic system, access door 196BB. (4) On the panel 125VU: - make sure that the ENG MASTER switches for the two engines are in the OFF position, - put a warning notice to tell persons not to supply power to the ECU. (5) On the panel 285VU: - make sure that the ON legend of the related ENG FADEC GND PWR pushbutton switch is off, - put a warning notice to tell persons not to supply power to the FADEC system. (6) Put a container below the Yellow hydraulic engine pump and below the case drain filter. Subtask 12-36-29-865-097 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 722VU HYD PUMP Y CTL 9JJ R36 722VU HYD PUMP Y ENG 2 12JY T46 742VU FADEC A ENG 2 12KS2 Q74
EFF : 701-749, 12-36-29 R SROS
Page A300 Apr 01/01
Subtask 12-36-29-010-094 D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Open the fan cowl doors: FOR 4030EM2 Open the door 426AR (Ref. TASK 71-13-00-010-805) Subtask 12-36-29-010-095 E. Get access to the avionics compartment. (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the door of the AC/DC emergency power-center 740VU. (4) Put the adjustable access platform in position. 4. Procedure _________ Subtask 12-36-29-860-096 A. Preparation before the flushing of the Case-Drain line (Ref. Fig. 319/TASK 12-36-29-991-045) R R
CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE ON THE GROUND HYDRAULIC CART _______ IS SET TO A MINIMUM OF 7 BARS (101.53 PSI). CAUTION : BE CAREFUL WHEN YOU DISCONNECT THE RETURN LINE FROM THE _______ RESERVOIR. THE HYDRAULIC FLUID IN THE LINE WILL FLOW OUT. (1) Disconnect and remove the return line from the reservoir and from the filter (5011JM3). (2) Put a blanking plug on the reservoir. (3) Connect the return hose of the hydraulic power cart to the filter (5011JM3) with the hydraulic power cart/return line interface (98F12303000100) of the HYDRAULIC CONNECTORS (98F12303000000). (4) Attach the return hose of the hydraulic power cart to the aircraft structure with a strap.
EFF : 701-749, 12-36-29 SROS
Page A301 Oct 01/04
Hydraulic Connections Figure 319/TASK 12-36-29-991-045- 12 (SHEET 1) EFF : 701-749, 12-36-29 R SROS
Page A302 Apr 01/01
Hydraulic Connections Figure 319/TASK 12-36-29-991-045- 22 (SHEET 2) EFF : 701-749, 12-36-29 R SROS
Page A303 Apr 01/01
(5) Disconnect the case drain line from the engine pump. (6) Put a blanking plug to the case drain. (7) Connect the pressure hose of the hydraulic power cart to the case drain line with the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000). Subtask 12-36-29-170-072 B. Flushing of the Case-Drain Line (Ref. Fig. 320/TASK 12-36-29-991-023) (1) Operate the hydraulic power cart for 2mn at 20 bars. (2) Stop the hydraulic power cart. (3) Replace the hydraulic filters, case drain and LP: - the case drain filter 5013JM2 (Ref. TASK 29-11-43-600-809), - the LP filter 5011JM3 (Ref. TASK 29-13-44-600-801). Subtask 12-36-29-420-072 C. Connection of the Hydraulic Line (1) Remove the strap which attach the return hose of the hydraulic power cart to the aircraft structure. (2) Remove the blanking plug from the reservoir. (3) Remove the hydraulic power cart/return line interface (98F12303000100) of the HYDRAULIC CONNECTORS (98F12303000000) from the filter (5011JM3) and from the hydraulic power cart. (4) Connect the return line to the reservoir and to the filter (5011JM3). (5) Remove the blanking plug from the case drain. (6) Remove the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000) from the case drain line and from the hydraulic power cart. (7) Connect the case drain line to the engine pump. (8) TORQUE the case drain line to between 2.43 and 3.16 m.daN (17.92 and 23.30 lbf.ft).
EFF : 701-749, 12-36-29 R SROS
Page A304 Apr 01/01
Flushing of the Case-Drain line of the Yellow Hydraulic System Figure 320/TASK 12-36-29-991-023 EFF : 701-749, 12-36-29 R SROS
Page A305 Apr 01/01
Subtask 12-36-29-865-098 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 4030EM2 9JJ, 12JY, 12KS2, 13KS2 Subtask 12-36-29-611-072 E. Fill the Yellow hydraulic reservoir (Ref. TASK 12-12-29-611-805) or (Ref. TASK 12-12-29-611-806). Subtask 12-36-29-863-072 F. Pressurize the Yellow hydraulic reservoir (Ref. TASK 29-14-00-614-804). Subtask 12-36-29-410-094 G. Close the fan cowl doors. FOR 4030EM2 - close the door 426AR (Ref. TASK 71-13-00-410-805). Subtask 12-36-29-281-072 H. Sampling (1) Perform a fluid sampling for particular contamination (Ref. TASK 1232-29-281-801). (2) Perform in daily check, the check of the clogging indicators, of the case drain filter 5013JM2, HP filter 5111JM3, LP filter 5011JM3. Do this operation again until the clogging indicator stay in. 5. Close-up ________ Subtask 12-36-29-410-095 A. Close Access (1) Close the door of the AC/DC emergency power-center 740VU. (2) Close the access door 811. (3) Remove the access platform(s). (4) Close the MLG doors (Ref. TASK 32-12-00-410-801).
R EFF : 701-749, 12-36-29 SROS
Page A306 Apr 01/01
Subtask 12-36-29-942-072 B. Remove the safety devices. (1) Remove the warning notice(s). Subtask 12-36-29-862-072 C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 701-749, 12-36-29 SROS
Page A307 Apr 01/01
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, TASK 12-36-29-170-806 Flushing of the HP line of the Yellow Hydraulic System WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job To flush the Yellow hydraulic system after a failure of the engine pump. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No
specific specific specific specific specific specific specific specific
No specific
adjustable access platform blanking plugs circuit breaker(s) safety clip(s) hydraulic power cart warning notice access platform 2.5 m (8 ft. 2 in.) container 5 l (1.3208 USgal) Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft) Torque Wrench : range 1.00 to 10.00 m.daN (8.00 to 75.00 lbf.ft)
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A308 Jul 01/05
------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific 98F12303000000
Torque Wrench : range 2.00 to 20.00 m.daN (15.00 to 150.00 lbf.ft) 1 HYDRAULIC CONNECTORS
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-805 12-12-29-611-806 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-13-45-600-801 29-14-00-614-803 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 78-30-00-040-804 78-30-00-440-804 78-31-11-000-801 12-36-29-991-047 12-36-29-991-018 FOR FIN 4030EM2 71-13-00-010-802 71-13-00-410-802 78-30-00-010-801 78-30-00-410-801
Fill the Yellow Hydraulic Reservoir with a Hydraulic Service Cart Fill the Yellow Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Servicing of the Yellow HP Filter (5111JM3) Depressurization of the Yellow Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Deactivation of the Thrust Reverser for Maintenance Reactivation of the Thrust Reverser after Maintenance Removal of the Hydraulic Filter Element Fig. 321 Fig. 322 Opening of (5120EA) Closing of (5120EA) Opening of 4130KS) Closing of 4130KS)
the Aft Fan Cowl Doors (5110EA) and the Aft Fan Cowl Doors (5110EA) and the Thrust Reverser Cowl Doors (4120KS to the Thrust Reverser Cowl Doors (4120KS to
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A309 Jul 01/05
3. __________ Job Set-up Subtask 12-36-29-860-067 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Make sure that the Yellow hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-804). (3) Depressurize the reservoir of the Yellow hydraulic system (Ref. TASK 29-14-00-614-803). Subtask 12-36-29-941-067 B. Safety Precautions (1) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure. (2) On the panel 225VU, make sure that the APU BLEED pushbutton switch is released (ON legend off) and install a warning notice to tell persons not to use it. (3) Put a warning notice in position to tell persons not to pressurize the hydraulic system: - on the HYD/FUEL control panel 245VU in the cockpit, - on the Yellow hydraulic system, access door 197BB. (4) On the panel 125VU: - make sure that the ENG MASTER switches for the two engines are in the OFF position, - put a warning notice to tell persons not to supply power to the EEC. (5) On the panel 285VU: - make sure that the ON legend of the related ENG FADEC GND PWR pushbutton switch is off, - put a warning notice to tell persons not to supply power to the FADEC system. (6) Put a container below the Yellow hydraulic engine pump and below the case drain filter.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A310 Jul 01/05
Subtask 12-36-29-865-086 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 722VU HYD PUMP Y CTL 9JJ R36 722VU HYD PUMP Y ENG 2 12JY T46 742VU FADEC A ENG 2 12KS2 Q74 Subtask 12-36-29-010-085 D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Open the fan cowl doors: FOR 4030EM2 Open the door 425BL (Ref. TASK 71-13-00-010-802) Subtask 12-36-29-040-067 E. Make the thrust reverser unserviceable for maintenance (Ref. TASK 78-3000-040-804). Subtask 12-36-29-010-137 F. Get Access (1) Open the right thrust-reverser door: FOR 4030EM2 Open the door 427AL (Ref. TASK 78-30-00-010-801). Subtask 12-36-29-010-086 G. Get access to the avionics compartment. (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the door of the AC/DC emergency power-center 740VU. (4) Put the adjustable access platform in position.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A311 Jul 01/05
4. Procedure _________ Subtask 12-36-29-860-091 A. Preparation before the flushing of the HP line (Ref. Fig. 321/TASK 12-36-29-991-047) CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE ON THE GROUND HYDRAULIC CART _______ IS SET TO A MINIMUM OF 7 BARS (101.53 PSI). (1) Disconnect the case drain line from the engine pump. (2) Disconnect the pressure line from the engine pump. (3) Disconnect the case drain line from the case drain filter. (4) Connect the pressure line and the case drain line together with the engine pump case drain/engine pump pressure connection (98F12303000104) of the HYDRAULIC CONNECTORS (98F12303000000). (5) Connect the pressure hose of the hydraulic power cart to the case drain line with the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000). (6) Connect the return hose of the hydraulic power cart to the interface (98F12303000106) of the HYDRAULIC CONNECTORS (98F12303000000). (7) Connect the free end of the interface to the delivery ground connector 5131JM2. (8) Put blanking plugs on the disconnected line ends. (9) Close the leak measurement valve. - on the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/YELLOW pushbutton switch (the OFF legend comes on). Subtask 12-36-29-170-067 B. Flushing of the HP Line (Ref. Fig. 322/TASK 12-36-29-991-018) (1) Operate the hydraulic power cart for 2mn at 20 bars. (2) Stop the hydraulic power cart.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A312 Jul 01/05
Hydraulic Connections Figure 321/TASK 12-36-29-991-047 R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A313 Jul 01/05
Flushing of the HP Line of the Yellow Hydraulic System Figure 322/TASK 12-36-29-991-018 R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A314 Jul 01/05
(3) Open the leak measurement valve: - on the HYD section of the maintenance panel 285VU, push the LEAK MEASUREMENT VALVES/YELLOW pushbutton switch (the OFF legend goes off). (4) Replace the hydraulic filters, HP and HCU: - replace the HP filter 5111JM3 (Ref. TASK 29-13-45-600-801), - replace the HCU filter 5000EG2 (Ref. TASK 78-31-11-000-801). Subtask 12-36-29-420-067 C. Connection of the Hydraulic Line (1) Remove the blanking plugs from the disconnected line ends. (2) Remove the engine pump case drain/engine pump pressure connection (98F12303000104) of the HYDRAULIC CONNECTORS (98F12303000000) from the pressure line and from the case drain line. (3) Remove the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000) from the case drain line and from the hydraulic power cart. (4) Connect the pressure line to the engine pump. (5) TORQUE the pressure line to between 12.88 and 14.24 m.daN (94.98 and 105.01 lbf.ft). (6) Connect the case drain line to the engine pump. (7) TORQUE the case drain line to between 2.43 and 3.16 m.daN (17.92 and 23.30 lbf.ft). (8) Connect the pump case drain hose to the case drain. (9) TORQUE the case drain hose to between 5.31 and 6.21 m.daN (39.15 and 45.79 lbf.ft). Subtask 12-36-29-865-087 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 4030EM2 9JJ, 12JY, 12KS2, 13KS2
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A315 Jul 01/05
Subtask 12-36-29-611-067 E. Fill the Yellow hydraulic reservoir (Ref. TASK 12-12-29-611-805) or (Ref. TASK 12-12-29-611-806). Subtask 12-36-29-863-067 F. Pressurize the Yellow hydraulic reservoir (Ref. TASK 29-14-00-614-804). Subtask 12-36-29-410-136 G. Close the right thrust reverser : - FOR 4030EM2 close the door 427AL (Ref. TASK 78-30-00-410-801) Subtask 12-36-29-440-067 H. Make sure that the thrust reverser is serviceable after maintenance (Ref. TASK 78-30-00-440-804). Subtask 12-36-29-410-084 J. Close the fan cowl doors. FOR 4030EM2 - close the door 425BL (Ref. TASK 71-13-00-410-802). Subtask 12-36-29-281-067 K. Sampling (1) Perform a fluid sampling for particular contamination (Ref. TASK 1232-29-281-801). (2) Perform in daily check, the check of the clogging indicators of the HP filter 5111JM3 and the HCU filter 5001EG2. Do this operation again until the clogging indicator stay in. 5. Close-up ________ Subtask 12-36-29-410-085 A. Close Access (1) Close the door of the AC/DC emergency power-center 740VU. (2) Close the access door 811.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A316 Jul 01/05
(3) Remove the access platform(s). (4) Close the MLG doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-942-067 B. Remove the safety devices. (1) Remove the warning notice(s). Subtask 12-36-29-862-067 C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A317 Jul 01/05
**ON A/C 701-749, TASK 12-36-29-170-806-A Flushing of the HP line of the Yellow Hydraulic System WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job To flush the Yellow hydraulic system after a failure of the engine pump. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No No No No No
specific specific specific specific specific specific specific specific
No specific 98F12303000000
adjustable access platform blanking plugs circuit breaker(s) safety clip(s) hydraulic power cart warning notice access platform 2.5 m (8 ft. 2 in.) container 5 l (1.3208 USgal) Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft) Torque Wrench : range 2.00 to 20.00 m.daN (15.00 to 150.00 lbf.ft) 1 HYDRAULIC CONNECTORS
EFF : 701-749, 12-36-29 R SROS
Page A318 Apr 01/01
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-805 12-12-29-611-806 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-13-45-600-801 29-14-00-614-803 R 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 78-31-41-000-803 12-36-29-991-048 12-36-29-991-024 FOR FIN 4030EM2 71-13-00-010-805 71-13-00-410-805
Fill the Yellow Hydraulic Reservoir with a Hydraulic Service Cart Fill the Yellow Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Servicing of the Yellow HP Filter (5111JM3) Depressurization of the Yellow Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Removal of the Isolation Control Unit (4117KS) Fig. 323 Fig. 324 Open the Fan Cowl Doors Close the Fan Cowl Doors
3. __________ Job Set-up Subtask 12-36-29-860-073 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Make sure that the Yellow hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-804). (3) Depressurize the reservoir of the Yellow hydraulic system (Ref. TASK 29-14-00-614-803).
EFF : 701-749, 12-36-29 SROS
Page A319 Apr 01/05
Subtask 12-36-29-941-073 B. Safety Precautions (1) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure. (2) On the panel 225VU, make sure that the APU BLEED pushbutton switch is released (ON legend off) and install a warning notice to tell persons not to use it. (3) Put a warning notice in position to tell persons not to pressurize the hydraulic system: - on the HYD/FUEL control panel 245VU in the cockpit, - on the Yellow hydraulic system, access door 197BB. (4) On the panel 125VU: - make sure that the ENG MASTER switches for the two engines are in the OFF position, - put a warning notice to tell persons not to supply power to the ECU. (5) On the panel 285VU: - make sure that the ON legend of the related ENG FADEC GND PWR pushbutton switch is off, - put a warning notice to tell persons not to supply power to the FADEC system. (6) Put a container below the Yellow hydraulic engine pump and below the case drain filter. Subtask 12-36-29-865-099 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 722VU HYD PUMP Y CTL 9JJ R36 722VU HYD PUMP Y ENG 2 12JY T46 742VU FADEC A ENG 2 12KS2 Q74
EFF : 701-749, 12-36-29 R SROS
Page A320 Apr 01/01
Subtask 12-36-29-010-096 D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Open the fan cowl doors: FOR 4030EM2 Open the door 426AR (Ref. TASK 71-13-00-010-805) Subtask 12-36-29-010-097 E. Get access to the avionics compartment. (1) Put the access platform in position at the access door 811. (2) Open the access door 811. (3) Open the door of the AC/DC emergency power-center 740VU. (4) Put the adjustable access platform in position. 4. Procedure _________ Subtask 12-36-29-860-097 A. Preparation before the flushing of the HP line (Ref. Fig. 323/TASK 12-36-29-991-048) R R
CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE ON THE GROUND HYDRAULIC CART _______ IS SET TO A MINIMUM OF 7 BARS (101.53 PSI). (1) Disconnect the case drain line from the engine pump. (2) Disconnect the pressure line from the engine pump. (3) Disconnect the case drain line from the case drain filter. (4) Connect the pressure line and the case drain line together with the engine pump case drain/engine pump pressure connection (98F12303000104) of the HYDRAULIC CONNECTORS (98F12303000000). (5) Connect the pressure hose of the hydraulic power cart to the case drain line with the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000).
EFF : 701-749, 12-36-29 SROS
Page A321 Oct 01/04
Hydraulic Connections Figure 323/TASK 12-36-29-991-048 EFF : 701-749, 12-36-29 R SROS
Page A322 Apr 01/01
(6) Connect the return hose of the hydraulic power cart to the interface (98F12303000106) of the HYDRAULIC CONNECTORS (98F12303000000). (7) Connect the free end of the interface to the delivery ground connector 5131JM2. (8) Put blanking plugs on the disconnected line ends. (9) Close the leak measurement valve. - on the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/YELLOW pushbutton switch (the OFF legend comes on). Subtask 12-36-29-170-073 B. Flushing of the HP Line (Ref. Fig. 324/TASK 12-36-29-991-024) (1) Operate the hydraulic power cart for 2mn at 20 bars. (2) Stop the hydraulic power cart. (3) Open the leak measurement valve: - on the HYD section of the maintenance panel 285VU, push the LEAK MEASUREMENT VALVES/YELLOW pushbutton switch (the OFF legend goes off). (4) Replace the hydraulic filters, HP and filter element: - replace the HP filter 5111JM3 (Ref. TASK 29-13-45-600-801), - remove the filter element of the located on the Isolation Control Unit 4117KS (Ref. TASK 78-31-41-000-803). Subtask 12-36-29-420-073 C. Connection of the Hydraulic Line (1) Remove the blanking plugs from the disconnected line ends. (2) Remove the engine pump case drain/engine pump pressure connection (98F12303000104) of the HYDRAULIC CONNECTORS (98F12303000000) from the pressure line and from the case drain line. (3) Remove the hydraulic power cart/case drain interface (98F12303000102) of the HYDRAULIC CONNECTORS (98F12303000000) from the case drain line and from the hydraulic power cart. (4) Connect the pressure line to the engine pump.
EFF : 701-749, 12-36-29 R SROS
Page A323 Apr 01/01
Flushing of the HP line of the Yellow Hydraulic System Figure 324/TASK 12-36-29-991-024 EFF : 701-749, 12-36-29 R SROS
Page A324 Apr 01/01
(5) TORQUE the pressure line to between 12.88 and 14.24 m.daN (94.98 and 105.01 lbf.ft). (6) Connect the case drain line to the engine pump. (7) Connect the pump case drain hose to the case drain. (8) TORQUE the case drain line to between 2.43 and 3.16 m.daN (17.92 and 23.30 lbf.ft). Subtask 12-36-29-865-100 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 4030EM2 9JJ, 12JY, 12KS2, 13KS2 Subtask 12-36-29-611-073 E. Fill the Yellow hydraulic reservoir (Ref. TASK 12-12-29-611-805) or (Ref. TASK 12-12-29-611-806). Subtask 12-36-29-863-073 F. Pressurize the Yellow hydraulic reservoir (Ref. TASK 29-14-00-614-804). Subtask 12-36-29-410-096 G. Close the fan cowl doors. FOR 4030EM2 - close the door 426AR (Ref. TASK 71-13-00-410-805). Subtask 12-36-29-281-073 H. Sampling (1) Perform a fluid sampling for particular contamination (Ref. TASK 1232-29-281-801). (2) Perform in daily check, the check of the clogging indicators of the HP filter 5111JM3 and the filter element of the located on the Isolation Control Unit 4117KS. Do this operation again until the clogging indicator stay in.
R EFF : 701-749, 12-36-29 SROS
Page A325 Apr 01/01
5. Close-up ________ Subtask 12-36-29-410-097 A. Close Access (1) Close the door of the AC/DC emergency power-center 740VU. (2) Close the access door 811. (3) Remove the access platform(s). (4) Close the MLG doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-942-073 B. Remove the safety devices. (1) Remove the warning notice(s). Subtask 12-36-29-862-073 C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 701-749, 12-36-29 SROS
Page A326 Apr 01/01
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, TASK 12-36-29-170-807 Flushing of the Green Hydraulic System with the Aircraft Pumps WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-801 12-12-29-611-802 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-10-00-200-804 29-10-00-200-806
Fill the Green Hydraulic Reservoir with a Hydraulic Service Cart Fill the Green Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Check of the Clogging Indicators of the Hydraulic System Filter in the Hydraulics Compartment. Check of the Clogging Indicators of the Hydraulic System Filters on the Engines.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A327 Jul 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-11-43-600-802 29-11-44-600-801 29-11-45-600-801 29-14-00-614-804 31-60-00-860-801 31-60-00-860-802 71-00-00-860-801 78-31-00-710-804
Servicing of the (Forward) Engine-Pump Case-Drain Filter Element 5013JM1 Servicing of the Green Reservoir LP-Filter (5011JM1) Servicing of the Green HP Filter (5111JM101,5111JM102) Pressurization of the Hydraulic Reservoirs with external bench EIS Start Procedure EIS Stop Procedure Engine Automatic Start Thrust Reverser Cycling Test (MCDU)
R 3. __________ Job Set-up Subtask 12-36-29-860-116 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Do the EIS start procedure (EWD, SD DU only) (Ref. TASK 31-60-00-860801). (3) On the ECAM control panel, push the HYD key (on the SD, the HYD page comes into view). (4) Make sure that the SD does not show any of these conditions: - low air pressure in the Green reservoir. If this message is shown, pressurize the reservoir (Ref. TASK 29-14-00-614-804), - low fluid level in the Green reservoir. If the fluid is not correct add fluid with a service cart or with a hand pump (Ref. TASK 12-1229-611-801), (Ref. TASK 12-12-29-611-802).
EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A328 Jan 01/07
Subtask 12-36-29-865-110 B. On the ECAM control panel, push the C/B key (on the SD the C/B page comes into view). Make sure that the SD does not show this(these) circuit breaker(s) : ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU HSMU B + PART G 6JG U10 721VU HYD PUMP G ENG 1 14JG2 X11 722VU HYD SOV BUS SWTG 8JG R33 742VU HYD FIRE ENG 1 SOV 15JG2 D75 FOR 4030EM2 722VU HYD SOV ENG 2 NORM 15JY R35 722VU HSMU Y + PART G 7JG X46 722VU HYD PUMP G ENG 2 14JG1 X45 742VU HYD FIRE ENG 2 SOV 15JG1 D72 4. Procedure _________ Subtask 12-36-29-170-083 A. Flushing of the Green hydraulic system with A/C (1) Start the engine 1 (Ref. TASK 71-00-00-860-801). R
(2) During 10 minutes approximately: - operate the Captain and F/O sidestick and rudder pedals over full travel so that the controls surfaces move continuously, - operate cycles of the thrust reversers (Ref. TASK 78-31-00-710-804) in order to cause a hydraulic flow through the filter. (3) Stop the engine 1. (4) Do the check of the clogging indicators of: - the case-drain filters 5013JM1 (Ref. TASK 29-10-00-200-806), - the HP filters 5111JM101, 5111JM102 (Ref. TASK 29-10-00-200-804), - the LP filter 5011JM1 (Ref. TASK 29-10-00-200-804).
R R
(5) If necessary replace the defective filter element: - the case-drain filters 5013JM1 (Ref. TASK 29-11-43-600-802), - the HP filters 5111JM101, 5111JM102 (Ref. TASK 29-11-45-600-801), - the LP filter 5011JM1 (Ref. TASK 29-11-44-600-801).
R R
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Page A329 Jan 01/07
(6) Start the engine 1 and do the step (2) again. (7) Stop the engine 1 and do the step (4) again. (8) Do the step (1) to (5) again until the clogging indicators stay in. (9) Do a fluid sampling for particles contamination (Ref. TASK 12-32-29281-801). (a) If particle contamination is out of limits do the step (1) to (5) again. 5. Close-up ________ Subtask 12-36-29-860-117 A. Do the EIS stop procedure (Ref. TASK 31-60-00-860-802). Subtask 12-36-29-862-083 B. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A330 Jul 01/05
**ON A/C 701-749, TASK 12-36-29-170-807-A Flushing of the Green Hydraulic System with the Aircraft Pumps WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-801 12-12-29-611-802 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-10-00-200-804 29-10-00-200-806
Fill the Green Hydraulic Reservoir with a Hydraulic Service Cart Fill the Green Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Check of the Clogging Indicators of the Hydraulic System Filter in the Hydraulics Compartment. Check of the Clogging Indicators of the Hydraulic System Filters on the Engines.
EFF : 701-749, 12-36-29 R SROS
Page A331 Apr 01/01
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-11-43-600-807 29-11-44-600-801 29-11-45-600-801 29-14-00-614-804 31-60-00-860-801 31-60-00-860-802 71-00-00-860-801 78-31-00-740-802 78-31-41-000-803
Servicing of the Engine-Pump Case Drain Filter (5013JM1) Servicing of the Green Reservoir LP-Filter (5011JM1) Servicing of the Green HP Filter (5111JM101,5111JM102) Pressurization of the Hydraulic Reservoirs with external bench EIS Start Procedure EIS Stop Procedure Engine Automatic Start Test of the Thrust Reverser Deployment and Stowage (Engine not Running) Removal of the Isolation Control Unit (4117KS)
3. __________ Job Set-up Subtask 12-36-29-860-104 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Do the EIS start procedure (EWD, SD DU only) (Ref. TASK 31-60-00-860801). (3) On the ECAM control panel, push the HYD key (on the SD, the HYD page comes into view). (4) Make sure that the SD does not show any of these conditions: - low air pressure in the Green reservoir. If this message is shown, pressurize the reservoir (Ref. TASK 29-14-00-614-804), - low fluid level in the Green reservoir. If the fluid is not correct add fluid with a service cart or with a hand pump (Ref. TASK 12-1229-611-801), (Ref. TASK 12-12-29-611-802).
EFF : 701-749, 12-36-29 R SROS
Page A332 Apr 01/01
Subtask 12-36-29-865-104 B. On the ECAM control panel, push the C/B key (on the SD the C/B page comes into view). Make sure that the SD does not show this(these) circuit breaker(s) : ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU HSMU B + PART G 6JG U10 722VU HYD SOV BUS SWTG 8JG R33 742VU HYD FIRE ENG 1 SOV 15JG2 D75 742VU HYD PUMP G ENG 1 14JG2 E67 FOR 4030EM2 722VU HYD SOV ENG 2 NORM 15JY R35 722VU HSMU Y + PART G 7JG X46 722VU HYD PUMP G ENG 2 14JG1 X45 742VU HYD FIRE ENG 2 SOV 15JG1 D72 4. Procedure _________ Subtask 12-36-29-170-077 A. Flushing of the Green hydraulic system with A/C (1) Start the engine 1 (Ref. TASK 71-00-00-860-801). (2) During 10mn approximately: - operate the Captain and F/O sidestick and rudder pedals over full travel so that the controls surfaces move continuously, - operate cycles of the thrust reversers (Ref. TASK 78-31-00-740-802) in order to cause a hydraulic flow through the filter. (3) Stop the engine 1. (4) Do the check of the clogging indicators of: - the case-drain filters 5013JM1 (Ref. TASK 29-10-00-200-806), - the HP filters 5111JM101, 5111JM102 (Ref. TASK 29-10-00-200-804), - the LP filter 5011JM1 (Ref. TASK 29-10-00-200-804), - the filter element located on the Isolation Control Unit 4117KS (Ref. TASK 78-31-41-000-803).
R EFF : 701-749, 12-36-29 SROS
Page A333 Apr 01/01
(5) If necessary replace the defective filter element: - the case-drain filters 5013JM1 (Ref. TASK 29-11-43-600-807), - the HP filters 5111JM101, 5111JM102 (Ref. TASK 29-11-45-600-801), - the LP filter 5011JM1 (Ref. TASK 29-11-44-600-801), - the filter element located on the Isolation Control Unit 4117KS (Ref. TASK 78-31-41-000-803). (6) Start the engine 1 and do the step (2) again. (7) Stop the engine 1 and do the step (4) again. (8) Do the step (1) to (5) again until the clogging indicators stay in. R
(9) Do a fluid sampling for particles contamination (Ref. TASK 12-32-29281-801).
