A330 Amm Ch05
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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 05 __________
L.E.P. 1- 7 Revised to Reflect this revision indicating new,revised, and/or deleted pages T. OF C. Revised to reflect this revision 1 05-00-00 Layout Improved or Effectivity Updated 1 05-21-00 601- 602
CORRECTION/ADDITION/AMPLIFICATION REVISED TASK TITLE. WARNING/NOTE/REASON FOR THE JOB AMENDED
ALL ALL
05-21-20 604- 611
Effectivity updated MOD.40056D16566 INCORPORATED A330-ELECTRICAL SYSTEMS-DEFINE THE DA-MBB BASIC PA RT
05-21-90 609- 610
Layout Improved or Effectivity Updated
05-22-40 605
Layout Improved or Effectivity Updated
05-23-10 601- 604
CORRECTION/ADDITION/AMPLIFICATION ADDED REMOVAL OF THE PUMP SEALING CASE.
ALL
05-23-20 620
CORRECTION/ADDITION/AMPLIFICATION DELETED INSPECTION OF BEARING 5 AREA.
ALL
05-23-30 617
CORRECTION/ADDITION/AMPLIFICATION REVISED TO SPECIFY HTP AREA.
ALL
05-25-00 601- 603, 605- 606
CORRECTION/ADDITION/AMPLIFICATION ADDED NOTE. WARNING/NOTE/REASON FOR THE JOB AMENDED
001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 701-749, ALL
CORRECTION/ADDITION/AMPLIFICATION
ALL
05-25-20
ALL
05-HIGHLIGHTS Page REVISION NO. 32 SROS
1 of 4 Jan 01/07
-------------------------------------------------------------------------------------CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES -------------------------------------------------------------------------------------604- 605 05-25-30 601- 608
DELETED ACCESS PANELS 522BT, 522CT, 622BT AND 622CT. CORRECTION/ADDITION/AMPLIFICATION ADDED NOTE. WARNING/NOTE/REASON FOR THE JOB AMENDED
ALL
05-27-10 605, 607608
CORRECTION/ADDITION/AMPLIFICATION ADDED NOTE. WARNING/NOTE/REASON FOR THE JOB AMENDED
ALL
05-28-00 602- 603
CORRECTION/ADDITION/AMPLIFICATION ADDED NOTE. WARNING/NOTE/REASON FOR THE JOB AMENDED
ALL
CORRECTION/ADDITION/AMPLIFICATION ADDED NOTE. WARNING/NOTE/REASON FOR THE JOB AMENDED
ALL
05-28-10 601
ALL
ALL
ALL
ALL
05-50-00 1
Layout Improved or Effectivity Updated
05-51-00 12
Layout Improved or Effectivity Updated
05-51-11 601- 607, 609- 673
Effectivity updated MOD.40000S10002 INCORPORATED FUSELAGE-DEFINE FORWARD SECTION 11/12 OF THE BASIC A/C MOD.44599H13557 REMOVED WINGS - GENERAL - DEFINE WINGS FOR A330-200/300B (230 MTOW) AIRCRAFT SB 31-3091 01 INCORPORATED INDICATING/RECORDING SYSTEMS - ACMS - INSTALL ACMS ENHANCED DMU SOFTWARE STEP 4.1 FOR A330 WITH PW ENGINES LAYOUT IMPROVED/MATERIAL RELOCATED
05-51-14 601- 604, 607- 608, 611- 616
05-51-16 601
ALL ALL 002-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 701-749, ALL
TECHNICAL CORRECTIONS CLERICAL CORRECTION CORRECTION/ADDITION/AMPLIFICATION NEW WARNING ADDED. TITLE OF TASK(S) DATA UPDATED WARNING/NOTE/REASON FOR THE JOB AMENDED
ALL
WARNING/NOTE/REASON FOR THE JOB AMENDED
ALL
ALL ALL ALL
05-HIGHLIGHTS Page REVISION NO. 32 SROS
2 of 4 Jan 01/07
-------------------------------------------------------------------------------------CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES -------------------------------------------------------------------------------------05-51-18 622
TECHNICAL CORRECTIONS CLERICAL CORRECTION
05-51-19 601- 602
Effectivity updated TECHNICAL CORRECTIONS ADDED WARNING FOR HEALTH RECOMMENDATION CORRECTION/ADDITION/AMPLIFICATION NEW WARNING ADDED. WARNING/NOTE/REASON FOR THE JOB AMENDED
05-51-21 601, 604
ALL
001-049, 255-299, 451-499, 001-049, 255-299, 451-499, ALL
TECHNICAL CORRECTIONS CLERICAL CORRECTION TITLE OF TASK(S) DATA UPDATED
ALL
TECHNICAL CORRECTIONS CLERICAL CORRECTION TITLE OF TASK(S) DATA UPDATED
ALL
CORRECTION/ADDITION/AMPLIFICATION CROSS-REFERENCE MODIFIED. WARNING/NOTE/REASON FOR THE JOB AMENDED
ALL
05-51-24 617
TECHNICAL CORRECTIONS CLERICAL CORRECTION
ALL
05-51-25 601- 605, 610, 620625, 631
TITLE OF TASK(S) DATA UPDATED WARNING/NOTE/REASON FOR THE JOB AMENDED
ALL ALL
05-51-26 601, 603, 605- 606, 608
Layout Improved or Effectivity Updated
05-51-42 602- 604
MOD.40307S10049 INCORPORATED POWER PLANT-DEFINE RR TRENT 768 POWER PLANT AND ASSOCIATED SYSTEMS EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
701-749,
LAYOUT IMPROVED/MATERIAL RELOCATED
ALL
05-51-22 602, 605 05-51-23 601
05-53-00 501- 510, 515- 516
201-249, 301-399, 701-749, 201-249, 301-399, 701-749,
251-252, 401-449,
ALL
ALL
ALL
001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499,
05-HIGHLIGHTS Page REVISION NO. 32 SROS
251-252, 401-449,
3 of 4 Jan 01/07
-------------------------------------------------------------------------------------CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES -------------------------------------------------------------------------------------05-54-00 201 05-57-00 201
TECHNICAL CORRECTIONS CLERICAL CORRECTION. WARNING/NOTE/REASON FOR THE JOB AMENDED
ALL
TECHNICAL CORRECTIONS CLERICAL CORRECTION. WARNING/NOTE/REASON FOR THE JOB AMENDED
ALL
ALL
ALL
05-HIGHLIGHTS Page REVISION NO. 32 SROS
4 of 4 Jan 01/07
CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS 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.
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DATE Jan01/07 Jan01/04 Jan01/04 Jul01/06 Jul01/06 Jan01/04 Jan01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jan01/04 Jan01/04 Jan01/04 Jan01/04 Jan01/04 Jan01/04 Jul01/06 Jul01/06 Oct01/04 Oct01/04 Jul01/04 Jul01/04 Apr01/04 Jul01/05 Oct01/04 Apr01/04 Jul01/06 Apr01/04 Apr01/04 Jan01/06 Jul01/06 Jul01/06 Jan01/04 Jan01/06 Jan01/04 Jan01/06 Jul01/06 Jul01/06 Jan01/06
CH/SE/SU 05-21-60 05-21-60 05-21-70 05-21-70 05-21-70 05-21-70 05-21-70 05-21-70 05-21-90 05-21-90 05-21-90 05-21-90 05-21-90 05-21-90 05-21-90 05-21-90 05-21-90 05-21-90 05-21-90 05-21-90 05-21-90 05-21-90 05-21-90 05-21-90 05-21-90 05-22-00 05-22-00 05-22-00 05-22-10 05-22-10 05-22-10 05-22-10 05-22-10 05-22-10 05-22-20 05-22-20 05-22-20 05-22-20 05-22-20 05-22-20 05-22-20
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601 602 603 601 602 603 604 605 606 601 602 603 604 605 606 607
Jan01/04 Jan01/04 Jan01/04 Jan01/06 Apr01/98 Jan01/06 Jul01/06 Jul01/06 Jul01/06 Jan01/06 Jul01/06 Jul01/06 Jul01/06 Jan01/06 Jul01/06 Jul01/06
05-L.E.P. Page 1 Jan 01/07 SROS
CH/SE/SU 05-22-30 05-22-30 05-22-30 05-22-30 05-22-30 05-22-30 05-22-30 05-22-40 05-22-40 05-22-40 05-22-40 05-22-40 05-22-50 05-22-50 05-22-50 05-22-50 05-22-50 05-22-50 05-22-60 05-22-60 05-22-60 05-22-60 05-22-60 05-22-60 05-22-70 05-22-70 05-22-70 05-22-70 05-22-70 05-22-70 05-22-70 05-23-00 05-23-00 05-23-00 05-23-10 05-23-10 05-23-10 05-23-10 05-23-10 05-23-10 05-23-10 05-23-10 05-23-10 05-23-10 05-23-10 05-23-10 05-23-10 05-23-20 05-23-20 05-23-20
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601 602 603 604 605 606 607 601 602 603 604 605 601 602 603 604 605 606 601 602 603 604 605 606 601 602 603 604 605 606 607
Jan01/04 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jan01/07 Jan01/04 Jan01/04 Jan01/04 Jan01/04 Jul01/06 Jul01/06 Apr01/04 Jul01/06 Apr01/04 Jul01/06 Jul01/06 Jul01/06 Jan01/05 Jan01/05 Jan01/05 Jan01/05 Apr01/04 Apr01/04 Jan01/04
601 602 603 601 602 603 604 605 606 607 608 609 610 611 612 613 601 602 603
Jan01/04 Jan01/04 Jan01/04 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Oct01/04 Oct01/04 Oct01/04 Oct01/04 Oct01/04 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jan01/04 Jul01/04 Jan01/04
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604 605 606 607 608 609 610 611 612 613 614 615 616 617 618 619 620 621 622 623 624 625 626 601 602 603 604 605 606 607 608 609 610 611 612 613 614 615 616 617 618 619 620 621
Jan01/04 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jan01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jan01/07 Jul01/04 Jul01/04 Apr01/05 Jul01/06 Jul01/06 Jul01/06 Jan01/04 Jan01/04 Jan01/04 Jan01/04 Jan01/04 Jan01/04 Jul01/04 Jul01/04 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/07 Jan01/06 Jan01/06 Jan01/06 Jan01/06
601 602 603 601 602 603
Jan01/04 Jan01/04 Jan01/04 Jul01/05 Jul01/05 Jul01/05
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05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10
02 02 02 02 02 02 02 02 02 02 02 02 02 02 02 02 02 02 02 02 02 02 02 02 02 02 02 02 02 02 02 02 02 03 03 03 03 03 03 03 03 03 03 03 03 03 03 03 03 03 03
604 605 606 607 608 609 610 611 612 613 614 615 616 617 618 619 620 621 622 623 624 625 626 627 628 629 630 631 632 633 634 635 636 601 602 603 604 605 606 607 608 609 610 611 612 613 614 615 616 617 618
DATE 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 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jan01/05 Jul01/04 Jul01/04 Jul01/04 Jul01/04
05-L.E.P. Page 2 Jan 01/07 SROS
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05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-10 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50
03 03 03 03 03 03 03 03 03 03 03 03 03 03 03 03 03 03 02 02 02 02 02 02 02 02 02 02 02 02 02 02 02 02 02 02 02 02 02 02 03 03 03 03 03 03 03 03 03 03 03
619 620 621 622 623 624 625 626 627 628 629 630 631 632 633 634 635 636 601 602 603 604 605 606 607 608 609 610 611 612 613 614 615 616 617 618 619 620 621 622 601 602 603 604 605 606 607 608 609 610 611
DATE Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Apr01/05 Jul01/04 Apr01/05 Apr01/05 Jul01/04 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 Jul01/06 Jul01/06 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jan01/05 Jul01/04 Jul01/04 Jul01/04
CH/SE/SU
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05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50 05-24-50
03 03 03 03 03 03 03 03 03 03 03 03
612 613 614 615 616 617 618 619 620 621 622 623
Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jan01/05 Jul01/04 Apr01/05 Apr01/05 Apr01/05
601 602 603 604 605 606 607 601 602 603 604 605 606 607 608 601 602 603 604 605 606 607 608 601 602 603 604 605 606 607 608 609 610 611 612 601 602 603
Jan01/07 Jan01/07 Jan01/07 Jul01/05 Jan01/07 Jan01/07 Jul01/05 Jan01/04 Jan01/04 Jan01/04 Jan01/07 Jan01/07 Apr01/04 Apr01/05 Apr01/05 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jul01/04 Jul01/04 Jan01/04 Jan01/04 Jan01/04 Jan01/04 Jan01/04 Jan01/04 Apr01/05 Apr01/05 Apr01/05 Apr01/05 Jan01/04 Jan01/04 Jan01/04
05-25-00 05-25-00 05-25-00 05-25-00 05-25-00 05-25-00 05-25-00 05-25-20 05-25-20 05-25-20 05-25-20 05-25-20 05-25-20 05-25-20 05-25-20 05-25-30 05-25-30 05-25-30 05-25-30 05-25-30 05-25-30 05-25-30 05-25-30 05-25-40 05-25-40 05-25-40 05-25-40 05-25-40 05-25-40 05-25-40 05-25-40 05-25-40 05-25-40 05-25-40 05-25-40 05-25-50 05-25-50 05-25-50
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05-25-70 05-25-70 05-25-70 05-25-70 05-25-70 05-25-70 05-25-70 05-25-70 05-25-70 05-25-70 05-25-70 05-25-70 05-25-70 05-25-90 05-25-90 05-25-90 05-25-90
601 602 603 604 605 606 607 608 609 610 611 612 613 601 602 603 604
Jan01/06 Jan01/06 Jan01/04 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jul01/06 Jan01/04 Jan01/04 Jan01/04 Jan01/04
05-27-00 05-27-10 05-27-10 05-27-10 05-27-10 05-27-10 05-27-10 05-27-10 05-27-10 05-27-30 05-27-30 05-27-30 05-27-30 05-27-30 05-27-30 05-27-30 05-27-30 05-27-30
601 601 602 603 604 605 606 607 608 601 602 603 604 605 606 607 608 609
Jan01/04 Jan01/04 Jan01/04 Jan01/04 Jan01/04 Jan01/07 Jan01/06 Jan01/07 Jan01/07 Jan01/04 Oct01/04 Jul01/03 Jan01/04 Jan01/04 Jan01/04 Jan01/04 Jan01/04 Jan01/04
601 602 603 601 602 603 601 602 603 604 605 606 607 608
Jan01/04 Jan01/07 Jan01/07 Jan01/07 Jan01/04 Jan01/04 Jan01/04 Jan01/04 Apr01/04 Apr01/04 Jan01/04 Jul01/04 Jan01/04 Jan01/04
05-28-00 05-28-00 05-28-00 05-28-10 05-28-10 05-28-10 05-28-20 05-28-20 05-28-20 05-28-20 05-28-20 05-28-20 05-28-20 05-28-20
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05-28-20 05-28-20 05-28-20 05-28-20 05-28-20 05-28-20 05-28-20 05-28-20 05-28-20 05-28-20 05-28-20 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30
609 610 611 612 613 614 615 616 617 618 619 601 602 603 604 605 606 607 608 609 610 611 612 613 614 615 616 617 618 619 620 621 622 623
DATE Jul01/04 Apr01/04 Jul01/04 Jul01/04 Jul01/04 Apr01/04 Apr01/04 Apr01/04 Apr01/04 Apr01/04 Apr01/04 Apr01/04 Apr01/04 Jan01/06 Apr01/04 Jan01/04 Apr01/04 Jul01/05 Jul01/06 Jul01/06 Jul01/06 Apr01/04 Apr01/04 Jan01/05 Jan01/06 Jan01/06 Jan01/06 Jul01/04 Apr01/04 Jan01/06 Jan01/06 Jan01/06 Jul01/04 Jul01/04
05-50-00 05-50-00 05-50-00
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05-51-00 05-51-00 05-51-00 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11
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1 2 3 601 602 603 604 605 606 607 608 609
R R R R R R R R
Jan01/07 Jan01/07 Apr01/98 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jul01/04 Jan01/07
CH/SE/SU 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11
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610 611 612 613 614 615 616 617 618 619 620 621 622 623 624 625 626 627 628 629 630 631 632 633 634 635 636 637 638 639 640 641 642 643 644 645 646 647 648 649 650 651 652 653 654 655 656 657 658 659 660
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 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-13 05-51-13 05-51-13 05-51-13 05-51-13 05-51-13 05-51-13 05-51-13 05-51-13 05-51-13 05-51-13 05-51-14 05-51-14 05-51-14
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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
Apr01/98 Jul01/05 Jan01/06 Jan01/02 Jan01/02 Jan01/02 Jan01/02 Apr01/98 Apr01/98 Apr01/98 Jan01/02 Jan01/02 Jan01/02 Jan01/06 Jul01/05 Jul01/05 Apr01/98 Apr01/98 Jul01/05 Jan01/02 Jul01/05 Oct01/03 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Oct01/03 Jan01/07 Jan01/07 Jan01/07
05-L.E.P. Page 4 Jan 01/07 SROS
CH/SE/SU 05-51-14 05-51-14 05-51-14 05-51-14 05-51-14 05-51-14 05-51-14 05-51-14 05-51-14 05-51-14 05-51-14 05-51-14 05-51-14 05-51-14 05-51-14 05-51-15 05-51-15 05-51-15 05-51-15 05-51-15 05-51-15 05-51-15 05-51-15 05-51-15 05-51-15 05-51-15 05-51-15 05-51-15 05-51-15 05-51-15 05-51-15 05-51-15 05-51-15 05-51-15 05-51-16 05-51-16 05-51-16 05-51-16 05-51-16 05-51-16 05-51-17 05-51-17 05-51-17 05-51-17 05-51-17 05-51-17 05-51-17 05-51-17 05-51-17 05-51-17 05-51-17
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DATE Jan01/07 Jul01/02 Apr01/02 Jan01/07 Jan01/07 Apr01/02 Jul01/05 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Apr01/98 Apr01/02 Jul01/05 Jul01/05 Apr01/98 Jul01/05 Apr01/02 Jan01/06 Jan01/06 Jan01/06 Jan01/02 Jan01/02 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jan01/02 Jul01/05 Oct01/00 Oct01/00 Jan01/07 Jul01/05 Jul01/05 Jul01/06 Jul01/06 Jul01/05 Jul01/05 Jul01/06 Jul01/06 Jul01/05 Jul01/05 Jul01/06 Jul01/06 Jul01/05 Jul01/05 Jul01/05 Jul01/05
CH/SE/SU 05-51-17 05-51-17 05-51-17 05-51-17 05-51-17 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-19 05-51-19 05-51-21 05-51-21 05-51-21 05-51-21
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DATE Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Apr01/99 Jul01/05 Jul01/05 Jan01/06 Apr01/98 Apr01/98 Apr01/98 Apr01/98 Apr01/98 Apr01/02 Apr01/02 Jan01/00 Jan01/00 Apr01/02 Apr01/02 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jan01/07 Apr01/02 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Apr01/02 Jul01/05 Jul01/05 Apr01/02 Apr01/02 Jan01/06 Jan01/06 Jul01/05 Apr01/02 Jul01/05 Jul01/05 Jul01/02 Jan01/07 Jan01/07 Jan01/07 Oct01/04 Apr01/98 Jan01/07
CH/SE/SU 05-51-22 05-51-22 05-51-22 05-51-22 05-51-22 05-51-22 05-51-22 05-51-23 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25
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DATE Apr01/98 Jan01/07 Jan01/02 Apr01/98 Jan01/07 Jan01/02 Oct01/00 Jan01/07 Jul01/05 Jul01/05 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jul01/04 Jan01/06 Jan01/06 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jan01/07 Jul01/05 Jul01/04 Jul01/04 Jul01/05 Jul01/04 Oct01/00 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/03 Jan01/03 Jan01/03 Jan01/03 Jan01/07 Jan01/03 Jan01/03 Jul01/05 Jul01/05 Jul01/06 Jul01/06 Jan01/03 Jan01/06 Jan01/06 Jan01/07
05-L.E.P. Page 5 Jan 01/07 SROS
CH/SE/SU 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-26 05-51-26 05-51-26 05-51-26 05-51-26 05-51-26 05-51-26 05-51-26 05-51-26 05-51-26 05-51-26 05-51-27 05-51-27 05-51-27 05-51-27 05-51-27 05-51-27 05-51-27 05-51-27 05-51-28 05-51-28 05-51-29 05-51-29 05-51-29 05-51-29 05-51-29 05-51-29 05-51-29
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DATE Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/03 Jan01/03 Jan01/03 Jan01/03 Jan01/03 Jan01/07 Jan01/03 Jul01/05 Jul01/05 Jul01/06 Jul01/06 Jan01/06 Jul01/03 Jan01/03 Jan01/03 Jan01/03 Jan01/03 Jul01/02 Jan01/07 Jul01/05 Jan01/07 Jul01/05 Jan01/07 Jan01/07 Jul01/05 Jan01/07 Apr01/02 Jul01/05 Oct01/00 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Oct01/03 Oct01/03 Oct01/03 Oct01/03 Oct01/03 Apr01/98 Apr01/98
CH/SE/SU 05-51-29 05-51-29 05-51-29 05-51-29 05-51-29 05-51-34 05-51-42 05-51-42 05-51-42 05-51-42 05-51-42 05-51-42 05-51-42 05-51-43 05-51-43 05-51-43 05-51-43 05-51-43 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44
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608 609 610 611 612 601 601 602 603 604 605 606 607 501 502 503 504 505 601 602 603 604 605 606 607 608 609 610 611 612 613 614 615 616 617 618 619 620 621 622 623 624 625 626 627 628 629 630 631 632 633
DATE Apr01/98 Oct01/03 Oct01/03 Oct01/03 Oct01/03 Jul01/05 Apr01/01 Jan01/07 Jan01/07 Jan01/07 Jul01/06 Apr01/01 Apr01/01 Jan01/06 Oct01/04 Oct01/04 Jul01/05 Oct01/04 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 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
CH/SE/SU
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05-51-44 05-51-44 05-51-44 05-51-44 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00
R R R R R R R R R R
05-54-00 05-54-00 05-54-00
R
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05-56-00 05-56-00 05-56-00 05-56-00 05-56-00 05-56-00 05-56-00 05-56-00 05-56-00 05-56-00 05-56-00 05-56-00 05-56-00 05-57-00 05-57-00 05-57-00 05-57-00 05-57-00 05-57-00 05-57-00
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634 635 636 637
Jul01/06 Jul01/06 Jul01/06 Jul01/06
501 502 503 504 505 506 507 508 509 510 511 512 513 514 515 516 517 518 519 520
Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jan01/07 Jan01/07 Jul01/05 Jul01/05 Jul01/05 Jul01/05
201 Jan01/07 202 Jul01/02 203 Apr01/98 601 602 603 604 605 606 607 608 609 610 611 612 613
Jul01/03 Apr01/98 Jul01/03 Apr01/98 Apr01/98 Apr01/98 Apr01/98 Apr01/98 Apr01/98 Apr01/98 Apr01/98 Apr01/98 Apr01/98
201 202 203 204 205 206 207
Jan01/07 Apr01/98 Apr01/98 Apr01/98 Apr01/98 Apr01/98 Apr01/98
05-L.E.P. Page 6 Jan 01/07 SROS
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05-57-00 05-57-00 05-57-00
208 Apr01/98 209 Apr01/98 210 Apr01/98
05-59-00 05-59-32 05-59-32 05-59-32 05-59-32
1 201 202 203 204
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Jul01/06 Jul01/06 Jul01/06 Jan01/05 Jan01/05
05-L.E.P. Page 7 Jan 01/07 SROS
CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS TABLE OF CONTENTS _________________ _______ SUBJECT TIME LIMITS - MAINTENANCE CHECKS __________________________________ _______ GENERAL DESCRIPTION AND OPERATION General Scheduled Maintenance Checks (05-20-00) Unscheduled Maintenance Checks (05-50-00) Time Limits And Maintenance Checks
________ CH/SE/SU 05-00-00
______________________________ SCHEDULED MAINTENANCE CHECKS MAINTENANCE MANUAL PROCEDURE ____________________________ DESCRIPTION AND OPERATION General Task Numbering Procedure Content
05-20-00
ZONAL INSPECTION : LOWER HALF OF FUSELAGE INSPECTION/CHECK General Visual Inspection as far as Visible from Ground of the Lower Half of the Fuselage Zonal Inspection of Lower Half of Fuselage General Visual Inspection of the Lower Half of the Fuselage ZONAL INSPECTION : RADOME INSPECTION/CHECK Zonal Inspection of Radome ZONAL INSPECTION : AVIONICS COMPARTMENT AND NOSE GEAR WELL INSPECTION/CHECK Zonal Inspection of Avionics Compartment Zonal Inspection of Avionics Compartment Zonal inspection of Nose Gear Well Zonal Inspection of the Nose Gear Well (zones 123 and 124). ZONAL INSPECTION : LOWER DECK FORWARD CARGO COMPARTMENT INSPECTION/CHECK Zonal Inspection of Forward Cargo Compartment Zonal Inspection of Forward Cargo
05-21-00
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PAGE ___________ ____ EFFECTIVITY 1 1 1
ALL ALL ALL
1
ALL
1
ALL
1 1 1 1
ALL ALL ALL ALL
601 601
ALL ALL
602
ALL
604
ALL
601 601
ALL ALL
601 601
ALL ALL
604
ALL
608 610
ALL ALL
601 601
ALL ALL
603
ALL
05-21-10 05-21-20
05-21-30
05-CONTENTS R SROS
Page 1 Jan 01/07
CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS TABLE OF CONTENTS _________________ _______ SUBJECT Compartment Zonal Inspection of the Forward Cargo Compartment Zonal Inspection of Bay Under FWD Cargo Compartment Zonal Inspection of Bay behind FWD Cargo Compartment ZONAL INSPECTION : WING CENTER BOX, AIR CONDITIONING AND HYDRAULICS COMPARTMENTS INSPECTION/CHECK Zonal Inspection of Wing Center Box Zonal Inspection of Area Between Keel Beams Zonal Inspection of Zone Under Cabin Floor Zonal Inspection of MLG Well and Hydraulic Compartment General Visual Inspection of Centerline Gear Well ZONAL INSPECTION : LOWER DECK AFT CARGO COMPARTMENT INSPECTION/CHECK Zonal Inspection of Aft Cargo Compartment (if LD-MCR or LDF and/or DCR and/or ACT(s) installed, as far as visible) Zonal Inspection of Aft Cargo Compartment Zonal Inspection of Aft Cargo Compartment Zonal Inspection of Bay Under Aft Cargo Compartment ZONAL INSPECTION : LOWER DECK BULK CARGO COMPARTMENT INSPECTION/CHECK Zonal Inspection of Bulk Cargo Compartment Zonal Inspection of Bulk Cargo Compartment Zonal Inspection of Bulk Cargo Compartment Zonal Inspection of Bay Under Bulk Cargo Compartment ZONAL INSPECTION : AFT CABIN UNDERFLOOR COMPARTMENT
CH/SE/SU ________
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PAGE ___________ ____ EFFECTIVITY 605
ALL
607
ALL
610
ALL
601 601
ALL ALL
603
ALL
605
ALL
607
ALL
609
ALL
601 601
ALL ALL
603
ALL
606
ALL
609
ALL
601 601
ALL ALL
603
ALL
605
ALL
607
ALL
05-21-40
05-21-50
05-21-60
05-21-70 05-CONTENTS
R SROS
Page 2 Oct 01/04
CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS TABLE OF CONTENTS _________________ _______ SUBJECT INSPECTION/CHECK Zonal Inspection of Aft Cabin Underfloor Compartment Zonal Inspection of Aft Cabin Underfloor Compartment ZONAL INSPECTION: AIR CONDITIONING, HYDRAULICS COMPARTMENTS AND FAIRINGS INSPECTION/CHECK Zonal Inspection of Air Conditioning Compt and Fairing Zonal Inspection of Air Conditioning Compt and Fairing Zonal Inspection of Hydraulic Compartment and Fairings Zonal Inspection of Hydraulics Compartment and Fairings Zonal Inspection of Rear Fairings Zonal Inspection of Rear Fairings Zonal Inspection of Air Conditioning Compartment and Fairing Zonal Inspection of Air Conditioning Compartment and Fairing
CH/SE/SU ________
ZONAL INSPECTION : UPPER HALF OF FUSELAGE INSPECTION/CHECK Zonal Inspection of the Upper Half of the fuselage (Zone 200). Zonal Inspection of Upper Half of Fuselage ZONAL INSPECTION : COCKPIT INSPECTION/CHECK Zonal Inspection of Cockpit Zonal Inspection of Cockpit ZONAL INSPECTION : FORWARD CABIN UTILITY AREAS INSPECTION/CHECK Zonal Inspection of FWD Cabin Utility Area Zonal Inspection of FWD Cabin Utility-Area Overhead-Compartment ZONAL INSPECTION: FORWARD CABIN AFT INSPECTION/CHECK Zonal Inspection of FWD Cabin
05-22-00
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____ ___________ PAGE EFFECTIVITY 601 ALL 601 ALL 604
ALL
601 601
ALL ALL
603
ALL
606
ALL
608
ALL
610 612 614
ALL ALL ALL
616
ALL
601 601
ALL ALL
602
ALL
601 601 604
ALL ALL ALL
601 601
ALL ALL
605
ALL
601 601
ALL ALL
05-21-90
05-22-10
05-22-20
05-22-30
05-CONTENTS R SROS
Page 3 Jan 01/06
CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS TABLE OF CONTENTS _________________ _______ SUBJECT Zonal Inspection of FWD Cabin Overhead Compartment ZONAL INSPECTION : MID CABIN UTILITY AREA AFT INSPECTION/CHECK Zonal Inspection of Mid Cabin Utility Area Zonal Inspection of Mid Cabin Utility Area Overhead Compt ZONAL INSPECTION : MID CABIN AFT OF MID CABIN UTILITY AREA TO FRONT OF AFT CABIN INSPECTION/CHECK Zonal Inspection of MID Cabin Zonal Inspection of MID Cabin Overhead Compartment ZONAL INSPECTION : AFT CABIN AFT OF MID CABIN TO FRONT OF AFT CABIN UTILITY AREA INSPECTION/CHECK Zonal Inspection of Aft Cabin Zonal Inspection of Aft Cabin Overhead Compartment ZONAL INSPECTION : AFT CABIN UTILITY AREA INSPECTION/CHECK Zonal Inspection of Aft Cabin Utility Area Zonal Inspection of Aft Cabin Utility Area Overhead Compt
CH/SE/SU ________
ZONAL INSPECTION : STABILIZERS AND FUSELAGE REAR SECTION INSPECTION/CHECK Zonal Inspection of the Stabilizers and the Fuselage Tail (zone 300). Zonal Inspection of Empennage and Rear Fuselage ZONAL INSPECTION : FUSELAGE REAR SECTION AFT OF AFT PRESSURE BULKHEAD INSPECTION/CHECK Zonal Inspection of Rear Fuselage Section Zonal Inspection of Tail Cone APU Air Intake Area Zonal Inspection of Tail Cone APU and Accessory Compt
05-23-00
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____ ___________ PAGE EFFECTIVITY 605 ALL
05-22-40 601 601
ALL ALL
604
ALL
601 601 604
ALL ALL ALL
601 601 604
ALL ALL ALL
601 601
ALL ALL
605
ALL
601 601
ALL ALL
602
ALL
601 601
ALL ALL
605
ALL
607
ALL
05-22-50
05-22-60
05-22-70
05-23-10
05-CONTENTS R SROS
Page 4 Oct 01/04
CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS TABLE OF CONTENTS _________________ _______ SUBJECT Zonal Inspection of Tail Cone APU Exhaust Area Zonal Inspection of Horizontal Stabilizer Center Box (Internal) ZONAL INSPECTION : VERTICAL STABILIZER AND RUDDER INSPECTION/CHECK Zonal Inspection of Dorsal Fin Zonal Inspection of Vertical Stabilizer Leading Edge Zonal Inspection of Vertical Stabilizer Spar Box Zonal Inspection of Vertical Stabilizer Spar Box Zonal Inspection of Vertical Stabilizer Tip Zonal Inspection of Vertical Stabilizer Trailing Edge Zonal Inspection of Vertical Stabilizer Trailing Edge Zonal Inspection of Rudder Zonal Inspection of Rudder Zonal Inspection of Rudder (Front Spar FWD Face and Internal Structure as far as visible) ZONAL INSPECTION : TRIMMABLE HORIZONTAL STABILIZER LEFT SIDE AND LEFT ELEVATOR INSPECTION/CHECK Zonal Inspection of Horizontal Stabilizer Leading Edge Zonal Inspection of Horizontal Stabilizer Tip Zonal Inspection of Horizontal Stabilizer Lateral Box Zonal Inspection of Horizontal Stabilizer Trailing Edge (From Fuselage Fairing to Rib 10) Zonal Inspection of Horizontal Stabilizer Trailing Edge (From Fuselage Fairing to Rib 21) Zonal Inspection of Elevator (Area between Ribs 8 and 9) Zonal Inspection of Elevator (Leading Edge as far as Visible)
CH/SE/SU ________
ZONAL INSPECTION : POWER PLANT, NACELLES
05-24-00
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____ ___________ PAGE EFFECTIVITY 609 ALL 611
ALL
601 601 604
ALL ALL ALL
606
ALL
609
ALL
612
ALL
615
ALL
617
ALL
619 622 624
ALL ALL ALL
601 601
ALL ALL
604
ALL
607
ALL
610
ALL
613
ALL
616
ALL
619
ALL
05-23-20
05-23-30
05-CONTENTS R SROS
Page 5 Jul 01/06
CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS TABLE OF CONTENTS _________________ _______ SUBJECT AND PYLONS INSPECTION/CHECK Zonal Inspection as far as visible from the ground of the Power Plant, the Nacelles and the Pylons (zone 400). Zonal Inspection of Power Plants, Nacelles and Pylons. ZONAL INSPECTION : ENGINE INSPECTION/CHECK
CH/SE/SU ________
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ALL ALL
602
ALL
601
601 601
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, 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,
609
701-749,
05-24-10 2
General Visual Inspection of the Engine Air Intake and Intake Lip
601
General Visual Inspection of the Engine Air Intake and Intake Lip
609
General Visual Inspection of the Fan Frame and Accessory Gear Box
614
General Visual Inspection of the Hot Section
618
General Visual Inspection of the Exhaust Nozzle
623
General Visual Inspection of the Fan Cowl
627
General Visual Inspection of the Thrust Reverser
632
INSPECTION/CHECK General Visual Inspection of Engine Air Intake and Intake General Visual Inspection of Engine Air Intake and Intake
3 the Lip the Lip
05-CONTENTS R SROS
201-249 255-299 401-449 201-249 255-299 401-449 201-249 255-299 401-449 201-249 255-299 401-449 201-249 255-299 401-449 201-249 255-299 401-449 201-249 255-299 401-449 201-249 255-299 401-449
Page 6 Jul 01/05
CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS TABLE OF CONTENTS _________________ _______ SUBJECT General Visual Inspection of Fan Frame and Accessory Gear General Visual Inspection of Hot Section General Visual Inspection of Exhaust Nozzle General Visual Inspection of Fan Cowl General Visual Inspection of Thrust Reverser ZONAL INSPECTION : ENGINE PYLON INSPECTION/CHECK
CH/SE/SU ________
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the Box the
____ ___________ PAGE EFFECTIVITY 614 701-749, 618
701-749,
the
623
701-749,
the
627
701-749,
the
632
701-749,
601
05-24-50 2
Pylon
601 601
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, 001-049, 251-252, 301-399, 451-499, 701-749, 701-749,
Upper
608
701-749,
Lower of
612
701-749,
Lower and
616
701-749,
Lower and
620
701-749,
Zonal Inspection of the Pylon Leading Edge
601
Zonal Inspection of the Upper Forward of the Pylon
607
Zonal Inspection of the Lower of the Pylon
611
Zonal Inspection of the Lower and Rear Pylon Fairings
615
Zonal Inspection of the Lower and Rear Pylon Fairings
619
INSPECTION/CHECK Zonal Inspection of the Leading Edge Zonal Inspection of the Forward of the Pylon Zonal Inspection of the the Pylon Zonal Inspection of the Rear Pylon Fairings Zonal Inspection of the Rear Pylon Fairings
3
05-CONTENTS R SROS
201-249 255-299 401-449 201-249 255-299 401-449 201-249 255-299 401-449 201-249 255-299 401-449 201-249 255-299 401-449 201-249 255-299 401-449
Page 7 Jul 01/05
CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS TABLE OF CONTENTS _________________ SUBJECT _______
CH/SE/SU ________
ZONAL INSPECTION : WING INSPECTION/CHECK Zonal Inspection as far as visible from the Ground of the Left and Right Wings (zone 500 and 600). Zonal Inspection of Wing Lower Surface Including Slats and Flaps Zonal Inspection of Wing Upper Surface (Including Slats, Flaps and Spoilers) ZONAL INSPECTION : WING FIXED LEADING EDGE INSPECTION/CHECK Zonal Inspection of Inboard Fixed Leading Edge Structure Zonal Inspection of Center Fixed Leading Edge Structure Zonal Inspection of Outer Fixed Leading Edge Structure ZONAL INSPECTION : WING FLAP TRACK FAIRINGS AND WING TIP INSPECTION/CHECK Zonal Inspection of Flap Tracks and Flap Track Fairings (Including RAT Attachment Points, as far as visible) Zonal inspection of Flap Tracks and Flap Track Fairings Zonal Inspection of Wing Tip. ZONAL INSPECTION : WING FUEL TANK INSPECTION/CHECK Zonal Inspection of Inner Fuel Tank. Zonal Inspection of Inner Fuel Tank (Rib 1 to Rib 23). Zonal Inspection of Outer Fuel Tank (Rib 23 to Rib 33). ZONAL INSPECTION : WING VENT SURGE TANK INSPECTION/CHECK Zonal Inspection of Vent Surge Tank ZONAL INSPECTION : AFT SECTION OF WING AND TRAILING EDGE FIXED STRUCTURE INSPECTION/CHECK Zonal Inspection of Main Landing
05-25-00
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ALL ALL
602
ALL
605
ALL
601 601
ALL ALL
603
ALL
606
ALL
601 601
ALL ALL
604
ALL
607
ALL
601 601
ALL ALL
605
ALL
609
ALL
601 601
ALL ALL
601 601
ALL ALL
05-25-20
05-25-30
05-25-40
05-25-50
05-25-70
05-CONTENTS R SROS
Page 8 Jul 01/05
CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS TABLE OF CONTENTS _________________ _______ SUBJECT Gear Well. Zonal Inspection of Shroud Box. Zonal Inspection of Inner Trailing Edge Fixed Structure (RIB 6 to RIB 12) Zonal Inspection of Center Trailing Edge Fixed Structure (RIB 12 to RIB 27) Zonal Inspection of Outer Trailing Edge Fixed Structure (RIB 27 to RIB 39) ZONAL INSPECTION : WING AILERON INSPECTION/CHECK Zonal Inspection of Inboard Aileron. Zonal Inspection of Outboard Aileron.
CH/SE/SU ________
ZONAL INSPECTION : LANDING GEAR AND LANDING GEAR DOORS INSPECTION/CHECK Zonal inspection of Landing Gear and Landing Gear Doors. ZONAL INSPECTION : NOSE GEAR AND DOORS INSPECTION/CHECK Zonal Inspection of Nose Landing Gear. Zonal Inspection of the Nose Landing Gear (Zones 710) Zonal Inspection of Nose Landing Gear Main Doors. Zonal Inspection of Nose Landing Gear Aft Doors. ZONAL INSPECTION : MAIN LANDING GEAR AND DOORS INSPECTION/CHECK Zonal Inspection of LH and RH Main Landing Gear. Zonal Inspection of the Main Landing Gear (Zones 730 and 740). Zonal Inspection of Main Landing Gear Leg Doors. Zonal Inspection of Main Landing Gear Hinge Door. Zonal Inspection of Main Landing Gear Main Doors.
05-27-00
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05-CONTENTS R SROS
Page 9 Jul 01/06
CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS TABLE OF CONTENTS _________________ SUBJECT _______
CH/SE/SU ________
ZONAL INSPECTION : PASSENGER/CREW DOORS, CARGO COMPARTMENT DOORS AND EMERGENCY EXITS INSPECTION/CHECK Zonal Inspection as far as visible from the ground of the Doors (zone 800) Zonal Inspection of Doors ZONAL INSPECTION : FORWARD AVIONICS COMPARTMENT INSPECTION/CHECK Zonal Inspection of Forward Avionics Compartment Door ZONAL INSPECTION : LOWER DECK FORWARD AFT AND BULK CARGO COMPARTMENT DOORS INSPECTION/CHECK Zonal Inspection of Forward Cargo Compartment Door Zonal Inspection of Forward Cargo Compartment Door (Including Door Hinge Arms Attachment Area) Zonal Inspection of Aft Cargo Compartment Door Zonal Inspection of Aft Cargo Compartment Door (Including Door Hinge Arms Attachment Area) Zonal Inspection of Bulk Cargo Compartment Door (Including Fuselage Frames, Stop Fittings at Fuselage Frames, Door Seals, and Visible Part of Door Sill). Zonal Inspection of Bulk Cargo Compartment Door. Zonal Inspection of Forward Cargo Compartment Door Zonal Inspection of AFT Cargo Compartment Door. ZONAL INSPECTION : LEFT PASSENGER/ CREW DOORS AND EMERGENCY EXITS INSPECTION/CHECK Zonal Inspection of FWD Passenger/Crew Door (Including Door Stops on Fuselage Side, Door Seals and Scuff Plates) Zonal Inspection of FWD
05-28-00
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05-CONTENTS R SROS
Page 10 Jul 01/05
CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS TABLE OF CONTENTS _________________ _______ SUBJECT Passenger/Crew Door Zonal Inspection of Emergency Exit (Including Door Stops on Fuselage Side, Door Seals and Scuff Plates) Zonal Inspection of Emergency Exit Zonal Inspection of Emergency Exit (Doors 3) Zonal Inspection of MID Passenger/Crew Doors Zonal Inspection of MID Passenger/Crew Door Zonal Inspection of AFT Passenger/Crew Doors Zonal Inspection of AFT Passenger/Crew Door
CH/SE/SU ________
______________________________ UNSCHEDULED MAINTENANCE CHECKS DESCRIPTION AND OPERATION General
05-50-00
_______________________________ UNSCHEDULED MAINTENANCE CHECKS MAINTENANCE PRACTICES Leaks - Permitted Values INSPECTIONS DESCRIPTION AND OPERATION General Inspection Coverage Inspection Sequence Inspection Presentation INSPECTION AFTER HARD/OVERWEIGHT LANDING INSPECTION/CHECK Inspection after Hard/Overweight Landing INSPECTION AFTER LANDING GEAR DOWN LIMITING SPEED EXCEEDED INSPECTION/CHECK Inspection After Landing Gear Extension at More than the Gear Down Limiting Speed. INSPECTION AFTER FLAP/SLAT LIMITING SPEED EXCEEDED INSPECTION/CHECK Inspection after Flap/Slat
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05-50-00
05-51-00
05-51-11
05-51-12
05-51-13
05-CONTENTS R SROS
Page 11 Jul 01/05
CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS TABLE OF CONTENTS _________________ _______ SUBJECT Extension at more than the Flap/Slat Limiting Speed INSPECTION OF AIRFRAME AFTER BIRD OR HAIL STRIKE INSPECTION/CHECK Inspection of the Aircraft after a Bird or a Hail Strike INSPECTION AFTER A TIRE BURST OR TREAD THROW OR WHEEL FAILURE INSPECTION/CHECK Inspection of the Aircraft after a Tire Burst or Tread Throw or Wheel Failure INSPECTION AFTER BRAKE EMERGENCY APPLICATION OR OVERHEAT INSPECTION/CHECK Inspection After Brake Overheat INSPECTION AFTER FLIGHT IN EXCESSIVE TURBULENCE OR IN EXCESS OF VMO INSPECTION/CHECK Inspection after Flight in Excessive Turbulence or in Excess of VMO/MMO INSPECTION AFTER LIGHTNING STRIKE INSPECTION/CHECK Inspection after Lightning Strike INSPECTION AFTER ENGINE BIRD STRIKE OR SLUSH INGESTION INSPECTION/CHECK Inspection after Engine Bird Strike or Slush Ingestion INSPECTION AFTER TAIL RUNWAY IMPACT INSPECTION/CHECK Inspection after a Tail Runway Impact INSPECTION AFTER NLG TOWING OVERLOAD OR OVERRUN INSPECTION/CHECK Inspection after NLG Towing Overload or Overrun INSPECTION AFTER NLG STEERING ANGLE EXCEEDED INSPECTION/CHECK Inspection of the Nose Landing Gear after a NLG Steering Angle of more than 95⁰
CH/SE/SU ________
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05-51-15
05-51-16
05-51-17
05-51-18 05-51-19
05-51-21
05-51-22
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05-CONTENTS R SROS
Page 12 Jul 01/05
CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS TABLE OF CONTENTS _________________ _______ SUBJECT INSPECTION AFTER LEAVING RUNWAY OR TAXIWAY INSPECTION/CHECK Inspection after Leaving a Runway or a Taxiway INSPECTION AFTER FLIGHT THROUGH DUST STORM/VOLCANIC ASH OR SEVERE CONDITION ON GROUND INSPECTION/CHECK Inspection after Flight through Dust Storm or Dust contamination on Ground Inspection after Flight through Volcanic Ash or Volcanic Ash contamination on Ground INSPECTION AFTER ENGINE FAILURE INSPECTION/CHECK Inspection of the Aircraft after Engine Failure INSPECTION AFTER IMPACT ON ENGINE COWLS INSPECTION/CHECK Inspection after Impact on Engine Cowls INSPECTION AFTER SPILLAGE INSPECTION/CHECK Inspection after Spillage INSPECTION AFTER ABNORMAL PAX/CREW DOOR MOVEMENT INSPECTION/CHECK Inspection after Abnormal Pax/Crew Door Movement. INSPECTION AFTER ENGINE WINDMILLING (AFTER ENGINE IN-FLIGHT SHUT-DOWN) INSPECTION/CHECK Inspection after Engine Windmilling (after Engine In-Flight Shut-Down) INSPECTION AFTER VERY HIGH WINDS ON GROUND INSPECTION/CHECK Inspection after Very High Winds on Ground INSPECTIONS AFTER WORK ON SYSTEM ELECTRICAL INSTALLATION ADJUSTMENT/TEST
________ CH/SE/SU 05-51-24
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05-51-28 05-51-29
05-51-34
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05-CONTENTS R SROS
Page 13 Jul 01/05
CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS TABLE OF CONTENTS _________________ _______ SUBJECT Inspection after Work on System Electrical Installation INSPECTION AFTER FLIGHT WITH HIGH LATERAL LOADS INSPECTION/CHECK INSPECTION AFTER FLIGHT WITH HIGH LATERAL LOADS
CH/SE/SU ________
PRESSURIZATION TEST OF FUSELAGE (LEAKAGE CHECKS) AFTER A/C ABNORMAL OPERATION OR REPAIR ADJUSTMENT/TEST Pressurization Retest and Leakage Rate Measurement Pressurization Retest and Leakage Rate Measurement (with ACMS)
05-53-00
DEMAGNETIZATION MAINTENANCE PRACTICES Demagnetization of the External Parts of the Frames of the Windshield and Sliding Windows
05-54-00
MEASUREMENT AFTER ABNORMAL OPERATION OF THE AIRCRAFT INSPECTION/CHECK Measurement of the Aircraft by Photogrammetry after Abnormal Operation of the Aircraft
05-56-00
AIRCRAFT STABILITY MAINTENANCE PRACTICES Aircraft Stability
05-57-00
NON-REVENUE FLIGHT - REQUIREMENTS FOLLOWING MAINTENANCE ACTIONS DESCRIPTION AND OPERATION General Engine Replacement Replacement or reinstallation of both engines does not require a non-revenue flight providing the engines have been successfully FERRY FLIGHT WITH GEAR DOWN MAINTENANCE PRACTICES Preparation For Ferry Flight with
05-59-00
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05-CONTENTS R SROS
Page 14 Jul 01/06
CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS TABLE OF CONTENTS _________________ _______ SUBJECT Gear Down Return in Normal Operation after a Ferry flight with Gear Down
CH/SE/SU ________
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05-CONTENTS SROS
Page 15 Jul 01/06
TIME LIMITS - MAINTENANCE CHECKS - GENERAL - DESCRIPTION AND OPERATION ______________________________________________________________________ R R R
1. _______ General This chapter includes the following sections: 05-20-00: SCHEDULED MAINTENANCE CHECKS 05-50-00: UNSCHEDULED MAINTENANCE CHECKS
R R R
A. Scheduled Maintenance Checks (05-20-00) This section includes all the zonal inspections that you must do on the aircraft.
R R R R R R
B. Unscheduled Maintenance Checks (05-50-00) This section includes the maintenance checks that you must do when a flight crew report shows abnormal flight conditions. This section is divided into two categories of information: - inspections - checks.
R R R R R R R R R R R
2. Time __________________________________ Limits And Maintenance Checks The part of the Aircraft Maintenance Manual (AMM) was previously issued in a separate Manual to this AMM with the title: ------------------------------------------------------------------------------Aircraft Maintenance Manual CHAPTER 05 Time Limits and Maintenance Checks ------------------------------------------------------------------------------The content of this manual, since revision 09 approved on NOV 13, 2001, is into the Maintenance Planning Document(MPD) - Section 9.1 : Life Limits/Monitored Parts.
EFF : ALL 05-00-00 SROS
Page 1 Jan 01/07
___________________________________________________________ SCHEDULED MAINTENANCE CHECKS - MAINTENANCE MANUAL PROCEDURE DESCRIPTION AND OPERATION _________________________ 1. General _______ A. Task Numbering This section gives the accomplishment instructions for zonal inspection tasks; - related to the requirements of the Maintenance Planning Document (MPD), a specific AMTOSS zonal task number which combines the ATA 05-20 and the concerned A/C zone is used as follows: Task Numbering System for Zonal Inspection Tasks. ATA Reference Number II TASK No. 0 5 - 2 2 - 6 0 - 2 0 0 - 0 0 1 I__I I I________I I_____I I_____I 1 2 3 4 5 1 : ATA 2 : Relates to ATA section 20 scheduled maintenance checks 3 : Zone 4 : Function code, e.g. 200 : INSPECTION CHECK 5 : Unique identification of discrete tasks B. Procedure Content (1) It is thought that people who do the zonal tasks have an adequate knowledge of the aircraft construction and systems installations; thus a list of all the items contained in the zones to be inspected is not given. (2) If you find damage, corrosion, leaks, it is recommended to refer to the related structure/system inspection ATA-chapter for detailed inspection and corrective action (3) During the zonal inspection, you must also examine any fairing, access panel, access door, etc. which you remove or open to gain access to zones. This requirement is not given in each individual procedure because it is a standard maintenance practice.
EFF : ALL 05-20-00 SROS
Page 1 Apr 01/98
ZONAL INSPECTION : LOWER HALF OF FUSELAGE - INSPECTION/CHECK ____________________________________________________________ TASK 05-21-00-200-801 General Visual Inspection as far as Visible from Ground of the Lower Half of the Fuselage 1. __________________ Reason for the Job R
NOTE : This task can contribute to fuel savings. ____ 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------53-35-00-200-801
Inspection of the Wing-to-Fuselage Fairings and Belly Fairing Access Panels for Missing Fasteners
3. __________ Job Set-up Subtask 05-21-00-869-050 A. Not applicable. 4. Procedure _________ Subtask 05-21-00-210-050 A. Inspection. (1) Do a general visual inspection of the lower half of the fuselage from the ground during the aircraft walkaround. (2) Inspect the belly fairing access panels and the wing-to-fuselage fairings for missing fasteners (Ref. TASK 53-35-00-200-801).
EFF : ALL 05-21-00 SROS
Page 601 Jan 01/07
TASK 05-21-00-200-802 Zonal Inspection of Lower Half of Fuselage 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-100-01 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
1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------53-35-00-200-801
Inspection of the Wing-to-Fuselage Fairings and Belly Fairing Access Panels for Missing Fasteners
3. __________ Job Set-up Subtask 05-21-00-010-050 A. Get Access R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at zone 100.
EFF : ALL 05-21-00 SROS
Page 602 Jan 01/07
4. Procedure _________ Subtask 05-21-00-210-051 A. Inspection R R
(1) Do a general visual inspection of the bottom half of the fuselage at zone 100 (below cabin floor). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see.
R R
(2) Inspect the belly-fairing access panels and the wing-to-fuselage fairings for missing fasteners (Ref. TASK 53-35-00-200-801).
R
5. Close-up ________
R
Subtask 05-21-00-860-051
R
A. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-00 SROS
Page 603 Jan 01/04
TASK 05-21-00-200-803 General Visual Inspection of the Lower Half of the Fuselage 1. __________________ Reason for the Job R R
Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
access platform 2.5 m (8 ft. 2 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------53-35-00-200-801
Inspection of the Wing-to-Fuselage Fairings and Belly Fairing Access Panels for Missing Fasteners
3. __________ Job Set-up Subtask 05-21-00-010-051 A. Get Access (1) Put an access platform in position in the lower half of the fuselage. 4. Procedure _________ Subtask 05-21-00-210-052 A. Inspection of the Lower Half of the Fuselage (1) Do a general visual inspection of the lower half of the fuselage zone 100 (below cabin floor). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see.
EFF : ALL 05-21-00 SROS
Page 604 Jan 01/06
R R
(2) Inspect the belly fairing access panels and the wing-to-fuselage fairings for missing fasteners (Ref. TASK 53-35-00-200-801). 5. Close-up ________ Subtask 05-21-00-410-051 A. Close Access (1) Remove the access platform(s).
EFF : ALL 05-21-00 SROS
Page 605 Oct 01/02
ZONAL INSPECTION : RADOME - INSPECTION/CHECK ____________________________________________ TASK 05-21-10-200-801 R
Zonal Inspection of Radome 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-110-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 4M (13 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R
53-15-11-010-801 53-15-11-410-801
Opening of the Radome Closing of the Radome
3. __________ Job Set-up Subtask 05-21-10-010-050 A. Get Access R R
(1) Put an ACCESS PLATFORM 4M (13 FT) in position at zone 110.
R
(2) Open the radome 110AL (Ref. TASK 53-15-11-010-801).
EFF : ALL 05-21-10 SROS
Page 601 Jan 01/04
4. Procedure _________ Subtask 05-21-10-210-050 A. Do a general visual inspection of the radome. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-21-10-410-050 A. Close Access (1) Close the radome 110AL (Ref. TASK 53-15-11-410-801). R R R
Subtask 05-21-10-860-050 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-10 SROS
Page 602 Jan 01/04
ZONAL INSPECTION : AVIONICS COMPARTMENT AND NOSE GEAR WELL - INSPECTION/CHECK _____________________________________________________________________________ TASK 05-21-20-200-801 R
Zonal Inspection of Avionics Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-121-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------52-30-00-010-801 52-30-00-410-801 R
05-21-20-991-002
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 Fig. 601
3. __________ Job Set-up Subtask 05-21-20-010-050 A. Get Access R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at zone 821. (2) Open the forward cargo-compartment door 821 (Ref. TASK 52-30-00-010801).
R R
(3) Open the access door 132AZ (Ref. Fig. 601/TASK 05-21-20-991-002)
EFF : ALL 05-21-20 SROS
Page 601 Jan 01/04
R R
Forward Cargo-Compartment Partition Panels, FR20 Figure 601/TASK 05-21-20-991-002
EFF : ALL 05-21-20 SROS
Page 602 Jan 01/04
4. Procedure _________ Subtask 05-21-20-210-050 A. Inspection (1) Do a general visual inspection of the forward avionics compartment (zones 121 and 122). (2) Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. (3) Make sure that all the installations (wiring, ducting, piping) are attached correctly. 5. Close-up ________ Subtask 05-21-20-410-050 A. Close Access (1) Close the access door 132AZ. (2) Close the forward cargo-compartment door 821 (Ref. TASK 52-30-00-410801). (3) Remove the access platform(s). R R
Subtask 05-21-20-860-050 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-20 SROS
Page 603 Jan 01/04
TASK 05-21-20-200-802 Zonal Inspection of Avionics Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-121-02 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 ------------------------------------------------------------------------------R R R R R
25-52-00-000-801 25-52-00-400-801 52-30-00-010-801 52-30-00-410-801
R
53-12-13-000-801 53-12-13-400-801 05-21-20-991-001-A
Removal of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the FWD Cargo Compartment Installation of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the FWD Cargo Compartment 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 Removal of the Avionics-Compartment Floor Panels Installation of the Avionics-Compartment Floor Panels Fig. 602
EFF : ALL 05-21-20 SROS
Page 604 Jan 01/07
3. __________ Job Set-up R R R
(Ref. Fig. 602/TASK 05-21-20-991-001-A) Subtask 05-21-20-010-051-A A. Get Access
R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at zone 821.
R R
(2) Open the forward cargo-compartment door 821 (Ref. TASK 52-30-00-010801).
R
(3) Open the access door 132AZ.
R R
(4) Remove the partition panels 131AW, 131BW and 132CW at FR20 (Ref. TASK 25-52-00-000-801).
R R R R
(5) Remove the floor panels: 121AF, 121BF, 121CF, 121DF, 121EF, 121FF, 121GF, 121HF, 121KF, 122CF, 122DF, 122FF, 122GF, 122HF, 122LF, 122KF, 122JF, 122NF and 122PF from the forward cabin utility-area (Ref. TASK 53-12-13-000-801). 4. Procedure _________ Subtask 05-21-20-210-051 A. Inspection (1) Do a general visual inspection of the forward avionics compartment (zones 121 and 122). (2) Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. (3) Make sure that all the installations (wiring, ducting, piping) are attached.
EFF : ALL 05-21-20 SROS
Page 605 Jan 01/07
R R
Floor Panels of the Avionics Compartment Figure 602/TASK 05-21-20-991-001-A
R EFF : ALL 05-21-20 SROS
Page 606 Jan 01/07
5. Close-up ________ R R
Subtask 05-21-20-410-051-A A. Close Access
R R R
(1) Install the floor panels: 121AF, 121BF, 121CF, 121DF, 121EF, 121FF, 121GF, 121HF, 121KF, 122CF, 122DF, 122FF, 122GF, 122HF, 122LF, 122KF, 122JF, 122NF and 122PF (Ref. TASK 53-12-13-400-801).
R R
(2) Install the partition panels 131AW, 131BW and 132CW at FR20 (Ref. TASK 25-52-00-400-801).
R
(3) Close the access door 132AZ.
R R
(4) Close the forward cargo-compartment door 821 (Ref. TASK 52-30-00-410801). Subtask 05-21-20-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-20 SROS
Page 607 Jan 01/07
TASK 05-21-20-200-803 Zonal inspection of Nose Gear Well 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 Refer to the MPD TASK: ZL-123-01 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 ------------------------------------------------------------------------------32-22-00-010-801 32-22-00-410-801
Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-21-20-010-052 A. Get Access (1) Open the nose landing gear doors 713, 714 (Ref. TASK 32-22-00-010801). (2) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at zone 713 (714).
EFF : ALL 05-21-20 R SROS
Page 608 Jan 01/07
4. Procedure _________ Subtask 05-21-20-210-052 A. Inspection (1) Do a general visual inspection of the nose gear well (zone 123). (2) Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. (3) Make sure that all the installations (wiring, ducting, piping) are attached correctly. 5. Close-up ________ Subtask 05-21-20-410-052 A. Close Access (1) Close the nose-landing-gear doors 713, 714 (Ref. TASK 32-22-00-410801). Subtask 05-21-20-860-052 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-20 R SROS
Page 609 Jan 01/07
TASK 05-21-20-200-804 Zonal Inspection of the Nose Gear Well (zones 123 and 124). 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-22-00-010-801 32-22-00-410-801
Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-21-20-010-053 A. Get Access (1) Open the nose landing gear doors 713, 714 (Ref. TASK 32-22-00-010801). 4. Procedure _________ Subtask 05-21-20-210-053 A. Inspection (1) Do a general visual inspection of the nose gear well, from the ground, as far as visible (zones 123 and 124). (2) Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. (3) Make sure that all the installations (wiring, ducting, piping) are attached correctly.
EFF : ALL 05-21-20 R SROS
Page 610 Jan 01/07
5. Close-up ________ Subtask 05-21-20-410-053 A. Close Access (1) Close the nose landing gear doors 713, 714 (Ref. TASK 32-22-00-410801).
EFF : ALL 05-21-20 R SROS
Page 611 Jan 01/07
ZONAL INSPECTION : LOWER DECK FORWARD CARGO COMPARTMENT - INSPECTION/CHECK __________________________________________________________________________ TASK 05-21-30-200-801 R
Zonal Inspection of Forward Cargo Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-131-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------52-30-00-010-801 52-30-00-410-801
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 05-21-30-010-050 A. Get Access R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at zone 821. (2) Open the forward cargo-compartment door 821 (Ref. TASK 52-30-00-010801).
EFF : ALL 05-21-30 SROS
Page 601 Jan 01/04
4. Procedure _________ Subtask 05-21-30-210-050 A. Do a general visual inspection of the forward cargo compartment (zones 131 and 132). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (wiring, ducting, piping) are attached correctly. 5. Close-up ________ Subtask 05-21-30-410-050 A. Close Access (1) Close the forward cargo door 821 (Ref. TASK 52-30-00-410-801). R R R
Subtask 05-21-30-860-050 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-30 SROS
Page 602 Jan 01/04
TASK 05-21-30-200-802 R
Zonal Inspection of Forward Cargo Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-131-02 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 ------------------------------------------------------------------------------25-52-00-000-801 25-52-00-400-801
Removal of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the FWD Cargo Compartment Installation of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the FWD Cargo Compartment 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
52-30-00-010-801 52-30-00-410-801 3. __________ Job Set-up Subtask 05-21-30-010-051-A A. Get Access
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at access door 821. (2) Open the forward cargo-compartment door 821 (Ref. TASK 52-30-00-010801).
EFF : ALL 05-21-30 SROS
Page 603 Jul 01/06
R R
(3) Remove the sidewall panels: 131FX, 131KW, 132UW, 132WW, 132FX (Ref. TASK 25-52-00-000-801).