R R R
(a) If particle contamination is out of limits do the step (1) to (5) again. 5. Close-up ________ Subtask 12-36-29-860-105 A. Do the EIS stop procedure (Ref. TASK 31-60-00-860-802). Subtask 12-36-29-862-077 B. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
EFF : 701-749, 12-36-29 SROS
Page A334 Oct 01/04
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, TASK 12-36-29-170-808 Flushing of the Blue Hydraulic System with the Aircraft Pump WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-803 12-12-29-611-804 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-10-00-200-804 29-10-00-200-806
Fill the Blue Hydraulic Reservoir with a Hydraulic Service Cart Fill the Blue Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Check of the Clogging Indicators of the Hydraulic System Filter in the Hydraulics Compartment. Check of the Clogging Indicators of the Hydraulic System Filters on the Engines.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A335 Jul 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-11-43-600-804 29-12-44-600-801 29-12-45-600-801 29-14-00-614-804 31-60-00-860-801 31-60-00-860-802 71-00-00-860-801 78-31-00-710-804 78-31-11-000-801
Servicing of the (Aft) Engine-Pump Case-Drain Filter Element 5013JM2 Servicing of the Blue Reservoir LP-Filter (5011JM2) Servicing of the Blue HP Filter (5111JM2) Pressurization of the Hydraulic Reservoirs with external bench EIS Start Procedure EIS Stop Procedure Engine Automatic Start Thrust Reverser Cycling Test (MCDU) Removal of the Hydraulic Filter Element
3. __________ Job Set-up Subtask 12-36-29-860-118 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Do the EIS start procedure (EWD, SD DU only) (Ref. TASK 31-60-00-860801). (3) On the ECAM control panel, push the HYD key (on the SD, the HYD page comes into view). (4) Make sure that the SD does not show any of these conditions: - low air pressure in the Blue reservoir. If this message is shown, pressurize the reservoir (Ref. TASK 29-14-00-614-804), - low fluid level in the Blue reservoir. If the fluid is not correct add fluid with a service cart or with a hand pump (Ref. TASK 12-1229-611-803), (Ref. TASK 12-12-29-611-804).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A336 Jul 01/05
Subtask 12-36-29-865-111 B. On the ECAM control panel, push the C/B key (on the SD the C/B page comes into view). Make sure that the SD does not show this(these) circuit breaker(s) : ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU HSMU B + PART G 6JG U10 721VU HYD PUMP G ENG 1 14JG2 X11 722VU HYD SOV BUS SWTG 8JG R33 742VU HYD FIRE ENG 1 SOV 15JG2 D75 4. Procedure _________ Subtask 12-36-29-170-084 A. Flushing of the Blue hydraulic system with A/C (1) Start the engine 1 (Ref. TASK 71-00-00-860-801). (2) During 10mn approximately: - operate the Captain and F/O sidestick and rudder pedals over full travel so that the controls surfaces move continuously, - operate cycles of the thrust reversers (Ref. TASK 78-31-00-710-804) in order to cause a hydraulic flow through the filter. (3) Stop the engine 1. (4) Do the check of the clogging indicators of: - the case-drain filter 5013JM2 (Ref. TASK 29-10-00-200-806), - the HP filter 5111JM2 (Ref. TASK 29-10-00-200-804), - the LP filter 5011JM2 (Ref. TASK 29-10-00-200-804), - the HCU filter 5000EG2 (Ref. TASK 78-31-11-000-801). (5) If necessary replace the defective filter element: - the case-drain filter 5013JM2 (Ref. TASK 29-11-43-600-804), - the HP filter 5111JM2 (Ref. TASK 29-12-45-600-801), - the LP filter 5011JM2 (Ref. TASK 29-12-44-600-801), - the HCU filter 5000EG2 (Ref. TASK 78-31-11-000-801). (6) Start the engine 1 and repeat step (2) again (7) Stop the engine 1 and repeat step (4) again.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A337 Jul 01/05
(8) Do the step (1) to (5) again until the clogging indicators stay in. (9) Do a fluid sampling for particles contamination (Ref. TASK 12-32-29281-801). (a) If particles contamination is out of limits do the step (1) to (5) again. 5. Close-up ________ Subtask 12-36-29-860-119 A. Do the EIS stop procedure (Ref. TASK 31-60-00-860-802). Subtask 12-36-29-862-084 B. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A338 Jul 01/05
**ON A/C 701-749, TASK 12-36-29-170-808-A Flushing of the Blue Hydraulic System with the Aircraft Pump WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-803 12-12-29-611-804 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-10-00-200-804 29-10-00-200-806
Fill the Blue Hydraulic Reservoir with a Hydraulic Service Cart Fill the Blue Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Check of the Clogging Indicators of the Hydraulic System Filter in the Hydraulics Compartment. Check of the Clogging Indicators of the Hydraulic System Filters on the Engines.
EFF : 701-749, 12-36-29 R SROS
Page A339 Apr 01/01
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-11-43-600-809 29-12-44-600-801 29-12-45-600-801 29-14-00-614-804 31-60-00-860-801 31-60-00-860-802 71-00-00-860-801 78-31-00-740-802 78-31-41-000-803
Servicing of the Engine Pump Case Drain Filter (5013JM2) Servicing of the Blue Reservoir LP-Filter (5011JM2) Servicing of the Blue HP Filter (5111JM2) Pressurization of the Hydraulic Reservoirs with external bench EIS Start Procedure EIS Stop Procedure Engine Automatic Start Test of the Thrust Reverser Deployment and Stowage (Engine not Running) Removal of the Isolation Control Unit (4117KS)
3. __________ Job Set-up Subtask 12-36-29-860-106 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Do the EIS start procedure (EWD, SD DU only) (Ref. TASK 31-60-00-860801). (3) On the ECAM control panel, push the HYD key (on the SD, the HYD page comes into view). (4) Make sure that the SD does not show any of these conditions: - low air pressure in the Blue reservoir. If this message is shown, pressurize the reservoir (Ref. TASK 29-14-00-614-804), - low fluid level in the Blue reservoir. If the fluid is not correct add fluid with a service cart or with a hand pump (Ref. TASK 12-1229-611-803), (Ref. TASK 12-12-29-611-804).
EFF : 701-749, 12-36-29 R SROS
Page A340 Apr 01/01
Subtask 12-36-29-865-105 B. On the ECAM control panel, push the C/B key (on the SD the C/B page comes into view). Make sure that the SD does not show this(these) circuit breaker(s) : ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM1 721VU HSMU B + PART G 6JG U10 722VU HYD SOV BUS SWTG 8JG R33 742VU HYD FIRE ENG 1 SOV 15JG2 D75 742VU HYD PUMP G ENG 1 14JG2 E67 4. Procedure _________ Subtask 12-36-29-170-078 A. Flushing of the Blue hydraulic system with A/C (1) Start the engine 1 (Ref. TASK 71-00-00-860-801). (2) During 10mn approximately: - operate the Captain and F/O sidestick and rudder pedals over full travel so that the controls surfaces move continuously, - operate cycles of the thrust reversers (Ref. TASK 78-31-00-740-802) in order to cause a hydraulic flow through the filter. (3) Stop the engine 1. (4) Do the check of the clogging indicators of: - the case-drain filter 5013JM2 (Ref. TASK 29-10-00-200-806), - the HP filter 5111JM2 (Ref. TASK 29-10-00-200-804), - the LP filter 5011JM2 (Ref. TASK 29-10-00-200-804), - the filter element located on the Isolation Control Unit 4117KS (Ref. TASK 78-31-41-000-803). (5) If necessary replace the defective filter element: - the case-drain filter 5013JM2 (Ref. TASK 29-11-43-600-809), - the HP filter 5111JM2 (Ref. TASK 29-12-45-600-801), - the LP filter 5011JM2 (Ref. TASK 29-12-44-600-801), - the filter element located on the Isolation Control Unit 4117KS (Ref. TASK 78-31-41-000-803). (6) Start the engine 1 and repeat step (2) again
R EFF : 701-749, 12-36-29 SROS
Page A341 Apr 01/01
(7) Stop the engine 1 and repeat step (4) again. (8) Do the step (1) to (5) again until the clogging indicators stay in. R
(9) Do a fluid sampling for particles contamination (Ref. TASK 12-32-29281-801).
R R R
(a) If particles contamination is out of limits do the step (1) to (5) again. 5. Close-up ________ Subtask 12-36-29-860-107 A. Do the EIS stop procedure (Ref. TASK 31-60-00-860-802). Subtask 12-36-29-862-078 B. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
EFF : 701-749, 12-36-29 SROS
Page A342 Oct 01/04
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, TASK 12-36-29-170-809 Flushing of the Yellow Hydraulic System with the Aircraft Pump WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-805 12-12-29-611-806 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-10-00-200-804 29-10-00-200-806
Fill the Yellow Hydraulic Reservoir with a Hydraulic Service Cart Fill the Yellow Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Check of the Clogging Indicators of the Hydraulic System Filter in the Hydraulics Compartment. Check of the Clogging Indicators of the Hydraulic System Filters on the Engines.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A343 Jul 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-11-43-600-804 29-13-44-600-801 29-13-45-600-801 29-14-00-614-804 31-60-00-860-801 31-60-00-860-802 71-00-00-860-801 78-31-00-710-804 78-31-11-000-801
Servicing of the (Aft) Engine-Pump Case-Drain Filter Element 5013JM2 Servicing of the Yellow Reservoir LP-Filter (5011JM3) Servicing of the Yellow HP Filter (5111JM3) Pressurization of the Hydraulic Reservoirs with external bench EIS Start Procedure EIS Stop Procedure Engine Automatic Start Thrust Reverser Cycling Test (MCDU) Removal of the Hydraulic Filter Element
3. __________ Job Set-up Subtask 12-36-29-860-120 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Do the EIS start procedure (EWD, SD DU only) (Ref. TASK 31-60-00-860801). (3) On the ECAM control panel, push the HYD key (on the SD, the HYD page comes into view). (4) Make sure that the SD does not show any of these conditions: - low air pressure in the Yellow reservoir. If this message is shown, pressurize the reservoir (Ref. TASK 29-14-00-614-804), - low fluid level in the Yellow reservoir. If the fluid is not correct add fluid with a service cart or with a hand pump (Ref. TASK 12-12-29-611-805), (Ref. TASK 12-12-29-611-806).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A344 Jul 01/05
Subtask 12-36-29-865-112 B. On the ECAM control panel, push the C/B key (on the SD the C/B page comes into view). Make sure that the SD does not show this(these) circuit breaker(s) : ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM2 722VU HYD SOV ENG 2 NORM 15JY R35 722VU HSMU Y + PART G 7JG X46 722VU HYD PUMP G ENG 2 14JG1 X45 742VU HYD FIRE ENG 2 SOV 15JG1 D72 4. Procedure _________ Subtask 12-36-29-170-085 A. Flushing of the Yellow hydraulic system with A/C (1) Start the engine 2 (Ref. TASK 71-00-00-860-801). (2) During 10mn approximately: - operate the Captain and F/O sidestick and rudder pedals over full travel so that the controls surfaces move continuously, - operate cycles of the thrust reversers (Ref. TASK 78-31-00-710-804) in order to cause a hydraulic flow through the filter. (3) Stop the engine 2. (4) Do the check of the clogging indicators of: - the case-drain filter 5013JM2 (Ref. TASK 29-10-00-200-806), - the HP filters 5111JM3 (Ref. TASK 29-10-00-200-804), - the LP filter 5011JM3 (Ref. TASK 29-10-00-200-804), - the HCU filter 5000EG3 (Ref. TASK 78-31-11-000-801). (5) If necessary replace the defective filter element: - the case-drain filter 5013JM2 (Ref. TASK 29-11-43-600-804), - the HP filter 5111JM3 (Ref. TASK 29-13-45-600-801), - the LP filter 5011JM3 (Ref. TASK 29-13-44-600-801), - the HCU filter 5000EG3 (Ref. TASK 78-31-11-000-801). (6) Start the engine 2 and do the step (2) again. (7) Stop the engine 2 and do the step (4) again.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A345 Jul 01/05
(8) Do the step (1) to (5) again until the clogging indicators stay in. (9) Do a fluid sampling for particles contamination (Ref. TASK 12-32-29281-801). (a) If particle contamination is out of limits do the steps (1) to (5) again. 5. Close-up ________ Subtask 12-36-29-860-121 A. Do the EIS stop procedure (Ref. TASK 31-60-00-860-802). Subtask 12-36-29-862-085 B. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A346 Jul 01/05
**ON A/C 701-749, TASK 12-36-29-170-809-A Flushing of the Yellow Hydraulic System with the Aircraft Pump WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-805 12-12-29-611-806 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-10-00-200-804 29-10-00-200-806
Fill the Yellow Hydraulic Reservoir with a Hydraulic Service Cart Fill the Yellow Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Check of the Clogging Indicators of the Hydraulic System Filter in the Hydraulics Compartment. Check of the Clogging Indicators of the Hydraulic System Filters on the Engines.
EFF : 701-749, 12-36-29 R SROS
Page A347 Apr 01/01
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-11-43-600-809 29-13-44-600-801 29-13-45-600-801 29-14-00-614-804 31-60-00-860-801 31-60-00-860-802 71-00-00-860-801 78-31-00-740-802 78-31-41-000-803
Servicing of the Engine Pump Case Drain Filter (5013JM2) Servicing of the Yellow Reservoir LP-Filter (5011JM3) Servicing of the Yellow HP Filter (5111JM3) Pressurization of the Hydraulic Reservoirs with external bench EIS Start Procedure EIS Stop Procedure Engine Automatic Start Test of the Thrust Reverser Deployment and Stowage (Engine not Running) Removal of the Isolation Control Unit (4117KS)
3. __________ Job Set-up Subtask 12-36-29-860-108 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Do the EIS start procedure (EWD, SD DU only) (Ref. TASK 31-60-00-860801). (3) On the ECAM control panel, push the HYD key (on the SD, the HYD page comes into view). (4) Make sure that the SD does not show any of these conditions: - low air pressure in the Yellow reservoir. If this message is shown, pressurize the reservoir (Ref. TASK 29-14-00-614-804), - low fluid level in the Yellow reservoir. If the fluid is not correct add fluid with a service cart or with a hand pump (Ref. TASK 12-12-29-611-805), (Ref. TASK 12-12-29-611-806).
EFF : 701-749, 12-36-29 R SROS
Page A348 Apr 01/01
Subtask 12-36-29-865-106 B. On the ECAM control panel, push the C/B key (on the SD the C/B page comes into view). Make sure that the SD does not show this(these) circuit breaker(s) : ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------FOR 4030EM2 722VU HYD SOV ENG 2 NORM 15JY R35 722VU HSMU Y + PART G 7JG X46 722VU HYD PUMP G ENG 2 14JG1 X45 742VU HYD FIRE ENG 2 SOV 15JG1 D72 4. Procedure _________ Subtask 12-36-29-170-079 A. Flushing of the Yellow hydraulic system with A/C (1) Start the engine 2 (Ref. TASK 71-00-00-860-801). (2) During 10mn approximately: - operate the Captain and F/O sidestick and rudder pedals over full travel so that the controls surfaces move continuously, - operate cycles of the thrust reversers (Ref. TASK 78-31-00-740-802) in order to cause a hydraulic flow through the filter. (3) Stop the engine 2. (4) Do the check of the clogging indicators of: - the case-drain filter 5013JM2 (Ref. TASK 29-10-00-200-806), - the HP filters 5111JM3 (Ref. TASK 29-10-00-200-804), - the LP filter 5011JM3 (Ref. TASK 29-10-00-200-804), - the filter element located on the Isolation Control Unit 4117KS (Ref. TASK 78-31-41-000-803). (5) If necessary replace the defective filter element: - the case-drain filter 5013JM2 (Ref. TASK 29-11-43-600-809), - the HP filter 5111JM3 (Ref. TASK 29-13-45-600-801), - the LP filter 5011JM3 (Ref. TASK 29-13-44-600-801), - the filter element located on the Isolation Control Unit 4117KS (Ref. TASK 78-31-41-000-803). (6) Start the engine 2 and do the step (2) again.
R EFF : 701-749, 12-36-29 SROS
Page A349 Apr 01/01
(7) Stop the engine 2 and do the step (4) again. (8) Do the step (1) to (5) again until the clogging indicators stay in. R
(9) Do a fluid sampling for particles contamination (Ref. TASK 12-32-29281-801).
R R R
(a) If particle contamination is out of limits do the steps (1) to (5) again. 5. Close-up ________ Subtask 12-36-29-860-109 A. Do the EIS stop procedure (Ref. TASK 31-60-00-860-802). Subtask 12-36-29-862-079 B. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
EFF : 701-749, 12-36-29 SROS
Page A350 Oct 01/04
**ON A/C ALL TASK 12-36-29-170-810 Flushing of the Suction line of the Green Hydraulic System. WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific No specific No specific
circuit breaker(s) safety clip(s) warning notice container 70 l (18.4918 USgal)
EFF : ALL 12-36-29 SROS
Page A351 Jan 01/07
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R R R R R R R R R R
12-12-29-611-801 12-12-29-611-802 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-10-00-710-805 29-11-38-000-803 29-11-38-000-804 29-11-38-400-803 29-11-38-400-804
R R R R R
29-14-00-614-801 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 71-13-00-410-805 FOR FIN 4030EM1 71-13-00-010-805
Fill the Green Hydraulic Reservoir with a Hydraulic Service Cart Fill the Green Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Operational Test of the Electric Motor of the Engine Pump Suction Fire Shut-Off Valve Removal of the Engine Pump Suction Self Sealing (Elbow) Coupling (5135JM1) Removal of the Hydraulic System Self-Sealing Coupling (5135JM1) Installation of the Engine Pump Suction Self Sealing (Elbow) Coupling (5135JM1) Installation of the Hydraulic System Self-Sealing Coupling (5135JM1) Depressurization of the Green Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Close the Fan Cowl Doors Open the Fan Cowl Doors
EFF : ALL 12-36-29 SROS
Page A352 Jan 01/07
3. __________ Job Set-up R R
Subtask 12-36-29-860-202 A. Aircraft Maintenance Configuration
R R
(1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801).
R R R
(2) Make sure that the Green hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-804).
R R
(3) Depressurize the reservoir of the Green hydraulic system (Ref. TASK 29-14-00-614-801). Subtask 12-36-29-941-080
R
B. Safety Precautions (1) Make sure that the engine 1, 2 shutdown occurred not less than 5 minutes before you do this procedure. (2) On the panel 225VU, make sure that the APU BLEED pushbutton switch is released (ON legend off) and install a warning notice to tell persons not to use it.
R
(3) Put a warning notice in position to tell persons not to pressurize the hydraulic system: - on the HYD/FUEL control panel 245VU in the cockpit - on the Green hydraulic system, access door 197CB.
R R R R R
(4) On the panel 125VU. - Make sure that the ENG MASTER switches for the two engines are in the OFF position. - Put a warning notice to tell persons not to supply power to the ECU.
R R R R R
(5) On the panel 285VU. - Make sure that the ON legend of the related ENG FADEC GND PWR pushbutton switch is off, - Put a warning notice to tell persons not to supply power to the FADEC system. (6) Put a container below the Green hydraulic engine pump.
EFF : ALL 12-36-29 SROS
Page A353 Jan 01/07
R R R
Subtask 12-36-29-865-176 C. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s):
R R R
------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION -------------------------------------------------------------------------------
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499,
R R R R R R R R R R R
721VU HYD PUMP G ENG 1
14JG2
X11
9JV 13KS1 13KS2 14JG1 12KS2 12KS1
U09 D44 K49 X45 Q74 Q73
14JG2
E67
**ON A/C ALL 721VU 722VU 722VU 722VU 742VU 742VU
HYD PUMP G CTL FADEC B ENG 1 FADEC B ENG 2 HYD PUMP G ENG 2 FADEC A ENG 2 FADEC A ENG 1
**ON A/C 701-749, 742VU HYD PUMP G ENG 1 **ON A/C ALL Subtask 12-36-29-010-147
R
D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801).
R
(2) Open the fan cowl doors. FOR 4030EM1 - Open the door 416AR (Ref. TASK 71-13-00-010-805).
R
EFF : ALL 12-36-29 SROS
Page A354 Jan 01/07
4. Procedure _________ **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 12-36-29-860-203 A. Preparation before the flushing of the Suction Line. NOTE : Keep the suction line connect to the self sealing coupling. ____ (1) Disconnect the self-sealing coupling (5135JM) from the engine pump. Ref to the applicable step (Ref. TASK 29-11-38-000-803).
R
(2) Put blanking plug on the suction port of the hydraulic pump. R **ON A/C 701-749, Subtask 12-36-29-860-203-A A. Preparation before the flushing of the Suction Line. NOTE : Keep the suction line connect to the self sealing coupling. ____ (1) Disconnect the self-sealing coupling (5135JM) from the engine pump. Ref to the applicable step (Ref. TASK 29-11-38-000-804).
R
(2) Put blanking plug on the suction port of the hydraulic pump. R
**ON A/C ALL
R
Subtask 12-36-29-170-095
R
B. Flushing of the Suction Line.
R
(1) Put the suction line in the container.
R R
(2) Pressurize the hydraulic reservoir (Ref. TASK 29-14-00-614-804) to flush the suction line until the FSOV close.
R
(3) Depressurize the hydraulic reservoir (Ref. TASK 29-14-00-614-801).
R
(4) On the panel 742VU, reset the C/B 5JR.
EFF : ALL 12-36-29 SROS
Page A355 Jan 01/07
R R
(5) Do the operational test of the electrical motor of the FSOV (Ref. TASK 29-10-00-710-805).
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499,
R
Subtask 12-36-29-420-105
R
C. Installation of the self sealing coupling on the engine pump.
R
(1) Remove the blanking cap on the engine pump.
R R
(2) Install the self sealing coupling on the engine pump. Refer to the applicable step (Ref. TASK 29-11-38-400-803).
R
**ON A/C 701-749, Subtask 12-36-29-420-105-A
R
C. Installation of the self sealing coupling on the engine pump. (1) Remove the blanking cap on the engine pump. (2) Install the self sealing coupling on the engine pump. Refer to the applicable step (Ref. TASK 29-11-38-400-804).
R
**ON A/C ALL
R
Subtask 12-36-29-865-177
R R R R R R R R
D. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 14JG1, 14JG2, 12KS1, 12KS2, 13KS1, 13KS2 Subtask 12-36-29-611-198 E. Fill the Green hydraulic reservoir (Ref. TASK 12-12-29-611-801) or (Ref. TASK 12-12-29-611-802). Subtask 12-36-29-863-080 F. Pressurize the Green hydraulic reservoir (Ref. TASK 29-14-00-614-804).
EFF : ALL 12-36-29 SROS
Page A356 Jan 01/07
R Subtask 12-36-29-410-152 R R R R
G. Close the fan cowl doors. FOR 4030EM1 - Close the door 416AR (Ref. TASK 71-13-00-410-805). Subtask 12-36-29-281-080 H. Sampling
R R
(1) Perform a fluid sampling for particular contamination (Ref. TASK 1232-29-281-801).
R R R R
(2) Perform in daily check, the check of the clogging indicators, of the case drain filters 5013JM, HP filters 5111JM101, 5111JM102 and the LP filter 5011JM1: Do this operation again until the clogging indicator stay in. 5. Close-up ________
R R R
Subtask 12-36-29-862-107 A. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862801). Subtask 12-36-29-860-204
R
B. Put the Aircraft back to its Initial Configuration
R
(1) Close the MLG doors (Ref. TASK 32-12-00-410-801).
R
(2) Make sure that the work area is clean and clear of tools and other items.
R
(3) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 12-36-29 SROS
Page A357 Jan 01/07
TASK 12-36-29-170-811 Flushing of the Suction line of the Blue Hydraulic System. R R
WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS.
R R
WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY.
R R R R R
WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH.
R R R
CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific No specific No specific
circuit breaker(s) safety clip(s) warning notice container 70 l (18.4918 USgal)
EFF : ALL 12-36-29 SROS
Page A358 Jan 01/07
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R R R R R R R R R R R R R R R R R R R R R R R
12-12-29-611-803 12-12-29-611-804 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-10-00-710-805 29-12-38-000-802 29-12-38-000-803 29-12-38-400-802 29-12-38-400-803 29-14-00-614-802 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 71-13-00-410-803 FOR FIN 4030EM1 71-13-00-010-803
Fill the Blue Hydraulic Reservoir with a Hydraulic Service Cart Fill the Blue Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Operational Test of the Electric Motor of the Engine Pump Suction Fire Shut-Off Valve Removal of the Blue Hydraulic System Self-Sealing Coupling Removal of the Blue Engine Pump Suction Self Sealing (Elbow) Coupling Installation of the Blue Hydraulic System Self-Sealing Coupling Installation of the Blue Engine Pump Suction Self Sealing (Elbow) Coupling Depressurization of the Blue Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Closing of the Fan Cowl Doors Opening of the Fan Cowl Doors
EFF : ALL 12-36-29 SROS
Page A359 Jan 01/07
3. __________ Job Set-up R R
Subtask 12-36-29-860-205 A. Aircraft Maintenance Configuration
R R
(1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801).
R R R
(2) Make sure that the Blue hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-804).
R R
(3) Depressurize the reservoir of the Blue hydraulic system (Ref. TASK 29-14-00-614-802). Subtask 12-36-29-941-081
R
B. Safety Precautions
R R
(1) Make sure that the engine 1, 2 shutdown occurred not less than 5 minutes before you do this procedure. (2) On the panel 225VU, make sure that the APU BLEED pushbutton switch is released (ON legend off) and install a warning notice to tell persons not to use it.
R
(3) Put a warning notice in position to tell persons not to pressurize the hydraulic system: - on the HYD/FUEL control panel 245VU in the cockpit - on the Blue hydraulic system, access door ZAC 196BB.
R R R R R
(4) On the panel 125VU. - Make sure that the ENG MASTER switches for the two engines are in the OFF position. - Put a warning notice to tell persons not to supply power to the ECU.
R R R R R
(5) On the panel 285VU. - Make sure that the ON legend of the related ENG FADEC GND PWR pushbutton switch is off. - Put a warning notice to tell persons not to supply power to the FADEC system. (6) Put a container below the Blue hydraulic engine pump.
EFF : ALL 12-36-29 SROS
Page A360 Jan 01/07
R R R R R R R R R R R R
Subtask 12-36-29-865-178 C. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU HYD PUMP B ENG 1 11JB U08 721VU HYD PUMP B CTL 9JC X12 722VU FADEC B ENG 1 13KS1 D44 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 742VU FADEC A ENG 1 12KS1 Q73 Subtask 12-36-29-010-148
R
D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801).
R
(2) Open the fan cowl doors. FOR 4030EM1 - Open the door 415AL (Ref. TASK 71-13-00-010-803).
R
4. Procedure _________ **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 12-36-29-860-206 A. Preparation before the flushing of the Suction Line. NOTE : Keep the suction line connect to the self sealing coupling. ____ (1) Disconnect the self-sealing coupling (5135JM) from the engine pump. Ref to the applicable step (Ref. TASK 29-12-38-000-803).
R
(2) Put blanking plug on the suction port of the hydraulic pump. R
EFF : ALL 12-36-29 SROS
Page A361 Jan 01/07
**ON A/C 701-749, Subtask 12-36-29-860-206-A A. Preparation before the flushing of the Suction Line. NOTE : Keep the suction line connect to the self sealing coupling. ____ (1) Disconnect the self-sealing coupling (5135JM) from the engine pump. Ref to the applicable step (Ref. TASK 29-12-38-000-802).
R
(2) Put blanking plug on the suction port of the hydraulic pump. R
**ON A/C ALL
R
Subtask 12-36-29-170-096
R
B. Flushing of the Suction Line.
R
(1) Put the suction line in the container.
R R
(2) Pressurize the Blue hydraulic reservoir (Ref. TASK 29-14-00-614-804) to flush the suction line until the FSOV close.
R R
(3) Depressurize the Blue hydraulic reservoir (Ref. TASK 29-14-00-614802).
R
(4) On the panel 742VU, reset the C/B 5JR.
R R
(5) Do the operational test of the electrical motor of the FSOV (Ref. TASK 29-10-00-710-805).
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499,
R
Subtask 12-36-29-420-106
R
C. Installation of the self sealing coupling on the engine pump.
R
(1) Remove the blanking cap on the engine pump.
R R
(2) Install the self sealing coupling on the engine pump. Refer to the applicable step (Ref. TASK 29-12-38-400-803).
EFF : ALL 12-36-29 SROS
Page A362 Jan 01/07
R
**ON A/C 701-749, Subtask 12-36-29-420-106-A
R
C. Installation of the self sealing coupling on the engine pump. (1) Remove the blanking cap on the engine pump. (2) Install the self sealing coupling on the engine pump. Refer to the applicable step (Ref. TASK 29-12-38-400-802).
R R
**ON A/C ALL
R
Subtask 12-36-29-865-179
R R R R R R R R R
D. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 11JB, 9JC, 12KS1, 12KS2, 13KS1, 13KS2 Subtask 12-36-29-611-199 E. Fill the Blue hydraulic reservoir (Ref. TASK 12-12-29-611-803) or (Ref. TASK 12-12-29-611-804). Subtask 12-36-29-863-081 F. Pressurize the Blue hydraulic reservoir (Ref. TASK 29-14-00-614-804). Subtask 12-36-29-410-153
R R
G. Close the fan cowl doors. FOR 4030EM1 - Close the door 415AL (Ref. TASK 71-13-00-410-803).
R EFF : ALL 12-36-29 SROS
Page A363 Jan 01/07
R R
Subtask 12-36-29-281-081 H. Sampling
R R
(1) Perform a fluid sampling for particular contamination (Ref. TASK 1232-29-281-801).
R R R R
(2) Perform in daily check, the check of the clogging indicators, of the case drain filters 5013JM, HP filters 5111JM101, 5111JM102 and the LP filter 5011JM1. Do this operation again until the clogging indicator stay in. 5. Close-up ________
R R R
Subtask 12-36-29-862-108 A. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862801). Subtask 12-36-29-860-207
R
B. Put the Aircraft back to its Initial Configuration
R
(1) Close the MLG doors (Ref. TASK 32-12-00-410-801).
R
(2) Make sure that the work area is clean and clear of tools and other items.
R
(3) Remove all the fixtures, tools, test and support equipment used during this procedure.
R EFF : ALL 12-36-29 SROS
Page A364 Jan 01/07
TASK 12-36-29-170-812 Flushing of the Suction line of the Yellow Hydraulic System. R R
WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS.
R R
WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY.
R R R R R
WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH.
R R R
CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific No specific No specific
circuit breaker(s) safety clip(s) warning notice container 70 l (18.4918 USgal)
R EFF : ALL 12-36-29 SROS
Page A365 Jan 01/07
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R R R R R R R R R R R R R R R R R R R R R R R R R
12-12-29-611-805 12-12-29-611-806 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-864-804 29-10-00-710-805 29-13-38-000-802 29-13-38-000-803 29-13-38-400-802 29-13-38-400-803 29-14-00-614-802 29-14-00-614-803 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 71-13-00-410-803 FOR FIN 4030EM2 71-13-00-010-803
Fill the Yellow Hydraulic Reservoir with a Hydraulic Service Cart Fill the Yellow Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Operational Test of the Electric Motor of the Engine Pump Suction Fire Shut-Off Valve Removal of the Yellow Hydraulic System Self-Sealing Coupling Removal of the Yellow Engine Pump Suction Self Sealing (Elbow) Coupling Installation of the Yellow Hydraulic System Self-Sealing Coupling Installation of the Yellow Engine Pump Suction Self Sealing (Elbow) Coupling Depressurization of the Blue Hydraulic Reservoir with Ground Equipment Depressurization of the Yellow Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Closing of the Fan Cowl Doors Opening of the Fan Cowl Doors
R EFF : ALL 12-36-29 SROS
Page A366 Jan 01/07
3. __________ Job Set-up R R
Subtask 12-36-29-860-208 A. Aircraft Maintenance Configuration
R R
(1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801).
R R R
(2) Make sure that the Yellow hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-804).
R R
(3) Depressurize the reservoir of the Yellow hydraulic system (Ref. TASK 29-14-00-614-803). Subtask 12-36-29-941-082
R
B. Safety Precautions (1) Make sure that the engine 1 and 2 shutdown occurred not less than 5 minutes before you do this procedure. (2) On the panel 225VU, make sure that the APU BLEED pushbutton switch is released (ON legend off) and install a warning notice to tell persons not to use it.
R
(3) Put a warning notice in position to tell persons not to pressurize the hydraulic system: - on the HYD/FUEL control panel 245VU in the cockpit - on the Yellow hydraulic system, access door ZAC 196BB.
R R R R R
(4) On the panel 125VU. - Make sure that the ENG MASTER switches for the two engines are in the OFF position. - Put a warning notice to tell persons not to supply power to the ECU.
R R R R R
(5) On the panel 285VU. - Make sure that the ON legend of the related ENG FADEC GND PWR pushbutton switch is off. - Put a warning notice to tell persons not to supply power to the FADEC system. (6) Put a container below the Yellow hydraulic engine pump.
EFF : ALL 12-36-29 SROS
Page A367 Jan 01/07
R R R R R R R R R R R R
Subtask 12-36-29-865-180 C. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------722VU FADEC B ENG 1 13KS1 D44 722VU FADEC B ENG 2 13KS2 K49 722VU HYD PUMP Y CTL 9JJ R36 722VU HYD PUMP Y ENG 2 12JY T46 742VU FADEC A ENG 2 12KS2 Q74 742VU FADEC A ENG 1 12KS1 Q73 Subtask 12-36-29-010-149
R
D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801).
R
(2) Open the fan cowl doors. FOR 4030EM2 - open the door 425AL (Ref. TASK 71-13-00-010-803).
R
4. Procedure _________ **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 12-36-29-860-209 A. Preparation before the flushing of the Suction Line. NOTE : Keep the suction line connect to the self sealing coupling. ____ (1) Disconnect the self-sealing coupling (5135JM) from the engine pump. Ref to the applicable step (Ref. TASK 29-13-38-000-803).
R
(2) Put blanking plug on the suction port of the hydraulic pump. R
R EFF : ALL 12-36-29 SROS
Page A368 Jan 01/07
**ON A/C 701-749, Subtask 12-36-29-860-209-A A. Preparation before the flushing of the Suction Line. NOTE : Keep the suction line connect to the self sealing coupling. ____ (1) Disconnect the self-sealing coupling (5135JM) from the engine pump. Ref to the applicable step (Ref. TASK 29-13-38-000-802).
R
(2) Put blanking plug on the suction port of the hydraulic pump. R
**ON A/C ALL
R
Subtask 12-36-29-170-097
R
B. Flushing of the Suction Line.
R
(1) Put the suction line in the container.
R R
(2) Pressurize the hydraulic reservoir (Ref. TASK 29-14-00-614-804) to flush the suction line until the FSOV close.
R
(3) Depressurize the hydraulic reservoir (Ref. TASK 29-14-00-614-802).
R
(4) On the panel 742VU, reset the C/B 5JR.
R R
(5) Do the operational test of the electrical motor of the FSOV (Ref. TASK 29-10-00-710-805).
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499,
R
Subtask 12-36-29-420-107
R
C. Installation of the self sealing coupling on the engine pump.
R
(1) Remove the blanking cap on the engine pump.
R R
(2) Install the self sealing coupling on the engine pump. Refer to the applicable step (Ref. TASK 29-13-38-400-803).
R EFF : ALL 12-36-29 SROS
Page A369 Jan 01/07
R
**ON A/C 701-749, Subtask 12-36-29-420-107-A
R
C. Installation of the self sealing coupling on the engine pump. (1) Remove the blanking cap on the engine pump. (2) Install the self sealing coupling on the engine pump. Refer to the applicable step (Ref. TASK 29-13-38-400-802).
R R
**ON A/C ALL
R
Subtask 12-36-29-865-181
R R R R R R R R R
D. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 9JJ, 12JY, 12KS1, 12KS2, 13KS1, 13KS2 Subtask 12-36-29-611-200 E. Fill the Yellow hydraulic reservoir (Ref. TASK 12-12-29-611-805) or (Ref. TASK 12-12-29-611-806). Subtask 12-36-29-863-082 F. Pressurize the Yellow hydraulic reservoir (Ref. TASK 29-14-00-614-804). Subtask 12-36-29-410-154
R R
G. Close the fan cowl doors. FOR 4030EM2 - Close the door 425AL (Ref. TASK 71-13-00-410-803).
R EFF : ALL 12-36-29 SROS
Page A370 Jan 01/07
R R
Subtask 12-36-29-281-082 H. Sampling
R R
(1) Perform a fluid sampling for particular contamination (Ref. TASK 1232-29-281-801).
R R R R
(2) Perform in daily check, the check of the clogging indicators, of the case drain filters 5013JM, HP filters 5111JM101, 5111JM102 and the LP filter 5011JM1. Do this operation again until the clogging indicator stay in. 5. Close-up ________
R R R
Subtask 12-36-29-862-109 A. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862801). Subtask 12-36-29-860-210
R
B. Put the Aircraft back to its Initial Configuration
R
(1) Close the MLG doors (Ref. TASK 32-12-00-410-801).
R
(2) Make sure that the work area is clean and clear of tools and other items.
R
(3) Remove all the fixtures, tools, test and support equipment used during this procedure.
R EFF : ALL 12-36-29 SROS
Page A371 Jan 01/07
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, TASK 12-36-29-611-801 Replacement of the Hydraulic Fluid of the Green Hydraulic System with a Fluid Replacement and Recovery Bench WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. CAUTION : DO NOT DEPRESSURIZE THE ENGINE PUMPS DURING THE DRY MOTORING. IF YOU _______ DO, YOU CAN CAUSE DAMAGE TO THE ENGINE PUMPS. 1. __________________ Reason for the Job You must replace the fluid only if the acidity is higher than the values given into the task of the sampling for analysis (Ref. TASK 12-32-29-281-80100).
EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page A372 Jan 01/07
2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific No specific No specific No specific AGE10600A DH0501
blanking plug circuit breaker(s) safety clip(s) hydraulic ground power supply plug type E0053R8B3APNE safety devices access platform 1.80 m (5 ft. 11 in.) 1 CHECK - MOTOR GROUND, RAT 1 TOOL - HYDRAULIC FLUID CHANGE
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 02-003
F NSA 307110 TYPE 4 HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------07-11-00-581-801 07-11-00-586-801 12-12-29-611-801 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-863-801 29-10-00-611-801 29-10-00-710-805
Lifting of the Aircraft for Maintenance Operations Lowering of the Aircraft for Maintenance Operations Fill the Green Hydraulic Reservoir with a Hydraulic Service Cart Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Pressurize the Green Hydraulic System with the Ground Hydraulic Supply Drainage of the Green Hydraulic Reservoir Operational Test of the Electric Motor of the Engine Pump Suction Fire Shut-Off Valve
EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page A373 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-11-43-600-802 29-11-44-600-801 29-11-45-600-801 29-14-00-614-801 29-14-00-614-804 29-24-00-720-801
29-24-00-869-802 32-00-00-481-802 32-11-15-400-801 32-12-00-010-801 32-12-00-410-801 32-22-00-010-801 32-30-00-867-801 32-30-00-867-802 32-42-00-710-801 32-42-00-870-801 32-42-12-000-801 32-42-12-400-801 32-51-00-860-801 71-00-00-720-816 78-31-00-710-804 12-36-29-991-094 12-36-29-991-061 12-36-29-991-063 12-36-29-991-062
Servicing of the (Forward) Engine-Pump Case-Drain Filter Element 5013JM1 Servicing of the Green Reservoir LP-Filter (5011JM1) Servicing of the Green HP Filter (5111JM101,5111JM102) Depressurization of the Green Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Operational Check of RAT Manual Deployment, Functional Check of RAT followed by Inspection of Filter Element by Ref. to Diff. Press.-Indicator (with ACMS) Retraction of the Ram Air Turbine (RAT) on the Ground Installation of the Safety Devices on the Landing Gear Doors Installation of the MLG Bogie-Alignment Pitch Trimmer (Weight on Wheels) Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Open the NLG Doors for Maintenance Retraction of the Landing Gear for Maintenance Extension of the Landing Gear After Maintenance Operational Test of the Normal Braking System Bleeding the Normal Braking System at the Wheel Brakes Removal of the Hydraulic Brake Filter (5200GG) Installation of the Hydraulic Brake Filter (5200GG) Put the Nose Wheels on Greased Plates for Nose Wheel Steering (NWS) Maintenance (A/C on Ground) Test No. 2 - Engine Motor Leak Test (Dry Method) Thrust Reverser Cowl Doors Open Thrust Reverser Cycling Test (MCDU) Fig. 325 Fig. 326 Fig. 327 Fig. 328
EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page A374 Jan 01/07
3. __________ Job Set-up Subtask 12-36-29-861-062 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). Subtask 12-36-29-860-147 B. Aircraft Maintenance Configuration (1) Pressurize the Green hydraulic system (Ref. TASK 29-00-00-863-801). (2) Set the flap and slat control lever on the panel 114VU to the position 1. (3) On the ECAM Engine/Warning Display, the indication 1+F comes into view. (4) On the HYD section of the maintenance panel 285VU, make sure that the LEAK MEASUREMENT VALVES/G pushbutton switch is pushed (the OFF legend is on). (5) On the Green HP manifold 5103JM, disconnect the pressure switches 7JS1 and 19CE1, and on the free end make a short circuit between the pins A and B with a plug type E0053R8B3APNE. (Ref. Fig. 325/TASK 12-36-29-991-094) Subtask 12-36-29-865-128 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------722VU HYD SOV ENG 2 NORM 19JG R34 722VU HYD SOV BUS SWTG 8JG R33 742VU HYD FIRE ENG 1 SOV 15JG2 D75 742VU HYD FIRE ENG 2 SOV 15JG1 D72
EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page A375 Jan 01/07
Manifolds of the Green Hydraulic System Figure 325/TASK 12-36-29-991-094 R EFF : ALL 12-36-29 SROS
Page A376 Jan 01/07
Subtask 12-36-29-010-108 D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Put an access platform at the zone 147. Subtask 12-36-29-680-056 E. Drain the reservoir of the Green hydraulic system (Ref. TASK 29-10-00611-801). Subtask 12-36-29-860-148 F. Set the hydraulic ground power supply to the correct configuration: (1) Make sure that the hydraulic ground power supply reservoir is filled with new HYDRAULIC FLUIDS (Material No. 02-003). (2) Make sure that no chlorinated solvent has been used to flush the tool lines. (3) Set the hydraulic ground power supply to the cart reservoir configuration. (4) Open the by-pass valve. (5) Start the hydraulic ground power supply. (6) Adjust the hydraulic ground power supply to the minimum pressure ( 20 bar (290.0754 psi) approx.) and to a flow of 45/lmn approx. and stop the hydraulic ground power supply. Subtask 12-36-29-860-149 G. Set the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the correct configuration. (Ref. Fig. 326/TASK 12-36-29-991-061, 327/TASK 12-36-29-991-063) NOTE : Make sure that the Green reservoir depressurization valve is open ____ when you set the hydraulic fluid replacement and recovery bench to the correct configuration. (1) On the fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501): - close the valve V1.
EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page A377 Jan 01/07
Connection of Tools to the Green Hydraulic System Figure 326/TASK 12-36-29-991-061- 12 (SHEET 1) EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page A378 Jan 01/07
Connection of Tools to the Green Hydraulic System Figure 326/TASK 12-36-29-991-061- 22 (SHEET 2) EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page A379 Jan 01/07
Green Hydraulic System-Schematic Diagram Figure 327/TASK 12-36-29-991-063- 12 (SHEET 1) EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page A380 Jan 01/07
Green Hydraulic System-Schematic Diagram Figure 327/TASK 12-36-29-991-063- 22 (SHEET 2) EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page A381 Jan 01/07
(2) Connect the connector LP1 of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the LP connector of the hydraulic ground power supply. (3) Connect the HP1 connector of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the HP connector of the hydraulic ground power supply. (4) Connect the LP3 connector of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the suction connector of the ground service panel. (5) On the HP manifold 5102JM: (a) Remove the Green HP filter 5111JM101 (Ref. TASK 29-11-45-600801). (b) Install a dummy bowl of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) in place of the Green HP filter 5111JM101. (c) Connect the HP2 line to the dummy bowl and to the valve V2. (6) On the LP filter 5011JM1: (a) Disconnect the tube (1) from the LP filter 5011JM1. (b) Put a blanking plug on the Green LP filter 5011JM1. (c) Loosen the tube (1) from the Green LP manifold 5004JM. (d) Turn the tube (1) 90 deg. and connect the LP2 line. (e) Tighten the tube (1) on the Green LP manifold 5004JM. (7) Start the hydraulic ground power supply and make sure that the pressure read on the gage of the hydraulic fluid replacement and recovery bench is 4 bar (58.0150 psi). (8) Stop the hydraulic ground power supply.
EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page A382 Jan 01/07
4. Procedure _________ (Ref. Fig. 327/TASK 12-36-29-991-063) Subtask 12-36-29-611-126 A. Fill the Green reservoir. (1) Open the depressurization valve of Green reservoir (Ref. TASK 29-1400-614-801). (2) Open the valve V1 of the TOOL - HYDRAULIC FLUID CHANGE (DH0501) and start the hydraulic ground power supply. (3) Fill the Green reservoir until the fluid is at the upper limit on the visual indicator (Ref. TASK 12-12-29-611-801). (4) Close the depressurization valve. (5) Pressurize the Green hydraulic reservoir (Ref. TASK 29-14-00-614804). (6) Close the valve V1. Subtask 12-36-29-865-148 B. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU L/G SAFETY VLV 3GA S12 722VU LGCIU 2 2GA U38 742VU LGCIU 1 1GA L63 Subtask 12-36-29-020-055 C. At the zone 148 disconnect the electrical connector of the safety valve 85GA . (Ref. Fig. 325/TASK 12-36-29-991-094) Subtask 12-36-29-865-149 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GA, 2GA, 3GA
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A383 Jan 01/07
Subtask 12-36-29-611-127 E. Replacement of the Fluid in the RAT Suction and Pressure Lines (1) Install the CHECK - MOTOR GROUND, RAT (AGE10600A). (2) Turn the RAT (Ref. TASK 29-24-00-720-801) (3) Monitor the reservoir level. (4) Stop the RAT if the advisory low level comes into view on the ECAM SD. (5) If necessary fill the Green hydraulic reservoir (Ref. TASK 12-12-29611-801). (6) Open the valve V2 until you collect 45 liters of fluid. (7) Close the valve V2. (8) Stop the RAT and retract it (Ref. TASK 29-24-00-869-802). Subtask 12-36-29-611-128 F. Replacement of the Fluid in the Engine Pump Suction and Pressure Lines (1) For 4030EM1 (a) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501) open the valve V1 and keep it open during the full procedure. (b) Dry motor the engine (Ref. TASK 71-00-00-720-816). NOTE : Stop the dry motoring if the advisory low level comes into ____ view on the ECAM System Display (SD). If necessary fill the Green hydraulic reservoir (Ref. TASK 12-12-29-611801). (c) Dry motor the engine (Ref. TASK 71-00-00-720-816). (d) Open the valve V2 until you collect 45 liters of fluid. (e) Close the valve V2. (f) Stop the dry motoring.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A384 Jan 01/07
(2) For 4030EM2 (a) Do the steps (a) thru (f) again. Subtask 12-36-29-611-129-A G. Replacement of the Fluid in the Suction, Pressure and Case Drain Lines of the Electric Pump (1JV) (1) Disconnect the case drain tube from the electric pump 1JV. (2) Put blanking plug on the end of the tube. (3) Connect the case drain elec hose of the TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the electric pump 1JV. (4) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501): - make sure that the valve V1 is open. (5) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV). (6) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501): - open the valve V2 until you collect 4 liters of fluid. (7) Close the valve V2. (8) On the HYD section of the overhead panel 245VU: - release the GREEN/ELEC/AUTO pushbutton switch (8JV). Subtask 12-36-29-611-130-A H. Replacement of the Fluid in the Thrust Reverser System (1) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV). (2) Do two deploy-to-stow cycles of the thrust reverser (Ref. TASK 78-3100-710-804). (3) On the HYD section of the overhead panel 245VU: - release the GREEN/ELEC/AUTO pushbutton switch (8JV). (4) Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 15JG1, 15JG2, 19JG, 8JG
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A385 Jan 01/07
(5) On the panel 255VU: - Push the ENG1/ENG2/FIRE pushbutton switch. (6) On the ECAM SD make sure that the fire shutoff valves are closed. Subtask 12-36-29-611-131-A J. Replacement of the Fluid in the Supply and Return Lines of the Primary Servocontrols (Ref. Fig. 328/TASK 12-36-29-991-062) (1) On the FLT CTL section of the overhead panel 212VU: - push the PRIM3 pushbutton switch. (2) On the FLT CTL section of the overhead panel 241VU: - push the PRIM1 and SEC1 pushbutton switches. (3) On the ground service manifold 5109JM1 open the valves which supply the right and left wing. (Ref. Fig. 325/TASK 12-36-29-991-094) (4) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV). (5) Do 5 operations over full travel range and make sure that the surfaces move. If they do not move, do the reset of the related computers. (6) On the HYD section of the overhead panel 245VU: - release the GREEN/ELEC/AUTO pushbutton switch (8JV). (7) On the ground service manifold 5109JM1 close the valves for the right and left wing and open the valve for the aft fuselage. (8) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV). (9) Operate the elevators over full travel range four times. (10) Operate the rudder over full travel range four times. (11) On the HYD section of the overhead panel 245VU: - release the GREEN/ELEC/AUTO pushbutton switch (8JV). (12) Close the valve for the aft fuselage.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A386 Jan 01/07
Flight Control Operations Figure 328/TASK 12-36-29-991-062 R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A387 Jan 01/07
Subtask 12-36-29-865-129 K. Make sure that this(these) circuit breaker(s) is(are) closed: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM 10CV X14 721VU SFCC 1 NORM AVAIL 10CW X13 722VU SFCC 2 FLAP 2CV T43 722VU SFCC 2 SLAT 2CW V40 742VU SFCC 1 SLAT 1CW L62 742VU SFCC 1 FLAP 1CV L61 Subtask 12-36-29-611-132-A L. Replacement of the Fluid in the Flap and Slat Supply and Return Systems (1) Make sure that the flap and slat control lever on the panel 114VU is in the position 1. (2) On the ground service manifold 5109JM1 open the valves which supply the right and left wing. (3) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV). (4) Set the flap and slat control lever on the panel 114VU to the position 2. (5) On the HYD section of the overhead panel 245VU: - release the GREEN/ELEC/AUTO pushbutton switch (8JV). (6) On the ground service manifold 5109JM1 close the valves which supply the right and left wing. Subtask 12-36-29-611-133 M. Replacement of the Fluid in the Normal Braking System (1) Push and release the brake pedals one time (Ref. TASK 32-42-00-710801). (2) Replace the hydraulic brake filter 5200GG on the manifold 5105JM (Ref. TASK 32-42-12-000-801) and (Ref. TASK 32-42-12-400-801). (3) Push and release the brake pedals 5 times.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A388 Jan 01/07
Subtask 12-36-29-611-134-A N. Replacement of the Fluid in the Nose Wheel Steering System (1) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV). (2) Operate the nose wheel steering over full travel 2 times (Ref. TASK 32-51-00-860-801). (3) On the HYD section of the overhead panel 245VU: - release the GREEN/ELEC/AUTO pushbutton switch (8JV). Subtask 12-36-29-865-150 P. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU L/G SAFETY VLV 3GA S12 722VU LGCIU 2 2GA U38 742VU LGCIU 1 1GA L63 Subtask 12-36-29-420-088 Q. At the zone 148 connect the electrical connector of the safety valve 85GA. (Ref. Fig. 325/TASK 12-36-29-991-094) Subtask 12-36-29-865-151 R. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GA, 2GA, 3GA Subtask 12-36-29-611-135-A S. Replacement of the Fluid in the Landing Gear Door System (1) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV). (2) Do 3 opening cycles of the NLG doors (Ref. TASK 32-22-00-010-801). (3) Do 3 opening cycles of the right MLG doors (Ref. TASK 32-12-00-010801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A389 Jan 01/07
(4) Do 3 opening cycles of the left MLG doors (Ref. TASK 32-12-00-010801). (5) On the HYD section of the overhead panel 245VU: - release the GREEN/ELEC/AUTO pushbutton switch (8JV). (6) Install safety devices on the landing gear door actuators (Ref. TASK 32-00-00-481-802). Subtask 12-36-29-611-136 T. Replacement of the Fluid in the Landing Gear System (1) Lift the aircraft on jacks (Ref. TASK 07-11-00-581-801). (2) Start with the NLG and do 2 extension/retraction operations of the landing gear (Ref. TASK 32-30-00-867-801) and (Ref. TASK 32-30-00867-802). (3) Lower the aircraft (Ref. TASK 07-11-00-586-801). 5. Close-up ________ Subtask 12-36-29-420-080 A. Replace these hydraulic filters: - the HP filter 5111JM102 (Ref. TASK 29-11-45-600-801) - the LP filter 5011JM1 (Ref. TASK 29-11-44-600-801) - the two case drain filters 5013JM1 (Ref. TASK 29-11-43-600-802). Subtask 12-36-29-942-086 B. Aircraft Maintenance Configuration (1) On the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/G pushbutton switch (the OFF legend is off). (2) On the Green HP manifold 5103JM, remove the plug type E0053R8B3APNE from the pressure switches 7JS1 and 19CE1 and connect the pressure switches 7JS1 and 19CE1. (3) On the panel 255VU: - release the ENG1/ENG2 FIRE pushbutton switch. (4) If the engine pump suction fire shut-off valves do not open, do a reset of the C/B 5JR.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A390 Jan 01/07
(5) Do the operational test of the electric motors of the engine pump suction fire shut-off valves (2JG1) and (2JG2) (Ref. TASK 29-10-00710-805). (6) Do the bleeding of the normal braking system (Ref. TASK 32-42-00-870801). (7) Do the bleeding of the pitch trimmer (Ref. TASK 32-11-15-400-801). (8) Close the valves V1 and V2 on the recovery bench. (9) Disconnect all the lines between the aircraft and the recovery bench. (10) Disconnect all the lines between the recovery bench and the hydraulic ground power supply. (11) Replace the MP hydraulic filter 5111JM101 (Ref. TASK 29-11-45-600801). (12) Pressurize the Green hydraulic reservoir (Ref. TASK 29-14-00-614804). (13) Operate the flight controls and monitor the reservoir level. If necessary fill the Green hydraulic reservoir (Ref. TASK 12-12-29-611801). (14) Each week, do a new sampling of the fluid (Ref. TASK 12-32-29-281801). Subtask 12-36-29-942-087 C. Remove the safety precautions. (1) Remove the warning notice(s). Subtask 12-36-29-410-107 D. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Remove the access platform(s). (3) Close the landing gear doors (Ref. TASK 32-12-00-410-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A391 Jan 01/07
Subtask 12-36-29-862-092 E. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page A392 Jan 01/07
**ON A/C 701-749, TASK 12-36-29-611-801-A Replacement of the Hydraulic Fluid of the Green Hydraulic System with a Fluid Replacement and Recovery Bench WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. CAUTION : DO NOT DEPRESSURIZE THE ENGINE PUMPS DURING THE DRY MOTORING. IF YOU _______ DO, YOU CAN CAUSE DAMAGE TO THE ENGINE PUMPS. 1. __________________ Reason for the Job You must replace the fluid only if the acidity is higher than the values given into the task of the sampling for analysis (Ref. TASK 12-32-29-281-80100).