R
(4) Remove the ceiling panels: 131BC, 131FC, 131XC, 131PC, 131RC, 131TC, 131VC (Ref. TASK 25-52-00-000-801). 4. Procedure _________ Subtask 05-21-30-210-051
R
A. Do a general visual inspection of the forward cargo compartment. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting, piping) are attached correctly. 5. Close-up ________ Subtask 05-21-30-410-051-A A. Close Access
R R
(1) Install the ceiling panels: 131BC, 131FC, 131XC, 131PC, 131RC, 131TC, 131VC (Ref. TASK 25-52-00-400-801).
R R
(2) Install the sidewall panels: 131FX, 131KW, 132UW, 132WW, 132FX (Ref. TASK 25-52-00-400-801). (3) Make sure that the work area is clean and clear of tools and other items. (4) Close the forward cargo-compartment door 821 (Ref. TASK 52-30-00-410801). Subtask 05-21-30-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-21-30 SROS
Page 604 Jul 01/06
TASK 05-21-30-200-803 R
Zonal Inspection of the Forward Cargo Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-131-03 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------25-52-00-000-801 25-52-00-400-801 52-30-00-010-801 52-30-00-410-801
Removal of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the FWD Cargo Compartment Installation of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the FWD Cargo Compartment 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 05-21-30-010-052 A. Get Access R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at access door 821. (2) Open the forward cargo door 821 (Ref. TASK 52-30-00-010-801). (3) Remove the sidewall and ceiling panels from FR20 to FR39.2 (Ref. TASK 25-52-00-000-801).
EFF : ALL 05-21-30 SROS
Page 605 Jan 01/04
4. Procedure _________ Subtask 05-21-30-210-052
R
A. Do a general visual inspection of the forward cargo compartment. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping) are attached correctly. NOTE : Lift the insulation sufficiently to make sure that there is no ____ corrosion or signs of leaks. 5. Close-up ________ Subtask 05-21-30-410-052 A. Close Access
R R
(1) Install the sidewall and ceiling panels from FR20 to FR39.2 (Ref. TASK 25-52-00-400-801).
R
(2) Make sure that the work area is clean and clear of tools and other items.
R R
(3) Close the forward cargo door (Ref. TASK 52-30-00-410-801).
R R
Subtask 05-21-30-860-052 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-30 SROS
Page 606 Jan 01/04
TASK 05-21-30-200-804 R
Zonal Inspection of Bay Under FWD Cargo Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-133-01 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 ------------------------------------------------------------------------------52-30-00-010-801 52-30-00-410-801 53-00-00-000-802 53-00-00-400-802 R
05-21-30-991-007
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 Removal of the Floor Panels in the FWD Cargo-Compartment Installation of the Floor Panels in the FWD Cargo-Compartment Fig. 601
3. __________ Job Set-up Subtask 05-21-30-010-053 A. Get Access R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at access door 821. (2) Open the forward cargo door 821 (Ref. TASK 52-30-00-010-801). (3) Remove the floor panels from FR20 to FR39 (Ref. TASK 53-00-00-000802).
EFF : ALL 05-21-30 SROS
Page 607 Jul 01/04
R
(4) Lift the insulation.
R R
(5) Remove the access panels 133AL, 133BL. (Ref. Fig. 601/TASK 05-21-30-991-007) 4. Procedure _________ Subtask 05-21-30-210-053
R R R
A. Do a general visual inspection of the bay below the forward cargo-compartment floor (Zones 133 and 134).
R
(1) Make sure that: (a) there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. (b) all the installations (wiring, ducting, piping) are attached correctly. 5. Close-up ________ Subtask 05-21-30-410-053 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Put the insulation back in position.
R
(3) Install the access panels 133AL, 133BL.
R
(4) Install the floor panels from FR20 to FR39 (Ref. TASK 53-00-00-400802).
R
(5) Close the forward cargo door 821 (Ref. TASK 52-30-00-410-801). Subtask 05-21-30-860-053 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-21-30 SROS
Page 608 Jul 01/04
R R
Access Panels of the Forward-Fuselage Lower Section Figure 601/TASK 05-21-30-991-007
EFF : ALL 05-21-30 SROS
Page 609 Jul 01/04
TASK 05-21-30-200-806 R
Zonal Inspection of Bay behind FWD Cargo Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-137-01 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 ------------------------------------------------------------------------------25-52-00-000-801 25-52-00-400-801 52-30-00-010-801 52-30-00-410-801 53-00-00-000-802 53-00-00-400-802
Removal of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the FWD Cargo Compartment Installation of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the FWD Cargo Compartment 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 Removal of the Floor Panels in the FWD Cargo-Compartment Installation of the Floor Panels in the FWD Cargo-Compartment
EFF : ALL 05-21-30 SROS
Page 610 Jul 01/04
3. __________ Job Set-up Subtask 05-21-30-010-055 A. Get Access R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at access door 821. (2) Open the forward cargo-compartment door 821 (Ref. TASK 52-30-00-010801).
R R
(3) Remove the partition panels: 132DX, 132CX, 131BX, 131CX, 131DX (Ref. TASK 25-52-00-000-801).
R
(4) Remove the floor panels: 131DG, 132CG, 132DG, 131CG (Ref. TASK 53-0000-000-802). 4. Procedure _________ Subtask 05-21-30-210-055 A. Do a general visual inspection of the bay behind the forward cargo compartment (zones 137 and 138). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping) are attached correctly. 5. Close-up ________ Subtask 05-21-30-410-055 A. Close Access
R
(1) Install the floor panels: 131DG, 131CG, 132DG, 132CG (Ref. TASK 5300-00-400-802).
R R
(2) Install the partition panels: 132DX, 132CX, 131BX, 131CX, 131DX (Ref. TASK 25-52-00-400-801). (3) Close the forward cargo door (Ref. TASK 52-30-00-410-801). (4) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-30 SROS
Page 611 Jul 01/04
Subtask 05-21-30-860-054 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-21-30 SROS
Page 612 Jul 01/04
___________________________________________________________________ ZONAL INSPECTION : WING CENTER BOX, AIR CONDITIONING AND HYDRAULICS COMPARTMENTS - INSPECTION/CHECK _______________________________ TASK 05-21-40-200-801 R
Zonal Inspection of Wing Center Box WARNING : OBEY THE SAFETY PROCEDURES WHEN YOU DO WORK IN A FUEL TANK. _______ THIS WILL PREVENT INJURY OR DAMAGE. WARNING : DO NOT GET AIRCRAFT FUEL: _______ - IN YOUR MOUTH - IN YOUR EYES - ON YOUR SKIN FOR A LONG TIME. 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 Refer to the MPD TASK: ZL-141-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-12-00-010-801 32-12-00-410-801 57-17-11-000-801 57-17-11-400-801
Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Removal of the Covers 147AZ (148AZ) Installation of the Covers 147AZ (148AZ)
EFF : ALL 05-21-40 SROS
Page 601 Jan 01/04
3. __________ Job Set-up Subtask 05-21-40-010-050 A. Get Access R
(1) Open the main-landing-gear doors: 734 and 744.(Ref. TASK 32-12-00010-801)
R R
(2) Put an ACCESS PLATFORM 2M (6 FT) in position at the access doors 734 and 744. (3) Remove the cover panels 147AZ, 148AZ (Ref. TASK 57-17-11-000-801). 4. Procedure _________ Subtask 05-21-40-210-050
R R
A. Do a general visual inspection of the wing center box (zones 141 and 142). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting) are attached correctly. 5. Close-up ________ Subtask 05-21-40-410-050 A. Close Access (1) Install the cover panels 147AZ, 148AZ, (Ref. TASK 57-17-11-400-801).
R R
(2) Close the main-landing gear doors 734 and 744. (Ref. TASK 32-12-00410-801)
EFF : ALL 05-21-40 SROS
Page 602 Jan 01/04
TASK 05-21-40-200-802 R R
Zonal Inspection of Area Between Keel Beams 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 Refer to the MPD TASK: ZL-143-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-12-00-010-801 32-12-00-410-801
Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-21-40-010-052 A. Get Access R
(1) Open the main-landing-gear doors 734, 744 (Ref. TASK 32-12-00-010801).
R
(2) Put an ACCESS PLATFORM 2M (6 FT) in position at the access doors 734 and 744.
EFF : ALL 05-21-40 SROS
Page 603 Jan 01/04
4. Procedure _________ Subtask 05-21-40-210-052 R R R
A. Do a general visual inspection of the area between the keel beams (zone 143). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping) are attached correctly. 5. Close-up ________ Subtask 05-21-40-410-052 A. Close Access
R R R R
(1) Close the main-landing-gear doors 734, 744 (Ref. TASK 32-12-00-410801). Subtask 05-21-40-860-051 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-40 SROS
Page 604 Jan 01/04
TASK 05-21-40-200-803 R R
Zonal Inspection of Zone Under Cabin Floor 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-145-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R R
52-10-00-010-801 52-10-00-410-801 53-00-00-000-801 53-00-00-400-801
Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door Removal of the Floor Panels in the Cabin from FR17 to FR80 Installation of the Floor Panels in the Cabin from FR17 to FR80
3. __________ Job Set-up Subtask 05-21-40-010-053 A. Get Access R R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the access doors 834 and 844. (2) Open the Mid passenger/crew door (Ref. TASK 52-10-00-010-801).
R R
(3) Remove the floor panels in the cabin from FR40 to FR53.2 (Ref. TASK 53-00-00-000-801).
EFF : ALL 05-21-40 SROS
Page 605 Jan 01/04
4. Procedure _________ Subtask 05-21-40-210-053
R
A. Do a general visual inspection of the pressurized zone under the cabin floor. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping) are attached correctly. 5. Close-up ________ Subtask 05-21-40-410-053 A. Close Access
R R
(1) Install the floor panels in the cabin from FR40 to FR53.2 (Ref. TASK 53-00-00-400-801). (2) Close the Mid Passenger/crew door (Ref. TASK 52-10-00-410-801).
R R R
Subtask 05-21-40-860-052 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-40 SROS
Page 606 Jan 01/04
TASK 05-21-40-200-804 Zonal Inspection of MLG Well and Hydraulic Compartment 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 Refer to the MPD TASK: ZL-147-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-12-00-010-801 32-12-00-410-801
Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-21-40-010-054 A. Get Access (1) Open the main-landing-gear doors 734, 744 (Ref. TASK 32-12-00-010801). (2) Put ACCESS PLATFORM 2M (6 FT) in position at the access doors 734 and 744.
EFF : ALL 05-21-40 R SROS
Page 607 Jul 01/06
4. Procedure _________ Subtask 05-21-40-210-054 R
A. Do a general visual inspection of the main-landing-gear well and the hydraulics compartment (zones 147 and 148). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts. - all the installations (ducting) are attached correctly. 5. Close-up ________ Subtask 05-21-40-410-054 A. Close Access (1) Close the main-landing-gear doors 734, 744 (Ref. TASK 32-12-00-410801). Subtask 05-21-40-860-054 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-40 SROS
Page 608 Jul 01/06
R
TASK 05-21-40-200-809
R
General Visual Inspection of Centerline Gear Well
R
1. __________________ Reason for the Job
R R R
Refer to the MPD TASK: ZL-149-05 2. ______________________ Job Set-up Information A. Referenced Information
R R R
------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R
32-12-00-010-801 32-12-00-410-801
R
3. __________ Job Set-up
R
Subtask 05-21-40-010-058
R
Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance
A. Get Access
R
(1) Open the ground opening-handle access-doors 149AB, 149CB.
R R
(2) Open the main landing gear doors 734, 744 (Ref. TASK 32-12-00-010801).
R
4. Procedure _________
R
Subtask 05-21-40-210-058
R
A. Visual Inspection
R
(1) Do a general visual inspection of the centerline gear well.
EFF : ALL 05-21-40 SROS
Page 609 Oct 01/04
R
5. Close-up ________
R
Subtask 05-21-40-410-058
R
A. Close Access
R R
(1) Close the main landing gear doors 734, 744 (Ref. TASK 32-12-00-410801).
R
(2) Close the ground opening-handle access-doors 149AB, 149CB.
EFF : ALL 05-21-40 SROS
Page 610 Oct 01/04
ZONAL INSPECTION : LOWER DECK AFT CARGO COMPARTMENT - INSPECTION/CHECK ______________________________________________________________________ TASK 05-21-50-200-801 R R
Zonal Inspection of Aft Cargo Compartment (if LD-MCR or LDF and/or DCR and/or ACT(s) installed, as far as visible) 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-151-01 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 ------------------------------------------------------------------------------52-30-00-010-801 52-30-00-410-801
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 05-21-50-010-050 A. Get Access R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at access door 822. (2) Open the aft cargo-compartment door 822 (Ref. TASK 52-30-00-010-801).
EFF : ALL 05-21-50 SROS
Page 601 Jul 01/04
4. Procedure _________ Subtask 05-21-50-210-050 R R
A. Do a general visual inspection of the aft cargo compartment at zones 151 and 152 (as far as you can see if LD-MCR or LDF and/or DCR and/or ACT(s) installed). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring, ducting) are attached correctly. 5. Close-up ________ Subtask 05-21-50-410-050 A. Close Access (1) Close the aft cargo-compartment door 822 (Ref. TASK 52-30-00-410801). Subtask 05-21-50-860-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-50 SROS
Page 602 Jul 01/04
TASK 05-21-50-200-802 Zonal Inspection of Aft Cargo Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-151-02 2. ______________________ Job Set-up Information R
A. Fixtures, Tools, Test and Support Equipment
R R R
------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
R
1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
B. Referenced Information
R R R
------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R R R R R R R R
25-53-00-000-801
R
3. __________ Job Set-up
R
Subtask 05-21-50-010-051-A
R
25-53-00-400-801
Removal of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the AFT Cargo Compartment Installation of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the AFT Cargo Compartment Removal of the Lower-Deck Mobile Crew-Rest (LD-MCR) 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
25-75-41-000-801 52-30-00-010-801 52-30-00-410-801
A. Get Access
R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at access door 822.
R
(2) Open the aft cargo compartment door 822 (Ref. TASK 52-30-00-010-801).
EFF : ALL 05-21-50 SROS
Page 603 Apr 01/04
(3) For aircraft that have the Lower Deck-Mobile Crew Rest: (a) Remove the LD-MCR (Ref. TASK 25-75-41-000-801). (b) Remove the panels that follow (Ref. TASK 25-53-00-000-801). - Ceiling panels 151FC, 151KC, 151PC, 151BY, 151HC. - Partition panels 151BW, 152BW. - Sidewall panels 151TW, 152DW, 152JW, 152AX, 152BX, 151JW. (4) For aircraft without the LD-MCR and without the Lower Deck Lavatories: (a) Remove the panels that follow (Ref. TASK 25-53-00-000-801): - Ceiling panels 151BC, 151FC. - Partition panels 151BW, 152BW. - Sidewall panels 151JW, 151TW, 152DW, 152EW, 152GW, 152JW. (5) For aircraft that have the Lower Deck Lavatories: (a) Remove the panels that follow (Ref. TASK 25-53-00-000-801): - Ceiling panels 151NC, 151EC. - Sidewall panels 151HX, 151LX, 152HX, 152FX, 152LX, 151FX. 4. Procedure _________ Subtask 05-21-50-210-051 R R
A. Do a general visual inspection of the aft cargo compartment. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring, ducting) are attached correctly. 5. Close-up ________ Subtask 05-21-50-410-051-A A. Close Access (1) For aircraft that have the Lower Deck-Mobile Crew Rest: (a) Install the panels that follow (Ref. TASK 25-53-00-400-801). - Ceiling panels 151FC, 151KC, 151PC, 151BY, 151HC. - Partition panels 151BW, 152BW. - Sidewall panels 151TW, 152DW, 152JW, 152AX, 152BX, 151JW.
EFF : ALL 05-21-50 SROS
Page 604 Jul 01/05
(2) For aircraft without the LD-MCR and without the Lower Deck Lavatories: (a) Install the panels that follow (Ref. TASK 25-53-00-400-801): - Ceiling panels 151BC, 151FC. - Partition panels 151BW, 152BW. - Sidewall panels 151JW, 151TW, 152DW, 152EW, 152GW, 152JW. (3) For aircraft that have the Lower Deck Lavatories: (a) Install the panels that follow (Ref. TASK 25-53-00-400-801): - Ceiling panels 151NC, 151EC. - Sidewall panels 151HX, 151LX, 152HX, 152FX, 152LX, 151FX. (4) Close the AFT cargo-compartment door (Ref. TASK 52-30-00-410-801) Subtask 05-21-50-860-052 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-50 R SROS
Page 605 Oct 01/04
TASK 05-21-50-200-803 Zonal Inspection of Aft Cargo Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-151-03 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 ------------------------------------------------------------------------------25-53-00-000-801 25-53-00-400-801 R R
25-75-41-000-801 25-75-41-400-801 28-11-27-000-801 28-11-27-400-801 52-30-00-010-801 52-30-00-410-801
Removal of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the AFT Cargo Compartment Installation of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the AFT Cargo Compartment Removal of the Lower-Deck Mobile Crew-Rest (LD-MCR) Installation of the Lower-Deck Mobile Crew-Rest (LD-MCR) Removal of the Additional Center Tank Installation of the Additional Center Tank 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 05-21-50 SROS
Page 606 Apr 01/04
3. __________ Job Set-up Subtask 05-21-50-010-052 A. Get Access (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at zone 822. (2) Open the aft cargo-compartment door 822 (Ref. TASK 52-30-00-010-801). (3) Remove the ACTs, if installed (Ref. TASK 28-11-27-000-801). R
(4) Remove the LDMCR, if installed (Ref. TASK 25-75-41-000-801).
R R
(5) Remove the sidewall panels and the ceiling panels from FR53.2 to FR66 (Ref. TASK 25-53-00-000-801).
R
(6) Lift the insulation. 4. Procedure _________ Subtask 05-21-50-210-052 A. Do a general visual inspection of the aft cargo compartment. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring, piping) are attached correctly. 5. Close-up ________ Subtask 05-21-50-410-052 A. Close Access
R
(1) Put the insulation back in position.
R R
(2) Install the sidewall panels and the ceiling panels from FR53.2 to FR66 (Ref. TASK 25-53-00-400-801).
R
(3) Install the ACTs, if removed (Ref. TASK 28-11-27-400-801).
R
(4) Install the LDMCR, if removed (Ref. TASK 25-75-41-400-801).
R
(5) Close the aft cargo-compartment door (Ref. TASK 52-30-00-410-801).
EFF : ALL 05-21-50 SROS
Page 607 Jul 01/06
Subtask 05-21-50-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-50 R SROS
Page 608 Apr 01/04
TASK 05-21-50-200-805 Zonal Inspection of Bay Under Aft Cargo Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-153-01 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 ------------------------------------------------------------------------------52-30-00-010-801 52-30-00-410-801
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 Removal of the Floor Panels in the AFT Cargo-Compartment Installation of the Floor Panels in the AFT Cargo-Compartment Fig. 601
53-00-00-000-803 53-00-00-400-803 05-21-50-991-006 3. __________ Job Set-up Subtask 05-21-50-010-054-A A. Get Access
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at zone 822. (2) Open the aft cargo-compartment door 822 (Ref. TASK 52-30-00-010-801). (3) Open the AFT potable-water drain door 154AR. (Ref. Fig. 601/TASK 05-21-50-991-006)
EFF : ALL 05-21-50 R SROS
Page 609 Apr 01/04
R
Aft Fuselage, Lower Deck, Access Panels Zones 152, 154, 164 and 171 Figure 601/TASK 05-21-50-991-006
EFF : ALL 05-21-50 SROS
Page 610 Jan 01/06
(4) Remove the floor panels from FR53.2 to FR66 (Ref. TASK 53-00-00-000803). (5) For aircraft equipped with the Lower Deck Lavatories: (a) Remove the access panels 152AR, 152BR, 152CR, 152DR, 152ER, 152FR, 152GR, 152HR, 152JR, 152KR, 152LR. R
(6) Lift the insulation. 4. Procedure _________ Subtask 05-21-50-210-054 A. Do a general visual inspection of the underfloor bay of the aft cargo compartment. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring, ducting) are attached correctly. 5. Close-up ________ Subtask 05-21-50-410-054-A A. Close Access (1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Put the insulation back in position.
R
(3) Install the floor panels from FR53.2 to FR66 (Ref. TASK 53-00-00-400803).
R
(4) For aircraft equipped with the Lower Deck Lavatories: (a) Close the access panels 152AR, 152BR, 152CR, 152DR, 152ER, 152FR, 152GR, 152HR, 152JR, 152KR, 152LR.
R
(5) Close the AFT potable-water drain door 154AR.
R
(6) Close the AFT cargo-compartment door (Ref. TASK 52-30-00-410-801).
EFF : ALL 05-21-50 SROS
Page 611 Jul 01/06
Subtask 05-21-50-860-053 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-21-50 SROS
Page 612 Jul 01/06
ZONAL INSPECTION : LOWER DECK BULK CARGO COMPARTMENT - INSPECTION/CHECK _______________________________________________________________________ TASK 05-21-60-200-801 R
Zonal Inspection of Bulk Cargo Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-161-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------52-30-00-010-801 52-30-00-410-801
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 05-21-60-010-050 A. Get Access R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at access door 822.
R
(2) Open the aft cargo-compartment door 822 (Ref. TASK 52-30-00-010-801).
EFF : ALL 05-21-60 SROS
Page 601 Jan 01/04
4. Procedure _________ Subtask 05-21-60-210-050 A. Do a general visual inspection of the bulk cargo compartment (zones 161 and 162), (if BCRC or waste chute container installed, as far as you can see). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-21-60-410-050 A. Close Access R R
(1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Close the aft cargo-compartment door 822 (Ref. TASK 52-30-00-410801). Subtask 05-21-60-860-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R
EFF : ALL 05-21-60 SROS
Page 602 Jan 01/06
TASK 05-21-60-200-802 R
Zonal Inspection of Bulk Cargo Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-161-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------25-54-00-000-801 25-54-00-400-801 R R R R
52-30-00-010-801 52-30-00-410-801
Removal of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the BULK Cargo-Compartment Installation of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the BULK Cargo-Compartment 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 05-21-60-010-051 A. Get Access R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at access door 822.
R
(2) Open the aft cargo-compartment door 822 (Ref. TASK 52-30-00-010-801). (3) Remove the ceiling panels: 161AC, 161BC, 161EC. (Ref. TASK 25-54-00000-801)
EFF : ALL 05-21-60 SROS
Page 603 Jan 01/04
(4) Remove the sidewall panels: 161CW, 162LW, 162RW, 162SW, 162TW, 162WW. (Ref. TASK 25-54-00-000-801) 4. Procedure _________ Subtask 05-21-60-210-051
R
A. Do a general visual inspection of the bulk cargo compartment (zones 161 and 162). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-21-60-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the ceiling panels: 161AC, 161BC, 161EC. (Ref. TASK 25-54-00400-801) (3) Install the access panels: 161CW, 162LW, 162RW, 162SW, 162TW, 162WW. (Ref. TASK 25-54-00-400-801) (4) Close the aft cargo-compartment door 822 (Ref. TASK 52-30-00-410801). Subtask 05-21-60-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-21-60 SROS
Page 604 Jan 01/06
TASK 05-21-60-200-803 Zonal Inspection of Bulk Cargo Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-161-03 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 ------------------------------------------------------------------------------25-54-00-000-801 25-54-00-400-801 R R
52-30-00-010-803 52-30-00-410-803
Removal of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the BULK Cargo-Compartment Installation of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the BULK Cargo-Compartment Opening of the BULK Cargo-Compartment Door Closing of the BULK Cargo-Compartment Door
3. __________ Job Set-up Subtask 05-21-60-010-052 A. Get Access R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at access door 823.
R R
(2) Open the BULK cargo-compartment door 823 (Ref. TASK 52-30-00-010803).
R
(3) Remove the sidewall and ceiling panels from FR65 to FR73. (Ref. TASK 25-54-00-000-801)
EFF : ALL 05-21-60 SROS
Page 605 Jul 01/06
4. Procedure _________ Subtask 05-21-60-210-052 A. Do a general visual inspection of the bulk cargo compartment (zones 161). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-21-60-410-052 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the sidewall and ceiling panels from FR65 to FR73. (Ref. TASK 25-54-00-400-801) R R
(3) Close the BULK cargo-compartment door 823 (Ref. TASK 52-30-00-410803). Subtask 05-21-60-860-052 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-21-60 SROS
Page 606 Jul 01/06
TASK 05-21-60-200-804 Zonal Inspection of Bay Under Bulk Cargo Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-163-01 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 ------------------------------------------------------------------------------25-54-00-000-801 25-54-00-400-801 52-30-00-010-801 52-30-00-410-801 05-21-60-991-005
Removal of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the BULK Cargo-Compartment Installation of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the BULK Cargo-Compartment 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 Fig. 601
3. __________ Job Set-up Subtask 05-21-60-010-053 A. Get Access (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the AFT cargo-compartment door. R
(2) Open the AFT cargo-compartment door 822 (Ref. TASK 52-30-00-010-801).
EFF : ALL 05-21-60 SROS
Page 607 Jan 01/06
(3) Open the potable-water service-panel door 164AR. (Ref. Fig. 601/TASK 05-21-60-991-005) R
(4) Remove the floor panels from FR65 to FR73 (Ref. TASK 25-54-00-000801). 4. Procedure _________ Subtask 05-21-60-210-053 A. Do a general visual inspection of the underfloor bay of the bulk cargo compartment (zones 163 and 164). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-21-60-410-053 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the floor panels from FR65 to FR73. (Ref. TASK 25-54-00-400801)
R
(3) Close the potable-water service-panel door 164AR. (4) Close the AFT cargo compartment door. (Ref. TASK 52-30-00-410-801) (5) Remove the access platform(s). Subtask 05-21-60-860-053 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-21-60 SROS
Page 608 Jan 01/06
R
Aft Fuselage, Lower Section, Access Panels Figure 601/TASK 05-21-60-991-005
EFF : ALL 05-21-60 SROS
Page 609 Jan 01/06
ZONAL INSPECTION : AFT CABIN UNDERFLOOR COMPARTMENT - INSPECTION/CHECK ______________________________________________________________________ TASK 05-21-70-200-801 Zonal Inspection of Aft Cabin Underfloor Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-171-01 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 ------------------------------------------------------------------------------25-54-00-000-801 25-54-00-400-801 52-30-00-010-801 52-30-00-410-801 05-21-70-991-003
Removal of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the BULK Cargo-Compartment Installation of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the BULK Cargo-Compartment 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 Fig. 601
3. __________ Job Set-up Subtask 05-21-70-010-050 A. Get Access R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the aft cargo-compartment door.
R
(2) Open the aft cargo-compartment door 822 (Ref. TASK 52-30-00-010-801).
EFF : ALL 05-21-70 SROS
Page 601 Jul 01/04
(3) Open the access door 171AL. (Ref. Fig. 601/TASK 05-21-70-991-003) R
(4) Remove the partition panel 162ZW (Ref. TASK 25-54-00-000-801). 4. Procedure _________ Subtask 05-21-70-210-050 A. Do a general visual inspection of the aft-cabin underfloor compartment (Zones 171 and 172). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (ducting, piping) are attached correctly. 5. Close-up ________ Subtask 05-21-70-410-050 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the partition panel 162ZW. (Ref. TASK 25-54-00-400-801) (3) Close the access door 171AL.
R
(4) Close the aft cargo-compartment door 822 (Ref. TASK 52-30-00-410801). Subtask 05-21-70-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-21-70 SROS
Page 602 Jul 01/04
R
Aft Fuselage, Lower Section, Access Panels Figure 601/TASK 05-21-70-991-003
EFF : ALL 05-21-70 SROS
Page 603 Jan 01/06
TASK 05-21-70-200-802 Zonal Inspection of Aft Cabin Underfloor Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-171-02 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 ------------------------------------------------------------------------------25-54-00-000-801 25-54-00-400-801 52-30-00-010-801 52-30-00-410-801 R R R
53-42-17-000-801 53-42-17-400-801 05-21-70-991-003
Removal of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the BULK Cargo-Compartment Installation of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the BULK Cargo-Compartment 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 Removal of the Floor Panels Between FR73 and FR79 Installation of the Floor Panels Between FR73 and FR79 Fig. 601
EFF : ALL 05-21-70 SROS
Page 604 Jul 01/05
3. __________ Job Set-up Subtask 05-21-70-010-051 A. Get Access (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the aft cargo-compartment door. (2) Open the aft cargo-compartment door 822 (Ref. TASK 52-30-00-010-801). (3) Open the access door 171AL. (Ref. Fig. 601/TASK 05-21-70-991-003) (4) Remove the partition panel 162ZW (Ref. TASK 25-54-00-000-801). R R
(5) Remove the floor panels from FR73 to FR80 (Ref. TASK 53-42-17-000801). (6) Lift the insulation. 4. Procedure _________ Subtask 05-21-70-210-051 A. Do a general visual inspection of the aft-cabin underfloor compartment (zones 171 and 172). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-21-70-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Put the insulation back in position.
R R
(3) Install the floor panels from FR73 to FR80 (Ref. TASK 53-42-17-400801). (4) Install the partition panel 162ZW (Ref. TASK 25-54-00-400-801).
EFF : ALL 05-21-70 SROS
Page 605 Jul 01/05
R
(5) Close the access door 171AL.
R R
(6) Close the aft cargo-compartment door 822 (Ref. TASK 52-30-00-410801). Subtask 05-21-70-860-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-21-70 SROS
Page 606 Jul 01/04
________________________________________________________________________ ZONAL INSPECTION: AIR CONDITIONING, HYDRAULICS COMPARTMENTS AND FAIRINGS ________________ INSPECTION/CHECK TASK 05-21-90-200-801 R R
Zonal Inspection of Air Conditioning Compt and Fairing 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-191-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------53-35-13-000-802 53-35-13-400-802
Removal of the Belly Fairing Access Panels Installation of the Belly Fairing Access Panels
3. __________ Job Set-up Subtask 05-21-90-010-050 A. Get Access R R
(1) Put an ACCESS PLATFORM 2M (6 FT) in position at the air conditioning compartment and fairings. (2) For the right side, zone 192: (a) Remove the access panels 192JB, 192PB (Ref. TASK 53-35-13-000802).
EFF : ALL 05-21-90 SROS
Page 601 Jan 01/04
(3) For left side, zone 191: (a) Remove the access panels 191FB, 191KB (Ref. TASK 53-35-13-000802). 4. Procedure _________ Subtask 05-21-90-210-050
R
A. Do a general visual inspection of the air conditioning compartment and fairings. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring, piping) are attached correctly. 5. Close-up ________ Subtask 05-21-90-410-050 A. Close Access
R R
(1) Make sure that the work area is clean and clear of tools and other items.
R
(2) For the right side zone 192: (a) Install the access panel 192JB, 192PB (Ref. TASK 53-35-13-400802).
R
(3) For the left side zone 191: (a) Install the access panels 191FB, 191KB (Ref. TASK 53-35-13-400802).
R R R
(4) Remove the access platform(s). Subtask 05-21-90-860-051 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-21-90 SROS
Page 602 Jan 01/04
TASK 05-21-90-200-802 R R
Zonal Inspection of Air Conditioning Compt and Fairing 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-191-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------53-35-11-000-801 53-35-11-400-801 53-35-13-000-801 53-35-13-000-802 53-35-13-400-801 53-35-13-400-802
Removal of the Wing-to-Fuselage Fairings Installation of the Wing-to-Fuselage Fairings Removal of the Access Panels 191AB, 191BB, 192BB, 191DB, 197AB, 197AT, 198AT, 197BB, 198BB, 197EB, 198EB, 197FB, 197GB, 198GB, 198HB and 197HB. Removal of the Belly Fairing Access Panels Installation of the Access Panels 191AB, 191BB, 192BB, 191DB, 197AB, 197AT, 198AT, 197BB, 198BB, 197EB, 198EB, 197FB, 197GB, 198GB, 198HB and 197HB. Installation of the Belly Fairing Access Panels
EFF : ALL 05-21-90 SROS
Page 603 Jan 01/04
3. __________ Job Set-up Subtask 05-21-90-010-051 A. Get Access R R
(1) Put an ACCESS PLATFORM 2M (6 FT)in position at the air conditioning compartment and fairings. (2) For the left side zone 191:
R R R R
(a) Remove the access panels 191AB, 191BB, 191CB, 191DB, 191FB, 191HB, 191KB, 191QB, 191AT, 191BT, 191CT 191EB (Ref. TASK 53-3511-000-801) (Ref. TASK 53-35-13-000-802) (Ref. TASK 53-35-13-000801). (3) For the right side zone 192:
R R R
(a) Remove the access panels: 192BB, 192CB, 192GB, 192HB, 192JB, 192MB, 192NB, 192PB, 192QB, 192AT, 192BT, 192CT (Ref. TASK 53-3513-000-801). (Ref. TASK 53-35-13-000-802) 4. Procedure _________ Subtask 05-21-90-210-051
R
A. Do a general visual inspection of the air conditioning compartment and fairings. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring, piping) are attached correctly.
EFF : ALL 05-21-90 SROS
Page 604 Jan 01/04
5. Close-up ________ Subtask 05-21-90-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) For the left side zone 191: (a) Install the access panels 191AB, 191BB, 191CB, 191DB, 191FB, 191HB, 191KB, 191QB, 191AT, 191BT, 191CT 191EB (Ref. TASK 53-3511-400-801) (Ref. TASK 53-35-13-400-801) (Ref. TASK 53-35-13-400802) (3) For the right side zone 192: (a) Install the access panels 192BB, 192CB, 192GB, 192HB, 192JB, 192MB, 192NB, 192PB, 192QB, 192AT, 192BT, 192CT, (Ref. TASK 5335-13-400-801), (Ref. TASK 53-35-13-400-802). (Ref. TASK 53-3511-400-801) Subtask 05-21-90-860-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-21-90 R SROS
Page 605 Jan 01/06
TASK 05-21-90-200-805 Zonal Inspection of Hydraulic Compartment and Fairings 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 Refer to the MPD TASK: ZL-195-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-12-00-010-801 32-12-00-410-801
Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-21-90-010-054 A. Get Access R R
(1) For the left side zone 147:
R
(a) Open the main landing-gear access door 734 (Ref. TASK 32-12-00010-801).
R
(2) For the right side zone 148:
R
(a) Open the main landing-gear access door 744 (Ref. TASK 32-12-00010-801).
EFF : ALL 05-21-90 SROS
Page 606 Jan 01/06
R R
(3) Put an ACCESS PLATFORM 2M (6 FT) in position at the hydraulic compartment and fairings. 4. Procedure _________ Subtask 05-21-90-210-054 A. Do a general visual inspection of the hydraulics compartment and fairings. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-21-90-410-054 A. Close Access
R
(1) For the left side zone 147:
R
(a) Close the access door 734 (Ref. TASK 32-12-00-410-801).
R
(2) For the right side zone 148:
R
(a) Close the access door 744 (Ref. TASK 32-12-00-410-801). Subtask 05-21-90-860-054 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-90 SROS
Page 607 Jan 01/06
TASK 05-21-90-200-806 R
Zonal Inspection of Hydraulics Compartment and Fairings 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-195-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------53-35-13-000-802 53-35-13-400-802
Removal of the Belly Fairing Access Panels Installation of the Belly Fairing Access Panels
3. __________ Job Set-up Subtask 05-21-90-010-055-A A. Get Access (1) Put an ACCESS PLATFORM 2M (6 FT) in position at the hydraulics compartment and fairings. (2) For the left side zone 195: (a) Open the blue ground service panel: 195BB. (b) Remove the access panels: 195CB, 195DB (Ref. TASK 53-35-13-000802).
EFF : ALL 05-21-90 SROS
Page 608 Jan 01/06
(3) For the right side zone 196: (a) Open the yellow ground service panel: 196BB. 4. Procedure _________ Subtask 05-21-90-210-055 A. Do a general visual inspection of the hydraulics compartment and fairings. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-21-90-410-055-A A. Close Access (1) For the left side zone 195: (a) Install the access panels: 195CB, 195DB (Ref. TASK 53-35-13-400802). (b) Close the blue ground service panel: 195BB. (2) For the right side zone 196: (a) Close the yellow ground service panel: 196BB. Subtask 05-21-90-860-055 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-90 R SROS
Page 609 Jan 01/07
TASK 05-21-90-200-807 Zonal Inspection of Rear Fairings 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-197-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-12-00-010-801 32-12-00-410-801
Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-21-90-010-056 A. Get Access R
(1) Put an ACCESS PLATFORM 2M (6 FT) in position at the rear fairing. (2) For the left side zone 197: (a) Open the access door 734. (Ref. TASK 32-12-00-010-801) (3) For the right side zone 198: (a) Open the access door 744. (Ref. TASK 32-12-00-010-801)
EFF : ALL 05-21-90 SROS
Page 610 Jan 01/07
4. Procedure _________ Subtask 05-21-90-210-056 A. Do a general visual inspection of the rear fairing. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-21-90-410-056 A. Close Access (1) For the left side zone 197: (a) Close the access door 734. (Ref. TASK 32-12-00-410-801) (2) For the right side zone 198: (a) Close the access door 744. (Ref. TASK 32-12-00-410-801) Subtask 05-21-90-860-056 B. Put the Aircraft back to its Initial Configuration R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-90 SROS
Page 611 Jan 01/06
TASK 05-21-90-200-808 Zonal Inspection of Rear Fairings 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-197-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------53-35-13-000-801 53-35-13-400-801
Removal of the Access Panels 191AB, 191BB, 192BB, 191DB, 197AB, 197AT, 198AT, 197BB, 198BB, 197EB, 198EB, 197FB, 197GB, 198GB, 198HB and 197HB. Installation of the Access Panels 191AB, 191BB, 192BB, 191DB, 197AB, 197AT, 198AT, 197BB, 198BB, 197EB, 198EB, 197FB, 197GB, 198GB, 198HB and 197HB.
3. __________ Job Set-up Subtask 05-21-90-010-057 A. Get Access (1) Put an ACCESS PLATFORM 2M (6 FT) in position at the rear fairing. (2) For the left side zone 197: (a) Remove the access panel 197EB. (Ref. TASK 53-35-13-000-801) (3) For the right side zone 198: (a) Remove the access panel 198EB. (Ref. TASK 53-35-13-000-801)
EFF : ALL 05-21-90 R SROS
Page 612 Jan 01/06
4. Procedure _________ Subtask 05-21-90-210-057 A. Do a general visual inspection of the rear fairing. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-21-90-410-057 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) For the left side zone 197: (a) Install the access panel 197EB. (Ref. TASK 53-35-13-400-801) (3) For the right side zone 198: (a) Install the access panel 198EB. (Ref. TASK 53-35-13-400-801) Subtask 05-21-90-860-057 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-21-90 R SROS
Page 613 Jan 01/06
TASK 05-21-90-200-810 Zonal Inspection of Air Conditioning Compartment and Fairing 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-193-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R
52-42-29-000-801 52-42-29-400-801 53-35-13-000-802 53-35-13-400-802
Removal of the Overpressure Door of the Panel 193DB Installation of the Overpressure Door of the Panel 193DB Removal of the Belly Fairing Access Panels Installation of the Belly Fairing Access Panels
3. __________ Job Set-up Subtask 05-21-90-010-059 A. Get Access (1) Put an ACCESS PLATFORM 2M (6 FT) in position at the air conditioning compartment and fairings. (a) Open the access panels 193BB, 193DB (Ref. TASK 53-35-13-000-802) (Ref. TASK 52-42-29-000-801).
EFF : ALL 05-21-90 SROS
Page 614 Jan 01/06
4. Procedure _________ Subtask 05-21-90-210-059 A. Do a general visual inspection of the air conditioning compartment and fairings. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring, piping) are attached correctly. 5. Close-up ________ Subtask 05-21-90-410-059 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels 193BB, 193DB (Ref. TASK 53-35-13-400-802) (Ref. TASK 52-42-29-400-801). Subtask 05-21-90-860-052 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-21-90 R SROS
Page 615 Jan 01/06
TASK 05-21-90-200-811 Zonal Inspection of Air Conditioning Compartment and Fairing 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-193-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R
52-42-29-000-801 52-42-29-400-801 53-35-13-000-802 53-35-13-400-802
Removal of the Overpressure Door of the Panel 193DB Installation of the Overpressure Door of the Panel 193DB Removal of the Belly Fairing Access Panels Installation of the Belly Fairing Access Panels
3. __________ Job Set-up Subtask 05-21-90-010-060 A. Get Access (1) Put an ACCESS PLATFORM 2M (6 FT) in position at the air conditioning compartment and fairings. (a) Remove the access panels 193AB, 193BB, 193DB (Ref. TASK 53-35-13000-802) (Ref. TASK 52-42-29-000-801). (b) Open the access door 193CB.
EFF : ALL 05-21-90 SROS
Page 616 Jan 01/06
4. Procedure _________ Subtask 05-21-90-210-060
R
A. Do a general visual inspection of the air conditioning compartment and fairings. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring, piping) are attached correctly. 5. Close-up ________ Subtask 05-21-90-410-060 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items.
R R
(2) Install the access panels 193AB, 193BB, 193DB (Ref. TASK 53-35-13400-802) (Ref. TASK 52-42-29-400-801). (3) Close the access door 193CB.
R R R
Subtask 05-21-90-860-053 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-21-90 SROS
Page 617 Jan 01/04
ZONAL INSPECTION : UPPER HALF OF FUSELAGE - INSPECTION/CHECK ____________________________________________________________ TASK 05-22-00-200-801 Zonal Inspection of the Upper Half of the fuselage (Zone 200). 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information Not Applicable 3. __________ Job Set-up Subtask 05-22-00-869-050 A. Not applicable. 4. Procedure _________ Subtask 05-22-00-210-050 A. Visual inspection. (1) Do a general visual inspection of the upper half of the fuselage from the ground.
EFF : ALL 05-22-00 R SROS
Page 601 Jan 01/04
TASK 05-22-00-200-802 R
Zonal Inspection of Upper Half of Fuselage 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-200-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R
No specific
1 ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE
3. __________ Job Set-up Subtask 05-22-00-010-051 A. Get Access R
(1) Put an ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE in position in the upper half of the fuselage. 4. Procedure _________ Subtask 05-22-00-210-051 A. Inspection (1) Do a general visual inspection of the upper half of the fuselage up to the stringer 26LH and RH (zone 200) and around the doors. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see.
R
R
EFF : ALL 05-22-00 SROS
Page 602 Jan 01/04
R
5. Close-up ________
R
Subtask 05-22-00-860-050
R
A. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-22-00 SROS
Page 603 Jan 01/04
ZONAL INSPECTION : COCKPIT - INSPECTION/CHECK _____________________________________________ TASK 05-22-10-200-801 Zonal Inspection of Cockpit 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-211-01 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
25-13-44-000-802 25-13-44-400-802 52-10-00-010-801 52-10-00-410-801 05-22-10-991-001
Removal of the Sidewall Panels Installation of the Sidewall Panels Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door Fig. 601
3. __________ Job Set-up Subtask 05-22-10-010-050 A. Get Access (Ref. Fig. 601/TASK 05-22-10-991-001) (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the access door 831 or 841. (2) Open the passenger/crew door (Ref. TASK 52-10-00-010-801). R
(3) Remove the sidewall panels (Ref. TASK 25-13-44-000-802): For the left side: 211JW, 211KW. For the right side: 212JW, 212KW.
EFF : ALL 05-22-10 SROS
Page 601 Jan 01/06
Ceiling and Sidewall Panels of the Cockpit Figure 601/TASK 05-22-10-991-001 EFF : ALL 05-22-10 SROS
Page 602 Apr 01/98
4. Procedure _________ Subtask 05-22-10-210-050 A. Do a general visual inspection of the cockpit. Make sure that: - there is no damage, corrosion, leaks or cracks on all the parts of the components and the structure you can see. - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-22-10-410-050 A. Close Access R R
(1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Install the sidewall panels (Ref. TASK 25-13-44-400-802): For the left side: 211JW, 211KW. For the right side: 212JW, 212KW.
R
(3) Close the passenger/crew door (Ref. TASK 52-10-00-410-801). Subtask 05-22-10-860-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R
EFF : ALL 05-22-10 SROS
Page 603 Jan 01/06
TASK 05-22-10-200-802 Zonal Inspection of Cockpit 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-211-02 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 ------------------------------------------------------------------------------25-13-44-000-801 25-13-44-000-802 25-13-44-400-801 25-13-44-400-802 52-10-00-010-801 52-10-00-410-801 53-12-11-000-801 53-12-11-400-801 05-22-10-991-001
Removal of the Ceiling Panels Removal of the Sidewall Panels Installation of the Ceiling Panels Installation of the Sidewall Panels Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door Removal of the Cockpit Floor Panels from FR1 thru FR11 Installation of the Cockpit Floor Panels from FR1 thru FR11 Fig. 601
3. __________ Job Set-up Subtask 05-22-10-010-051 A. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the access door 831 or 841. R
(2) Open the passenger/crew door 831 or 841 (Ref. TASK 52-10-00-010-801).
EFF : ALL 05-22-10 SROS
Page 604 Jul 01/06
(3) Remove the sidewall panels (Ref. TASK 25-13-44-000-802): (Ref. Fig. 601/TASK 05-22-10-991-001) For the left side: 211AW, 211BW, 211CW, 211DW, 211EW, 211FW, 211GW, 211HW, 211JW, 211KW, 211LW, 211MW, 211PW. For the right side: 212CW, 212DW, 212EW, 212FW, 212GW, 212HW, 212JW, 212KW, 212LW, 212MW, 212NW, 212QW.
R R
(4) Remove the ceiling panels (Ref. TASK 25-13-44-000-801): For the left side: 211AC, 211BC, 211CC, 211DC, 211EC, 211GC, 211HC, 211JC, 211KC, 211LC, 211MC. For the right side: 212BC, 212CC, 212DC, 212FC, 212GC, 212HC, 212JC, 212NC. (5) Remove the floor panels from FR1 to FR11 (Ref. TASK 53-12-11-000801). 4. Procedure _________ Subtask 05-22-10-210-051 A. Do a general visual inspection of the cockpit. Make sure that: - there is no damage, corrosion, leaks or cracks on all the parts of the components and the structure you can see. - all the installations (wiring, ducting) are attached correctly. NOTE : Lift the insulation sufficiently to make sure that there is no ____ corrosion or signs of leaks. 5. Close-up ________ Subtask 05-22-10-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the floor panels from FR1 to FR11 (Ref. TASK 53-12-11-400801).
EFF : ALL 05-22-10 SROS
Page 605 Jul 01/06
(3) Install the ceiling panels (Ref. TASK 25-13-44-400-801): For the left side: 211AC, 211BC, 211CC, 211DC, 211EC, 211GC, 211HC, 211JC, 211KC, 211LC, 211MC. For the right side: 212BC, 212CC, 212DC, 212FC, 212GC, 212HC, 212JC, 212NC. (4) Install the sidewall panels (Ref. TASK 25-13-44-400-802): For the left side: 211AW, 211BW, 211CW, 211DW, 211EW, 211FW, 211GW, 211HW, 211JW, 211KW, 211LW, 211MW, 211PW. For the right side: 212CW, 212DW, 212EW, 212FW, 212GW, 212HW, 212JW, 212KW, 212LW, 212MW, 212NW, 212QW. R
(5) Close the passenger/crew door 831 or 841 (Ref. TASK 52-10-00-410801). Subtask 05-22-10-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-22-10 SROS
Page 606 Jul 01/06
ZONAL INSPECTION : FORWARD CABIN UTILITY AREAS - INSPECTION/CHECK _________________________________________________________________ TASK 05-22-20-200-802 Zonal Inspection of FWD Cabin Utility Area 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-221-02 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 ------------------------------------------------------------------------------25-22-41-000-801 25-22-41-400-801 25-22-44-000-801 25-22-44-400-801 R
25-23-45-000-801
R
25-23-45-400-801 25-26-41-000-801 25-26-41-400-801 25-26-42-000-801 25-26-42-400-801 25-27-15-000-801 25-27-15-400-801 25-27-41-000-801 25-27-41-400-801 25-31-41-000-801 25-31-41-400-801 25-31-43-000-801
Removal of the Wall-Mounted Cabin-Attendant Seat Installation of the Wall-Mounted Cabin-Attendant Seat Removal of the Free-Standing Cabin-Attendant Seat, Seat Rail Mounted Installation of the Free-Standing Cabin-Attendant Seat, Seat Rail Mounted Removal of the Door Frame Linings of the Forward Passenger/Crew Door Installation of the Door Frame Linings of the Forward Passenger/Crew Door Removal of the Curtains and the Curtain Rails Installation of the Curtains and the Curtain Rails Removal of the Partitions Installation of the Partitions Removal of the Emergency Equipment Stowage Installation of the Emergency Equipment Stowage Removal of the Stowages Installation of the Stowages Removal of the FWD RH Galley Unit (6479ML) Installation of the FWD RH Galley Unit (6479ML) Removal of the FWD Center-Galley Unit 6477ML
EFF : ALL 05-22-20 SROS
Page 601 Jan 01/06
------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R
25-31-43-000-802 25-31-43-400-801 25-31-43-400-802 25-31-51-000-801 25-31-51-400-801 25-31-52-000-801 25-31-52-400-801 25-31-59-000-801 25-31-59-400-801 25-41-41-000-801 25-41-41-400-801 25-41-44-000-801 25-41-44-400-801 25-41-45-000-801 25-41-45-400-801 25-74-41-000-801 25-74-41-400-801
Removal of the FWD Center-Galley Unit 6477ML01 Installation of the FWD Center-Galley Unit 6477ML Installation of the FWD Center-Galley Unit 6477ML01 Removal of the FWD Galley Unit (6491ML) Installation of the FWD Galley Unit (6491ML) Removal of the FWD Galley Unit (6492ML) Installation of the FWD Galley Unit (6492ML) Removal of the Galley Unit (6489ML) Installation of the Galley Unit (6489ML) Removal of Lavatory A Installation of Lavatory A Removal of the Lavatory J Installation of the Lavatory J Removal of the Lavatory N Installation of the Lavatory N Removal of the Flight Crew Rest Compartment (FCRC) Installation of the Flight Crew Rest Compartment (FCRC) Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door Removal of the Cabin Floor Panels from FR11 thru FR17. Installation of the Cabin Floor Panels from FR11 thru FR17.
52-10-00-010-801 52-10-00-410-801 53-12-12-000-801 53-12-12-400-801 3. __________ Job Set-up Subtask 05-22-20-010-051 A. Get Access
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the FWD passenger/crew door. (2) Open the FWD passenger/crew door 831, 841 (Ref. TASK 52-10-00-010801). (3) Remove the (Ref. TASK (Ref. TASK (Ref. TASK (Ref. TASK
galleys, if installed 25-31-41-000-801), 25-31-43-000-801) or (Ref. TASK 25-31-43-000-802), 25-31-51-000-801), (Ref. TASK 25-31-52-000-801), 25-31-59-000-801).
EFF : ALL 05-22-20 SROS
Page 602 Jul 01/06
(4) Remove the (Ref. TASK (Ref. TASK (Ref. TASK
lavatories, if installed 25-41-41-000-801), 25-41-44-000-801), 25-41-45-000-801).
(5) Remove the (Ref. TASK (Ref. TASK (Ref. TASK
seats and the furnishings, if installed 25-22-41-000-801), (Ref. TASK 25-22-44-000-801), 25-26-41-000-801), (Ref. TASK 25-26-42-000-801), 25-27-15-000-801) or (Ref. TASK 25-27-41-000-801).
R R
(6) Remove the flight crew rest compartment, if installed (Ref. TASK 2574-41-000-801).
R
(7) Remove the floor panels around and below the galleys and the toilets (Ref. TASK 53-12-12-000-801).
R
(8) Remove the door frame linings (Ref. TASK 25-23-45-000-801).
R
(9) Lift the insulation sufficiently to do the inspection. 4. Procedure _________ Subtask 05-22-20-210-051 A. Do a general visual inspection of the forward cabin utility-area (zones 221 and 222). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, wiring) are attached correctly. 5. Close-up ________ Subtask 05-22-20-410-051 A. Close Access (1) Put the insulation back in position. (2) Install the door frame linings (Ref. TASK 25-23-45-400-801). (3) Install the floor panels (Ref. TASK 53-12-12-400-801).
R R
(4) Install the flight crew rest compartment, if removed (Ref. TASK 2574-41-400-801).
EFF : ALL 05-22-20 SROS
Page 603 Jul 01/06
R
(5) Install the seats and the furnishings, if removed (Ref. TASK 25-22-41-400-801), (Ref. TASK 25-22-44-400-801), (Ref. TASK 25-26-41-400-801), (Ref. TASK 25-26-42-400-801), (Ref. TASK 25-27-15-400-801) or (Ref. TASK 25-27-41-400-801).
R
(6) Install the galleys, if removed (Ref. TASK 25-31-41-400-801), (Ref. TASK 25-31-43-400-801) or (Ref. TASK 25-31-43-400-802), (Ref. TASK 25-31-51-400-801), (Ref. TASK 25-31-52-400-801), (Ref. TASK 25-31-59-400-801).
R
(7) Install the lavatories, if removed (Ref. TASK 25-41-41-400-801), (Ref. TASK 25-41-44-400-801), (Ref. TASK 25-41-45-400-801).
R
(8) Close the FWD passenger/crew door 831, 841 (Ref. TASK 52-10-00-410801). Subtask 05-22-20-860-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-22-20 SROS
Page 604 Jul 01/06
TASK 05-22-20-200-804 R
Zonal Inspection of FWD Cabin Utility-Area Overhead-Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-223-01 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
25-23-42-000-801 25-23-42-400-801 25-31-41-000-801 25-31-41-400-801 25-31-43-000-801 25-31-43-000-802 25-31-43-400-801 25-31-51-000-801 25-31-51-400-801 25-31-52-000-801 25-31-52-400-801 25-41-41-000-801 25-41-41-400-801 25-41-44-000-801 25-41-44-400-801 25-41-44-400-802 25-41-45-000-801 25-41-45-400-801 25-41-45-400-802 25-74-41-000-801 25-74-41-400-801 52-10-00-010-801
Removal of the FWD and AFT Exit Ceiling-Panels Installation of the FWD and AFT Exit Ceiling-Panels Removal of the FWD RH Galley Unit (6479ML) Installation of the FWD RH Galley Unit (6479ML) Removal of the FWD Center-Galley Unit 6477ML Removal of the FWD Center-Galley Unit 6477ML01 Installation of the FWD Center-Galley Unit 6477ML Removal of the FWD Galley Unit (6491ML) Installation of the FWD Galley Unit (6491ML) Removal of the FWD Galley Unit (6492ML) Installation of the FWD Galley Unit (6492ML) Removal of Lavatory A Installation of Lavatory A Removal of the Lavatory J Installation of the Lavatory J SPARE TASK FOR LATER USE Removal of the Lavatory N Installation of the Lavatory N SPARE TASK FOR LATER USE Removal of the Flight Crew Rest Compartment (FCRC) Installation of the Flight Crew Rest Compartment (FCRC) Opening of the Passenger/Crew Door
EFF : ALL 05-22-20 SROS
Page 605 Jan 01/06
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------52-10-00-410-801
Closing of the Passenger/Crew Door
3. __________ Job Set-up Subtask 05-22-20-010-053 A. Get Access R R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the FWD passenger/crew door. (2) Open the FWD passenger/crew door 831, 841 (Ref. TASK 52-10-00-010801). (3) Remove the (Ref. TASK (Ref. TASK (Ref. TASK
galleys, if installed 25-31-41-000-801), 25-31-43-000-801) or (Ref. TASK 25-31-43-000-802), 25-31-51-000-801), (Ref. TASK 25-31-52-000-801).
(4) Remove the (Ref. TASK (Ref. TASK (Ref. TASK
lavatories, if installed 25-41-41-000-801), 25-41-44-000-801), 25-41-45-000-801).
(5) Remove the rest room container, if installed (Ref. TASK 25-74-41-000-801). (6) Remove the ceiling panels 221AZ, 221BZ, 222AZ, 222BZ (Ref. TASK 25-23-42-000-801). R
(7) Lift the insulation sufficiently to do the inspection. 4. Procedure _________ Subtask 05-22-20-210-053 A. Do a general visual inspection of the forward cabin overhead-compartment (zones 223 and 224). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping, wiring) are attached correctly.
EFF : ALL 05-22-20 SROS
Page 606 Jul 01/06
5. Close-up ________ Subtask 05-22-20-410-053 A. Close Access (1) Put the insulation back in position. (2) Install the ceiling panels 221AZ, 221BZ, 222AZ, 222BZ (Ref. TASK 25-23-42-400-801). (3) Install the rest room container, if removed (Ref. TASK 25-74-41-400-801). (4) Install the lavatories, if removed (Ref. TASK 25-41-41-400-801), (Ref. TASK 25-41-44-400-801) or (Ref. TASK 25-41-44-400-802), (Ref. TASK 25-41-45-400-801) or (Ref. TASK 25-41-45-400-802). (5) Install the galleys, if removed (Ref. TASK 25-31-41-400-801), (Ref. TASK 25-31-43-400-801) or (Ref. TASK 25-31-43-000-802), (Ref. TASK 25-31-51-400-801) or (Ref. TASK 25-31-52-400-801).
R
(6) Close the FWD passenger/crew door 831, 841 (Ref. TASK 52-10-00-410801). Subtask 05-22-20-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-22-20 SROS
Page 607 Jul 01/06
ZONAL INSPECTION: FORWARD CABIN AFT - INSPECTION/CHECK ______________________________________________________ TASK 05-22-30-200-803 R
Zonal Inspection of FWD Cabin 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-231-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R R
25-21-41-000-801 25-21-41-400-801 25-23-43-000-802 25-23-43-400-802 25-32-41-000-801 25-32-41-400-801 25-32-42-000-801 25-32-42-000-802 25-32-42-400-801 25-32-42-400-802 25-32-43-000-801 25-32-43-000-802 25-32-43-400-801 25-32-43-400-802 25-32-44-000-801 25-32-44-400-801 25-32-46-000-801 25-32-46-400-801 25-32-47-000-801 25-32-47-400-801 25-32-48-000-801
Removal of the Passenger Seats Installation of the Passenger Seats Removal of the Sidewall Panel(s) Installation of the Sidewall Panel(s) Removal of the MID Galley Unit (7000ML) Installation of the MID Galley Unit (7000ML) Removal of the MID Galley Unit (7001ML) Removal of the MID Galley Unit (7001ML-01) Installation of the MID Galley Unit (7001ML) Installation of the MID Galley Unit (7001ML-01) Removal of the MID Galley Unit (7002ML) Removal of the MID Galley Unit (7002ML-01) Installation of the MID Galley Unit (7002ML) Installation of the MID Galley Unit (7002ML-01) Removal of the MID Galley Unit 7003ML Installation of the MID Galley Unit 7003ML Removal of the MID Galley Unit 7006ML Installation of the MID Galley Unit 7006ML Removal of the MID Galley Unit (7009ML) Installation of the MID Galley Unit (7009ML) Removal of the MID Galley Unit (7011ML)
EFF : ALL 05-22-30 SROS
Page 601 Jan 01/04
------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R R
25-32-48-400-801 25-32-52-000-801 25-32-52-400-801 25-32-61-000-801 25-32-61-400-801 25-32-62-000-801 25-32-62-400-801 25-32-69-000-801 25-32-69-400-801 25-32-73-000-801 25-32-73-400-801 25-42-41-000-801 25-42-41-000-802 25-42-41-400-801 25-42-41-400-802 25-42-42-000-801 25-42-42-400-801 25-46-41-000-801 25-46-41-400-801 25-46-42-000-801 25-46-42-400-801 52-10-00-010-801 52-10-00-410-801 53-00-00-000-801 53-00-00-400-801
Installation of the MID Galley Unit (7011ML) Removal of the MID Galley Unit (7010ML) Installation of the MID Galley Unit (7010ML) Removal of the MID Galley (6505ML) Installation of the MID Galley (6505ML) Removal of the MID Galley Unit (6506ML) Installation of the MID Galley Unit (6506ML) Removal of the MID Galley Unit (6507ML) Installation of the MID Galley Unit (6507ML) Removal of the MID Galley Unit (6511ML) Installation of the MID Galley Unit (6511ML) Removal of the Lavatory H SPARE TASK FOR LATER USE Installation of the Lavatory H SPARE TASK FOR LATER USE Removal of the Lavatory K Installation of the Lavatory K Removal of the Lavatory Block O/P Installation of the Lavatory Block O/P Removal of the Lavatory Block U/V Installation of the Lavatory Block U/V Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door Removal of the Floor Panels in the Cabin from FR17 to FR80 Installation of the Floor Panels in the Cabin from FR17 to FR80
3. __________ Job Set-up Subtask 05-22-30-010-052 A. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the FWD passenger/crew door. (2) Open the FWD passenger/crew door 831, 841 (Ref. TASK 52-10-00-010801). (3) Remove the seats and the furnishings (Ref. TASK 25-21-41-000-801).
EFF : ALL 05-22-30 SROS
Page 602 Jul 01/06
R
(4) Remove the (Ref. TASK (Ref. TASK (Ref. TASK (Ref. TASK (Ref. TASK (Ref. TASK (Ref. TASK (Ref. TASK
galleys, if installed 25-32-41-000-801), 25-32-42-000-801), (Ref. 25-32-43-000-801), (Ref. 25-32-44-000-801), (Ref. 25-32-47-000-801), (Ref. 25-32-52-000-801), (Ref. 25-32-62-000-801), (Ref. 25-32-73-000-801).
R
(5) Remove the (Ref. TASK (Ref. TASK (Ref. TASK
lavatories, if installed 25-42-41-000-801), (Ref. TASK 25-42-41-000-802), 25-42-42-000-801), (Ref. TASK 25-46-41-000-801), 25-46-42-000-801).
R R R
(6) Remove the sidewall panels and the floor panels from FR17 to FR31 (Ref. TASK 25-23-43-000-802) (Ref. TASK 53-00-00-000-801).
R R
TASK TASK TASK TASK TASK TASK
25-32-42-000-802), 25-32-43-000-802), 25-32-46-000-801), 25-32-48-000-801), 25-32-61-000-801), 25-32-69-000-801),
(7) Lift the insulation sufficiently to do the inspection. 4. Procedure _________ Subtask 05-22-30-210-052 A. Do a general visual inspection of the forward cabin (zones 231 and 232). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-22-30-410-052 A. Close Access (1) Put the insulation back in position. (2) Install all the floor panels and the sidewall panels from FR17 to FR31 (Ref. TASK 53-00-00-400-801) (Ref. TASK 25-23-43-400-802).
R R
(3) Install the lavatories, if removed (Ref. TASK 25-42-41-400-801), (Ref. TASK 25-42-41-400-802), (Ref. TASK 25-42-42-400-801), (Ref. TASK 25-46-41-400-801), (Ref. TASK 25-46-42-400-801).
EFF : ALL 05-22-30 SROS
Page 603 Jul 01/06
R
(4) Install the galleys, if removed (Ref. TASK 25-32-41-400-801), (Ref. TASK 25-32-42-400-801), (Ref. (Ref. TASK 25-32-43-400-801), (Ref. (Ref. TASK 25-32-44-400-801), (Ref. (Ref. TASK 25-32-47-400-801), (Ref. (Ref. TASK 25-32-52-400-801), (Ref. (Ref. TASK 25-32-62-400-801), (Ref. (Ref. TASK 25-32-73-400-801).
R R
TASK TASK TASK TASK TASK TASK
25-32-42-400-802), 25-32-43-400-802), 25-32-46-400-801), 25-32-48-400-801), 25-32-61-400-801), 25-32-69-400-801),
(5) Install the seats and furnishings (Ref. TASK 25-21-41-400-801). (6) Close the FWD passenger/crew door 831, 841 (Ref. TASK 52-10-00-410801). Subtask 05-22-30-860-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-22-30 SROS
Page 604 Jul 01/06
TASK 05-22-30-200-805 Zonal Inspection of FWD Cabin Overhead Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-233-01 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 ------------------------------------------------------------------------------25-23-41-000-801 25-23-41-400-801 25-24-51-000-801 25-24-51-400-801 25-24-61-000-801 25-24-61-400-801 52-10-00-010-801 52-10-00-410-801
Removal of the Ceiling Panels Installation of the Ceiling Panels Removal of the Lateral (Sidewall) Overhead Stowage-Compartment Installation of the Lateral (Sidewall) Overhead Stowage-Compartment Removal of the Center Overhead Stowage-Compartments Installation of the Center Overhead Stowage-Compartments Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door
3. __________ Job Set-up Subtask 05-22-30-010-054 A. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the passenger/crew door. (2) Open the FWD passenger/crew door 831, 841 (Ref. TASK 52-10-00-010801).
EFF : ALL 05-22-30 R SROS
Page 605 Jul 01/06
(3) Remove the galleys, if installed. (4) Remove the lavatories, if installed. (5) Remove the overhead stowage bins from FR17 to FR31 (Ref. TASK 25-24-51-000-801) and (Ref. TASK 25-24-61-000-801). (6) Remove the ceiling panels from FR17 to FR31 (Ref. TASK 25-23-41-000801). R R
(7) Lift the insulation sufficiently to do the inspection without removal of the wiring and ducting. 4. Procedure _________ Subtask 05-22-30-210-054 A. Do a general visual inspection of the forward cabin overhead-compartment (zones 233 and 234). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-22-30-410-054 A. Close Access (1) Put the insulation back in position. (2) Install all the ceiling panels from FR17 to FR31 (Ref. TASK 25-23-41400-801). (3) Install the overhead stowage bins from FR17 to FR31 (Ref. TASK 25-24-51-400-801) and (Ref. TASK 25-24-61-400-801). (4) Install the lavatories, if removed. (5) Install the galleys, if removed. (6) Close the FWD passenger/crew door 831, 841 (Ref. TASK 52-10-00-410801).
EFF : ALL 05-22-30 SROS
Page 606 Jul 01/06
Subtask 05-22-30-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-22-30 R SROS
Page 607 Jul 01/06
ZONAL INSPECTION : MID CABIN UTILITY AREA AFT - INSPECTION/CHECK ________________________________________________________________ TASK 05-22-40-200-802 Zonal Inspection of Mid Cabin Utility Area 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-241-02 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 ------------------------------------------------------------------------------25-22-41-000-801 25-22-41-400-801 25-22-44-000-801 25-22-44-400-801 R
25-23-46-000-801
R
25-23-46-400-801 25-26-41-000-801 25-26-41-400-801 25-26-42-000-801 25-26-42-400-801 25-27-41-000-801 25-27-41-400-801 52-10-00-010-801 52-10-00-410-801 53-00-00-000-801
Removal of the Wall-Mounted Cabin-Attendant Seat Installation of the Wall-Mounted Cabin-Attendant Seat Removal of the Free-Standing Cabin-Attendant Seat, Seat Rail Mounted Installation of the Free-Standing Cabin-Attendant Seat, Seat Rail Mounted Removal of the Door Frame Linings of the Middle Passenger/Crew Door Installation of the Door Frame Linings of the Middle Passenger/Crew Door Removal of the Curtains and the Curtain Rails Installation of the Curtains and the Curtain Rails Removal of the Partitions Installation of the Partitions Removal of the Stowages Installation of the Stowages Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door Removal of the Floor Panels in the Cabin from FR17 to FR80
EFF : ALL 05-22-40 SROS
Page 601 Jul 01/06
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------53-00-00-400-801
Installation of the Floor Panels in the Cabin from FR17 to FR80
3. __________ Job Set-up Subtask 05-22-40-010-051 A. Get Access R R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the MID passenger/crew door. (2) Open the Mid passenger/crew door (Ref. TASK 52-10-00-010-801). (3) Remove the (Ref. TASK (Ref. TASK (Ref. TASK
seats and the furnishings, if installed: 25-27-41-000-801), 25-22-41-000-801), (Ref. TASK 25-22-44-000-801), 25-26-41-000-801), (Ref. TASK 25-26-42-000-801).
(4) Remove the galleys, if installed. (5) Remove the lavatories, if installed. R R
(6) Remove the door frame linings and the floor panels from FR31 to FR36 (Ref. TASK 25-23-46-000-801), (Ref. TASK 53-00-00-000-801). (7) Lift the insulation sufficiently to do the inspection. 4. Procedure _________ Subtask 05-22-40-210-051 A. Do a general visual inspection of the MID cabin utility-area (zones 241 and 242). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping, wiring) are attached correctly.
EFF : ALL 05-22-40 SROS
Page 602 Jul 01/06
5. Close-up ________ Subtask 05-22-40-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. R
(2) Put the insulation back in position.
R
(3) Install the floor panels and the door frame linings from FR31 to FR36 (Ref. TASK 53-00-00-400-801), (Ref. TASK 25-23-46-400-801).
R
(4) Install the lavatories, if removed.
R
(5) Install the galleys, if removed.
R
(6) Install the seats and the furnishings, if removed: (Ref. TASK 25-27-41-400-801), (Ref. TASK 25-22-41-400-801), (Ref. TASK 25-22-44-400-801), (Ref. TASK 25-26-41-400-801), (Ref. TASK 25-26-42-400-801).
R
(7) Make sure that the work area is clean and clear of tools and other items.
R
(8) Close the MID passenger/crew door (Ref. TASK 52-10-00-410-801). Subtask 05-22-40-860-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-22-40 SROS
Page 603 Jul 01/06
TASK 05-22-40-200-804 Zonal Inspection of Mid Cabin Utility Area Overhead Compt 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-243-01 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 ------------------------------------------------------------------------------25-23-41-000-801 25-23-41-400-801 52-10-00-010-801 52-10-00-410-801
Removal of the Ceiling Panels Installation of the Ceiling Panels Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door
3. __________ Job Set-up Subtask 05-22-40-010-053 A. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the MID passenger/crew door. (2) Open the MID passenger/crew door (Ref. TASK 52-10-00-010-801). (3) Remove the galleys, if installed. (4) Remove the lavatories, if installed. (5) Remove the ceiling panels from FR31 to FR36 (Ref. TASK 25-23-41-000801).
EFF : ALL 05-22-40 R SROS
Page 604 Jul 01/06
(6) Lift the insulation sufficiently to do the inspection. 4. Procedure _________ Subtask 05-22-40-210-053 A. Do a general visual inspection of the MID cabin overhead-compartment (zones 243 and 244). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-22-40-410-053 A. Close Access R R
(1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Put the insulation back in position.
R
(3) Install the ceiling panels from FR31 to FR36 (Ref. TASK 25-23-41-400801).
R
(4) Install the lavatories, if removed.
R
(5) Install the galleys, if removed.
R
(6) Close the MID passenger/crew door (Ref. TASK 52-10-00-410-801). Subtask 05-22-40-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-22-40 SROS
Page 605 Jan 01/07
__________________________________________________________________________ ZONAL INSPECTION : MID CABIN AFT OF MID CABIN UTILITY AREA TO FRONT OF AFT CABIN - INSPECTION/CHECK ________________________ TASK 05-22-50-200-802 R
Zonal Inspection of MID Cabin 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-251-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
25-21-41-000-801 25-21-41-400-801 25-23-43-000-802 25-23-43-400-802
Removal of the Passenger Seats Installation of the Passenger Seats Removal of the Sidewall Panel(s) Installation of the Sidewall Panel(s)
52-10-00-010-801 52-10-00-410-801 53-00-00-000-801
Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door Removal of the Floor Panels in the Cabin from FR17 to FR80 Installation of the Floor Panels in the Cabin from FR17 to FR80
R
53-00-00-400-801
EFF : ALL 05-22-50 SROS
Page 601 Jan 01/04
3. __________ Job Set-up Subtask 05-22-50-010-051 A. Get Access R R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the MID passenger/crew door (2) Open the MID passenger/crew door (Ref. TASK 52-10-00-010-801). (3) Remove the galleys, if installed.
R (4) Remove the lavatories, if installed. R R R
(5) Remove the seats (Ref. TASK 25-21-41-000-801).
R R
(6) Remove the sidewall panels and the floor panels from FR36 to FR53.5 (Ref. TASK 25-23-43-000-802), (Ref. TASK 53-00-00-000-801). NOTE : Lift the insulation to do the inspection. ____ 4. Procedure _________ Subtask 05-22-50-210-051
R
A. Do a general visual inspection of the MID cabin (zones 251 and 252). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-22-50-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the floor panels and the sidewall panels from FR36 to FR53.5 (Ref. TASK 53-00-00-400-801), (Ref. TASK 25-23-43-400-802).
EFF : ALL 05-22-50 SROS
Page 602 Jan 01/04
R R
(3) Install the seat (Ref. TASK 25-21-41-400-801). (4) Install the lavatories, if removed.
R R R
(5) Install the galleys, if removed.
R R
(6) Close the MID passenger/crew door (Ref. TASK 52-10-00-410-801).
R R
Subtask 05-22-50-860-050 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-22-50 SROS
Page 603 Jan 01/04
TASK 05-22-50-200-804 R
Zonal Inspection of MID Cabin Overhead Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-253-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R
No specific No specific
1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 STEPLADDER 1.0 M (3.3 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------25-23-41-000-801 25-23-41-400-801 25-24-51-000-801 25-24-51-400-801 25-24-61-000-801 25-24-61-400-801
Removal of the Ceiling Panels Installation of the Ceiling Panels Removal of the Lateral (Sidewall) Overhead Stowage-Compartment Installation of the Lateral (Sidewall) Overhead Stowage-Compartment Removal of the Center Overhead Stowage-Compartments Installation of the Center Overhead Stowage-Compartments
R 52-10-00-010-801 52-10-00-410-801
Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door
EFF : ALL 05-22-50 SROS
Page 604 Jan 01/04
3. __________ Job Set-up Subtask 05-22-50-010-053 A. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the MID passenger/crew door and a STEPLADDER 1.0 M (3.3 FT) in the position (2) Open the MID passenger/crew door (Ref. TASK 52-10-00-010-801). (3) Remove the galleys, if installed. (4) Remove the lavatories, if installed. (5) Remove the overhead stowage compartments (Ref. TASK 25-24-51-000-801), (Ref. TASK 25-24-61-000-801). (6) Remove the ceiling panels from FR36 to FR53.5 (Ref. TASK 25-23-41000-801). R R
(7) Lift the insulation sufficiently to do the inspection without removal of the wiring and ducting. 4. Procedure _________ Subtask 05-22-50-210-053 A. Do a general visual inspection of the MID cabin overhead-compartment (zones 253 and 254). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, wiring) are attached correctly. 5. Close-up ________ Subtask 05-22-50-410-053 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Put the insulation back in position.
EFF : ALL 05-22-50 SROS
Page 605 Jul 01/06
R
(3) Install the ceiling panels from FR36 to FR53.5 (Ref. TASK 25-23-41400-801).
R
(4) Install the overhead stowage compartment (Ref. TASK 25-24-51-400-801), (Ref. TASK 25-24-61-400-801).
R
(5) Install the lavatories, if removed.
R
(6) Install the galleys, if removed.
R
(7) Close the MID passenger/crew door (Ref. TASK 52-10-00-410-801). Subtask 05-22-50-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-22-50 SROS
Page 606 Jul 01/06
___________________________________________________________________________ ZONAL INSPECTION : AFT CABIN AFT OF MID CABIN TO FRONT OF AFT CABIN UTILITY AREA - INSPECTION/CHECK _______________________ TASK 05-22-60-200-802 Zonal Inspection of Aft Cabin 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-261-02 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 ------------------------------------------------------------------------------25-21-41-000-801 25-21-41-400-801 25-23-43-000-802 25-23-43-400-802 25-23-48-000-801 R R
25-23-48-400-801 52-10-00-010-801 52-10-00-410-801 53-00-00-000-801 53-00-00-400-801
Removal of the Passenger Seats Installation of the Passenger Seats Removal of the Sidewall Panel(s) Installation of the Sidewall Panel(s) Removal of the Door Frame Linings of the Emergency Exit Installation of the Door Frame Linings of the Emergency Exit Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door Removal of the Floor Panels in the Cabin from FR17 to FR80 Installation of the Floor Panels in the Cabin from FR17 to FR80
EFF : ALL 05-22-60 SROS
Page 601 Apr 01/04
3. __________ Job Set-up Subtask 05-22-60-010-051 A. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the aft passenger/crew door. R
(2) Open the aft passenger/crew door 833, 843 (Ref. TASK 52-10-00-010801). (3) Remove the seats (Ref. TASK 25-21-41-000-801). (4) Remove the lavatories, if installed. (5) Remove the door frame linings (Ref. TASK 25-23-48-000-801). (6) Remove the sidewall panels and the floor panels from FR53.5 to FR72 (Ref. TASK 53-00-00-000-801), (Ref. TASK 25-23-43-000-802).
R
NOTE : Lift the insulation to do the inspection. ____ 4. Procedure _________ Subtask 05-22-60-210-051 A. Do a general visual inspection of the aft cabin (zones 261 and 262). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-22-60-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the floor panels and the sidewall panels from FR53.5 to FR72 (Ref. TASK 53-00-00-400-801), (Ref. TASK 25-23-43-400-802). (3) Install the door frame linings (Ref. TASK 25-23-48-400-801).
EFF : ALL 05-22-60 SROS
Page 602 Jul 01/06
R
(4) Install the lavatories, if removed.
R
(5) Install the seats (Ref. TASK 25-21-41-400-801).
R
(6) Close the aft passenger/crew door 833, 843, (Ref. TASK 52-10-00-410801). Subtask 05-22-60-860-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-22-60 SROS
Page 603 Apr 01/04
TASK 05-22-60-200-804 Zonal Inspection of Aft Cabin Overhead Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-263-01 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 ------------------------------------------------------------------------------25-23-41-000-801 25-23-41-400-801 25-24-51-000-801 25-24-51-400-801 25-24-61-000-801 25-24-61-400-801 52-10-00-010-801 52-10-00-410-801
Removal of the Ceiling Panels Installation of the Ceiling Panels Removal of the Lateral (Sidewall) Overhead Stowage-Compartment Installation of the Lateral (Sidewall) Overhead Stowage-Compartment Removal of the Center Overhead Stowage-Compartments Installation of the Center Overhead Stowage-Compartments Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door
3. __________ Job Set-up Subtask 05-22-60-010-053 A. Get Access R R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the aft passenger/crew door. (2) Open the aft passenger/crew door 833 (843) (Ref. TASK 52-10-00-010801).
EFF : ALL 05-22-60 SROS
Page 604 Jul 01/06
(3) Remove the lavatories, if installed. (4) Remove the overhead stowage compartments (Ref. TASK 25-24-51-000-801), (Ref. TASK 25-24-61-000-801). (5) Remove the ceiling panels from FR53.5 to FR72 (Ref. TASK 25-23-41000-801). R R
(6) Lift the insulation sufficiently to do the inspection without removal of the wiring and ducting. 4. Procedure _________ Subtask 05-22-60-210-053 A. Do a general visual inspection of the aft cabin overhead compartment (zones 263 and 264). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-22-60-410-053 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Put the insulation back in position.
R
(3) Install the ceiling panels from FR53.5 to FR72 (Ref. TASK 25-23-41400-801).
R
(4) Install the lavatories, if removed.
R
(5) Install the overhead stowage compartment (Ref. TASK 25-24-51-400-801), (Ref. TASK 25-24-61-400-801).
R
(6) Close the aft passenger/crew door 833 (843) (Ref. TASK 52-10-00-410801).
EFF : ALL 05-22-60 SROS
Page 605 Jul 01/06
Subtask 05-22-60-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-22-60 SROS
Page 606 Jul 01/06
ZONAL INSPECTION : AFT CABIN UTILITY AREA - INSPECTION/CHECK ____________________________________________________________ TASK 05-22-70-200-802 Zonal Inspection of Aft Cabin Utility Area 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-271-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R R
No specific No specific
R
non-metallic scraper with a width of approximately 9 mm (0.35 in.) 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
B. Consumable Materials
R R R
------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R
Material No. 15-010
R
USA MIL-C-11796-C CLASS 1A CORROSION PREVENTIVE FILLER COMPOUND (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------25-22-41-000-801 25-22-41-400-801 25-22-44-000-801 25-22-44-400-801 25-23-47-000-801 25-23-47-400-801
Removal of the Wall-Mounted Cabin-Attendant Seat Installation of the Wall-Mounted Cabin-Attendant Seat Removal of the Free-Standing Cabin-Attendant Seat, Seat Rail Mounted Installation of the Free-Standing Cabin-Attendant Seat, Seat Rail Mounted Removal of the Door Frame Linings of the AFT Passenger/Crew Door Installation of the Door Frame Linings of the AFT Passenger/Crew Door
EFF : ALL 05-22-70 SROS
Page 601 Jan 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------25-27-15-000-801 25-27-15-400-801 25-27-41-000-801 25-27-41-400-801 25-27-42-000-801 25-27-42-400-801 52-10-00-010-801 52-10-00-410-801 53-00-00-000-801 53-00-00-400-801
Removal of the Emergency Equipment Stowage Installation of the Emergency Equipment Stowage Removal of the Stowages Installation of the Stowages Removal of the Doghouses Installation of the Doghouses Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door Removal of the Floor Panels in the Cabin from FR17 to FR80 Installation of the Floor Panels in the Cabin from FR17 to FR80
3. __________ Job Set-up Subtask 05-22-70-010-051 A. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the aft passenger/crew door (2) Open the aft passenger/crew door 833 (843) (Ref. TASK 52-10-00-010801). (3) Remove the galleys, if installed. (4) Remove the lavatories, if installed. (5) Remove the cabin attendant seats, if installed (Ref. TASK 25-22-41-000-801), (Ref. TASK 25-22-44-000-801). (6) Remove the stowages, if installed (Ref. TASK 25-27-15-000-801), (Ref. TASK 25-27-41-000-801), (Ref. TASK 25-27-42-000-801). (7) Remove the door frame linings (Ref. TASK 25-23-47-000-801). (8) Remove the floor panels from FR72 to FR80 (Ref. TASK 53-00-00-000801). NOTE : Lift the insulation sufficiently to do the inspection. ____
EFF : ALL 05-22-70 R SROS
Page 602 Jan 01/05
R R R
(9) Remove the corrosion preventive filling compound STORAGE PRESERVATION (Material No. 15-010) in the seat track with a non-metallic scraper with a width of approximately 9 mm (0.35 in.) 4. Procedure _________ Subtask 05-22-70-210-051 A. Do a general visual inspection of the aft cabin utility-area (zones 271 and 272). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-22-70-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items.
R R
(2) Install the corrosion preventive filling compound STORAGE PRESERVATION (Material No. 15-010) in the seat track.
R
(3) Install the floor panels from FR72 to FR80 (Ref. TASK 53-00-00-400801).
R
(4) Install the door frame linings (Ref. TASK 25-23-47-400-801).
R
(5) Install the stowages, if removed (Ref. TASK 25-27-15-400-801), (Ref. TASK 25-27-41-400-801), (Ref. TASK 25-27-42-400-801).
R
(6) Install the cabin attendant seats, if removed (Ref. TASK 25-22-41-400-801), (Ref. TASK 25-22-44-400-801).
R
(7) Install the lavatories, if removed.
R
(8) Install the galleys, if removed.
R
(9) Close the aft passenger/crew door 833 (843) (Ref. TASK 52-10-00-410801). Subtask 05-22-70-860-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-22-70 SROS
Page 603 Jan 01/05
INTENTIONALLY BLANK
R 05-22-70 SROS
Page 604 Jan 01/05
TASK 05-22-70-200-804 Zonal Inspection of Aft Cabin Utility Area Overhead Compt 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-273-01 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 R R
25-23-41-000-801 25-23-41-400-801 25-23-47-000-801 25-23-47-400-801 25-80-00-000-801 25-80-00-400-801 52-10-00-010-801 52-10-00-410-801
Removal of the Ceiling Panels Installation of the Ceiling Panels Removal of the Door Frame Linings of the AFT Passenger/Crew Door Installation of the Door Frame Linings of the AFT Passenger/Crew Door Removal of the Insulation Blankets Installation of the Insulation Blankets Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door
3. __________ Job Set-up Subtask 05-22-70-010-053 A. Get Access R R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the aft passenger/crew door. (2) Open the aft passenger/crew door 833 (843) (Ref. TASK 52-10-00-010801).
EFF : ALL 05-22-70 SROS
Page 605 Apr 01/04
(3) Remove the galleys, if installed. (4) Remove the lavatories, if installed. R
(5) Remove the door frame linings (Ref. TASK 25-23-47-000-801).
R
(6) Remove the ceiling panels from FR72 to FR80 271AZ, 271BZ, 271CZ, 272AZ, 272BZ, 272CZ (Ref. TASK 25-23-41-000-801).
R
(7) Remove the insulation (Ref. TASK 25-80-00-000-801). 4. Procedure _________ Subtask 05-22-70-210-053 A. Do a general visual inspection of the aft cabin overhead-compartment (zones 273 and 274). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-22-70-410-053 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the insulation (Ref. TASK 25-80-00-400-801). (3) Install the ceiling panels from FR72 to FR80 271AZ, 271BZ, 271CZ, 272AZ, 272BZ, 272CZ (Ref. TASK 25-23-41-400-801).
R
(4) Install the door frame linings (Ref. TASK 25-23-47-400-801).
R
(5) Install the lavatories, if removed.
R
(6) Install the galleys, if removed.
R
(7) Close the aft passenger/crew door 833 (843) (Ref. TASK 52-10-00-410801).
EFF : ALL 05-22-70 SROS
Page 606 Apr 01/04
R R
Subtask 05-22-70-860-051 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-22-70 SROS
Page 607 Jan 01/04
ZONAL INSPECTION : STABILIZERS AND FUSELAGE REAR SECTION - INSPECTION/CHECK ___________________________________________________________________________ TASK 05-23-00-200-801 Zonal Inspection of the Stabilizers and the Fuselage Tail (zone 300). 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information Not Applicable 3. __________ Job Set-up Subtask 05-23-00-869-050 A. Not applicable. 4. Procedure _________ Subtask 05-23-00-210-050 A. Visual inspection. (1) Do a general visual inspection of the stabilizers and the fuselage tail from the ground.
EFF : ALL 05-23-00 R SROS
Page 601 Jan 01/04
TASK 05-23-00-200-802 R
Zonal Inspection of Empennage and Rear Fuselage 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-300-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 15M (49 FT) - ADJUSTABLE
3. __________ Job Set-up Subtask 05-23-00-010-050 A. Get Access R R
(1) Put an ACCESS PLATFORM 15M (49 FT) - ADJUSTABLE in position at the stabilizers and the rear fuselage section (zone 300). 4. Procedure _________ Subtask 05-23-00-210-051 A. Do a general visual inspection of the stabilizers and the rear fuselage (zone 300). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see.
EFF : ALL 05-23-00 SROS
Page 602 Jan 01/04
5. Close-up ________ Subtask 05-23-00-410-050 R
A. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-23-00 SROS
Page 603 Jan 01/04
_____________________________________________________________________ ZONAL INSPECTION : FUSELAGE REAR SECTION AFT OF AFT PRESSURE BULKHEAD ________________ INSPECTION/CHECK TASK 05-23-10-200-801 Zonal Inspection of Rear Fuselage Section 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: ZL-311-01 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
28-27-48-000-801 28-27-48-400-801 05-23-10-991-001-A 05-23-10-991-002-A
Removal of the Trim Tank Transfer Pump (709QN) Installation of the Trim Tank Transfer Pump (709QN) Fig. 601 Fig. 602
EFF : ALL 05-23-10 SROS
Page 601 Jan 01/07
3. __________ Job Set-up Subtask 05-23-10-010-050 A. Get Access (Ref. Fig. 601/TASK 05-23-10-991-001-A, 602/TASK 05-23-10-991-002-A) (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the rear fuselage section (zone 311 and 312). R
(2) Open the access doors 312AR, 313AL and lock them in position.
R R
(3) Remove the pump sealing case, if installed (Ref. TASK 28-27-48-000801). 4. Procedure _________ Subtask 05-23-10-210-050 A. Do a general visual inspection of the rear fuselage section (Zones 311, 312 and 313). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, wiring) are attached correctly. 5. Close-up ________ Subtask 05-23-10-410-050 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items.
R R
(2) Install the pump sealing case, if removed (Ref. TASK 28-27-48-400801).
R
(3) Close the access doors 312AR, 313AL. Subtask 05-23-10-860-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-10 SROS
Page 602 Jan 01/07
Access Panel on the Fuselage Aft Tail-Section (Zones 311 and 312) Figure 601/TASK 05-23-10-991-001-A EFF : ALL 05-23-10 R SROS
Page 603 Jan 01/07
Access Panels on the Fuselage Tail-Cone APU-Compartment (Zones 313, 314, 315, 316 and 317). Figure 602/TASK 05-23-10-991-002-A EFF : ALL Page 604 Jan 01/07 R SROS
05-23-10
TASK 05-23-10-200-802 Zonal Inspection of Tail Cone APU Air Intake Area 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-313-01 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
05-23-10-991-002-A
Fig. 602
3. __________ Job Set-up Subtask 05-23-10-010-051 R
A. Get Access (Ref. Fig. 602/TASK 05-23-10-991-002-A) (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the tail cone, APU air-intake area (zone 313 and 314). (2) Open and secure the access door 313AL.
EFF : ALL 05-23-10 SROS
Page 605 Oct 01/04
4. Procedure _________ Subtask 05-23-10-210-051 A. Do a general visual inspection of the tail cone, APU air-intake area (zones 313 and 314). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-23-10-410-051 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. Subtask 05-23-10-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-10 R SROS
Page 606 Oct 01/04
TASK 05-23-10-200-803 Zonal Inspection of Tail Cone APU and Accessory Compt 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-315-01 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
05-23-10-991-002-A
Fig. 602
3. __________ Job Set-up Subtask 05-23-10-010-052 R
A. Get Access (Ref. Fig. 602/TASK 05-23-10-991-002-A) (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the tail cone, APU and accessory compartment(zones 315 and 316). (2) Open and secure the APU access doors 315AL, 316AR.
EFF : ALL 05-23-10 SROS
Page 607 Oct 01/04
4. Procedure _________ Subtask 05-23-10-210-052 A. Do a general visual inspection of the tail cone, APU accessory compartment (zones 315 and 316). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping) are attached correctly. 5. Close-up ________ Subtask 05-23-10-410-052 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the APU access doors 315AL, 316AR. Subtask 05-23-10-860-052 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-10 R SROS
Page 608 Oct 01/04
TASK 05-23-10-200-804 Zonal Inspection of Tail Cone APU Exhaust Area 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: ZL-317-01 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
05-23-10-991-002-A
Fig. 602
3. __________ Job Set-up Subtask 05-23-10-010-053 R
A. Get Access (Ref. Fig. 602/TASK 05-23-10-991-002-A) (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the tail cone, APU exhaust-area (zone 317). (2) Open and secure the APU-Exhaust access fairing 317AL.
EFF : ALL 05-23-10 SROS
Page 609 Oct 01/04
4. Procedure _________ Subtask 05-23-10-210-053 A. Do a general visual inspection of the tail cone, APU exhaust area (zone 317). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (piping) are attached correctly. 5. Close-up ________ Subtask 05-23-10-410-053 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the APU-Exhaust access fairing 317AL. Subtask 05-23-10-860-053 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. R
EFF : ALL 05-23-10 SROS
Page 610 Jul 01/05
TASK 05-23-10-200-806 Zonal Inspection of Horizontal Stabilizer Center Box (Internal) 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: ZL-319-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R R
No specific No specific
adjustable access platform 8.30 m (27 ft. 3 in.) 1 WARNING NOTICE
B. Referenced Information
R R R
------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R R R R
55-11-14-000-801 55-11-14-400-801 05-23-10-991-001-A 05-23-10-991-002-A
Removal of the THS Front-Spar Center-Box Access-Panels 319AL, 319BL, 319AR, 319BR/319DR, 319ER Installation of the THS Front-Spar Center-Box Access-Panels 319AL, 319BL, 319AR, 319BR/319DR, 319ER Fig. 601 Fig. 602
EFF : ALL 05-23-10 SROS
Page 611 Jul 01/05
3. __________ Job Set-up Subtask 05-23-10-941-051 A. Safety Precautions (1) Put a WARNING NOTICE in position - to tell persons not to operate the flight controls. - to tell persons not to operate the fuel system. R R R
Subtask 05-23-10-010-055-C B. Get Access (Ref. Fig. 601/TASK 05-23-10-991-001-A, 602/TASK 05-23-10-991-002-A)
R R
(1) Put an adjustable access platform in position at the horizontal-stabilizer center box (zone 319).
R
(2) Open and secure the access doors 312AR, 313AL.
R
(3) Remove the access panels 319DR, 319ER (Ref. TASK 55-11-14-000-801).
R
(4) Disconnect the pipe of the scavenge water system. 4. Procedure _________ Subtask 05-23-10-210-055 A. Do a general visual inspection of the horizontal-stabilizer center box (Internal) (zone 319). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (piping) are attached correctly. 5. Close-up ________
R R
Subtask 05-23-10-410-055-C A. Close Access
R
(1) Connect the pipe of the scavenge water system.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
R
(3) Install the access panels 319DR, 319ER (Ref. TASK 55-11-14-400-801).
EFF : ALL 05-23-10 SROS
Page 612 Jul 01/05
R
(4) Close the access doors 312AR, 313AL. Subtask 05-23-10-942-051
R
B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-10 SROS
Page 613 Jul 01/05
ZONAL INSPECTION : VERTICAL STABILIZER AND RUDDER - INSPECTION/CHECK ____________________________________________________________________ TASK 05-23-20-200-801 R
Zonal Inspection of Dorsal Fin 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 Refer to the MPD TASK: ZL-321-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R
No specific No specific
1 ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------53-45-11-000-801 53-45-11-400-801
Removal of the Dorsal Fin (321AL) Installation of the Dorsal Fin (321AL)
EFF : ALL 05-23-20 SROS
Page 601 Jan 01/04
3. __________ Job Set-up Subtask 05-23-20-941-050 A. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-23-20-010-050 B. Get Access (1) Put an ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE in position at the dorsal fin (zone 321). (2) Remove the access panel 321AL (Ref. TASK 53-45-11-000-801). 4. Procedure _________ Subtask 05-23-20-210-050 R
A. Inspection
R
(1) Do a general visual inspection of the dorsal fin (zone 321).
R
(2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and structure you can see. - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-23-20-410-050 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the dorsal fin 321AL (Ref. TASK 53-45-11-400-801).
EFF : ALL 05-23-20 SROS
Page 602 Jul 01/04
Subtask 05-23-20-942-050 B. Put the Aircraft back to its Initial Configuration R R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-20 SROS
Page 603 Jan 01/04
TASK 05-23-20-200-802 R
Zonal Inspection of Vertical Stabilizer Leading Edge 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 Refer to the MPD TASK: ZL-322-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R
No specific No specific
1 ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------55-32-11-000-801 55-32-11-400-801
Removal of the Vertical Stabilizer Leading-Edge Installation of the Vertical Stabilizer Leading-Edge
EFF : ALL 05-23-20 SROS
Page 604 Jan 01/04
3. __________ Job Set-up Subtask 05-23-20-941-051 A. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. R R
Subtask 05-23-20-010-051-A B. Get Access
R R
(1) Put an ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE in position at the vertical-stabilizer leading edge (zone 322).
R R
(2) Remove the access panels 322AL, 322BL, 322CL, 322DL (Ref. TASK 55-3211-000-801). 4. Procedure _________ Subtask 05-23-20-210-051
R
A. Do a general visual inspection of the vertical-stabilizer leading edge (zone 322). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (wiring) are attached correctly. 5. Close-up ________
R R
Subtask 05-23-20-410-051-A 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 access panels 322AL, 322BL, 322CL, 322DL (Ref. TASK 5532-11-400-801). Subtask 05-23-20-942-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-20 SROS
Page 605 Jul 01/06
TASK 05-23-20-200-803 Zonal Inspection of Vertical Stabilizer Spar Box 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 Refer to the MPD TASK: ZL-323-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
1 ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------05-23-20-991-002
Fig. 601
3. __________ Job Set-up Subtask 05-23-20-941-052 A. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls.
EFF : ALL 05-23-20 R SROS
Page 606 Jul 01/06
Subtask 05-23-20-010-052 B. Get Access (Ref. Fig. 601/TASK 05-23-20-991-002) (1) Put an ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE in position at the vertical-stabilizer spar box (zone 323). R
(2) Open and safety the access door 312AR. (3) Remove the access panels 311AZ, 311BZ. 4. Procedure _________ Subtask 05-23-20-210-052 A. Do a general visual inspection of the vertical-stabilizer spar box (zone 323). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (piping) are attached correctly. 5. Close-up ________ Subtask 05-23-20-410-052 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels 311AZ, 311BZ. (3) Close the access door 312AR. Subtask 05-23-20-942-052 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-20 SROS
Page 607 Jul 01/06
Access Panels on the Fuselage Aft Tail-Section Figure 601/TASK 05-23-20-991-002 EFF : ALL 05-23-20 R SROS
Page 608 Jul 01/06
TASK 05-23-20-200-804 Zonal Inspection of Vertical Stabilizer Spar Box 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 Refer to the MPD TASK: ZL-323-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific No specific
adjustable access platform 16.80 m (55 ft. 1 in.) 1 WARNING NOTICE
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 05-052 SELF-ADHES.PVC DISKS FOR HOISTING POINT BLANKING (Ref. 20-31-00)
EFF : ALL 05-23-20 SROS
Page 609 Jul 01/06
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------53-55-11-000-801 53-55-11-400-801 55-32-11-000-801 55-32-11-400-801 55-33-13-000-801 55-33-13-400-801
Removal of the Vertical Stabilizer Fairings Installation of the Vertical Stabilizer Fairings Removal of the Vertical Stabilizer Leading-Edge Installation of the Vertical Stabilizer Leading-Edge Removal of the Vertical-Stabilizer Trailing-Edge Access-Panels Installation of the Vertical-Stabilizer Trailing-Edge Access-Panels
R 3. __________ Job Set-up Subtask 05-23-20-941-053 A. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. R R
Subtask 05-23-20-010-053-A B. Get Access
R R
(1) Put an adjustable access platform in position at the vertical-stabilizer spar box (zone 323).
R
(2) Open the access door 312AR
R
(3) Remove the access panels 311AZ, 311BZ.
R R R
(4) Remove the access panels 322AL, 322BL, 322CL, 322DL (Ref. TASK 55-3211-000-801), 323CL, 323DL, 325LL. (Ref. TASK 53-55-11-000-801)
R R
(5) Remove the access panels 325ML, 325NL, 325PL, 325QL, 325RL (Ref. TASK 55-33-13-000-801).
R R
(6) Remove the vertical stabilizer fairings 323CL, 323DL and 325LL (Ref. TASK 53-55-11-000-801).
R
(7) Remove and discard the self-adhesive discs from the hoisting points.
EFF : ALL 05-23-20 SROS
Page 610 Jul 01/06
4. Procedure _________ Subtask 05-23-20-210-053
R
A. Do a general visual inspection of the vertical-stabilizer spar box (zone 323). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (piping) are attached correctly. 5. Close-up ________
R R
Subtask 05-23-20-410-053-A A. Close Access
R R
(1) Put the SPECIAL MATERIALS (Material No. 05-052) on the hoisting points.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
R R
(3) Install the access panels 325ML, 325NL, 325PL, 325QL, 325RL. (Ref. TASK 55-33-13-400-801)
R R
(4) Install the fairings 323CL, 323DL, 325LL. (Ref. TASK 53-55-11-400801)
R R
(5) Install the access panels 322AL, 322BL, 322CL, 322DL. (Ref. TASK 5532-11-400-801)
R
(6) Install the access panels 311AZ, 311BZ.
R
(7) Close the access door 312AR.
R
(8) Remove the access platform(s). Subtask 05-23-20-942-053 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-20 SROS
Page 611 Jul 01/06
TASK 05-23-20-200-805 Zonal Inspection of Vertical Stabilizer Tip 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 Refer to the MPD TASK: ZL-324-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
1 ACCESS PLATFORM 15M (49 FT) - ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------55-34-11-000-801 55-34-11-400-801
Removal of the Vertical Stabilizer Tip Installation of the Vertical Stabilizer Tip
EFF : ALL 05-23-20 R SROS
Page 612 Jul 01/06
3. __________ Job Set-up Subtask 05-23-20-941-054 A. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. R R
Subtask 05-23-20-010-054-A B. Get Access
R R
(1) Put an ACCESS PLATFORM 15M (49 FT) - ADJUSTABLE in position at the vertical stabilizer tip (zone 324).
R
(2) Remove the access panel 324CT (Ref. TASK 55-34-11-000-801). 4. Procedure _________ Subtask 05-23-20-210-054 A. Do a general visual inspection of the vertical stabilizer tip (zone 324). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring) are attached correctly. 5. Close-up ________
R R
Subtask 05-23-20-410-054-A A. Close Access
R R
(1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Install the access panel 324CT (Ref. TASK 55-34-11-400-801). Subtask 05-23-20-942-054 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-20 SROS
Page 613 Jul 01/06
INTENTIONALLY BLANK
R 05-23-20 SROS
Page 614 Jul 01/06
TASK 05-23-20-200-806 R
Zonal Inspection of Vertical Stabilizer Trailing Edge 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 Refer to the MPD TASK: ZL-325-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R
No specific No specific
1 ACCESS PLATFORM 15M (49 FT) - ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------55-33-13-000-801 55-33-13-400-801
Removal of the Vertical-Stabilizer Trailing-Edge Access-Panels Installation of the Vertical-Stabilizer Trailing-Edge Access-Panels
EFF : ALL 05-23-20 SROS
Page 615 Jan 01/04
3. __________ Job Set-up Subtask 05-23-20-941-055 A. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. R R
Subtask 05-23-20-010-055-A B. Get Access
R R
(1) Put an ACCESS PLATFORM 15M (49 FT) - ADJUSTABLE in position at the vertical-stabilizer trailing edge (zone 325).
R
(2) Remove the access panel 325NL (Ref. TASK 55-33-13-000-801). 4. Procedure _________ Subtask 05-23-20-210-055 A. Do a general visual inspection of the vertical-stabilizer trailing edge (zone 325). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring) are attached correctly. 5. Close-up ________
R R
Subtask 05-23-20-410-055-A A. Close Access
R R
(1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Install the access panel 325NL (Ref. TASK 55-33-13-400-801). Subtask 05-23-20-942-055 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-20 SROS
Page 616 Jul 01/04
TASK 05-23-20-200-807 Zonal Inspection of Vertical Stabilizer Trailing Edge 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 Refer to the MPD TASK: ZL-325-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific No specific
adjustable access platform 16.80 m (55 ft. 1 in.) 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------55-33-13-000-801 55-33-13-400-801
Removal of the Vertical-Stabilizer Trailing-Edge Access-Panels Installation of the Vertical-Stabilizer Trailing-Edge Access-Panels
EFF : ALL 05-23-20 SROS
Page 617 Jul 01/04
3. __________ Job Set-up Subtask 05-23-20-941-056 A. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. R R
Subtask 05-23-20-010-056-A B. Get Access
R R
(1) Put an adjustable access platform in position at the vertical-stabilizer trailing edge (zone 325).
R R
(2) Remove the access panels 325LL, 325ML, 325NL, 325PL, 325QL, 325RL (Ref. TASK 55-33-13-000-801). 4. Procedure _________ Subtask 05-23-20-210-056 A. Do a general visual inspection of the vertical-stabilizer trailing edge (zone 325). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring) are attached correctly. 5. Close-up ________
R R
Subtask 05-23-20-410-056-A 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 access panels 325LL, 325ML, 325NL, 325PL, 325QL, 325RL (Ref. TASK 55-33-13-400-801). Subtask 05-23-20-942-056 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-20 SROS
Page 618 Jul 01/04
TASK 05-23-20-200-809 Zonal Inspection of Rudder 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 Refer to the MPD TASK: ZL-326-01 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 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R R R
55-33-13-000-801 55-33-13-400-801 55-42-13-000-801 55-42-13-400-801
Removal of the Vertical-Stabilizer Trailing-Edge Access-Panels Installation of the Vertical-Stabilizer Trailing-Edge Access-Panels Removal of the Leading Edge Access-Panels 326 Installation of the Leading Edge Access-Panels 326
EFF : ALL 05-23-20 SROS
Page 619 Jul 01/04
3. __________ Job Set-up Subtask 05-23-20-941-058 A. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-23-20-010-058-A B. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the rudder (zone 326). (2) Remove the trailing-edge panel 325NL (Ref. TASK 55-33-13-000-801). (3) Remove the vertical stabilizer leading-edge panels 326ML, 326NL, 326PL (Ref. TASK 55-42-13-000-801). 4. Procedure _________ Subtask 05-23-20-210-058 R
A. Do a general visual inspection of the rudder (zone 326) in the area of the bearings 2, 3 and 4. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-23-20-410-058-A A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the leading-edge panels 326ML, 326NL, 326PL (Ref. TASK 55-4213-400-801). (3) Install the vertical stabilizer trailing-edge panels 325NL (Ref. TASK 55-33-13-400-801).
EFF : ALL 05-23-20 SROS
Page 620 Jan 01/07
Subtask 05-23-20-942-058 R
B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-20 SROS
Page 621 Jul 01/04
TASK 05-23-20-200-810 Zonal Inspection of Rudder 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 Refer to the MPD TASK: ZL-326-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific No specific
adjustable access platform 16.80 m (55 ft. 1 in.) 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R R
55-33-13-000-801 55-33-13-400-801 55-42-13-000-801 55-42-13-400-801
Removal of the Vertical-Stabilizer Trailing-Edge Access-Panels Installation of the Vertical-Stabilizer Trailing-Edge Access-Panels Removal of the Leading Edge Access-Panels 326 Installation of the Leading Edge Access-Panels 326
EFF : ALL 05-23-20 SROS
Page 622 Jul 01/04
3. __________ Job Set-up Subtask 05-23-20-941-059 A. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-23-20-010-059-A B. Get Access (1) Put an adjustable access platform in position at the rudder (zone 326). (2) Remove the access panels 325NL, 325SL, 325UL, 325VL (Ref. TASK 55-3313-000-801), 326ML, 326NL, 326PL, 326RL, 326SL (Ref. TASK 55-42-13-000-801). 4. Procedure _________ R R R R R
Subtask 05-23-20-210-059-A A. Do a general visual inspection of the rudder (zone 326) in the area of the bearings 1 to 8. Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-23-20-410-059-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 326ML, 326NL, 326PL, 326RL, 326SL (Ref. TASK 55-42-13-400-801). 325NL, 325SL, 325UL, 325VL (Ref. TASK 55-33-13-400-801). Subtask 05-23-20-942-059 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-20 SROS
Page 623 Apr 01/05
TASK 05-23-20-200-811 Zonal Inspection of Rudder (Front Spar FWD Face and Internal Structure as far as visible) 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 Refer to the MPD TASK: ZL-326-03 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
1 ACCESS PLATFORM 17M (56 FT) - ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------53-55-11-000-801 53-55-11-400-801 55-33-13-000-801 55-33-13-400-801 55-34-11-000-801 55-34-11-400-801 55-42-13-000-801
Removal of the Vertical Stabilizer Fairings Installation of the Vertical Stabilizer Fairings Removal of the Vertical-Stabilizer Trailing-Edge Access-Panels Installation of the Vertical-Stabilizer Trailing-Edge Access-Panels Removal of the Vertical Stabilizer Tip Installation of the Vertical Stabilizer Tip Removal of the Leading Edge Access-Panels 326
R EFF : ALL 05-23-20 SROS
Page 624 Jul 01/06
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------55-42-13-400-801 55-44-11-000-801 55-44-11-400-801
Installation of the Leading Edge Access-Panels 326 Removal of the Rudder Tip Installation of the Rudder Tip
3. __________ Job Set-up Subtask 05-23-20-941-060 A. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-23-20-010-060-A B. Get Access (1) Put an ACCESS PLATFORM 17M (56 FT) - ADJUSTABLE in position at the rudder (zone 326). (2) Remove the access panels 325ML, 325NL, 325PL, 325QL, 325RL, 325MR, 325NR, 325PR, 325QR, 325RR (Ref. TASK 55-33-13-000-801). (3) Remove the access panels 326ML, 326NL, 326PL, 326QL (Ref. TASK 55-4213-000-801). R
(4) Remove the access panels 325LL, 325LR, (Ref. TASK 53-55-11-000-801). (5) Remove the rudder tip 326AT (Ref. TASK 55-44-11-000-801). (6) Remove the tip 324CT (Ref. TASK 55-34-11-000-801). 4. Procedure _________ Subtask 05-23-20-210-060
R R R
A. Do a general visual inspection of the front spar forward face and the internal structure of the rudder (zone 326) as far as you can see. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (wiring) are attached correctly.
EFF : ALL 05-23-20 SROS
Page 625 Jul 01/06
5. Close-up ________ Subtask 05-23-20-410-060-A A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the tip 324CT (Ref. TASK 55-34-11-400-801). (3) Install the rudder tip 326AT (Ref. TASK 55-44-11-400-801). R
(4) Install the access panels 325LL, 325LR (Ref. TASK 53-55-11-400-801). (5) Install the access panels 325ML, 325NL, 325PL, 325QL, 325RL, 325MR, 325NR, 325PR, 325QR, 325RR (Ref. TASK 55-33-13-400-801). (6) Install the access panels 326ML, 326NL, 326PL, 326QL (Ref. TASK 5542-13-400-801). Subtask 05-23-20-942-060 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-20 SROS
Page 626 Jul 01/06
______________________________________________________________________________ ZONAL INSPECTION : TRIMMABLE HORIZONTAL STABILIZER LEFT SIDE AND LEFT ELEVATOR ________________ INSPECTION/CHECK TASK 05-23-30-200-801 R
Zonal Inspection of Horizontal Stabilizer Leading Edge 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 Refer to the MPD TASK: ZL-331-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R
No specific No specific
1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------55-12-11-000-801 55-12-11-400-801 55-15-11-000-801 55-15-11-400-801
Removal of the Horizontal Stabilizer Leading-Edge Installation of the Horizontal Stabilizer Leading-Edge Removal of the THS Apron Fairing Assemblies Installation of the THS Apron Fairing Assemblies
EFF : ALL 05-23-30 SROS
Page 601 Jan 01/04
3. __________ Job Set-up Subtask 05-23-30-941-050 A. Safety Precautions R R
(1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-23-30-010-050 B. Get Access
R R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the horizontal-stabilizer leading edge (zones 331 and 341).
R
(2) Remove the access panels:
R R
(a) For the left side 331AT, 333AB, 333AT (Ref. TASK 55-15-11-000801). 331BT, 331CT, 331DT, 331ET (Ref. TASK 55-12-11-000-801).
R R
(b) For the right side 341AT, 343AT, 343AB (Ref. TASK 55-15-11-000801). 341BT, 341CT, 341DT, 341ET (Ref. TASK 55-12-11-000-801). 4. Procedure _________ Subtask 05-23-30-210-050 A. Do a general visual inspection of the horizontal-stabilizers leading edge (zones 331 and 341). Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-23-30-410-050 A. Close Access
R R
(1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Install the access panels
R R
(a) For the left side 331AT, 333AB, 333AT (Ref. TASK 55-15-11-400801). 331BT, 331CT, 331DT (Ref. TASK 55-12-11-400-801).
EFF : ALL 05-23-30 SROS
Page 602 Jan 01/04
R R R
(b) For the right side: 341AT, 343AT, 343AB (Ref. TASK 55-15-11-400801). 341BT, 341CT, 341DT, 341ET (Ref. TASK 55-12-11-400-801). Subtask 05-23-30-942-050 B. Put the Aircraft back to its Initial Configuration
R R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-30 SROS
Page 603 Jan 01/04
TASK 05-23-30-200-802 R
Zonal Inspection of Horizontal Stabilizer Tip 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 Refer to the MPD TASK: ZL-332-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R
No specific No specific
1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------55-14-11-000-801 55-14-11-400-801
Removal of the Trimmable Horizontal Stabilizer Tips Installation of the Trimmable Horizontal Stabilizer Tips
EFF : ALL 05-23-30 SROS
Page 604 Jan 01/04
3. __________ Job Set-up Subtask 05-23-30-941-051 A. Safety Precautions R R
(1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-23-30-010-051 B. Get Access
R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the horizontal stabilizer tip (zones 332 and 342).
R R
(2) Remove the tip on the left and right sides 332AB, 332AT, 342AB, 342AT (Ref. TASK 55-14-11-000-801). 4. Procedure _________ Subtask 05-23-30-210-051 A. Do a general visual inspection of the horizontal stabilizer tip (zones 332 and 342). Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-23-30-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items.
R R R
(2) Install the tip on the left and right sides 332AB, 332AT, 342AB, 342AT (Ref. TASK 55-14-11-400-801).
EFF : ALL 05-23-30 SROS
Page 605 Jan 01/04
Subtask 05-23-30-942-051 B. Put the Aircraft back to its Initial Configuration R R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-30 SROS
Page 606 Jan 01/04
TASK 05-23-30-200-804 Zonal Inspection of Horizontal Stabilizer Lateral Box 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 Refer to the MPD TASK: ZL-333-01 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 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R R
55-11-14-000-802 55-11-14-400-802 55-12-11-000-801 55-12-11-400-801 55-15-11-000-801 55-15-11-400-801
Removal of the THS Front-Spar Access-Panels 333AL, 343AR Installation of the THS Front-Spar Access-Panels 333AL, 343AR Removal of the Horizontal Stabilizer Leading-Edge Installation of the Horizontal Stabilizer Leading-Edge Removal of the THS Apron Fairing Assemblies Installation of the THS Apron Fairing Assemblies
EFF : ALL 05-23-30 SROS
Page 607 Jul 01/04
3. __________ Job Set-up Subtask 05-23-30-941-053 A. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-23-30-010-053 B. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the horizontal-stabilizer side box (zone 333 and 343). (2) Remove the access panels (a) For the left side 331AT, 333AT, 333AB (Ref. TASK 55-15-11-000801). 331BT (Ref. TASK 55-12-11-000-801). 333AL (Ref. TASK 55-1114-000-802). (b) For the right side 341AT, 343AT, 343AB (Ref. TASK 55-15-11-000801). 341BT (Ref. TASK 55-12-11-000-801). 343AR (Ref. TASK 55-1114-000-802). 4. Procedure _________ Subtask 05-23-30-210-053 A. Do a general visual inspection of the horizontal-stabilizer side box (Rib 3 to Rib 4) (zones 333 and 343). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (piping) are attached correctly.
EFF : ALL 05-23-30 R SROS
Page 608 Jul 01/04
5. Close-up ________ Subtask 05-23-30-410-053 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels (a) For the left side 331AT, 333AT, 333AB (Ref. TASK 55-15-11-400801). 331BT (Ref. TASK 55-12-11-400-801). 333AL (Ref. TASK 55-1114-400-802). (b) For the right side 341AT, 343AT, 343AB (Ref. TASK 55-15-11-400801). 341BT (Ref. TASK 55-12-11-400-801). 343AR (Ref. TASK 55-1114-400-802). Subtask 05-23-30-942-053 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-30 R SROS
Page 609 Jan 01/06
TASK 05-23-30-200-805 Zonal Inspection of Horizontal Stabilizer Trailing Edge (From Fuselage Fairing to Rib 10) 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 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-334-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
warning notices 1 ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------55-13-11-000-801 55-13-11-400-801
Removal of the Trailing-Edge Access Panels Installation of the Trailing-Edge Access Panels
3. __________ Job Set-up Subtask 05-23-30-941-054 A. Safety Precautions R R
(1) Put warning notices in the cockpit to tell persons not to operate the flight controls.
EFF : ALL 05-23-30 SROS
Page 610 Jan 01/06
Subtask 05-23-30-010-054 B. Get Access (1) Put an ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE in position at the horizontal-stabilizer trailing edge (zones 334 and 344). (2) Remove the access panels - For the left side: 334AB, 334BB, 334CB (Ref. TASK 55-13-11-000-801). - For the right side: 344AB, 344BB, 344CB (Ref. TASK 55-13-11-000-801). 4. Procedure _________ Subtask 05-23-30-210-054 A. Do a general visual inspection of the horizontal-stabilizer trailing edge from fuselage fairing to rib 10 (zones 334 and 344). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (piping) are attached correctly. 5. Close-up ________ Subtask 05-23-30-410-054 A. Close Access (1) Install the access panels - For the left side: 334AB, 334BB, 334CB (Ref. TASK 55-13-11-400-801). - For the right side: 344AB, 344BB, 344CB (Ref. TASK 55-13-11-400-801).
EFF : ALL 05-23-30 R SROS
Page 611 Jan 01/06
Subtask 05-23-30-942-054 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-23-30 R SROS
Page 612 Jan 01/06
TASK 05-23-30-200-806 Zonal Inspection of Horizontal Stabilizer Trailing Edge (From Fuselage Fairing to Rib 21) 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 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-334-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
warning notices 1 ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------55-13-11-000-801 55-13-11-400-801
Removal of the Trailing-Edge Access Panels Installation of the Trailing-Edge Access Panels
3. __________ Job Set-up Subtask 05-23-30-941-055 A. Safety Precautions R R
(1) Put warning notices in the cockpit to tell persons not to operate the flight controls.
EFF : ALL 05-23-30 SROS
Page 613 Jan 01/06
Subtask 05-23-30-010-055 B. Get Access (1) Put an ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE in position at the horizontal-stabilizer trailing edge (zones 334 and 344). (2) Remove the access panels - For the left side: 334AB, 334BB, 334CB, 334DB, 334EB, 334FB, 334GB (Ref. TASK 55-13-11-000-801). - For the right side: 344AB, 344BB, 344CB, 344DB, 344EB, 344FB, 344GB (Ref. TASK 55-13-11-000-801). 4. Procedure _________ Subtask 05-23-30-210-055 A. Do a general visual inspection of the horizontal-stabilizer trailing edge from fuselage fairing to rib 21 (zones 334 and 344). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (piping) are attached correctly. 5. Close-up ________ Subtask 05-23-30-410-055 A. Close Access (1) Install the access panels - For the left side: 334AB, 334BB, 334CB, 334DB, 334EB, 334FB, 334GB (Ref. TASK 55-13-11-400-801). - For the right side: 344AB, 344BB, 344CB, 344DB, 344EB, 344FB, 344GB (Ref. TASK 55-13-11-400-801).
EFF : ALL 05-23-30 R SROS
Page 614 Jan 01/06
Subtask 05-23-30-942-055 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-23-30 R SROS
Page 615 Jan 01/06
TASK 05-23-30-200-807 Zonal Inspection of Elevator (Area between Ribs 8 and 9) 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 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-335-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
warning notices 1 ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------55-13-11-000-801 55-13-11-400-801 55-22-11-000-801 55-22-11-400-801
Removal of the Trailing-Edge Access Panels Installation of the Trailing-Edge Access Panels Removal of the Elevator Leading Edge Installation of the Elevator Leading Edge
EFF : ALL 05-23-30 SROS
Page 616 Jan 01/06
3. __________ Job Set-up Subtask 05-23-30-941-056 A. Safety Precautions (1) Put warning notices in the cockpit to tell persons not to operate the flight controls. Subtask 05-23-30-010-056 B. Get Access (1) Put an ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE in position at the elevator (zones 335 and 345). (2) Remove the access panels - For the left side: 335BB (Ref. TASK 55-22-11-000-801), 334BB, 334CB, 334DB (Ref. TASK 55-13-11-000-801). - For the right side: 345BB (Ref. TASK 55-22-11-000-801), 344BB, 344CB, 344DB (Ref. TASK 55-13-11-000-801). 4. Procedure _________ Subtask 05-23-30-210-056 R R
A. Do a general visual inspection of the elevator between HTP ribs 8 and 9 (zones 335 and 345). Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see.
EFF : ALL 05-23-30 SROS
Page 617 Jan 01/07
5. Close-up ________ Subtask 05-23-30-410-056 A. Close Access (1) Install the access panels - For the left side: 335BB (Ref. TASK 55-22-11-400-801), 334BB, 334CB, 334DB (Ref. TASK 55-13-11-400-801). - For the right side: 345BB (Ref. TASK 55-22-11-400-801), 344BB, 344CB, 344DB (Ref. TASK 55-13-11-400-801).
R
R
Subtask 05-23-30-942-056 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-23-30 SROS
Page 618 Jan 01/06
TASK 05-23-30-200-808 Zonal Inspection of Elevator (Leading Edge as far as Visible) 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 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-335-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
1 ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------55-13-11-000-801 55-13-11-400-801 55-22-11-000-801 55-22-11-400-801
Removal of the Trailing-Edge Access Panels Installation of the Trailing-Edge Access Panels Removal of the Elevator Leading Edge Installation of the Elevator Leading Edge
EFF : ALL 05-23-30 SROS
Page 619 Jan 01/06
3. __________ Job Set-up Subtask 05-23-30-941-057 A. Safety Precautions R R
(1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-23-30-010-057 B. Get Access (1) Put an ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE in position at the elevator (zones 335 and 345). (2) Remove the access panels: - For the left side: 335AB, 335BB, 335CB, 335DB, 335EB, (Ref. TASK 55-22-11-000-801), 334AB, 334BB, 334CB, 334DB, 334EB, (Ref. TASK 55-13-11-000-801). - For the right side: 345AB, 345BB, 345CB, 345DB, 345EB, (Ref. TASK 55-22-11-000-801), 344AB, 344BB, 344CB, 344DB, 344EB, (Ref. TASK 55-13-11-000-801).
R
R
335FB 334FB, 334GB 345FB 344FB, 344GB
4. Procedure _________ Subtask 05-23-30-210-057 A. Do a general visual inspection of the elevator (zones 335 and 345) leading edge, as far as you can see. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see.
EFF : ALL 05-23-30 SROS
Page 620 Jan 01/06
5. Close-up ________ Subtask 05-23-30-410-057 A. Close Access (1) Install the access panels: - For the left side: 335AB, 335BB, 335CB, 335DB, 335EB, (Ref. TASK 55-22-11-400-801), 334AB, 334BB, 334CB, 334DB, 334EB, (Ref. TASK 55-13-11-400-801). - For the right side: 345AB, 345BB, 345CB, 345DB, 345EB, (Ref. TASK 55-22-11-400-801), 344AB, 344BB, 344CB, 344DB, 344EB, (Ref. TASK 55-13-11-400-801).
R
R
335FB 334FB, 334GB 345FB 344FB, 344GB
Subtask 05-23-30-942-057 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-23-30 SROS
Page 621 Jan 01/06
ZONAL INSPECTION : POWER PLANT, NACELLES AND PYLONS - INSPECTION/CHECK ______________________________________________________________________ TASK 05-24-00-200-801 Zonal Inspection as far as visible from the ground of the Power Plant, the Nacelles and the Pylons (zone 400). 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------54-50-00-200-804
Inspection for Missing Fasteners on the Pylon Fairing Panels
3. __________ Job Set-up Subtask 05-24-00-869-050 A. Not applicable. 4. Procedure _________ Subtask 05-24-00-210-050 A. Inspection (1) Do a general visual inspection of the power plant, the nacelles and the pylons from the ground during the aircraft walkaround. (2) Inspect the pylon fairing panels for missing fasteners (Ref. TASK 5450-00-200-804).
EFF : ALL 05-24-00 R SROS
Page 601 Jan 01/04
TASK 05-24-00-200-802 R
Zonal Inspection of Power Plants, Nacelles and Pylons. 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-400-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------54-50-00-200-804
Inspection for Missing Fasteners on the Pylon Fairing Panels
3. __________ Job Set-up Subtask 05-24-00-010-050 A. Get Access R R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at zone 400. 4. Procedure _________ Subtask 05-24-00-210-051 A. Inspection
R R
(1) Do a general visual inspection of the power plants, the nacelles and the pylons (zone 400). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see.
EFF : ALL 05-24-00 SROS
Page 602 Jan 01/04
(2) Inspect the pylon fairing panels for missing fasteners (Ref. TASK 5450-00-200-804). R
5. Close-up ________
R
Subtask 05-24-00-860-050
R
A. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-24-00 SROS
Page 603 Jan 01/04
ZONAL INSPECTION : ENGINE - INSPECTION/CHECK ____________________________________________ TASK 05-24-10-200-808-A General Visual Inspection of the Engine Air Intake and Intake Lip 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-411-03 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) warning notice adjustable access platform 2.30 m (7 ft. 7 in.) access platform 2.5 m (8 ft. 2 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 78-30-00-040-804 78-30-00-440-804 05-24-10-991-045 05-24-10-991-046 05-24-10-991-047 05-24-10-991-048
Energize the Ground Service Network De-energize the Ground Service Network Deactivation of the Thrust Reverser for Maintenance Reactivation of the Thrust Reverser after Maintenance Fig. 601 Fig. 602 Fig. 603 Fig. 604
3. __________ Job Set-up Subtask 05-24-10-861-066 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-10 Page 601 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
Subtask 05-24-10-941-095 B. Safety Precautions (1) Make sure that the engine 1 (2) shutdown occurred not less than 5 minutes before you do the inspection. (2) Put a warning notice in the cockpit to tell persons not to start the engines. Subtask 05-24-10-010-099 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 05-24-10-865-098 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 05-24-10-040-074 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3000-040-804).