R EFF : 701-749, 12-36-29 SROS
Page A393 Jan 01/07
2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific No specific No specific No specific AGE10600A DH0501
blanking plug circuit breaker(s) safety clip(s) hydraulic ground power supply plug type E0053R8B3APNE safety devices access platform 1.80 m (5 ft. 11 in.) 1 CHECK - MOTOR GROUND, RAT 1 TOOL - HYDRAULIC FLUID CHANGE
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 02-003
F NSA 307110 TYPE 4 HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------07-11-00-581-801 07-11-00-586-801 12-12-29-611-801 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-863-801 29-10-00-611-801 29-10-00-710-805
Lifting of the Aircraft for Maintenance Operations Lowering of the Aircraft for Maintenance Operations Fill the Green Hydraulic Reservoir with a Hydraulic Service Cart Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Pressurize the Green Hydraulic System with the Ground Hydraulic Supply Drainage of the Green Hydraulic Reservoir Operational Test of the Electric Motor of the Engine Pump Suction Fire Shut-Off Valve
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-11-43-600-807 29-11-44-600-801 29-11-45-600-801 29-14-00-614-801 29-14-00-614-804 29-24-00-720-801
29-24-00-869-802 32-00-00-481-802 32-11-15-400-801 32-12-00-010-801 32-12-00-410-801 32-22-00-010-801 32-30-00-867-801 32-30-00-867-802 32-42-00-710-801 32-42-00-870-801 32-42-12-000-801 32-42-12-400-801 32-51-00-860-801 71-00-00-720-828 78-31-00-740-802 12-36-29-991-094 12-36-29-991-064 12-36-29-991-066 12-36-29-991-065
Servicing of the Engine-Pump Case Drain Filter (5013JM1) Servicing of the Green Reservoir LP-Filter (5011JM1) Servicing of the Green HP Filter (5111JM101,5111JM102) Depressurization of the Green Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Operational Check of RAT Manual Deployment, Functional Check of RAT followed by Inspection of Filter Element by Ref. to Diff. Press.-Indicator (with ACMS) Retraction of the Ram Air Turbine (RAT) on the Ground Installation of the Safety Devices on the Landing Gear Doors Installation of the MLG Bogie-Alignment Pitch Trimmer (Weight on Wheels) Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Open the NLG Doors for Maintenance Retraction of the Landing Gear for Maintenance Extension of the Landing Gear After Maintenance Operational Test of the Normal Braking System Bleeding the Normal Braking System at the Wheel Brakes Removal of the Hydraulic Brake Filter (5200GG) Installation of the Hydraulic Brake Filter (5200GG) Put the Nose Wheels on Greased Plates for Nose Wheel Steering (NWS) Maintenance (A/C on Ground) Dry Motoring Engine Test of the Thrust Reverser Deployment and Stowage (Engine not Running) Fig. 325 Fig. 329 Fig. 330 Fig. 331
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3. __________ Job Set-up Subtask 12-36-29-861-065 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). Subtask 12-36-29-860-156 B. Aircraft Maintenance Configuration (1) Pressurize the Green hydraulic system (Ref. TASK 29-00-00-863-801). (2) Set the flap and slat control lever on the panel 114VU to the position 1. (3) On the ECAM Engine/Warning Display, the indication 1+F comes into view. (4) On the HYD section of the maintenance panel 285VU, make sure that the LEAK MEASUREMENT VALVES/G pushbutton switch is pushed (the OFF legend is on). (5) On the Green HP manifold 5103JM, disconnect the pressure switches 7JS1 and 19CE1, and on the free end make a short circuit between the pins A and B with a plug type E0053R8B3APNE. (Ref. Fig. 325/TASK 12-36-29-991-094) Subtask 12-36-29-865-134 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------722VU HYD SOV ENG 2 NORM 19JG R34 722VU HYD SOV BUS SWTG 8JG R33 742VU HYD FIRE ENG 1 SOV 15JG2 D75 742VU HYD FIRE ENG 2 SOV 15JG1 D72
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Subtask 12-36-29-010-111 D. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Put an access platform at the zone 147. Subtask 12-36-29-680-059 E. Drain the reservoir of the Green hydraulic system (Ref. TASK 29-10-00611-801). Subtask 12-36-29-860-157 F. Set the hydraulic ground power supply to the correct configuration: (1) Make sure that the hydraulic ground power supply reservoir is filled with new HYDRAULIC FLUIDS (Material No. 02-003). (2) Make sure that no chlorinated solvent has been used to flush the tool lines. (3) Set the hydraulic ground power supply to the cart reservoir configuration. (4) Open the by-pass valve. (5) Start the hydraulic ground power supply. (6) Adjust the hydraulic ground power supply to the minimum pressure ( 20 bar (290.0754 psi) approx.) and to a flow of 45/lmn approx. and stop the hydraulic ground power supply. Subtask 12-36-29-860-158 G. Set the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the correct configuration. (Ref. Fig. 329/TASK 12-36-29-991-064, 330/TASK 12-36-29-991-066) NOTE : Make sure that the Green reservoir depressurization valve is open ____ when you set the hydraulic fluid replacement and recovery bench to the correct configuration. (1) On the fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501): - close the valve V1.
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Connection of the Tools to the Green Hydraulic System Figure 329/TASK 12-36-29-991-064- 12 (SHEET 1) EFF : 701-749, 12-36-29 R SROS
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Connection of the Tools to the Green Hydraulic System Figure 329/TASK 12-36-29-991-064- 22 (SHEET 2) EFF : 701-749, 12-36-29 R SROS
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Green Hydraulic System-Schematic Diagram Figure 330/TASK 12-36-29-991-066- 12 (SHEET 1) EFF : 701-749, 12-36-29 R SROS
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Green Hydraulic System-Schematic Diagram Figure 330/TASK 12-36-29-991-066- 22 (SHEET 2) EFF : 701-749, 12-36-29 R SROS
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(2) Connect the connector LP1 of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the LP connector of the hydraulic ground power supply. (3) Connect the HP1 connector of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the HP connector of the hydraulic ground power supply. (4) Connect the LP3 connector of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the suction connector of the ground service panel. (5) On the HP manifold 5102JM (a) Remove the Green HP filter 5111JM101 (Ref. TASK 29-11-45-600801). (b) Install a dummy bowl of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) in place of the Green HP filter 5111JM101. (c) Connect the HP2 line to the dummy bowl and to the valve V2. (6) On the LP filter 5011JM1: (a) Disconnect the tube (1) from the LP filter 5011JM1. (b) Put a blanking plug on the Green LP filter 5011JM1. (c) Loosen the tube (1) from the Green LP manifold 5004JM. (d) Turn the tube (1) 90 deg. and connect the LP2 line. (e) Tighten the tube (1) on the Green LP manifold 5004JM. (7) Start the hydraulic ground power supply and make sure that the pressure read on the gage of the hydraulic fluid replacement and recovery bench is 4 bar (58.0150 psi). (8) Stop the hydraulic ground power supply.
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4. Procedure _________ (Ref. Fig. 330/TASK 12-36-29-991-066) Subtask 12-36-29-611-152 A. Fill the Green reservoir. (1) Open the depressurization valve of Green reservoir (Ref. TASK 29-1400-614-801). (2) Open the valve V1 of the TOOL - HYDRAULIC FLUID CHANGE (DH0501) and start the hydraulic ground power supply. (3) Fill the Green reservoir until the fluid is at the upper limit on the visual indicator (Ref. TASK 12-12-29-611-801). (4) Close the depressurization valve of Green reservoir. (5) Pressurize the Green hydraulic reservoir (Ref. TASK 29-14-00-614804). (6) Close the valve V1. Subtask 12-36-29-865-152 B. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU L/G SAFETY VLV 3GA S12 722VU LGCIU 2 2GA U38 742VU LGCIU 1 1GA L63 Subtask 12-36-29-020-056 C. At the zone 148 disconnect the electrical connector of the safety valve 85GA. (Ref. Fig. 325/TASK 12-36-29-991-094) Subtask 12-36-29-865-153 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GA, 2GA, 3GA
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Subtask 12-36-29-611-153 E. Replacement of the Fluid in the RAT Suction and Pressure Lines (1) Install the CHECK - MOTOR GROUND, RAT (AGE10600A). (2) Turn the RAT (Ref. TASK 29-24-00-720-801). (3) Monitor the reservoir level. (4) Stop the RAT if the advisory low level comes into view on the ECAM SD. (5) If necessary fill the Green hydraulic reservoir (Ref. TASK 12-12-29611-801). (6) Open the valve V2 until you collect 45 liters of fluid. (7) Close the valve V2. (8) Stop the RAT and retract it (Ref. TASK 29-24-00-869-802). Subtask 12-36-29-611-154 F. Replacement of the Fluid in the Engine Pump Suction and Pressure Lines (1) For 4030EM1 (a) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501) open the valve V1 and keep it open during the full procedure. (b) Dry motor the engine (Ref. TASK 71-00-00-720-828). NOTE : Stop the dry motoring if the advisory low level comes into ____ view on the ECAM System Display (SD). If necessary fill the Green hydraulic reservoir (Ref. TASK 12-12-29-611801). (c) Dry motor the engine (Ref. TASK 71-00-00-720-828). (d) Open the valve V2 until you collect 45 filters of fluid. (e) Close the valve V2. (f) Stop the dry motoring.
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(2) For 4030EM2 (a) Do the steps (a) thru (f) again. Subtask 12-36-29-611-155 G. Replacement of the Fluid in the Suction, Pressure and Case Drain Lines of the Electric Pump (1JV) (1) Disconnect the case drain tube from the electric pump (1JV). (2) Put blanking plug on the end of the tube. (3) Connect the case drain elec hose of the TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the electric pump (1JV). (4) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501): - make sure that the valve V1 is open. (5) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV). (6) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501): - open the valve V2 until you collect 4 liters of fluid. (7) Close the valve V2. (8) On the HYD section of the overhead panel 245VU: - release the GREEN/ELEC/AUTO pushbutton switch (8JV). Subtask 12-36-29-611-156 H. Replacement of the Fluid in the Thrust Reverser System (1) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV). (2) Do two deploy-to-stow cycles of the thrust reverser (Ref. TASK 78-3100-740-802). (3) On the HYD section of the overhead panel 245VU: - release the GREEN/ELEC/AUTO pushbutton switch (8JV). (4) Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 15JG1, 15JG2, 19JG, 8JG.
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(5) On the panel 255VU: Push the ENG1/ENG2/FIRE pushbutton switch. (6) On the ECAM SD make sure that the fire shutoff valves are closed. Subtask 12-36-29-611-157 J. Replacement of the Fluid in the Supply and Return Lines of the Primary Servocontrols (Ref. Fig. 331/TASK 12-36-29-991-065) (1) On the FLT CTL section of the overhead panel 212VU: - push the PRIM3 pushbutton switch. (2) On the FLT CTL section of the overhead panel 241VU: - push the PRIM1 and SEC1 pushbutton switches. (3) On the ground service manifold 5109JM1 open the valves which supply the right and left wing. (Ref. Fig. 325/TASK 12-36-29-991-094) (4) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV). (5) Do 5 operations over full travel range and make sure that the surfaces move. If they do not move, do the reset of the related computers. (6) On the HYD section of the overhead panel 245VU: - release the GREEN/ELEC/AUTO pushbutton switch (8JV). (7) On the ground service manifold 5109JM1 close the valves for the right and left wing and open the valve for the aft fuselage. (8) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV). (9) Operate the elevators over full travel range four times. (10) Operate the rudder over full travel range four times. (11) On the HYD section of the overhead panel 245VU: - release the GREEN/ELEC/AUTO pushbutton switch (8JV). (12) Close the valve for the aft fuselage.
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Flight Control Operations Figure 331/TASK 12-36-29-991-065 R EFF : 701-749, 12-36-29 SROS
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Subtask 12-36-29-865-135 K. Make sure that this(these) circuit breaker(s) is(are) closed: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM 10CV X14 721VU SFCC 1 NORM AVAIL 10CW X13 722VU SFCC 2 FLAP 2CV T43 722VU SFCC 2 SLAT 2CW V40 742VU SFCC 1 SLAT 1CW L62 742VU SFCC 1 FLAP 1CV L61 Subtask 12-36-29-611-158 L. Replacement of the Fluid in the Flap and Slat Supply and Return Systems (1) Make sure that the flap and slat control lever on the panel 114VU is in the position 1. (2) On the ground service manifold 5109JM1 open the valves which supply the right and left wing. (3) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV). (4) Set the flap and slat control lever on the panel 114VU to the position 2. (5) On the HYD section of the overhead panel 245VU: - release the GREEN/ELEC/AUTO pushbutton switch (8JV). (6) On the ground service manifold 5109JM1 close the valves which supply the right and left wing. Subtask 12-36-29-611-159 M. Replacement of the Fluid in the Normal Braking System (1) Push and release the brake pedals one time (Ref. TASK 32-42-00-710801). (2) Replace the hydraulic brake filter 5200GG on the manifold 5105JM (Ref. TASK 32-42-12-000-801) and (Ref. TASK 32-42-12-400-801). (3) Push and release the brake pedals 5 times.
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Subtask 12-36-29-611-160 N. Replacement of the Fluid in the Nose Wheel Steering System (1) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV). (2) Operate the nose wheel steering over full travel 2 times (Ref. TASK 32-51-00-860-801). (3) On the HYD section of the overhead panel 245VU: - release the GREEN/ELEC/AUTO pushbutton switch (8JV). Subtask 12-36-29-865-154 P. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU L/G SAFETY VLV 3GA S12 722VU LGCIU 2 2GA U38 742VU LGCIU 1 1GA L63 Subtask 12-36-29-420-089 Q. At the zone 148 connect the electrical connector of the safety valve 85GA. (Ref. Fig. 325/TASK 12-36-29-991-094) Subtask 12-36-29-865-155 R. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GA, 2GA, 3GA Subtask 12-36-29-611-161 S. Replacement of the Fluid in the Landing Gear Door System (1) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV). (2) Do 3 opening cycles of the NLG doors (Ref. TASK 32-22-00-010-801). (3) Do 3 opening cycles of the right MLG doors (Ref. TASK 32-12-00-010801).
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(4) Do 3 opening cycles of the left MLG doors (Ref. TASK 32-12-00-010801). (5) On the HYD section of the overhead panel 245VU: - release the GREEN/ELEC/AUTO pushbutton switch (8JV). (6) Install safety devices on the landing gear door actuators (Ref. TASK 32-00-00-481-802). Subtask 12-36-29-611-162 T. Replacement of the Fluid in the Landing Gear System (1) Lift the aircraft on jacks (Ref. TASK 07-11-00-581-801). (2) Start with the NLG and do 2 extension/retraction operations of the landing gear (Ref. TASK 32-30-00-867-801) and (Ref. TASK 32-30-00867-802). (3) Lower the aircraft (Ref. TASK 07-11-00-586-801). 5. Close-up ________ Subtask 12-36-29-420-083 A. Replace these hydraulic filters: - the HP filter 5111JM102 (Ref. TASK 29-11-45-600-801), - the LP filter 5011JM1 (Ref. TASK 29-11-44-600-801), - the two case drain filters 5013JM1 (Ref. TASK 29-11-43-600-807). Subtask 12-36-29-942-092 B. Aircraft Maintenance Configuration (1) On the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/G pushbutton switch (the OFF legend is off). (2) On the Green HP manifold 5103JM, remove the plug type E0053R8B3APNE from the pressure switches 7JS1 and 19CE1 and connect the pressure switches 7JS1 and 19CE1. (3) On the panel 255VU: - release the ENG1/ENG2/FIRE pushbutton switch. (4) If the engine pump suction fire shut-off valves do not open, do a reset of the C/B 5JR.
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(5) Do the operational test of the electric motors of the engine pump suction fire shut-off valves (2JG1) and (2JG2) (Ref. TASK 29-10-00710-805). (6) Do the bleeding of the normal braking system (Ref. TASK 32-42-00-870801). (7) Do the bleeding of the pitch trimmer (Ref. TASK 32-11-15-400-801). (8) Close the valves V1 and V2 on the recovery bench. (9) Disconnect all the lines between the aircraft and the recovery bench. (10) Disconnect all the lines between the recovery bench and the hydraulic ground power supply. (11) Replace the HP hydraulic filter 5111JM101 (Ref. TASK 29-11-45-600801). (12) Pressurize the Green hydraulic reservoir (Ref. TASK 29-14-00-614804). (13) Operate the flight controls and monitor the reservoir level. If necessary fill the Green hydraulic reservoir (Ref. TASK 12-12-29-611801). (14) Each week, do a new sampling of the fluid (Ref. TASK 12-32-29-281801). Subtask 12-36-29-942-093 C. Remove the safety precautions. (1) Remove the warning notice(s). Subtask 12-36-29-410-110 D. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Remove the access platform(s). (3) Close the landing gear doors (Ref. TASK 32-12-00-410-801).
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Subtask 12-36-29-862-095 E. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
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**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, TASK 12-36-29-611-802 Replacement of the Hydraulic Fluid of the Blue Hydraulic System with a Fluid Replacement and Recovery Bench WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. CAUTION : DO NOT DEPRESSURIZE THE ENGINE PUMPS DURING THE DRY MOTORING. IF YOU _______ DO, YOU CAN CAUSE DAMAGE TO THE ENGINE PUMPS. 1. __________________ Reason for the Job You must replace the fluid only if the acidity is higher than the values given into the task of the sampling for analysis (Ref. TASK 12-32-29-281-80100).
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2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific No specific No specific DH0501
blanking plug hydraulic ground power supply plug type E0053R8B3APNE access platform 1.8 m (5 ft. 11 in.) access platform 1.80 m (5 ft. 11 in.) 1 TOOL - HYDRAULIC FLUID CHANGE
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 02-003
F NSA 307110 TYPE 4 HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-803 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-863-801 29-10-00-611-802 29-10-00-710-805 29-11-43-600-804 29-12-44-600-801 29-12-45-600-801
Fill the Blue Hydraulic Reservoir with a Hydraulic Service Cart Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Pressurize the Green Hydraulic System with the Ground Hydraulic Supply Drainage of the Blue Hydraulic Reservoir Operational Test of the Electric Motor of the Engine Pump Suction Fire Shut-Off Valve Servicing of the (Aft) Engine-Pump Case-Drain Filter Element 5013JM2 Servicing of the Blue Reservoir LP-Filter (5011JM2) Servicing of the Blue HP Filter (5111JM2)
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-14-00-614-802 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 32-43-00-870-801 32-45-00-864-801 71-00-00-720-816 78-31-00-710-804 12-36-29-991-095 12-36-29-991-070 12-36-29-991-072 12-36-29-991-071
Depressurization of the Blue Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Bleeding the Alternate Braking System at the Wheel Brakes Release the Pressure from the Parking Brake System after Depressurization Test No. 2 - Engine Motor Leak Test (Dry Method) Thrust Reverser Cowl Doors Open Thrust Reverser Cycling Test (MCDU) Fig. 332 Fig. 333 Fig. 334 Fig. 335
3. __________ Job Set-up Subtask 12-36-29-861-063 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). Subtask 12-36-29-860-150 B. Aircraft Maintenance Configuration (1) Pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-801). (2) Set the flap and slat control lever on the panel 114VU to the position 1. (3) On the ECAM engine/warning display the indication 1+F comes into view. (4) On the HYD section of the maintenance panel 285VU, make sure that the LEAK MEASUREMENT VALVES/B pushbutton switch is pushed (the OFF legend is on).
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(5) On the Blue HP manifold 6103JM, disconnect the pressure switches 7JS2 and 19CE2, and on the free end make a short circuit between the pin A and B with an plug type E0053R8B3APNE. (Ref. Fig. 332/TASK 12-36-29-991-095) Subtask 12-36-29-010-109-A C. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Put an access platform at the zone 147. (3) Put an access platform in position at the zone 195. (4) Remove the access panel 195CB. Subtask 12-36-29-680-057 D. Drain the reservoir of the Blue hydraulic system (Ref. TASK 29-10-00-611802). Subtask 12-36-29-860-151 E. Set the hydraulic ground power supply to the correct configuration: (1) Make sure that the hydraulic ground power supply reservoir is filled with new HYDRAULIC FLUIDS (Material No. 02-003). (2) Make sure that no chlorinated solvent has been used to flush the tool lines. (3) Set the hydraulic ground power supply to the cart reservoir configuration. (4) Open the by-pass valve. (5) Start the hydraulic ground power supply. (6) Adjust the hydraulic ground power supply to the minimum pressure (20 bar (290.0754 psi) approx.) and to a flow of 45/lmn approx. and stop the hydraulic ground power supply.
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Manifolds of the Blue Hydraulic System Figure 332/TASK 12-36-29-991-095 R EFF : ALL 12-36-29 SROS
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Subtask 12-36-29-860-152 F. Set the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the correct configuration. (Ref. Fig. 333/TASK 12-36-29-991-070, 334/TASK 12-36-29-991-072) NOTE : Make sure that the Blue reservoir depressurization valve is open ____ when you set the hydraulic fluid replacement and recovery bench to the correct configuration. (1) On the fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501): - close the valve V1. (2) Connect the connector LP1 of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the LP connector of the hydraulic ground power supply. (3) Connect the HP1 connector of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the HP connector of the hydraulic ground power supply. (4) connect the LP3 connector of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the suction connector of the ground service panel. (5) On the HP manifold 6103JM: (a) Remove the Blue HP filter 5111JM2 (Ref. TASK 29-12-45-600-801). (b) Install a dummy bowl of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) in place of the Blue HP filter 5111JM2. (c) Connect the HP2 line to the dummy bowl and to the valve V2. (6) On the LP filter 5011JM2: (a) Disconnect the flexible hose (1) from the Blue LP manifold 6005JM, and connect the LP2 line. (7) Put a blanking plug on the Blue LP filter 5011JM2. (8) Start the hydraulic ground power supply and make sure that the pressure read on the gage of the hydraulic fluid replacement and recovery bench is 4 bar (58.0150 psi).
EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page B318 Jan 01/07
INTENTIONALLY BLANK
R 12-36-29 SROS
Page B319 Jan 01/07
Connections of Tools to the Blue Hydraulic System Figure 333/TASK 12-36-29-991-070- 12 (SHEET 1) EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page B320 Jan 01/07
Connections of Tools to the Blue Hydraulic System Figure 333/TASK 12-36-29-991-070- 22 (SHEET 2) R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B321 Jan 01/07
Blue Hydraulic System-Schematic Diagram Figure 334/TASK 12-36-29-991-072- 12 (SHEET 1) R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B322 Jan 01/07
Blue Hydraulic System-Schematic Diagram Figure 334/TASK 12-36-29-991-072- 22 (SHEET 2) R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B323 Jan 01/07
(9) Stop the hydraulic ground power supply. 4. Procedure _________ (Ref. Fig. 334/TASK 12-36-29-991-072) Subtask 12-36-29-611-137 A. Fill the Blue reservoir. (1) Open the depressurization valve of Blue reservoir (Ref. TASK 29-1400-614-802). (2) Open the valve V1 of the TOOL - HYDRAULIC FLUID CHANGE (DH0501) and start the hydraulic ground power supply. (3) Fill the Blue reservoir until the fluid is at the upper limit on the visual indicator (Ref. TASK 12-12-29-611-803). (4) Close the depressurization valve of Blue reservoir. (5) Pressurize the Blue hydraulic reservoir (Ref. TASK 29-14-00-614-804). (6) Close the valve V1. Subtask 12-36-29-611-138 B. Replacement of the Fluid in the Engine Pump Suction and Pressure Lines (1) For 4030EM1 (a) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501) open the valve V1 and keep it open during the full procedure. (b) Dry motor the engine (Ref. TASK 71-00-00-720-816). NOTE : Stop the dry motoring if the advisory low level comes into ____ view on the ECAM SYSTEM DISPLAY. If necessary fill the Blue hydraulic reservoir (Ref. TASK 12-12-29-611-803). (c) Dry motor the engine (Ref. TASK 71-00-00-720-816). (d) Open the valve V2 until you collect 40 liters of fluid. (e) Close the valve V2. (f) Stop the dry motoring.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B324 Jan 01/07
Subtask 12-36-29-611-139 C. Replacement of the Fluid in the Suction, Pressure and Case Drain Lines of the Electric Pump (1JC) (1) Disconnect the case drain tube from the electric pump (1JC). (2) Put blanking plug on the end of the tube. (3) Connect the case drain elec hose of the TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the electric pump (1JC). (4) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501): - make sure that the valve V1 is open. (5) On the HYD section of the overhead panel 245VU: - push the BLUE/ELEC pushbutton switch (4JC). (6) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501): - open the valve V2 until you collect 4 liters of fluid. (7) Close the valve V2. (8) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC). Subtask 12-36-29-611-140 D. Replacement of the Fluid in the Alternate Brake Accumulators (1) On the manifold 5401GG depressurize the brake accumulators (Ref. TASK 32-45-00-864-801). Subtask 12-36-29-611-141 E. Replacement of the Fluid in the Thrust Reverser System (1) On the HYD section of the overhead panel 245VU: - push the BLUE/ELEC pushbutton switch (4JC). (2) Do two deploy-to-stow cycles of the thrust reverser (Ref. TASK 78-3100-710-804) . (3) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B325 Jan 01/07
(4) On the panel 255VU: - Push the ENG1/FIRE pushbutton switch. On the ECAM SD make sure that the fire shutoff valve is closed. Subtask 12-36-29-611-142 F. Replacement of the Fluid in the Supply and Return Lines of the Primary Servocontrols (Ref. Fig. 335/TASK 12-36-29-991-071) (1) On the FLT CTL section of the overhead panel 212VU: - push the SEC2, PRIM2 and PRIM3 pushbutton switches. (2) On the ground service manifold 5109JM2 open the valves which supply the right and left wing. (Ref. Fig. 332/TASK 12-36-29-991-095) (3) On the HYD section of the overhead panel 245VU: - push the BLUE/ELEC pushbutton switch (4JC). (4) Do 5 operations over full travel range and make sure that the surfaces move. If they do not move, do the reset of the related computers. (5) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC). (6) On the ground service manifold 5109JM2 close the valves for the right and left wing and open the valve for the aft fuselage. (7) On the HYD section of the overhead panel 245VU: - push the BLUE/ELEC pushbutton switch (4JC). (8) Operate the elevators over full travel range four times. (9) Operate the rudder over full travel range four times. (10) Operate the THS until you collect 5 liters of fluid. (11) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC). (12) Close the valve for the aft fuselage.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B326 Jan 01/07
Flight Control Operations Figure 335/TASK 12-36-29-991-071 R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B327 Jan 01/07
Subtask 12-36-29-865-131 G. Make sure that this(these) circuit breaker(s) is(are) closed: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM AVAIL 10CW X13 722VU SFCC 2 SLAT 2CW V40 742VU SFCC 1 SLAT 1CW L62 Subtask 12-36-29-611-143 H. Replacement of the Fluid in the Flap and Slat Supply and Return Systems (1) Make sure that the flap and slat control lever on the panel 114VU is in the position 1. (2) On the ground service manifold 5109JM2 open the valves which supply the right and left wing. (3) On the HYD section of the overhead panel 245VU: - push the BLUE/ELEC pushbutton switch (4JC). (4) Set the flap and slat control lever on the panel 114VU to the position 2. (5) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC). (6) On the ground service manifold 5109JM2 close the valves which supply the right and left wing. Subtask 12-36-29-611-144 J. Replacement of the Fluid in the Alternate Braking System (1) On the panel 312VU, set the PARK BRK switch to the OFF position. (2) On the HYD section of the overhead panel 245VU: - push the BLUE/ELEC pushbutton switch (4JC). (3) Push and release the brake pedals five times. (4) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B328 Jan 01/07
5. Close-up ________ Subtask 12-36-29-420-081 A. Replace these hydraulic filters: - the LP filter 5011JM2 (Ref. TASK 29-12-44-600-801) - the case drain filter 5013JM2 (Ref. TASK 29-11-43-600-804). Subtask 12-36-29-942-088 B. Aircraft Maintenance Configuration (1) On the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/B pushbutton switch (the OFF legend is off). (2) On the Blue HP manifold 6103JM, remove the plug type E0053R8B3APNE from the pressure switches 7JS2 and 19CE2 and connect the pressure switches 7JS2 and 19CE2. (3) On the panel 255VU: - release the ENG2/FIRE pushbutton switch. (4) Do the operational test of the electric motor of the engine pump suction fire shut-off valve (4JB) (Ref. TASK 29-10-00-710-805). (5) Do the bleeding of the alternate brake system (Ref. TASK 32-43-00870-801). (6) Close the valves V1 and V2 on the recovery bench. (7) Disconnect all the lines between the aircraft and the recovery bench. (8) Disconnect all the lines between the recovery bench and the hydraulic ground power supply. (9) Replace the HP hydraulic filter 5111JM2 (Ref. TASK 29-12-45-600-801). (10) Pressurize the Blue hydraulic reservoir (Ref. TASK 29-14-00-614-804). (11) Operate the flight controls and monitor the reservoir level. If necessary fill the Blue hydraulic reservoir (Ref. TASK 12-12-29-611803). (12) Each week, do a new sampling of the fluid (Ref. TASK 12-32-29-281801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B329 Jan 01/07
Subtask 12-36-29-942-089 C. Remove the safety precautions. (1) Remove the warning notice(s). Subtask 12-36-29-410-108 D. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Remove the access platform(s). (3) Close the landing gear doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-862-093 E. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
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**ON A/C 701-749, TASK 12-36-29-611-802-A Replacement of the Hydraulic Fluid of the Blue Hydraulic System with a Fluid Replacement and Recovery Bench WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. CAUTION : DO NOT DEPRESSURIZE THE ENGINE PUMPS DURING THE DRY MOTORING. IF YOU _______ DO, YOU CAN CAUSE DAMAGE TO THE ENGINE PUMPS. 1. __________________ Reason for the Job You must replace the fluid only if the acidity is higher than the values given into the task of the sampling for analysis (Ref. TASK 12-32-29-281-80100).