R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-10 Page 602 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
Subtask 05-24-10-010-100 F. Get Access (Ref. Fig. 601/TASK 05-24-10-991-045, 602/TASK 05-24-10-991-046, 603/TASK 05-24-10-991-047, 604/TASK 05-24-10-991-048) (1) Put an adjustable access platform in position at the engine air intake and intake lip (zones 411 and 421). (2) Remove the access panels FOR 4030EM1 411AR, 411AL FOR 4030EM2 421AR, 421AL 4. Procedure _________ Subtask 05-24-10-210-088 A. Inspection. (1) Do a general visual inspection of the engine air intake and intake lip (zones 411 and 421). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting) are attached correctly. 5. Close-up ________ Subtask 05-24-10-440-074 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3000-440-804). Subtask 05-24-10-865-099 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
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Access Doors/ Panels of the Engine 1 Nacelle - Right Side Figure 601/TASK 05-24-10-991-045 R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-10 Page 604 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
Access Doors/ Panels of the Engine 1 Nacelle - Left Side Figure 602/TASK 05-24-10-991-046 R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-10 Page 605 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
Access Doors/ Panels of the Engine 2 Nacelle - Right Side Figure 603/TASK 05-24-10-991-047 R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-10 Page 606 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
Access Doors/ Panels of the Engine 2 Nacelle - Left Side Figure 604/TASK 05-24-10-991-048 R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-10 Page 607 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
Subtask 05-24-10-410-090 C. Installation of the Panels. (Ref. Fig. 601/TASK 05-24-10-991-045, 602/TASK 05-24-10-991-046, 603/TASK 05-24-10-991-047, 604/TASK 05-24-10-991-048) (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels: FOR 4030EM1 411AR, 411AL FOR 4030EM2 421AR, 421AL Subtask 05-24-10-942-094 D. Close Access (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Remove the warning notice in the cockpit. (4) Close the access door 811. (5) Remove the access platform(s). Subtask 05-24-10-862-065 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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TASK 05-24-10-200-809-A General Visual Inspection of the Engine Air Intake and Intake Lip 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-411-04 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 notice adjustable access platform 2.30 m (7 ft. 7 in.) access platform 2.5 m (8 ft. 2 in.)
B. 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 05-24-10-991-045 05-24-10-991-046 05-24-10-991-047 05-24-10-991-048
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. 601 Fig. 602 Fig. 603 Fig. 604
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3. __________ Job Set-up Subtask 05-24-10-861-067 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 05-24-10-941-096 B. Safety Precautions (1) Make sure that the engine 1 (2) shutdown occurred not less than 5 minutes before you do the inspection. (2) Put a warning notice in the cockpit to tell persons not to start the engines. Subtask 05-24-10-010-101 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 05-24-10-865-100 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 05-24-10-040-075 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3000-040-804). Subtask 05-24-10-010-102 F. Get Access (Ref. Fig. 601/TASK 05-24-10-991-045, 602/TASK 05-24-10-991-046, 603/TASK 05-24-10-991-047, 604/TASK 05-24-10-991-048) (1) Put an adjustable access platform in position at the engine air intake and intake lip (zones 411 and 421). (2) Open the fan cowl doors (Ref. TASK 71-13-00-010-802) FOR 4030EM1 415AL, 415BL, 416AR, 416BR FOR 4030EM2 425AL, 425BL, 426AR, 426BR (3) Remove the access panels: FOR 4030EM1 411AL, 411AR FOR 4030EM2 421AL, 421AR 4. Procedure _________ Subtask 05-24-10-210-089 A. Inspection. (1) Do a general visual inspection of the engine air intake and intake lip (zones 411 and 421). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting, wiring) are attached correctly.
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5. Close-up ________ Subtask 05-24-10-440-075 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3000-440-804). Subtask 05-24-10-865-101 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 05-24-10-410-091 C. Installation of the Panels. (Ref. Fig. 601/TASK 05-24-10-991-045, 602/TASK 05-24-10-991-046, 603/TASK 05-24-10-991-047, 604/TASK 05-24-10-991-048) (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels: FOR 4030EM1 411AL, 411AR FOR 4030EM2 421AL, 421AR (3) Close the fan cowl doors (Ref. TASK 71-13-00-410-802) FOR 4030EM1 415AL, 415BL, 416AR, 416BR FOR 4030EM2 425AL, 425BL, 426AR, 426BR Subtask 05-24-10-942-095 D. Close Access (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items. (2) Close the protective door of the AC/DC emergency power center 740VU.
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(3) Remove the warning notice in the cockpit. (4) Close the access door 811. (5) Remove the access platform(s). Subtask 05-24-10-862-066 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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TASK 05-24-10-200-810-A General Visual Inspection of the Fan Frame and Accessory Gear Box 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-412-02 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) 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 WARNING NOTICE
B. 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
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
3. __________ Job Set-up Subtask 05-24-10-861-068 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801).
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Subtask 05-24-10-941-097 B. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to start the engines. Subtask 05-24-10-865-102 C. Get access to the avionics compartment. Then 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 05-24-10-010-103 D. Get Access (1) Open the fan cowl doors (Ref. TASK 71-13-00-010-802). FOR 4030EM1 415AL, 415BL, 416AR, 416BR FOR 4030EM2 425AL, 425BL, 426AR, 426BR. (2) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the fan frame and accessory gear box (zones 412 and 422). Subtask 05-24-10-040-076 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3000-040-804).
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4. Procedure _________ Subtask 05-24-10-210-090 A. Inspection. (1) Do a general visual inspection of the fan frame and accessory gear box (zones 412 and 422). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting) are attached correctly. 5. Close-up ________ Subtask 05-24-10-440-076 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3000-440-804). Subtask 05-24-10-865-103 B. Get access to the avionics compartment. Then 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 05-24-10-410-092 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the fan cowl doors (Ref. TASK 71-13-00-410-802). FOR 4030EM1 415AL, 415BL, 416AR, 416BR FOR 4030EM2 425AL, 425BL, 426AR, 426BR
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Subtask 05-24-10-942-096 D. Close Access (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Close the protective door of the AC/DC emergency power center 740VU. Subtask 05-24-10-862-067 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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TASK 05-24-10-200-811-A General Visual Inspection of the Hot Section 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-413-02 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) warning notice adjustable access platform 2.30 m (7 ft. 7 in.) access platform 2.5 m (8 ft. 2 in.)
B. 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 78-30-00-860-801 78-30-00-860-802 05-24-10-991-045 05-24-10-991-046 05-24-10-991-047 05-24-10-991-048
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 Manually Deploy the Translating Cowl (5047EG1 5047EG2) Manually Stow the Translating Cowl (5047EG1 Or 5047EG2) Fig. 601 Fig. 602 Fig. 603 Fig. 604
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3. __________ Job Set-up Subtask 05-24-10-861-069 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 05-24-10-941-098 B. Safety Precautions (1) Make sure that the engine 1 (2) shutdown occurred not less than 5 minutes before you do the inspection. (2) Put a warning notice in the cockpit to tell persons not to start the engines. Subtask 05-24-10-010-104 C. Get Access to the Avionics Compartment. (1) Put an 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 05-24-10-865-104 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 05-24-10-040-077 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3000-040-804). Subtask 05-24-10-010-105 F. Get Access (Ref. Fig. 601/TASK 05-24-10-991-045, 602/TASK 05-24-10-991-046, 603/TASK 05-24-10-991-047, 604/TASK 05-24-10-991-048) (1) Put an adjustable access platform in position at the engine hot section (zones 413 and 423). (2) Open the fan cowl doors (Ref. TASK 71-13-00-010-802). FOR 4030EM1 415AL, 415BL, 416AR, 416BR FOR 4030EM2 425AL, 425BL, 426AR, 426BR (3) Manually deploy the thrust reverser (Ref. TASK 78-30-00-860-801). (4) Open the thrust reverser doors (Ref. TASK 78-30-00-010-801). FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR 4. Procedure _________ Subtask 05-24-10-210-091 A. Inspection. (1) Do a general visual inspection of the engine hot section (zones 413 and 423). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting) are attached correctly.
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5. Close-up ________ Subtask 05-24-10-440-077 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3000-440-804). Subtask 05-24-10-865-105 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 05-24-10-410-093 C. Close Access (Ref. Fig. 601/TASK 05-24-10-991-045, 602/TASK 05-24-10-991-046, 603/TASK 05-24-10-991-047, 604/TASK 05-24-10-991-048) (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the thrust reverser doors (Ref. TASK 78-30-00-410-801). FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR (3) Manually stow the thrust reverser (Ref. TASK 78-30-00-860-802). (4) Close the fan cowl doors (Ref. TASK 71-13-00-410-802). FOR 4030EM1 415AL, 415BL, 416AR, 416BR FOR 4030EM2 425AL, 425BL, 426AR, 426BR
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Subtask 05-24-10-942-097 D. Close Access (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Remove the warning notice in the cockpit. (4) Close the access door 811. (5) Remove the access platform(s). Subtask 05-24-10-862-068 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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TASK 05-24-10-200-812-A General Visual Inspection of the Exhaust Nozzle 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-414-02 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) warning notice adjustable access platform 2.30 m (7 ft. 7 in.) access platform 2.5 m (8 ft. 2 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 78-30-00-010-801 78-30-00-040-804 78-30-00-410-801 78-30-00-440-804 05-24-10-991-045 05-24-10-991-046 05-24-10-991-047 05-24-10-991-048
Energize the Ground Service Network De-energize the Ground Service Network 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. 601 Fig. 602 Fig. 603 Fig. 604
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3. __________ Job Set-up Subtask 05-24-10-861-070 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 05-24-10-941-099 B. Safety Precautions (1) Make sure that the engine 1 (2) shutdown occurred not less than 5 minutes before you do the inspection. (2) Put a warning notice in the cockpit to tell persons not to start the engines. Subtask 05-24-10-010-106 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 05-24-10-865-106 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 05-24-10-040-078 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3000-040-804). Subtask 05-24-10-010-107 F. Get Access (Ref. Fig. 601/TASK 05-24-10-991-045, 602/TASK 05-24-10-991-046, 603/TASK 05-24-10-991-047, 604/TASK 05-24-10-991-048) (1) Put an adjustable access platform in position at the exhaust nozzle (zones 410 and 420). (2) Open the thrust reverser doors (Ref. TASK 78-30-00-010-801). FOR 4030EM1 415BL, 416BR, 417AL, 418AR FOR 4030EM2 425BL, 426BR, 427AL, 428AR 4. Procedure _________ Subtask 05-24-10-210-092 A. Inspection. (1) Do a general visual inspection of the exhaust nozzle (zones 410 and 420). (2) Make sure that: - there is no damage, corrosion, leaks or cracks on all the parts of the components and the structure you can see, - all the installations are attached correctly. 5. Close-up ________ Subtask 05-24-10-440-078 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3000-440-804).
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Subtask 05-24-10-865-107 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 05-24-10-410-094 C. Closing of the Thrust Reverser Doors. (Ref. Fig. 601/TASK 05-24-10-991-045, 602/TASK 05-24-10-991-046, 603/TASK 05-24-10-991-047, 604/TASK 05-24-10-991-048) (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the thrust reverser doors (Ref. TASK 78-30-00-410-801). FOR 4030EM1 415BL, 416BR, 417AL, 418AR FOR 4030EM2 425BL, 426BR, 427AL, 428AR Subtask 05-24-10-942-098 D. Close Access (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Remove the warning notice in the cockpit. (4) Close the access door 811. (5) Remove the access platform(s). Subtask 05-24-10-862-069 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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TASK 05-24-10-200-813-A General Visual Inspection of the Fan Cowl 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-415-02 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) warning notice adjustable access platform 2.30 m (7 ft. 7 in.) access platform 2.5 m (8 ft. 2 in.)
B. 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 05-24-10-991-045 05-24-10-991-046 05-24-10-991-047 05-24-10-991-048
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. 601 Fig. 602 Fig. 603 Fig. 604
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3. __________ Job Set-up Subtask 05-24-10-861-071 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 05-24-10-941-100 B. Safety Precautions (1) Make sure that the engine 1 (2) shutdown occurred not less than 5 minutes before you do the inspection. (2) Put a warning notice in the cockpit to tell persons not to start the engines Subtask 05-24-10-010-108 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 05-24-10-865-108 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 05-24-10-040-079 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3000-040-804). Subtask 05-24-10-010-109 F. Get Access (Ref. Fig. 601/TASK 05-24-10-991-045, 602/TASK 05-24-10-991-046, 603/TASK 05-24-10-991-047, 604/TASK 05-24-10-991-048) (1) Put an adjustable access platform in position at the fan cowl (zones 410 and 420). (2) Open the fan cowl doors (Ref. TASK 71-13-00-010-802). FOR 4030EM1 415AL, 415BL, 416AR, 416BR FOR 4030EM2 425AL, 425BL, 426AR, 426BR (3) Remove the access panels FOR 4030EM1 415CL FOR 4030EM2 425CL 4. Procedure _________ Subtask 05-24-10-210-093 A. Inspection. (1) Do a general visual inspection of the fan cowls (zones 410 and 420). (2) Make sure that: - there is no damage, corrosion, leaks or cracks on all the parts of the components and the structure you can see, - all the installations (ducting) are attached correctly.
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5. Close-up ________ Subtask 05-24-10-440-079 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3000-440-804). Subtask 05-24-10-865-109 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 05-24-10-410-095 C. Installation of the Panels. (Ref. Fig. 601/TASK 05-24-10-991-045, 602/TASK 05-24-10-991-046, 603/TASK 05-24-10-991-047, 604/TASK 05-24-10-991-048) (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels: FOR 4030EM1 415CL FOR 4030EM2 425CL (3) Close the fan cowl doors (Ref. TASK 71-13-00-410-802). FOR 4030EM1 415AL, 415BL, 416AR, 416BR FOR 4030EM2 425AL, 425BL, 426AR, 426BR Subtask 05-24-10-942-099 D. Close Access (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items. (2) Close the protective door of the AC/DC emergency power center 740VU.
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(3) Remove the warning notice in the cockpit. (4) Close the access door 811. (5) Remove the access platform(s). Subtask 05-24-10-862-070 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-10 Page 631 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
TASK 05-24-10-200-814-A General Visual Inspection of the Thrust Reverser 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-417-02 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) 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 71-13-00-010-803 71-13-00-410-803 78-30-00-040-804 78-30-00-440-804 78-30-00-860-801 78-30-00-860-802 78-36-00-010-802 78-36-00-410-802 05-24-10-991-045 05-24-10-991-046 05-24-10-991-047 05-24-10-991-048
Energize the Ground Service Network De-energize the Ground Service Network Opening of the Fan Cowl Doors Closing of the Fan Cowl Doors Deactivation of the Thrust Reverser for Maintenance Reactivation of the Thrust Reverser after Maintenance Manually Deploy the Translating Cowl (5047EG1 5047EG2) Manually Stow the Translating Cowl (5047EG1 Or 5047EG2) Opening of the Thrust Reverser Cowl Doors Closing of the Thrust Reverser Cowl Doors Fig. 601 Fig. 602 Fig. 603 Fig. 604
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3. __________ Job Set-up Subtask 05-24-10-861-072 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 05-24-10-941-101 B. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to start the engines. Subtask 05-24-10-865-110 C. Get access to the avionics compartment. Then 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 05-24-10-040-080 D. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3000-040-804).
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Subtask 05-24-10-010-110 E. Get Access (Ref. Fig. 601/TASK 05-24-10-991-045, 602/TASK 05-24-10-991-046, 603/TASK 05-24-10-991-047, 604/TASK 05-24-10-991-048) (1) Open the fan cowl doors (Ref. TASK 71-13-00-010-803) FOR 4030EM1 415BL, 416BR FOR 4030EM2 425BL, 426BR (2) Manually deploy the thrust reverser (Ref. TASK 78-30-00-860-801). (3) Open the thrust reverser doors (Ref. TASK 78-36-00-010-802). FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR (4) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the thrust reverser (zones 410 and 420). (5) Open or remove the access panels: FOR 4030EM1 417DL, 417EL, 417FL, 417GL, 417HL, 418BR, 418CR, 418FR, 418GR, 418HR, 418JR FOR 4030EM2 427DL, 427EL, 427FL, 427GL, 427HL, 428BR, 428CR, 428FR, 428GR, 428HR, 428JR 4. Procedure _________ Subtask 05-24-10-210-094 A. Inspection. (1) Do a general visual inspection of the thrust reverser (zones 410 and 420). (2) Make sure that: - there is no damage, corrosion, leaks or cracks on all the parts of the components and the structure you can see, - all the installations (ducting) are attached correctly.
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5. Close-up ________ Subtask 05-24-10-410-096 A. Installation of the Panels (Ref. Fig. 601/TASK 05-24-10-991-045, 602/TASK 05-24-10-991-046, 603/TASK 05-24-10-991-047, 604/TASK 05-24-10-991-048) (1) Close or install the access panels: FOR 4030EM1 417DL, 417EL, 417FL, 417GL, 417HL, 418BR, 418CR, 418FR, 418GR, 418HR, 418JR. FOR 4030EM2 427DL, 427EL, 427FL, 427GL, 427HL, 428BR, 428CR, 428FR, 428GR, 428HR, 428JR. (2) Close the thrust reverser doors (Ref. TASK 78-36-00-410-802). FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR (3) Manually stow the thrust reverser (Ref. TASK 78-30-00-860-802). (4) Close the fan cowl doors (Ref. TASK 71-13-00-410-803) FOR 4030EM1 415BL, 416BR FOR 4030EM2 425BL, 426BR Subtask 05-24-10-440-080 B. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3000-440-804). Subtask 05-24-10-865-111 C. Get access to the avionics compartment. Then 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 05-24-10-862-071 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 all the fixtures, tools, test and support equipment used during this procedure. (3) Make sure that the work area is clean and clear of tools and other items.
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ZONAL INSPECTION : ENGINE - INSPECTION/CHECK ____________________________________________ TASK 05-24-10-200-808-B General Visual Inspection of the Engine Air Intake and Intake Lip 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-411-03 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) warning notice adjustable access platform 2.30 m (7 ft. 7 in.) access platform 2.5 m (8 ft. 2 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 78-31-00-040-805 78-31-00-440-805 05-24-10-991-049 05-24-10-991-050 05-24-10-991-051 05-24-10-991-052
Energize the Ground Service Network De-energize the Ground Service Network Deactivation of the Thrust Reverser for Maintenance Activation of the Thrust Reverser after Maintenance Fig. 601 Fig. 602 Fig. 603 Fig. 604
3. __________ Job Set-up Subtask 05-24-10-861-073 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801).
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Subtask 05-24-10-941-102 B. Safety Precautions (1) Make sure that the engine 1 (2) shutdown occurred not less than 5 minutes before you do the inspection. (2) Put a warning notice in the cockpit to tell persons not to start the engines. Subtask 05-24-10-010-111 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 05-24-10-865-112 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 05-24-10-040-081 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3100-040-805).
EFF : 701-749, 05-24-10 Page 602 Config-3 Jul 01/04 SROS
Subtask 05-24-10-010-112 F. Get Access (Ref. Fig. 601/TASK 05-24-10-991-049, 602/TASK 05-24-10-991-050, 603/TASK 05-24-10-991-051, 604/TASK 05-24-10-991-052) (1) Put an adjustable access platform in position at the engine air intake and intake lip (zones 411 and 421). (2) Remove the access panels FOR 4030EM1 411AR, 411AL FOR 4030EM2 421AR, 421AL 4. Procedure _________ Subtask 05-24-10-210-095 A. Inspection. (1) Do a general visual inspection of the engine air intake and intake lip (zones 411 and 421). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting) are attached correctly. 5. Close-up ________ Subtask 05-24-10-440-081 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3100-440-805). Subtask 05-24-10-865-113 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
EFF : 701-749, 05-24-10 Page 603 Config-3 Jul 01/04 SROS
Access Door/ Panels of the Engine 1 Nacelle - Right Side Figure 601/TASK 05-24-10-991-049 EFF : 701-749, 05-24-10 Page 604 Config-3 Jul 01/04 SROS
Access Door/ Panels of the Engine 1 Nacelle - Left Side Figure 602/TASK 05-24-10-991-050 EFF : 701-749, 05-24-10 Page 605 Config-3 Jul 01/04 SROS
Access Door/ Panels of the Engine 2 Nacelle - Right Side Figure 603/TASK 05-24-10-991-051 EFF : 701-749, 05-24-10 Page 606 Config-3 Jul 01/04 SROS
Access Door/ Panels of the Engine 2 Nacelle - Left Side Figure 604/TASK 05-24-10-991-052 EFF : 701-749, 05-24-10 Page 607 Config-3 Jul 01/04 SROS
Subtask 05-24-10-410-097 C. Installation of the Panels. (Ref. Fig. 601/TASK 05-24-10-991-049, 602/TASK 05-24-10-991-050, 603/TASK 05-24-10-991-051, 604/TASK 05-24-10-991-052) (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels FOR 4030EM1 411AR, 411AL FOR 4030EM2 421AR, 421AL Subtask 05-24-10-942-100 D. Close Access (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Remove the warning notice in the cockpit. (4) Close the access door 811. (5) Remove the access platform(s). Subtask 05-24-10-862-072 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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TASK 05-24-10-200-809-B General Visual Inspection of the Engine Air Intake and Intake Lip 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-411-04 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 notice adjustable access platform 2.30 m (7 ft. 7 in.) access platform 2.5 m (8 ft. 2 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------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 05-24-10-991-049 05-24-10-991-050 05-24-10-991-051 05-24-10-991-052
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. 601 Fig. 602 Fig. 603 Fig. 604
3. __________ Job Set-up Subtask 05-24-10-861-074 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801).
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Subtask 05-24-10-941-103 B. Safety Precautions (1) Make sure that the engine 1 (2) shutdown occurred not less than 5 minutes before you do the inspection. (2) Put a warning notice in the cockpit to tell persons not to start the engines. Subtask 05-24-10-010-113 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 05-24-10-865-114 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 05-24-10-040-082 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3100-040-805).
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Subtask 05-24-10-010-114 F. Get Access (Ref. Fig. 601/TASK 05-24-10-991-049, 602/TASK 05-24-10-991-050, 603/TASK 05-24-10-991-051, 604/TASK 05-24-10-991-052) (1) Put an adjustable access platform in position at the engine air intake and intake lip (zones 411 and 421). (2) Open the fan cowl doors (Ref. TASK 71-13-00-010-805) FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR (3) Remove the access panels: FOR 4030EM1 411AL, 411AR FOR 4030EM2 421AL, 421AR 4. Procedure _________ Subtask 05-24-10-210-096 A. Inspection. (1) Do a general visual inspection of the engine air intake and intake lip (zones 411 and 421). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting, wiring) are attached correctly. 5. Close-up ________ Subtask 05-24-10-440-082 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3100-440-805).
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Subtask 05-24-10-865-115 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 05-24-10-410-098 C. Installation of the Panels. (Ref. Fig. 601/TASK 05-24-10-991-049, 602/TASK 05-24-10-991-050, 603/TASK 05-24-10-991-051, 604/TASK 05-24-10-991-052) (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels: FOR 4030EM1 411AL, 411AR FOR 4030EM2 421AL, 421AR (3) Close the fan cowl doors (Ref. TASK 71-13-00-410-805) FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR Subtask 05-24-10-942-101 D. Close Access (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Remove the warning notice in the cockpit. (4) Close the access door 811. (5) Remove the access platform(s).
EFF : 701-749, 05-24-10 Page 612 Config-3 Jul 01/04 SROS
Subtask 05-24-10-862-073 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : 701-749, 05-24-10 Page 613 Config-3 Jul 01/04 SROS
TASK 05-24-10-200-810-B General Visual Inspection of the Fan Frame and Accessory Gear Box 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-412-02 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) 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------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
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
3. __________ Job Set-up Subtask 05-24-10-861-075 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 05-24-10-941-104 B. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to start the engines.
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Subtask 05-24-10-865-116 C. Get access to the avionics compartment. Then 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 05-24-10-010-115 D. 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 an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the fan frame and accessory gear box (zones 412 and 422). Subtask 05-24-10-040-083 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3100-040-805).
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4. Procedure _________ Subtask 05-24-10-210-097 A. Inspection. (1) Do a general visual inspection of the fan frame and accessory gear box (zones 412 and 422). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting) are attached correctly. 5. Close-up ________ Subtask 05-24-10-440-083 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3100-440-805). Subtask 05-24-10-865-117 B. Get access to the avionics compartment. Then 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 05-24-10-410-099 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the fan cowl doors (Ref. TASK 71-13-00-410-805). FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR
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Subtask 05-24-10-942-102 D. Close Access (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Close the protective door of the AC/DC emergency power center 740VU. Subtask 05-24-10-862-074 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : 701-749, 05-24-10 Page 617 Config-3 Jul 01/04 SROS
TASK 05-24-10-200-811-B General Visual Inspection of the Hot Section 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-413-02 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) warning notice adjustable access platform 2.30 m (7 ft. 7 in.) access platform 2.5 m (8 ft. 2 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 71-13-00-010-805 71-13-00-410-805 78-30-00-010-803 78-30-00-410-803 78-31-00-040-805 78-31-00-440-805 05-24-10-991-049 05-24-10-991-050 05-24-10-991-051 05-24-10-991-052
Energize the Ground Service Network De-energize the Ground Service Network Open the Fan Cowl Doors Close the Fan Cowl Doors Open the Thrust Reverser Cowl Doors Close the Thrust Reverser Cowl Doors Deactivation of the Thrust Reverser for Maintenance Activation of the Thrust Reverser after Maintenance Fig. 601 Fig. 602 Fig. 603 Fig. 604
EFF : 701-749, 05-24-10 Page 618 Config-3 Jul 01/04 SROS
3. __________ Job Set-up Subtask 05-24-10-861-076 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 05-24-10-941-105 B. Safety Precautions (1) Make sure that the engine 1 (2) shutdown occurred not less than 5 minutes before you do the inspection. (2) Put a warning notice in the cockpit to tell persons not to start the engines. Subtask 05-24-10-010-116 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 05-24-10-865-118 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, 05-24-10 Page 619 Config-3 Jul 01/04 SROS
Subtask 05-24-10-040-084 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3100-040-805). Subtask 05-24-10-010-117 F. Get Access (Ref. Fig. 601/TASK 05-24-10-991-049, 602/TASK 05-24-10-991-050, 603/TASK 05-24-10-991-051, 604/TASK 05-24-10-991-052) (1) Put an adjustable access platform in position at the engine hot section (zones 413 and 423). (2) Open the fan cowl doors (Ref. TASK 71-13-00-010-805). FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR (3) Open the thrust reverser doors (Ref. TASK 78-30-00-010-803). FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR 4. Procedure _________ Subtask 05-24-10-210-098 A. Inspection. (1) Do a general visual inspection of the engine hot section (zones 413 and 423). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting) are attached correctly.
EFF : 701-749, 05-24-10 Page 620 Config-3 Jul 01/04 SROS
5. Close-up ________ Subtask 05-24-10-440-084 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3100-440-805). Subtask 05-24-10-865-119 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 05-24-10-410-100 C. Close Access (Ref. Fig. 601/TASK 05-24-10-991-049, 602/TASK 05-24-10-991-050, 603/TASK 05-24-10-991-051, 604/TASK 05-24-10-991-052) (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the thrust reverser doors (Ref. TASK 78-30-00-410-803). FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR (3) Close the fan cowl doors (Ref. TASK 71-13-00-410-805). FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR Subtask 05-24-10-942-103 D. Close Access (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items. (2) Close the protective door of the AC/DC emergency power center 740VU.
EFF : 701-749, 05-24-10 Page 621 Config-3 Jul 01/04 SROS
(3) Remove the warning notice in the cockpit. (4) Close the access door 811. (5) Remove the access platform(s). Subtask 05-24-10-862-075 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : 701-749, 05-24-10 Page 622 Config-3 Jul 01/04 SROS
TASK 05-24-10-200-812-B General Visual Inspection of the Exhaust Nozzle 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-414-02 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) warning notice adjustable access platform 2.30 m (7 ft. 7 in.) access platform 2.5 m (8 ft. 2 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 78-30-00-010-803 78-30-00-410-803 78-31-00-040-805 78-31-00-440-805 05-24-10-991-049 05-24-10-991-050 05-24-10-991-051 05-24-10-991-052
Energize the Ground Service Network De-energize the Ground Service Network Open the Thrust Reverser Cowl Doors Close the Thrust Reverser Cowl Doors Deactivation of the Thrust Reverser for Maintenance Activation of the Thrust Reverser after Maintenance Fig. 601 Fig. 602 Fig. 603 Fig. 604
3. __________ Job Set-up Subtask 05-24-10-861-077 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801).
EFF : 701-749, 05-24-10 Page 623 Config-3 Jul 01/04 SROS
Subtask 05-24-10-941-106 B. Safety Precautions (1) Make sure that the engine 1 (2) shutdown occurred not less than 5 minutes before you do the inspection. (2) Put a warning notice in the cockpit to tell persons not to start the engines. Subtask 05-24-10-010-118 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 05-24-10-865-120 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 05-24-10-040-085 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3100-040-805).
EFF : 701-749, 05-24-10 Page 624 Config-3 Jul 01/04 SROS
Subtask 05-24-10-010-119 F. Get Access (Ref. Fig. 601/TASK 05-24-10-991-049, 602/TASK 05-24-10-991-050, 603/TASK 05-24-10-991-051, 604/TASK 05-24-10-991-052) (1) Put an adjustable access platform in position at the exhaust nozzle (zones 410 and 420). (2) Open the thrust reverser doors (Ref. TASK 78-30-00-010-803). FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AR, 428AR 4. Procedure _________ Subtask 05-24-10-210-099 A. Inspection. (1) Do a general visual inspection of the exhaust nozzle (zones 410 and 420). (2) Make sure that: - there is no damage, corrosion, leaks or cracks on all the parts of the components and the structure you can see, - all the installations are attached correctly. 5. Close-up ________ Subtask 05-24-10-440-085 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3100-440-805). Subtask 05-24-10-865-121 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
EFF : 701-749, 05-24-10 Page 625 Config-3 Jul 01/04 SROS
Subtask 05-24-10-410-101 C. Closing of the Thrust Reverser Doors. (Ref. Fig. 601/TASK 05-24-10-991-049, 602/TASK 05-24-10-991-050, 603/TASK 05-24-10-991-051, 604/TASK 05-24-10-991-052) (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the thrust reverser doors (Ref. TASK 78-30-00-410-803). FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR Subtask 05-24-10-942-104 D. Close Access (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Remove the warning notice in the cockpit. (4) Close the access door 811. (5) Remove the access platform(s). Subtask 05-24-10-862-076 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : 701-749, 05-24-10 Page 626 Config-3 Jul 01/04 SROS
TASK 05-24-10-200-813-B General Visual Inspection of the Fan Cowl 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-415-02 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) warning notice adjustable access platform 2.30 m (7 ft. 7 in.) access platform 2.5 m (8 ft. 2 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------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 05-24-10-991-049 05-24-10-991-050 05-24-10-991-051 05-24-10-991-052
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. 601 Fig. 602 Fig. 603 Fig. 604
3. __________ Job Set-up Subtask 05-24-10-861-078 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801).
EFF : 701-749, 05-24-10 Page 627 Config-3 Jul 01/04 SROS
Subtask 05-24-10-941-107 B. Safety Precautions (1) Make sure that the engine 1 (2) shutdown occurred not less than 5 minutes before you do the inspection. (2) Put a warning notice in the cockpit to tell persons not to start the engines Subtask 05-24-10-010-120 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 05-24-10-865-122 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 05-24-10-040-086 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3100-040-805).
EFF : 701-749, 05-24-10 Page 628 Config-3 Jul 01/04 SROS
Subtask 05-24-10-010-121 F. Get Access (Ref. Fig. 601/TASK 05-24-10-991-049, 602/TASK 05-24-10-991-050, 603/TASK 05-24-10-991-051, 604/TASK 05-24-10-991-052) (1) Put an adjustable access platform in position at the fan cowl (zones 410 and 420). (2) Open the fan cowl doors (Ref. TASK 71-13-00-010-805). FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR (3) Remove the access panels FOR 4030EM1 415BL, 415CL, 416BR, 416CR FOR 4030EM2 425BL, 425CL, 426BR, 426CR 4. Procedure _________ Subtask 05-24-10-210-100 A. Inspection. (1) Do a general visual inspection of the fan cowls (zones 410 and 420). (2) Make sure that: - there is no damage, corrosion, leaks or cracks on all the parts of the components and the structure you can see, - all the installations (ducting) are attached correctly. 5. Close-up ________ Subtask 05-24-10-440-086 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3100-440-805).
EFF : 701-749, 05-24-10 Page 629 Config-3 Jul 01/04 SROS
Subtask 05-24-10-865-123 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 05-24-10-410-102 C. Installation of the Panels. (Ref. Fig. 601/TASK 05-24-10-991-049, 602/TASK 05-24-10-991-050, 603/TASK 05-24-10-991-051, 604/TASK 05-24-10-991-052) (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels: FOR 4030EM1 415BL, 415CL, 416BR, 416CR FOR 4030EM2 425BL, 425CL, 426BR, 426CR (3) Close the fan cowl doors (Ref. TASK 71-13-00-410-805). FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR Subtask 05-24-10-942-105 D. Close Access (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Remove the warning notice in the cockpit. (4) Close the access door 811. (5) Remove the access platform(s).
EFF : 701-749, 05-24-10 Page 630 Config-3 Jul 01/04 SROS
Subtask 05-24-10-862-077 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : 701-749, 05-24-10 Page 631 Config-3 Jul 01/04 SROS
TASK 05-24-10-200-814-B General Visual Inspection of the Thrust Reverser 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-417-02 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) 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R
24-42-00-861-801 24-42-00-862-801 71-13-00-010-805 71-13-00-410-805 78-30-00-010-803 78-30-00-410-803
Energize the Ground Service Network De-energize the Ground Service Network Open the Fan Cowl Doors Close the Fan Cowl Doors Open the Thrust Reverser Cowl Doors Close the Thrust Reverser Cowl Doors
78-31-00-040-805 78-31-00-440-805 05-24-10-991-049 05-24-10-991-050 05-24-10-991-051 05-24-10-991-052
Deactivation of the Thrust Reverser for Maintenance Activation of the Thrust Reverser after Maintenance Fig. 601 Fig. 602 Fig. 603 Fig. 604
R
R
EFF : 701-749, 05-24-10 Page 632 Config-3 Apr 01/05 SROS
3. __________ Job Set-up Subtask 05-24-10-865-124 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 05-24-10-941-108 B. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to start the engines. Subtask 05-24-10-865-125 C. Get access to the avionics compartment. Then 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 05-24-10-040-087 D. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3100-040-805).
EFF : 701-749, 05-24-10 Page 633 Config-3 Jul 01/04 SROS
Subtask 05-24-10-010-122 E. Get Access (Ref. Fig. 601/TASK 05-24-10-991-049, 602/TASK 05-24-10-991-050, 603/TASK 05-24-10-991-051, 604/TASK 05-24-10-991-052) R
(1) Open the fan cowl doors (Ref. TASK 71-13-00-010-805). FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR
R R R R
(2) Open the thrust reverser doors (Ref. TASK 78-30-00-010-803). FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR
R
(3) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the thrust reverser (zones 410 and 420).
R
(4) Open or remove the access panels: FOR 4030EM1 417BL, 417CL, 417DL, 417EL, 417FL, 417GL, 418BR, 418CR, 418DR, 418ER, 418FR, 418GR, 418HR, 418JR. FOR 4030EM2 427BL, 427CL, 427DL, 427EL, 427FL, 427GL, 428BR, 428CR, 428DR, 428ER, 428FR, 428GR, 428HR, 428JR 4. Procedure _________ Subtask 05-24-10-210-101 A. Inspection. (1) Do a general visual inspection of the thrust reverser (zones 410 and 420). (2) Make sure that: - there is no damage, corrosion, leaks or cracks on all the parts of the components and the structure you can see, - all the installations (ducting) are attached correctly.
EFF : 701-749, 05-24-10 Page 634 Config-3 Apr 01/05 SROS
5. Close-up ________ Subtask 05-24-10-410-103 A. Installation of the Panels (Ref. Fig. 601/TASK 05-24-10-991-049, 602/TASK 05-24-10-991-050, 603/TASK 05-24-10-991-051, 604/TASK 05-24-10-991-052) (1) Close or install the FOR 4030EM1 417BL, 417CL, 417DL, 418FR, 418GR, 418HR, FOR 4030EM2 427BL, 427CL, 427DL, 428FR, 428GR, 428HR,
access panels: 417EL, 417FL, 417GL, 418BR, 418CR, 418DR, 418ER, 418JR. 427EL, 427FL, 427GL, 428BR, 428CR, 428DR, 428ER, 428JR.
(2) Close the thrust reverser doors (Ref. TASK 78-30-00-410-803). FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR R R
(3) Close the fan cowl doors (Ref. TASK 71-13-00-410-805). FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR
R R
Subtask 05-24-10-440-087 B. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3100-440-805). Subtask 05-24-10-865-126 C. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2
EFF : 701-749, 05-24-10 Page 635 Config-3 Apr 01/05 SROS
Subtask 05-24-10-862-078 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 all the fixtures, tools, test and support equipment used during this procedure. (3) Make sure that the work area is clean and clear of tools and other items.
EFF : 701-749, 05-24-10 Page 636 Config-3 Jul 01/04 SROS
ZONAL INSPECTION : ENGINE PYLON - INSPECTION/CHECK __________________________________________________ TASK 05-24-50-200-806-A Zonal Inspection of the Pylon Leading Edge 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-451-02 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) warning notice access platform 2.5 m (8 ft. 2 in.) adjustable access platform 4.60 m (15 ft. 1 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 78-30-00-040-804 78-30-00-440-804 05-24-50-991-034 05-24-50-991-033
Energize the Ground Service Network De-energize the Ground Service Network Deactivation of the Thrust Reverser for Maintenance Reactivation of the Thrust Reverser after Maintenance Fig. 601 Fig. 602
3. __________ Job Set-up Subtask 05-24-50-861-065 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-50 Page 601 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
Subtask 05-24-50-941-080 B. Safety Precautions (1) Make sure that the engine 1(2) shutdown occurred no less than 5 minutes before you do the inspection. (2) Put a warning notice in the cockpit to tell persons not to start the engines. Subtask 05-24-50-010-086 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 05-24-50-865-090 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 05-24-50-040-070 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3000-040-804).
R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-50 Page 602 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
Subtask 05-24-50-010-087 F. Get Access (Ref. Fig. 601/TASK 05-24-50-991-034, 602/TASK 05-24-50-991-033) (1) Put an adjustable access platform in position at the pylon leading edge (zones 451, 461). (2) Remove the access panels: (a) For the pylon 1 451BL, 451CL, 451DL, 451BR, 451CR, 451DR (b) For the pylon 2 461BL, 461CL, 461DL, 461BR, 461CR, 461DR 4. Procedure _________ Subtask 05-24-50-210-080 A. Inspection. (1) Do a general visual inspection of the pylon leading edge (zones 451, 461). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-24-50-440-070 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3000-440-804). Subtask 05-24-50-865-091 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
R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-50 Page 603 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
Access Door/ Panels, Engine 1 Pylon Figure 601/TASK 05-24-50-991-034 R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-50 Page 604 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
Access Doors/ Panels, Engine 2 Pylon Figure 602/TASK 05-24-50-991-033 R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-50 Page 605 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
Subtask 05-24-50-410-080 C. Installation of the Panels. (Ref. Fig. 601/TASK 05-24-50-991-034, 602/TASK 05-24-50-991-033) (1) Make sure that the work area is clean and clear of tools and other items. (2) Close Access (3) Install the access panels: (a) For the pylon 2 461BL, 461CL, 461DL, 461BR, 461CR, 461DR (b) For the pylon 1 451BL, 451CL, 451DL, 451BR, 451CR, 451DR Subtask 05-24-50-942-085 D. Close Access (1) Close the protective door of the AC/DC emergency power-center 740VU. (2) Remove the warning notice in the cockpit. (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. Subtask 05-24-50-862-061 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-50 Page 606 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
TASK 05-24-50-200-802 Zonal Inspection of the Upper Forward of the Pylon 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-452-01 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) 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 54-52-11-000-809 54-52-11-400-809 78-30-00-040-804 78-30-00-440-804
Energize the Ground Service Network De-energize the Ground Service Network Removal of the Access Panels (RIBJ8 to RIB8A) Installation of the Access Panels (RIBJ8 to RIB8A) Deactivation of the Thrust Reverser for Maintenance Reactivation of the Thrust Reverser after Maintenance
3. __________ Job Set-up Subtask 05-24-50-861-066 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 05-24-50-941-081 B. Safety Precautions (1) Put a WARNING NOTICE to tell persons not to start the engines.
R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-50 Page 607 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
Subtask 05-24-50-865-092 C. Get access to the avionics compartment. Then 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 05-24-50-040-071 D. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3000-040-804). Subtask 05-24-50-010-088 E. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the pylon leading edge (zones 452, 462). (2) Remove the access panels (Ref. TASK 54-52-11-000-809): (a) For the pylon 1 452AL, 452BL, 452CL 452BR, 452CR. (b) For the pylon 2 462AL, 462BL, 462CL 462BR, 462CR.
R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-50 Page 608 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
4. Procedure _________ Subtask 05-24-50-210-081 A. Inspection. (1) Do a general visual inspection of the upper forward section of the pylon (zones 452, 462). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-24-50-440-071 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3000-440-804). Subtask 05-24-50-865-093 B. Get access to the avionics compartment. Then 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 05-24-50-410-081 C. Installation of the Panels. CAUTION : WHEN YOU INSTALL THE ACCESS PANELS 452AL AND 462AL, MAKE SURE _______ THAT THE OVERPRESSURE DOOR IS CLOSED CORRECTLY. IF THE OVERPRESSURE DOOR IS NOT CLOSED, A FLOW OF HOT AIR CAN CAUSE A BLEED OVERHEAT DETECTION. (1) Make sure that the work area is clean and clear of tools and other items.
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(2) Install the access panels (Ref. TASK 54-52-11-400-809): (a) For the pylon 2 462AL, 462BL, 462CL 462BR, 462CR . (b) For the pylon 1 452AL, 452BL, 452CL 452BR, 452CR. Subtask 05-24-50-862-062 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 all the fixtures, tools, test and support equipment used during this procedure.
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TASK 05-24-50-200-808-A Zonal Inspection of the Lower of the Pylon 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-453-01 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 notice access platform 2.5 m (8 ft. 2 in.) adjustable access platform 4.60 m (15 ft. 1 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 78-30-00-440-804 78-31-00-040-802 05-24-50-991-034 05-24-50-991-033
Energize the Ground Service Network De-energize the Ground Service Network Reactivation of the Thrust Reverser after Maintenance Deactivation of the Thrust Reverser System for Maintenance Fig. 601 Fig. 602
3. __________ Job Set-up Subtask 05-24-50-861-067 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801).
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Subtask 05-24-50-941-082 B. Safety Precautions (1) Make sure that the engine 1(2) shutdown occurred no less than 5 minutes before you do the inspection. (2) Put a warning notice to tell persons not to start the engines. Subtask 05-24-50-010-089 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 05-24-50-865-094 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 05-24-50-040-072 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3100-040-802). Subtask 05-24-50-010-090 F. Get Access (Ref. Fig. 601/TASK 05-24-50-991-034, 602/TASK 05-24-50-991-033) (1) Put an adjustable access platform in position at the pylon leading edge (zones 453, 463).
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(2) Remove the access panels: (a) For the pylon 1 453AL, 453BL, 453CL, 453AR, 453BR, 453CR (b) For the pylon 2 463AL, 463BL, 463CL, 463AR, 463BR, 463CR 4. Procedure _________ Subtask 05-24-50-210-082 A. Inspection. (1) Do a general visual inspection of the lower section of the pylon (zones 453, 463). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-24-50-440-072 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3000-440-804). Subtask 05-24-50-865-095 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
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Subtask 05-24-50-410-082 C. Installation of the Panels. (Ref. Fig. 601/TASK 05-24-50-991-034, 602/TASK 05-24-50-991-033) CAUTION : MAKE SURE THAT THE SPRING RETAINER AT THE FWD EDGE OF THE PANEL _______ (453AL, 453AR, 463AL, 463AR) IS IN THE CORRECT POSITION BELOW THE ADJACENT PANEL. IF NOT, THE PANEL IS NOT CORRECTLY ATTACHED. (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels: (a) For the pylon 2 463AL, 463BL, 463CL, 463AR, 463BR, 463CR (b) For the pylon 1 453AL, 453BL, 453CL, 453AR, 453BR, 453CR Subtask 05-24-50-942-086 D. Close Access (1) Close the protective door of the AC/DC emergency power-center 740VU. (2) Remove the warning notice in the cockpit. (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. Subtask 05-24-50-862-063 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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TASK 05-24-50-200-809-A Zonal Inspection of the Lower and Rear Pylon Fairings 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-454-05 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 notice access platform 2.5 m (8 ft. 2 in.) 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 78-30-00-040-804 78-30-00-440-804 05-24-50-991-034 05-24-50-991-033
Energize the Ground Service Network De-energize the Ground Service Network Deactivation of the Thrust Reverser for Maintenance Reactivation of the Thrust Reverser after Maintenance Fig. 601 Fig. 602
3. __________ Job Set-up Subtask 05-24-50-861-068 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801).
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Subtask 05-24-50-941-083 B. Safety Precautions (1) Make sure that the engine 1(2) shutdown occurred no less than 5 minutes before you do the inspection. (2) Put a warning notice to tell persons not to start the engines. Subtask 05-24-50-010-091 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 05-24-50-865-096 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 05-24-50-040-073 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3000-040-804). Subtask 05-24-50-010-092 F. Get Access (Ref. Fig. 601/TASK 05-24-50-991-034, 602/TASK 05-24-50-991-033) (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the pylon leading edge (zones 454, 464).
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(2) Remove the access panels: (a) For the pylon 1 454BL, 454CL, 454KL, 454EL, 454ML, 454GL, 454HL, 454JL, 454BR, 454KR, 454NR, 454ER. (b) For the pylon 2 464BL, 464CL, 464KL, 464EL, 464ML, 464GL, 464HL, 464JL, 464BR, 464NR, 464KR 464ER. 4. Procedure _________ Subtask 05-24-50-210-083 A. Inspection. (1) Do a general visual inspection of the lower and rear pylon fairings (zones 454, 464). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-24-50-440-073 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3000-440-804). Subtask 05-24-50-865-097 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
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Subtask 05-24-50-410-083 C. Installation of the Panels. (Ref. Fig. 601/TASK 05-24-50-991-034, 602/TASK 05-24-50-991-033) (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels: (a) For the pylon 2 464BL, 464CL, 464KL, 464EL, 464ML, 464GL, 464HL, 464JL, 464BR, 464NR, 464KR, 464ER. (b) For the pylon 1 454BL, 454CL, 454KL, 454EL, 454ML, 454GL, 454HL, 454JL, 454BR, 454NR, 454KR, 454ER. Subtask 05-24-50-942-087 D. Close Access (1) Close the protective door of the AC/DC emergency power-center 740VU. (2) Close the access door 811. Subtask 05-24-50-862-064 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801). (2) Remove all the fixtures, tools, test and support equipment used during this procedure.
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TASK 05-24-50-200-810-A Zonal Inspection of the Lower and Rear Pylon Fairings 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-454-06 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 notice access platform 2.5 m (8 ft. 2 in.) 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 78-30-00-040-804 78-30-00-440-804 05-24-50-991-034 05-24-50-991-033
Energize the Ground Service Network De-energize the Ground Service Network Deactivation of the Thrust Reverser for Maintenance Reactivation of the Thrust Reverser after Maintenance Fig. 601 Fig. 602
3. __________ Job Set-up Subtask 05-24-50-861-069 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801).
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Subtask 05-24-50-941-084 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred no less than 5 minutes before you do the inspection. (2) Put a warning notice to tell persons not to start the engines. Subtask 05-24-50-010-093 C. Get Access to the Avionics Compartment (1) Put an 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 05-24-50-865-098 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 05-24-50-040-074 E. Deactivation of the Thrust Reverser (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3000-040-804). Subtask 05-24-50-010-094-A F. Get Access (Ref. Fig. 601/TASK 05-24-50-991-034, 602/TASK 05-24-50-991-033) (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the aft side of the engine pylon (zones 454 and 464).
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(2) Remove the access panels:
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(a) For pylon 1: 454AL, 454BL, 454CL, 454KL, 454EL, 454ML, 454GL, 454HL, 454JL, 454BR, 454NR, 454KR, 454ER, 454MR, 454GR, 454HR.
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(b) For pylon 2: 464AL, 464BL, 464CL, 464KL, 464EL, 464ML, 464GL, 464HL, 464JL, 464BR, 464NR, 464KR, 464ER, 464MR, 464GR, 464HR. 4. Procedure _________ Subtask 05-24-50-210-084 A. Inspection (1) Do a general visual inspection of the lower and aft pylon fairings (zones 454 and 464). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-24-50-440-074 A. Reactivation of the Thrust Reverser (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3000-440-804). Subtask 05-24-50-865-099 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
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Subtask 05-24-50-410-084-A C. Installation of the Panels (Ref. Fig. 601/TASK 05-24-50-991-034, 602/TASK 05-24-50-991-033) (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels:
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(a) For pylon 2: 464AL, 464BL, 464CL, 464KL, 464EL, 464ML, 464GL, 464HL, 464JL, 464BR, 464NR, 464KR, 464ER, 464MR, 464GR, 464HR.
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(b) For pylon 1: 454AL, 454BL, 454CL, 454KL, 454EL, 454ML, 454GL, 454HL, 454JL, 454BR, 454NR, 454KR, 454ER, 454MR, 454GR, 454HR. Subtask 05-24-50-942-088 D. Close Access (1) Close the protective door of the AC/DC emergency power-center 740VU. (2) Close the access door 811. Subtask 05-24-50-862-065 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801). (2) Remove all the fixtures, tools, test and support equipment used during this procedure.
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ZONAL INSPECTION : ENGINE PYLON - INSPECTION/CHECK __________________________________________________ TASK 05-24-50-200-806-B Zonal Inspection of the Pylon Leading Edge 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-451-02 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) warning notice access platform 2.5 m (8 ft. 2 in.) adjustable access platform 4.60 m (15 ft. 1 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 78-31-00-040-805 78-31-00-440-805 05-24-50-991-035 05-24-50-991-036
Energize the Ground Service Network De-energize the Ground Service Network Deactivation of the Thrust Reverser for Maintenance Activation of the Thrust Reverser after Maintenance Fig. 601 Fig. 602
3. __________ Job Set-up Subtask 05-24-50-861-071 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801).
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Subtask 05-24-50-941-086 B. Safety Precautions (1) Make sure that the engine 1(2) shutdown occurred no less than 5 minutes before you do the inspection. (2) Put a warning notice in the cockpit to tell persons not to start the engines. Subtask 05-24-50-010-096 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 05-24-50-865-102 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 05-24-50-040-076 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3100-040-805).
EFF : 701-749, 05-24-50 Page 602 Config-3 Jul 01/04 SROS
Subtask 05-24-50-010-097 F. Get Access (Ref. Fig. 601/TASK 05-24-50-991-035, 602/TASK 05-24-50-991-036) (1) Put an adjustable access platform in position at the pylon leading edge (zones 451, 461). (2) Remove the access panels: (a) For the pylon 1 451AL, 451BL, 451CL, 451DL, 451EL, 451BR, 451CR, 451DR (b) For the pylon 2 461AL, 461BL, 461CL, 461DL, 461EL, 461BR, 461CR, 461DR 4. Procedure _________ Subtask 05-24-50-210-086 A. Inspection. (1) Do a general visual inspection of the pylon leading edge (zones 451, 461). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-24-50-440-076 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser serviceable (Ref. TASK 78-31-00440-805).
EFF : 701-749, 05-24-50 Page 603 Config-3 Jul 01/04 SROS
Access Door/ Panels, Engine 1 Pylon Figure 601/TASK 05-24-50-991-035 EFF : 701-749, 05-24-50 Page 604 Config-3 Jul 01/04 SROS
Access Door/ Panels, Engine 2 Pylon Figure 602/TASK 05-24-50-991-036 EFF : 701-749, 05-24-50 Page 605 Config-3 Jul 01/04 SROS
Subtask 05-24-50-865-103 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 05-24-50-410-086 C. Installation of the Panels. (Ref. Fig. 601/TASK 05-24-50-991-035, 602/TASK 05-24-50-991-036) (1) Make sure that the work area is clean and clear of tools and other items. (2) Close Access (3) Install the access panels: (a) For the pylon 2 461AL, 461BL, 461CL, 461DL, 461EL, 461BR, 461CR, 461DR (b) For the pylon 1 451AL, 451BL, 451CL, 451DL, 451EL, 451BR, 451CR, 451DR Subtask 05-24-50-942-089 D. Close Access (1) Close the protective door of the AC/DC emergency power-center 740VU. (2) Remove the warning notice in the cockpit. (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.
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Subtask 05-24-50-862-067 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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TASK 05-24-50-200-802-A Zonal Inspection of the Upper Forward of the Pylon 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-452-01 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) 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 54-52-11-000-809 54-52-11-400-809 78-31-00-040-805 78-31-00-440-805
Energize the Ground Service Network De-energize the Ground Service Network Removal of the Access Panels (RIBJ8 to RIB8A) Installation of the Access Panels (RIBJ8 to RIB8A) Deactivation of the Thrust Reverser for Maintenance Activation of the Thrust Reverser after Maintenance
3. __________ Job Set-up Subtask 05-24-50-861-070 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 05-24-50-941-085 B. Safety Precautions (1) Put a WARNING NOTICE to tell persons not to start the engines.
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Subtask 05-24-50-865-100 C. Get access to the avionics compartment. Then 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 05-24-50-040-075 D. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3100-040-805). Subtask 05-24-50-010-095 E. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the pylon leading edge (zones 452, 462). (2) Remove the access panels (Ref. TASK 54-52-11-000-809): (a) For the pylon 1 452AL, 452BL, 452CL 452BR, 452CR. (b) For the pylon 2 462AL, 462BL, 462CL 462BR, 462CR.
EFF : 701-749, 05-24-50 Page 609 Config-3 Jul 01/04 SROS
4. Procedure _________ Subtask 05-24-50-210-085 A. Inspection. (1) Do a general visual inspection of the upper forward section of the pylon (zones 452, 462). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-24-50-440-075 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3100-440-805). Subtask 05-24-50-865-101 B. Get access to the avionics compartment. Then 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 05-24-50-410-085 C. Installation of the Panels. CAUTION : WHEN YOU INSTALL THE ACCESS PANELS 452AL AND 462AL, MAKE SURE _______ THAT THE OVERPRESSURE DOOR IS CLOSED CORRECTLY. IF THE OVERPRESSURE DOOR IS NOT CLOSED, A FLOW OF HOT AIR CAN CAUSE A BLEED OVERHEAT DETECTION. (1) Make sure that the work area is clean and clear of tools and other items.
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(2) Install the access panels (Ref. TASK 54-52-11-400-809): (a) For the pylon 2 462AL, 462BL, 462CL 462BR, 462CR . (b) For the pylon 1 452AL, 452BL, 452CL 452BR, 452CR. Subtask 05-24-50-862-066 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 all the fixtures, tools, test and support equipment used during this procedure.
EFF : 701-749, 05-24-50 Page 611 Config-3 Jul 01/04 SROS
TASK 05-24-50-200-808-B Zonal Inspection of the Lower of the Pylon 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-453-01 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 notice access platform 2.5 m (8 ft. 2 in.) adjustable access platform 4.60 m (15 ft. 1 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 78-31-00-040-805 78-31-00-440-805 05-24-50-991-035 05-24-50-991-036
Energize the Ground Service Network De-energize the Ground Service Network Deactivation of the Thrust Reverser for Maintenance Activation of the Thrust Reverser after Maintenance Fig. 601 Fig. 602
3. __________ Job Set-up Subtask 05-24-50-861-072 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801).
EFF : 701-749, 05-24-50 Page 612 Config-3 Jul 01/04 SROS
Subtask 05-24-50-941-087 B. Safety Precautions (1) Make sure that the engine 1(2) shutdown occurred no less than 5 minutes before you do the inspection. (2) Put a warning notice to tell persons not to start the engines. Subtask 05-24-50-010-098 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 05-24-50-865-104 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 05-24-50-040-077 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3100-040-805). Subtask 05-24-50-010-099 F. Get Access (Ref. Fig. 601/TASK 05-24-50-991-035, 602/TASK 05-24-50-991-036) (1) Put an adjustable access platform in position at the pylon leading edge (zones 453, 463).
EFF : 701-749, 05-24-50 Page 613 Config-3 Jul 01/04 SROS
(2) Remove the access panels: (a) For the pylon 1 453BL, 453CL, 453BR, 453CR (b) For the pylon 2 463BL, 463CL, 463BR, 463CR 4. Procedure _________ Subtask 05-24-50-210-087 A. Inspection. (1) Do a general visual inspection of the lower section of the pylon (zones 453, 463). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-24-50-440-077 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3100-440-805). Subtask 05-24-50-865-105 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 05-24-50-410-087 C. Installation of the Panels. (Ref. Fig. 601/TASK 05-24-50-991-035, 602/TASK 05-24-50-991-036) (1) Make sure that the work area is clean and clear of tools and other items.
EFF : 701-749, 05-24-50 Page 614 Config-3 Jul 01/04 SROS
(2) Install the access panels: (a) For the pylon 2 463BL, 463CL, 463BR, 463CR (b) For the pylon 1 453BL, 453CL, 463BR, 453CR Subtask 05-24-50-942-090 D. Close Access (1) Close the protective door of the AC/DC emergency power-center 740VU. (2) Remove the warning notice in the cockpit. (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. Subtask 05-24-50-862-068 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : 701-749, 05-24-50 Page 615 Config-3 Jul 01/04 SROS
TASK 05-24-50-200-809-B Zonal Inspection of the Lower and Rear Pylon Fairings 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-454-05 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 notice access platform 2.5 m (8 ft. 2 in.) 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 78-31-00-040-805 78-31-00-440-805 05-24-50-991-035 05-24-50-991-036
Energize the Ground Service Network De-energize the Ground Service Network Deactivation of the Thrust Reverser for Maintenance Activation of the Thrust Reverser after Maintenance Fig. 601 Fig. 602
3. __________ Job Set-up Subtask 05-24-50-861-073 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801).
EFF : 701-749, 05-24-50 Page 616 Config-3 Jul 01/04 SROS
Subtask 05-24-50-941-088 B. Safety Precautions (1) Make sure that the engine 1(2) shutdown occurred no less than 5 minutes before you do the inspection. (2) Put a warning notice to tell persons not to start the engines. Subtask 05-24-50-010-100 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 05-24-50-865-106 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 05-24-50-040-078 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3100-040-805). Subtask 05-24-50-010-101 F. Get Access (Ref. Fig. 601/TASK 05-24-50-991-035, 602/TASK 05-24-50-991-036) (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the pylon leading edge (zones 454, 464).
EFF : 701-749, 05-24-50 Page 617 Config-3 Jul 01/04 SROS
(2) Remove the access panels: (a) For the pylon 1 454BL, 454CL, 454KL, 454EL, 454ML, 454GL, 454HL, 454JL, 454BR, 454NR, 454KR, 454ER. (b) For the pylon 2 464BL, 464CL, 464KL, 464EL, 464ML, 464GL, 464HL, 464JL, 464BR, 464NR, 464KR, 464ER. 4. Procedure _________ Subtask 05-24-50-210-088 A. Inspection. (1) Do a general visual inspection of the lower and rear pylon fairings (zones 454, 464). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-24-50-440-078 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3100-440-805). Subtask 05-24-50-865-107 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
EFF : 701-749, 05-24-50 Page 618 Config-3 Jul 01/04 SROS
R R R
Subtask 05-24-50-410-088 C. Installation of the Panels. (Ref. Fig. 601/TASK 05-24-50-991-035, 602/TASK 05-24-50-991-036)
R R
(1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Install the access panels:
R R
(a) For the pylon 2 464BL, 464CL, 464KL, 464EL, 464ML, 464GL, 464HL, 464JL, 464BR, 464NR, 464KR, 464ER.
R R
(b) For the pylon 1 454BL, 454CL, 454KL, 454EL, 454ML, 454GL, 454HL, 454JL, 454BR, 454NR, 454KR, 454ER. Subtask 05-24-50-942-091
R
D. Close Access (1) Close the protective door of the AC/DC emergency power-center 740VU. (2) Close the access door 811. Subtask 05-24-50-862-069
R
E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801). (2) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : 701-749, 05-24-50 Page 619 Config-3 Jan 01/05 SROS
TASK 05-24-50-200-810-B Zonal Inspection of the Lower and Rear Pylon Fairings 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-454-06 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 notice access platform 2.5 m (8 ft. 2 in.) 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 78-31-00-040-805 78-31-00-440-805 05-24-50-991-035 05-24-50-991-036
Energize the Ground Service Network De-energize the Ground Service Network Deactivation of the Thrust Reverser for Maintenance Activation of the Thrust Reverser after Maintenance Fig. 601 Fig. 602
3. __________ Job Set-up Subtask 05-24-50-861-074 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801).
EFF : 701-749, 05-24-50 Page 620 Config-3 Jul 01/04 SROS
Subtask 05-24-50-941-089 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred no less than 5 minutes before you do the inspection. (2) Put a warning notice to tell persons not to start the engines. Subtask 05-24-50-010-102 R
C. Get Access to the Avionics Compartment
R
(1) Put an 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 05-24-50-865-108 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 05-24-50-040-079
R
E. Deactivation of the Thrust Reverser (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3100-040-805).
R R R
Subtask 05-24-50-010-103-A F. Get Access (Ref. Fig. 601/TASK 05-24-50-991-035, 602/TASK 05-24-50-991-036)
R R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the aft side of the engine pylon (zones 454 and 464).
EFF : 701-749, 05-24-50 Page 621 Config-3 Apr 01/05 SROS
R
(2) Remove the access panels:
R R R
(a) For pylon 1: 454AL, 454BL, 454CL, 454KL, 454EL, 454ML, 454GL, 454HL, 454JL, 454BR, 454NR, 454KR, 454ER, 454MR, 454GR, 454HR.
R R R
(b) For pylon 2: 464AL, 464BL, 464CL, 464KL, 464EL, 464ML, 464GL, 464HL, 464JL, 464BR, 464NR, 464KR, 464ER, 464MR, 464GR, 464HR. 4. Procedure _________ Subtask 05-24-50-210-089
R
A. Inspection (1) Do a general visual inspection of the lower and aft pylon fairings (zones 454 and 464). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-24-50-440-079
R
A. Reactivation of the Thrust Reverser (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3100-440-805). Subtask 05-24-50-865-109 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
EFF : 701-749, 05-24-50 Page 622 Config-3 Apr 01/05 SROS
R R R
Subtask 05-24-50-410-089-A C. Installation of the Panels (Ref. Fig. 601/TASK 05-24-50-991-035, 602/TASK 05-24-50-991-036)
R R
(1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Install the access panels:
R R R
(a) For pylon 2: 464AL, 464BL, 464CL, 464KL, 464EL, 464ML, 464GL, 464HL, 464JL, 464BR, 464NR, 464KR, 464ER, 464MR, 464GR, 464HR.
R R R
(b) For pylon 1: 454AL, 454BL, 454CL, 454KL, 454EL, 454ML, 454GL, 454HL, 454JL, 454BR, 454NR, 454KR, 454ER, 454MR, 454GR, 454HR. Subtask 05-24-50-942-092 D. Close Access (1) Close the protective door of the AC/DC emergency power-center 740VU. (2) Close the access door 811. Subtask 05-24-50-862-070 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801). (2) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : 701-749, 05-24-50 Page 623 Config-3 Apr 01/05 SROS
ZONAL INSPECTION : WING - INSPECTION/CHECK __________________________________________ TASK 05-25-00-200-801 Zonal Inspection as far as visible from the Ground of the Left and Right Wings (zone 500 and 600). 1. __________________ Reason for the Job R
NOTE : This task can contribute to fuel savings. ____ 2. ______________________ Job Set-up Information Not Applicable 3. __________ Job Set-up Subtask 05-25-00-869-050 A. Not applicable. 4. Procedure _________ Subtask 05-25-00-210-050 A. Do a general visual inspection of the left and right wing (zone 500 and 600) from the ground.
EFF : ALL 05-25-00 SROS
Page 601 Jan 01/07
TASK 05-25-00-200-802 Zonal Inspection of Wing Lower Surface Including Slats and Flaps 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: ZL-500-01 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
1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------27-50-00-866-801 27-50-00-866-801 27-50-00-866-802 27-50-00-866-802
Extension of the Flaps/Slats on the Ground Extension of the Flaps/Slats on the Ground (RR-Engines) Retraction of the Flaps/Slats on the Ground Retraction of the Flaps/Slats on the Ground (RR-Engines)
EFF : ALL 05-25-00 SROS
Page 602 Jan 01/07
3. __________ Job Set-up **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-25-00-866-050 A. Aircraft Maintenance Configuration R
(1) Fully extend the flaps/slats (Ref. TASK 27-50-00-866-801). **ON A/C 701-749, Subtask 05-25-00-866-050-A A. Aircraft Maintenance Configuration (1) Fully extend the flaps/slats (Ref. TASK 27-50-00-866-801). **ON A/C ALL Subtask 05-25-00-941-051 B. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-25-00-010-050 C. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the left and right lower wing surface. 4. Procedure _________ Subtask 05-25-00-210-051 A. Do a general visual inspection of the wing lower surface. This includes the slats and flaps (Zones 500 and 600). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see.
EFF : ALL 05-25-00 SROS
Page 603 Jan 01/07
5. Close-up ________ R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-25-00-942-050 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) Retract the flaps/slats (Ref. TASK 27-50-00-866-802). (3) Remove all the fixtures, tools, test and support equipment used during this procedure. **ON A/C 701-749, Subtask 05-25-00-942-050-A 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) Retract the flaps/slats (Ref. TASK 27-50-00-866-802). (3) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-25-00 SROS
Page 604 Jul 01/05
**ON A/C ALL TASK 05-25-00-200-803 Zonal Inspection of Wing Upper Surface (Including Slats, Flaps and Spoilers) 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: ZL-500-02 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
1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------27-50-00-866-801 27-50-00-866-801 27-50-00-866-802 27-50-00-866-802 27-60-00-866-801 27-60-00-866-802
Extension of the Flaps/Slats on the Ground Extension of the Flaps/Slats on the Ground (RR-Engines) Retraction of the Flaps/Slats on the Ground Retraction of the Flaps/Slats on the Ground (RR-Engines) Extension of the Spoilers for Maintenance Retraction of the Spoilers after Maintenance
EFF : ALL 05-25-00 SROS
Page 605 Jan 01/07
3. __________ Job Set-up **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-25-00-866-052 A. Aircraft Maintenance Configuration (1) Extend the spoilers (Ref. TASK 27-60-00-866-801). (2) Fully extend the flaps/slats (Ref. TASK 27-50-00-866-801). **ON A/C 701-749, Subtask 05-25-00-866-052-A A. Aircraft Maintenance Configuration R
(1) Extend the spoilers (Ref. TASK 27-60-00-866-801). (2) Fully extend the flaps/slats (Ref. TASK 27-50-00-866-801). **ON A/C ALL Subtask 05-25-00-941-052 B. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-25-00-010-051 C. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the left and right upper wing surface.
EFF : ALL 05-25-00 SROS
Page 606 Jan 01/07
4. Procedure _________ Subtask 05-25-00-210-052 A. Do a general visual inspection of the wing upper surface. This includes the slats, flaps and spoilers (zones 500 and 600). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-25-00-942-051 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) Retract the flaps/slats (Ref. TASK 27-50-00-866-802). (3) Retract the spoilers (Ref. TASK 27-60-00-866-802). (4) Remove all the fixtures, tools, test and support equipment used during this procedure. **ON A/C 701-749, Subtask 05-25-00-942-051-A 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) Retract the flaps/slats (Ref. TASK 27-50-00-866-802). (3) Retract the spoilers (Ref. TASK 27-60-00-866-802). (4) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-25-00 SROS
Page 607 Jul 01/05
ZONAL INSPECTION : WING FIXED LEADING EDGE - INSPECTION/CHECK _____________________________________________________________ TASK 05-25-20-200-801 R R
Zonal Inspection of Inboard Fixed Leading Edge Structure 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: ZL-521-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------27-80-00-866-801 27-80-00-866-802
Extension of the Slats on the Ground Retraction of the Slats on the Ground
R 3. __________ Job Set-up Subtask 05-25-20-866-050 A. Aircraft Maintenance Configuration R R
(1) Fully extend the slats (Ref. TASK 27-80-00-866-801).
EFF : ALL 05-25-20 SROS
Page 601 Jan 01/04
Subtask 05-25-20-941-050 B. Safety Precautions R R R
(1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. 4. Procedure _________ Subtask 05-25-20-210-050
R
A. Do a general visual inspection of the inboard fixed leading-edge structure (Zones 521 and 621). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, wiring) are attached correctly. 5. Close-up ________
R Subtask 05-25-20-866-051 R R
A. Put the Aircraft back to its Initial Configuration
R
(1) Retract the slats (Ref. TASK 27-80-00-866-802). Subtask 05-25-20-942-050
R R R
B. Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-25-20 SROS
Page 602 Jan 01/04
TASK 05-25-20-200-802 R
Zonal Inspection of Center Fixed Leading Edge Structure 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: ZL-522-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R
No specific No specific
1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R
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
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
3. __________ Job Set-up Subtask 05-25-20-866-052 A. Aircraft Maintenance Configuration (1) Fully extend the slats (Ref. TASK 27-80-00-866-801).
EFF : ALL 05-25-20 SROS
Page 603 Jan 01/04
Subtask 05-25-20-941-051 B. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-25-20-010-051-B C. Get Access (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the slats (Zones 522 and 622). (2) Remove the access panels: R
(a) For the left side: 522BB, 522CB, 522EB, 522HB, 522JB, 522LB, 522NB, 522TB, 522UB, 522AT (Ref. TASK 57-42-37-000-801), 522AB (Ref. TASK 57-41-37-000-801).
R
(b) For the right side: 622BB, 622CB, 622EB, 622HB, 622JB, 622LB, 622NB, 622TB, 622UB, 622AT, (Ref. TASK 57-42-37-000-801), 622AB (Ref. TASK 57-41-37-000-801). 4. Procedure _________ Subtask 05-25-20-210-051 A. Do a general visual inspection of the center fixed leading-edge structure (Zones 522 and 622). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, wiring) are attached correctly.
EFF : ALL 05-25-20 SROS
Page 604 Jan 01/07
5. Close-up ________ Subtask 05-25-20-410-051-B A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels: R
(a) For the left side: 522BB, 522CB, 522EB, 522HB, 522JB, 522LB, 522NB, 522TB, 522UB, 522AT (Ref. TASK 57-42-37-400-801), 522AB (Ref. TASK 57-41-37-400-801).
R
(b) For the right side: 622BB, 622CB, 622EB, 622HB, 622JB, 622LB, 622NB, 622TB, 622UB, 622AT, (Ref. TASK 57-42-37-400-801), 622AB (Ref. TASK 57-41-37-400-801). Subtask 05-25-20-866-053 B. 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) Retract the slats (Ref. TASK 27-80-00-866-802). Subtask 05-25-20-942-051 C. Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-25-20 SROS
Page 605 Jan 01/07
TASK 05-25-20-200-803 Zonal Inspection of Outer Fixed Leading Edge Structure 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: ZL-523-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific No specific
1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R
27-80-00-866-801 27-80-00-866-802 57-42-37-000-801 57-42-37-400-801
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
3. __________ Job Set-up Subtask 05-25-20-866-054 A. Aircraft Maintenance Configuration R
(1) Fully extend the slats (Ref. TASK 27-80-00-866-801).
EFF : ALL 05-25-20 SROS
Page 606 Apr 01/04
Subtask 05-25-20-941-052 B. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-25-20-010-052-A C. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the slats (Zones 523 and 623). (2) Remove the access panels: R R
(a) For the left side: 523CB, 523EB, 523GB, 523JB, 523LB, 523NB (Ref. TASK 57-42-37-000-801).
R R
(b) For the right side: 623CB, 623EB, 623GB, 623JB, 623LB, 623NB (Ref. TASK 57-42-37-000-801). 4. Procedure _________ Subtask 05-25-20-210-052 A. Do a general visual inspection of the outer fixed leading edge structure (Zones 523 and 623). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, wiring) are attached correctly. 5. Close-up ________ Subtask 05-25-20-410-052-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:
R R
(a) For the left side: 523CB, 523EB, 523GB, 523JB, 523LB, 523NB (Ref. TASK 57-42-37-400-801).
EFF : ALL 05-25-20 SROS
Page 607 Apr 01/05
R R
(b) For the right side: 623CB, 623EB, 623GB, 623JB, 623LB, 623NB (Ref. TASK 57-42-37-400-801). Subtask 05-25-20-942-052 B. Put the Aircraft back to its Initial Configuration (1) Retract the slats (Ref. TASK 27-80-00-866-802). (2) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-25-20 SROS
Page 608 Apr 01/05
ZONAL INSPECTION : WING FLAP TRACK FAIRINGS AND WING TIP - INSPECTION/CHECK ___________________________________________________________________________ TASK 05-25-30-200-801 Zonal Inspection of Flap Tracks and Flap Track Fairings (Including RAT Attachment Points, as far as visible) 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: ZL-531-01 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
1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------27-50-00-866-801 27-50-00-866-802 57-56-11-000-801 57-56-11-000-802 57-56-11-000-803 57-56-11-000-804 57-56-11-400-801 57-56-11-400-802 57-56-11-400-803
Extension of the Flaps on the Ground Retraction of the Flaps on the Ground Removal of the Movable Flap Track Fairing No. 2 Removal of the Movable Flap Track Fairing No. 3 Removal of the Movable Flap Track Fairing No. 4 Removal of the Movable Flap Track Fairing No. 5 Installation of Movable Flap Track Fairing No. 2 Installation of Movable Flap Track Fairing No. 3 Installation of the Movable Flap Track Fairing No. 4
EFF : ALL 05-25-30 SROS
Page 601 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------57-56-11-400-804
Installation of the Movable Flap Track Fairing No. 5
3. __________ Job Set-up Subtask 05-25-30-866-050 A. Aircraft Maintenance Configuration R
(1) Fully extend the flaps (Ref. TASK 27-50-00-866-801). Subtask 05-25-30-941-050 B. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-25-30-010-050 C. Get Access
R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at zone 530(630). (2) Remove the flap track fairings 531CB, 532CB, 533CB, 534CB, 631CB, 632CB, 633CB, 634CB (Ref. TASK 57-56-11-000-801), (Ref. TASK 57-5611-000-802), (Ref. TASK 57-56-11-000-803), (Ref. TASK 57-56-11-000804). 4. Procedure _________ Subtask 05-25-30-210-050
R
A. Do a general visual inspection of all the flap tracks and flap track fairings. This includes the RAT attachment points, as far as you can see. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations are attached correctly.
EFF : ALL 05-25-30 SROS
Page 602 Jan 01/07
5. Close-up ________ Subtask 05-25-30-410-050 A. Close Access (1) Install the flap track fairings 531CB, 532CB, 533CB, 534CB, 631CB, 632CB, 633CB, 634CB (Ref. TASK 57-56-11-400-801), (Ref. TASK 57-5611-400-802), (Ref. TASK 57-56-11-400-803), (Ref. TASK 57-56-11-400804). Subtask 05-25-30-866-051 B. Put the Aircraft back to its Initial Configuration (1) Fully retract the flaps (Ref. TASK 27-50-00-866-802). Subtask 05-25-30-942-051 C. Remove all the fixtures, tools, test and support equipment used during this procedure. (1) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-25-30 R SROS
Page 603 Jan 01/07
TASK 05-25-30-200-802 Zonal inspection of Flap Tracks and Flap Track Fairings 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: ZL-531-02 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
1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------27-50-00-866-801 27-50-00-866-802 57-56-11-000-801 57-56-11-000-802 57-56-11-000-803 57-56-11-000-804 57-56-11-000-805 57-56-11-000-806 57-56-11-400-801
Extension of the Flaps on the Ground Retraction of the Flaps on the Ground Removal of the Movable Flap Track Fairing No. 2 Removal of the Movable Flap Track Fairing No. 3 Removal of the Movable Flap Track Fairing No. 4 Removal of the Movable Flap Track Fairing No. 5 Removal of the Fixed Flap Track Fairings Nos. 2 thru 5 (without Fixed Flap Track Fairing No 4 on the Right Side) Removal of the Fixed Flap Track Fairing No. 4 on the Right Side Installation of Movable Flap Track Fairing No. 2
EFF : ALL 05-25-30 SROS
Page 604 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------57-56-11-400-802 57-56-11-400-803 57-56-11-400-804 57-56-11-400-805 57-56-11-400-806
Installation of Installation of Installation of Installation of thru 5 (without Right Side) Installation of the Right Side
Movable Flap Track Fairing No. 3 the Movable Flap Track Fairing No. 4 the Movable Flap Track Fairing No. 5 the Fixed Flap Track Fairings Nos 2 Fixed Flap Track Fairing No. 4 on the the Fixed Flap Track Fairing No. 4 on
3. __________ Job Set-up Subtask 05-25-30-866-052 A. Aircraft Maintenance Configuration R
(1) Fully extend the flaps (Ref. TASK 27-50-00-866-801). Subtask 05-25-30-941-051 B. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-25-30-010-051 C. Get Access (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the flap track fairings. (2) Remove the movable flap track fairings 531CB, 532CB, 533CB, 534CB, 631CB, 632CB, 633CB, 634CB (Ref. TASK 57-56-11-000-801), (Ref. TASK 57-56-11-000-802), (Ref. TASK 57-56-11-000-803), (Ref. TASK 57-56-11000-804). (3) Remove the fixed flap track fairings 531AB, 532AB, 533AB, 534AB, 631AB, 632AB, 633AB, 634AB (Ref. TASK 57-56-11-000-805), (Ref. TASK 57-56-11-000-806).
EFF : ALL 05-25-30 SROS
Page 605 Jan 01/07
4. Procedure _________ Subtask 05-25-30-210-051 A. Do a general visual inspection of the flap tracks and the flap track fairings. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations are attached correctly. 5. Close-up ________ Subtask 05-25-30-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the fixed flap track fairings 531AB, 532AB, 533AB, 534AB, 631AB, 632AB, 633AB, 634AB, (Ref. TASK 57-56-11-400-805), (Ref. TASK 57-56-11-400-806). (3) Install the movable flap track fairings 531CB, 532CB, 533CB, 534CB, 631CB, 632CB, 633CB, 634CB (Ref. TASK 57-56-11-400-801), (Ref. TASK 57-56-11-400-802), (Ref. TASK 57-56-11-400-803), (Ref. TASK 57-56-11400-804). Subtask 05-25-30-866-053 B. Put the Aircraft back to its Initial Configuration (1) Fully retract the flaps (Ref. TASK 27-50-00-866-802). Subtask 05-25-30-942-052 C. Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-25-30 R SROS
Page 606 Jan 01/07
TASK 05-25-30-200-809 Zonal Inspection of Wing Tip. 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: ZL-535-01 R
NOTE : This task can contribute to fuel saving. ____ 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------57-37-11-000-801 57-37-11-400-801
Removal of the Winglet Access Panels Installation of the Winglet Access Panels
EFF : ALL 05-25-30 SROS
Page 607 Jan 01/07
3. __________ Job Set-up Subtask 05-25-30-010-058 A. Get Access (1) Put an ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE in position at the wing tip (zones 535 and 635). (2) For the left side: Remove the access panels 535AB, 535BB (Ref. TASK 57-37-11-000-801).
R
(3) For the right side: Remove the access panels 635AB, 635BB (Ref. TASK 57-37-11-000-801). 4. Procedure _________ Subtask 05-25-30-210-058 A. Do a general visual inspection of the wing tip (zones 535 and 635). Make sure that: - there is no damage (corrosion or cracks) on all the parts of the components and the structure you can see - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-25-30-410-058 A. Close Access (1) For the left side Install the access panels 535AB, 535BB (Ref. TASK 57-37-11-400-801). (2) For the right side Install the access panels 635AB, 635BB (Ref. TASK 57-37-11-400-801). Subtask 05-25-30-942-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-25-30 SROS
Page 608 Jan 01/07
ZONAL INSPECTION : WING FUEL TANK - INSPECTION/CHECK ____________________________________________________ TASK 05-25-40-200-801 R
Zonal Inspection of Inner Fuel Tank. 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 : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND DAMAGE. _______ 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 Refer to the MPD TASK: ZL-541-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
safety barriers warning notices 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
EFF : ALL 05-25-40 SROS
Page 601 Jul 01/04
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-11-28-650-803 28-00-00-610-801 28-10-00-910-802 28-25-00-650-801 57-27-11-000-801 57-27-11-400-801
Pressure Refuel with Automatic Control from the Panel 990VU Fuel Safety Procedures Access to Fuel Tanks and Work Areas Pressure Defuel Procedure Removal of the Underwing Tank Access-Panels Installation of the Underwing Tank Access-Panels
3. __________ Job Set-up Subtask 05-25-40-650-050 R
A. Defuel the tanks (Ref. TASK 28-25-00-650-801). Subtask 05-25-40-941-053 B. Safety Precautions (1) Put the safety barriers in position. (2) Put the warning notices in position: - to tell persons not to operate the fuel system - to tell persons not to refuel the aircraft - to tell persons not to operate the flight controls. Subtask 05-25-40-010-050 C. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the inner fuel tank (zones 541 and 641). (2) Remove the access panels: (a) For the left side: 541AB, 541BB, 541BZ, 541CB, 541CZ (Ref. TASK 57-27-11-000-801). (b) For the right side: 641AB, 641BB, 641BZ, 641CB, 641CZ (Ref. TASK 57-27-11-000-801).
EFF : ALL 05-25-40 SROS
Page 602 Jul 01/04
Subtask 05-25-40-941-050 D. Safety Precautions (1) Obey the fuel safety procedures (Ref. TASK 28-00-00-610-801). (2) Get access to the fuel tank (Ref. TASK 28-10-00-910-802). 4. Procedure _________ Subtask 05-25-40-210-050 R R
A. Do a general visual inspection of the inner fuel tank between rib 1 and rib 7 (zones 541 and 641). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - All the installations (ducting, wiring) are attached correctly. 5. Close-up ________ Subtask 05-25-40-410-050 A. Close Access
R R
(1) Install the access panels:
R R
(a) For the left side: 541AB, 541BB, 541BZ, 541CB, 541CZ (Ref. TASK 57-27-11-400-801).
R R
(b) For the right side: 641AB, 641BB, 641BZ, 641CB, 641CZ (Ref. TASK 57-27-11-400-801). Subtask 05-25-40-650-051 B. Refuel the tanks (Ref. TASK 12-11-28-650-803) Subtask 05-25-40-942-051
R R
C. Put the Aircraft back to its Initial Configuration
R R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-25-40 SROS
Page 603 Jan 01/04
R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-25-40 SROS
Page 604 Jan 01/04
TASK 05-25-40-200-802 R R
Zonal Inspection of Inner Fuel Tank (Rib 1 to Rib 23). 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 : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND DAMAGE. _______ 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 Refer to the MPD TASK: ZL-541-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific No specific No specific
safety barriers warning notices 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
EFF : ALL 05-25-40 SROS
Page 605 Jan 01/04
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-11-28-650-803 28-00-00-610-801 28-10-00-910-802 28-25-00-650-801 57-27-11-000-801 57-27-11-400-801
Pressure Refuel with Automatic Control from the Panel 990VU Fuel Safety Procedures Access to Fuel Tanks and Work Areas Pressure Defuel Procedure Removal of the Underwing Tank Access-Panels Installation of the Underwing Tank Access-Panels
3. __________ Job Set-up Subtask 05-25-40-650-052 R
A. Defuel the tanks (Ref. TASK 28-25-00-650-801) Subtask 05-25-40-941-054 B. Safety Precautions (1) Put the safety barriers in position. (2) Put the warning notices in position: - to tell persons not to operate the fuel system - to tell persons not to refuel the aircraft - to tell persons not to operate the flight controls.
R R
Subtask 05-25-40-010-051 C. Get Access R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the inner fuel tank (zones 541 and 641). (2) Remove the access panels:
R R
(a) For the left side: 541AB, 541BB, 541CB, 541DB, 541EB, 541FB, 541GB, 541HB, 541JB, 541KB, 541LB, 541MB, 541NB, 541PB, 541QB, 541RB, 541SB, 541AZ, 541BZ, 541CZ, 541DZ, 541EZ, 541FZ, 541GZ (Ref. TASK 57-27-11-000-801).
R
EFF : ALL 05-25-40 SROS
Page 606 Jan 01/04
R R
(b) For the right side: 641AB, 641BB, 641CB, 641DB, 641EB, 641FB, 641GB, 641HB, 641JB, 641KB, 641LB, 641MB, 641NB, 641PB, 641QB, 641RB, 641SB, 641AZ, 641BZ, 641CZ, 641DZ, 641EZ, 641FZ, 641GZ (Ref. TASK 57-27-11-000-801).
R
Subtask 05-25-40-941-051 D. Safety Precautions (1) Obey the fuel safety procedures (Ref. TASK 28-00-00-610-801). (2) Get access to the fuel tank (Ref. TASK 28-10-00-910-802). 4. Procedure _________ Subtask 05-25-40-210-051 R R
A. Do a general visual inspection of the inner fuel tank between rib 1 and rib 23 (zones 541 and 641). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (ducting, wiring) are attached correctly. 5. Close-up ________ Subtask 05-25-40-410-051 A. Close Access
R R
(1) Install the access panels:
R R
(a) For the left side: 541AB, 541BB, 541CB, 541DB, 541EB, 541FB, 541GB, 541HB, 541JB, 541KB, 541LB, 541MB, 541NB, 541PB, 541QB, 541RB, 541SB, 541AZ, 541BZ, 541CZ, 541DZ, 541EZ, 541FZ, 541GZ (Ref. TASK 57-27-11-400-801).
R R R
(b) For the right side: 641AB, 641BB, 641CB, 641DB, 641EB, 641FB, 641GB, 641HB, 641JB, 641KB, 641LB, 641MB, 641NB, 641PB, 641QB, 641RB, 641SB, 641AZ, 641BZ, 641CZ, 641DZ, 641EZ, 641FZ, 641GZ (Ref. TASK 57-27-11-400-801).
R
Subtask 05-25-40-650-053 B. Refuel the tanks. (Ref. TASK 12-11-28-650-803)
EFF : ALL 05-25-40 SROS
Page 607 Jan 01/04
Subtask 05-25-40-942-050 R R
C. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-25-40 SROS
Page 608 Jan 01/04
TASK 05-25-40-200-803 Zonal Inspection of Outer Fuel Tank (Rib 23 to Rib 33). 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 : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND DAMAGE. _______ 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 Refer to the MPD TASK: ZL-542-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
safety barriers warning notices 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
EFF : ALL 05-25-40 R SROS
Page 609 Apr 01/05
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-11-28-650-803 28-00-00-610-801 28-10-00-910-802 28-25-00-650-801 57-27-11-000-801 57-27-11-400-801
Pressure Refuel with Automatic Control from the Panel 990VU Fuel Safety Procedures Access to Fuel Tanks and Work Areas Pressure Defuel Procedure Removal of the Underwing Tank Access-Panels Installation of the Underwing Tank Access-Panels
R 3. __________ Job Set-up Subtask 05-25-40-650-054 A. Defuel the tanks (Ref. TASK 28-25-00-650-801) Subtask 05-25-40-941-055 B. Safety Precautions (1) Put the safety barriers in position. (2) Put the warning notices in position: - to tell persons not to operate the fuel system - to tell persons not to refuel the aircraft - to tell persons not to operate the flight controls. Subtask 05-25-40-010-052 C. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the outer fuel tank (zones 542 and 642). (2) Remove the access panels: (a) For the left side: 542AB, 542BB, 542CB, 542DB, 542EB, 542FB, 542GB, 542HB, 542JB, 542KB (Ref. TASK 57-27-11-000-801). R
EFF : ALL 05-25-40 SROS
Page 610 Apr 01/05
(b) For the right side: 642AB, 642BB, 642CB, 642DB, 642EB, 642FB, 642GB, 642HB, 642JB, 642KB (Ref. TASK 57-27-11-000-801). R Subtask 05-25-40-941-052 D. Safety Precautions (1) Obey the fuel safety procedures (Ref. TASK 28-00-00-610-801). (2) Get access to the fuel tank (Ref. TASK 28-10-00-910-802). 4. Procedure _________ Subtask 05-25-40-210-052 A. Do a general inspection of the outer fuel tank from rib 23 to rib 33 (zones 542 and 642). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-25-40-410-052 A. Close Access (1) Install the access panels: (a) For the left side: 542AB, 542BB, 542CB, 542DB, 542EB, 542FB, 542GB, 542HB, 542JB, 542KB (Ref. TASK 57-27-11-400-801). R (b) For the right side: 642AB, 642BB, 642CB, 642DB, 642EB, 642FB, 642GB, 642HB, 642JB, 642KB (Ref. TASK 57-27-11-400-801). R
EFF : ALL 05-25-40 SROS
Page 611 Apr 01/05
Subtask 05-25-40-650-055 B. Refuel the tanks. (Ref. TASK 12-11-28-650-803) Subtask 05-25-40-942-052 C. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-25-40 R SROS
Page 612 Apr 01/05
ZONAL INSPECTION : WING VENT SURGE TANK - INSPECTION/CHECK __________________________________________________________ TASK 05-25-50-200-802 R
Zonal Inspection of Vent Surge Tank WARNING : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND DAMAGE. _______ 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 Refer to the MPD TASK: ZL-550-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific No specific No specific
safety barriers warning notices 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-11-28-650-803 28-00-00-610-801 28-10-00-910-802 28-25-00-650-804 57-27-11-000-801 57-27-11-400-801
Pressure Refuel with Automatic Control from the Panel 990VU Fuel Safety Procedures Access to Fuel Tanks and Work Areas To Defuel One Wing (Inner and Outer Tanks) Only (For Access) Removal of the Underwing Tank Access-Panels Installation of the Underwing Tank Access-Panels
EFF : ALL 05-25-50 SROS
Page 601 Jan 01/04
3. __________ Job Set-up Subtask 05-25-50-650-050 R
A. Defuel the wings (Ref. TASK 28-25-00-650-804). Subtask 05-25-50-941-052 B. Safety Precautions (1) Put the safety barriers in position. (2) Put the warning notices in position: - to tell persons not to operate the fuel system - to tell persons not to refuel the aircraft - to tell persons not to operate the flight controls.
R R
Subtask 05-25-50-010-051 C. Get Access R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the vent surge tank (zones 550 and 650). (2) Remove the access panels:
R R
(a) For the left side: 550AB, 550BB, 550CB, 550DB, 550EB, 550FB (Ref. TASK 57-27-11-000-801).
R R
(b) For the right side: 650AB, 650BB, 650CB, 650DB, 650EB, 650FB (Ref. TASK 57-27-11-000-801). Subtask 05-25-50-941-053 D. Safety Precautions (1) Obey the fuel safety procedures (Ref. TASK 28-00-00-610-801). (2) Get access to the vent surge tank (Ref. TASK 28-10-00-910-802)
EFF : ALL 05-25-50 SROS
Page 602 Jan 01/04
4. Procedure _________ Subtask 05-25-50-210-051 A. Do a general visual inspection of the vent surge tank (zones 550 and 650). Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-25-50-410-051 A. Close Access R R
(1) Install the access panels:
R
(a) For the left side: 550AB, 550BB, 550CB, 550DB, 550EB, 550FB (Ref. TASK 57-27-11-400-801).
R
(b) For the right side: 650AB, 650BB, 650CB, 650DB, 650EB, 650FB (Ref. TASK 57-27-11-400-801).
R Subtask 05-25-50-650-051 B. Refuel the tanks. (Ref. TASK 12-11-28-650-803) Subtask 05-25-50-942-050 R R
C. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-25-50 SROS
Page 603 Jan 01/04
________________________________________________________________________ ZONAL INSPECTION : AFT SECTION OF WING AND TRAILING EDGE FIXED STRUCTURE ________________ INSPECTION/CHECK TASK 05-25-70-200-803 Zonal Inspection of Main Landing Gear Well. 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 Refer to the MPD TASK: ZL-571-01 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 ------------------------------------------------------------------------------32-12-00-010-801 32-12-00-410-801
Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-25-70-010-051 A. Get Access R
(1) Open the main landing-gear doors 734, 744 (Ref. TASK 32-12-00-010801).
R R R
(2) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the main landing-gear well (zones 571 and 671).
EFF : ALL 05-25-70 SROS
Page 601 Jan 01/06
4. Procedure _________ Subtask 05-25-70-210-051 R R
A. Do a general visual inspection of the main landing-gear well (zones 571 and 671). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-25-70-410-051 A. Close Access
R R
(1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Close the main landing-gear doors 734 and 744 (Ref. TASK 32-12-00410-801). Subtask 05-25-70-860-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R
EFF : ALL 05-25-70 SROS
Page 602 Jan 01/06
TASK 05-25-70-200-804 R
Zonal Inspection of Shroud Box. 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 Refer to the MPD TASK: ZL-572-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific No specific
warning notices 1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
3. __________ Job Set-up R
Subtask 05-25-70-941-050
R
A. Safety Precautions
R R
(1) Put warning notices in the cockpit to tell persons not to operate the flight controls.
EFF : ALL 05-25-70 SROS
Page 603 Jan 01/04
R
**ON A/C 001-001, 201-202, 251-252, 401-449, Subtask 05-25-70-010-052-A B. Get Access (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the shroud box (zones 572 and 672). (2) Remove the access panels:
R
(a) For the left side: 572AB.
R
(b) For the right side: 672AB.
R
**ON A/C 002-049, 203-249, 255-299, 301-399, 451-499, 701-749,
R
Subtask 05-25-70-010-052
R
B. Get Access
R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the shroud box (zones 572 and 672).
R
(2) Remove the access panels:
R
(a) For the left side: 572BB, 572CB and 572EB.
R
(b) For the right side: 672BB, 672CB and 672EB.
R
**ON A/C ALL 4. Procedure _________ Subtask 05-25-70-210-052 A. Do a general visual inspection of the shroud box (zones 572 and 672). Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see.
EFF : ALL 05-25-70 SROS
Page 604 Jul 01/06
5. Close-up ________ R
**ON A/C 001-001, 201-202, 251-252, 401-449, Subtask 05-25-70-410-052-A A. Close Access (1) Install the access panels:
R
(a) For the left side: 572AB.
R
(b) For the right side: 672AB.
R
**ON A/C 002-049, 203-249, 255-299, 301-399, 451-499, 701-749,
R
Subtask 05-25-70-410-052
R
A. Close Access
R
(1) Install the access panels:
R
(a) For the left side: 572BB, 572CB and 572EB.
R
(b) For the right side: 672BB, 672CB and 672EB.
R
**ON A/C ALL Subtask 05-25-70-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-25-70 SROS
Page 605 Jul 01/06
TASK 05-25-70-200-805 Zonal Inspection of Inner Trailing Edge Fixed Structure (RIB 6 to RIB 12) 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 Refer to the MPD TASK: ZL-573-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
27-50-00-866-801 27-50-00-866-802
Extension of the Flaps on the Ground Retraction of the Flaps on the Ground
R
EFF : ALL 05-25-70 SROS
Page 606 Jul 01/06
3. __________ Job Set-up Subtask 05-25-70-866-050 A. Aircraft Maintenance Configuration R
(1) Fully extend the flaps (Ref. TASK 27-50-00-866-801). Subtask 05-25-70-941-051 B. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-25-70-010-053 C. Get Access (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the zone 573(673). (2) Remove the access panels: (a) For the left side: 573CB, 573DB, 573FB, 573GB. (b) For the right side: 673CB, 673DB, 673FB, 673GB. 4. Procedure _________ Subtask 05-25-70-210-053
R
A. Do a general visual inspection of the inner trailing-edge fixed structure (RIB6 to RIB12). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (wiring) are attached correctly.
EFF : ALL 05-25-70 SROS
Page 607 Jul 01/06
5. Close-up ________ Subtask 05-25-70-410-053 A. Close Access (1) Install the access panels: (a) For the left side: 573CB, 573DB, 573FB, 573GB. (b) For the right side: 673CB, 673DB, 673FB, 673GB. Subtask 05-25-70-860-052 B. Put the Aircraft back to its Initial Configuration (1) Retract the flaps (Ref. TASK 27-50-00-866-802). (2) Remove all the fixtures, tools, test and support equipment used during this procedure. (3) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-25-70 R SROS
Page 608 Jul 01/06
TASK 05-25-70-200-806 Zonal Inspection of Center Trailing Edge Fixed Structure (RIB 12 to RIB 27) 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 Refer to the MPD TASK: ZL-574-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------27-50-00-866-801 27-50-00-866-802
Extension of the Flaps on the Ground Retraction of the Flaps on the Ground
3. __________ Job Set-up Subtask 05-25-70-866-052 A. Aircraft Maintenance Configuration (1) Fully extend the flaps (Ref. TASK 27-50-00-866-801).
EFF : ALL 05-25-70 R SROS
Page 609 Jul 01/06
Subtask 05-25-70-941-052 B. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-25-70-010-054 C. Get Access (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the zone 574(674). (2) Remove the access panels: (a) For the left side: 574AT. (b) For the right side: 674AT. 4. Procedure _________ Subtask 05-25-70-210-054 A. Do a general visual inspection of the center trailing-edge fixed structure (RIB12 to RIB27). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-25-70-410-054 A. Close Access (1) Install the access panels: (a) For the left side: 574AT. (b) For the right side: 674AT.
EFF : ALL 05-25-70 R SROS
Page 610 Jul 01/06
Subtask 05-25-70-860-053 B. Put the Aircraft back to its Initial Configuration (1) Retract the flaps (Ref. TASK 27-50-00-866-802). (2) Remove all the fixtures, tools, test and support equipment used during this procedure. (3) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-25-70 R SROS
Page 611 Jul 01/06
TASK 05-25-70-200-807 Zonal Inspection of Outer Trailing Edge Fixed Structure (RIB 27 to RIB 39) 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 Refer to the MPD TASK: ZL-575-01 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 WARNING NOTICE
3. __________ Job Set-up Subtask 05-25-70-941-053 A. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls.
EFF : ALL 05-25-70 R SROS
Page 612 Jul 01/06
Subtask 05-25-70-010-055 B. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at zone 575(675). (2) Remove the access panels: (a) For the left side: 575AB, 575BB, 575CB, 575DB, 575AT, 575BT. (b) For the right side: 675AB, 675BB, 675CB, 675DB, 675AT, 675BT. 4. Procedure _________ Subtask 05-25-70-210-055 A. Do a general visual inspection of the outer trailing-edge fixed structure (RIB27 to RIB39). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-25-70-410-055 A. Close Access (1) Install the access panels: (a) For the left side: 575AB, 575BB, 575CB, 575DB, 575AT, 575BT. (b) For the right side: 675AB, 675BB, 675CB, 675DB, 675AT, 675BT. Subtask 05-25-70-860-054 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-25-70 SROS
Page 613 Jul 01/06
ZONAL INSPECTION : WING AILERON - INSPECTION/CHECK __________________________________________________ TASK 05-25-90-200-801 R
Zonal Inspection of Inboard Aileron. 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 Refer to the MPD TASK: ZL-591-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific No specific
warning notices 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
3. __________ Job Set-up R
Subtask 05-25-90-941-050
R
A. Safety Precautions
R R
(1) Put warning notices in the cockpit to tell persons not to operate the flight controls.
EFF : ALL 05-25-90 SROS
Page 601 Jan 01/04
Subtask 05-25-90-010-050 R
B. Get Access
R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the inboard aileron (zones 591 and 691). (2) Remove the access panels:
R
(a) For the left side: 591AB, 591BB, 591CB, 591DB, 575AB, 575BB.
R
(b) for the right side: 691AB, 691BB, 691CB, 691DB, 675AB, 675BB. 4. Procedure _________ Subtask 05-25-90-210-050 A. Do a general visual inspection of the inboard aileron (zones 591 and 691). Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-25-90-410-050 A. Close Access
R R
(1) Install the access panels:
R
(a) For the left side: 591AB, 591BB, 591CB, 591DB, 575AB, 575BB.
R R
(b) For the right side: 691AB, 691BB, 691CB, 691DB, 675AB, 675BB.
R R
Subtask 05-25-90-860-050 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-25-90 SROS
Page 602 Jan 01/04
TASK 05-25-90-200-802 R
Zonal Inspection of Outboard Aileron. 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 Refer to the MPD TASK: ZL-592-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific No specific
warning notices 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
3. __________ Job Set-up Subtask 05-25-90-010-051 A. Get Access R R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the outboard aileron (zones 592 and 692). (2) Put warning notices in the cockpit to tell persons not to operate the flight controls.
EFF : ALL 05-25-90 SROS
Page 603 Jan 01/04
(3) Remove the access panels: R
(a) For the left side: 592AB, 592BB, 592CB, 592DB, 575CB, 575DB.
R
(b) For the right side: 692AB, 692BB, 692CB, 692DB, 675CB, 675DB. 4. Procedure _________ Subtask 05-25-90-210-051 A. Do a general visual inspection of the outboard aileron (zones 592 and 692). Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-25-90-410-051 A. Close Access
R R
(1) Install the access panels:
R
(a) For the left side: 592AB, 592BB, 592CB, 592DB, 575CB, 575DB.
R R
(b) For the right side: 692AB, 692BB, 692CB, 692DB, 675CB, 675DB.
R R
Subtask 05-25-90-860-051 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-25-90 SROS
Page 604 Jan 01/04
ZONAL INSPECTION : LANDING GEAR AND LANDING GEAR DOORS - INSPECTION/CHECK _________________________________________________________________________ TASK 05-27-00-200-803 R
Zonal inspection of Landing Gear and Landing Gear Doors. 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-700-01 2. ______________________ Job Set-up Information Not Applicable 3. __________ Job Set-up Subtask 05-27-00-869-051
R R
A. Not applicable. 4. Procedure _________ Subtask 05-27-00-210-051 A. Inspection (1) Do a general visual inspection of the landing gears and the landing gear doors (zone 700). (2) Make sure that: - There is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - All the installations (wiring) are attached correctly.
EFF : ALL 05-27-00 SROS
Page 601 Jan 01/04
ZONAL INSPECTION : NOSE GEAR AND DOORS - INSPECTION/CHECK _________________________________________________________ TASK 05-27-10-200-804 R
Zonal Inspection of Nose Landing Gear. 1. __________________ Reason for the Job
R
Refer to the MPD TASK: ZL-711-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-22-00-010-801 32-22-00-410-801
Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-27-10-010-052 A. Get Access R R
(1) Put an ACCESS PLATFORM 2M (6 FT) in position at the NLG main doors 713 and 714.
R
(2) Open the nose landing-gear main-doors 713, 714 (Ref. TASK 32-22-00010-801).
EFF : ALL 05-27-10 SROS
Page 601 Jan 01/04
4. Procedure _________ Subtask 05-27-10-210-053 A. Inspection R
(1) Do a general visual inspection of the nose landing-gear (zone 711). (2) Make sure that: - There is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - All the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-27-10-410-052 A. Close Access (1) Close the nose landing-gear main-doors. (Ref. TASK 32-22-00-410-801).
R R R
Subtask 05-27-10-860-050 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-27-10 SROS
Page 602 Jan 01/04
TASK 05-27-10-200-806 Zonal Inspection of the Nose Landing Gear (Zones 710) 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-22-00-010-801 32-22-00-410-801
Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-27-10-010-053 A. Get Access (1) Open the nose landing-gear main-doors 713, 714, (Ref. TASK 32-22-00010-801). 4. Procedure _________ Subtask 05-27-10-210-055 A. Do a general visual inspection of the nose landing gear, from the ground ,as far as visible (including zones 713 and 714). Make sure that: - There is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - All the installations (wiring) are attached correctly.
EFF : ALL 05-27-10 R SROS
Page 603 Jan 01/04
5. Close-up ________ Subtask 05-27-10-410-053 A. Close Access (1) Close the nose landing gear doors (Ref. TASK 32-22-00-410-801). (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-27-10 R SROS
Page 604 Jan 01/04
TASK 05-27-10-200-807 Zonal Inspection of Nose Landing Gear Main Doors. 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 Refer to the MPD TASK: ZL-713-01 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
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-22-00-010-801 32-22-00-410-801
Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-27-10-010-054 A. Get Access R
(1) Open the nose landing-gear doors 713, 714 (Ref. TASK 32-22-00-010801). (2) Put an ACCESS PLATFORM 2M (6 FT) in position at the nose landing-gear doors 713 and 714.
EFF : ALL 05-27-10 SROS
Page 605 Jan 01/07
4. Procedure _________ Subtask 05-27-10-210-056 A. Inspection (1) Do a general visual inspection of the nose landing-gear main-doors (zones 713 and 714). (2) Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-27-10-410-054 A. Close Access R R
(1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Close the nose landing-gear doors. (Ref. TASK 32-22-00-410-801). Subtask 05-27-10-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R
EFF : ALL 05-27-10 SROS
Page 606 Jan 01/06
TASK 05-27-10-200-808 Zonal Inspection of Nose Landing Gear Aft Doors. 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-715-01 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
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-22-00-010-801 32-22-00-410-801
Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-27-10-010-055 A. Get Access (1) Put an ACCESS PLATFORM 2M (6 FT) in position at the nose landing-gear (NLG) doors 715 and 716. R
(2) Open the nose landing-gear doors (Ref. TASK 32-22-00-010-801).
EFF : ALL 05-27-10 SROS
Page 607 Jan 01/07
4. Procedure _________ Subtask 05-27-10-210-057 A. Inspection (1) Do a general visual inspection of the NLG aft doors (zones 715 and 716). (2) Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-27-10-410-055 A. Close Access (1) Close the nose landing-gear doors (Ref. TASK 32-22-00-410-801). Subtask 05-27-10-860-052 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-27-10 R SROS
Page 608 Jan 01/07
ZONAL INSPECTION : MAIN LANDING GEAR AND DOORS - INSPECTION/CHECK _________________________________________________________________ TASK 05-27-30-200-804 R
Zonal Inspection of LH and RH Main Landing Gear. 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-731-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-12-00-010-801 32-12-00-410-801
Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-27-30-010-051 A. Get Access R
(1) Open the main landing-gear (MLG) doors (Ref. TASK 32-12-00-010-801). (2) Put an ACCESS PLATFORM 2M (6 FT) in position at the main landing gear (zones 730 and 740).
EFF : ALL 05-27-30 SROS
Page 601 Jan 01/04
4. Procedure _________ Subtask 05-27-30-210-052 A. Inspection R R
(1) Do a general visual inspection of the main landing gears (zones 731 and 741). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-27-30-410-051 A. Close Access (1) Close the main landing-gear doors (Ref. TASK 32-12-00-410-801). Subtask 05-27-30-860-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-27-30 SROS
Page 602 Oct 01/04
TASK 05-27-30-200-809 Zonal Inspection of the Main Landing Gear (Zones 730 and 740). 1. __________________ Reason for the Job R R
Self Explanatory 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-12-00-010-801 32-12-00-410-801
Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-27-30-010-052 A. Get Access R
(1) Open is main landing gear main doors 734, 744 (Ref. TASK 32-12-00010-801). 4. Procedure _________ Subtask 05-27-30-210-057 A. Make a general visual inspection of the main landing gear, from the ground, as far as visible (zones 731 and 741). Make sure that: - there is no damage, corrosion, leaks or cracks on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-27-30-410-052 A. Close Access (1) Close the main landing-gear main doors 734, 744 (Ref. TASK 32-12-00410-801). (2) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-27-30 SROS
Page 603 Jul 01/03
TASK 05-27-30-200-810 R
Zonal Inspection of Main Landing Gear Leg Doors. 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-732-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-12-00-010-801 32-12-00-410-801
Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-27-30-010-053 A. Get Access R
(1) Open the main landing-gear (MLG) doors (Ref. TASK 32-12-00-010-801). (2) Put an ACCESS PLATFORM 2M (6 FT) in position at the main landing gear (zones 730 and 740).
R EFF : ALL 05-27-30 SROS
Page 604 Jan 01/04
4. Procedure _________ Subtask 05-27-30-210-058 A. Inspection R R
(1) Do a general visual inspection of the MLG leg doors (zone 732 and 742). (2) Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see 5. Close-up ________ Subtask 05-27-30-410-053 A. Close Access
R R R R
(1) Close the main landing-gear doors (Ref. TASK 32-12-00-410-801). Subtask 05-27-30-860-051 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-27-30 SROS
Page 605 Jan 01/04
TASK 05-27-30-200-811 R
Zonal Inspection of Main Landing Gear Hinge Door. 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-733-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-12-00-010-801 32-12-00-410-801
Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-27-30-010-054 A. Get Access R
(1) Open the main landing-gear (MLG) doors (Ref. TASK 32-12-00-010-801). (2) Put an ACCESS PLATFORM 2M (6 FT) in position at the main landing gear (zones 730 and 740). 4. Procedure _________ Subtask 05-27-30-210-059 A. Inspection
R R R
(1) Do a general visual inspection of the MLG hinge doors (zones 733 and 743).
EFF : ALL 05-27-30 SROS
Page 606 Jan 01/04
(2) Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see 5. Close-up ________ Subtask 05-27-30-410-054 A. Close Access R R R R
(1) Close the main landing-gear doors (Ref. TASK 32-12-00-410-801). Subtask 05-27-30-860-052 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-27-30 SROS
Page 607 Jan 01/04
TASK 05-27-30-200-812 R
Zonal Inspection of Main Landing Gear Main Doors. 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-734-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-12-00-010-801 32-12-00-410-801
Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-27-30-010-055 A. Get Access R
(1) Open the main landing-gear (MLG) doors (Ref. TASK 32-12-00-010-801). (2) Put an ACCESS PLATFORM 2M (6 FT) in position at the main landing gear (zones 730 and 740).
EFF : ALL 05-27-30 SROS
Page 608 Jan 01/04
4. Procedure _________ Subtask 05-27-30-210-060 A. Inspection R R
(1) Do a general visual inspection of the main landing-gear main-doors (zone 734 and 744). (2) Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see 5. Close-up ________ Subtask 05-27-30-410-055 A. Close Access
R R R R R
(1) Close the MLG doors (Ref. TASK 32-12-00-410-801). Subtask 05-27-30-860-053 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-27-30 SROS
Page 609 Jan 01/04
______________________________________________________________________________ ZONAL INSPECTION : PASSENGER/CREW DOORS, CARGO COMPARTMENT DOORS AND EMERGENCY EXITS - INSPECTION/CHECK ________________________ TASK 05-28-00-200-801 Zonal Inspection as far as visible from the ground of the Doors (zone 800) 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information Not Applicable 3. __________ Job Set-up Subtask 05-28-00-869-050 A. Not applicable. 4. Procedure _________ Subtask 05-28-00-210-050 A. Do a general visual inspection of the passenger/crew doors, the emergency exits and the cargo doors as far as visible from the ground during the aircraft walkaround.
EFF : ALL 05-28-00 R SROS
Page 601 Jan 01/04
TASK 05-28-00-200-802 Zonal Inspection of Doors 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-800-01 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
1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
3. __________ Job Set-up Subtask 05-28-00-010-050 A. Get Access R R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position next to the doors. 4. Procedure _________ Subtask 05-28-00-210-051 A. Do a general visual inspection of the Passenger/Crew doors, the emergency exits, the cargo compartment doors and the forward avionics compartment doors (zones 811, 821, 822, 831, 832, 833, 834, 841, 842, 843 and 844). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see.
EFF : ALL 05-28-00 SROS
Page 602 Jan 01/07
5. Close-up ________ Subtask 05-28-00-410-050 A. Close Access (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-28-00 SROS
Page 603 Jan 01/07
ZONAL INSPECTION : FORWARD AVIONICS COMPARTMENT - INSPECTION/CHECK __________________________________________________________________ TASK 05-28-10-200-801 Zonal Inspection of Forward Avionics Compartment Door 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-811-01 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
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 53-12-13-000-801 53-12-13-400-801 05-28-10-991-001
Energize the Ground Service Network De-energize the Ground Service Network Removal of the Avionics-Compartment Floor Panels Installation of the Avionics-Compartment Floor Panels Fig. 601
3. __________ Job Set-up Subtask 05-28-10-861-050 R
A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 05-28-10-010-050 B. Get Access (Ref. Fig. 601/TASK 05-28-10-991-001) (1) Put an ACCESS PLATFORM 2M (6 FT) in position at the access door 811. (2) Open the forward avionics compartment door 811.
EFF : ALL 05-28-10 SROS
Page 601 Jan 01/07
R R
FWD Avionics Compartment Door (Zone 811) Figure 601/TASK 05-28-10-991-001
EFF : ALL 05-28-10 SROS
Page 602 Jan 01/04
R
(3) Open the access floor panel 121EF (Ref. TASK 53-12-13-000-801). 4. Procedure _________ Subtask 05-28-10-210-050
R R
A. Do a general visual inspection of the forward avionics compartment door (zone 811). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-28-10-410-050 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Close the forward avionics compartment door 811.
R R
(3) Close the access floor panel 121EF (Ref. TASK 53-12-13-400-801). Subtask 05-28-10-862-050
R
B. Put the Aircraft back to its Initial Configuration
R R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R
(2) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 05-28-10 SROS
Page 603 Jan 01/04
__________________________________________________________________________ ZONAL INSPECTION : LOWER DECK FORWARD AFT AND BULK CARGO COMPARTMENT DOORS ________________ INSPECTION/CHECK TASK 05-28-20-200-802 R
Zonal Inspection of Forward Cargo Compartment Door 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-821-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------52-30-00-010-801 52-30-00-410-801 R
05-28-20-991-001
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 Fig. 601
3. __________ Job Set-up Subtask 05-28-20-010-051 R
A. Get Access (Ref. Fig. 601/TASK 05-28-20-991-001)
R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the access door 821.
R
(2) Open the forward cargo-compartment door 821 (Ref. TASK 52-30-00-010801).
EFF : ALL 05-28-20 SROS
Page 601 Jan 01/04
Access Panels on the Cargo-Compartment Door Zone 821-822 Figure 601/TASK 05-28-20-991-001 EFF : ALL 05-28-20 R SROS
Page 602 Jan 01/04
4. Procedure _________ Subtask 05-28-20-210-051 A. Do a general visual inspection of the forward cargo compartment door (zone 821). This includes: - The lock fittings at the door sill. - The door frames at the fuselage door seals. - The visible part of the door sill. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-28-20-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the forward cargo-compartment door 821 (Ref. TASK 52-30-00-410801). Subtask 05-28-20-860-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-28-20 R SROS
Page 603 Apr 01/04
TASK 05-28-20-200-803 R R
Zonal Inspection of Forward Cargo Compartment Door (Including Door Hinge Arms Attachment Area) 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-821-02 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 ------------------------------------------------------------------------------52-30-00-010-801 52-30-00-410-801 05-28-20-991-001 05-28-20-991-002
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 Fig. 601 Fig. 602
3. __________ Job Set-up Subtask 05-28-20-010-052 A. Get Access (Ref. Fig. 601/TASK 05-28-20-991-001, 602/TASK 05-28-20-991-002) R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at zone 821.
R
(2) Open the forward cargo-compartment door 821, (Ref. TASK 52-30-00-010801). (3) Remove the access panels 821AR, 821BR, 821CR, 821DR, 132AR, 132BR, 132CR, 132DR, 132ER, 132FR, 132GR, 132HR, 132JR, 132KR, 132LR.
EFF : ALL 05-28-20 SROS
Page 604 Apr 01/04
R R
Forward-Fuselage Lower Section Figure 602/TASK 05-28-20-991-002
EFF : ALL 05-28-20 SROS
Page 605 Jan 01/04
4. Procedure _________ Subtask 05-28-20-210-052 R
A. Do a general visual inspection of the forward cargo-compartment door (zone 821). This includes the door-hinge arms attachment-area. Make sure that : - there is no damage(corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (piping) are attached correctly. 5. Close-up ________ Subtask 05-28-20-410-052 A. Close Access (1) Install the access panels 821AR, 821BR, 821CR, 821DR, 132AR, 132BR, 132CR, 132DR, 132ER, 132FR, 132GR, 132HR, 132JR, 132KR, 132LR. (2) Close the forward cargo-compartment door 821, (Ref. TASK 52-30-00410-801). Subtask 05-28-20-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-28-20 SROS
Page 606 Jul 01/04
TASK 05-28-20-200-804 R
Zonal Inspection of Aft Cargo Compartment Door 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-822-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------52-30-00-010-801 52-30-00-410-801
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 05-28-20-010-053 A. Get Access R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the access door 822.
R
(2) Open the aft cargo-compartment door 822 (Ref. TASK 52-30-00-010-801).
EFF : ALL 05-28-20 SROS
Page 607 Jan 01/04
4. Procedure _________ Subtask 05-28-20-210-053 R R R R R R R
A. Do a general visual inspection of the aft cargo-compartment door (zone 822). This includes: - The lock fittings at the door sill. - The door frames at the fuselage door seals. - The visible part of the door sill. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (piping, wiring) are attached correctly.
R
5. Close-up ________ Subtask 05-28-20-410-053 A. Close Access R R
(1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Close the aft cargo-compartment door 822 (Ref. TASK 52-30-00-410801).
R R R
Subtask 05-28-20-860-053 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-28-20 SROS
Page 608 Jan 01/04
TASK 05-28-20-200-805 Zonal Inspection of Aft Cargo Compartment Door (Including Door Hinge Arms Attachment Area) 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-822-02 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 ------------------------------------------------------------------------------52-30-00-010-801 52-30-00-410-801 05-28-20-991-001 05-28-20-991-003
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 Fig. 601 Fig. 603
3. __________ Job Set-up Subtask 05-28-20-010-054 A. Get Access (Ref. Fig. 601/TASK 05-28-20-991-001, 603/TASK 05-28-20-991-003) (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at zone 822. R
(2) Open the aft cargo-compartment door 822, (Ref. TASK 52-30-00-010801). (3) Remove the access panels 822AR, 822BR, 822CR, 822DR, 152AR, 152BR, 152CR, 152DR, 152ER, 152FR, 152GR, 152HR, 152JR, 152KR, 152LR.
EFF : ALL 05-28-20 SROS
Page 609 Jul 01/04
R R
Aft-Fuselage Lower-Section Access-Panels - Zone 822 Figure 603/TASK 05-28-20-991-003
EFF : ALL 05-28-20 SROS
Page 610 Apr 01/04
4. Procedure _________ Subtask 05-28-20-210-054 R
A. Do a general visual inspection of the aft cargo-compartment door (zone 822). This includes the door-hinge arms attachment-area. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-28-20-410-054 A. Close Access (1) Install the access panels 822AR, 822BR, 822CR, 822DR, 152AR, 152BR, 152CR, 152DR, 152ER, 152FR, 152GR, 152HR, 152JR, 152KR, 152LR. (2) Close the aft cargo-compartment door 822, (Ref. TASK 52-30-00-410801). Subtask 05-28-20-860-054 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-28-20 SROS
Page 611 Jul 01/04
TASK 05-28-20-200-806 R
Zonal Inspection of Bulk Cargo Compartment Door (Including Fuselage Frames, Stop Fittings at Fuselage Frames, Door Seals, and Visible Part of Door Sill). 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-823-01 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 ------------------------------------------------------------------------------52-30-00-010-803 52-30-00-410-803
Opening of the BULK Cargo-Compartment Door Closing of the BULK Cargo-Compartment Door
3. __________ Job Set-up Subtask 05-28-20-010-055 A. Get Access R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the bulk cargo-compartment door 823. (2) Open the bulk cargo-compartment door 823 (Ref. TASK 52-30-00-010803).
EFF : ALL 05-28-20 SROS
Page 612 Jul 01/04
4. Procedure _________ Subtask 05-28-20-210-055 R R
A. Do a general visual inspection of the bulk cargo-compartment door (zone 823). This inspection includes the fuselage frames, the stop fittings, the door seals and the visible part of the door sill. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-28-20-410-055 A. Close Access (1) Close the bulk cargo-compartment door 823 (Ref. TASK 52-30-00-410803). Subtask 05-28-20-860-056 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-28-20 SROS
Page 613 Jul 01/04
TASK 05-28-20-200-807 Zonal Inspection of Bulk Cargo Compartment Door. 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-823-02 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 ------------------------------------------------------------------------------25-80-00-000-801 25-80-00-400-801 52-30-00-010-803 52-30-00-410-803
Removal of the Insulation Blankets Installation of the Insulation Blankets Opening of the BULK Cargo-Compartment Door Closing of the BULK Cargo-Compartment Door
3. __________ Job Set-up Subtask 05-28-20-010-056 A. Get Access (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the bulk cargo-compartment door 823. (2) Open the bulk cargo-compartment door 823 (Ref. TASK 52-30-00-010803). (3) Lift or remove the insulation blankets (Ref. TASK 25-80-00-000-801).
EFF : ALL 05-28-20 R SROS
Page 614 Apr 01/04
4. Procedure _________ Subtask 05-28-20-210-056 A. Do a general visual inspection of the bulk cargo-compartment door (zone 823). Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-28-20-410-056 A. Close Access (1) Install the insulation blankets, if removed (Ref. TASK 25-80-00-400801). (2) Close the bulk cargo-compartment door 823 (Ref. TASK 52-30-00-410803). Subtask 05-28-20-860-057 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-28-20 R SROS
Page 615 Apr 01/04
TASK 05-28-20-200-808 Zonal Inspection of Forward Cargo Compartment Door 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-821-03 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 ------------------------------------------------------------------------------25-80-00-000-801 25-80-00-400-801 52-30-00-010-801 52-30-00-410-801 05-28-20-991-001
Removal of the Insulation Blankets Installation of the Insulation Blankets 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 Fig. 601
3. __________ Job Set-up Subtask 05-28-20-010-057 A. Get Access (Ref. Fig. 601/TASK 05-28-20-991-001) (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the access door 821. (2) Open the forward cargo-compartment door 821 (Ref. TASK 52-30-00-010801). (3) Remove the access panels 821AR, 821BR, 821CR, 821DR.
EFF : ALL 05-28-20 R SROS
Page 616 Apr 01/04
(4) Remove the insulation blankets (Ref. TASK 25-80-00-000-801). 4. Procedure _________ Subtask 05-28-20-210-057 A. Do a general visual inspection of the forward cargo-compartment door (zone 821). Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-28-20-410-057 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the insulation blankets (Ref. TASK 25-80-00-400-801). (3) Install the access panels 821AR, 821BR, 821CR, 821DR. (4) Close the forward cargo-compartment door 821 (Ref. TASK 52-30-00-410801). Subtask 05-28-20-860-052 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-28-20 R SROS
Page 617 Apr 01/04
TASK 05-28-20-200-809 Zonal Inspection of AFT Cargo Compartment Door. 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-822-03 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 ------------------------------------------------------------------------------25-80-00-000-801 25-80-00-400-801 52-30-00-010-801 52-30-00-410-801
Removal of the Insulation Blankets Installation of the Insulation Blankets 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 05-28-20-010-058 A. Get Access (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the aft cargo-compartment door 822. (2) Open the aft cargo-compartment door 822 (Ref. TASK 52-30-00-010-801). (3) Remove the access panels 822AR, 822BR, 822CR, 822DR. (4) Remove or lift the insulation blankets (Ref. TASK 25-80-00-000-801).