EFF : 701-749, 12-36-29 R SROS
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2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific No specific No specific DH0501
blanking plug hydraulic ground power supply plug type E0053R8B3APNE access platform 1.8 m (5 ft. 11 in.) access platform 1.80 m (5 ft. 11 in.) 1 TOOL - HYDRAULIC FLUID CHANGE
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 02-003
F NSA 307110 TYPE 4 HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-803 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-863-801 29-10-00-611-802 29-10-00-710-805 29-11-43-600-809 29-12-44-600-801 29-12-45-600-801
Fill the Blue Hydraulic Reservoir with a Hydraulic Service Cart Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Pressurize the Green Hydraulic System with the Ground Hydraulic Supply Drainage of the Blue Hydraulic Reservoir Operational Test of the Electric Motor of the Engine Pump Suction Fire Shut-Off Valve Servicing of the Engine Pump Case Drain Filter (5013JM2) Servicing of the Blue Reservoir LP-Filter (5011JM2) Servicing of the Blue HP Filter (5111JM2)
EFF : 701-749, 12-36-29 R SROS
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-14-00-614-802 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 32-43-00-870-801 32-45-00-864-801 71-00-00-720-828 78-31-00-740-802 12-36-29-991-095 12-36-29-991-073 12-36-29-991-075 12-36-29-991-074
Depressurization of the Blue Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Bleeding the Alternate Braking System at the Wheel Brakes Release the Pressure from the Parking Brake System after Depressurization Dry Motoring Engine Test of the Thrust Reverser Deployment and Stowage (Engine not Running) Fig. 332 Fig. 336 Fig. 337 Fig. 338
3. __________ Job Set-up Subtask 12-36-29-861-066 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). Subtask 12-36-29-860-159 B. Aircraft Maintenance Configuration (1) Pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-801). (2) Set the flap and slat control lever on the panel 114VU to the position 1. (3) On the ECAM Engine/Warning Display the indication 1+F comes into view. (4) On the HYD section of the maintenance panel 285VU, make sure that the LEAK MEASUREMENT VALVES/B pushbutton switch is pushed (the OFF legend is on).
EFF : 701-749, 12-36-29 R SROS
Page B333 Jan 01/07
(5) On the Blue HP manifold 6103JM, disconnect the pressure switches 7JS2 and 19CE2 and on the free end make a short circuit between the pin A and B with a plug type E0053R8B3APNE. (Ref. Fig. 332/TASK 12-36-29-991-095) Subtask 12-36-29-010-112-A C. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Put an access platform at the zone 147. (3) Put an access platform in position at the zone 195. (4) Remove the access panel 195CB. Subtask 12-36-29-680-060 D. Drain the reservoir of the Blue hydraulic system (Ref. TASK 29-10-00-611802). Subtask 12-36-29-860-160 E. Set the hydraulic ground power supply to the correct configuration: (1) Make sure that the hydraulic ground power supply reservoir is filled with new HYDRAULIC FLUIDS (Material No. 02-003). (2) Make sure that no chlorinated solvent has been used to flush the tool lines. (3) Set the hydraulic ground power supply to the cart reservoir configuration. (4) Open the by-pass valve. (5) Start the hydraulic ground power supply. (6) Adjust the hydraulic ground power supply to the minimum pressure ( 20 bar (290.0754 psi) approx.) and to a flow of 45/lmn approx. and stop the hydraulic ground power supply.
EFF : 701-749, 12-36-29 R SROS
Page B334 Jan 01/07
Subtask 12-36-29-860-161 F. Set the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the correct configuration. (Ref. Fig. 336/TASK 12-36-29-991-073, 337/TASK 12-36-29-991-075) NOTE : Make sure that the Blue reservoir depressurization valve is open ____ when you set the hydraulic fluid replacement and recovery bench to the correct configuration. (1) On the fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501): - close the valve V1. (2) Connect the connector LP1 of the of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the LP connector of the hydraulic ground power supply. (3) Connect the HP1 connector of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the HP connector of the hydraulic ground power supply. (4) Connect the LP3 connector of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the suction connector of the ground service panel. (5) On the HP manifold 6103JM (a) Remove the Blue HP filter 5111JM2 (Ref. TASK 29-12-45-600-801). (b) Install a dummy bowl of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) in place on the Blue HP filter 5111JM2. (c) Connect the HP2 line to the dummy bowl and to the valve V2. (6) On the LP filter 5011JM2 (a) Disconnect the flexible hose (1) from the Blue LP manifold 6005JM, and connect the LP2 line. (7) Put a blanking plug on the Blue LP filter 5011JM2. (8) Start the hydraulic ground power supply and make sure that the pressure read on the gage of the hydraulic fluid replacement and recovery bench is 4 bar (58.0150 psi).
EFF : 701-749, 12-36-29 R SROS
Page B335 Jan 01/07
Connections of Tools to the Blue Hydraulic System Figure 336/TASK 12-36-29-991-073- 12 (SHEET 1) EFF : 701-749, 12-36-29 R SROS
Page B336 Jan 01/07
Connections of Tools to the Blue Hydraulic System Figure 336/TASK 12-36-29-991-073- 22 (SHEET 2) R EFF : 701-749, 12-36-29 SROS
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Blue Hydraulic System-Schematic Diagram Figure 337/TASK 12-36-29-991-075- 12 (SHEET 1) R EFF : 701-749, 12-36-29 SROS
Page B338 Jan 01/07
Blue Hydraulic System-Schematic Diagram Figure 337/TASK 12-36-29-991-075- 22 (SHEET 2) R EFF : 701-749, 12-36-29 SROS
Page B339 Jan 01/07
(9) Stop the hydraulic ground power supply. 4. Procedure _________ (Ref. Fig. 337/TASK 12-36-29-991-075) Subtask 12-36-29-611-163 A. Fill the Blue reservoir. (1) Open the depressurization valve of Blue reservoir (Ref. TASK 29-1400-614-802). (2) Open the valve V1 of the TOOL - HYDRAULIC FLUID CHANGE (DH0501) and start the hydraulic ground power supply. (3) Fill the Blue reservoir until the fluid is at the upper limit on the visual indicator (Ref. TASK 12-12-29-611-803). (4) Close the depressurization valve of Blue reservoir. (5) Pressurize the Blue hydraulic reservoir (Ref. TASK 29-14-00-614-804). (6) Close the valve V1. Subtask 12-36-29-611-164 B. Replacement of the Fluid in the Engine Pump Suction and Pressure Lines (1) For 4030EM1 (a) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501) open the valve V1 and keep it open during the full procedure. (b) Dry motor the engine (Ref. TASK 71-00-00-720-828). NOTE : Stop the dry motoring if the advisory low level comes into ____ view on the ECAM SYSTEM DISPLAY. If necessary fill the Blue hydraulic reservoir (Ref. TASK 12-12-29-611-803). (c) Dry motor the engine (Ref. TASK 71-00-00-720-828). (d) Open the valve V2 until you collect 40 liters of fluid. (e) Close the valve V2. (f) Stop the dry motoring.
R EFF : 701-749, 12-36-29 SROS
Page B340 Jan 01/07
Subtask 12-36-29-611-165 C. Replacement of the Fluid in the Suction, Pressure and Case Drain Lines of the Electric Pump (1JC) (1) Disconnect the case drain tube from the electric pump (1JC). (2) Put blanking plug on the end of the tube. (3) Connect the case drain elec hose of the TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the electric pump (1JC). (4) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501): - make sure that the valve V1 is open. (5) On the HYD section of the overhead panel 245VU: - push the BLUE/ELEC pushbutton switch (4JC). (6) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501): - open the valve V2 until you collect 4 liters of fluid. (7) Close the valve V2. (8) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC) Subtask 12-36-29-611-166 D. Replacement of the Fluid in the Alternate Brake Accumulators (1) On the manifold 5401GG depressurize the brake accumulators (Ref. TASK 32-45-00-864-801). Subtask 12-36-29-611-167 E. Replacement of the Fluid in the Thrust Reverser System (1) On the HYD section of the overhead panel 245VU: - push the BLUE/ELEC pushbutton switch (4JC). (2) Do two deploy-to-stow cycles of the thrust reverser (Ref. TASK 78-3100-740-802). (3) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC).
R EFF : 701-749, 12-36-29 SROS
Page B341 Jan 01/07
(4) On the panel 255VU: Push the ENG1 FIRE pushbutton switch: - On the ECAM SD make sure that the fire shutoff valve is closed. Subtask 12-36-29-611-168 F. Replacement of the Fluid in the Supply and Return Lines of the Primary Servocontrols (Ref. Fig. 338/TASK 12-36-29-991-074) (1) On the FLT CTL section of the overhead panel 212VU: - push the SEC2, PRIM2 and PRIM3 pushbutton switches. (2) On the ground service manifold 5109JM2 open the valves which supply the right and left wing. (Ref. Fig. 332/TASK 12-36-29-991-095) (3) On the HYD section of the overhead panel 245VU: - push the BLUE/ELEC pushbutton switch (4JC). (4) Do 5 operations over full travel range and make sure that the surfaces move. If they do not move, do the reset of the related computers. (5) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC). (6) On the ground service manifold 5109JM2 close the valves for the right and left wing and open the valve for the aft fuselage. (7) On the HYD section of the overhead panel 245VU: - push the BLUE/ELEC pushbutton switch (4JC). (8) Operate the elevators over full travel range four times. (9) Operate the rudder over full travel range four times. (10) Operate the THS until you collect 5 liters of fluid. (11) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC). (12) Close the valve for the aft fuselage.
R EFF : 701-749, 12-36-29 SROS
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Flight Control Operations Figure 338/TASK 12-36-29-991-074 R EFF : 701-749, 12-36-29 SROS
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Subtask 12-36-29-865-137 G. Make sure that this(these) circuit breaker(s) is(are) closed: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM AVAIL 10CW X13 722VU SFCC 2 SLAT 2CW V40 742VU SFCC 1 SLAT 1CW L62 Subtask 12-36-29-611-169 H. Replacement of the Fluid in the Flap and Slat Supply and Return Systems (1) Make sure that the flap and slat control lever on the panel 114VU is in the position 1. (2) On the ground service manifold 5109JM2 open the valves which supply the right and left wing. (3) On the HYD section of the overhead panel 245VU: - push the BLUE/ELEC pushbutton switch (4JC). (4) Set the flap and slat control lever on the panel 114VU to the position 2. (5) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC). (6) On the ground service manifold 5109JM2 close the valves which supply the right and left wing. Subtask 12-36-29-611-170 J. Replacement of the Fluid in the Alternate Braking System (1) On the panel 312VU, set the PARK BRK switch to the OFF position. (2) On the HYD section of the overhead panel 245VU: - push the BLUE/ELEC pushbutton switch (4JC). (3) Push and release the brake pedals five times. (4) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC).
R EFF : 701-749, 12-36-29 SROS
Page B344 Jan 01/07
5. Close-up ________ Subtask 12-36-29-420-084 A. Replace these hydraulic filters: - the LP filter 5011JM2 (Ref. TASK 29-12-44-600-801) - the case drain filter 5013JM2 (Ref. TASK 29-11-43-600-809). Subtask 12-36-29-942-094 B. Aircraft Maintenance Configuration (1) On the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/B pushbutton switch (the OFF legend is off). (2) On the Blue HP manifold 6103JM, remove the plug type E0053R8B3APNE from the pressure switches 7JS2 and 19CE2 and connect the pressure switches 7JS2 and 19CE2. (3) On the panel 255VU: - release the ENG2/FIRE pushbutton switch. (4) Do the operational test of the electric motor of the engine pump suction fire shut-off valve (4JB) (Ref. TASK 29-10-00-710-805). (5) Do the bleeding of the alternate brake system (Ref. TASK 32-43-00870-801). (6) Close the valves V1 and V2 on the recovery bench. (7) Disconnect all the lines between the aircraft and the recovery bench. (8) Disconnect all the lines between the recovery bench and the hydraulic ground power supply. (9) Replace the HP hydraulic filter 5111JM2 (Ref. TASK 29-12-45-600-801). (10) Pressurize the Blue hydraulic reservoir (Ref. TASK 29-14-00-614-804). (11) Operate the flight controls and monitor the reservoir level. If necessary fill the Blue hydraulic reservoir (Ref. TASK 12-12-29-611803). (12) Each week, do a new sampling of the fluid (Ref. TASK 12-32-29-281801).
R EFF : 701-749, 12-36-29 SROS
Page B345 Jan 01/07
Subtask 12-36-29-942-095 C. Remove the safety precautions. (1) Remove the warning notice(s). Subtask 12-36-29-410-111 D. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Remove the access platform(s). (3) Close the landing doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-862-096 E. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 701-749, 12-36-29 SROS
Page B346 Jan 01/07
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, TASK 12-36-29-611-803 Replacement of the Hydraulic Fluid of the Yellow Hydraulic System with a Fluid Replacement and Recovery Bench WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. CAUTION : DO NOT DEPRESSURIZE THE ENGINE PUMPS DURING THE DRY MOTORING. IF YOU _______ DO, YOU CAN CAUSE DAMAGE TO THE ENGINE PUMPS. 1. __________________ Reason for the Job You must replace the fluid only if the acidity is higher than the values given into the task of the sampling for analysis (Ref. TASK 12-32-29-281-80100).
EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page B347 Jan 01/07
2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific No specific DH0501
blanking plug hydraulic ground power supply plug type E0053R8B3APNE access platform 1.8 m (5 ft. 11 in.) 1 TOOL - HYDRAULIC FLUID CHANGE
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 02-003
F NSA 307110 TYPE 4 HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-805 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-863-801 29-10-00-611-803 29-10-00-710-805 29-11-43-600-804 29-13-44-600-801 29-13-45-600-801
Fill the Yellow Hydraulic Reservoir with a Hydraulic Service Cart Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Pressurize the Green Hydraulic System with the Ground Hydraulic Supply Drainage of the Yellow Hydraulic Reservoir Operational Test of the Electric Motor of the Engine Pump Suction Fire Shut-Off Valve Servicing of the (Aft) Engine-Pump Case-Drain Filter Element 5013JM2 Servicing of the Yellow Reservoir LP-Filter (5011JM3) Servicing of the Yellow HP Filter (5111JM3)
EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page B348 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-14-00-614-803 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 52-30-00-010-801 52-30-00-410-801 71-00-00-720-816 78-31-00-710-804 12-36-29-991-096 12-36-29-991-079 12-36-29-991-081 12-36-29-991-080
Depressurization of the Yellow Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Opening of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Closing of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Test No. 2 - Engine Motor Leak Test (Dry Method) Thrust Reverser Cowl Doors Open Thrust Reverser Cycling Test (MCDU) Fig. 339 Fig. 340 Fig. 341 Fig. 342
3. __________ Job Set-up Subtask 12-36-29-861-064 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). Subtask 12-36-29-860-153 B. Aircraft Maintenance Configuration (1) Pressurize the Yellow hydraulic system (Ref. TASK 29-00-00-863-801). (2) Set the flap and slat control lever on the panel 114VU to the position 1. (3) On the ECAM engine/warning display the indication 1+F comes into view. (4) On the HYD section of the maintenance panel 285VU, make sure that the LEAK MEASUREMENT VALVES/Y pushbutton switch is pushed (the OFF legend is on).
EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page B349 Jan 01/07
(5) On the Yellow HP manifold 7103JM, disconnect the pressure switches 7JS3 and 19CE3 and on the free end make a short circuit between the pin A and B with a plug type E0053R8B3APNE. (Ref. Fig. 339/TASK 12-36-29-991-096) Subtask 12-36-29-010-110-A C. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Put an access platform in position at the zone 147. (3) Put an access platform in position at the zone 196. (4) Remove the access panel 196EB. Subtask 12-36-29-680-058 D. Drain the reservoir of the Yellow hydraulic system (Ref. TASK 29-10-00611-803). Subtask 12-36-29-860-154 E. Set the hydraulic ground power supply to the correct configuration: (1) Make sure that the hydraulic ground power supply reservoir is filled with new HYDRAULIC FLUIDS (Material No. 02-003). (2) Make sure that no chlorinated solvent has been used to flush the tool lines. (3) Set the hydraulic ground power supply to the cart reservoir configuration. (4) Open the by-pass valve. (5) Start the hydraulic ground power supply. (6) Adjust the hydraulic ground power supply to the minimum pressure ( 20 bar (290.0754 psi) approx.) and to a flow of 45l/mn approx. and stop the hydraulic ground power supply.
EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page B350 Jan 01/07
Manifolds of the Yellow Hydraulic System Figure 339/TASK 12-36-29-991-096 R EFF : ALL 12-36-29 SROS
Page B351 Jan 01/07
Subtask 12-36-29-860-155 F. Set the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the correct configuration. (Ref. Fig. 340/TASK 12-36-29-991-079, 341/TASK 12-36-29-991-081) NOTE : Make sure that the Yellow reservoir depressurization valve is open ____ when you set the hydraulic fluid replacement and recovery bench to the correct configuration. (1) On the fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501): - close the valve V1. (2) Connect the connector LP1 of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the LP connector of the hydraulic ground power supply. (3) Connect the HP1 connector of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the HP connector of the hydraulic ground power supply. (4) Connect the LP3 connector of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the suction connector of the ground service panel. (5) On the HP manifold 7103JM: (a) Remove the Yellow HP filter 5111JM3 (Ref. TASK 29-13-45-600-801). (b) Install a dummy bowl of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) in place of the Yellow HP filter 5111JM3. (c) Connect the HP2 line to the dummy bowl and to the valve V2. (6) On the LP filter 5011JM3: (a) Disconnect the tube (1) from the LP filter 5011JM3. (b) Put a blanking plug on the Yellow LP filter 5011JM3. (c) Loosen the tube (1) from the Yellow LP manifold 7005JM. (d) Turn the tube (1) on the Yellow LP manifold 7005JM, and connect the LP2 line.
EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, R SROS
Page B352 Jan 01/07
INTENTIONALLY BLANK
R 12-36-29 SROS
Page B353 Jan 01/07
Connections of Tools to the Yellow Hydraulic System Figure 340/TASK 12-36-29-991-079- 12 (SHEET 1) R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B354 Jan 01/07
Connections of Tools to the Yellow Hydraulic System Figure 340/TASK 12-36-29-991-079- 22 (SHEET 2) R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B355 Jan 01/07
Yellow Hydraulic System-Schematic Diagram Figure 341/TASK 12-36-29-991-081- 12 (SHEET 1) R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B356 Jan 01/07
Yellow Hydraulic System-Schematic Diagram Figure 341/TASK 12-36-29-991-081- 22 (SHEET 2) R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B357 Jan 01/07
(e) Tighten the tube (1) on the Yellow LP manifold 7005JM. (7) Start the hydraulic ground power supply and make sure that the pressure read on the gage of the hydraulic fluid replacement and recovery bench is 4 bar (58.0150 psi). (8) Stop the hydraulic ground power supply. 4. Procedure _________ (Ref. Fig. 341/TASK 12-36-29-991-081) Subtask 12-36-29-611-145 A. Fill the Yellow reservoir. (1) Open the depressurization valve of Yellow reservoir (Ref. TASK 29-1400-614-803). (2) Open the valve V1 of the TOOL - HYDRAULIC FLUID CHANGE (DH0501) and start the hydraulic ground power supply. (3) Fill the Yellow reservoir until the fluid is at the upper limit on the visual indicator (Ref. TASK 12-12-29-611-805). (4) Close the depressurization valve of Yellow reservoir. (5) Pressurize the Yellow hydraulic reservoir (Ref. TASK 29-14-00-614804). (6) Close the valve V1. Subtask 12-36-29-611-146 B. Replacement of the Fluid in the Engine Pump Suction and Pressure Lines (1) For 4030EM2 (a) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501) open the valve V1 and keep it open during the full procedure. (b) Dry motor the engine (Ref. TASK 71-00-00-720-816). NOTE : Stop the dry motoring if the advisory low level comes into ____ view on the ECAM SYSTEM DISPLAY. If necessary fill the Blue hydraulic reservoir (Ref. TASK 12-12-29-611-805).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B358 Jan 01/07
(c) Dry motor the engine (Ref. TASK 71-00-00-720-816). (d) Open the valve V2 until you collect 40 liters of fluid. (e) Close the valve V2. (f) Stop the dry motoring. Subtask 12-36-29-611-147-A C. Replacement of the Fluid in the Suction, Pressure and Case Drain Lines of the Electric Pump (1JJ) (1) Disconnect the case drain tube from the electric pump (1JJ). (2) Put blanking plug on the end of the tube. (3) Connect the case drain elec hose of the TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the electric pump (1JJ). (4) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501): - make sure that the valve V1 is open. (5) On the HYD section of the overhead panel 245VU: - push the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (6) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501): - open the valve V2 until you collect 4 liters of fluid. (7) Close the valve V2. (8) On the HYD section of the overhead panel 245VU: - release the YELLOW/ELEC/AUTO pushbutton switch (6JJ). Subtask 12-36-29-611-148-A D. Replacement of the Fluid in the Thrust Reverser System (1) On the HYD section of the overhead panel 245VU: - push the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (2) Do two deploy-to-stow cycles of the thrust reverser (Ref. TASK 78-3100-710-804). (3) On the HYD section of the overhead panel 245VU: - release the YELLOW/ELEC/AUTO pushbutton switch (6JJ).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B359 Jan 01/07
(4) On the panel 255VU: - Push the ENG2/FIRE pushbutton switch. (5) On the ECAM SD make sure that the fire shutoff valves are closed. Subtask 12-36-29-611-149-A E. Replacement of the Fluid in the Supply and Return Lines of the Primary Servocontrols (Ref. Fig. 342/TASK 12-36-29-991-080) (1) On the FLT CTL section of the overhead panel 212VU: - push the SEC2, PRIM2 and PRIM3 pushbutton switches. (2) On the FLT CTL section of the overhead panel 241VU: - push the SEC1 pushbutton switch. (3) On the ground service manifold 5109JM3 open the valves which supply the right and left wing. (Ref. Fig. 339/TASK 12-36-29-991-096) (4) On the HYD section of the overhead panel 245VU: - push the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (5) Do 5 operations over full travel range and make sure that the surfaces move. If they do not move, do the reset of the related computers. (6) On the HYD section of the overhead panel 245VU: - release the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (7) On the ground service manifold 5109JM3 close the valves for the right and left wing and open the valve for the aft fuselage. (8) On the HYD section of the overhead panel 245VU: - push the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (9) Operate the elevators over full travel range four times. (10) Operate the rudder over full travel range four times. (11) Operate the THS until you collect 5 liters of fluid. (12) On the HYD section of the overhead panel 245VU: - release the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (13) Close the valve for the aft fuselage.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B360 Jan 01/07
Flight Control Operations Figure 342/TASK 12-36-29-991-080 R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B361 Jan 01/07
Subtask 12-36-29-865-133 F. Make sure that this(these) circuit breaker(s) is(are) closed: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM 10CV X14 722VU SFCC 2 FLAP 2CV T43 742VU SFCC 1 FLAP 1CV L61 Subtask 12-36-29-611-150-A G. Replacement of the Fluid in the Flap and Slat Supply and Return Systems (1) Make sure that the flap and slat control lever on the panel 114VU is in the position 1. (2) On the ground service manifold 5109JM3 open the valves which supply the right and left wing. (3) On the HYD section of the overhead panel 245VU: - push the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (4) Set the flap and slat control lever on the panel 114VU to the position 2. (5) On the HYD section of the overhead panel 245VU: - release the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (6) On the ground service manifold 5109JM3 close the valves which supply the right and left wing. Subtask 12-36-29-611-151 H. Replacement of the Fluid in the Cargo Door Systems (1) Do 2 opening and closing cycles of the cargo doors (Ref. TASK 52-3000-010-801) and (Ref. TASK 52-30-00-410-801). 5. Close-up ________ Subtask 12-36-29-420-082 A. Replace these hydraulic filters: - the LP filter 5011JM3 (Ref. TASK 29-13-44-600-801) - the case drain filter 5013JM2 (Ref. TASK 29-11-43-600-804).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B362 Jan 01/07
Subtask 12-36-29-942-090 B. Aircraft Maintenance Configuration (1) On the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/Y pushbutton switch (the OFF legend is off). (2) On the Yellow HP manifold 7103JM, remove the plug type E0053R8B3APNE from the pressure switches 7JS3 and 19CE3 and connect the pressure switches 7JS3 and 19CE3. (3) On the panel 255VU: - release the ENG3/FIRE pushbutton switch. (4) Do the operational test of the electric motor of the engine pump suction fire shut-off valve (4JY) (Ref. TASK 29-10-00-710-805). (5) Close the valves V1 and V2 on the recovery bench. (6) Disconnect all the lines between the aircraft and the recovery bench. (7) Disconnect all the lines between the recovery bench and the hydraulic ground power supply. (8) Replace the HP hydraulic filter 5111JM3 (Ref. TASK 29-13-45-600-801). (9) Pressurize the Yellow hydraulic reservoir (Ref. TASK 29-14-00-614804). (10) Operate the flight controls and monitor the reservoir level. If necessary fill the Yellow hydraulic reservoir (Ref. TASK 12-12-29611-805). Each week, do a new sampling of fluid (Ref. TASK 12-32-29-281-801). Subtask 12-36-29-942-091 C. Remove the safety precautions (1) Remove the warning notice(s).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B363 Jan 01/07
Subtask 12-36-29-410-109 D. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Remove the access platform(s). (3) close the landing gear doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-862-094 E. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B364 Jan 01/07
**ON A/C 701-749, TASK 12-36-29-611-803-A Replacement of the Hydraulic Fluid of the Yellow Hydraulic System with a Fluid Replacement and Recovery Bench WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. CAUTION : DO NOT DEPRESSURIZE THE ENGINE PUMPS DURING THE DRY MOTORING. IF YOU _______ DO, YOU CAN CAUSE DAMAGE TO THE ENGINE PUMPS. 1. __________________ Reason for the Job You must replace the fluid only if the acidity is higher than the values given into the task of the sampling for analysis (Ref. TASK 12-32-29-281-80100).
EFF : 701-749, 12-36-29 R SROS
Page B365 Jan 01/07
2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific No specific No specific DH0501
blanking plug hydraulic ground power supply plug type E0053R8B3APNE access platform 1.8 m (5 ft. 11 in.) access platform 1.80 m (5 ft. 11 in.) 1 TOOL - HYDRAULIC FLUID CHANGE
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 02-003
F NSA 307110 TYPE 4 HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-805 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-863-801 29-10-00-611-803 29-10-00-710-805 29-11-43-600-809 29-13-44-600-801 29-13-45-600-801
Fill the Yellow Hydraulic Reservoir with a Hydraulic Service Cart Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Pressurize the Green Hydraulic System with the Ground Hydraulic Supply Drainage of the Yellow Hydraulic Reservoir Operational Test of the Electric Motor of the Engine Pump Suction Fire Shut-Off Valve Servicing of the Engine Pump Case Drain Filter (5013JM2) Servicing of the Yellow Reservoir LP-Filter (5011JM3) Servicing of the Yellow HP Filter (5111JM3)
EFF : 701-749, 12-36-29 R SROS
Page B366 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------29-14-00-614-803 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 52-30-00-010-801 52-30-00-410-801 71-00-00-720-828 78-31-00-740-802 12-36-29-991-095 12-36-29-991-096 12-36-29-991-082 12-36-29-991-084 12-36-29-991-083
Depressurization of the Yellow Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Opening of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Closing of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Dry Motoring Engine Test of the Thrust Reverser Deployment and Stowage (Engine not Running) Fig. 332 Fig. 339 Fig. 343 Fig. 344 Fig. 345
3. __________ Job Set-up Subtask 12-36-29-861-067 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). Subtask 12-36-29-860-162 B. Aircraft Maintenance Configuration (1) Pressurize the Yellow hydraulic system (Ref. TASK 29-00-00-863-801). (2) Set the flap and slat control lever on the panel 114VU to the position 1. (3) On the ECAM Engine/Warning Display, the indication 1+F comes into view. (4) On the HYD section of the maintenance panel 285VU, make sure that the LEAK MEASUREMENT VALVES/Y pushbutton switch is pushed (the OFF legend is on).
EFF : 701-749, 12-36-29 R SROS
Page B367 Jan 01/07
(5) On the Yellow HP manifold 7103JM, disconnect the pressure switches 7JS3 and 19CE3, and on the free end make a short circuit between the pins A and B with a plug type E0053R8B3APNE. (Ref. Fig. 332/TASK 12-36-29-991-095) Subtask 12-36-29-010-113 C. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Put an access platform in position at the zone 147. (3) Put an access platform in position at the zone 196. (4) Remove the access panel 196AB. Subtask 12-36-29-680-061 D. Drain the reservoir of the Yellow hydraulic system (Ref. TASK 29-10-00611-803). Subtask 12-36-29-860-163 E. Set the hydraulic ground power supply to the correct configuration: (1) Make sure that the hydraulic ground power supply reservoir is filled with new HYDRAULIC FLUIDS (Material No. 02-003). (2) Make sure that no chlorinated solvent has been used to flush the tool lines. (3) Set the hydraulic ground power supply to the cart reservoir configuration. (4) Open the by-pass valve. (5) Start the hydraulic ground power supply. (6) Adjust the hydraulic ground power supply to the minimum pressure ( 20 bar (290.0754 psi) approx.) and to a flow of 45/lmn approx. and stop the hydraulic ground power supply.
EFF : 701-749, 12-36-29 R SROS
Page B368 Jan 01/07
Subtask 12-36-29-860-164 F. Set the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the correct configuration. (Ref. Fig. 343/TASK 12-36-29-991-082, 344/TASK 12-36-29-991-084) NOTE : Make sure that the Yellow reservoir depressurization valve is open ____ when you set the hydraulic fluid replacement and recovery bench to the correct configuration. (1) On the fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501): - close the valve V1. (2) Connect the connector LP1 of the hydraulic fluid replacement and recovery bench to the LP connector of the hydraulic ground power supply. (3) Connect the HP1 connector of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the HP connector of the hydraulic ground power supply. (4) Connect the LP3 connector of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the suction connector of the ground service panel. (5) On the HP manifold 7103JM (a) Remove the Yellow HP filter 5111JM3 (Ref. TASK 29-13-45-600-801). (b) Install a dummy bowl of the hydraulic fluid replacement and recovery bench TOOL - HYDRAULIC FLUID CHANGE (DH0501) in place on the Yellow HP filter 5111JM3. (c) Connect the HP2 line to the dummy bowl and to the valve V2. (6) On the LP filter 5011JM3: (a) Disconnect the tube (1) from the LP filter 5011JM3. (b) Put a blanking plug on the Yellow LP filter 5011JM3. (c) Loosen the tube (1) from the Yellow LP manifold 7005JM. (d) Turn the tube (1) on the Yellow LP manifold 7005JM, and connect the LP2 line.
EFF : 701-749, 12-36-29 R SROS
Page B369 Jan 01/07
Connections of Tools to the Yellow Hydraulic System Figure 343/TASK 12-36-29-991-082- 12 (SHEET 1) EFF : 701-749, 12-36-29 R SROS
Page B370 Jan 01/07
Connections of Tools to the Yellow Hydraulic System Figure 343/TASK 12-36-29-991-082- 22 (SHEET 2) R EFF : 701-749, 12-36-29 SROS
Page B371 Jan 01/07
Yellow Hydraulic System-Schematic Diagram Figure 344/TASK 12-36-29-991-084- 12 (SHEET 1) R EFF : 701-749, 12-36-29 SROS
Page B372 Jan 01/07
Yellow Hydraulic System-Schematic Diagram Figure 344/TASK 12-36-29-991-084- 22 (SHEET 2) R EFF : 701-749, 12-36-29 SROS
Page B373 Jan 01/07
(e) Tighten the tube (1) on the Yellow LP manifold 7005JM. (7) Start the hydraulic ground power supply and make sure that the pressure read on the gage of the hydraulic fluid replacement and recovery bench is 4 bar (58.0150 psi). (8) Stop the hydraulic ground power supply. 4. Procedure _________ (Ref. Fig. 344/TASK 12-36-29-991-084) Subtask 12-36-29-611-171 A. Fill the Yellow reservoir. (1) Open the depressurization valve of Yellow reservoir (Ref. TASK 29-1400-614-803). (2) Open the valve V1 of the TOOL - HYDRAULIC FLUID CHANGE (DH0501) and start the hydraulic ground power supply. (3) Fill the Yellow reservoir until the fluid is at the upper limit on the visual indicator (Ref. TASK 12-12-29-611-805). (4) Close the depressurization valve of Yellow reservoir. (5) Pressurize the Yellow hydraulic reservoir (Ref. TASK 29-14-00-614804). (6) Close the valve V1. Subtask 12-36-29-611-172 B. Replacement of the Fluid in the Engine Pump Suction and Pressure Lines (1) For 4030EM2 (a) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501) open the valve V1 and keep it open during the full procedure. (b) Dry motor the engine (Ref. TASK 71-00-00-720-828). NOTE : Stop the dry motoring if the advisory low level comes into ____ view on the ECAM SYSTEM DISPLAY. If necessary fill the Blue hydraulic reservoir (Ref. TASK 12-12-29-611-805).
R EFF : 701-749, 12-36-29 SROS
Page B374 Jan 01/07
(c) Dry motor the engine (Ref. TASK 71-00-00-720-828). (d) Open the valve V2 until you collect 40 liters of fluid. (e) Close the valve V2. (f) Stop the dry motoring. Subtask 12-36-29-611-173 C. Replacement of the Fluid in the Suction, Pressure and Case Drain Lines of the Electric Pump (1JJ) (1) Disconnect the case drain tube from the electric pump (1JJ). (2) Put blanking plug on the end of the tube. (3) Connect the case drain elec hose of the TOOL - HYDRAULIC FLUID CHANGE (DH0501) to the electric pump (1JJ). (4) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501): - make sure that the valve V1 is open. (5) On the HYD section of the overhead panel 245VU: - push the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (6) On the TOOL - HYDRAULIC FLUID CHANGE (DH0501): - open the valve V2 until you collect 4 liters of fluid. (7) Close the valve V2. (8) On the HYD section of the overhead panel 245VU: - release the YELLOW/ELEC/AUTO pushbutton switch (6JJ). Subtask 12-36-29-611-174 D. Replacement of the Fluid in the Thrust Reverser System (1) On the HYD section of the overhead panel 245VU: - push the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (2) Do two deploy-to-stow cycles of the thrust reverser (Ref. TASK 78-3100-740-802). (3) On the HYD section of the overhead panel 245VU: - release the YELLOW/ELEC/AUTO pushbutton switch (6JJ).
R EFF : 701-749, 12-36-29 SROS
Page B375 Jan 01/07
(4) On the panel 255VU: Push the ENG2 FIRE pushbutton switch. On the ECAM SD make sure that the fire shutoff valves are closed. Subtask 12-36-29-611-175 E. Replacement of the Fluid in the Supply and Return Lines of the Primary Servocontrols (Ref. Fig. 345/TASK 12-36-29-991-083) (1) On the FLT CTL section of the overhead panel 212VU: - push the SEC2 PRIM2 and PRIM3 pushbutton switches. (2) On the FLT CTL section of the overhead panel 241VU: - push the SEC1 pushbutton switch. (3) On the ground service manifold 5109JM3 open the valves which supply the right and left wing. (Ref. Fig. 339/TASK 12-36-29-991-096) (4) On the HYD section of the overhead panel 245VU: - push the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (5) Do 5 operations over full travel range and make sure that the surfaces move. If they do not move, do the reset of the related computers. (6) On the HYD section of the overhead panel 245VU: - release the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (7) On the ground service manifold 5109JM3 close the valves for the right and left wing and open the valve for the aft fuselage. (8) On the HYD section of the overhead panel 245VU: - push the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (9) Operate the elevators over full travel range four times. (10) Operate the rudder over full travel range four times. (11) Operate the THS until you collect 5 liters of fluid. (12) On the HYD section of the overhead panel 245VU: - release the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (13) Close the valve for the aft fuselage.
R EFF : 701-749, 12-36-29 SROS
Page B376 Jan 01/07
Flight Control Operations Figure 345/TASK 12-36-29-991-083 R EFF : 701-749, 12-36-29 SROS
Page B377 Jan 01/07
Subtask 12-36-29-865-139 F. Make sure that this(these) circuit breaker(s) is(are) closed: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM 10CV X14 722VU SFCC 2 FLAP 2CV T43 742VU SFCC 1 FLAP 1CV L61 Subtask 12-36-29-611-176 G. Replacement of the Fluid in the Flap and Slat Supply and Return Systems (1) Make sure that the flap and slat control lever on the panel 114VU is in the position 1. (2) On the ground service manifold 5109JM3 open the valves which supply the right and left wing. (3) On the ground service manifold 5109JM3 open the valves which supply the right and left wing. (4) On the HYD section of the overhead panel 245VU: - push the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (5) Set the flap and slat control lever on the panel 114VU to the position 2. (6) On the HYD section of the overhead panel 245VU: - release the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (7) On the ground service manifold 5109JM3 close the valves which supply the right and left wing. Subtask 12-36-29-611-177 H. Replacement of the Fluid in the Cargo Door Systems (1) Do 2 opening and closing cycles of the cargo doors (Ref. TASK 52-3000-010-801) and (Ref. TASK 52-30-00-410-801).
EFF : 701-749, 12-36-29 R SROS
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5. Close-up ________ Subtask 12-36-29-420-085 A. Replace these hydraulic filters: - the LP filter 5011JM3 (Ref. TASK 29-13-44-600-801) - the case drain filter 5013JM2 (Ref. TASK 29-11-43-600-809). Subtask 12-36-29-942-096 B. Aircraft Maintenance Configuration (1) On the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/Y pushbutton switch (the OFF legend is off). (2) On the Yellow HP manifold 7103JM, remove the plug type E0053R8B3APNE from the pressure switches 7JS3 and 19CE3 and connect the pressure switches 7JS3 and 19CE3. (3) On the panel 255VU: - release the ENG3/FIRE pushbutton switch. (4) Do the operational test of the electric motor of the engine pump suction fire shut-off valve (4JY) (Ref. TASK 29-10-00-710-805). (5) Close the valves V1 and V2 on the recovery bench. (6) Disconnect all the lines between the aircraft and the recovery bench. (7) Disconnect all the lines between the recovery bench and the hydraulic ground power supply. (8) Replace the HP hydraulic filter 5111JM3 (Ref. TASK 29-13-45-600-801). (9) Pressurize the Yellow hydraulic reservoir (Ref. TASK 29-14-00-614804). (10) Operate the flight controls and monitor the reservoir level. If necessary fill the Yellow hydraulic reservoir (Ref. TASK 12-12-29611-805). (11) Each week, do a new sampling of fluid (Ref. TASK 12-32-29-281-801).
R EFF : 701-749, 12-36-29 SROS
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Subtask 12-36-29-942-097 C. Remove the safety precautions. (1) Remove the warning notice(s). Subtask 12-36-29-410-112 D. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Remove the access platform(s). (3) Close the landing gear doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-862-097 E. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R EFF : 701-749, 12-36-29 SROS
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**ON A/C ALL TASK 12-36-29-611-807 Replacement of the Hydraulic Fluid of the Green Hydraulic System with the Green Electric Pump WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job You must replace the fluid only if the acidity is higher than the values given into the task of the sampling for analysis (Ref. TASK 12-32-29-281-801).
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2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
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No specific No specific No specific No specific No specific No specific 98F12303001000 98F29103005001
blanking plug circuit breaker(s) safety clip(s) flexible hose plug type E0053R8B3APNE access platform 1.8 m (5 ft. 11 in.) container 100 l (26.4169 USgal) 1 HYDRAULIC CONNECTOR 1 TBD
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-801 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-863-801 29-10-00-611-801 29-11-43-600-802 29-11-43-600-807 29-11-44-600-801 29-11-45-600-801 29-14-00-614-804 32-11-15-400-801 32-12-00-010-801 32-12-00-410-801
Fill the Green Hydraulic Reservoir with a Hydraulic Service Cart Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Pressurize the Green Hydraulic System with the Electric Pump Drainage of the Green Hydraulic Reservoir Servicing of the (Forward) Engine-Pump Case-Drain Filter Element 5013JM1 Servicing of the Engine-Pump Case Drain Filter (5013JM1) Servicing of the Green Reservoir LP-Filter (5011JM1) Servicing of the Green HP Filter (5111JM101,5111JM102) Pressurization of the Hydraulic Reservoirs with external bench Installation of the MLG Bogie-Alignment Pitch Trimmer (Weight on Wheels) Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-42-00-870-801
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32-42-12-000-801 32-42-12-400-801 71-00-00-720-816 71-00-00-720-828 12-36-29-991-085
Bleeding the Normal Braking System at the Wheel Brakes Removal of the Hydraulic Brake Filter (5200GG) Installation of the Hydraulic Brake Filter (5200GG) Test No. 2 - Engine Motor Leak Test (Dry Method) Thrust Reverser Cowl Doors Open Dry Motoring Engine Fig. 346
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 12-36-29-991-086
Fig. 347
**ON A/C 701-749, 12-36-29-991-086-A
Fig. 347A
**ON A/C ALL 12-36-29-991-099 12-36-29-991-091
Fig. 348 Fig. 349
3. __________ Job Set-up Subtask 12-36-29-860-165 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Pressurize the Green hydraulic system (Ref. TASK 29-00-00-863-801). (3) On the panel 114VU, set the flap and slat control lever to the position 1. (4) On the ECAM Engine/Warning Display, the indication 1+F comes into view.
EFF : ALL 12-36-29 SROS
Page B383 Jan 01/07
(5) On the HYD section of the maintenance panel 285VU, make sure that the LEAK MEASUREMENT VALVES/G pushbutton switch is pushed (the OFF legend is on). (6) On the Green HP manifold 5103JM, disconnect the pressure switches 7JS1 and 19CE1. On the free end make a short circuit between the pins A and B with a plug type E0053R8B3APNE. Subtask 12-36-29-865-156 B. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------722VU HYD SOV ENG 2 NORM 19JG R34 722VU HYD SOV BUS SWTG 8JG R33 742VU HYD FIRE ENG 1 SOV 15JG2 D75 742VU HYD FIRE ENG 2 SOV 15JG1 D72 Subtask 12-36-29-010-114 C. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Put an access platform at the zone 147. Subtask 12-36-29-680-062 D. Drain the reservoir of the Green hydraulic system (Ref. TASK 29-10-00611-801). Subtask 12-36-29-420-090 R
E. Connection of the Flexible Hose to the LP Manifold 5004JM. (Ref. Fig. 346/TASK 12-36-29-991-085) **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, (Ref. Fig. 347/TASK 12-36-29-991-086)
EFF : ALL 12-36-29 SROS
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Hydraulic Connections for the Replacement of the Fluid Figure 346/TASK 12-36-29-991-085
EFF : ALL 12-36-29 SROS
Page B385 Jan 01/07
Green Hydraulic System-Schematic Diagram Figure 347/TASK 12-36-29-991-086 R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page B386 Jan 01/07
**ON A/C 701-749, (Ref. Fig. 347A/TASK 12-36-29-991-086-A) **ON A/C ALL (1) On the LP filter 5011JM1: (a) Disconnect the tube (1) from the LP filter 5011JM1. (b) Put a blanking plug on the Green LP filter 5011JM1. (c) Loosen the tube (1) on the Green LP manifold 5004JM. (d) Turn the tube (1) 90 deg. and connect a flexible hose (2). R R R
(e) Connect at the end of the flexible hose (2) a TBD (98F29103005001) (3).
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(f) Tighten the tube (1) on the Green LP manifold 5004JM. (2) Put a container to collect the fluid. (3) Fill the Green hydraulic reservoir. (4) Pressurize the Green hydraulic reservoir (Ref. TASK 29-14-00-614804). Subtask 12-36-29-420-097 F. Connection of the Fill Cart Unit to the suction port 5132JM1. (Ref. Fig. 348/TASK 12-36-29-991-099) (1) Open the green ground service panel. (2) Connect the HYDRAULIC CONNECTOR (98F12303001000) to 5132JM1. (3) Connect the Fill Cart Unit to the adaptor 98F12303001000. (4) Operate the Fill Cart Unit. CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE FROM THE FILL UNIT CART _______ IS NOT MORE THAN 4 BARS (58.0150 PSI). TOO MUCH PRESSURE CAN CAUSE DAMAGE TO THE SYSTEM.
EFF : ALL 12-36-29 SROS
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Green Hydraulic System-Schematic Diagram Figure 347A/TASK 12-36-29-991-086-A R EFF : 701-749, 12-36-29 SROS
Page B388 Jan 01/07
Connection between the Fill Unit Cart and the Ground Service Panel Figure 348/TASK 12-36-29-991-099 EFF : ALL 12-36-29 R SROS
Page B389 Jan 01/07
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Operate the hydraulic service cart and monitor the increase of the fluid level on the reservoir hydraulic quantity indicator 5JS.
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(5) Stop the flow when the pointer is in the center position on the reservoir hydraulic quantity indicator 5JS. 4. Procedure _________ **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, (Ref. Fig. 347/TASK 12-36-29-991-086) **ON A/C 701-749, (Ref. Fig. 347A/TASK 12-36-29-991-086-A)
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**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499,
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Subtask 12-36-29-611-178-A
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A. Replacement of the Fluid in the Engine Pump Suction and Pressure Lines.
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NOTE : The quantity of fluid in the Green system is approximately 210 ____ liters. This procedure permits to replace approximately 90 percent of the fluid.
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(1) -For 4000EM1.
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(a) Dry motor the engine (Ref. TASK 71-00-00-720-816) until you collect 20 l (5.2833 USgal) approximately.
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NOTE : Stop the dry motoring if the advisory low level comes into ____ view on the ECAM system (SD). If necessary fill the reservoir.
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(b) Stop the dry motoring.
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(c) Repeat the dry motoring until you collect 45 l (11.8876 USgal) approximately.
EFF : ALL 12-36-29 SROS
Page B390 Jan 01/07
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(2) -For 4000EM2.
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(a) Dry motor the engine (Ref. TASK 71-00-00-720-816) until you collect 20 l (5.2833 USgal) approximately.
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NOTE : Stop the dry motoring if the advisory low level comes into ____ view on the ECAM system (SD). If necessary fill the reservoir.
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(b) Stop the dry motoring.
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(c) Repeat the dry motoring until you collect 45 l (11.8876 USgal) approximately.
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**ON A/C 701-749,
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Subtask 12-36-29-611-178-B
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A. Replacement of the Fluid in the Engine Pump Suction and Pressure Lines.
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NOTE : The quantity of fluid in the Green system is approximately 210 ____ liters. This procedure permits to replace approximately 90 percent of the fluid.
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(1) -For 4000EM1.
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(a) Dry motor the engine (Ref. TASK 71-00-00-720-828) until you collect 20 l (5.2833 USgal) approximately.
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NOTE : Stop the dry motoring if the advisory low level comes into ____ view on the ECAM system (SD). If necessary fill the reservoir.
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(b) Stop the dry motoring.
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(c) Repeat the dry motoring until you collect 45 l (11.8876 USgal) approximately.
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(2) -For 4000EM2.
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(a) Dry motor the engine (Ref. TASK 71-00-00-720-828) until you collect 20 l (5.2833 USgal) approximately.
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NOTE : Stop the dry motoring if the advisory low level comes into ____ view on the ECAM system (SD). If necessary fill the reservoir.
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, 701-749, SROS
Page B391 Jan 01/07
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(b) Stop the dry motoring.
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(c) Repeat the dry motoring until you collect 45 l (11.8876 USgal) approximately.
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**ON A/C ALL Subtask 12-36-29-611-179-A B. Replacement of the Fluid in the Supply and Return Lines of the Primary Servocontrols (Ref. Fig. 349/TASK 12-36-29-991-091) (1) On the FLT CTL section of the panel 212VU, push the PRIM3 pushbutton switch (the OFF legend is off). (2) On the FLT CTL section of the panel 241VU, push the PRIM1 and SEC1 pushbutton switches (the OFF legend are off). (3) On the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/G pushbutton switch (the OFF legend is off). (4) On the ground service manifold (5109JM1), open the valves which supply the right and left wings. CAUTION : STOP THE OPERATION OF: _______ - THE HYDRAULIC USERS (FLIGHT CONTROLS, ETC.) - THE ELECTRIC PUMP WHEN THE FLUID LEVEL GETS TO THE MIDDLE OF THE AMBER ZONE. IF NOT, AIR CAN GET INTO THE HYDRAULIC SYSTEM AND CAUSE CAVITATION OF THE PUMP. (5) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV) (the ON legend is on). (6) Do 2 cycles over the full travel range and make sure that the surfaces move. If they do not move, do the reset of the related computers while the pump operates. (7) Monitor the level of the fluid in the Green reservoir. If necessary, fill the Green reservoir with the fill unit cart. (8) Do the steps (5) and (6) again and then do one more cycle.
EFF : ALL 12-36-29 SROS
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Flight Control Operations Figure 349/TASK 12-36-29-991-091 EFF : ALL 12-36-29 R SROS
Page B393 Jan 01/07
(9) On the HYD section of the overhead panel 245VU: - Release the GREEN/ELEC/AUTO pushbutton switch (8JV) (the ON legend is off).
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(10) On the ground service manifold (5109JM1), close the valves for the right and left wings and open the valve for the aft fuselage. (11) On the HYD section of the overhead panel 245VU: - push the GREEN/ELEC/AUTO pushbutton switch (8JV) (the ON legend is on). (12) Operate the elevators over the full travel range two times. (13) Monitor the level of the fluid in the Green reservoir. If necessary, fill the Green reservoir with the fill unit cart. (14) Do the steps (11) and (12) again. (15) Operate the rudder over the full travel range two times. (16) Monitor the level of the fluid in the Green reservoir. If necessary fill the Green reservoir with the fill unit cart. (17) Do the steps (14) and (15) again. (18) On the HYD section of the overhead panel 245VU: - Release the GREEN/ELEC/AUTO pushbutton switch (8JV) (the ON legend is off).
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(19) Close the valve for the aft fuselage. Subtask 12-36-29-865-157 C. Make sure that this(these) circuit breaker(s) is(are) closed: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM 10CV X14 721VU SFCC 1 NORM AVAIL 10CW X13 722VU SFCC 2 FLAP 2CV T43 722VU SFCC 2 SLAT 2CW V40 742VU SFCC 1 SLAT 1CW L62 742VU SFCC 1 FLAP 1CV L61
EFF : ALL 12-36-29 SROS
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Subtask 12-36-29-611-180-A D. Replacement of the Fluid in the Flap and Slat Supply and Return System CAUTION : STOP THE OPERATION OF: _______ - THE HYDRAULIC USERS (FLIGHT CONTROLS, ETC.) - THE ELECTRIC PUMP WHEN THE FLUID LEVEL GETS TO THE MIDDLE OF THE AMBER ZONE. IF NOT, AIR CAN GET INTO THE HYDRAULIC SYSTEM AND CAUSE CAVITATION OF THE PUMP. (1) On the panel 114VU, make sure that the flap and slat control lever is in the position 1. (2) Make sure that the level of the Green Hydraulic reservoir is at the maximum level. If necessary fill the Green hydraulic reservoir . (3) On the ground service manifold (5109JM1), open the valves which supply the right and left wings. (4) On the HYD section of the overhead panel 245VU: - Push the GREEN/ELEC/AUTO pushbutton switch (8JV).
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(5) On the panel 114VU, set the flap and slat control lever to the position 2. (6) Monitor the level of the fluid in the Green reservoir. If necessary fill the Green reservoir with the fill unit cart. (7) On the HYD section of the overhead panel 245VU: - Release the GREEN/ELEC/AUTO pushbutton switch (8JV).
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(8) On the ground service manifold (5109JM1), close the valves for the right and left wings. Subtask 12-36-29-611-181 E. Replacement of the Fluid in the Normal Braking System CAUTION : STOP THE OPERATION OF: _______ - THE HYDRAULIC USERS (FLIGHT CONTROLS, ETC.) - THE ELECTRIC PUMP WHEN THE FLUID LEVEL GETS TO THE MIDDLE OF THE AMBER ZONE. IF NOT, AIR CAN GET INTO THE HYDRAULIC SYSTEM AND CAUSE CAVITATION OF THE PUMP. (1) Push and release the brake pedals one time.
R EFF : ALL 12-36-29 SROS
Page B395 Jan 01/07
(2) Replace the hydraulic brake filter 5200GG on the manifold 5105JM (Ref. TASK 32-42-12-000-801) and (Ref. TASK 32-42-12-400-801). (3) Push and release the brake pedals 5 times. (4) Fill the Green hydraulic reservoir with the Fill Cart Unit. Subtask 12-36-29-611-182-A F. Replacement of the Fluid in the Nose Wheel Steering System CAUTION : STOP THE OPERATION OF: _______ - THE HYDRAULIC USERS (FLIGHT CONTROLS, ETC.) - THE ELECTRIC PUMP WHEN THE FLUID LEVEL GETS TO THE MIDDLE OF THE AMBER ZONE. IF NOT, AIR CAN GET INTO THE HYDRAULIC SYSTEM AND CAUSE CAVITATION OF THE PUMP. (1) On the HYD section of the overhead panel 245VU: - Push the GREEN/ELEC/AUTO pushbutton switch (8JV).
R
(2) Operate the nose wheel steering over the full travel one time . (3) Monitor the level of the fluid in the Green reservoir. If necessary fill the Green hydraulic reservoir with the Fill Cart Unit. (4) Operate the nose wheel steering over full travel one time again. (5) On the HYD section of the overhead panel 245VU: - Release the GREEN/ELEC/AUTO pushbutton switch (8JV).
R
Subtask 12-36-29-611-183-A G. Replacement of the Fluid in the Landing Gear Door System CAUTION : STOP THE OPERATION OF: _______ - THE HYDRAULIC USERS (FLIGHT CONTROLS, ETC.) - THE ELECTRIC PUMP WHEN THE FLUID LEVEL GETS TO THE MIDDLE OF THE AMBER ZONE. IF NOT, AIR CAN GET INTO THE HYDRAULIC SYSTEM AND CAUSE CAVITATION OF THE PUMP. (1) Remove the access platform from the zone 147. (2) Fill the Green hydraulic reservoir to the maximum level . (3) On the HYD section of the overhead panel 245VU: - Push the GREEN/ELEC/AUTO pushbutton switch (8JV).
R
R EFF : ALL 12-36-29 SROS
Page B396 Jan 01/07
(4) Do 3 opening cycles of the NLG doors. (5) Monitor the level of the fluid in the Green reservoir. If necessary fill the Green hydraulic reservoir . (6) Do 3 opening cycles of the right MLG doors. (7) Monitor the level of the fluid in the Green reservoir. If necessary, fill the Green hydraulic reservoir . (8) Do 3 opening cycles of the left MLG doors. (9) Monitor the level of the fluid in the Green reservoir. If necessary fill the Green hydraulic reservoir . (10) On the HYD section of the overhead panel 245VU: - Release the GREEN/ELEC/AUTO pushbutton switch (8JV).
R
(11) Install the access platform at the zone 147. 5. Close-up ________ **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 12-36-29-420-091 A. Connection of the hydraulic tube after replacement of the fluid R R
(1) Remove the flexible hose (2) and the restricting union (3). (2) Remove the blanking plug from the filter (5011JM1). (3) Loosen the tube (1), turn the tube 90 deg. and connect to the filter (5011JM1). (4) Tighten the tube (1) on the Green LP manifold (5004JM). (5) Replace these hydraulic filters: - the HP filters 5111JM101 and 5111JM102 (Ref. TASK 29-11-45-600801), - the LP filter 5011JM1 (Ref. TASK 29-11-44-600-801), - the two case drain filters 5013JM1 (Ref. TASK 29-11-43-600-802).
EFF : ALL 12-36-29 SROS
Page B397 Jan 01/07
**ON A/C 701-749, Subtask 12-36-29-420-091-A A. Connection of the hydraulic tube after replacement of the fluid R R
(1) Remove the flexible hose (2) and the restricting union (3). (2) Remove the blanking plug from the filter (5011JM1). (3) Loosen the tube (1), turn the tube 90 deg. and connect to the filter (5011JM1). (4) Tighten the tube (1) on the Green LP manifold (5004JM). (5) Replace these hydraulic filters: - the HP filters 5111JM101 and 5111JM102 (Ref. TASK 29-11-45-600801), - the LP filter 5011JM1 (Ref. TASK 29-11-44-600-801), - the two case drain filters 5013JM1 (Ref. TASK 29-11-43-600-807). **ON A/C ALL Subtask 12-36-29-020-059 B. Disconnect the Hydraulic Connector. (1) Disconnect the HYDRAULIC CONNECTOR (98F12303001000) from the port 5132JM1. (2) Disconnect the HYDRAULIC CONNECTOR (98F12303001000) from the Fill Cart Unit. Subtask 12-36-29-942-098 C. Aircraft Maintenance Configuration (1) On the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/G pushbutton switch (the OFF legend is off). (2) On the Green HP manifold 5103JM, remove the plug type E0053R8B3APNE from the pressure switches 7JS1 and 19CE1 and connect the pressure switches 7JS1 and 19CE1.
EFF : ALL 12-36-29 SROS
Page B398 Jan 01/07
Subtask 12-36-29-865-158 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 8JG, 19JG. Subtask 12-36-29-942-099 E. Aircraft Maintenance Configuration (1) If the fire shutoff valves close, do a reset of the C/B 5JR. (2) Do the bleeding of the Normal braking system (Ref. TASK 32-42-00-870801). (3) Do the bleeding of the pitch trimmer (Ref. TASK 32-11-15-400-801). (4) Fill the Green hydraulic reservoir (Ref. TASK 12-12-29-611-801). (5) Operate the flight controls and monitor the reservoir level. (6) Each week, do a new sampling of the fluid (Ref. TASK 12-32-29-281801). Subtask 12-36-29-410-113 F. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Remove the access platform(s). (3) Close the landing gear doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-862-098 G. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
EFF : ALL 12-36-29 R SROS
Page B399 Jan 01/07
TASK 12-36-29-611-808 Replacement of the Hydraulic Fluid of the Blue Hydraulic System with the Blue Electric Pump WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job You must replace the fluid only if the acidity is higher than the values given into the task of the sampling for analysis (Ref. TASK 12-32-29-281-80100).