EFF : ALL 05-28-20 R SROS
Page 618 Apr 01/04
4. Procedure _________ Subtask 05-28-20-210-058 A. Do a general visual inspection of the aft cargo-compartment door (zone 822). Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-28-20-410-058 A. Close Access (1) Install the insulation blankets (Ref. TASK 25-80-00-400-801). (2) Install the access panels 822AR, 822BR, 822CR, 822DR. (3) Close the aft cargo-compartment door 822 (Ref. TASK 52-30-00-410801). Subtask 05-28-20-860-055 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-28-20 SROS
Page 619 Apr 01/04
_________________________________________________________________ ZONAL INSPECTION : LEFT PASSENGER/ CREW DOORS AND EMERGENCY EXITS ________________ INSPECTION/CHECK TASK 05-28-30-200-801 R
Zonal Inspection of FWD Passenger/Crew Door (Including Door Stops on Fuselage Side, Door Seals and Scuff Plates) 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-831-01 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 ------------------------------------------------------------------------------52-10-00-010-801 52-10-00-410-801
Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door
3. __________ Job Set-up Subtask 05-28-30-010-050 A. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the passenger/crew doors 831 and 841 . (2) Open the passenger/crew doors 831 and 841 (Ref. TASK 52-10-00-010801).
EFF : ALL 05-28-30 SROS
Page 601 Apr 01/04
4. Procedure _________ Subtask 05-28-30-210-050 A. Do a general visual inspection of the passenger/crew doors (zones 831 and 841). This inspection includes the door stops on the fuselage side, the door seals and the scuff plates. Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-28-30-410-050 A. Close Access (1) Close the passenger/crew doors 831 and 841 (Ref. TASK 52-10-00-410801). Subtask 05-28-30-860-056 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-28-30 R SROS
Page 602 Apr 01/04
TASK 05-28-30-200-802 Zonal Inspection of FWD Passenger/Crew Door 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-831-02 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
25-23-49-000-801
R R
25-23-49-400-801 25-80-00-000-801 25-80-00-400-801 52-10-00-010-801 52-10-00-410-801
Removal of the Lining of the Forward Passenger/Crew Door(s) Installation of the Lining of the Forward Passenger/Crew Door(s) Removal of the Insulation Blankets Installation of the Insulation Blankets Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door
3. __________ Job Set-up Subtask 05-28-30-010-051 A. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the passenger/crew doors 831 and 841. (2) Open the passenger/crew doors 831 and 841 (Ref. TASK 52-10-00-010801).
EFF : ALL 05-28-30 SROS
Page 603 Jan 01/06
(3) Remove the access panels: (a) For the FWD passenger/crew door 831 (left side): 831AZ, 831BZ, 831CZ, 831DZ, 831EZ, 831FZ, 831GZ, 831HZ, 831JZ (Ref. TASK 25-23-49-000-801). (b) For the FWD passenger/crew door 841 (right side): 841AZ, 841BZ, 841CZ, 841DZ, 841EZ, 841FZ, 841GZ, 841HZ, 841JZ (Ref. TASK 25-23-49-000-801). (4) Lift or remove the insulation blankets (Ref. TASK 25-80-00-000-801). 4. Procedure _________ Subtask 05-28-30-210-051 A. Do a general visual inspection of the forward passenger/crew doors (zones 831 and 841) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-28-30-410-051 A. Close Access (1) Install the insulation blankets (Ref. TASK 25-80-00-400-801). (2) Install the access panels: (a) For the FWD passenger/crew door 831 (left side): 831AZ, 831BZ, 831CZ, 831DZ, 831EZ, 831FZ, 831GZ, 831HZ, 831JZ (Ref. TASK 25-23-49-400-801). (b) For the FWD passenger/crew door 841 (right side): 841AZ, 841BZ, 841CZ, 841DZ, 841EZ, 841FZ, 841GZ, 841HZ, 841JZ (Ref. TASK 25-23-49-400-801). (3) Close the passenger/crew doors 831 and 841 (Ref. TASK 52-10-00-410801).
EFF : ALL 05-28-30 R SROS
Page 604 Apr 01/04
R R
Subtask 05-28-30-860-057 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-28-30 SROS
Page 605 Jan 01/04
TASK 05-28-30-200-809 R
Zonal Inspection of Emergency Exit (Including Door Stops on Fuselage Side, Door Seals and Scuff Plates) 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-834-01 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
52-20-00-010-801 52-20-00-410-801
Opening of the Emergency Exit Door Closing of the Emergency Exit Door
3. __________ Job Set-up Subtask 05-28-30-010-058 A. Get Access R R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at zone 834(844).
R
(2) Open the emergency exit doors 834, 844, (Ref. TASK 52-20-00-010-801).
EFF : ALL 05-28-30 SROS
Page 606 Apr 01/04
4. Procedure _________ Subtask 05-28-30-210-058 R R
A. Do a general visual inspection of the emergency exit doors (zones 834 and 844). This inspection includes the door stops on the fuselage side, the door seals and the scuff plates. - Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-28-30-410-058 A. Close Access (1) Close the emergency exit doors 834, 844, (Ref. TASK 52-20-00-410801). Subtask 05-28-30-860-052 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-28-30 SROS
Page 607 Jul 01/05
TASK 05-28-30-200-810 Zonal Inspection of Emergency Exit 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-834-02 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 ------------------------------------------------------------------------------25-23-53-000-801 25-23-53-400-801
Removal of the Lining of the Emergency Exit Door Installation of the Lining of the Emergency Exit Door
3. __________ Job Set-up R
**ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499,
R
Subtask 05-28-30-010-059-A
R
A. Get Access
R R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at zone 834(844).
R
(2) Remove the access panels.
R R
(a) For the emergency exit 834: 834KZ, 834LZ, 834MZ, 834NZ, 834PZ, 834QZ, (Ref. TASK 25-23-53-000-801).
R R
(b) For the emergency exit 844: 844KZ, 844LZ, 844MZ, 844NZ, 844PZ, 844QZ, (Ref. TASK 25-23-53-000-801).
EFF : ALL 05-28-30 SROS
Page 608 Jul 01/06
R
(3) Lift the insulation blankets. **ON A/C 301-399, 701-749, Subtask 05-28-30-010-059 A. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at zone 834(844). (2) Remove the access panels. (a) For the emergency exit 834: 834AZ, 834BZ, 834CZ, 834DZ, 834EZ, 834FZ, 834GZ, 834HZ, 834JZ, (Ref. TASK 25-23-53-000-801). (b) For the emergency exit 844: 844AZ, 844BZ, 844CZ, 844DZ, 844EZ, 844FZ, 844GZ, 844HZ, 844JZ, (Ref. TASK 25-23-53-000-801). (3) Lift the insulation blankets. **ON A/C ALL 4. Procedure _________ Subtask 05-28-30-210-059 A. Do a general visual inspection of the emergency exits (zones 834 and 844). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring) are attached correctly. 5. Close-up ________
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499,
R
Subtask 05-28-30-410-059-A
R
A. Close Access
R
(1) Put in position back the insulation.
R
(2) Install the access panels.
R R
(a) For the emergency exit 834: 834KZ, 834LZ, 834MZ, 834NZ, 834PZ, 834QZ, (Ref. TASK 25-23-53-400-801).
EFF : ALL 05-28-30 SROS
Page 609 Jul 01/06
R R
(b) For the emergency exit 844: 844KZ, 844LZ, 844MZ, 844NZ, 844PZ, 844QZ, (Ref. TASK 25-23-53-400-801). **ON A/C 301-399, 701-749, Subtask 05-28-30-410-059 A. Close Access (1) Put in position back the insulation. (2) Install the access panels. (a) For the emergency exit 834: 834AZ, 834BZ, 834CZ, 834DZ, 834EZ, 834FZ, 834GZ, 834HZ, 834JZ, (Ref. TASK 25-23-53-400-801). (b) For the emergency exit 844: 844AZ, 844BZ, 844CZ, 844DZ, 844EZ, 844FZ, 844GZ, 844HZ, 844JZ, (Ref. TASK 25-23-53-400-801). **ON A/C ALL Subtask 05-28-30-860-053 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-28-30 SROS
Page 610 Jul 01/06
TASK 05-28-30-200-811 R
Zonal Inspection of Emergency Exit (Doors 3) 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-834-03 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------25-23-48-000-801 25-23-48-400-801
Removal of the Door Frame Linings of the Emergency Exit Installation of the Door Frame Linings of the Emergency Exit Removal of the Lining of the Emergency Exit Door Installation of the Lining of the Emergency Exit Door
25-23-53-000-801 25-23-53-400-801 R 3. __________ Job Set-up R R
Subtask 05-28-30-010-060-B A. Get Access
R R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the zone 834(844).
R
(2) Remove the access panels.
R R
(a) For the emergency exit 834: 834KZ, 834LZ, 834MZ, 834NZ, 834PZ, 834QZ, (Ref. TASK 25-23-53-000-801).
EFF : ALL 05-28-30 SROS
Page 611 Apr 01/04
R R
(b) For the emergency exit 844: 844KZ, 844LZ, 844MZ, 844NZ, 834PZ, 834QZ, (Ref. TASK 25-23-53-000-801).
R
(3) Remove the frame lining panels.
R R
(a) For the emergency exit 834: 261TX, 261UX, 261XX, 261YX, (Ref. TASK 25-23-48-000-801).
R R
(b) For the emergency exit 844: 262TX, 262UX, 262XX, 262YX, (Ref. TASK 25-23-48-000-801).
R
(4) Lift the insulation. 4. Procedure _________
R R R R R R R
Subtask 05-28-30-210-060-B A. Do a general visual inspection of the emergency exits 834 and 844 (Type 1). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring) are attached correctly. 5. Close-up ________
R R
Subtask 05-28-30-410-060-B A. Close Access
R
(1) Put in position back the insulation.
R
(2) Install the frame lining panels.
R R
(a) For the emergency exit 834: 261TX, 261UX, 261XX, 261YX, (Ref. TASK 25-23-48-400-801).
R R
(b) For the emergency exit 844: 262TX, 262UX, 262XX, 262YX, (Ref. TASK 25-23-48-400-801).
R
(3) Install the access panels
R R
(a) For the emergency exit 834: 834KZ, 834LZ, 834MZ, 834NZ, 834PZ, 834QZ, (Ref. TASK 25-23-53-400-801).
R R
(b) For the emergency exit 844: 844KZ, 844LZ, 844MZ, 844NZ, 844PZ, 844QZ, (Ref. TASK 25-23-53-400-801).
EFF : ALL 05-28-30 SROS
Page 612 Apr 01/04
R R
Subtask 05-28-30-860-060-A B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-28-30 SROS
Page 613 Jan 01/05
TASK 05-28-30-200-812 Zonal Inspection of MID Passenger/Crew Doors 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-832-01 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 ------------------------------------------------------------------------------52-10-00-010-801 52-10-00-410-801
Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door
3. __________ Job Set-up Subtask 05-28-30-010-061 A. Get Access R R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at zone 832(842). (2) Open the MID passenger/crew doors 832, 842, (Ref. TASK 52-10-00-010801).
EFF : ALL 05-28-30 SROS
Page 614 Jan 01/06
4. Procedure _________ Subtask 05-28-30-210-061 R R R
A. Do a general visual inspection of the MID passenger/crew doors (this includes door stops on fuselage side, door seals and scuff plates) (zones 832 and 842). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-28-30-410-061 A. Close Access (1) Close the MID passenger/crew doors 832, 842, (Ref. TASK 52-10-00-410801). Subtask 05-28-30-860-058 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-28-30 SROS
Page 615 Jan 01/06
TASK 05-28-30-200-813 Zonal Inspection of MID Passenger/Crew Door 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-832-02 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
25-23-51-000-801
R R
25-23-51-400-801 25-80-00-000-801 25-80-00-400-801 52-10-00-010-801 52-10-00-410-801
Removal of the Lining of the Middle Passenger/Crew Door(s) Installation of the Lining of the Middle Passenger/Crew Door(s) Removal of the Insulation Blankets Installation of the Insulation Blankets Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door
3. __________ Job Set-up Subtask 05-28-30-010-062 A. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the MID passenger/crew doors 832 and 842. (2) Open the MID passenger/crew doors 832 and 842 (Ref. TASK 52-10-00010-801).
EFF : ALL 05-28-30 SROS
Page 616 Jan 01/06
(3) Remove the access panels:
R
(a) For the MID passenger/crew door 832 (left side): 832AZ, 832BZ, 832CZ, 832DZ, 832EZ, 832FZ, 832GZ, 832HZ, 832JZ (Ref. TASK 25-23-51-000-801).
R
(b) For the MID passenger/crew door 842 (right side): 842AZ, 842BZ, 842CZ, 842DZ, 842EZ, 842FZ, 842GZ, 842HZ, 842JZ (Ref. TASK 25-23-51-000-801). (4) Lift or remove the insulation blankets (Ref. TASK 25-80-00-000-801). 4. Procedure _________ Subtask 05-28-30-210-062
R
A. Inspection
R R R
(1) Do a general visual inspection of the MID passenger/crew doors (zones 832 and 842).
R
(2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring) are attached correctly.
R
5. Close-up ________ Subtask 05-28-30-410-062 A. Close Access R
(1) Install the insulation blankets (Ref. TASK 25-80-00-400-801). (2) Install the access panels:
R
(a) For the MID passenger/crew door 832 (left side): 832AZ, 832BZ, 832CZ, 832DZ, 832EZ, 832FZ, 832GZ, 832HZ, 832JZ (Ref. TASK 25-23-51-400-801).
R R
(b) For the MID passenger/crew door 842 (right side): 842AZ, 842BZ, 842CZ, 842DZ, 842EZ, 842FZ, 842GZ, 842HZ, 842JZ (Ref. TASK 25-23-51-400-801).
R
(3) Close the passenger/crew doors 832 and 842 (Ref. TASK 52-10-00-410801).
EFF : ALL 05-28-30 SROS
Page 617 Jul 01/04
Subtask 05-28-30-860-059 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-28-30 R SROS
Page 618 Apr 01/04
TASK 05-28-30-200-814 Zonal Inspection of AFT Passenger/Crew Doors 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-833-01 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 ------------------------------------------------------------------------------52-10-00-010-801 52-10-00-410-801
Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door
3. __________ Job Set-up Subtask 05-28-30-010-063 A. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the aft passenger/crew doors 833 and 843. (2) Open the passenger/crew doors 833 and 843 (Ref. TASK 52-10-00-010801).
EFF : ALL 05-28-30 R SROS
Page 619 Jan 01/06
4. Procedure _________ Subtask 05-28-30-210-063 R R R
A. Do a general visual inspection of the AFT passenger/crew doors (this includes door stops on fuselage side, door seals and scuff plates) (zones 833 and 843). Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-28-30-410-063 A. Close Access (1) Close the passenger/crew doors 833 and 843 (Ref. TASK 52-10-00-410801). Subtask 05-28-30-860-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-28-30 SROS
Page 620 Jan 01/06
TASK 05-28-30-200-815 Zonal Inspection of AFT Passenger/Crew Door 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-833-02 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
25-23-52-000-802 25-23-52-400-802 25-80-00-000-801 25-80-00-400-801 52-10-00-010-801 52-10-00-410-801
Removal of the Lining of the Aft Passenger/Crew Door Installation of the Lining of the Aft Passenger/Crew Door Removal of the Insulation Blankets Installation of the Insulation Blankets Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door
3. __________ Job Set-up Subtask 05-28-30-010-064 A. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the passenger/crew doors 833 and 843. (2) Open the passenger/crew doors 833 and 843 (Ref. TASK 52-10-00-010801).
EFF : ALL 05-28-30 SROS
Page 621 Jan 01/06
(3) Remove the access panels: (a) For the AFT passenger/crew door 833 (left side): 833AZ, 833BZ, 833CZ, 833DZ, 833EZ, 833FZ, 833GZ, 833HZ, 833JZ (Ref. TASK 25-23-52-000-802). (b) For the AFT passenger/crew door 843 (right side): 843AZ, 843BZ, 843CZ, 843DZ, 843EZ, 843FZ, 843GZ, 843HZ, 843JZ (Ref. TASK 25-23-52-000-802). (4) Lift or remove the insulation blankets (Ref. TASK 25-80-00-000-801). 4. Procedure _________ Subtask 05-28-30-210-064 A. Do a general visual inspection of the passenger/crew doors (zones 833 and 843). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-28-30-410-064 A. Close Access (1) Install the insulation blankets (Ref. TASK 25-80-00-400-801) (2) Install the access panels: R
(a) For the AFT passenger/crew door 833 (left side): 833AZ, 833BZ, 833CZ, 833DZ, 833EZ, 833FZ, 833GZ, 833HZ, 833JZ (Ref. TASK 25-23-52-400-802). (b) For the AFT passenger/crew door 843 (right side): 843AZ, 843BZ, 843CZ, 843DZ, 843EZ, 843FZ, 843GZ, 843HZ, 843JZ (Ref. TASK 25-23-52-400-802). (3) Close the passenger/crew doors 833 and 843 (Ref. TASK 52-10-00-410801).
R EFF : ALL 05-28-30 SROS
Page 622 Jul 01/04
Subtask 05-28-30-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-28-30 R SROS
Page 623 Jul 01/04
UNSCHEDULED MAINTENANCE CHECKS - DESCRIPTION AND OPERATION __________________________________________________________ R R R R R R R R R R R R R R R R R R R R R R R
1. _______ General Section 05-51 gives the checks and inspections that you must do after the aircraft has gone through special or abnormal conditions, such as: - hard/overweight landing - landing-gear-down limit speed exceeded - flap/slat limit speed exceeded - bird or hail strike - tire burst or tread throw - brake emergency application or overheat - flight in excessive turbulence or in excess of VMO - lightning strike or static discharge - engine bird strike or slush ingestion - tail runway impact - NLG towing overload or overrun - NLG steering angle exceeded - leaving runway or taxiway - flight through dust storm or dust contamination on ground - flight through volcanic ash or volcanic ash contamination on ground - engine failure - engine side loads - mercury spillage - abnormal pax/crew door movement. It also contains the manufacturers recommendations for non revenue flight requirements following maintenance actions (REF. ATA 05-59).
EFF : ALL 05-50-00 SROS
Page 1 Jan 01/07
UNSCHEDULED MAINTENANCE CHECKS - MAINTENANCE PRACTICES ______________________________________________________ TASK 05-50-00-790-801 Leaks - Permitted Values 1. __________________ Reason for the Job This task gives you all the fluid leak measurement procedures for flight control, fuel, hydraulic, landing gear, cargo door and power plant systems. 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------28-11-00-280-802 29-00-00-790-801 71-00-00-860-817 71-71-00-200-801
Fuel Tank Leaks - General Information Check of the External Leakage of Hydraulic Components Engine Operation Limits and Guidelines Leakage Rates at Drains Mast
3. __________ Job Set-up Subtask 05-50-00-869-050 A. Not applicable. 4. Procedure _________ R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-50-00-360-050 A. Measurement of Leaks (1) Measurement of hydraulic system leaks (Ref. TASK 29-00-00-790-801). (2) Measurement of flight-control system leaks (Ref. TASK 29-00-00-790801). (3) Measurement of fuel system leaks (Ref. TASK 28-11-00-280-802).
EFF : ALL 05-50-00 SROS
Page 201 Jul 01/05
(4) Measurement of landing-gear system leaks (Ref. TASK 29-00-00-790801). (5) Measurement of cargo door leaks (Ref. TASK 29-00-00-790-801). (6) Measurement of power-plant system leaks (Ref. TASK 71-00-00-860-817). **ON A/C 701-749, Subtask 05-50-00-360-050-A A. Measurement of Leaks (1) Measurement of hydraulic system leaks (Ref. TASK 29-00-00-790-801). (2) Measurement of flight-control system leaks (Ref. TASK 29-00-00-790801). (3) Measurement of fuel system leaks (Ref. TASK 28-11-00-280-802). (4) Measurement of landing-gear system leaks (Ref. TASK 29-00-00-790801). (5) Measurement of cargo door leaks (Ref. TASK 29-00-00-790-801). (6) Measurement of power-plant system leaks (Ref. TASK 71-71-00-200-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 05-50-00 301-399, 401-449, 451-499, 701-749, SROS
Page 202 Jul 01/05
INSPECTIONS - DESCRIPTION AND OPERATION _______________________________________ R R R R R R
1. _______ General This section contains the inspections that are necessary after an incident or flight in abnormal conditions; and will in most cases, be called for as a result of flight crew report. If there is no inspection in this section applicable to incident or abnormal flight conditions that occurred, operators must tell Airbus and make a request for more instructions.
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A. Inspection Coverage It is not possible to give precise details of the inspection procedure to be adopted after every incident because of the wide variations of weight, speed, nature and direction of loads, weather conditions and component failure patterns. Therefore these inspections have been written for the worst possible case. In order to gain an indication of the severity of the incident and to facilitate rapid location of primary damage it is essential that full information be obtained from the flight crew. Therefore before you start an inspection, consult the crew and get data on the following: - Weather conditions - Aircraft speed and flight attitude - Aircraft weight and fuel distribution - Landing : was touchdown straight, drifting, wing low, nose up or down? - Was any noise of impact or indicative of structure or component failure heard? - Applicable instrument indications Printout of the maintenance data recorder-tape will give valuable additional data and indication of system malfunction.
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B. Inspection Sequence To permit simultaneous inspection of several areas of the aircraft the inspection has been divided into a number of Packages. For example: Inspection after Hail Impact requires on Phase 1 a complete airframe external check. Therefore this is divided into four major zones: fuselage, wings, nacelles/pylons and stabilizers. These major zones are further divided into smaller zones or major components. The small zones are then broken down into items, which can be individually signed off when inspection is completed. The inspections are divided into three phases: - Phase 1: is a general inspection for primary damage and indication of remote damage and is mainly external. - Phase 2: is a more detailed inspection and is mainly internal. It can be necessary to remove some components. - Phase 3: is a very detailed inspection with component removal and strip down.
EFF : ALL 05-51-00 SROS
Page 1 Jan 01/07
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If the Phase 1 inspection shows no damage, no further examination is necessary. If Phase 1 shows damage then Phase 2 must be done. If Phase 2 shows damage then Phase 3 must be done. C. Inspection Presentation (Ref. Fig. 001) The layout of the inspection form is as follows: - columns 1, 3, 4, 5, 6 and 8 are explained on the figure - columns 2 and 7 are provided for use by the operators inspectors, if they wish to use them, for inspection intensity code and accomplishment signature. The forms may thus be photo-copied, used as job cards and then filed with the aircraft technical record on completion.
EFF : ALL 05-51-00 SROS
Page 2 Jan 01/07
Inspection Layout Table Figure 001 EFF : ALL 05-51-00 SROS
Page 3 Apr 01/98
INSPECTION AFTER HARD/OVERWEIGHT LANDING - INSPECTION/CHECK ___________________________________________________________ R
TASK 05-51-11-200-802
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Inspection after Hard/Overweight Landing
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1. __________________ Reason for the Job
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After a flight crew report of a hard/overweight landing, you must do the following inspection before the subsequent flight. 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 No specific FOR FIN 4030EM2 No specific
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safety barriers warning notices wheel chocks 1 ACCESS PLATFORM 17M (56 FT) - ADJUSTABLE
B. Referenced Information
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------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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07-11-00-581-801 23-71-00-710-801 24-38-00-740-801 24-41-00-861-801 24-41-00-862-801 27-50-00-866-801 27-50-00-866-802 27-54-00-200-801 27-54-00-710-801 27-60-00-866-801 27-60-00-866-802 27-80-00-866-801
Lifting of the Aircraft for Maintenance Operations Operational Test of the CVR and of the Recording on all Four Channels BITE Test of the BCL (1PB1, 1PB2, 1PB3) Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Extension of the Flaps on the Ground Retraction of the Flaps on the Ground Detailed Visual Inspection of the Flap Transmission Assy Operational Test of the Flap System Extension of the Spoilers for Maintenance Retraction of the Spoilers after Maintenance Extension of the Slats on the Ground
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------------------------------------------------------------------------------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 R R R R R R R R R R R R R R R R
27-80-00-866-802 28-25-00-650-803 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 31-33-00-710-803 31-36-00-200-803 32-00-00-481-801 32-11-00-220-801
32-11-00-220-802 32-12-00-010-801 32-12-00-410-801 32-22-00-010-801 32-22-00-410-801 32-31-00-710-801 49-12-00-200-801 57-56-11-000-801 57-56-11-000-802 57-56-11-000-803 71-00-00-000-803 71-00-00-000-805 71-00-00-700-834 71-00-00-720-821 71-13-00-010-802 71-13-00-010-805
Retraction of the Slats on the Ground To Drain the Remaining Fuel (Wing Tanks) 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) Operational Check for Digital Flight Data Recorder System by using MCDU Check of the Load-Report Parameter after Hard/Overweight Landing or Excessive Turbulence Installation of the Safety Devices on the Landing Gears Detailed Inspection of Main Gear Structure comprising: Main Fittings, Sliding Piston, Bogie Beam, Pitch Trimmer, Sidestay Assy, Lock Pins Assembly ... Check of Shock Absorber Nitrogen Charge Pressure Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance Functional Test of the Normal Extension and Retraction System Visual Check of APU Suspension System Including Shockmount Structure And Brackets Removal of the Movable Flap Track Fairing No. 2 Removal of the Movable Flap Track Fairing No. 3 Removal of the Movable Flap Track Fairing No. 4 Removal of the Engine Removal of the Demountable Power Plant Test No.7 The Engine Performance Test Test No. 9 - Power Assurance Test Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Open the Fan Cowl Doors
EFF : ALL 05-51-11 SROS
Page 602 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R R R R R R R R
78-30-00-410-801
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**ON A/C 002-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 701-749, Post SB 31-3091 For A/C 401-449,451-499,
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05-51-11-991-054 05-51-11-991-057 05-51-11-991-058
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**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499,
R
05-51-11-991-005
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**ON A/C 701-749,
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05-51-11-991-005-A
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**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499,
R
05-51-11-991-009
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**ON A/C 701-749,
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05-51-11-991-009-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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05-51-11-991-018
78-30-00-410-803 78-31-00-710-804 78-31-00-740-802 79-00-00-200-805 79-22-11-200-801 05-51-11-991-001
Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Close the Thrust Reverser Cowl Doors Thrust Reverser Cycling Test (MCDU) Test of the Thrust Reverser Deployment and Stowage (Engine not Running) Inspect Master Magnetic Chip Detector for Evidence of Abnormal Deposits Inspection of the Magnetic Chip Detector (5006EN) Fig. 601
Fig. 602 Fig. 603 Fig. 604
Fig. 605
Fig. 605A
Fig. 606
Fig. 606A
Fig. 607
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
**ON A/C 701-749,
R
05-51-11-991-018-A
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499,
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05-51-11-991-021
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**ON A/C 701-749,
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05-51-11-991-021-A
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499,
R
05-51-11-991-022
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**ON A/C 701-749,
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05-51-11-991-022-A
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**ON A/C ALL
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05-51-11-991-023 05-51-11-991-025 05-51-11-991-026 05-51-11-991-027 05-51-11-991-028 05-51-11-991-029 05-51-11-991-030 05-51-11-991-031 05-51-11-991-032 05-51-11-991-033 FOR FIN 4030EM2 71-13-00-410-802 71-13-00-410-805
Fig. 607A
Fig. 608
Fig. 608A
Fig. 609
Fig. 609A
Fig. Fig. Fig. Fig. Fig. Fig. Fig. Fig. Fig. Fig.
610 611 612 613 614 615 616 617 618 619
Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Close the Fan Cowl Doors
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R
78-30-00-010-801
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3. __________ Job Set-up
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Subtask 05-51-11-210-103
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78-30-00-010-803
Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Open the Thrust Reverser Cowl Doors
A. General
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(1) Definitions
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(a) A hard landing is: - a landing with a vertical the center of gravity or - a vertical speed (V/S) of weight less than 155 tons - a vertical speed (V/S) of weight more than or equal
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(b) An overweight landing is: - a landing at more than the maximum landing weight with a vertical acceleration of more than 1.4g at the center of gravity or - a landing at more than the maximum landing weight with a vertical speed (V/S) of more than 360 ft/min.
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acceleration of more than 1.75g at more than 600 ft/min for an A/C or more than 540 ft/min for an A/C to 155 tons.
(2) Inspection requirements
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(a) After a hard/overweight landing, it is necessary to do the hard/overweight landing inspection before the subsequent flight. To prevent inspection that is not necessary, when there is a suspected hard/overweight landing (flight crew report, damage found on the aircraft, etc.), it is possible to refer to the DFDRS landing impact parameters to know if the landing was a hard/overweight landing.
EFF : ALL 05-51-11 SROS
Page 605 Jan 01/07
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Subtask 05-51-11-941-056 B. Procedure to Confirm a Suspected Hard/Overweight Landing
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(1) Definition of a suspected Hard/Overweight Landing A suspected hard/overweight landing is a landing after which the flight crew makes a report of a hard/overweight landing.
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NOTE : It is the responsibility of the flight crew to make a report ____ if they think there was a hard/overweight landing.
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(2) Confirmation of a hard/overweight landing
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(a) After a suspected hard/overweight landing, and to prevent inspection that is not necessary, it is possible to refer to the DFDRS landing impact parameters to confirm that a hard/overweight landing occurred and that the inspection is necessary.
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NOTE : If you do not (or if you cannot) read the landing impact ____ parameters, you must do the inspection after hard/overweight landing before the subsequent flight. - To know the impact parameters, refer to the DFDRS readout. - If the landing impact parameters confirm hard/overweight landing, you must do the inspection after hard/overweight landing.
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Subtask 05-51-11-941-057 C. Inspection Preparation
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(1) We cannot give you accurate instruction for the inspection procedure to be done after each incident. This is because there can be important differences in the weight, the speed and the direction of the loads. Thus, before you start, we recommend that you get data:
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(a) From the crew about the landing conditions. For example, find out: - If the touchdown was on main gears or on main and nose gears or high pitch rate on nose gear - If the landing was straight, drifting, wing-low, tail or nose heavy - If the crew heard a noise possibly related to a structural failure.
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NOTE : After a hard/overweight landing, there are two possible ____ cases with their applicable requirements:
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Page 606 Jan 01/07
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- Hard touchdown on In this case, the not necessary. - Hard touchdown on In this case, the
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main gears only: inspection of the nose gear area is nose and main gears: full inspection is necessary.
NOTE : Inspections are visual unless specified differently in the ____ text. Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures.
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(b) From the flight recorder (DFDR): - vertical acceleration, vertical speed (V/S), weight of the aircraft.
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(2) With these items of data, refer to the inspection definition diagram. (Ref. Fig. 601/TASK 05-51-11-991-001)
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**ON A/C 002-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 701-749, Post SB 31-3091 For A/C 401-449,451-499,
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Subtask 05-51-11-210-103-A
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A. General
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(1) Definitions
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(a) Delta VRTA Vertical acceleration Increment (DELTA VRTA): It is the difference between the Vertical Acceleration (VRTA) before the aircraft touch down (representing the aircraft actual lift) and the peak of VRTA after touch down.
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(b) RALR Radio Altitude Rate (RALR): It represents the aircraft vertical rate of descent.
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(c) A Hard Landing (GW <= MLW) is defined as: RALR < -10 ft/s and DELTA VRTA > 0.75 g or DELTA VRTA > 1.0 g or RALR < -13 ft/s
R EFF : ALL 05-51-11 SROS
Page 607 Jan 01/07
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Inspection - Definition Diagram Figure 601/TASK 05-51-11-991-001
EFF : ALL 05-51-11 SROS
Page 608 Jul 01/04
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(d) An Overweight Landing (GW > MLW) is defined as: RALR < -6 ft/s and DELTA VRTA > 0.5 g or DELTA VRTA > 0.7 g or VALR < -9 ft/s
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(e) Load report 15: - The ACMS load report 15 is not a hard landing detector. As stated in 3.B.(1), the primary source of identifying a suspected hard landing is the flight crew. Load report 15 data provides a snapshot of aircraft parameters before, at, and after an abnormal load condition either in the air or at touchdown. The report is generated for all landing, and is automatically printed or transmitted via ACARS, when one of its triggering conditions is met. These parameters give additional information which can be used by maintenance crew further to a flight crew report, in order to confirm if a hard landing occured and determine the need for, and level of, any subsequent inspection. Therefore, triggering of a load report 15 does not necessarily mean that a hard landing has occured. Nevertheless there have been cases on which load report 15 has triggered without pilot report and subsequent investigation has confirmed the hard landing. Hence Airbus recommend that whenever load report 15 is generated with trigger code 4XXX other than 4000, it should be systematically investigated and handled as a suspected hard landing and classified as detailed in subtask 05-51-11-941-052 B.(3) Action following a confirmed hard/overweight landing.
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NOTE : RALR, VRTA and GW are landing impact parameters indicated ____ on the FDIMU load report 15 (Ref. TASK 31-36-00-200-803).
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(2) Inspection requirements
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(a) After a hard / overweight landing, it is necessary to perform the hard / overweight landing inspection prior to the subsequent flight. To avoid unnecessary inspection, when there is a suspected hard / overweight landing (flight crew report, damage found on the aircraft, etc), it is possible to refer to the DFDRS / DMU / Load report 15 landing impact parameters to know if the landing was a hard / overweight landing.
R EFF : 002-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, 701-749, SROS
Page 609 Jan 01/07
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Subtask 05-51-11-941-056-A B. Procedure to confirm a Suspected Hard / Overweight Landing
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(1) Suspected Hard / Overweight Landing Definition. A suspected hard / overweight landing is a landing after which the flight crew make a reports of a hard / overweight landing.
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NOTE : It is the responsibility of the flight crew to make a report ____ if they think there was a hard / overweight landing.
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(2) Hard / Overweight landing confirmation After a suspected Hard / Overweight landing, and to avoid doing an unnecessary inspection, it is possible to consult the DFDRS or DMU / FDIMU load report 15 action chart to confirm that a hard / overweight landing occured and that the inspection is necessary.
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NOTE : If you do not (or if you cannot) read the landing impact ____ parameters from the load report 15, you must do the inspection after hard / overweight landing before the subsequent flight as in the instruction in paragraph 2.B.(3)(a)3 or paragraph 2.B.(3)(b)3. You can refer to the DMU / FDIMU load report 15 read out. You must do the inspection after hard / overweight landing.
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(3) Actions following a confirmed Hard / Overweight landing. (Ref. Fig. 602/TASK 05-51-11-991-054, 603/TASK 05-51-11-991-057, 604/TASK 05-51-11-991-058)
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(a) With GW <= MLW, the hard landing is split according to severity in 3 areas:
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1 _
ZONE 1: DELTA VRTA <= 1.0 g and RALR >= -10 ft/s or DELTA VRTA <= 0.75 g and |RALR| >= -13 ft/s No maintenance required
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2 _
ZONE 2: 1.0 g < DELTA VRTA <= 1.2 g and RALR >= -13 ft/s or 0.75 g < DELTA VRTA <= 1.2 g and -10 ft/s > RALR >= -13 ft/s Do this procedure: - perform the inspection as per paragraph 4 - download DFDR data (or QAR if available) - provide Airbus with DFDR raw data of the event, load report 15, pilot report, load trim sheet.
R EFF : 002-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, 701-749, SROS
Page 610 Jan 01/07
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Definition of Hard Landing (GW <= MLW) Figure 602/TASK 05-51-11-991-054
R EFF : 002-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, 701-749, SROS
Page 611 Jan 01/07
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Definition of Overweight Landing (GW > MLW) Figure 603/TASK 05-51-11-991-057
R EFF : 002-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, 701-749, SROS
Page 612 Jan 01/07
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Load Report 15 - Overweight / Hard Landing routes Figure 604/TASK 05-51-11-991-058
R EFF : 002-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, 701-749, SROS
Page 613 Jan 01/07
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- if no findings / damages as per paragraph 4., A/C can be returned temporarily to service for 30 days 100 Flight Cycles max (which ever occurs first) pending Airbus analysis of the event. - Airbus will assess the event for final clearance or further in structions.
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3 _
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ZONE 3: RALR < -13 ft/s or DELTA VRTA > 1.2 g Do this procedure: - Aircraft cannot return to service at this step without Airbus advice. - download DFDR data (or QAR if available) - immediately contact Airbus and provide DFDR raw data of the event, load report 15, pilot report, load trim sheet. - perform inspection as per paragraph 4 and report any findings / damages. - Airbus will analyse the event to assess if the aircraft can return to service.
(b) With GW > MLW, the overweight landing is described as follows:
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1 _
ZONE 1: DELTA VRTA <= 0.7 g and RALR >= -6 ft/s or DELTA VRTA <= 0.5 g and RALR >= -9 ft/s No maintenance required
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2 _
ZONE 2: 0.7 g < DELTA VRTA <= 0.8 g and RALR > -9 ft/s or 0.5 g < DELTA VRTA <= 0.8 g and -6 ft/s > RALR >= -9 ft/s Do this procedure: - perform the inspection as per paragraph 4 - download DFDR data (or QAR if available) - provide Airbus with DFDR raw data of the event, load report 15, pilot report, load trim sheet. - if no findings / damages as per paragraph 4., A/C can be returned temporarily to service for 30 days 100 Flight Cycles max (which ever occurs first) pending Airbus analysis of the event. - Airbus will assess the event for final clearance or further instructions.
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3 _
ZONE 3: RALR < -9 ft/s or DELTA VRTA > 0.8 g Aircraft cannot return to service at this step without Airbus advice Do this procedure: - download DFDR data (or QAR if available)
R EFF : 002-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, 701-749, SROS
Page 614 Jan 01/07
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- immediately contact Airbus and provide DFDR raw data of the event, load report 15, pilot report, load trim sheet. - perform inspection as per paragraph 4 and report any findings / damages. - Airbus will analyse the event to assess if the A/C can return to service. Subtask 05-51-11-941-057-A C. Inspection Preparation
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(1) We cannot give you accurate details of the inspection procedure to be applied after each incident. This is because there can be important variations in the weight, the speed and the direction of the loads. Thus, before you start, we recommand that you get information:
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(a) From the crew about the landing conditions. For exemple, find out: - if the touch down was on main gears or on main and nose gears or high pitch rate on nose gear. - if the landing was straight, drifting, wing-low, tail or nose heavy. - if the crew heard a noise possibly related to a structural failure.
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NOTE : After a hard / overweight landing, two cases have to be ____ considered with their applicable requirements: - hard touchdown on main gears only: In this case, the inspection of nose gear area is not required. - hard touchdown on nose and main gears: In this case the complete inspection is required.
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NOTE : Inspection are visual unless specified differently in the ____ text. Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures.
R EFF : 002-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, 701-749, SROS
Page 615 Jan 01/07
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**ON A/C ALL
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Subtask 05-51-11-941-058
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D. Safety Precautions
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(1) Put warning notices in the cockpit to tell persons not to operate the aircraft systems.
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(2) Install the safety devices on the landing gears (Ref. TASK 32-00-00481-801).
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(3) Put wheel chocks in position on the landing gears.
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(4) Lift the aircraft (Ref. TASK 07-11-00-581-801).
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NOTE : Lifting the aircraft is only necessary for the PHASE 2 ____ inspections.
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(5) Put the safety barriers in position.
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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 05-51-11-010-052
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E. Get Access
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(1) Open the main landing gear doors (Ref. TASK 32-12-00-010-801).
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(2) Open the nose landing gear doors (Ref. TASK 32-22-00-010-801).
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(3) Open the fan cowl doors (Ref. TASK 71-13-00-010-802). FOR 4030EM1 415BL, 416BR FOR 4030EM2 425BL, 426BR
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(4) Open the thrust reverser doors (Ref. TASK 78-30-00-010-801). FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR
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(5) Put an ACCESS PLATFORM 17M (56 FT) - ADJUSTABLE in position near the aircraft to do the inspection procedure.
R EFF : ALL 05-51-11 SROS
Page 616 Jan 01/07
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**ON A/C 701-749,
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Subtask 05-51-11-010-052-A
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E. Get Access
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(1) Open the main landing gear doors (Ref. TASK 32-12-00-010-801).
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(2) Open the nose landing gear doors (Ref. TASK 32-22-00-010-801).
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(3) Open the fan cowl doors (Ref. TASK 71-13-00-010-805). FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR
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(4) Open the thrust reverser doors (Ref. TASK 78-30-00-010-803). FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR
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(5) Put an ACCESS PLATFORM 17M (56 FT) - ADJUSTABLE in position near the aircraft to do the inspection procedure.
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**ON A/C ALL
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Subtask 05-51-11-860-052
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F. Aircraft Maintenance Configuration
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(1) Pressurize the Green hydraulic system (Ref. TASK 29-00-00-863-801).
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(2) Pressurize the Yellow hydraulic system (Ref. TASK 29-00-00-863-803).
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(3) Pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-802).
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(4) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801).
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(5) Fully extend the flaps (Ref. TASK 27-50-00-866-801)
R EFF : ALL 05-51-11 SROS
Page 617 Jan 01/07
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(6) Fully extend the slats (Ref. TASK 27-80-00-866-801).
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(7) Fully extend the spoilers (Ref. TASK 27-60-00-866-801).
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(8) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801).
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(9) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803).
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(10) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802).
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(11) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
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4. Procedure _________
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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 05-51-11-210-087
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A. Inspection of the Pylon (Ref. Fig. 605/TASK 05-51-11-991-005, 606/TASK 05-51-11-991-009, 607/TASK 05-51-11-991-018, 608/TASK 05-51-11-991-021, 609/TASK 05-51-11-991-022) (Ref. TASK 71-00-00-000-803), (Ref. TASK 28-25-00-650-803).
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NOTE : Inspections are visual unless specified differently in the text. ____ Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures.
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If there is damage on the aircraft structure, refer to the Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures. If it is necessary to open (remove) access panels and doors, examine them. Make sure that : - They are aligned correctly, - They have no distortion or cracks, - The paint is not damaged, - All the fasteners and safety devices are in the correct position
R EFF : ALL 05-51-11 SROS
Page 618 Jan 01/07
Inboard Engine-Pylon Station Figure 605/TASK 05-51-11-991-005
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EFF : 001-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, SROS
Page 619 Jan 01/07
Engine-Pylon Station Figure 605A/TASK 05-51-11-991-005-A
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EFF : 701-749, 05-51-11 SROS
Page 620 Jan 01/07
Pylon Box Figure 606/TASK 05-51-11-991-009
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EFF : 001-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, SROS
Page 621 Jan 01/07
Pylon Box Figure 606A/TASK 05-51-11-991-009-A
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EFF : 701-749, 05-51-11 SROS
Page 622 Jan 01/07
Engine-to-pylon Attach Fittings Figure 607/TASK 05-51-11-991-018
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R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, SROS
Page 623 Jan 01/07
Engine-to-pylon Attach Fittings Figure 607A/TASK 05-51-11-991-018-A
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R EFF : 701-749, 05-51-11 SROS
Page 624 Jan 01/07
Pylon-to-Wing Forward Attach-Fittings Figure 608/TASK 05-51-11-991-021
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R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, SROS
Page 625 Jan 01/07
Pylon-to-Wing Forward Attach Fittings Figure 608A/TASK 05-51-11-991-021-A
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R EFF : 701-749, 05-51-11 SROS
Page 626 Jan 01/07
Pylon-to-Wing Aft Attach-Fittings Figure 609/TASK 05-51-11-991-022
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R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, SROS
Page 627 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Engine Pylons | | | | | | | | | | | | | | | | A.| | Examine externally: | X | | | | | | | | the doors, all the pylon panels, the | | | | | | | | | secondary structure (forward and aft) | | | | | | | | | and the bottom fairing (forward, | | | | | | | | | center and aft) for: | | | | | | | | | - buckling, cracks and pulled or | | | | | | | | | missing fasteners. | | | | | | | | | | | | | | | | B.| | Examine the primary structure and | X | | | | | | | | pylon lower area for distortion | | | | | | | | | and cracks, the condition of the | | | | | | | | | paint, loose rivets, signs of | | | | | | | | | shearing. | | | | | | | | | | | | | | | | C.| | If you find damage during the | | | | | | | | | inspection of the Pylon: | | | | | | | | | | | | | | | | | | (1) Remove or open the access doors | | X | | | | | | | and panels. | | | | | | | | | (2) Examine the panels and the | | X | | | | | | | adjacent structure for | | | | | | | | | distortion, buckles, wrinkles or | | | | | | | | | tears. | | | | | | | | | - the plates have no buckles, | | | | | | | | | wrinkles or tears where they | | | | | | | | | are riveted to the panels. | | | | | | | | | (3) Do an internal inspection of the | | X | | | | | | | pylon box (primary structure) for | | | | | | | | | distortion. | | | | | | | | | (4) Examine the spars connected to | | X | | | | | | | the side panels for: | | | | | | | | | - correct condition and damage. | | | | | | | | | (5) Examine the attachment between | | X | | | | | | | the main ribs (1, 10, 12 and 18A),| | | | | | | | | the side panels, the upper and | | | | | | | | | lower spars for damage. | | | | | | | | | (6) Examine the fire protection | | X | | | | | | | system for damage, specially the | | | | | | | | | the attachments of the fire | | | | | | | | | extinguisher bottles and | | | | | | | | | extinguishing distribution pipes. | | | | | |
R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, SROS
Page 628 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (7) Examine the electrical cables, | | X | | | | | | | the hydraulic pipes, the fuel | | | | | | | | | pipes, the components of the | | | | | | | | | engine air-bleed system and | | | | | | | | | draining pipes for damage. | | | | | | | | | (8) Examine the different components | | | | | | | | | installed on the primary | | | | | | | | | structure. | | | | | | | | | | | | | | | | | | If you find damage: | | | | | | | | | (a) Remove the engine | | | X | | | | | | (Ref. TASK 71-00-00-000-803). | | | | | | | | | (b) Examine the engine-to-pylon | | | X | | | | | | attach fitting at the head of | | | | | | | | | Rib 1 (pyramid) and under Rib 10 | | | | | | | | | for: | | | | | | | | | - cracks, distortion, rupture and | | | | | | | | | signs of oxydation or burning. | | | | | | | | | (c) Remove the pylon-to-wing center | | | | | | | | | fillets. | | | | | | | | | (d) Do a detailed visual inspection | | | | | | | | | of the forward attach fitting | | | | | | | | | at Rib 12. | | | | | | | | | (e) Do a detailed visual inspection | | | X | | | | | | of the spigot between Rib 12 | | | | | | | | | and 13 for: | | | | | | | | | - damage buckling, cracks and | | | | | | | | | pulled or missing fasteners. | | | | | | | | | (f) Do a detailed visual inspection | | | X | | | | | | of the rear attach fitting at | | | | | | | | | Rib 18. | | | | | | | | | (g) Do a detailed visual inspection | | | X | | | | | | of the ball-bearings installed at | | | | | | | | | Rib 18A and examine the inner and | | | | | | | | | outer ball surfaces for cracks. | | | | | | | | | | | | | | | | | | If you find damage: | | | | | | | | | (h) Defuel the wing | | | X | | | | | | (Ref. TASK 28-25-00-650-803). | | | | | | | | | (i) Get access to the internal | | | X | | | | | | structure adjacent to Ribs 14, | | | | | | | | | 14A, 25 and 26. | | | | | | | | | Examine these items: | | | | | |
R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, SROS
Page 629 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - the rear face of the front spar | | | | | | | | | - the front face of the rear spar | | | | | | | | | - the pylon forward attachment | | | | | | | | | - the pylon aft attachment | | | | | | | | | - the stringers and brackets for: | | | | | | | | | - no damage, cracks, correct | | | | | | | | | condition of the paint and | | | | | | | | | sealant. | | | | | | | | | (j) Examine all the pipes and holes | | | X | | | | | | for: | | | | | | | | | - correct attachment and leakage. | | | | | | -------------------------------------------------------------------------------
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Subtask 05-51-11-210-088
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B. Inspection of the nacelles (Ref. TASK 78-31-00-710-804)
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NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Nacelles | | | | | | | | | | | | | | | | A.| | Do an external inspection of: | X | | | | | | | | the air intake cowls, the fan cowls | | | | | | | | | and the thrust reverser cowls for | | | | | | | | | distortion, cracks and delamination. | | | | | | | | | Make sure that: | | | | | | | | | - the paint is not cracked or flaked | | | | | | | | | - the rivets are not loose | | | | | | | | | - there are no signs of shearing. | | | | | | | | | | | | | | | | | | If you find damage during the | | | | | | | | | inspection : | | | | | | | | | | | | | | | | B.| | Do an internal inspection of the | | X | | | | | | | same items for damage. | | | | | |
R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, SROS
Page 630 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | | | | | | | | C.| | Examine all the cowl latches for | | X | | | | | | | damage. | | | | | | | | | Make sure that they operate | | | | | | | | | correctly. | | | | | | | | | If you find damage on the thrust | | | | | | | | | reverser cowls: | | | | | | | | | - do an operational test of the | | | X | | | | | | thrust reverser system. Make sure | | | | | | | | | that the thrust reversers can move | | | | | | | | | fully and freely | | | | | | | | | (Ref. TASK 78-31-00-710-804). | | | | | | -------------------------------------------------------------------------------
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Subtask 05-51-11-210-089
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C. Inspection of the Engines (Ref. TASK 71-00-00-720-821), (Ref. TASK 79-2211-200-801), (Ref. TASK 71-00-00-000-803)
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Engines | | | | | | | | | | | | | | | | A.| | Turn the fan rotor by hand | X | | | | | | | | Make sure that: | | | | | | | | | there is no bearing roughness, | | | | | | | | | unusual noises and bindings (high | | | | | | | | | rubbing of the seals and the | | | | | | | | | shrouds is normal). | | | | | | | | | | | | | | | | B.| | Examine the primary nozzle for damage | X | | | | | | | | (distortion, cracks, loose and | | | | | | | | | missing rivets, signs of shearing | | | | | | | | | or delamination). | | | | | | | | | Make sure that it is correctly | | | | | | | | | attached to the engine. | | | | | | | | | | | | | | | | C.| | Examine the nose cowl attachments | X | | | | | | | | to the fan case for distortion, | | | | | | | | | delamination, cracks. | | | | | | | | | Make sure that the fasteners are not | | | | | |
R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, SROS
Page 631 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | pulled or torn. | | | | | | | | | | | | | | | | D.| | If you find damage during the | | | | | | | | | inspection on the Engines: | | | | | | | | | | | | | | | | | | (1) Do a full inspection of the | | X | | | | | | | engine. | | | | | | | | | (2) If you find a minor seal or | | X | | | | | | | shroud interference the engine | | | | | | | | | is serviceable after you do a | | | | | | | | | satisfactory power assurance | | | | | | | | | check. | | | | | | | | | (3) After the test, examine the | | X | | | | | | | magnetic chip detectors and | | | | | | | | | the elements of the scavenge | | | | | | | | | oil filter. | | | | | | | | | Make sure that there are no | | | | | | | | | signs of bearing distress. | | | | | | | | | (Ref. TASK 79-22-11-200-801). | | | | | | | | | If you find damage: | | | | | | | | | - remove the engine | | | X | | | -------------------------------------------------------------------------------
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**ON A/C 701-749,
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Subtask 05-51-11-210-087-A
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A. Inspection of the Pylon (Ref. Fig. 605A/TASK 05-51-11-991-005-A, 606A/TASK 05-51-11-991-009-A, 607A/TASK 05-51-11-991-018-A, 608A/TASK 05-51-11-991-021-A, 609A/TASK 0551-11-991-022-A) (Ref. TASK 71-00-00-000-805), (Ref. TASK 28-25-00-650-803).
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NOTE : Inspections are visual unless specified differently in the text. ____ Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures.
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If there is damage on the aircraft structure, refer to the Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures. If it is necessary to open (remove) access panels and doors, examine them. Make sure that :
R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, 701-749, SROS
Page 632 Jan 01/07
Pylon-to-Wing Aft Attach-fittings Figure 609A/TASK 05-51-11-991-022-A
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R EFF : 701-749, 05-51-11 SROS
Page 633 Jan 01/07
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They are aligned correctly, They have no distortion or cracks, The paint is not damaged, All the fasteners and safety devices are in the correct position
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Engine Pylons | | | | | | | | | | | | | | | | A.| | Examine externally: | X | | | | | | | | the doors, all the pylon panels, the | | | | | | | | | secondary structure (forward and aft) | | | | | | | | | and the bottom fairing (forward, | | | | | | | | | center and aft) for: | | | | | | | | | - buckling, cracks and pulled or | | | | | | | | | missing fasteners. | | | | | | | | | | | | | | | | B.| | Examine the primary structure and | X | | | | | | | | pylon lower area for distortion | | | | | | | | | and cracks, the condition of the | | | | | | | | | paint, loose rivets, signs of | | | | | | | | | shearing. | | | | | | | | | | | | | | | | C.| | If you find damage during the | | | | | | | | | inspection of the pylon: | | | | | | | | | | | | | | | | | | (1) Remove or open the access doors | | X | | | | | | | and panels. | | | | | | | | | (2) Examine the panels and the | | X | | | | | | | adjacent structure for | | | | | | | | | distortion buckles, wrinkles or | | | | | | | | | tears: | | | | | | | | | - the plates have no buckles, | | | | | | | | | wrinkles or tears where they | | | | | | | | | are riveted to the panels. | | | | | | | | | (3) Do an internal inspection of the | | X | | | | | | | pylon box (primary structure) for | | | | | | | | | distortion. | | | | | | | | | (4) Examine the spars connected to | | X | | | | | | | the side panels for: | | | | | | | | | - correct condition and damage. | | | | | | | | | (5) Examine the attachment between | | X | | | | | | | the main ribs (1, 10, 12 and 18A),| | | | | | | | | the side panels, the upper and | | | | | | | | | lower spars for damage. | | | | | |
R EFF : 701-749, 05-51-11 SROS
Page 634 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (6) Examine the fire protection | | X | | | | | | | system for damage, specially the | | | | | | | | | the attachments of the fire | | | | | | | | | extinguisher bottles and | | | | | | | | | extinguishing distribution pipes. | | | | | | | | | (7) Examine the electrical cables, | | X | | | | | | | the hydraulic pipes, the fuel | | | | | | | | | pipes, the components of the | | | | | | | | | engine air-bleed system and | | | | | | | | | draining pipes for damage. | | | | | | | | | (8) Examine the different components | | | | | | | | | installed on the primary | | | | | | | | | structure. | | | | | | | | | | | | | | | | | | If you find damage: | | | | | | | | | (a) Remove the engine | | | X | | | | | | (Ref. TASK 71-00-00-000-805). | | | | | | | | | (b) Examine the engine-to-pylon | | | X | | | | | | attach fitting at the head of | | | | | | | | | Rib 1 (pyramid) and under Rib 10 | | | | | | | | | for: | | | | | | | | | - cracks distorsion rupture and | | | | | | | | | signs of oxydation or burning. | | | | | | | | | (c) Remove the pylon-to-wing center | | | | | | | | | fillets. | | | | | | | | | (d) Do a detailed visual inspection | | | | | | | | | of the forward attach fitting | | | | | | | | | at Rib 12. | | | | | | | | | (e) Do a detailed visual inspection | | | X | | | | | | of the spigot between Rib 12 | | | | | | | | | and 13 for: | | | | | | | | | - damage bulking, cracks and | | | | | | | | | pulled or missing fasteners. | | | | | | | | | (f) Do a detailed visual inspection | | | X | | | | | | of the rear attach fitting at | | | | | | | | | Rib 18. | | | | | | | | | (g) Do a detailed visual inspection | | | X | | | | | | of the ball-bearings installed at | | | | | | | | | Rib 18A and examine the inner and | | | | | | | | | outer ball surfaces for cracks. | | | | | | | | | | | | | | | | | | If you find damage: | | | | | | | | | (h) Defuel the wing | | | X | | |
R EFF : 701-749, 05-51-11 SROS
Page 635 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (Ref. TASK 28-25-00-650-803). | | | | | | | | | (i) Get access to the internal | | | X | | | | | | structure adjacent to Ribs 14, | | | | | | | | | 14A, 25 and 26. | | | | | | | | | Examine of these items: | | | | | | | | | - the rear face of the front spar | | | | | | | | | - the front face of the rear spar | | | | | | | | | - the pylon forward attachment | | | | | | | | | - the pylon aft attachment | | | | | | | | | - the stringers and brackets for: | | | | | | | | | - no damage, cracks, correct | | | | | | | | | condition of the paint and | | | | | | | | | sealant. | | | | | | | | | (j) Examine all the pipes and holes | | | X | | | | | | for: | | | | | | | | | - correct attachment and leakege | | | | | | -------------------------------------------------------------------------------
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Subtask 05-51-11-210-088-A
R R
B. Inspection of the nacelles (Ref. TASK 78-31-00-740-802)
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NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures.
R R R R R R R R R R R R R R R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Nacelles | | | | | | | | | | | | | | | | A.| | Do an external inspection of: | X | | | | | | | | the air intake cowls, the fan cowls | | | | | | | | | and the thrust reverser cowls for | | | | | | | | | distortion, cracks and delamination. | | | | | | | | | Make sure that: | | | | | | | | | - the paint is not cracked or flaked | | | | | | | | | - the rivets are not loose | | | | | | | | | - there are no signs of shearing. | | | | | | | | | | | | | | |
R EFF : 701-749, 05-51-11 SROS
Page 636 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | If you find damage during the | | | | | | | | | inspection : | | | | | | | | | | | | | | | | B.| | Do an internal inspection of the | | X | | | | | | | same items for damage. | | | | | | | | | | | | | | | | C.| | Examine all the cowl latches for | | X | | | | | | | damage. | | | | | | | | | Make sure that they operate | | | | | | | | | correctly. | | | | | | | | | If you find damage on the thrust | | | | | | | | | reverser cowls: | | | | | | | | | - do an operational test of the | | | X | | | | | | thrust reverser system. Make sure | | | | | | | | | that the thrust reversers can move | | | | | | | | | fully and freely | | | | | | | | | ( ref. TASK 78-31-00-740-802). | | | | | | -------------------------------------------------------------------------------
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Subtask 05-51-11-210-089-A
R R
C. Inspection of the Engines (Ref. TASK 71-00-00-700-834), (Ref. TASK 79-0000-200-805), (Ref. TASK 71-00-00-000-805)
R R R R R R R R R R R R R R R R R R R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Engines | | | | | | | | | | | | | | | | A.| | Turn the fan rotor by hand | X | | | | | | | | Make sure that: | | | | | | | | | there is no bearing roughness, | | | | | | | | | unusual noises and bindings (high | | | | | | | | | rubbing of the seals and the | | | | | | | | | shrouds is normal). | | | | | | | | | | | | | | | | B.| | Examine the primary nozzle for damage | X | | | | | | | | (distortion, cracks, loose and | | | | | | | | | missing rivets, signs of shearing | | | | | | | | | or delamination). | | | | | | | | | Make sure that it is correctly | | | | | | | | | attached to the engine. | | | | | |
R EFF : 701-749, 05-51-11 SROS
Page 637 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | | | | | | | | C.| | Examine the nose cowl attachments | X | | | | | | | | to the fan case for distortion, | | | | | | | | | delamination, cracks. | | | | | | | | | Make sure that the fasteners are not | | | | | | | | | pulled or torn. | | | | | | | | | | | | | | | | D.| | If you find damage during the | | | | | | | | | inspection on the Engines: | | | | | | | | | | | | | | | | | | (1) Do a full inspection of the | | X | | | | | | | engine. | | | | | | | | | (2) If you find a minor seal or | | X | | | | | | | shroud interference the engine | | | | | | | | | is serviceable after you do a | | | | | | | | | satisfactory power assurance | | | | | | | | | check. | | | | | | | | | (3) After the test, examine the | | X | | | | | | | magnetic chip detectors and | | | | | | | | | the elements of the scavenge | | | | | | | | | oil filter. | | | | | | | | | Make sure that there are no | | | | | | | | | signs of bearing distress. | | | | | | | | | (Ref. TASK 79-00-00-200-805). | | | | | | | | | If you find damage: | | | | | | | | | - remove the engine | | | X | | | -------------------------------------------------------------------------------
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**ON A/C ALL
R
Subtask 05-51-11-210-090
R R R
D. Inspection of the Landing Gears (Ref. Fig. 610/TASK 05-51-11-991-023) (Ref. TASK 32-11-00-220-801), (Ref. TASK 32-11-00-220-802).
R R R R
NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures.
R EFF : ALL 05-51-11 SROS
Page 638 Jan 01/07
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 R R R R R R R R R R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Main Landing Gear | | | | | | | | | | | | | | | | | | Do a detailed inspection of these | X | | | | | | | | parts: | | | | | | | | | - the MLG leg assembly | | | | | | | | | - the MLG side stay assembly | | | | | | | | | - the articulating link | | | | | | | | | - the bogie beam assembly | | | | | | | | | - the bogie alignement pitch trimmer | | | | | | | | | - the torque links | | | | | | | | | - the brake rod | | | | | | | | | Make sure that there is no: | | | | | | | | | - distortion | | | | | | | | | - neckings | | | | | | | | | - damage to protective finish | | | | | | | | | - cracking | | | | | | | | | - excessive wear | | | | | | | | | - fretting | | | | | | | | | - scores, dents and burrs | | | | | | | | | | | | | | | | B.| | Make sure that the MLG sefety lock | X | | | | | | | | can be installed easily. | | | | | | | | | | | | | | | | C.| | Examine the wheels and the tires for | X | | | | | | | | unusual damage or distortion. | | | | | | | | | | | | | | | | D.| | Do a detailed visual inspection of | X | | | | | | | | the main gear for damage or distortion| | | | | | | | | at static and dynamic joints | | | | | | | | | (Ref. TASK 32-11-00-220-801). | | | | | | | | | | | | | | | | E.| | Remove and do a detailed inspection | | X | | | | | | | of the MLG lower articulating link. | | | | | | | | | Measure the dimention z between the | | | | | | | | | hole centers. | | | | | | | | | NOTE: If the distance is more than | | | | | | | | | 599.05 mm (23.5846 in.), you | | | | | | | | | must tell Airbus and wait for | | | | | | | | | instructions. | | | | | | | | | | | | | | | | | | If you find damage or distortion, or | | | | | | | | | if you think that a distortion | | | | | | | | | occured. | | | | | |
R EFF : ALL 05-51-11 SROS
Page 639 Jan 01/07
Main Landing Gear Figure 610/TASK 05-51-11-991-023- 14 (SHEET 1)
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R EFF : ALL 05-51-11 SROS
Page 640 Jan 01/07
Main Landing Gear Figure 610/TASK 05-51-11-991-023- 24 (SHEET 2)
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R EFF : ALL 05-51-11 SROS
Page 641 Jan 01/07
Main Landing Gear Figure 610/TASK 05-51-11-991-023- 34 (SHEET 3)
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R EFF : ALL 05-51-11 SROS
Page 642 Jan 01/07
Main Landing Gear Figure 610/TASK 05-51-11-991-023- 44 (SHEET 4)
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R EFF : ALL 05-51-11 SROS
Page 643 Jan 01/07
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 R R R R R R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | | | | | | | | | | (1) Do a check of these parts: | | X | | | | | | | - main gear complete | | | | | | | | | - main fitting | | | | | | | | | - side stay assembly | | | | | | | | | - shock absorber | | | | | | | | | - pitch trimmer and articulating | | | | | | | | | link | | | | | | | | | - bogie beam | | | | | | | | | - axles. | | | | | | | | | If you can isolate the source of | | | | | | | | | the damage or distortion. | | | | | | | | | | | | | | | | | | (2) Remove the applicable primary | | | X | | | | | | component for maintenance. | | | | | | | | | | | | | | | | | | (3) Do a pressure/extension check of | | X | | | | | | | the shock absorber. | | | | | | | | | (Ref. TASK 32-11-00-220-802) | | | | | | | | | | | | | | | | | | | | | | | | |2. | | Inspection of the Main Gear Fittings | | | | | | | | | | | | | | | | A.| | Do a detailed visual inspection of | X | | | | | | | | these parts (and their attachment | | | | | | | | | points): | | | | | | | | | - the forward pintle-pin fitting | | | | | | | | | - the rear pintle-pin fitting | | | | | | | | | - the gear rib 6 | | | | | | | | | - the bellcrank of the main gear | | | | | | | | | actuator | | | | | | | | | - the side stay attachment fitting | | | | | | | | | - the main gear actuator fittings. | | | | | | | | | Make sure that: | | | | | | | | | - there are no cracks, damage or | | | | | | | | | distortion | | | | | | | | | - the paint is not damaged | | | | | | | | | - the sealant is in correct condition | | | | | | | | | - there are no fluid leaks (fuel | | | | | | | | | where applicable). | | | | | | | | | | | | | | | | B.| | If there is damage or distortion at | | | | | | | | | the rear spar, get access to the fuel | | | | | |
R EFF : ALL 05-51-11 SROS
Page 644 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | tank (adjacent to the applicable area)| | | | | | | | | | | | | | | | | | (1) Do a detailed visual inspection | | X | | | | | | | of the internal structure adjacent| | | | | | | | | to the external damage. | | | | | | | | | Make sure that: | | | | | | | | | - there is no damaged paint | | | | | | | | | - there are no cracks in the | | | | | | | | | structure | | | | | | | | | - the sealant and the sealant bead| | | | | | | | | are in the correct condition | | | | | | | | | - the fasteners are correct | | | | | | | | | - the secondary structure, ribs, | | | | | | | | | riblets, stringers, brackets | | | | | | | | | and plates are not damaged | | | | | | | | | - the pipes, electrical cables | | | | | | | | | and raceways are not damaged. | | | | | | -------------------------------------------------------------------------------
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Subtask 05-51-11-210-091
R R
E. Inspection of the Nose Landing Gear (Ref. Fig. 611/TASK 05-51-11-991-025, 612/TASK 05-51-11-991-026)
R R R R
NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures.
R R R R R R R R R R R R R R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Nose Landing Gear | | | | | | | | | | | | | | | | A.| | Examine the wheels and tires for | X | | | | | | | | unusual damage or distortion. | | | | | | | | | (Ref. TASK 32-41-00-210-802) | | | | | | | | | | | | | | | | B.| | Do a detailed visual inspection of | X | | | | | | | | these parts: | | | | | | | | | - the NLG leg assembly | | | | | | | | | - the NLG drag stay assembly | | | | | |
R EFF : ALL 05-51-11 SROS
Page 645 Jan 01/07
Nose Landing Gear Figure 611/TASK 05-51-11-991-025
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R EFF : ALL 05-51-11 SROS
Page 646 Jan 01/07
Nose Landing-Gear Section between FR11 and FR17 Figure 612/TASK 05-51-11-991-026
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R EFF : ALL 05-51-11 SROS
Page 647 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - the torque links | | | | | | | | | Make sure that there is no: | | | | | | | | | - distortion | | | | | | | | | - necking | | | | | | | | | - damage to protective finish | | | | | | | | | - cracking | | | | | | | | | - excessive wear | | | | | | | | | - fretting | | | | | | | | | - scores, dents and burrs. | | | | | | | | | | | | | | | | | | If you find damage or distortion, or | | | | | | | | | if you think that a distortion | | | | | | | | | occurred. | | | | | | | | | | | | | | | | | | (1) Do a check of these parts: | | X | | | | | | | - nose gear complete | | | | | | | | | - nose fitting | | | | | | | | | - drag stay assembly | | | | | | | | | - shock absorber | | | | | | | | | - axles. | | | | | | | | | If you can isolate the source of | | | | | | | | | damage or distortion: | | | | | | | | | (2) Remove the applicable primary | | | X | | | | | | component for maintenance. | | | | | | | | | (3) Do a pressure/extension check of | | X | | | | | | | the shock absorber. | | | | | | | | | (Ref. TASk 32-21-00-220-803) | | | | | | | | | | | | | | | | C.| | Make sure that the NLG safety lock | X | | | | | | | | can be installed easily. | | | | | | | | | | | | | | | | D.| | Examine the nose gear upper strut | X | | | | | | | | attachments between FR11 and FR11A. | | | | | | | | | Examine the area around the bearing, | | | | | | | | | the attachment of the fitting on the | | | | | | | | | forward frame and roof of the nose | | | | | | | | | wheel well and the link rods. | | | | | | | | | | | | | | | | E.| | Examin the nose gear actuating | X | | | | | | | | cylinder attachment fitting (FR13). | | | | | | | | | Examin the attachment of the actuating| | | | | | | | | cylinder fitting to the apper link | | | | | | | | | at FR13 and FR14. | | | | | |
R EFF : ALL 05-51-11 SROS
Page 648 Jan 01/07
R R R R R R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | | | | | | | | F. | Examin the nose gear leg attachments | X | | | | | | | | between FR16A and FR17. | | | | | | | | | Examine the attachments and the | | | | | | | | | longitudinal beams. | | | | | | -------------------------------------------------------------------------------
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Subtask 05-51-11-210-101
R
F. Inspection of the Landing Gear Doors (Ref. TASK 32-31-00-710-801).
R R R R
NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures.
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
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Main Landing Gear | | | | | | | | | Doors | | | | | | | | | | | | | | | | A.| | Do an inspection of the doors, the | X | | | | | | | | hinges and the adjacent structure. | | | | | | | | | | | | | | | | | | If you find damage on the doors, the | | | | | | | | | attached parts or adjacent structure: | | | | | | | | | (1) Do a check of the into-wind and | | X | | | | | | | out-of-wind tolerances of the | | | | | | | | | doors with the landing gear | | | | | | | | | retracted | | | | | | | | | | | | | | | |2. | | Inspection of the Nose-Landing-Gear | | | | | | | | | Doors | | | | | | | | | | | | | | | | A.| | Do an inspection of the doors, the | X | | | | | | | | hinges and the adjacent structure. | | | | | | | | | | | | | | | | | | If you find damage on the doors, the | | | | | | | | | attached parts or adjacent structure: | | | | | | | | | (1) Do a check of the into-wind and | | X | | | | | | | out-of-wind tolerances of the | | | | | |
R EFF : ALL 05-51-11 SROS
Page 649 Jan 01/07
R R R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | doors with the landing gear | | | | | | | | | retracted | | | | | | -------------------------------------------------------------------------------
R
Subtask 05-51-11-210-093
R
G. Inspection of the Flap Operating Mechanism (Ref. TASK 27-54-00-200-801).
R R R R
NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures.
R R R R R R R R R R R R R R R R R R R R R R R R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Flap Operating | | | | | | | | | Mechanism | | | | | | | | | | | | | | | | A.| | Do an inspection of the flap | X | | | | | | | | operating mechanism | | | | | | | | | (Ref. TASK 27-54-00-200-80100). | | | | | | | | | | | | | | | | B.| | If you find damage on the Flap | | | | | | | | | operating mechanism: | | | | | | | | | (1) Remove the applicable components | | X | | | | | | | for maintenance. | | | | | | | | | | | | | | | | C.| | Do an inspection of the component | | X | | | | | | | attachments. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the component attachments | | | X | | | | | | and do an inspection of the | | | | | | | | | component attachment/structure | | | | | | | | | interface. | | | | | | -------------------------------------------------------------------------------
R EFF : ALL 05-51-11 SROS
Page 650 Jan 01/07
R R R
Subtask 05-51-11-210-094 H. Check after damage on the Flap-Track Attachment Fittings (Ref. TASK 2825-00-650-803).
R R R R
NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures.
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
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Flap-Track Forward | | | | | | | | | Attachment-Fittings, Tracks 2 thru | | | | | | | | | 5 | | | | | | | | | | | | | | | | A.| | Do a detailed visual inspection of | X | | | | | | | | the forward attachment brackets of | | | | | | | | | the flap track beam. | | | | | | | | | Make sure that: | | | | | | | | | - all fasteners are in the correct | | | | | | | | | condition | | | | | | | | | - there are no cracks | | | | | | | | | - the spherical bearings did not | | | | | | | | | move | | | | | | | | | - there are no leaks in the area of | | | | | | | | | the brackets | | | | | | | | | - the structure in the area of the | | | | | | | | | brackets is not distorted | | | | | | | | | - the beam-to-wing clearance is | | | | | | | | | correct. | | | | | | | | | | | | | | | | | | If you find damage: | | | | | | | | | (1) Defuel the wing | | X | | | | | | | (2) Open the tank to the air. | | X | | | | | | | (3) Remove the flap track beam. | | X | | | | | | | (4) Do a general internal inspection | | X | | | | | | | at the area of damage and the | | | | | | | | | adjacent area. | | | | | | | | | | | | | | | |2. | | Inspection of the Attachment Fittings | | | | | | | | | of the Aft Flap Tracks No. 2 thru | | | | | | | | | No. 5 | | | | | | | | | | | | | | | | A.| | Do a detailed visual inspection of the| X | | | | |
R EFF : ALL 05-51-11 SROS
Page 651 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | attachment fittings of flap track | | | | | | | | | No. 2 for cracks, damage or | | | | | | | | | distortion. | | | | | | | | | Make sure that the spherical bearing | | | | | | | | | did not move on: | | | | | | | | | - the spigot fitting | | | | | | | | | - the spherical bearing | | | | | | | | | - the cantilever structure of the | | | | | | | | | bearing support ribs. | | | | | | | | | | | | | | | | B.| | Attachment fittings of the Aft-Flap | | | | | | | | | tracks 2 thru 5 | | | | | | | | | | | | | | | | | | If you find damage: | | | | | | | | | (1) Defuel the wing | | X | | | | | | | (2) Open the wing tank to the air. | | X | | | | | | | (3) Do a general internal inspection | | X | | | | | | | at the damaged area and the | | | | | | | | | adjacent area. | | | | | | | | | | | | | | | | B.| | Do a detailed visual inspection of | X | | | | | | | | the flap-tracks No. 3 thru 5 aft | | | | | | | | | attachment-fittings attached to the | | | | | | | | | rear spar for cracks, fuel leaks or | | | | | | | | | damage. | | | | | | | | | Make sure that the fasteners are in | | | | | | | | | the correct condition. | | | | | | -------------------------------------------------------------------------------
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Subtask 05-51-11-210-102
R R R R R
J. Inspection of the Wing (Ref. Fig. 613/TASK 05-51-11-991-027) (Ref. TASK 57-56-11-000-801), (Ref. TASK 57-56-11-000-802), (Ref. TASK 28-25-00-650-803), (Ref. TASK 27-54-00-710-801), (Ref. TASK 57-56-11-000803).
R R R
NOTE : Refer to the AD F-2006-008 for other possible inspection ____ requirements for the wing bottom skin (at Rib 6 - STGR20) before the subsequent flight.
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NOTE : All the inspections are visual unless specified differently in the ____ text.
R EFF : ALL 05-51-11 SROS
Page 652 Jan 01/07
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Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Upper Wing Skin from| | | | | | | | | Rib 1 to Wing Tip | | | | | | | | | | | | | | | | A.| | Examine this part for cracks, | X | | | | | | | | distortion, paint and sealant | | | | | | | | | damage. | | | | | | | | | Make sure that the fasteners are | | | | | | | | | in the correct condition. | | | | | | | | | Carefully examine the | | | | | | | | | fasteners at the rear spar between | | | | | | | | | rib 10 and rib 10A and between | | | | | | | | | rib 25 and rib 26. | | | | | | | | | | | | | | | | B.| | If you find damage adjacent to the | | | | | | | | | flap beams No. 2, 3, or 4. | | | | | | | | | (1) Remove the applicable flap beam | | X | | | | | | | fairing: | | | | | | | | | - for fairing No. 2 | | | | | | | | | (Ref. TASK 57-56-11-000-801) | | | | | | | | | - for fairing No. 3 | | | | | | | | | (Ref. TASK 57-56-11-000-802). | | | | | | | | | - for fairing No. 4 | | | | | | | | | (Ref. TASK 57-56-11-000-803). | | | | | | | | | | | | | | | |2. | | Inspection of the Lower Wing Skin | | | | | | | | | from Rib 1 to Wing Tip | | | | | | | | | | | | | | | | A.| | Carefully examine the areas adjacent | X | | | | | | | | to the flap beams, the engine pylons | | | | | | | | | and the MLG attachments for cracks, | | | | | | | | | distortion, fluid leaks, paint and | | | | | | | | | sealant damage. Make sure that the | | | | | | | | | fasteners are in the correct | | | | | | | | | condition. | | | | | | | | | | | | | | | |3. | | Inspection of the Flap Beam Assembly | | | | | | | | | and the Flap Track | | | | | | | | | | | | | | | | A.| | Examine these parts for damage or | X | | | | | | | | cracks. | | | | | |
R EFF : ALL 05-51-11 SROS
Page 653 Jan 01/07
Structure of the Wing Figure 613/TASK 05-51-11-991-027- 13 (SHEET 1)
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R EFF : ALL 05-51-11 SROS
Page 654 Jan 01/07
Structure of the Wing Figure 613/TASK 05-51-11-991-027- 23 (SHEET 2)
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R EFF : ALL 05-51-11 SROS
Page 655 Jan 01/07
Structure of the Wing Figure 613/TASK 05-51-11-991-027- 33 (SHEET 3)
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R EFF : ALL 05-51-11 SROS
Page 656 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | Make sure that: | | | | | | | | | - the paint and sealant are not | | | | | | | | | damaged | | | | | | | | | - the fasteners and safety devices | | | | | | | | | are in the correct condition | | | | | | | | | - the clearance to the wing is | | | | | | | | | correct. | | | | | | | | | | | | | | | | B.| | If you find damage to the flap beam | | | | | | | | | or flap track: | | | | | | | | | (1) Remove the applicable flap beam | | | X | | | | | | assembly for component | | | | | | | | | maintenance. | | | | | | | | | (2) Get access to the area adjacent | | | X | | | | | | to the applicable flap beam. | | | | | | | | | Do a general internal inspection | | | | | | | | | of the ribs, the internal side of | | | | | | | | | the lower skin, the internal face | | | | | | | | | of the rear spar for beams 3 and | | | | | | | | | 4, the internal face of the false | | | | | | | | | rear spar for the No. 2 beam and | | | | | | | | | the applicable flap beam | | | | | | | | | attachments. | | | | | | | | | | | | | | | | C.| | Do an inspection of the ram air | X | | | | | | | | turbine for correct stowage. | | | | | | | | | | | | | | | | | | If it is not latched: | | | | | | | | | (1) Examine all the installation. | | X | | | | | | | If you find damage: | | | | | | | | | (2) Do a functional test of the ram | | X | | | | | | | air turbine and system. | | | | | | | | | | | | | | | |4. | | Inspection of the Trailing Edge | | | | | | | | | | | | | | | | A.| | Do a detailed visual inspection of | X | | | | | | | | the inner, mid and outer rear spar and| | | | | | | | | all supporting structure parts for | | | | | | | | | cracks, damage, distortion or fluid | | | | | | | | | leaks. | | | | | | | | | Make sure that: | | | | | | | | | - the paint and sealant are not | | | | | | | | | damaged | | | | | |
R EFF : ALL 05-51-11 SROS
Page 657 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - the fasteners and safety devices | | | | | | | | | are in the correct condition. | | | | | | | | | | | | | | | | | | If there are signs of damage on the | | | | | | | | | rear spar: | | | | | | | | | (1) Defuel the wing | | X | | | | | | | (Ref. TASK 28-25-00-650-80300). | | | | | | | | | (2) Get access to the internal wing | | X | | | | | | | at the area of damage. | | | | | | | | | (3) Do a general internal inspection | | X | | | | | | | of all the ribs, riblets, | | | | | | | | | stringers, brackets and plates | | | | | | | | | in the damaged area for damage | | | | | | | | | (cracks). | | | | | | | | | Make sure that: | | | | | | | | | - the paint and sealant are not | | | | | | | | | damaged | | | | | | | | | - the fasteners are in the correct| | | | | | | | | condition. | | | | | | | | | | | | | | | | B.| | If you find damage on the wing, do an | | X | | | | | | | operational test of the flaps | | | | | | | | | (Ref. TASK 27-54-00-710-80100). | | | | | | | | | Make sure the flaps and the spoilers | | | | | | | | | move smoothly and freely. | | | | | | | | | | | | | | | | C.| | Do a detailed visual inspection of all| X | | | | | | | | the supporting structure parts for | | | | | | | | | cracks, damage, distortion or fluid | | | | | | | | | leaks. | | | | | | | | | Make sure that: | | | | | | | | | - the fasteners and safety devices | | | | | | | | | are in the correct condition | | | | | | | | | - the paint and sealant are not | | | | | | | | | damaged. | | | | | | | | | | | | | | | | | | If there are signs of damage to the | | | | | | | | | trailing edge false-work. | | | | | | | | | (1) Do a general inspection of these | | X | | | | | | | items: | | | | | | | | | - fixed shroud | | | | | | | | | - fixed shroud attachments | | | | | | | | | - shroud box | | | | | |
EFF : ALL 05-51-11 SROS
Page 658 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - shroud box attachments | | | | | | | | | - support ribs | | | | | | | | | - support rib attachments | | | | | | | | | - lower panel-support struts | | | | | | | | | - riblets stringers and | | | | | | | | | brackets. | | | | | | | | | Make sure that: | | | | | | | | | - there is no damage | | | | | | | | | - the paint and sealant are not | | | | | | | | | damaged | | | | | | | | | - the fasteners are in the | | | | | | | | | correct condition. | | | | | | | | | | | | | | | | C.| | Do an inspection of all the pipes, | X | | | | | | | | the hoses, the electrical looms and | | | | | | | | | the raceways. | | | | | | -------------------------------------------------------------------------------
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Subtask 05-51-11-210-096
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K. Inspection of the Center Fuselage between FR38 and FR54 (Ref. Fig. 614/TASK 05-51-11-991-028, 615/TASK 05-51-11-991-029, 616/TASK 05-51-11-991-030, 617/TASK 05-51-11-991-031)
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NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Center Fuselage | | | | | | | | | | | | | | | | A.| | Examine the belly fairing panels for | X | | | | | | | | loose fasteners, cracked or flaking | | | | | | | | | paint and delamination. | | | | | | | | | Make sure that: | | | | | | | | | -the attachments are correct. | | | | | | | | | | | | | | | | | | If you find damage during the | | | | | | | | | inspection: | | | | | |
EFF : ALL 05-51-11 SROS
Page 659 Jan 01/07
Main Structure Figure 614/TASK 05-51-11-991-028
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EFF : ALL 05-51-11 SROS
Page 660 Jan 01/07
Center Wing Box (Section 21) Figure 615/TASK 05-51-11-991-029
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EFF : ALL 05-51-11 SROS
Page 661 Jan 01/07
Aft Pressure Bulkhead Figure 616/TASK 05-51-11-991-030
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EFF : ALL 05-51-11 SROS
Page 662 Jan 01/07
Belly Fairing Figure 617/TASK 05-51-11-991-031
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EFF : ALL 05-51-11 SROS
Page 663 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | | | | | | | | | | (1) Remove the panels and examine | | X | | | | | | | internally the belly fairing. | | | | | | | | | Make sure that the attachments | | | | | | | | | of all the components are correct | | | | | | | | | and that the rivets are not loose.| | | | | | | | | (2) Examine the fuselage skin | | X | | | | | | | externally, below the belly | | | | | | | | | fairing zone for buckling, loose | | | | | | | | | rivets, cracked or flaking paint. | | | | | | | | | | | | | | | | B.| | Examine the canted frames at the | X | | | | | | | | boundaries of the wheel wells, their | | | | | | | | | junctions, the fittings at FR47 and | | | | | | | | | the adjacent areas. | | | | | | | | | | | | | | | | C.| | Examine the main gear and the center- | X | | | | | | | | gear locking-system attachment. | | | | | | | | | Examine the center gear mounting | | | | | | | | | at FR53.2. | | | | | | | | | | | | | | | | D.| | Examine the longitudinal edging | X | | | | | | | | spars of the keel beam section. | | | | | | | | | | | | | | | | | | If you find damage: | | | | | | | | | (1) Examine the structure of the | | X | | | | | | | keel beam. | | | | | | | | | (2) Examine the structure of the | | X | | | | | | | passenger compartment floor in | | | | | | | | | the main and center gear well. | | | | | | | | | If you find damage: | | | | | | | | | (3) From FR38 to FR54 examine | | | X | | | | | | internally the junction of the | | | | | | | | | panels of the upper fuselage at | | | | | | | | | stingers 5L and 5R. | | | | | | -------------------------------------------------------------------------------
EFF : ALL 05-51-11 SROS
Page 664 Jan 01/07
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Subtask 05-51-11-210-097 L. Inspection of the Tail Section (Zone 310) (Ref. Fig. 618/TASK 05-51-11-991-032, 619/TASK 05-51-11-991-033) (Ref. TASK 31-33-00-710-803), (Ref. TASK 23-71-00-710-801), (Ref. TASK 49-12-00-200-801)
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NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Tail Section | | | | | | | | | | | | | | | | A.| | Examine externally the skin panels | X | | | | | | | | for cracked or flaking paint, loose | | | | | | | | | rivets, wrinkles or buckling. | | | | | | | | | | | | | | | | | | If you find damage on the skin panels:| | | | | | | | | | | | | | | | | | (1) Examine the skin panels and | | X | | | | | | | stringers for cracked or flaking | | | | | | | | | paint, loose rivets, wrinkles or | | | | | | | | | buckles, signs of shearing, | | | | | | | | | distorted and twisted stringers. | | | | | | | | | | | | | | | | B.| | Do a general visual inspection of: | X | | | | | | | | - the attachment areas of the | | | | | | | | | horizontal stabilizer | | | | | | | | | - the attachment area of the vertical | | | | | | | | | stabilizer. | | | | | | | | | | | | | | | | | | If you find damage on the attachment | | | | | | | | | area: | | | | | | | | | | | | | | | | | | (1) Examine the horizontal stabilizer | | X | | | | | | | attachments for damage and signs | | | | | | | | | of movement. | | | | | | | | | (2) Examine the hinges of the elevator| | X | | | | | | | and the rudder for cracks | | | | | | | | | (3) Make sure the DFDR operates | | X | | | | | | | correctly. | | | | | | | | | | | | | | |
EFF : ALL 05-51-11 SROS
Page 665 Jan 01/07
Cone/Rear Fuselage Figure 618/TASK 05-51-11-991-032
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EFF : ALL 05-51-11 SROS
Page 666 Jan 01/07
Structure Components Figure 619/TASK 05-51-11-991-033
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EFF : ALL 05-51-11 SROS
Page 667 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | C.| | Open the access door 312AR for DFDR: | X | | | | | | | | - make sure that the recording unit | | | | | | | | | is not damaged and is attached | | | | | | | | | correctly. | | | | | | | | | | | | | | | | D.| | Do a general inspection of the APU | X | | | | | | | | compartment for leakage and damage. | | | | | | | | | | | | | | | | | | If you find damage: | | | | | | | | | | | | | | | | | | (1) Make sure that the APU is | | X | | | | | | | correctly installed. | | | | | | | | | (2) Examine the mountings for damage, | | X | | | | | | | distortion and signs of movement: | | | | | | | | | (3) Examine the container brackets | | X | | | | | | | and the container of the APU fire | | | | | | | | | extinguisher for damage. | | | | | | | | | Make sure that the installation | | | | | | | | | and attachment are correct. | | | | | | | | | | | | | | | | | | If you find damage in the | | | | | | | | | unpressurized area: | | | | | | | | | - make sure that the CVR operates | | | | | | | | | correctly: | | | | | | ------------------------------------------------------------------------------|
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Subtask 05-51-11-210-098
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M. Inspection of Avionics Compartment (Ref. TASK 24-38-00-740-801).
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NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures.
EFF : ALL 05-51-11 SROS
Page 668 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Avionics | | | | | | | | | Compartment | | | | | | | | | | | | | | | | A.| | Open the access doors to the avionics | X | | | | | | | | compartment. Examine the electrical | | | | | | | | | and electronic components, the | | | | | | | | | batteries and the racks. | | | | | | | | | Make sure that they are not damaged | | | | | | | | | and are installed correctly. | | | | | | | | | | | | | | | | | | If you find damage on the avionics | | | | | | | | | compartment: | | | | | | | | | (1) If there is structural damage | | X | | | | | | | that makes repairs necessary: | | | | | | | | | refer to the NTM. | | | | | | | | | | | | | | | | B.| | Make sure that the quick access | | X | | | | | | | recorder (QAR) operates correctly | | | | | | | | | | | | | | | | C.| | Make sure that the batteries are | X | | | | | | | | attached correctly. Make sure that | | | | | | | | | there are no leaks. | | | | | | | | | | | | | | | | D.| | Make sure that the batteries operate | | X | | | | | | | correctly | | | | | | -------------------------------------------------------------------------------
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Subtask 05-51-11-210-099
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N. Inspection of the Cargo Compartments (Ref. TASK 24-38-00-740-801)
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NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures.
EFF : ALL 05-51-11 SROS
Page 669 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Cargo Compartment | | | | | | | | | | | | | | | | A.| | Do a visual inspection of the cargo | X | | | | | | | | compartments for general condition | | | | | | | | | and damage. | | | | | | | | | | | | | | | | B.| | Open the bulk cargo-compartment | X | | | | | | | | door: | | | | | | | | | - make sure that the APU battery is | | | | | | | | | attached correctly. Make sure that | | | | | | | | | there are no leaks. | | | | | | | | | | | | | | | | C.| | Examine the unpressurized area behind | X | | | | | | | | the pressure bulkhead. | | | | | | | | | Open the access door 162TW for CVR | | | | | | | | | and water system inspection. | | | | | | | | | - Make sure that the CVR is not | | | | | | | | | damaged and is attached correctly. | | | | | | | | | - Do an inspection of the water | | | | | | | | | system. | | | | | | | | | Make sure that the water tanks are | | | | | | | | | correctly attached and that there | | | | | | | | | are no leaks. | | | | | | | | | | | | | | | | | | If you find damage on the Cargo | | | | | | | | | compartment: | | | | | | | | | (1) Examine the loading and | | X | | | | | | | unloading systems of the | | | | | | | | | containers/pallets and examine | | | | | | | | | the cargo restraint system. In | | | | | | | | | the forward and aft cargo | | | | | | | | | compartments, examine the side | | | | | | | | | guides, pallet locks and rollers | | | | | | | | | (ball units, roller assemblies, | | | | | | | | | drive units, guide latches and | | | | | | | | | tracks). | | | | | | | | | Make sure that they can move | | | | | | | | | freely. | | | | | | | | | (2) Make sure that the APU battery | | X | | | | | | | operates correctly | | | | | | -------------------------------------------------------------------------------
EFF : ALL 05-51-11 SROS
Page 670 Jan 01/07
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Subtask 05-51-11-210-100 P. Inspection of the Equipment/Furnishings
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Equipment/ | | | | | | | | | Furnishings | | | | | | | | | | | | | | | | A.| | Do a check of the equipment/ | X | | | | | | | | furnishings below: | | | | | | | | | - the passenger and crew seats | | | | | | | | | - the coat stowages | | | | | | | | | - the partitions | | | | | | | | | - the side and ceiling panels in the | | | | | | | | | passenger compartment | | | | | | | | | - the flight and passenger compartment| | | | | | | | | stowages | | | | | | | | | - the buffet/galley | | | | | | | | | - the lavatories | | | | | | | | | - the emergency evacuation equipment. | | | | | | -------------------------------------------------------------------------------
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5. Close-up ________
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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 05-51-11-410-052
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A. Close Access
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(1) Remove the safety devices installed on the landing gears.
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(2) Close all the access doors opened during the inspection procedure.
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(3) Close the main landing gear doors (Ref. TASK 32-12-00-410-801).
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(4) Close the nose landing gear doors (Ref. TASK 32-22-00-410-801).
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(5) Close the thrust reverser doors (Ref. TASK 78-30-00-410-801). FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR
EFF : ALL 05-51-11 SROS
Page 671 Jan 01/07
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(6) Close the fan cowl doors (Ref. TASK 71-13-00-410-802). FOR 4030EM1 415BL, 416BR FOR 4030EM2 425BL, 426BR
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**ON A/C 701-749,
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Subtask 05-51-11-410-052-A
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A. Close Access
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(1) Remove the safety devices installed on the landing gears.
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(2) Close all the access doors opened during the inspection procedure.
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(3) Close the main landing gear doors (Ref. TASK 32-12-00-410-801).
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(4) Close the nose landing gear doors (Ref. TASK 32-22-00-410-801).
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(5) Close the thrust reverser doors (Ref. TASK 78-30-00-410-803). FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR
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(6) Close the fan cowl doors (Ref. TASK 71-13-00-410-805). FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR
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**ON A/C ALL
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Subtask 05-51-11-866-052
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B. Aircraft Maintenance Configuration
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(1) Retract the spoilers (Ref. TASK 27-60-00-866-802).
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(2) Retract the slats (Ref. TASK 27-80-00-866-802).
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(3) Retract the flaps (Ref. TASK 27-50-00-866-802)
EFF : ALL 05-51-11 SROS
Page 672 Jan 01/07
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(4) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801).
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(5) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803).
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(6) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802).
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(7) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
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Subtask 05-51-11-942-052 C. Close Access
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(1) Remove the warning notice(s).
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(2) Make sure that the work area is clean and clear of tools and other items.
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(3) Remove the access platform(s).
EFF : ALL 05-51-11 SROS
Page 673 Jan 01/07
INSPECTION AFTER LANDING GEAR DOWN LIMITING SPEED EXCEEDED - INSPECTION/CHECK _____________________________________________________________________________ TASK 05-51-12-200-801 Inspection After Landing Gear Extension at More than the Gear Down Limiting Speed. 1. __________________ Reason for the Job This inspection is applicable if: - the landing gear extends/retracts, while the aircraft speed is more than the limit speed (VLO). - the aircraft speed increases to more than the limit speed (VLE), while the landing gear is downlocked. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
safety barriers warning notice
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------07-11-00-581-801 07-11-00-586-801 24-41-00-862-801 27-50-00-866-801 27-50-00-866-802 28-10-00-910-802 29-00-00-864-801 29-00-00-864-802 29-00-00-864-803 32-00-00-481-801
Lifting of the Aircraft for Maintenance Operations Lowering of the Aircraft for Maintenance Operations De-energize the Aircraft Electrical Circuits from the External Power A Extension of the Flaps on the Ground Retraction of the Flaps on the Ground Access to Fuel Tanks and Work Areas 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) Installation of the Safety Devices on the Landing Gears
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Page 601 Apr 01/98
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
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32-11-00-220-802 32-11-13-000-801 32-11-13-860-801 32-12-00-010-801 32-12-00-410-801 32-12-14-000-801 32-12-14-200-801 32-21-00-220-803 32-21-13-000-801 32-22-00-010-801 32-22-00-410-801 32-22-11-000-801 32-31-16-000-801 53-35-11-000-801 05-51-12-991-001 05-51-12-991-002 05-51-12-991-003 05-51-12-991-004 05-51-12-991-005 05-51-12-991-007 05-51-12-991-008
Check of Shock Absorber Nitrogen Charge Pressure Removal of the MLG Shock Absorber To Close the Seal Changeover Valve Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Removal of the MLG Fixed Fairing Assembly Inspection of the MLG Fixed Fairing Assembly Check Nose Gear Shock Absorber Nitrogen Charge Pressure Removal of the NLG Shock Absorber Assembly Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance Removal of the NLG Main Door Assy Removal of the NLG Door Actuator (5203GA,5204GA) Removal of the Wing-to-Fuselage Fairings Fig. 601 Fig. 602 Fig. 603 Fig. 604 Fig. 605 Fig. 606 Fig. 607
3. __________ Job Set-up Subtask 05-51-12-941-050 A. Safety Precautions (1) Put a warning notice in the cockpit to tell persons not to operate the aircraft system. (2) Put the safety barriers in position. Subtask 05-51-12-010-050 B. Get Access (1) Open the main landing gear doors (Ref. TASK 32-12-00-010-801). (2) Open the nose landing gear doors (Ref. TASK 32-22-00-010-801).
EFF : ALL 05-51-12 SROS
Page 602 Jul 01/05
Subtask 05-51-12-091-050 C. Safety Precautions (1) Install the safety devices on the landing gears (Ref. TASK 32-00-00481-801). (2) Lift the aircraft (Ref. TASK 07-11-00-581-801). R R
NOTE : Lifting of the aircraft is only necessary for the PHASE 2 ____ inspection. Subtask 05-51-12-866-050 D. Aircraft Maintenance Configuration (1) Fully extend the flap (Ref. TASK 27-50-00-866-801). Subtask 05-51-12-864-050 E. Aircraft Maintenance Configuration (1) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (2) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803). (3) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-802). (4) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). Subtask 05-51-12-010-051 F. Get Access (1) Open all the access panels in the main landing gear compartment.
EFF : ALL 05-51-12 SROS
Page 603 Jan 01/06
4. Procedure _________ Subtask 05-51-12-210-050 A. Inspection of the Fuselage NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non-Destructive Testing Manual (NTM) and use non destructive test procedures. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Fuselage | | | | | | | | | | | | | | | | A.| | Examine the external fuselage | X | | | | | | | | and the skin panels for: | | | | | | | | | - distortion, cracks, pulled or torn | | | | | | | | | fasteners and damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Internally examine the frames, | | X | | | | | | | the stringers and the cleats for: | | | | | | | | | buckling, cracks and damaged | | | | | | | | | paintwork. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-12-210-051 B. Inspection of Nose Landing Gear Well and Doors (Ref. Fig. 601/TASK 05-51-12-991-001) (Ref. TASK 32-22-11-000-801), (Ref. TASK 32-31-16-000-801). ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Nose Landing Gear | | | | | | | | | Bay | | | | | | | | | (Ref. Fig. 601/TASK 05-51-12-991-001) | | | | | | | | | | | | | | | | A.| | Examine the hinge fittings of the nose| X | | | | | | | | landing gear, the attach fitting of | | | | | | | | | the actuating cylinder, the drag | | | | | | | | | strut, the attach fittings for: | | | | | | | | | - distortion, cracks, pulled or torn | | | | | |
EFF : ALL 05-51-12 R SROS
Page 604 Jan 01/02
Nose Landing Gear Figure 601/TASK 05-51-12-991-001 EFF : ALL 05-51-12 R SROS
Page 605 Jan 01/02
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | fasteners and damaged paintwork. | | | | | | | | | | | | | | | | B.| | Examine the NLG well roof, the | X | | | | | | | | forward and aft side wall | | | | | | | | | structure for: | | | | | | | | | - distortion, cracks, pulled or torn | | | | | | | | | fasteners and damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Get access to the avionics | | X | | | | | | | compartment and internally | | | | | | | | | examine the NLG well roof, and | | | | | | | | | the forward and aft side | | | | | | | | | wall, the struts for: | | | | | | | | | - distortion, cracks, pulled or | | | | | | | | | torn fasteners and damage | | | | | | | | | paintwork. | | | | | | | | | | | | | | | | C.| | Examine the components installed in | X | | | | | | | | the nose landing gear well, the | | | | | | | | | manifold, the electrical looms, the | | | | | | | | | rods, the pipes, the bellcranks for: | | | | | | | | | - distortion, cracks, rupture and | | | | | | | | | fluid leakage. | | | | | | | | | | | | | | | |2. | | Examine the nose landing gear doors. | | | | | | | | | | | | | | | | A.| | Examine the doors, the door hinge | X | | | | | | | | fittings and the adjacent structure | | | | | | | | | for: | | | | | | | | | - distortion, cracks, pulled or torn | | | | | | | | | fasteners, delamination and damaged | | | | | | | | | paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the doors | X | | | | | | | | (Ref. TASK 32-22-11-000-801). | | | | | | | | | | | | | | | | B.| | Examine the door actuating cylinder, | X | | | | | | | | the rods, the related linkages, the | | | | | | | | | valve for fluid leakage, cracks, | | | | | | | | | pulled or torn fasteners. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the nose landing gear door | | X | | | | | | | actuating cylinder | | | | | |
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Page 606 Jan 01/02
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (Ref. TASK 32-31-16-000-801). | | | | | | ------------------------------------------------------------------------------Subtask 05-51-12-210-052 C. Inspection of the Belly Fairing (Ref. Fig. 602/TASK 05-51-12-991-002, 603/TASK 05-51-12-991-003, 604/TASK 05-51-12-991-004) (Ref. TASK 53-35-11-000-801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the belly fairing | | | | | | | | | (Ref. Fig. 602/TASK 05-51-12-991-002) | | | | | | | | | (Ref. Fig. 603/TASK 05-51-12-991-003) | | | | | | | | | (Ref. Fig. 604/TASK 05-51-12-991-004) | | | | | | | | | | | | | | | | A.| | Examine the panels, the rods, the | X | | | | | | | | external surface, for: | | | | | | | | | - distortion, cracks, pulled or torn | | | | | | | | | fasteners, delamination, and | | | | | | | | | damaged paintwork. | | | | | | | | | Make sure that the panels and the rods| | | | | | | | | are correctly installed. | | | | | | | | | | | | | | | | B.| | Externally examine the cover of the | X | | | | | | | | keel beam for: | | | | | | | | | - distortion, cracks, delamination, | | | | | | | | | damaged paintwork, pulled or torn | | | | | | | | | fasteners. | | | | | | | | | Make sure that the attachment is | | | | | | | | | correct. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the panels and internally | | X | | | | | | | examine the structure of the belly| | | | | | | | | fairing, the skin for: | | | | | | | | | - distortion, cracks, buckling | | | | | | | | | and damaged paintwork, box | | | | | | | | | rivets | | | | | | | | | (Ref. TASK 53-35-11-000-801). | | | | | | | | | (2) Examine all the components | | X | | | |
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Page 607 Jan 01/02
Wing Center Box Figure 602/TASK 05-51-12-991-002 EFF : ALL 05-51-12 SROS
Page 608 Apr 01/98
Wing Center Box - Main Structure Figure 603/TASK 05-51-12-991-003 EFF : ALL 05-51-12 SROS
Page 609 Apr 01/98
Belly Fairing Structure Figure 604/TASK 05-51-12-991-004 EFF : ALL 05-51-12 SROS
Page 610 Apr 01/98
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | installed in the belly fairing, | | | | | | | | | the ducts, the pipes, the | | | | | | | | | electrical loom and their mount, | | | | | | | | | the safety devices, for: | | | | | | | | | - distortion, cracks, fluid | | | | | | | | | leakage, breaks, rupture, | | | | | | | | | pulled or torn fasteners, | | | | | | | | | damaged paintwork, loose rivets.| | | | | | | | | Make sure that the attachment is | | | | | | | | | correct and that the components | | | | | | | | | are in the correct condition. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-12-210-053 D. Inspection of Main Landing Gear Bay FR47 to FR53 and Doors (Ref. Fig. 605/TASK 05-51-12-991-005) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Main Landing Gear | | | | | | | | | Well FR47 to FR53 | | | | | | | | | (Ref. Fig. 605/TASK 05-51-12-991-005) | | | | | | | | | | | | | | | | A.| | Examine the diagonal frames at the | X | | | | | | | | edges of the wheel wells, their | | | | | | | | | junctions at FR47 and the adjacent | | | | | | | | | structure for: | | | | | | | | | - distortion, cracks, pulled or torn | | | | | | | | | fasteners and damaged paintwork. | | | | | | | | | | | | | | | | B.| | Examine the attachment of the main | X | | | | | | | | landing gear for: | | | | | | | | | - distortion, cracks. | | | | | | | | | If you find damage: | | | | | | | | | (1) Examine the components, the pipes,| | X | | | | | | | the ducts, the electrical looms | | | | | | | | | and their mounts, the control | | | | | | | | | cables, the pulleys, the | | | | | | | | | transmission systems, the | | | | | | | | | manifold, the safety devices for: | | | | | |
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Page 611 Jan 01/02
Main Landing Gear and Doors Figure 605/TASK 05-51-12-991-005 EFF : ALL 05-51-12 R SROS
Page 612 Jan 01/02
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - distortion, cracks, pulled or | | | | | | | | | torn fasteners, fluid leakage | | | | | | | | | and damaged paintwork. | | | | | | | | | Make sure that the attachment is | | | | | | | | | correct and that the components | | | | | | | | | are in the correct condition. | | | | | | | | | | | | | | | |2. | | Inspection of the Landing Gear Doors | | | | | | | | | | | | | | | | A.| | Examine the landing gear doors, their | X | | | | | | | | hinges and the adjacent structure for:| | | | | | | | | - cracks, delamination, pulled or torn| | | | | | | | | fasteners and damaged paintwork. | | | | | | | | | | | | | | | | B.| | Examine the door actuating cylinders, | X | | | | | | | | the selector valves and their hoses | | | | | | | | | and pipes for: | | | | | | | | | - damage. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-12-210-054 E. Inspection of Nose Landing Gear (Ref. Fig. 601/TASK 05-51-12-991-001) (Ref. TASK 32-21-00-220-803) (Ref. TASK 32-21-13-000-801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Nose Landing Gear | | | | | | | | | (Ref. Fig. 601/TASK 05-51-12-991-001) | | | | | | | | | | | | | | | | A.| | Examine the nose landing gear | X | | | | | | | | components, the pipes, the electrical | | | | | | | | | looms, the hoses for: | | | | | | | | | - damage, fluid leakage and damaged | | | | | | | | | paintwork. | | | | | | | | | | | | | | | | B.| | Examine the shock absorber for: | X | | | | | | | | - correct pressure charge, fluid | | | | | | | | | leakage, and damage | | | | | | | | | (Ref. TASK 32-21-00-220-803). | | | | | |
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Page 613 Jan 01/02
R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | If you find leaks: | | | | | | | | | (1) Remove the shock absorber for | | X | | | | | | | maintenance. | | | | | | | | | (Ref. TASK 32-21-13-000-801) | | | | | | |2. | | Inspection of the Fixed Fairing | | | | | | | | | | | | | | | | A.| | Examine the door, the linkage rollers,| X | | | | | | | | the uplock hooks for: | | | | | | | | | - damage. | | | | | | | | | Make sure that the attachment is | | | | | | | | | correct. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-12-210-055 F. Inspection of the Main Landing Gear (Ref. Fig. 605/TASK 05-51-12-991-005) (Ref. TASK 32-11-13-000-801) (Ref. TASK 32-11-00-220-802) (Ref. TASK 3211-13-860-801) (Ref. TASK 32-12-14-000-801) (Ref. TASK 32-12-14-200-801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Main Landing Gear | | | | | | | | | (Ref. Fig. 605/TASK 05-51-12-991-005) | | | | | | | | | | | | | | | | A.| | Examine the main landing gear and its | X | | | | | | | | components, hoses, pipes and | | | | | | | | | electrical harnesses for damage and | | | | | | | | | distortion. | | | | | | | | | Examine dynamic and static joints for:| | | | | | | | | - distortion. | | | | | | | | | | | | | | | | B.| | Examine the shock absorber for: | X | | | | | | | | - hydraulic fluid leaks. | | | | | | | | | If you find leaks: | | | | | | | | | - remove the shock absorber for | | X | | | | | | | maintenance. | | | | | | | | | (Ref. TASK 32-11-13-000-801) | | | | | | | | | | | | | | | | C.| | Examine the gland seals for: | X | | | | | | | | - hydraulic fluid leakage. | | | | | |
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Page 614 Jan 01/06
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | If you find leaks: | | | | | | | | | (1) Close the seal change-over valve | | X | | | | | | | (Ref. TASK 32-11-13-860-801). | | | | | | | | | If the seal change-over valve is | | | | | | | | | already closed: | | | | | | | | | (2) Remove the shock absorber for | | | X | | | | | | maintenance | | | | | | | | | (Ref. TASK 32-11-13-000-801). | | | | | | | | | | | | | | | | D.| | Do a pressure/extension check of the | X | | | | | | | | shock absorber | | | | | | | | | (Ref. TASK 32-11-00-220-802). | | | | | | | | | | | | | | | |2. | | Inspection of the fixed fairing doors | | | | | | | | | and hinged fairing | | | | | | | | | (Ref. Fig. 605/TASK 05-51-12-991-005).| | | | | | | | | | | | | | | | A.| | Examine the fixed fairing for: | X | | | | | | | | - damage | | | | | | | | | (Ref. TASK 32-12-14-200-801). | | | | | | | | | Make sure that the attachment is | | | | | | | | | correct. | | | | | | | | | If found: | | | | | | | | | (1) Remove the fixed fairing | | X | | | | | | | (Ref. TASK 32-12-14-000-801). | | | | | | -------------------------------------------------------------------------------
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Page 615 Jul 01/05
Subtask 05-51-12-210-057 G. Inspection of the Wing (RIB1 to RIB39) (Ref. Fig. 606/TASK 05-51-12-991-007, 607/TASK 05-51-12-991-008) (Ref. TASK 28-10-00-910-802)
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Wing (MLG | | | | | | | | | Attachment Points) | | | | | | | | | (Ref. Fig. 608/TASK 05-51-12-991-008) | | | | | | | A.| | Examine these parts (and their points | X | | | | | | | | of attachment): | | | | | | | | | - the forward pintle-pin fitting | | | | | | | | | - the rear pintle-pin fitting | | | | | | | | | - the gear rib 6 | | | | | | | | | - the bellcrank of the MLG actuator | | | | | | | | | - the side stay attachment fitting | | | | | | | | | - the retraction actuator attachment | | | | | | | | | fittings for: | | | | | | | | | - cracks, damage and distortion, | | | | | | | | | flaked point, cracked sealant, | | | | | | | | | fluid leaks (fuel, where | | | | | | | | | applicable). | | | | | | | | | If you find damage on the rear spar: | | | | | | | | | (1) Get access to the fuel tank | | X | | | | | | | adjacent to the applicable area. | | | | | | | | | (2) Examine the internal structure | | | | | | | | | adjacent to the external damage or| | X | | | | | | | distortion for: | | | | | | | | | - damaged paint, cracks in | | | | | | | | | structure or sealant | | | | | | | | | (especially cracks in the | | | | | | | | | sealant bead), damaged | | | | | | | | | fasteners, damaged secondary | | | | | | | | | structure (ribs, riblets, | | | | | | | | | stringers, brackets and plates),| | | | | | | | | damaged pipes, electrical cables| | | | | | | | | and raceways. | | | | | | | | | | | | | | | |2. | | Inspection of the Wing | | | | | | | | | (Ref. Fig. 607/TASK 05-51-12-991-007) | | | | | | | A.| | Examine the wing lower skin for: | X | | | | | | | | - fuel leaks, pulled or missing | | | | | | | | | fasteners, cracks and distortion. | | | | | |
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Page 616 Jul 01/05
Wing Box - Structure Figure 606/TASK 05-51-12-991-007 EFF : ALL 05-51-12 SROS
Page 617 Apr 01/98
Main Landing Gear Attachments - Structure Figure 607/TASK 05-51-12-991-008 EFF : ALL 05-51-12 SROS
Page 618 Apr 01/98
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | If you find damage: | | | | | | | | | (1) Defuel the wing and get access | | X | | | | | | | into it | | | | | | | | | (Ref. TASK 28-10-00-910-902). | | | | | | | | | (2) Examine the internal structure | | | | | | | | | adjacent to the damage for: | | | | | | | | | - missing or pulled fasteners, | | X | | | | | | | damaged ribs, damaged riblets, | | | | | | | | | damaged stringers, cracks. | | | | | | | | | Make sure that the sealant bead is| | | | | | | | | in the correct condition. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-12-210-058 H. Inspection of the Pylon
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Pylon | | | | | | | | | | | | | | | | A.| | Examine the external panels, the skin,| X | | | | | | | | the external structure for: | | | | | | | | | - distortion, cracks, pulled or torn | | | | | | | | | fasteners and damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Open the access doors and panels | | X | | | | | | | in the aircraft structure. | | | | | | | | | (2) Examine the adjacent structure | | | | | | | | | for: | | | | | | | | | - cracks, damaged paintwork, | | | | | | | | | distortion, pulled or torn | | | | | | | | | fasteners. | | | | | | | | | (3) Do a visual check of the fire | | X | | | | | | | protection system, extinguisher | | | | | | | | | bottle attachment, electrical | | | | | | | | | wires, fuel lines, air | | | | | | | | | conditioning ducts, and other | | | | | | | | | components for: | | | | | | | | | - distortion, cracks, correct | | | | | | | | | attachment, fluid leakage, | | | | | |
EFF : ALL 05-51-12 SROS
Page 619 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | and damaged paintwork. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-12-410-050 J. Close Access (1) Close all the access doors opened during the inspection. (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). Subtask 05-51-12-866-051 K. Aircraft Maintenance Configuration (1) Retract the flaps (Ref. TASK 27-50-00-866-802). 5. Close-up ________ Subtask 05-51-12-586-050 A. Lower the Aircraft (1) Lower the aircraft (Ref. TASK 07-11-00-586-801). Subtask 05-51-12-942-050 B. 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) Remove the warning notice(s). (3) Remove the access platform(s).
EFF : ALL 05-51-12 R SROS
Page 620 Jan 01/02
INSPECTION AFTER FLAP/SLAT LIMITING SPEED EXCEEDED - INSPECTION/CHECK _____________________________________________________________________ TASK 05-51-13-200-801 Inspection after Flap/Slat Extension at more than the Flap/Slat Limiting Speed 1. __________________ Reason for the Job This inspection is necessary after an activation of the overspeed audio warning: - If the overspeed was not more than 10 Kts higher than the value shown on the VFE placard, only an extension and retraction test of the flaps and slats is necessary (refer to the operational test of the flight control surfaces paragraph given in this procedure). NOTE : If you find unsatisfactory condition(s) during the operational test, ____ you must do the full inspection given in this procedure. - If the overspeed was more than 10 Kts higher than the value shown on the VFE placard, you must do the full inspection given in this procedure. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
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No No No No
specific specific specific specific
adjustable access platform safety barriers warning notice wheel chocks
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Page 601 Jul 01/05
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 24-41-00-862-801 27-50-00-866-801 27-50-00-866-802 27-54-00-200-801 27-54-00-200-802 27-54-00-710-801 27-60-00-866-801 27-60-00-866-802 27-64-00-710-801 27-80-00-866-801 27-80-00-866-802 27-84-00-210-801 27-84-00-710-801 28-10-00-910-802 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 32-00-00-481-801 32-12-00-010-801 52-30-00-010-801 52-30-00-410-801
Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Extension of the Flaps on the Ground Retraction of the Flaps on the Ground Detailed Visual Inspection of the Flap Transmission Assy Detailed Visual Inspection of the Cruise Rollers, Flap Tracks and Carriages, Rotary Actuators and Attachments Operational Test of the Flap System Extension of the Spoilers for Maintenance Retraction of the Spoilers after Maintenance Operational Test of the Spoilers Extension of the Slats on the Ground Retraction of the Slats on the Ground Detailed Visual Inspection of the Slat Transmission Assy, Slat Tracks and Rollers, Pinions and Curved Rack Gears Operational Test of the Slat System Access to Fuel Tanks and Work Areas 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) Installation of the Safety Devices on the Landing Gears Open the MLG Doors for 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
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------57-56-11-000-801 57-56-11-000-802 57-56-11-000-803 57-56-11-000-804 57-56-11-000-805
Removal of Removal of Removal of Removal of Removal of 5 (without Side)
the Movable Flap Track Fairing No. 2 the Movable Flap Track Fairing No. 3 the Movable Flap Track Fairing No. 4 the Movable Flap Track Fairing No. 5 the Fixed Flap Track Fairings Nos. 2 thru Fixed Flap Track Fairing No 4 on the Right
3. __________ Job Set-up Subtask 05-51-13-941-050 A. Safety Precautions (1) Put the safety barriers in position. R
(2) Put the wheel chocks in position at the main landing gear. (3) Put a warning notice in position in the cockpit to tell persons not to operate the systems. Subtask 05-51-13-010-050 B. Get Access (1) Open the main landing gear doors (Ref. TASK 32-12-00-010-801). (2) Open the aft cargo compartment door (Ref. TASK 52-30-00-010-801). (3) Put an adjustable access platform in position near the area you want to inspect. (4) Install the safety devices on the landing gear (Ref. TASK 32-00-00481-801). Subtask 05-51-13-860-050 C. 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).
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(3) Fully extend the spoilers (Ref. TASK 27-60-00-866-801). (4) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (5) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803). (6) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802). (7) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). 4. Procedure _________ Subtask 05-51-13-210-050 A. Inspection of the Wing NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non-destructive Testing Manual (NTM) and use the non-destructive test procedures.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the wing leading edge | | | | | | | | | | | | | | | | A. | |Examine the upper and lower skin panels| x | | | | | | | |of the leading edge for: | | | | | | | | |- distorted, cracked, pulled or damaged| | | | | | | | | fasteners, damaged paintwork and | | | | | | | | | distortion. | | | | | | | | |If you find damage: | | | | | | | | |(1)Get access to the area near the | | x | | | | | | | leading edge (the other side of the | | | | | | | | | damage). | | | | | | | | |(2)Examine the area for distortion and | | x | | | | | | | damage on ribs, riblets, stringers | | | | | | | | | and plates. | | | | | | | | | | | | | | | |2. | |Inspection of the wing trailing edge | | | | | | | | | | | | | | | | A. | |Examine the upper and lower skin panels| x | | | | | | | |of the trailing edge for: | | | | | |
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | |- distortion, cracks, pulled and | | | | | | | | | damaged fasteners, damaged paintwork,| | | | | | | | | damaged electrical harnesses. | | | | | | | | |If you find damage: | | | | | | | | |(1)Get access to the external structure| | x | | | | | | | of the trailing edge (the other | | | | | | | | | side of the damage) | | | | | | | | |(2)Examine the area for distortion, | | x | | | | | | | damage on ribs, riblets, brackets, | | | | | | | | | stringers and plates for damage. | | | | | | | | | | | | | | | |3. | |Inspection of the wing tip | | | | | | | | | | | | | | | | A. | |Examine the upper and lower skin panels| x | | | | | | | |of the wing tip, the attachment fitting| | | | | | | | |of the winglet for: | | | | | | | | |- distortion and damage, pulled and | | | | | | | | | damaged fasteners, damaged paintwork,| | | | | | | | | defective attachment. | | | | | | | | |If you find damage: | | | | | | | | |(1)Get access to the internal structure| | x | | | | | | | of the wing tip (the opposite side | | | | | | | | | to the damage). | | | | | | | | |(2)Examine the area for distortion, | | | | | | | | | damage on ribs, riblets, brackets, | | x | | | | | | | stringers and plates for damage. | | | | | | | | | | | | | | | |4. | |Inspection of the winglet assembly | | | | | | | | | | | | | | | | A. | |Examine the upper and lower skin panels| x | | | | | | | |of the winglet assembly and the winglet| | | | | | | | |attachment fittings for: | | | | | | | | |- distortion, cracked skin, pulled and | | | | | | | | | damaged fasteners, damaged paintwork,| | | | | | | | | delamination. | | | | | | | | |Also examine, the winglet attachment | | | | | | | | |fittings for: | | | | | | | | |- distortion and damage to the fittings| | | | | | | | | and the adjacent structure. | | | | | | | | |If you find damage: | | | | | | | | |(1)Get access to the internal structure| | x | | | | | | | of the winglet assembly. | | | | | | | | |(2)Examine the area for distortion, | | x | | | |
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NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non-destructive Testing Manual and use non-destructive test procedures. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the flap assemblies and | | | | | | | | |flap transmission system | | | | | | | | | | | | | | | | A. | |Examine the inboard and outboard flaps,| x | | | | | | | |the attachment fittings, the torque | | | | | | | | |limiters of the flap transmission | | | | | | | | |system for: | | | | | | | | |- cracks, distortion, pulled or torn | | | | | | | | | fasteners, honeycomb and core | | | | | | | | | delamination, damaged paintwork. | | | | | | | | |Make sure that the torque limiter | | | | | | | | |operates correctly. | | | | | | | | |If you find damage: | | | | | | | | |(1)Examine the flap transmission | | x | | | | | | | assemblies for damage | | | | | | | | | (Ref. TASK 27-54-00-200-801). | | | | | | | | | If you find damage: | | | | | |
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (a)Remove the system actuator, the | | | x | | | | | | shafts, the bearings, the | | | | | | | | | gearboxes for inspection and | | | | | | | | | servicing. | | | | | | | | |(2)Examine the flap tracks and the | | | x | | | | | | rollers for damage | | | | | | | | | (Ref. TASK 27-54-00-200-802). | | | | | | | | | | | | | | | |2. | |Inspection of the flap track | | | | | | | | |attachments | | | | | | | | | | | | | | | | A. | |Examine the attachment of the flap | | | | | | | | |tracks 1 at the wing root and their | x | | | | | | | |attachment fittings for: | | | | | | | | |- distortion, cracks, pulled or torn | | | | | | | | | fasteners and damaged paintwork. | | | | | | | | |If you find damage: | | | | | | | | |(1)Get access to the main landing gear | | x | | | | | | | well and to the aft cargo | | | | | | | | | compartment. | | | | | | | | |(2)Examine the frames, the structure, | | | | | | | | | the cleats, the stringers for | | | | | | | | | distortion, cracks, pulled or torn | | x | | | | | | | fasteners and damaged paintwork. | | | | | | | | | | | | | | | | B. | |Examine the attachments, the beam | | | | | | | | |assemblies of the flap tracks No. 2 to | x | | | | | | | |No. 5 for: | | | | | | | | |- distortion, cracks, pulled or torn | | | | | | | | | fasteners and damaged paintwork. | | | | | | | | | Do a check of the clearance. | | | | | | | | |If you find damage: | | | | | | | | |(1)Remove the flap track fairings | | x | | | | | | | No. 2 to No. 5. | | | | | | | | | (Ref. TASK 57-56-11-000-801) | | | | | | | | | (Ref. TASK 57-56-11-000-802) | | | | | | | | | (Ref. TASK 57-56-11-000-803) | | | | | | | | | (Ref. TASK 57-56-11-000-804) | | | | | | | | | (Ref. TASK 57-56-11-000-805) | | | | | | | | |(2)Examine the beam assemblies of the | | | | | | | | | flap tracks No. 2 to No. 5, their | | x | | | | | | | forward pins and their aft spigots | | | | | | | | | for: | | | | | |
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - distortion, cracks, pulled or torn| | | | | | | | | fasteners and damaged paintwork. | | | | | | | | | Do a check of the clearance. | | | | | | | | |(3)Defuel the tanks | | | | | | | | | (Ref. TASK 28-10-00-910-802) and | | | | | | | | | examine the rib near the flap track | | x | | | | | | | attachment fittings for: | | | | | | | | | - cracks, distortion, damaged, | | | | | | | | | pulled or torn fasteners and | | | | | | | | | damaged paintwork. | | | | | | | | |Also examine the sealant beads. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-13-210-052
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C. Inspection of the Slat System (Ref. TASK 27-84-00-210-801) NOTE : All the inspection are visual unless specified differently in the ____ text. Operators can refer to the Non-destructive Testing Manual (NTM) and use non-destructive test procedures.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the slat assemblies | | | | | | | | |and slat transmission | | | | | | | | | | | | | | | | A. | |Examine the slats, the hold down stop | | | | | | | | |brackets, the attachments, the anti-ice| x | | | | | | | |telescopic duct attachment, the torque | | | | | | | | |limiters of the slat system for: | | | | | | | | |- cracks, distortion, honeycomb and | | | | | | | | | core delamination, pulled or torn | | | | | | | | | fasteners, damaged paintwork. | | | | | | | | |Make sure that the torque limiters | | | | | | | | |operate correctly. | | | | | | | | |If you find damage: | | | | | | | | |(1)Examine the slat transmission | | x | | | | | | | system for damage | | | | | | | | | (Ref. TASK 27-84-00-210-801). | | | | | |
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | If you find damage: | | | | | | | | | (a)Remove the system actuator, the | | | | | | | | | shafts, the bearings, the gear | | | x | | | | | | boxes for inspection and | | | | | | | | | servicing. | | | | | | | | |(2)Examine the slat track rollers for | | x | | | | | | | damage | | | | | | | | | (Ref. TASK 27-84-00-210-801). | | | | | | | | |(3)Examine the pipes, the hoses, | | x | | | | | | | the components, the electrical | | | | | | | | | harnesses and their brackets for: | | | | | | | | | - cracks, distortion, pulled or torn| | | | | | | | | fasteners, fluid leakage and | | | | | | | | | damaged paintwork. | | | | | | | | | | | | | | | |2. | |Inspection of the slat track | | | | | | | | |attachments | | | | | | | | | | | | | | | | A. | |Examine the tracks No. 1 to No.7 and | | | | | | | | |their mountings, the rack teeth of the | | | | | | | | |tracks No. 1 to No. 7 and their | x | | | | | | | |attachments for: | | | | | | | | | - distortion, cracks, pulled or torn | | | | | | | | | fasteners and damaged paintwork. | | | | | | | | |If you find damage: | | | | | | | | |(1)Open all the access panels of the | | x | | | | | | | wing. | | | | | | | | |(2)Examine the remaining tracks and | | x | | | | | | | their mountings, the rack teeth of | | | | | | | | | the remaining tracks and their | | | | | | | | | attachments for: | | | | | | | | | - cracks, distortion, pulled or torn| | | | | | | | | fasteners and damaged paintwork. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-13-410-050 D. Close Access (1) Close the aft cargo compartment door (Ref. TASK 52-30-00-410-801). (2) Close all the access panels opened during the procedure.