EFF : ALL 12-36-29 R SROS
Page C300 Jan 01/07
2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R R
No specific No specific No specific No specific 98F12303001000 98F29103005001
blanking plug plug type E0053R8B3APNE access platform 1.8 m (5 ft. 11 in.) container 100 l (26.4169 USgal) 1 HYDRAULIC CONNECTOR 1 TBD
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-803 12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-863-802 29-10-00-611-802 29-11-43-600-804 29-11-43-600-809 29-12-44-600-801 29-12-45-600-801 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 32-43-00-870-801 71-00-00-720-802 12-36-29-991-087
Fill the Blue Hydraulic Reservoir with a Hydraulic Service Cart Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Pressurize the Blue Hydraulic System with the Electric Pump Drainage of the Blue Hydraulic Reservoir Servicing of the (Aft) Engine-Pump Case-Drain Filter Element 5013JM2 Servicing of the Engine Pump Case Drain Filter (5013JM2) Servicing of the Blue Reservoir LP-Filter (5011JM2) Servicing of the Blue HP Filter (5111JM2) Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Bleeding the Alternate Braking System at the Wheel Brakes Dry Motoring Check Fig. 350
EFF : ALL 12-36-29 SROS
Page C301 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 12-36-29-991-088
Fig. 351
**ON A/C 701-749, 12-36-29-991-088-A
Fig. 351A
**ON A/C ALL 12-36-29-991-098 12-36-29-991-092
Fig. 352 Fig. 353
3. __________ Job Set-up Subtask 12-36-29-860-166 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-802). (3) On the panel 114VU, set the flap and slat control lever to the position 1. (4) On the ECAM Engine/Warning Display, the indication 1+F comes into view. (5) On the HYD section of the maintenance panel 285VU, make sure that the LEAK MEASUREMENT VALVES/B pushbutton switch is pushed (the OFF legend is on). (6) On the Blue HP manifold 6103JM, disconnect the pressure switches 7JS2 and 19CE2. On the free end make a short circuit between the pins A and B with a plug type E0053R8B3APNE.
EFF : ALL 12-36-29 R SROS
Page C302 Jan 01/07
Subtask 12-36-29-010-115 B. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Put an access platform at the zone 147. Subtask 12-36-29-680-063 C. Drain the reservoir of the Blue hydraulic system (Ref. TASK 29-10-00-611802). Subtask 12-36-29-420-092 R
D. Connection of the Flexible Hose to the LP Manifold 6005JM (Ref. Fig. 350/TASK 12-36-29-991-087) **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, (Ref. Fig. 351/TASK 12-36-29-991-088) **ON A/C 701-749, (Ref. Fig. 351A/TASK 12-36-29-991-088-A) **ON A/C ALL (1) On the LP filter 5011JM2: (a) Disconnect the flexible hose (2) from the Blue LP filter 5011JM2. (b) Put a blanking plug on the Blue LP filter 5011JM2.
R R R
(c) Connect at the end of the flexible hose (2) a TBD (98F29103005001) (3). (2) Put a container to collect the fluid. (3) Fill the Blue hydraulic reservoir (Ref. TASK 12-12-29-611-803). (4) Pressurize the Blue hydraulic reservoir (Ref. TASK 29-14-00-614-804).
EFF : ALL 12-36-29 SROS
Page C303 Jan 01/07
R
Hydraulic Connections for the Replacement of the Fluid Figure 350/TASK 12-36-29-991-087
EFF : ALL 12-36-29 SROS
Page C304 Jan 01/07
Blue Hydraulic System-Schematic Diagram Figure 351/TASK 12-36-29-991-088 R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page C305 Jan 01/07
Blue Hydraulic System-Schematic Diagram Figure 351A/TASK 12-36-29-991-088-A R EFF : 701-749, 12-36-29 SROS
Page C306 Jan 01/07
Subtask 12-36-29-420-098 E. Connection of the Fill Cart Unit to the suction port 5132JM2. (Ref. Fig. 352/TASK 12-36-29-991-098) (1) open the Blue ground service panel. (2) connect the HYDRAULIC CONNECTOR (98F12303001000) to the port 5132JM2 (3) connect the Fill Cart Unit to the HYDRAULIC CONNECTOR (98F12303001000). (4) operate the hydraulic service cart. CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE FROM THE FILL UNIT CART _______ IS NOT MORE THAN 4 BARS (58.0150 PSI). TOO MUCH PRESSURE CAN CAUSE DAMAGE TO THE SYSTEM. operate the hydraulic service cart and monitor the increase of the fluid level on the reservoir hydraulic quantity indicator 5JS. (5) stop the flow when the pointer is in the center position on the reservoir hydraulic quantity indicator 5JS. 4. Procedure _________ **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, (Ref. Fig. 351/TASK 12-36-29-991-088) **ON A/C 701-749, (Ref. Fig. 351A/TASK 12-36-29-991-088-A) **ON A/C ALL Subtask 12-36-29-611-184 A. Replacement of the Fluid in the Engine Pump Suction and Pressure Lines. NOTE : The quantity of fluid in the Blue system is approximately 150 ____ liters. This procedure permits to replace approximately 90 percent of the fluid.
EFF : ALL 12-36-29 R SROS
Page C307 Jan 01/07
Connection between the Fill Unit Cart and the Ground Service Panel Figure 352/TASK 12-36-29-991-098 EFF : ALL 12-36-29 R SROS
Page C308 Jan 01/07
(1) -FOR 4000EM2 (a) Dry motor the engine (Ref. TASK 71-00-00-720-802) until you collect 15 l (3.9625 USgal) NOTE : Stop the dry motoring if the advisory low level comes into ____ view on the ECAM system display (SD). If necessary fill the reservoir again. (b) Stop the dry motoring (c) Repeat the dry motoring until you collect 45 l (11.8876 USgal). Subtask 12-36-29-611-185 B. Replacement of the Fluid in the Supply and Return Lines of the Primary Servocontrols (Ref. Fig. 353/TASK 12-36-29-991-092) (1) On the panel 212VU, push the SEC2, PRIM2 and PRIM3 pushbutton switches (the OFF legend are off). (2) On the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/B pushbutton switch (the OFF legend is off). (3) On the ground service manifold 5109JM2 open the valves which supply the right and left wing. CAUTION : STOP THE OPERATION OF: _______ - THE HYDRAULIC USERS (FLIGHT CONTROLS, ETC.) - THE ELECTRIC PUMP WHEN THE FLUID LEVEL GETS TO THE MIDDLE OF THE AMBER ZONE. IF NOT, AIR CAN GET INTO THE HYDRAULIC SYSTEM AND CAUSE CAVITATION OF THE PUMP. (4) On the HYD section of the overhead panel 245VU: - push the BLUE/ELEC pushbutton switch (4JC) (the ON legend is on). (5) Do 2 cycles over the full travel range and make sure that the surfaces move. If they do not move, do the reset of the related computers while the pump operates. (6) Monitor the level of the fluid in the Blue reservoir. If necessary, fill the Blue hydraulic reservoir with the Fill Cart Unit. (7) Do the steps (4) and (5) again and then do one more cycle.
EFF : ALL 12-36-29 R SROS
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Flight Control Operations Figure 353/TASK 12-36-29-991-092 EFF : ALL 12-36-29 R SROS
Page C310 Jan 01/07
(8) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC) (the ON legend is off). (9) On the ground service manifold 5109JM2 close the valves for the right and left wing and open the valve for the aft fuselage. (10) On the HYD section of the overhead panel 245VU: - push the BLUE/ELEC pushbutton switch (4JC) (the ON legend is on). (11) Operate the elevators over the full travel range two times. (12) Monitor the level of the fluid in the Blue reservoir. If necessary fill the Blue hydraulic reservoir with the Fill Cart Unit. (13) Do the steps (8) and (9) again. (14) Operate the rudder over the full travel range two times. (15) Monitor the level of the fluid in the Blue reservoir. If necessary fill the Blue hydraulic reservoir (Ref. TASK 12-12-29-611-803). (16) Do the steps (11) and (12) again. (17) Operate the THS one time. (18) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC) (the ON legend is off). (19) Close the valve for the aft fuselage. Subtask 12-36-29-865-159 C. Make sure that this(these) circuit breaker(s) is(are) closed: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM AVAIL 10CW X13 722VU SFCC 2 SLAT 2CW V40 742VU SFCC 1 SLAT 1CW L62
R EFF : ALL 12-36-29 SROS
Page C311 Jan 01/07
Subtask 12-36-29-611-186 D. Replacement of the Fluid in the Slat Supply and Return System (Ref. Fig. 353/TASK 12-36-29-991-092) CAUTION : STOP THE OPERATION OF: _______ - THE HYDRAULIC USERS (FLIGHT CONTROLS, ETC.) - THE ELECTRIC PUMP WHEN THE FLUID LEVEL GETS TO THE MIDDLE OF THE AMBER ZONE. IF NOT, AIR CAN GET INTO THE HYDRAULIC SYSTEM AND CAUSE CAVITATION OF THE PUMP. (1) On the panel 114VU, make sure that the flap and slat control lever is in the position 1. (2) Make sure that the level of the Blue hydraulic reservoir is at the maximum level. If necessary fill the Blue hydraulic reservoir with the Fill Cart Unit. (3) On the ground service manifold 5109JM2 open the valves which supply the right and left wing. (4) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC). (5) On the panel 114VU, set the flap and slat control lever to the position 2. (6) Monitor the level of the fluid in the Blue reservoir. If necessary fill the Blue hydraulic reservoir with the Fill Cart Unit. (7) On the HYD section of the overhead panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC). (8) On the ground service manifold 5109JM2 close the valves for the right and left wing. Subtask 12-36-29-611-187 E. Replacement of the Fluid in the Alternate Brake System CAUTION : STOP THE OPERATION OF: _______ - THE HYDRAULIC USERS (FLIGHT CONTROLS, ETC.) - THE ELECTRIC PUMP WHEN THE FLUID LEVEL GETS TO THE MIDDLE OF THE AMBER ZONE. IF NOT, AIR CAN GET INTO THE HYDRAULIC SYSTEM AND CAUSE CAVITATION OF THE PUMP.
R EFF : ALL 12-36-29 SROS
Page C312 Jan 01/07
(1) On the PARK BRK control panel 117VU, set the PARK BRK switch to the OFF position. (2) On the HYD section of the panel 245VU: - push the BLUE/ELEC pushbutton switch (4JC). (3) Push and release the brake pedals five times. (4) On the HYD section of the panel 245VU: - release the BLUE/ELEC pushbutton switch (4JC). 5. Close-up ________ **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 12-36-29-420-093 A. Connection of the hydraulic tube after replacement of the fluid R R
(1) Remove the flexible hose (2) and the restricting union (3). (2) Remove the blanking plug from the filter (5011JM2). (3) Connect the flexible hose to the filter (5011JM2). (4) Replace these hydraulic - the HP filter 5111JM2 - the LP filter 5011JM2 - the case drain filter
filters: (Ref. TASK 29-12-45-600-801), (Ref. TASK 29-12-44-600-801), 5013JM2 (Ref. TASK 29-11-43-600-804).
**ON A/C 701-749, Subtask 12-36-29-420-093-A A. Connection of the hydraulic tube after replacement of the fluid R R
(1) Remove the flexible hose (2) and the restricting union (3). (2) Remove the blanking plug from the filter (5011JM2). (3) Connect the flexible hose to the filter (5011JM2).
EFF : ALL 12-36-29 SROS
Page C313 Jan 01/07
(4) Replace these hydraulic - the HP filter 5111JM2 - the LP filter 5011JM2 - the case drain filter
filters: (Ref. TASK 29-12-45-600-801), (Ref. TASK 29-12-44-600-801), 5013JM2 (Ref. TASK 29-11-43-600-809).
**ON A/C ALL Subtask 12-36-29-020-057 B. Disconnect the Hydraulic Connector. (1) Disconnect the HYDRAULIC CONNECTOR (98F12303001000) from the port 5132JM2. (2) Disconnect the HYDRAULIC CONNECTOR (98F12303001000) from the Fill Cart Unit. Subtask 12-36-29-942-101 C. Aircraft Maintenance Configuration (1) On the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/B pushbutton switch (the OFF legend is off). (2) On the Blue HP manifold 6103JM, remove the plug type E0053R8B3APNE from the pressure switches 7JS2 and 19CE2 and connect the pressure switches 7JS2 and 19CE2. (3) Do the bleeding of the alternate brake system (Ref. TASK 32-43-00870-801). (4) Fill the Blue hydraulic reservoir (Ref. TASK 12-12-29-611-803). (5) Operate the flight controls and monitor the reservoir level. If necessary fill the Blue hydraulic reservoir (Ref. TASK 12-12-29-611803). (6) Each week, do a new sampling of the fluid (Ref. TASK 12-32-29-281801).
EFF : ALL 12-36-29 R SROS
Page C314 Jan 01/07
Subtask 12-36-29-410-114 D. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Remove the access platform(s). (3) Close the landing gear doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-862-099 E. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
EFF : ALL 12-36-29 R SROS
Page C315 Jan 01/07
TASK 12-36-29-611-809 Replacement of the Hydraulic Fluid of the Yellow Hydraulic System with the Yellow Electric Pump WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job You must replace the fluid only if the acidity is higher than the values given into the task of the sampling for analysis (Ref. TASK 12-32-29-281-80100).
EFF : ALL 12-36-29 R SROS
Page C316 Jan 01/07
2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R R
No specific No specific No specific No specific No specific 98F12303001000 98F29103005001
blanking plug flexible hose plug type E0053R8B3APNE access platform 1.8 m (5 ft. 11 in.) container 100 l (26.4169 USgal) 2 HYDRAULIC CONNECTOR 1 TBD
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-32-29-281-801 24-41-00-861-801 24-41-00-862-801 29-00-00-863-803 29-10-00-611-803 29-11-43-600-804 29-11-43-600-809 29-13-44-600-801 29-13-45-600-801 29-14-00-614-804 32-12-00-010-801 32-12-00-410-801 52-30-00-010-801 52-30-00-410-801 71-00-00-720-802 12-36-29-991-089
Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Pressurize the Yellow Hydraulic System with the Electric Pump Drainage of the Yellow Hydraulic Reservoir Servicing of the (Aft) Engine-Pump Case-Drain Filter Element 5013JM2 Servicing of the Engine Pump Case Drain Filter (5013JM2) Servicing of the Yellow Reservoir LP-Filter (5011JM3) Servicing of the Yellow HP Filter (5111JM3) Pressurization of the Hydraulic Reservoirs with external bench Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Opening of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Closing of the FWD and AFT Cargo-Compartment Doors with the Yellow Electric Pump Dry Motoring Check Fig. 354
EFF : ALL 12-36-29 SROS
Page C317 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 12-36-29-991-090
Fig. 355
**ON A/C 701-749, 12-36-29-991-090-A
Fig. 355A
**ON A/C ALL 12-36-29-991-097 12-36-29-991-093
Fig. 356 Fig. 357
3. __________ Job Set-up Subtask 12-36-29-860-167 A. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Pressurize the Yellow hydraulic system (Ref. TASK 29-00-00-863-803). (3) On the panel 114VU, set the flap and slat control lever to the position 1. (4) On the ECAM Engine/Warning Display, the indication 1+F comes into view. (5) On the HYD section of the maintenance panel 285VU, make sure that the LEAK MEASUREMENT VALVES/Y pushbutton switch is pushed (the OFF legend is on). (6) On the Yellow HP manifold 7103JM, disconnect the pressure switches 7JS3 and 19CE3. On the free end make a short circuit between the pins A and B with a plug type E0053R8B3APNE.
EFF : ALL 12-36-29 R SROS
Page C318 Jan 01/07
Subtask 12-36-29-010-116 B. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Put an access platform at the zone 147. Subtask 12-36-29-680-064 C. Drain the Reservoir of the Yellow Hydraulic System (Ref. TASK 29-10-00611-803) Subtask 12-36-29-420-094 R
D. Connection of the Flexible Hose to the LP Filter 5011JM3 (Ref. Fig. 354/TASK 12-36-29-991-089) **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, (Ref. Fig. 355/TASK 12-36-29-991-090) **ON A/C 701-749, (Ref. Fig. 355A/TASK 12-36-29-991-090-A) **ON A/C ALL (1) On the LP filter 5011JM3: (a) Disconnect the hose (1) from the LP filter 5011JM3. (b) Put a blanking plug on the hose (1). (c) Connect the flexible hose (2) to the LP filter 5011JM3.
R R R
(d) Connect at the end of the flexible hose (2) a TBD (98F29103005001) (3). (2) Put a container to collect the fluid. (3) Fill the Yellow hydraulic reservoir at the maximum level with the Fill Cart Unit.
EFF : ALL 12-36-29 SROS
Page C319 Jan 01/07
R
Hydraulic Connections for the Replacement of the Fluid Figure 354/TASK 12-36-29-991-089
EFF : ALL 12-36-29 SROS
Page C320 Jan 01/07
Yellow Hydraulic System-Schematic Diagram Figure 355/TASK 12-36-29-991-090 R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, SROS
Page C321 Jan 01/07
Yellow Hydraulic System-Schematic Diagram Figure 355A/TASK 12-36-29-991-090-A R EFF : 701-749, 12-36-29 SROS
Page C322 Jan 01/07
(4) Pressurize the Yellow hydraulic reservoir (Ref. TASK 29-14-00-614804). Subtask 12-36-29-420-096 E. Connection of the FILL CART UNIT to the suction port 5132JM3. (Ref. Fig. 356/TASK 12-36-29-991-097) (1) Open the yellow ground service panel. (2) Connect the HYDRAULIC CONNECTOR (98F12303001000) to the 5132JM3. (3) Connect the FILL CART UNIT to the adaptor HYDRAULIC CONNECTOR (98F12303001000). (4) Operate the hydraulic service cart. CAUTION : MAKE SURE THAT THE SUPPLY PRESSURE FROM THE FILL UNIT CART _______ IS NOT MORE THAN 4 BARS (58.0150 PSI). TOO MUCH PRESSURE CAN CAUSE DAMAGE TO THE SYSTEM. Operate the hydraulic service cart and monitor the increase of the fluid level in the reservoir hydraulic quantity indicator 5JS. (5) Stop the flow when the pointer is in the center position on the reservoir hydraulic quantity indicator 5JS. 4. Procedure _________ (Ref. Fig. 354/TASK 12-36-29-991-089) **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, (Ref. Fig. 355/TASK 12-36-29-991-090) **ON A/C 701-749, (Ref. Fig. 355A/TASK 12-36-29-991-090-A)
EFF : ALL 12-36-29 R SROS
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Connection between the Fill Unit Cart and the Ground Service Panel Figure 356/TASK 12-36-29-991-097 EFF : ALL 12-36-29 R SROS
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**ON A/C ALL Subtask 12-36-29-611-188 A. Replacement of the Fluid in the Engine Pump Suction and Pressure lines. NOTE : The quantity of fluid in the Yellow system is approximately 110 ____ liters. This procedure permits to replace approximately 90 percent of the fluid. (1) -For 4000EM3 (a) Dry motor the engine (Ref. TASK 71-00-00-720-802) until you collect 13l approximately. NOTE : Stop the dry motoring if the advisory low level comes into ____ view on the ECAM system display. (b) If necessary fill the reservoir again. (c) Repeat the dry motoring until you collect 40l approximately. Subtask 12-36-29-611-189-A B. Replacement of the Fluid in the Supply and Return Lines of the Primary Servocontrols (Ref. Fig. 357/TASK 12-36-29-991-093) (1) On the FLT CTL section of the panel 212VU, push the SEC2, PRIM2 and PRIM3 pushbutton switches (the OFF legend are off). (2) On the FLT CTL section of the panel 241VU, push the SEC1 pushbutton switch (the OFF legend is off). (3) On the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/Y pushbutton switch (the OFF legend is off). (4) On the ground service manifold (5109JM3), open the valves which supply the right and left wings. CAUTION : STOP THE OPERATION OF: _______ - THE HYDRAULIC USERS (FLIGHT CONTROLS, ETC.) - THE ELECTRIC PUMP WHEN THE FLUID LEVEL GETS TO THE MIDDLE OF THE AMBER ZONE. IF NOT, AIR CAN GET INTO THE HYDRAULIC SYSTEM AND CAUSE CAVITATION OF THE PUMP.
R EFF : ALL 12-36-29 SROS
Page C325 Jan 01/07
Flight Control Operations Figure 357/TASK 12-36-29-991-093 EFF : ALL 12-36-29 R SROS
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(5) On the HYD section of the overhead panel 245VU: - push the YELLOW/ELEC/AUTO pushbutton switch (6JJ) (the ON legend is on). (6) Do 2 cycles over the full travel range and make sure that the surfaces move. If they do not move, do the reset of the related computers while the pump is operates. (7) Monitor the level of the fluid in the Yellow reservoir. If necessary fill the Yellow reservoir. (8) Do the steps (5) and (6) again and then do one more cycle. (9) On the HYD section of the overhead panel 245VU: - release the YELLOW/ELEC/AUTO pushbutton switch (6JJ) (the ON legend is off). (10) On the ground service manifold (5109JM3), close the valves for the right and left wings and open the valves for the aft fuselage. (11) On the HYD section of the overhead panel 245VU: - push the YELLOW/ELEC/AUTO pushbutton switch (6JJ) (the ON legend is on). (12) Operate the elevators over the full travel range two times. (13) Monitor the level of the fluid in the Yellow reservoir. If necessary fill the Yellow reservoir with the fill unit cart. (14) Do the steps (11) and (12) again. (15) Operate the rudder over the full travel range two times. (16) Monitor the level of the fluid in the Yellow reservoir. If necessary fill the Yellow reservoir with the fill unit cart. (17) Do the steps (14) and (15) again. (18) Operate the THS one time. (19) On the HYD section of the overhead panel 245VU: - release the YELLOW/ELEC/AUTO pushbutton switch (6JJ) (the ON legend is off). (20) Close the valve for the aft fuselage.
EFF : ALL 12-36-29 R SROS
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Subtask 12-36-29-865-160 C. Make sure that this(these) circuit breaker(s) is(are) closed: ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU SFCC 1 NORM 10CV X14 722VU SFCC 2 FLAP 2CV T43 742VU SFCC 1 FLAP 1CV L61 Subtask 12-36-29-611-190-A D. Replacement of the Fluid in the Flap Supply and Return System (Ref. Fig. 357/TASK 12-36-29-991-093) CAUTION : STOP THE OPERATION OF: _______ - THE HYDRAULIC USERS (FLIGHT CONTROLS, ETC.) - THE ELECTRIC PUMP WHEN THE FLUID LEVEL GETS TO THE MIDDLE OF THE AMBER ZONE. IF NOT, AIR CAN GET INTO THE HYDRAULIC SYSTEM AND CAUSE CAVITATION OF THE PUMP. (1) On the panel 114VU, make sure that the flap and slat control lever is in the position 1. (2) Make sure that the level of the Yellow reservoir is at the maximum level. If necessary fill the Yellow reservoir with the fill unit cart. (3) On the ground service manifold (5109JM3), open the valves which supply the right and the left wings. (4) On the HYD section of the overhead panel 245VU: - release the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (5) On the panel 114VU, set the flap and slat control lever to the position 2. (6) Monitor the level of the fluid in the Yellow reservoir. If necessary fill the Yellow reservoir with the fill unit cart. (7) On the HYD section of the overhead panel 245VU: - release the YELLOW/ELEC/AUTO pushbutton switch (6JJ). (8) On the ground service manifold (5109JM3), close the valves for the right and left wings.
EFF : ALL 12-36-29 R SROS
Page C328 Jan 01/07
Subtask 12-36-29-611-191 E. Replacement of the Fluid in the Cargo Doors System CAUTION : STOP THE OPERATION OF: _______ - THE HYDRAULIC USERS (FLIGHT CONTROLS, ETC.) - THE ELECTRIC PUMP WHEN THE FLUID LEVEL GETS TO THE MIDDLE OF THE AMBER ZONE. IF NOT, AIR CAN GET INTO THE HYDRAULIC SYSTEM AND CAUSE CAVITATION OF THE PUMP. Do one opening and closing cycle of the cargo doors (Ref. TASK 52-30-00010-801) and (Ref. TASK 52-30-00-410-801). 5. Close-up ________ **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 12-36-29-420-095 A. Connection of the hydraulic tube after replacement of the fluid (1) Remove the flexible hose (2) from the LP filter 5011JM3. (2) Remove the blanking plug from the hose (1). (3) Connect the hose (1) to the LP filter 5011JM3. (4) Replace these hydraulic - the HP filter 5111JM3 - the LP filter 5011JM3 - the case drain filter
filters: (Ref. TASK 29-13-45-600-801), (Ref. TASK 29-13-44-600-801), 5013JM2 (Ref. TASK 29-11-43-600-804).
**ON A/C 701-749, Subtask 12-36-29-420-095-A A. Connection of the hydraulic tube after replacement of the fluid (1) Remove the flexible hose (2) from the LP filter 5011JM3. (2) Remove the blanking plug from the hose (1). (3) Connect the hose (1) to the LP filter 5011JM3.
EFF : ALL 12-36-29 R SROS
Page C329 Jan 01/07
(4) Replace these hydraulic - the HP filter 5111JM3 - the LP filter 5011JM3 - the case drain filter
filters: (Ref. TASK 29-13-45-600-801), (Ref. TASK 29-13-44-600-801), 5013JM2 (Ref. TASK 29-11-43-600-809).
**ON A/C ALL Subtask 12-36-29-020-058 B. Disconnect the Hydraulic Connector. (1) Disconnect the HYDRAULIC CONNECTOR (98F12303001000) from the port 5132JM3. (2) Disconnect the HYDRAULIC CONNECTOR (98F12303001000) from the Fill Cart Unit. Subtask 12-36-29-942-103 C. Get Access (1) On the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVES/Y pushbutton switch (the OFF legend is off). (2) On the Yellow HP manifold 7103JM, remove the plug type E0053R8B3APNE from the pressure switches 7JS3 and 19CE3 and connect the pressure switches 7JS3 and 19CE3. (3) Fill the Yellow hydraulic reservoir with the Fill Cart Unit. (4) Operate the flight controls and monitor the reservoir level. If necessary fill the Yellow hydraulic reservoir with the Fill Cart Unit. (5) Each week, do a new sampling of the fluid (Ref. TASK 12-32-29-281801). Subtask 12-36-29-410-115 D. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Remove the access platform(s).
R EFF : ALL 12-36-29 SROS
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(3) Close the landing gear doors (Ref. TASK 32-12-00-410-801). Subtask 12-36-29-862-100 E. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
EFF : ALL 12-36-29 R SROS
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TASK 12-36-29-611-804 Reclaim the Fluid in the Green Hydraulic System WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. 1. __________________ Reason for the Job Clean the fluid when the rate of particle contamination is higher than the values of NSA 307-110 class 9 (Ref. TASK 12-32-29-281-80100). 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
ground hydraulic supply hydraulic ground power supply access platform 1.8 m (5 ft. 11 in.)
EFF : ALL 12-36-29 R SROS
Page C332 Jan 01/07
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-801 12-12-29-611-802 12-32-29-281-801 24-41-00-861-801 29-00-00-280-801 29-00-00-280-801 29-00-00-863-801 29-00-00-864-801 29-10-00-200-804 29-10-00-200-806 29-10-00-200-806 29-14-00-614-804 31-60-00-860-801 32-12-00-010-801 32-12-00-410-801 78-31-11-200-801 78-31-41-200-802
Fill the Green Hydraulic Reservoir with a Hydraulic Service Cart Fill the Green Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A Check of the Green Hydraulic System after Operation of the Engine Pumps in Possible Starvation or Cavitation condition. Check of the Green Hydraulic System after Operation of the Engine Pumps in Possible Starvation or Cavitation Condition. Pressurize the Green Hydraulic System with the Ground Hydraulic Supply Depressurize the Green Hydraulic System (Pressurized with the Hydraulic Ground Supply) Check of the Clogging Indicators of the Hydraulic System Filter in the Hydraulics Compartment. Check of the Clogging Indicators of the Hydraulic System Filters on the Engines. Check of the Clogging Indicators of the Hydraulic System Filters on the Engines. Pressurization of the Hydraulic Reservoirs with external bench EIS Start Procedure Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Inspection of the Hydraulic Filter Assembly Element Inspection of the Thrust Reverser Isolation Control Unit
3. __________ Job Set-up Subtask 12-36-29-861-056 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801).
EFF : ALL 12-36-29 R SROS
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Subtask 12-36-29-860-132 B. Aircraft Maintenance Configuration (1) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00860-801). (2) On the ECAM control panel, push the HYD key (on the SD the HYD page comes into view). (3) On the SD make sure that: - the LO AIR PRESS indication of the Green reservoir is not shown. If it is shown, pressurize the reservoir (Ref. TASK 29-14-00-614-804). - the level index of the Green reservoir shows that the fluid level is correct. If the level of the fluid is not correct add fluid with a service cart or with a hand pump (Ref. TASK 12-12-29-611-801), (Ref. TASK 12-12-29-611-802). (4) Connect the suction and delivery lines of the hydraulic ground power supply to the aircraft connectors, access door 197CB: - 5132JM1 suction - 5131JM1 delivery. Subtask 12-36-29-010-102 C. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Put an access platform in position at the zone 147. 4. Procedure _________ **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 12-36-29-611-100 A. Clean the Fluid in the Green Hydraulic System NOTE : If the fluid is contaminated because of engine pump deterioration, ____ do the procedure for the check of the Green hydraulic system after operation of the engine pump in possible cavitation condition (Ref. TASK 29-00-00-280-801). (1) Pressurize the system that you must clean with the ground hydraulic supply (Ref. TASK 29-00-00-863-801).
EFF : ALL 12-36-29 R SROS
Page C334 Jan 01/07
(2) Operate all the flight controls and brakes to make a fluid flow in the system. (3) Do a fluid sampling for particle contamination (Ref. TASK 12-32-29281-801). (4) Continue to operate the flight controls and the brakes until you get a sample that is correct (contamination lower than NSA 307-110 class 9). (5) Do a check of the clogging indicator of: - the case drain filter 5013JM1 (Ref. TASK 29-10-00-200-806), - the HP filters 5111JM101, 5111JM102 (Ref. TASK 29-10-00-200-804), - the LP filter 5011JM1 (Ref. TASK 29-10-00-200-804), - the HCU filter 5001EG1 (Ref. TASK 78-31-11-200-801). **ON A/C 701-749, Subtask 12-36-29-611-100-A A. Clean the Fluid in the Green Hydraulic System NOTE : If the fluid is contaminated because of engine pump deterioration, ____ do the procedure for the check of the Green hydraulic system after operation of the engine pump in possible cavitation condition (Ref. TASK 29-00-00-280-801). (1) Pressurize the system that you must clean with the ground hydraulic supply (Ref. TASK 29-00-00-863-801). (2) Operate all the flight controls and brakes to make a fluid flow in the system. (3) Do a fluid sampling for particle contamination (Ref. TASK 12-32-29281-801). (4) Continue to operate the flight controls and the brakes until you get a sample that is correct (contamination lower than NSA 307-110 class 9). (5) Do a check of the clogging indicator of: - the case drain filter 5013JM1 (Ref. TASK 29-10-00-200-806), - the HP filters 5111JM101, 5111JM102 (Ref. TASK 29-10-00-200-804), - the LP filter 5011JM1 (Ref. TASK 29-10-00-200-804), - the filter element installed on the Isolation Control Unit 4117KS (Ref. TASK 78-31-41-200-802).
EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, 701-749, R SROS
Page C335 Jan 01/07
**ON A/C ALL 5. Close-up ________ Subtask 12-36-29-864-050 A. Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). Subtask 12-36-29-860-133 B. Disconnect the suction and delivery lines of the hydraulic ground power supply from the aircraft connectors, access door 197CB: - 5132JM1 suction - 5131JM1 delivery. Subtask 12-36-29-410-101 C. Close Access (1) Close the MLG doors (Ref. TASK 32-12-00-410-801) (2) Remove the access platform(s).
EFF : ALL 12-36-29 R SROS
Page C336 Jan 01/07
TASK 12-36-29-611-805 Reclaim the Fluid in the Blue Hydraulic System WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. 1. __________________ Reason for the Job Clean the fluid when the rate of particle contamination is higher than the values of NSA 307-110 class 9 (Ref. TASK 12-32-29-281-80100). 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
ground hydraulic supply hydraulic ground power supply access platform 1.8 m (5 ft. 11 in.)
EFF : ALL 12-36-29 R SROS
Page C337 Jan 01/07
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-803 12-12-29-611-804 12-32-29-281-801 24-41-00-861-801 29-00-00-280-802 29-00-00-280-802 29-00-00-863-802 29-00-00-864-802 29-10-00-200-804 29-10-00-200-806 29-10-00-200-806 29-14-00-614-804 31-60-00-860-801 32-12-00-010-801 32-12-00-410-801 78-31-11-200-801 78-31-41-200-802
Fill the Blue Hydraulic Reservoir with a Hydraulic Service Cart Fill the Blue Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A Check of the Blue Hydraulic System after Operation of the Engine Pump in Possible Starvation or Cavitation Condition. Check of the Blue Hydraulic System after Operation of the Engine Pump in Possible Starvation or Cavitation Condition. Pressurize the Blue Hydraulic System with the Ground Hydraulic Supply Depressurize the Blue Hydraulic System (Pressurized with the Hydraulic Ground Supply) Check of the Clogging Indicators of the Hydraulic System Filter in the Hydraulics Compartment. Check of the Clogging Indicators of the Hydraulic System Filters on the Engines. Check of the Clogging Indicators of the Hydraulic System Filters on the Engines. Pressurization of the Hydraulic Reservoirs with external bench EIS Start Procedure Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Inspection of the Hydraulic Filter Assembly Element Inspection of the Thrust Reverser Isolation Control Unit
3. __________ Job Set-up Subtask 12-36-29-861-057 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801).
EFF : ALL 12-36-29 R SROS
Page C338 Jan 01/07
Subtask 12-36-29-860-134 B. Aircraft Maintenance Configuration (1) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00860-801). (2) On the ECAM control panel, push the HYD key (on the SD the HYD page comes into view). (3) On the SD make sure that: - the LO AIR PRESS indication of the Blue reservoir is not shown. If it is shown, pressurize the reservoir (Ref. TASK 29-14-00-614-804), - the level index of the Blue reservoir shows that the fluid level is correct. If the level of the fluid is not correct add fluid with a service cart or with a hand pump (Ref. TASK 12-12-29-611-803), (Ref. TASK 12-12-29-611-804). (4) Connect the suction and delivery lines of the hydraulic ground power supply to the aircraft connectors, access door 195BB: - 5132JM2 suction - 5131JM2 delivery. Subtask 12-36-29-010-103 C. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Put an access platform in position at the zone 195. 4. Procedure _________ **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 12-36-29-611-101 A. Clean the Fluid in the Blue Hydraulic System NOTE : If the fluid is contaminated because of engine pump deterioration, ____ do the procedure for the check of the Blue hydraulic system after operation of the engine pump in possible cavitation condition (Ref. TASK 29-00-00-280-802). (1) Pressurize the system that you must clean with the ground hydraulic supply (Ref. TASK 29-00-00-863-802).
EFF : ALL 12-36-29 R SROS
Page C339 Jan 01/07
(2) Operate all the flight controls and brakes to make a fluid flow in the system. (3) Do a fluid sampling for particle contamination (Ref. TASK 12-32-29281-801). (4) Continue to operate the flight controls and the brakes until you get a sample that is correct (contamination lower than NSA 307-110 class 9). (5) Do a check of the clogging indicator of: - the case drain filter 5013JM2 (Ref. TASK 29-10-00-200-806), - the HP filter 5111JM2 (Ref. TASK 29-10-00-200-804), - the LP filter 5011JM1 (Ref. TASK 29-10-00-200-804), - the HCU filter 5001EG2 (Ref. TASK 78-31-11-200-801). **ON A/C 701-749, Subtask 12-36-29-611-101-A A. Clean the Fluid in the Blue Hydraulic System NOTE : If the fluid is contaminated because of engine pump deterioration, ____ do the procedure for the check of the Blue hydraulic system after operation of the engine pump in possible cavitation condition (Ref. TASK 29-00-00-280-802). (1) Pressurize the system that you must clean with the ground hydraulic supply (Ref. TASK 29-00-00-863-802). (2) Operate all the flight controls and brakes to make a fluid flow in the system. (3) Do a fluid sampling for particle contamination (Ref. TASK 12-32-29281-801). (4) Continue to operate the flight controls and the brakes until you get a sample that is correct (contamination lower than NSA 307-110 class 9). (5) Do a check of the clogging indicator of: - the case drain filter 5013JM2 (Ref. TASK 29-10-00-200-806), - the HP filter 5111JM2 (Ref. TASK 29-10-00-200-804), - the LP filter 5011JM1 (Ref. TASK 29-10-00-200-804), - the filter element installed on the Isolation Control Unit 4117KS (Ref. TASK 78-31-41-200-802).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, 701-749, SROS
Page C340 Jan 01/07
**ON A/C ALL 5. Close-up ________ Subtask 12-36-29-864-051 A. Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802). Subtask 12-36-29-860-135 B. Disconnect the suction and delivery lines of the hydraulic ground power supply from the aircraft connectors, access door 195BB: - 5132JM2 suction - 5131JM2 delivery. Subtask 12-36-29-410-102 C. Close Access (1) Close the MLG doors (Ref. TASK 32-12-00-410-801). (2) Remove the access platform(s).
EFF : ALL 12-36-29 R SROS
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TASK 12-36-29-611-806 Reclaim the Fluid in the Yellow Hydraulic System WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. 1. __________________ Reason for the Job Clean the fluid when the rate of particle contamination is higher than the values of NSA 307-110 class 9 (Ref. TASK 12-32-29-281-80100). 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
ground hydraulic supply hydraulic ground power supply access platform 1.8 m (5 ft. 11 in.)
EFF : ALL 12-36-29 R SROS
Page C342 Jan 01/07
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-805 12-12-29-611-806 12-32-29-281-801 24-41-00-861-801 29-00-00-280-803 29-00-00-863-803 29-00-00-864-803 29-10-00-200-804 29-10-00-200-806 29-14-00-614-804 31-60-00-860-801 32-12-00-010-801 32-12-00-410-801 78-31-11-200-801 78-31-41-200-802
Fill the Yellow Hydraulic Reservoir with a Hydraulic Service Cart Fill the Yellow Hydraulic Reservoir with a Hand Pump Sampling for Analysis Energize the Aircraft Electrical Circuits from the External Power A Check of the Yellow Hydraulic System after Operation of the Engine Pump in Possible Starvation or Cavitation Condition. Pressurize the Yellow Hydraulic System with the Ground Hydraulic Supply Depressurize the Yellow Hydraulic System (Pressurized with the Hydraulic Ground Supply) Check of the Clogging Indicators of the Hydraulic System Filter in the Hydraulics Compartment. Check of the Clogging Indicators of the Hydraulic System Filters on the Engines. Pressurization of the Hydraulic Reservoirs with external bench EIS Start Procedure Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Inspection of the Hydraulic Filter Assembly Element Inspection of the Thrust Reverser Isolation Control Unit
3. __________ Job Set-up Subtask 12-36-29-861-058 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801).
EFF : ALL 12-36-29 R SROS
Page C343 Jan 01/07
Subtask 12-36-29-860-136 B. Aircraft Maintenance Configuration (1) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00860-801). (2) On the ECAM control panel, push the HYD key (on the SD the HYD page comes into view). (3) On the SD make sure that: - the LO AIR PRESS indication of the Yellow reservoir is not shown. If it is shown, pressurize the reservoir (Ref. TASK 29-14-00-614804), - the level index of the Yellow reservoir shows that the fluid level is correct. If the level of the fluid is not correct add fluid with a service cart or with a hand pump (Ref. TASK 12-12-29-611-805), (Ref. TASK 12-12-29-611-806). (4) Connect the suction and delivery lines of the hydraulic ground power supply to the aircraft connectors, access door 196BB: - 5132JM3 suction - 5131JM3 delivery. Subtask 12-36-29-010-104 C. Get Access (1) Open the MLG doors (Ref. TASK 32-12-00-010-801). (2) Put an access platform in position at the zone 196. 4. Procedure _________ **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 12-36-29-611-102 A. Clean the Fluid in the Yellow Hydraulic System NOTE : If the fluid is contaminated because of engine pump deterioration, ____ do the procedure for the check of the Yellow hydraulic system after operation of the engine pump in possible cavitation condition (Ref. TASK 29-00-00-280-803).
EFF : ALL 12-36-29 R SROS
Page C344 Jan 01/07
(1) Pressurize the system that you must clean with the ground hydraulic supply (Ref. TASK 29-00-00-863-803). (2) Operate all the flight controls to make a fluid flow in the system. (3) Do a fluid sampling for particle contamination (Ref. TASK 12-32-29281-801). (4) Continue to operate the flight controls until you get a sample that is correct (contamination lower than NSA 307-110 class 9). (5) Do a check of the clogging indicator of: - the case drain filter 5013JM2 (Ref. TASK 29-10-00-200-806), - the HP filter 5111JM2 (Ref. TASK 29-10-00-200-804), - the LP filter 5011JM2 (Ref. TASK 29-10-00-200-804), - the HCU filter 5001EG2 (Ref. TASK 78-31-11-200-801). **ON A/C 701-749, Subtask 12-36-29-611-102-A A. Clean the Fluid in the Yellow Hydraulic System NOTE : If the fluid is contaminated because of engine pump deterioration, ____ do the procedure for the check of the Yellow hydraulic system after operation of the engine pump in possible cavitation condition (Ref. TASK 29-00-00-280-803). (1) Pressurize the system that you must clean with the ground hydraulic supply (Ref. TASK 29-00-00-863-803). (2) Operate all the flight controls to make a fluid flow in the system. (3) Do a fluid sampling for particle contamination (Ref. TASK 12-32-29281-801). (4) Continue to operate the flight controls until you get a sample that is correct (contamination lower than NSA 307-110 class 9). (5) Do a check of the clogging indicator of: - the case drain filter 5013JM2 (Ref. TASK 29-10-00-200-806), - the HP filter 5111JM2 (Ref. TASK 29-10-00-200-804), - the LP filter 5011JM2 (Ref. TASK 29-10-00-200-804), - the filter element installed on the Isolation Control Unit 4117KS (Ref. TASK 78-31-41-200-802).
R EFF : 001-049, 201-249, 251-252, 255-299, 12-36-29 301-399, 401-449, 451-499, 701-749, SROS
Page C345 Jan 01/07
**ON A/C ALL 5. Close-up ________ Subtask 12-36-29-864-052 A. Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803). Subtask 12-36-29-860-137 B. Disconnect the suction and delivery lines of the hydraulic ground power supply from the aircraft connectors, access door 196BB: - 5132JM3 suction - 5131JM3 delivery. Subtask 12-36-29-410-103 C. Close Access (1) Close the MLG doors (Ref. TASK 32-12-00-410-801). (2) Remove the access platform(s).
EFF : ALL 12-36-29 R SROS
Page C346 Jan 01/07
TASK 12-36-29-615-801 Clean the Fluid in the Green Hydraulic System (with the Pall Purifier) WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job Clean the fluid when the chemical analysis (without the acid number check) is equal to or higher than the values of the NSA 307-110 (Ref. TASK 12-32-29-281-80100). 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------HSPA181-380J
1 HYDRAULIC PURIFIER
EFF : ALL 12-36-29 R SROS
Page C347 Jan 01/07
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-801 12-12-29-611-802 24-41-00-861-801 24-41-00-862-801 29-00-00-864-801 29-14-00-614-801 29-14-00-614-804 31-60-00-860-801
Fill the Green Hydraulic Reservoir with a Hydraulic Service Cart Fill the Green Hydraulic Reservoir with a Hand Pump Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Depressurize the Green Hydraulic System (Pressurized with the Hydraulic Ground Supply) Depressurization of the Green Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench EIS Start Procedure
3. __________ Job Set-up Subtask 12-36-29-010-117 A. Get Access (1) Open the access door 197CB. Subtask 12-36-29-860-168 B. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (3) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00860-801).
EFF : ALL 12-36-29 R SROS
Page C348 Jan 01/07
(4) On the SD, make sure that: - the LO AIR PRESS indication of the Green reservoir is not in view. If this indication is shown pressurize the reservoir (Ref. TASK 2914-00-614-801), - the level index of the Green reservoir shows that the fluid level is correct. If the level is not correct, add fluid to the reservoir with a hydraulic service cart (Ref. TASK 12-12-29-611-801) or with a hand pump (Ref. TASK 12-12-29-611-802). (5) Connect the suction and delivery lines of the hydraulic Pall Purifier to the hydraulic ground service panel: - 5132JM1 ground connector-suction, - 5131JM1 ground connector-delivery. (6) On the FLT CTL section of the overhead panel 241VU, make sure that the PRIM1 and SEC1 pushbutton switches are pushed (the OFF and FAULT legends are off). (7) On the FLT CTL section of the overhead panel 212VU make sure that the PRIM2, PRIM3 and SEC2 pushbutton switches are pushed (the OFF and FAULT legends are off). (8) On the ECAM control panel, push the F/CTL key (on the SD the F/CTL page comes into view). (9) Make sure that the IRS are not aligned. 4. Procedure _________ Subtask 12-36-29-615-050 A. Clean the Fluid in the Green Hydraulic System WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED _______ ON THE LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE _______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE. NOTE : Obey the manufacturer instructions for the hydraulic purifier. ____ (1) Set the main pump of the HYDRAULIC PURIFIER (HSPA181-380J) to ON.
EFF : ALL 12-36-29 R SROS
Page C349 Jan 01/07
(2) Operate the purifier for 30 minutes. (3) Operation of the flight controls from the CAPT side. (a) Move the side stick in the full nose-up, nose down, left roll and right roll directions: - the ailerons, the elevators, the spoiler 5 move in relation to the side stick orders. (b) Put the side stick in the neutral position: - the surfaces go back to the neutral position. (c) Push the right then the left pedal to the mechanical stop: - the rudder moves in relation to the pedals orders. (d) Put the pedals in the neutral position: - the rudder goes back to the neutral position. (e) Put the SPEED BRAKE control lever in the FULL position: - the spoilers 1 and 5 extend. (f) Put the SPEED BRAKE control lever in the RET position: - the spoilers 1 and 5 retract. (g) On the panel 114VU, put the flap and slat control lever in the FULL position: - the slats and the flaps extend. (h) On the panel 114VU, put the flap and slat control lever in the O position: - the slats and the flaps retract. (4) Do a check of the water contents indicators at the purifier. (5) If the water contents is high, continue to operate the purifier. (6) Stop the cleaning procedure, when the water contents indicator shows a low water contents. (7) Set the main pump of the HYDRAULIC PURIFIER (HSPA181-380J) to OFF. (8) Disconnect the suction and delivery lines of the hydraulic purifier from the aircraft connectors.
EFF : ALL 12-36-29 R SROS
Page C350 Jan 01/07
5. Close-up ________ Subtask 12-36-29-860-169 A. Put the aircraft back to its operational configuration. (1) On the SD, make sure that: - the LO AIR PRESS indication of the Green reservoir is not in view. If this indication is shown pressurize the Green hydraulic reservoir (Ref. TASK 29-14-00-614-804). - the level index of the Green reservoir shows that the fluid level is correct. If the level is not correct, add fluid to the reservoir with a hydraulic service cart (Ref. TASK 12-12-29-611-801) or with a hand pump (Ref. TASK 12-12-29-611-802). (2) Make sure that the work area is clean and clear of tools and other items. (3) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). Subtask 12-36-29-410-116 B. Close Access (1) Close the access door 197CB.
EFF : ALL 12-36-29 R SROS
Page C351 Jan 01/07
TASK 12-36-29-615-802 Clean the Fluid in the Blue Hydraulic System (with the Pall Purifier) WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job Clean the fluid when the chemical analysis (without the acid number check) is equal to or higher than the values of the NSA 307-110 (Ref. TASK 12-32-29-281-80100). 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------HSPA181-380J
1 HYDRAULIC PURIFIER
EFF : ALL 12-36-29 SROS
Page C352 Jan 01/07
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-803 12-12-29-611-804 24-41-00-861-801 24-41-00-862-801 29-00-00-864-802 29-14-00-614-801 29-14-00-614-804 31-60-00-860-801
Fill the Blue Hydraulic Reservoir with a Hydraulic Service Cart Fill the Blue Hydraulic Reservoir with a Hand Pump Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Depressurize the Blue Hydraulic System (Pressurized with the Hydraulic Ground Supply) Depressurization of the Green Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench EIS Start Procedure
3. __________ Job Set-up Subtask 12-36-29-010-118 A. Get Access (1) Open the access door 195BB. Subtask 12-36-29-860-170 B. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802). (3) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00860-801).
EFF : ALL 12-36-29 SROS
Page C353 Jan 01/07
(4) On the SD, make sure that: - the LO AIR PRESS indication of the Blue reservoir is not in view. If this indication is shown pressurize the reservoir (Ref. TASK 2914-00-614-801), - the level index of the Blue reservoir shows that the fluid level is correct. If the level is not correct, add fluid to the reservoir with a hydraulic service cart (Ref. TASK 12-12-29-611-803) or with a hand pump (Ref. TASK 12-12-29-611-804). (5) Connect the suction and delivery lines of the hydraulic Pall Purifier to the hydraulic ground service panel: - 5132JM2 ground connector-suction, - 5131JM2 ground connector-delivery. (6) On the FLT CTL section of the overhead panel 241VU make sure that the PRIM1 and SEC1 pushbutton switches are pushed (the OFF and FAULT legends are off). (7) On the FLT CTL section of the overhead panel 212VU make sure that the PRIM2, PRIM3 and SEC2 pushbutton switches are pushed (the OFF and FAULT legends are off). (8) On the ECAM control panel, push the F/CTL key (on the SD the F/CTL page comes into view). (9) Make sure that the IRS are not aligned. 4. Procedure _________ Subtask 12-36-29-615-051 A. Clean the Fluid in the Blue Hydraulic System WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED _______ ON THE LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE _______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE. NOTE : Obey the manufacturer instructions for the hydraulic purifier. ____ (1) Set the main pump of the HYDRAULIC PURIFIER (HSPA181-380J) to ON.
EFF : ALL 12-36-29 SROS
Page C354 Jan 01/07
(2) Operate the purifier for 30 minutes. (3) Operation of the flight controls from the CAPT side. (a) Move the side stick in the full nose-up, nose down, left roll and right roll directions: - the inboard ailerons and one elevator move in relation to the side stick orders. (b) Put the side stick in the neutral position: - the surfaces go back to the neutral position. (c) Push the right then the left pedal to the mechanical stop: - the rudder moves in relation to the pedals orders. (d) Put the pedals in the neutral position: - the rudder goes back to the neutral position. (e) On the center pedestal, move the pitch-trim control wheel in the full nose-up and nose-down directions: - the THS moves in relation to the wheel orders. (f) Put the pitch-trim control wheel in the neutral position: - the THS goes back to the neutral position. (g) Put the SPEED BRAKE control lever in the FULL position: - the spoilers 2 and 3 extend. (h) Put the SPEED BRAKE control lever in the RET position: - the spoilers 2 and 3 retract. (i) On the panel 114VU, put the flap and slat control lever in the FULL position: - the slats extend. (j) On the panel 114VU, put the flap and slat control lever in the O position: - the slats retract. (4) Do a check of the water contents indicators of the purifier. (5) If the water contents is high, continue to operate the purifier. (6) Stop the cleaning procedure when the water contents indicator shows a low water contents. (7) Set the main pump of the HYDRAULIC PURIFIER (HSPA181-380J) to OFF.
EFF : ALL 12-36-29 SROS
Page C355 Jan 01/07
(8) Disconnect the suction and delivery lines of the hydraulic purifier from the aircraft connectors. 5. Close-up ________ Subtask 12-36-29-860-171 A. Put the aircraft back to its operational configuration. (1) On the SD, make sure that: - the LO AIR PRESS indication of the Blue reservoir is not in view. If this indication is shown pressurize the Blue hydraulic reservoir (Ref. TASK 29-14-00-614-804). - the level index of the Blue reservoir shows that the fluid level is correct. If the level is not correct, add fluid to the reservoir with a hydraulic service cart (Ref. TASK 12-12-29-611-803) or with a hand pump (Ref. TASK 12-12-29-611-804). (2) Make sure that the work area is clean and clear of tools and other items. (3) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). Subtask 12-36-29-410-117 B. Close Access (1) Close the access door 195BB.
EFF : ALL 12-36-29 SROS
Page C356 Jan 01/07
TASK 12-36-29-615-803 Clean the Fluid in the Yellow Hydraulic System (with the Pall Purifier) WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES. _______ WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS. WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS UNTIL THEY ARE COOL. _______ THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY. WARNING : DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR _______ MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH. WARNING : MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN _______ POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC _______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. 1. __________________ Reason for the Job Clean the fluid when the chemical analysis (without the acid number check) is equal to or higher than the values of the NSA 307-110 (Ref. TASK 12-32-29-281-80100). 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------HSPA181-380J
1 HYDRAULIC PURIFIER
EFF : ALL 12-36-29 SROS
Page C357 Jan 01/07
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-12-29-611-805 12-12-29-611-806 24-41-00-861-801 24-41-00-862-801 29-00-00-864-803 29-14-00-614-801 29-14-00-614-804 31-60-00-860-801
Fill the Yellow Hydraulic Reservoir with a Hydraulic Service Cart Fill the Yellow Hydraulic Reservoir with a Hand Pump Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Depressurize the Yellow Hydraulic System (Pressurized with the Hydraulic Ground Supply) Depressurization of the Green Hydraulic Reservoir with Ground Equipment Pressurization of the Hydraulic Reservoirs with external bench EIS Start Procedure
3. __________ Job Set-up Subtask 12-36-29-010-119 A. Get Access (1) Open the access door 196BB. Subtask 12-36-29-860-172 B. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803). (3) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00860-801).
EFF : ALL 12-36-29 SROS
Page C358 Jan 01/07
(4) On the SD make sure that: - the LO AIR PRESS indication of the Yellow reservoir is not in view. If this indication is shown pressurize the reservoir (Ref. TASK 2914-00-614-801). - the level index of the Yellow reservoir shows that the fluid level is correct. If the level is not correct, add fluid to the reservoir with a hydraulic service cart (Ref. TASK 12-12-29-611-805) or with a hand pump (Ref. TASK 12-12-29-611-806). (5) Connect the suction and delivery lines of the hydraulic Pall Purifier to the hydraulic ground service panel: - 5132JM3 ground connector-suction, - 5131JM3 ground connector-delivery. (6) On the FLT CTL section of the overhead panel 241VU make sure that the PRIM1 and SEC1 pushbutton switches are pushed (the OFF and FAULT legends are off). (7) On the FLT CTL section of the overhead panel 212VU make sure that the PRIM2, PRIM3 and SEC2 pushbutton switches are pushed (the OFF and FAULT legends are off). (8) On the ECAM control panel, push the F/CTL key (on the SD the F/CTL page comes into view). (9) Make sure that the IRS are not aligned. 4. Procedure _________ Subtask 12-36-29-615-052 A. Clean the Fluid in the Yellow Hydraulic System WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED _______ ON THE LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR. WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE _______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE. NOTE : Obey the manufacturer instructions for the hydraulic purifier. ____ (1) Set the main pump of the HYDRAULIC PURIFIER (HSPA181-380J) to ON.
EFF : ALL 12-36-29 SROS
Page C359 Jan 01/07
(2) Operate the purifier for 30 minutes. (3) Operation of the flight controls from the CAPT side. (a) Move the side stick in the full nose-up, nose-down, left roll and right roll directions: - the outboard aileron, spoilers and one elevator move in relation to the side stick orders. (b) Put the side stick in the neutral position: - the surfaces go back to the neutral position. (c) Push the right then the left pedal to the mechanical stop. - the rudder moves in relation to the pedals orders. (d) Put the pedals in the neutral position: - the rudder goes back to the neutral position. (e) On the center pedestal, move the pitch-trim control wheel in the full nose-up and nose-down directions: - the THS moves in relation to the wheel orders. (f) Put the pitch-trim control wheel in the neutral position: - the THS goes back to the neutral position. (g) Put the SPEED BRAKE control lever in the FULL position: - the spoilers 4 and 6 extend (h) Put the SPEED BRAKE control lever in the RET position. - the spoilers 4 and 6 retract. (i) On the panel 114VU, put the flap and slat control lever in the FULL position: - the flaps extend. (j) On the panel 114VU, put the flap and slat control lever in the O position: - the flaps retract. (4) Do a check of the water contents indicators at the purifier. (5) If the water contents is high, continue to operate the purifier. (6) Stop the cleaning procedure when the water contents indicator shows a low water contents. (7) Set the main pump of the HYDRAULIC PURIFIER (HSPA181-380J) to OFF.
EFF : ALL 12-36-29 SROS
Page C360 Jan 01/07
(8) Disconnect the suction and delivery lines of the hydraulic purifier from the aircraft connectors. 5. Close-up ________ Subtask 12-36-29-860-173 A. Put the aircraft back to its operational configuration. (1) On the SD, make sure that: - the LO AIR PRESS indication of the Yellow reservoir is not in view. If this indication is shown pressurize the (Ref. TASK 29-14-00-614804). - the level index of the Yellow reservoir shows that the fluid level is correct. If the level is not correct, add fluid to the reservoir with a hydraulic service cart (Ref. TASK 12-12-29-611-805) or with a hand pump (Ref. TASK 12-12-29-611-806). (2) Make sure that the work area is clean and clear of tools and other items. (3) Depressurize the aircraft hydraulic systems (Ref. TASK 24-41-00-862-801). Subtask 12-36-29-410-118 B. Close Access (1) Close the access door 196BB.
EFF : ALL 12-36-29 SROS
Page C361 Jan 01/07
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