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Subtask 05-51-13-860-051 E. Put the system back to its operational 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) Pressurize the Yellow hydraulic system (Ref. TASK 29-00-00-863-803). (4) Pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-802). (5) Retract the flaps (Ref. TASK 27-50-00-866-802). (6) Retract the slats (Ref. TASK 27-80-00-866-802). (7) Retract the spoilers (Ref. TASK 27-60-00-866-802). Subtask 05-51-13-710-050 R
F. Do this test. (1) Operate the flap system. Make sure that the travel is full and that the flaps move freely (Ref. TASK 27-54-00-710-801). (2) Operate the slat system. Make sure that the travel is full and that the slats move freely (Ref. TASK 27-84-00-710-801). (3) Operate the spoiler system. Make sure that the travel is full and that the spoilers move freely (Ref. TASK 27-64-00-710-801). Subtask 05-51-13-860-052 G. Put the Aircraft back to its Initial Configuration (1) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (2) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803).
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(3) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802). (4) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). 5. Close-up ________ Subtask 05-51-13-942-050 A. Put the Aircraft back to its Initial Configuration (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. (4) Make sure that the work area is clean and clear of tools and other items.
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INSPECTION OF AIRFRAME AFTER BIRD OR HAIL STRIKE - INSPECTION/CHECK ___________________________________________________________________ TASK 05-51-14-200-801 Inspection of the Aircraft after a Bird or a Hail Strike 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 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. 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
safety barriers warning notice wheel chocks adjustable access platform 16.8 m (55 ft. 1 in.)
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B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 24-41-00-862-801 27-14-00-710-801 27-24-00-710-801 27-34-00-710-801 27-44-00-710-801 27-50-00-866-801 27-50-00-866-802 27-54-00-710-801 27-60-00-866-801 27-60-00-866-802 27-64-00-710-801 27-80-00-866-802 27-84-00-710-801 28-10-00-910-801 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 32-00-00-081-801 32-00-00-481-801 32-11-00-220-801
32-12-00-010-801
Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Operational Test of the Aileron and Hydraulic Actuation Operational Test of the Rudder Servo Control with each Hydraulic System Operational Test of the Elevator and Hydraulic Actuation Operational Test of the Trimmable Horizontal Stabilizer (THS) Actuator Jamming Protection Device Extension of the Flaps on the Ground Retraction of the Flaps on the Ground Operational Test of the Flap System Extension of the Spoilers for Maintenance Retraction of the Spoilers after Maintenance Operational Test of the Spoilers Retraction of the Slats on the Ground Operational Test of the Slat System Safety Procedures When You Do Work in a Fuel Tank 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) Removal of the Safety Devices from the Landing Gears Installation of the Safety Devices on the Landing Gears Detailed Inspection of Main Gear Structure comprising: Main Fittings, Sliding Piston, Bogie Beam, Pitch Trimmer, Sidestay Assy, Lock Pins Assembly ... Open the MLG Doors for Maintenance
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-12-00-410-801 32-21-00-220-801 32-22-00-010-801 32-22-00-410-801 32-31-00-710-801 34-11-15-200-801
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Close the MLG Doors after Maintenance Detailed Inspection of the Nose Gear Structure comprising : Main Fitting (Barrel), Sliding Member, Torque Links, Drag Stay Upper and Lower Arm .... Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance Functional Test of the Normal Extension and Retraction System Inspection/Check of the Pitot Probe (9DA1, 9DA2, 9DA3) Detailed Inspection of the Radome (110AL) Inspection of the Windshields (3DG1,3DG2). Inspection of the Fixed Windows (7DG1,7DG2) Inspection of the Sliding Windows (8DG1,8DG2). Detailed Visual Inspection of Passenger Cabin Window Panes including Passenger/ Crew Door and Emergency Exit Window Panes Inspection after a Birdstrike and Foreign Object Damage Inspection Procedure After Birdstrike (Foreign Object Damage) Fig. 601
3. __________ Job Set-up Subtask 05-51-14-941-050 A. Safety Precautions (1) Put the safety barriers in position. (2) Put wheel chocks in position at the main landing gears. (3) Put a warning notice in position in the cockpit to tell persons not to operate the systems. Subtask 05-51-14-860-052 B. 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) Pressurize the Yellow hydraulic system (Ref. TASK 29-00-00-863-803). EFF : ALL 05-51-14 SROS
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(4) Pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-802). Subtask 05-51-14-010-050 C. Get Access (1) Open the NLG doors (Ref. TASK 32-22-00-010-801). (2) Open the MLG doors (Ref. TASK 32-12-00-010-801). (3) Put an adjustable access platform in position near the area you must inspect. (4) Install the safety devices on the landing gear (Ref. TASK 32-00-00481-801). Subtask 05-51-14-860-050 D. Aircraft Maintenance Configuration (1) Extend the flaps to the FULL position (Ref. TASK 27-50-00-866-801). (2) Extend the spoilers (Ref. TASK 27-60-00-866-801). (3) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (4) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802). (5) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803). (6) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). 4. Procedure _________ Subtask 05-51-14-869-050 A. General NOTE : All the necessary inspections are visual unless the text gives ____ other instructions. Operators can refer to the Non-destructive Testing Manual (NTM) and use non-destructive procedures.
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(1) Inspection recommendations on composite parts (a) if you find damage (signs of impact, damaged paintwork, abrasions, scratches or dents) on a composite part, you must do an inspection of the related damaged area for delamination and internal damage. (2) If there is damage to the aircraft structure, refer to the Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures. Subtask 05-51-14-210-050 B. Inspection of the Radome the Windows and the external structure of the fuselage (Ref. TASK 53-15-11-200-801) (Ref. TASK 56-11-11-200-801) (Ref. TASK 5611-12-200-801) (Ref. TASK 56-12-11-200-801) (Ref. TASK 56-21-15-200-801) (Ref. TASK 34-11-15-200-801) (Ref. Fig. 601/TASK 05-51-14-991-001) NOTE : All the necessary inspections are visual unless specified ____ differently in the text procedure. Operators can refer to the Non Destructive Testing Manual (NTM) and use non destructive procedure.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the Radome | | | | | | | | | | | | | | | | A.| |Examine the radome for erosion, | X | | | | | | | |delamination and core damage. | | | | | | | | |Make sure that the lightning arrestors | | | | | | | | |are in the correct condition | | | | | | | | |(Ref. TASK 53-15-11-200-801) | | | | | | | | | | | | | | | |2. | |Inspection of the Windshields, the | | | | | | | | |Fixed Windows and the Sliding Windows | | | | | | | | | | | | | | | | A.| |Examine the windshields, the fixed | X | | | | | | | |windows and the sliding windows for: | | | | | | | | |-delamination, cracking, change in | | | | | | | | | color | | | | | | | | | (Ref. TASK 56-11-11-200-801) | | | | | | | | | (Ref. TASK 56-11-12-200-801) | | | | | | | | | (Ref. TASK 56-12-11-200-801) | | | | | |
EFF : ALL 05-51-14 SROS
Page 605 Jul 01/02
Belly Fairing Structure Figure 601/TASK 05-51-14-991-001 EFF : ALL 05-51-14 R SROS
Page 606 Apr 01/02
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | |If you find damage (heavy bird strike) | | X | | | | | | |(1) Examine the windshield and sliding | | | | | | | | | window pillars and frames | | | | | | | | | internally for : | | | | | | | | | .distortion,cracks and pulled or | | | | | | | | | torn fasteners. | | | | | | | | | | | | | | | |3. | |Inspection of the Cabin Windows | | | | | | | | | | | | | | | | A.| |Examine the cabin windows for: | X | | | | | | | |-cracks, delamination and crazing. | | | | | | | | | (Ref. TASK 56-21-15-200-801). | | | | | | | | | | | | | | | |4. | |Inspection of the External Structure of| | | | | | | | |the Fuselage | | | | | | | | | | | | | | | | A.| |Examine the skin, the doors, the | X | | | | | | | |fairings, the fillets for: | | | | | | | | |-distortion, cracks, pulled or torn | | | | | | | | | fasteners and erosion and damaged | | | | | | | | | paintwork. | | | | | | | | |(1) If you find erosion | | | | | | | | | - check for delamination. | | X | | | | | | |(2) If you find other damage, get | | X | | | | | | | access to and internally examine: | | | | | | | | | - all the frames, the stringers, | | | | | | | | | the clips, the fittings and the | | | | | | | | | component mounts at and near the | | | | | | | | | location of the damage for: | | | | | | | | | . damaged paintwork, distortion | | | | | | | | | and pulled or torn fasteners | | | | | | | | | - all the components, the pipes, | | | | | | | | | the ducts, the electrical | | | | | | | | | harnesses, the cables, the | | | | | | | | | pulleys and the mechanical | | | | | | | | | linkages for: | | | | | | | | | - distortion, cracks, rupture, | | | | | | | | | breaks and fluid leakage. | | | | | | | B.| |Examine all the antennas, the | | | | | | | | |TAT sensor, the pitot probe | X | | | | | | | |the angle-of-attack sensor the | | | | | | | | |drain masts for: | | | | | | | | |- cracks and damage. | | | | | |
EFF : ALL 05-51-14 SROS
Page 607 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | C.| |Examine all the exterior lights (anti- | X | | | | | | | |collision lights, landing lights, | | | | | | | | |navigation lights, wing and engine scan| | | | | | | | |lights, logo lights) for: | | | | | | | | |-damage. | | | | | | | D.| |Examine all the exterior video systems | X | | | | | | | |(if installed) for: | | | | | | | | |- damage. | | | | | | | | | | | | | | | |5. | |Inspection of the Belly Fairing | | | | | | | | | | | | | | | | A.| |Examine externally all the belly | X | | | | | | | |fairing panels, specially the leading- | | | | | | | | |edge root fairing and the upper and | | | | | | | | |lower wing fairings, for: | | | | | | | | |- erosion, distortion, cracks, pulled | | | | | | | | | or torn fasteners and damaged | | | | | | | | | paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the damaged panels and | | X | | | | | | | internally examine the belly | | | | | | | | | fairing structure for: | | | | | | | | | .cracks, buckling and damaged | | | | | | | | | paintwork. | | | | | | | | | (2) Examine all the components, | | | | | | | | | pipes, ducts, electrical | | | | | | | | | harnesses and their mounts, for: | | | | | | | | | -distortion, cracks, breaks and | | X | | | | | | | fluid leakage. | | | | | | | | | Make sure that the components | | | | | | | | | are correctly installed and | | | | | | | | | attached | | | | | | ------------------------------------------------------------------------------Subtask 05-51-14-210-053 C. Inspection of the Landing Gear and the Landing Gear Doors (Ref. TASK 32-11-00-220-801) (Ref. TASK 32-21-00-220-801) NOTE : All the necessary inspections are visual unless specified ____ differently in the test procedure. Operators can refer to the Non Destructive Testing Manual (NTM) and use non destructive procedure.
EFF : ALL 05-51-14 SROS
Page 608 Jan 01/07
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the Nose Landing Gear and| | | | | | | | |NLG Doors | | | | | | | | | | | | | | | | A.| |If the NLG was extended when the bird | X | | | | | | | |or hail strike occurred, examine: | | | | | | | | |- the rods, the components, the lights,| | | | | | | | | the electrical harnesses that are on | | | | | | | | | the NLG, for: | | | | | | | | | . damage | | | | | | | | | (Ref. TASK 32-21-00-220-801) | | | | | | | | |- the forward and aft doors and the | | | | | | | | | fixed fairing, for: | | | | | | | | | . erosion, cracks, damaged paintwork | | | | | | | | | and pulled or torn fasteners | | | | | | | | | | | | | | | | B.| |If the NLG was retracted when the bird | X | | | | | | | |or hail strike occurred, examine the | | | | | | | | |forward and aft doors and the fixed | | | | | | | | |fairing, for: | | | | | | | | |- erosion, cracks, dents, scratches, | | | | | | | | | damaged paintwork and pulled or torn | | | | | | | | | fasteners | | | | | | | | | | | | | | | | | | | | | | | | |2. | |Inspection of the Main Landing Gear and| | | | | | | | |MLG Doors | | | | | | | | | | | | | | | | A.| |If the MLG was extended when the bird | X | | | | | | | |or hail strike occurred, examine: | | | | | | | | |- the rods, the components, the pipes, | | | | | | | | | the electrical harnesses that are on | | | | | | | | | the MLG, for: | | | | | | | | | . damage | | | | | | | | | (Ref. TASK 32-11-00-220-801) | | | | | | | | |- the hinged doors and the fixed and | | | | | | | | | hinged fairings, for: | | | | | | | | | . erosion, cracks, damaged paintwork | | | | | | | | | and pulled or torn fasteners. | | | | | | | | | | | | | | | | B.| |If the MLG was retracted when the bird | X | | | | | | | |or hail strike occurred, examine the | | | | | | | | |hinged doors and the fixed and hinged | | | | | | | | |fairings, for: | | | | | |
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Page 609 Apr 01/02
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | |- erosion, cracks, dents, scratches, | | | | | | | | | damaged paintwork and pulled or torn | | | | | | | | | fasteners. | | | | | | ------------------------------------------------------------------------------R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-14-210-058 D. Inspection of the Nacelles and the Engines (Ref. TASK 72-00-00-200-811) NOTE : All the necessary inspections are visual unless specified ____ differently in the test procedure. Operators can refer to the Non Destructive Testing Manual (NTM) and use the non destructive procedure. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the Engines and the | | | | | | | | |Nacelles | | | | | | | | | | | | | | | | A.| |Examine the engine and the nacelle | X | | | | | | | |(Ref. TASK 72-00-00-200-811) | | | | | | ------------------------------------------------------------------------------**ON A/C 701-749, Subtask 05-51-14-210-058-A D. Inspection of the Nacelles and the Engines (Ref. TASK 71-00-00-200-803) NOTE : All the necessary inspections are visual unless specified ____ differently in the test procedure. Operators can refer to the Non Destructive Testing Manual (NTM) and use the non destructive procedure.
EFF : ALL 05-51-14 SROS
Page 610 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the Engines and the | | | | | | | | |Nacelles | | | | | | | | | | | | | | | | A.| |Examine the engine and the nacelle | X | | | | | | | |(Ref. TASK 71-00-00-200-803) | | | | | | ------------------------------------------------------------------------------**ON A/C ALL Subtask 05-51-14-210-055 E. Inspection of the Pylons NOTE : All the necessary inspections are visual unless specified ____ differently in the text procedure. Operators can refer to the Non Destructive Testing Manual (NTM) and use non destructive procedure.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the Pylons | | | | | | | | | | | | | | | | A.| |Examine the pylons externally for | X | | | | | | | |erosion, distortion, cracks, pulled | | | | | | | | |or torn fasteners and damaged | | | | | | | | |paintwork. | | | | | | | | |If you find damage: | | | | | | | | |(1) If you find only erosion: | | | | | | | | | - no other inspection operations | | | | | | | | | are necessary. | | | | | | | | |(2) If you find other damage: | | X | | | | | | | - examine the pylon internally for:| | | | | | | | | .distortion, cracks, pulled or | | | | | | | | | torn fasteners and damaged | | | | | | | | | paintwork | | | | | | | | | - examine the components, the | | | | | | | | | pipes, the ducts, the electrical | | | | | | | | | harnesses and their mounts for: | | | | | | | | | distortion, cracks, rupture, | | | | | | | | | breaks and fluid leakage. | | | | | |
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Page 611 Jan 01/07
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| ------------------------------------------------------------------------------Subtask 05-51-14-210-056 F. Inspection of the Stabilizer NOTE : All the necessary inspections are visual unless specified ____ differently on the text procedure. Operators can refer to the Non Destructive Testing Manual (NTM) and use non destructive procedure.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the Vertical Stabilizer | | | | | | | | | | | | | | | | A.| |Examine the dorsal fin, the leading | | | | | | | | |edge and the tip fairing | X | | | | | | | |externally for: | | | | | | | | |- erosion, delamination, cracks, pulled| | | | | | | | | or torn fasteners, honeycomb | | | | | | | | | delamination, core damage and damaged| | | | | | | | | paintwork. | | | | | | | | | If you find damaged: | | | | | | | | | (1) If you find erosion | | | | | | | | | - check for delamination | | X | | | | | | | (2) If you find other damage: | | | | | | | | | - examine internally the area at | | X | | | | | | | and near the damage for: | | | | | | | | | . distortion, cracks, pulled or| | | | | | | | | torn fasteners, honeycomb | | | | | | | | | delamination, core damage | | | | | | | | | and damaged paintwork. | | | | | | | | | | | | | | | | B.| |Examine the spar box of the vertical | X | | | | | | | |stabilizer for erosion, scores and | | | | | | | | |damaged paintwork. | | | | | | | | | | | | | | | | C.| |Examine the rudder and the trailing| | | | | | | | |edge access doors externally for: | | | | | | | | |- erosion, distortion, cracks, pulled | X | | | | | | | | or torn fasteners, honeycomb | | | | | |
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Page 612 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | delamination, core damage and damaged| | | | | | | | | paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) If you find only erosion | | | | | | | | | - no other inspection operations | | | | | | | | | are necessary. | | | | | | | | | (2) If you find other damage | | | | | | | | | - examine the rudder hinge and | | X | | | | | | | the actuator attach fittings | | | | | | | | | for: | | | | | | | | | .damaged paintwork,cracks and | | | | | | | | | distortion. | | | | | | | | | | | | | | | |2. | |Inspection of the Horizontal Stabilizer| | | | | | | | | | | | | | | | A.| |Examine the leading edge and the tip | X | | | | | | | |fairing externally for: | | | | | | | | |- erosion, distortion, cracks, pulled | | | | | | | | | or torn fasteners, core damage and | | | | | | | | | damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) If you find only erosion | | | | | | | | | - no other inspection operations | | | | | | | | | are necessary. | | | | | | | | | (2) If you find other damage | | | | | | | | | - examine the leading edge and | | | | | | | | | tip fairing internally for: | | | | | | | | | .cracks, distortion, pulled or | | X | | | | | | | torn fasteners and damage | | | | | | | | | paintwork. | | | | | | | | | | | | | | | | B.| |Examine the spar box of the horizontal | | | | | | | | |stabilizer for erosion, scores and | X | | | | | | | |damaged paintwork. | | | | | | | | | | | | | | | | C.| |Examine the elevators and the trailing | | | | | | | | |access doors externally for erosion, | X | | | | | | | |cracks, pulled or torn fasteners, | | | | | | | | |honeycomb delamination, core damage and| | | | | | | | |damaged paintwork. | | | | | | | | |If you find damage | | | | | | | | |(1) If you find only erosion | | | | | | | | | - no other inspection operations | | | | | |
EFF : ALL 05-51-14 SROS
Page 613 Jan 01/07
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | are necessary. | | | | | | | | |(2) If you find other damage | | | | | | | | | - examine the elevator hinge and | | X | | | | | | | the actuator attach fittings for:| | | | | | | | | .distortion, cracks and damaged | | | | | | | | | paintwork. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-14-210-057 G. Inspection of the Wing (Ref. TASK 28-10-00-910-801). NOTE : All the necessary inspections are visual unless specified in the ____ text procedure. Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive testing procedure.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the Wing | | | | | | | | | | | | | | | | A.| |Examine the upper and lower surface of | | | | | | | | |wing for: | X | | | | | | | |-erosion distortion and damage | | | | | | | | | If you find damage | | | | | | | | | (1) Get access to the internal | | X | | | | | | | structure (the other side of the | | | | | | | | | damage) | | | | | | | | | (Ref. TASK 28-10-00-910-801) | | | | | | | | | (2) Examine the fuel tank sealant | | | | | | | | | the ribs, the riblets, the | | | | | | | | | stringers, the brackets, the | | | | | | | | | plates, the components, the | | | | | | | | | harnesses for: | | | | | | | | | - damage | | | | | | | | | | | | | | | | B.| |Examine externally the leading edge, | | | | | | | | |the fillets and the slats for erosion, | X | | | | | | | |distortion, cracks, pulled or torn | | | | | | | | |fasteners and damaged paintwork. | | | | | |
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | |If you find damage: | | | | | | | | |(1) If you find only erosion | | | | | | | | | - no other inspection operations | | | | | | | | | are necessary. | | | | | | | | |(2) If you find other damage | | | | | | | | | - examine internally the leading | | | | | | | | | edge section at and near the | | X | | | | | | | damage for distortion, cracks, | | | | | | | | | pulled or torn fasteners and | | | | | | | | | damaged paintwork. | | | | | | | | |(3) Examine the ducts and the related | | | | | | | | | attach points for damage. | | | | | | | | | - examine the slat section for | | | | | | | | | distortion, cracks, pulled or | | | | | | | | | torn fasteners and damaged | | | | | | | | | paintwork | | | | | | | | | - examine the actuators, the slat | | X | | | | | | | tracks and the slat-track attach | | | | | | | | | points for damage | | | | | | | | | - examine the rollers of the slat | | X | | | | | | | tracks for brinelling. | | | | | | | | | | | | | | | | C.| |Examine externally the trailing edge | | | | | | | | |falsework, the flaps, the ailerons | | | | | | | | |and spoilers for erosion, distortion, | X | | | | | | | |cracks, pulled or torn fasteners and | | | | | | | | |damaged paintwork. | | | | | | | | |If you find damage: | | | | | | | | |(1) If you find only erosion: | | | | | | | | | - no other inspection operations | | | | | | | | | are necessary. | | | | | | | | |(2) If you find other damage: | | | | | | | | | - get access to the internal | | X | | | | | | | structure (the other side of the | | | | | | | | | damage). | | | | | | | | | - examine the falsework internally | | X | | | | | | | at and near the damage for | | | | | | | | | damaged paintwork, distortion, | | | | | | | | | cracks, pulled or torn fasteners | | | | | | | | | - examine the flap carriages and | | X | | | | | | | the fairings for distortion, | | | | | | | | | cracks and damaged paintwork | | | | | | | | | - examine the flap tracks for | | X | | | | | | | brinelling | | | | | | | | | - examine the aileron servo| | | | | | | | | controls and the hinge fittings | | | | | | | | | for damage | | | | | | | | | - examine the spoiler servo| | X | | | |
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Page 615 Jan 01/07
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | controls and the hinge fittings | | | | | | | | | for damage. | | | | | | | | | | | | | | | | D.| |Examine the wing tips for erosion, | X | | | | | | | |distortion, cracks, pulled or torn | | | | | | | | |fasteners and damaged paintwork. | | | | | | | | | | | | | | | | E.| |Examine the exterior lights (strobe | X | | | | | | | |lights at the wing tips, navigation | | | | | | | | |lights). | | | | | | | | | | | | | | | | F.| |Examine the main structure of the wing | X | | | | | | | |for erosion and scores. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-14-410-050 H. Close Access (1) Remove the safety devices from on the landing gears (Ref. TASK 32-0000-081-801) . (2) Close all the access panels that you opened during the procedure. (3) Close the NLG doors (Ref. TASK 32-22-00-410-801). (4) Close the MLG doors (Ref. TASK 32-12-00-410-801). (5) Remove the access platform(s). Subtask 05-51-14-860-051 J. Put the system back to its operational configuration. (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Retract the flaps (Ref. TASK 27-50-00-866-802). (3) Retract the slats (Ref. TASK 27-80-00-866-802). (4) Retract the spoilers (Ref. TASK 27-60-00-866-802).
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Subtask 05-51-14-710-050 K. Do the tests below NOTE : The tests below are necessary only if: ____ - you did work on the system subsequent to the inspection for damage - you found damage on the structure adjacent to the landing gear doors or a flight control surface. (1) Operate the ailerons 3 times. Make sure that the travel is full and that the ailerons move freely (Ref. TASK 27-14-00-710-801). (2) |Operate the rudder 3 times. Make sure that the travel is full and that the rudder moves freely (Ref. TASK 27-24-00-710-801). (3) Operate the elevator 3 times. Make sure that the travel is full and that the elevator moves freely (Ref. TASK 27-34-00-710-801). (4) Operate the THS 3 times. Make sure that the travel is full that the THS moves freely (Ref. TASK 27-44-00-710-801). (5) Operate the flaps 3 times. Make sure that the travel is full and that the flaps move freely (Ref. TASK 27-54-00-710-801). (6) Operate the spoilers 3 times. Make sure that the travel is full and that the spoilers move freely (Ref. TASK 27-64-00-710-801). (7) Operate the slats 3 times. Make sure that the travel is full and that the slats move freely (Ref. TASK 27-84-00-710-801). (8) Retract and extend the landing gear 3 times. Make sure that the landing gear and the doors move freely (Ref. TASK 32-31-00-710-801). (9) If you find damage only on the landing gear doors or on the structure adjacent to the landing gear doors: (a) Open the NLG doors (Ref. TASK 32-22-00-010-801). (b) Make sure that the NLG doors move freely. (c) Close the NLG doors (Ref. TASK 32-22-00-410-801). (d) Open the MLG doors (Ref. TASK 32-12-00-010-801). (e) Make sure that the MLG doors move freely.
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(f) Close the MLG doors (Ref. TASK 32-12-00-410-801). 5. Close-up ________ R R
Subtask 05-51-14-860-054 A. Put the Aircraft back to its Initial Configuration
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(1) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801).
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(2) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802).
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(3) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803).
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(4) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). Subtask 05-51-14-942-050
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B. Put the Aircraft back to its Initial Configuration (1) Remove the warning notice(s). (2) Remove the ground support and maintenance equipment, the special and standard tools and all other items. (3) Make sure that the work area is clean and clear of tools and other items.
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Page 618 Apr 01/02
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_____________________________________________________________ INSPECTION AFTER A TIRE BURST OR TREAD THROW OR WHEEL FAILURE ________________ INSPECTION/CHECK TASK 05-51-15-200-801
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Inspection of the Aircraft after a Tire Burst or Tread Throw or Wheel Failure 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
safety barriers warning notice wheel chocks adjustable access platform 16.8 m (55 ft. 1 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------05-51-16-200-801 24-41-00-861-801 24-41-00-862-801 27-14-00-710-801 27-50-00-866-801 27-50-00-866-802 27-54-00-710-801 27-60-00-866-801 27-60-00-866-802 27-80-00-866-801 27-80-00-866-802 27-84-00-710-801 29-00-00-863-801
Inspection After Brake Overheat Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Operational Test of the Aileron and Hydraulic Actuation Extension of the Flaps on the Ground Retraction of the Flaps on the Ground Operational Test of the Flap System Extension of the Spoilers for Maintenance Retraction of the Spoilers after Maintenance Extension of the Slats on the Ground Retraction of the Slats on the Ground Operational Test of the Slat System Pressurize the Green Hydraulic System with the Ground Hydraulic Supply
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Page 601 Jul 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------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 32-00-00-081-801 32-00-00-481-801
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32-12-00-010-801 32-12-00-410-801 32-22-00-010-801 32-22-00-410-801 32-31-00-710-801 34-51-00-740-801 34-52-00-710-801 53-12-13-000-801 72-00-00-200-811 78-31-00-710-804 78-31-00-740-802 05-51-15-991-001
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) Removal of the Safety Devices from the Landing Gears Installation of the Safety Devices on the Landing Gears Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance Functional Test of the Normal Extension and Retraction System BITE Test of the DME Operational test of the lights of the ATC control unit Removal of the Avionics-Compartment Floor Panels Inspection Procedure After Birdstrike (Foreign Object Damage) Thrust Reverser Cycling Test (MCDU) Test of the Thrust Reverser Deployment and Stowage (Engine not Running) Fig. 601
3. __________ Job Set-up Subtask 05-51-15-941-050 A. Safety Precautions (1) Put the safety barriers in position. R
(2) Put wheel chocks in position at the main landing gear. (3) Put a warning notice in position in the cockpit to tell persons not to operate the systems.
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Page 602 Jul 01/05
Subtask 05-51-15-860-052 B. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Pressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (3) Pressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803). (4) Pressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802). Subtask 05-51-15-010-050 C. Get Access (1) Open the NLG doors (Ref. TASK 32-22-00-010-801). (2) Open the MLG doors (Ref. TASK 32-12-00-010-801). (3) Put an adjustable access platform in position near the area that you must inspect. (4) Install the safety devices on the landing gear (Ref. TASK 32-00-00481-801). Subtask 05-51-15-860-050 D. Aircraft Maintenance Configuration (1) Extend the flaps to full position (Ref. TASK 27-50-00-866-801). (2) Extend the slats to full position (Ref. TASK 27-80-00-866-801). (3) Extend the spoilers to full position (Ref. TASK 27-60-00-866-801). (4) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (5) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803).
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Page 603 Apr 01/98
(6) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802). (7) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). 4. Procedure _________ (Ref. Fig. 601/TASK 05-51-15-991-001) Subtask 05-51-15-869-050 A. General NOTE : All the necessary inspections are visual unless the text gives ____ other instructions. Operators can refer to the Non-destructive Testing Manual (NTM) and use non-destructive procedures. (1) Inspection recommendations on composite parts R R
(a) If you find damage (signs of impact, damaged paintwork, abrasions, scratches or dents) on a composite part, you must do an inspection of the related damaged area for delamination and internal damage. (2) If there is damage to the aircraft structure, refer to the Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures. (3) If a tire burst occurs when the landing gear is fully retracted, then only examine the items of equipment below: - the landing gear well, - the landing gear doors, - the landing gear assemblies, - the hydraulic bay compartment. (4) If you replace a component because of an inspection, you must do an operational test of the related system.
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Page 604 Jul 01/05
Structure of the Belly Fairing Figure 601/TASK 05-51-15-991-001 EFF : ALL 05-51-15 R SROS
Page 605 Apr 01/02
Subtask 05-51-15-210-051 B. Inspection of the Brakes (1) If a tire burst occurs because of an emergency operation or locking of the brackes, examine the brakes (Ref. TASK 05-51-16-200-801). (2) During the inspection, if you find tire debris, remove them. Subtask 05-51-15-210-050 C. Inspection of the Fuselage Lower Section (Ref. Fig. 601/TASK 05-51-15-991-001) (Ref. TASK 34-51-00-740-801) (Ref. TASK 34-52-00-710-801) (Ref. TASK 5312-13-000-801) NOTE : All the necessary inspections are visual unless specified ____ differently in the procedure text. Operators can refer to the Non-Destructive Testing Manual (NTM) and use non destructive procedures. If a tire burst occurs when the landing gear is fully retracted, examine only: - the landing gear well - the landing gear doors - the landing gear - the hydraulics compartment. If you replace a component after an inspection, you must do an operational test of the related system.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Fuselage Lower | | | | | | | | | Section. This includes the | | | | | | | | | cargo doors | | | | | | | | | | | | | | | | A.| | Examine the skin panels for | X | | | | | | | | distortion, pulled or torn fasteners, | | | | | | | | | scratches, dents, damaged paintwork. | | | | | | | | | If you find damage : | | | | | | | | | (1) Remove the floor panels of the | | X | | | | | | | FWD cargo compartment | | | | | | | | | Remove the floor panels of the | | | | | | | | | avionics compartment. | | | | | | | | | (Ref. TASK 53-12-13-000-801) | | | | | | | | | - examine the frames, the | | | | | |
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Page 606 Jan 01/06
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | stringers, the clips, the | | | | | | | | | fittings for: | | | | | | | | | . distortion, cracks, pulled or | | | | | | | | | torn fasteners and damaged | | | | | | | | | paintwork adjacent to the | | | | | | | | | damaged area. | | | | | | | | | | | | | | | | | | (2) Examine the components, the | | X | | | | | | | pipes, the ducts, the electrical | | | | | | | | | harnesses, the control cables, the| | | | | | | | | pulleys, the mounts, the safety | | | | | | | | | devices, for : | | | | | | | | | - rupture, cracks, impacts, and | | | | | | | | | fluid leakage. | | | | | | | | | | | | | | | | B.| | Examine externally : | | | | | | | | | - the ATC, DME and TCAS antennas which| | | | | | | | | are on the lower fuselage | | | | | | | | | - the drain mast | X | | | | | | | | - the TAT sensor | | | | | | | | | - the pitot probes | | | | | | | | | - the angle-of-attack sensor | | | | | | | | | for cracks, dents, scratches. | | | | | | | | | If you find damage : | | | | | | | | | (1) Do an operational test of the DME | | X | | | | | | | (Ref. TASK 34-51-00-740-801). | | | | | | | | | | | | | | | | | | (2) Do an operational test of the | | X | | | | | | | ATC/MODE | | | | | | | | | (Ref. TASK 34-52-00-710-801). | | | | | | | | | | | | | | | |2. | | Inspection of the NLG well. | | | | | | | | | | | | | | | | A.| | Examine the structure, the components,| | | | | | | | | the pipes, the ducts, the electrical | X | | | | | | | | harnesses, the manifolds, the mounts | | | | | | | | | for: | | | | | | | | | - cracks, rupture, pulled or torn | | | | | | | | | fasteners, impacts, fluid leakage, | | | | | | | | | condition of the safety devices, and| | | | | | | | | damaged paintwork. | | | | | | | | | | | | | | | |3. | | Inspection of the Belly Fairing | | | | | | | | | (Ref. Fig 601/TASK 05-51-15-991-001) | | | | | | | | | | | | | | | | A.| | Examine externally all the access | | | | | | | | | panels and doors of the belly fairing | X | | | | | | | | and the lower wing fairing for : | | | | | | EFF : ALL 05-51-15 R SROS
Page 607 Jan 01/06
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - cracks, impacts, loose, pulled or | | | | | | | | | torn fasteners and damaged | | | | | | | | | paintwork. | | | | | | | | | Make sure that the panels are | | | | | | | | | correctly attached. | | | | | | | | | If you find damage : | | | | | | | | | (1) Remove the access panels or open | | | | | | | | | the access doors and internally | | | | | | | | | examine the belly fairing | | X | | | | | | | structure, the hydraulics | | | | | | | | | compartment, all the components | | | | | | | | | for : | | | | | | | | | - cracks, buckling, damaged | | | | | | | | | paintwork. | | | | | | | | | | | | | | | | | | (2) Examine all the components, the | | | | | | | | | pipes, the ducts, the electrical | | X | | | | | | | harnesses and the mounts for : | | | | | | | | | - distortion, cracks, breaks, | | | | | | | | | fluid leakage. | | | | | | | | | Also examine the safety devices | | | | | | | | | and make sure that the components | | | | | | | | | are correctly installed. | | | | | | | | | | | | | | | |4. | | Inspection of the MLG Well | | | | | | | | | | | | | | | | A.| | Examine the protective panels, the | X | | | | | | | | structure of the main landing gear | | | | | | | | | well for : | | | | | | | | | - distortion, damage, pulled or torn | | | | | | | | | fasteners, delamination, honeycomb | | | | | | | | | damage and damaged components. | | | | | | | | | | | | | | | | B.| | Examine the fuel and hydraulic | | | | | | | | | components, the mounts for : | X | | | | | | | | - distortion, leakage, burns marks or | | | | | | | | | damage. | | | | | | | | | Make sure that they are correctly | | | | | | | | | attached. | | | | | |
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Page 608 Jan 01/06
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| ------------------------------------------------------------------------------Subtask 05-51-15-210-053 D. Inspection of the Landing Gear and the Landing Gear Doors NOTE : All the necessary inspections are visual unless specified ____ differently in the text procedure. Operators can refer to the Non-Destructive Testing Manual (NTM) and use non destructive procedures. If a tire burst occurs when the landing gear is fully retracted, examine only: - the landing gear well - the landing gear doors - the landing gear - the hydraulics compartment. If you replace a component after an inspection, you must do an operational test of the related system. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Main Landing Gear | | | | | | | | | | | | | | | | A.| | Examine the applicable main landing | | | | | | | | | gear in the area of the incident for: | X | | | | | | | | - fluid and hydraulic leakage damage | | | | | | | | | to hydraulic hoses | | | | | | | | | - damage to hydraulic pipes and | | | | | | | | | harnesses. | | | | | | | | | | | | | | | | B.| | Examine the bogie beam assembly and | | | | | | | | | its components for: | | | | | | | | | - damaged paintwork, distorsion, | | | | | | | | | damage. | | | | | | | | | Make sure that the components are in | | | | | | | | | good condition and correctly attached.| | | | | | | | | | | | | | | | C.| | Examine the sliding tube, the main | | | | | | | | | fitting the components for: | | | | | | | | | - damaged chromium plating, damaged | | | | | | | | | paintwork, hydraulic and fluid | | | | | |
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Page 609 Jan 01/02
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | leakage, distorsion, damage of the | | | | | | | | | hose and hydraulic pipes. | | | | | | | | | Make sure that the MLG leg components | | | | | | | | | are correctly attached. | | | | | | | | | | | | | | | |2. | | Inspection of the Main Landing Gear | | | | | | | | | Door | | | | | | | | | | | | | | | | A.| | Examine the honeycomb structure of the| | | | | | | | | MLG door for: | | | | | | | | | - delamination, core damage and | X | | | | | | | | cracks. | | | | | | | | | | | | | | | | B.| | Examine the door hinge actuator | | | | | | | | | attachment, the proximity sensor | | | | | | | | | attachment and the uplock roller | | | | | | | | | attachment for: | X | | | | | | | | - separation distorsion and damage. | | | | | | | | | | | | | | | | C.| | Examine the door actuator and its | | | | | | | | | hydraulic hoses and pipes for: | X | | | | | | | | - fluid leakage, distorsion and | | | | | | | | | damage. | | | | | | | | | | | | | | | |3. | | Inspection of the Nose Landing Gear | | | | | | | | | | | | | | | | A.| | Examine the nose landing gear in the | | | | | | | | | area of the incident. | X | | | | | | | | Examine the harnesses for: | | | | | | | | | - distorsion and damage. | | | | | | | | | | | | | | | | B.| | Examine the hydraulic hoses, the | | | | | | | | | hydraulic pipes, the components of the| X | | | | | | | | nose wheel steering system for: | | | | | | | | | - hydraulic leakage, distorsion and | | | | | | | | | damage. | | | | | | | | | | | | | | | | C.| | Examine the nose landing gear shock | | | | | | | | | absorber, the strut for: | X | | | | | | | | - chromium plating damage, loose | | | | | | | | | fittings and fluid leakage. | | | | | | | | | | | | | | | |4. | | Inspection of the NLG Doors | | | | | |
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Page 610 Jan 01/02
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | | | | | | | | A.| | Examine the honeycomb structure of the| | | | | | | | | aft and forward doors | | | | | | | | | - for delamination, pulled or torn | X | | | | | | | | fasteners, dents, scratches and | | | | | | | | | damaged paintwork. | | | | | | | | | | | | | | | | B.| | Examine the door actuator, the hinges,| | | | | | | | | the attachments and the actuating | | | | | | | | | cylinder for: | X | | | | | | | | - fluid leakage, distorsion, damage | | | | | | | | | and damaged paintwork. | | | | | | ------------------------------------------------------------------------------R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-15-210-057 E. Inspection of the Nacelles and the Engines (Ref. TASK 72-00-00-200-811) NOTE : All the necessary inspections are visual unless specified ____ differently in the text procedure. Operators can refer to the Non-Destructive Testing Manual (NTM) and use non destructive procedures. If a tire burst occurs when the landing gear is fully retracted, examine only: - the landing gear well - the landing gear doors - the landing gear - the hydraulics compartment. If you replace a component after an inspection, you must do an operational test of the related system.
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Page 611 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Engines and the | | | | | | | | | Nacelles | | | | | | | | | | | | | | | | A.| | Examine the engines and the nacelles | X | | | | | | | |(Ref. TASK 72-00-00-200-811) | | | | | | ------------------------------------------------------------------------------**ON A/C 701-749, Subtask 05-51-15-210-057-A E. Inspection of the Nacelles and the Engines NOTE : All the necessary inspections are visual unless specified ____ differently in the text procedure. Operators can refer to the Non-Destructive Testing Manual (NTM) and use non destructive procedures. If a tire burst occurs when the landing gear is fully retracted, examine only: - the landing gear well - the landing gear doors - the landing gear - the hydraulics compartment. If you replace a component after an inspection, you must do an operational test of the related system. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Engines and the | | | | | | | | | Nacelles | | | | | | | | | | | | | | | | A.| | Examine the engines and the nacelles | X | | | | | -------------------------------------------------------------------------------
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Page 612 Jul 01/05
**ON A/C ALL Subtask 05-51-15-210-055 F. Inspection of the Pylons NOTE : All the necessary inspections are visual unless specified ____ differently in the procedure text. Operators can refer to the Non-Destructive Testing Manual (NTM) and use non destructive procedures. If a tire burst occurs when the landing gear is fully retracted, examine only: - the landing gear well - the landing gear doors - the landing gear - the hydraulics compartment. If you replace a component after an inspection, you must do an operational test of the related system.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Pylons | | | | | | | | | | | | | | | | A.| | Examine the pylons externally for | | | | | | | | | distortions, cracks, scratches, dents | | | | | | | | | pulled or torn fasteners and damaged | X | | | | | | | | paintwork. | | | | | | | | | If you find damage : | | | | | | | | | (1) Examine the internal structure of | | | | | | | | | the pylon for distortion, cracks, | | X | | | | | | | pulled or torn fasteners, damaged | | | | | | | | | structure and damaged paintwork. | | | | | | | | | (2) Examine the components, the pipes,| | X | | | | | | | the ducts, the electrical | | | | | | | | | harnesses, the mounts for | | | | | | | | | distortion, rupture, breaks, and | | | | | | | | | fluid leakage. | | | | | | -------------------------------------------------------------------------------
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Page 613 Jul 01/05
Subtask 05-51-15-210-056 G. Inspection of the Wings NOTE : All the necessary inspections are visual unless specified ____ differently in the procedure text. Operators can refer to the Non-Destructive Testing Manual (NTM) and use non destructive procedures. If a tire burst occurs when the landing gear is fully retracted, examine only: - the landing gear well - the landing gear doors - the landing gear - the hydraulics compartment. If you replace a component after an inspection, you must do an operational test of the related system.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Trailing Edge | | | | | | | | | Falsework | | | | | | | | | | | | | | | | A.| | Examine the shroud box, the composite | | | | | | | | | closure panel for: | X | | | | | | | | - skin damage, and distortion. | | | | | | | | | | | | | | | | B.| | Examine the flap seal, the trailing | | | | | | | | | edge composite structure for: | X | | | | | | | | - damage and distortion. | | | | | | | | | | | | | | | | C.| | Examine the trailing edge falsework, | | | | | | | | | the structure of the rear spar for: | X | | | | | | | | - damaged paintwork, dents, tears, | | | | | | | | | damage and distortion. | | | | | | | | | If you find damage: | | | | | | | | | (1) Get access to the internal | | | | | | | | | structure | | X | | | | | | | (2) Examine the internal structure | | | | | | | | | the pipes, the electrical wiring | | | | | | | | | and the conduits for | | X | | | | | | | . cracks pulled or torn fasteners | | | | | | | | | and distortion. | | | | | | | | | | | | | | | |2. | | Inspection of the Leading Edge | | | | | | | | | | | | | | |
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Page 614 Jul 01/05
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | Examine the leading edge from the | | | | | | | | | RIB 1 to the RIB 10A for: | X | | | | | | | | - damage, distortion, dents, skin | | | | | | | | | tears and damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Get access to the inside area. | | X | | | | | | | (2) Examine the area of the damage, | | | | | | | | | the riblets for: | | X | | | | | | | . distortion, pulled or torn | | | | | | | | | fasteners damage, electrical | | | | | | | | | conduits. | | | | | | | | | | | | | | | |3. | | Inspection of the Slat | | | | | | | | | | | | | | | | A.| | Examine the internal structure of the | | | | | | | | | slats for: | | | | | | | | | - distortion, cracks, pulled or torn | | | | | | | | | fasteners, scratches, dents and | | | | | | | | | damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Examine the slat section at and | | | | | | | | | near the damage for: | | | | | | | | | - distortion, cracks, pulled or | | X | | | | | | | torn fasteners and damaged | | | | | | | | | paintwork. | | | | | | | | | (2) Examine the slat tracks and the | | X | | | | | | | slat track attachments for damage.| | | | | | | | | (3) Examine the rollers of the slat | | X | | | | | | | tracks for damage. | | | | | | | | | | | | | | | |4. | | Inspection of the Flaps and the | | | | | | | | | Ailerons | | | | | | | | | | | | | | | | A.| | Examine externally the flaps, and the | | | | | | | | | ailerons for : | | | | | | | | | - distortion, cracks, pulled or torn | X | | | | | | | | fasteners, scratches, dents and | | | | | | | | | damaged paintwork. | | | | | | | | | If you find damage : | | | | | | | | | (1) Examine the flap carriages and the| | X | | | | | | | fairings for : | | | | | | | | | - distortion, cracks and damaged | | | | | | | | | paintwork. | | | | | |
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Page 615 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (2) Examine the flap tracks for | | X | | | | | | | damage. | | | | | | | | | (3) Examine the aileron servo controls| | X | | | | | | | and the hinge fittings for damage.| | | | | | ------------------------------------------------------------------------------Subtask 05-51-15-410-050 H. Close Access (1) Remove the safety devices installed on the landing gears (Ref. TASK 32-00-00-081-801). (2) Close all the access panels that you opened during the procedure. (3) Close the NLG doors (Ref. TASK 32-22-00-410-801). (4) Close the MLG doors (Ref. TASK 32-12-00-410-801). Subtask 05-51-15-860-051 J. 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) Pressurize the Yellow hydraulic system (Ref. TASK 29-00-00-863-803). (4) Pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-802). (5) Retract the flaps (Ref. TASK 27-50-00-866-802). (6) Retract the slats (Ref. TASK 27-80-00-866-802). (7) Retract the spoilers (Ref. TASK 27-60-00-866-802).
EFF : ALL 05-51-15 R SROS
Page 616 Jan 01/02
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**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-15-710-050 K. Do the tests below. NOTE : The tests below are necessary only if: ____ - you did work on the system after you have done the inspection for damage - you found damage on the structure adjacent to the landing gear doors or a flight control surfaces. (1) Operate the flap system. Make sure that the travel is full and that the flap moves freely (Ref. TASK 27-54-00-710-801). (2) Operate the slat system. Make sure that the travel is full and that the slat moves freely (Ref. TASK 27-84-00-710-801). (3) Operate the aileron system. Make sure that the travel is full and that the aileron moves freely (Ref. TASK 27-14-00-710-801). (4) Extend and retract the landing gear. Make sure that landing gear and the landing gear doors move freely (Ref. TASK 32-31-00-710-801). (5) If you find damage only on the landing gear doors or on the structure adjacent to the landing gear doors: (a) Open the NLG doors (Ref. TASK 32-22-00-010-801). (b) Make sure that the NLG doors move freely. (c) Close the NLG doors (Ref. TASK 32-22-00-410-801). (d) Open the MLG doors (Ref. TASK 32-12-00-010-801). Make sure that the MLG doors move freely. (e) Close the MLG doors (Ref. TASK 32-12-00-410-801). (6) Operate the thrust reverser system for correct operation. (Ref. TASK 78-31-00-710-804)
R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-15 301-399, 401-449, 451-499, SROS
Page 617 Jul 01/05
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**ON A/C 701-749,
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Subtask 05-51-15-710-050-A
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K. Do the tests below.
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NOTE : The tests below are necessary only if: ____ - you did work on the system after you have done the inspection for damage - you found damage on the structure adjacent to the landing gear doors or a flight control surfaces.
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(1) Operate the flap system. Make sure that the travel is full and that the flap moves freely (Ref. TASK 27-54-00-710-801).
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(2) Operate the slat system. Make sure that the travel is full and that the slat moves freely (Ref. TASK 27-84-00-710-801).
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(3) Operate the aileron system. Make sure that the travel is full and that the aileron moves freely (Ref. TASK 27-14-00-710-801).
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(4) Extend and retract the landing gear. Make sure that landing gear and the landing gear doors move freely (Ref. TASK 32-31-00-710-801).
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(5) If you find damage only on the landing gear doors or on the structure adjacent to the landing gear doors:
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(a) Open the NLG doors (Ref. TASK 32-22-00-010-801).
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(b) Make sure that the NLG doors move freely.
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(c) Close the NLG doors (Ref. TASK 32-22-00-410-801).
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(d) Open the MLG doors (Ref. TASK 32-12-00-010-801). Make sure that the MLG doors move freely.
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(e) Close the MLG doors (Ref. TASK 32-12-00-410-801).
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(6) Operate the thrust reverser system for correct operation. (Ref. TASK 78-31-00-740-802)
R EFF : 701-749, 05-51-15 SROS
Page 618 Oct 01/00
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**ON A/C ALL Subtask 05-51-15-860-053 L. Put the Aircraft back to its Initial Configuration (1) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (2) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803). (3) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802). (4) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). 5. Close-up ________ Subtask 05-51-15-942-050 A. Put the Aircraft back to its Initial Configuration (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. (4) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-51-15 SROS
Page 619 Oct 01/00
INSPECTION AFTER BRAKE EMERGENCY APPLICATION OR OVERHEAT - INSPECTION/CHECK ___________________________________________________________________________ TASK 05-51-16-200-801 Inspection After Brake Overheat 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 : 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. R R R R R R R R
CAUTION : DO NOT USE POWDER EXTINGUISHANTS. THE DEPOSITS EXTINGUISH THE FIRE, _______ BUT THEY ALSO PREVENT SATISFACTORY DISSIPATION OF THE HEAT. THIS CAN CAUSE PERMANENT STRUCTURAL DAMAGE TO: - THE BRAKE - THE WHEEL - THE WHEEL AXLE. YOU MUST NOT APPLY THE EXTINGUISHANT (WATER MIST INCLUDED) WITH A SPRAY GUN DIRECTLY ON THE CARBON HEAT PACK OF THE BRAKE. THIS CAN CAUSE THERMAL SHOCK. 1. __________________ Reason for the Job This inspection is necessary after a crew report of: - a brake temperature of more than 800 deg. C, - wheel fuse plug(s) melt. The temperature of the brakes can be too high after: - an acceleration stop, - the emergency application of the brakes, - frequent use of the brakes, - a failure of the braking control. If the temperature of the brakes is too high, one or more of the fuse plugs can melt. This causes: - damage to the tire, - possible damage to the wheel, - too much load on the opposite tire which can cause damage.
EFF : ALL 05-51-16 SROS
Page 601 Jan 01/07
2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
warning notice wheel chocks
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------05-51-15-200-801 R 32-11-00-210-801 32-40-00-200-801 32-41-11-000-801 32-41-11-400-801 32-41-14-000-801 32-41-14-400-801 32-42-00-710-801 32-42-27-000-801 32-42-27-400-801 32-43-00-710-801
Inspection of the Aircraft after a Tire Burst or Tread Throw or Wheel Failure Inspection for Discoloration of the Overheat Indication Paint Inspection/Check of the Brakes Removal of the MLG Wheel Installation of the MLG Wheel 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) Operational Test of the Normal Braking System Removal of the Wheel Brake Installation of the Wheel Brake Operational Test of the Alternate Braking System
3. __________ Job Set-up Subtask 05-51-16-941-050 A. Safety Precautions R
(1) Instructions after brake overheat:
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(a) If a tire is inflated, do not go near the area around the wheel for approximately one hour. When you go near, go from the front or rear and not from the side of the wheel.
EFF : ALL 05-51-16 SROS
Page 602 Jul 01/05
(b) Unless there is a fire, do not apply the extinguishing agent (liquid, water, mist, foam, etc.) with a spray gun into a hot tire if it is inflated. Do not apply the extinguishing agent directly into the heat pack of the brake or into the wheel. This can cause thermal shock to the stressed parts. Specially, do not use CO2 as this has a strong cooling effect which is not the same in all areas. It can cause an explosion in the stressed parts. Extinguishant on hot wheels can: - increase the time necessary for the fuse(s) to melt, or - prevent operation of the fuse(s). You must let the brake get cool by itself for at least one hour or use the cooling fans (if installed).
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NOTE : You can use blowers or air conditioning equipment only ____ after: - the temperature of the fuses decreases (more than one hour after the aircraft stops) or - the fuses are melted. You must not use these if you can see flames or burning embers.
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(c) If there is a fire, immediately extinguish the fire. Do not wait until the tires are deflated. Come near the wheel only from the front or from the rear.
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NOTE : We do not recommend that you use multi-purpose powders as ____ they can change into solid or enameled deposit. These agents extinguish the fire but they decrease the heat dissipation speed. This can cause permanent structural damage to the brake, the wheel or wheel axle. (d) Do not apply the parking brake. (e) Put a warning notice in the cockpit to tell persons not to operate the landing gear control lever.
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(f) Put the wheel chocks in position. (g) Clean all the parts if extinguishing agents were used.
EFF : ALL 05-51-16 SROS
Page 603 Jul 01/05
4. Procedure _________ Subtask 05-51-16-210-052 A. Inspection of the Aircraft (1) If there is a tire burst: - do the Inspection of the Aircraft after a Tire Burst or Tread Throw (Ref. TASK 05-51-15-200-801). Subtask 05-51-16-210-050 B. Inspection of the Wheels and Brakes (Ref. TASK 32-42-27-000-801) (Ref. TASK 32-42-27-400-801) (Ref. TASK 3240-00-200-801) (Ref. TASK 32-11-00-210-801) (Ref. TASK 32-41-11-000-801) (Ref. TASK 32-41-11-400-801) (Ref. TASK 32-41-14-000-801) (Ref. TASK 3241-14-400-801)
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| |Inspection after wheel fuse plug(s) | | | | | | | | |melt and the reported cockpit | | | | | | | | |indication of the brake temperature is | | | | | | | | |not more than 800 deg.C. | | | | | | | | | | | | | | | | | |(1) Remove the related wheel and the | X | | | | | | | | adjacent wheel for overhaul | | | | | | | | | (Ref. TASK 32-41-11-000-801). | | | | | | | | | (Refer to the manufacturers | | | | | | | | | instructions for the overhaul | | | | | | | | | procedure). | | | | | | | | |(2) Examine the brake unit for damage | X | | | | | | | | or distortion. | | | | | | | | | (Ref. TASK 32-40-00-200-801) | | | | | | | | | (a) Make sure that there is no | | | | | | | | | hydraulic fluid leakage at | | | | | | | | | the piston, liners, supply | | | | | | | | | lines, self blanking unions and| | | | | | | | | bleed screws. | | | | | | | | | (b) Clean the piston housing with | | | | | | | | | a cloth and make sure it is in | | | | | | | | | the correct condition (no | | | | | | | | | separation, no blisters). | | | | | | | | | (c) Make sure that the heat pack is| | | | | | | | | serviceable: | | | | | |
EFF : ALL 05-51-16 SROS
Page 604 Jul 01/06
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - carbon integrity | | | | | | | | | - free movement of the rotor | | | | | | | | | discs | | | | | | | | | - cracks or signs of oxidation | | | | | | | | | on the part of the rotor | | | | | | | | | discs you can see. | | | | | | | | | NOTE: Be careful with the | | | | | | | | | discs to prevent damage| | | | | | | | | to the protective | | | | | | | | | finish (anti-oxidation | | | | | | | | | paint). | | | | | | | | |If you find damage: | | | | | | | | |- Remove the damaged brake unit for | | X | | | | | | | overhaul | | | | | | | | | (Ref. TASK 32-42-27-000-801). | | | | | | | | | (Refer to the manufacturers | | | | | | | | | instructions for the overhaul | | | | | | | | | procedure). | | | | | | | | |(3) Installation of the removed | | | | | | | | | components | | | | | | | | | (a) Install serviceable components:| | | | | | | | | - for the wheels | | | | | | | | | (Ref. TASK 32-41-11-400-801) | | | | | | | | | - for the brakes | | | | | | | | | (Ref. TASK 32-42-27-400-801). | | | | | | | | | | | | | | | | B.| |Inspection after wheel fuse plug(s) | | | | | | | | |melt and/or the reported cockpit | | | | | | | | |indication of the brake temperature is | | | | | | | | |equal to or more than 800 deg.C. | | | | | | | | | | | | | | | | | |(1) Remove the related wheel for | X | | | | | | | | overhaul | | | | | | | | | (Ref. TASK 32-41-11-000-801). | | | | | | | | | (Refer to the manufacturers | | | | | | | | | instructions for the overhaul | | | | | | | | | procedure). | | | | | | | | | NOTE: If fuse plug is melted, also | | | | | | | | | remove the adjacent wheel for| | | | | | | | | overhaul. | | | | | | | | |(2) Remove the brake for overhaul | X | | | | | | | | (Ref. TASK 32-42-27-000-801). | | | | | | | | | (Refer to the manufacturers | | | | | |
EFF : ALL 05-51-16 SROS
Page 605 Jul 01/06
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R R R
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | instructions for the overhaul | | | | | | | | | procedure). | | | | | | | | |(3) Remove the axle sleeve | X | | | | | | | | (Ref. TASK 32-41-14-000-801). | | | | | | | | |(4) Do the inspection of the Axle for | X | | | | | | | | Discoloration of the overheat | | | | | | | | | indication paint | | | | | | | | | (Ref. TASK 32-11-00-200-801). | | | | | | | | |(5) Examine the axle sleeve for | X | | | | | | | | distortion and damaged surface. | | | | | | | | |(6) Installation of the removed | | | | | | | | | components | | | | | | | | | (a) Install serviceable components:| | | | | | | | | - for the axle sleeve | | | | | | | | | (Ref. TASK 32-41-14-400-801) | | | | | | | | | - for the brakes | | | | | | | | | (Ref. TASK 32-42-27-400-801) | | | | | | | | | - for the wheels | | | | | | | | | (Ref. TASK 32-41-11-400-801). | | | | | | ------------------------------------------------------------------------------Subtask 05-51-16-710-050 C. Operational Test
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(1) Do an operational test of the normal braking system (Ref. TASK 32-4200-710-801). (2) Do an operational test of the alternate braking system (Ref. TASK 3243-00-710-801). 5. Close-up ________ Subtask 05-51-16-942-050 A. Put the Aircraft back to its Initial Configuration (1) Remove the warning notice(s). (2) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
R EFF : ALL 05-51-16 SROS
Page 606 Jul 01/05
___________________________________________________________________ INSPECTION AFTER FLIGHT IN EXCESSIVE TURBULENCE OR IN EXCESS OF VMO ________________ INSPECTION/CHECK TASK 05-51-17-200-801 Inspection after Flight in Excessive Turbulence or in Excess of VMO/MMO 1. __________________ Reason for the Job To do an inspection of the aircraft for structural damage after a flight where excessive load factors occurred. Such load factors can be caused by high turbulence, maneuvers not in the usual limits or in excess of VMO/MMO. To know if the inspection is necessary, refer to Para.3.A.
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2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No
specific specific specific specific
safety barriers warning notice wheel chocks adjustable access platform 16.8 m (55 ft. 1 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 24-41-00-862-801 27-14-00-710-801 27-24-00-710-801 27-34-00-710-801 27-50-00-866-801 27-54-00-710-801 27-64-00-710-801 27-84-00-710-801
Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Operational Test of the Aileron and Hydraulic Actuation Operational Test of the Rudder Servo Control with each Hydraulic System Operational Test of the Elevator and Hydraulic Actuation Extension of the Flaps on the Ground Operational Test of the Flap System Operational Test of the Spoilers Operational Test of the Slat System
EFF : ALL 05-51-17 SROS
Page 601 Jul 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------28-10-00-910-802 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
31-36-00-200-803 32-00-00-481-801 32-12-00-010-801 32-12-00-410-801 53-35-11-000-802 71-13-00-010-802 71-13-00-010-805 71-13-00-410-802 71-13-00-410-805 78-30-00-010-801 78-30-00-010-803 78-30-00-410-801 78-30-00-410-803 78-31-00-710-804 78-31-00-740-802
Access to Fuel Tanks and Work Areas 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) Check of the Load-Report Parameter after Hard/Overweight Landing or Excessive Turbulence Installation of the Safety Devices on the Landing Gears Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Removal of the Fillet Fairings Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Open the Fan Cowl Doors Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Close the Fan Cowl Doors Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Open the Thrust Reverser Cowl Doors Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Close the Thrust Reverser Cowl Doors Thrust Reverser Cycling Test (MCDU) Test of the Thrust Reverser Deployment and Stowage (Engine not Running)
EFF : ALL 05-51-17 SROS
Page 602 Jul 01/06
3. __________ Job Set-up Subtask 05-51-17-200-050 A. Inspection Requirements (1) Definitions R R
NOTE : Excessive turbulence is identified as turbulence that causes ____ large, sudden changes in altitude and/or attitude. It usually causes large variations in airspeed. Passengers and crew are moved violently against their seat belts and loose objects are moved around the aircraft. A flight in excessive turbulence or maneuvering is specified as a flight in which the vertical load factor is out of the range -1g to +2.5g (inclusive) in clean configuration or is out of the range 0g to +2g (inclusive) with the flaps extended. A flight in excess of VM0/MMO is specified as a flight in which:
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(a) the speed is equal to or more than VM0 + 20kts, or
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(b) the mach number is equal to or more than MM0 + 0.02M, or
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(c) the speed or mach number is equal to or more than VMO or MMO, and at which there is a vertical load factor out of the range 0g to +2g (inclusive).
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(2) Confirmation that inspection is necessary (a) After a flight crew report of flight in excessive turbulence, you must do the inspection unless: - The parameters recorded by the DFDR or the DMU load report 15 are less than the values specified above. To know the impact parameters, refer to the DFDR readout or to the DMU load report 15 (Ref. TASK 31-36-00-200-803).
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(b) After a flight crew report of flight in excess of VMO/MMO, you must do the inspection unless: - the values in the flight crew report are less than the values specified above,
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or - the parameters recorded by the DFDR are less than the values specified above.
EFF : ALL 05-51-17 SROS
Page 603 Jul 01/06
Subtask 05-51-17-941-050 B. Safety Precautions (1) Put the safety barriers in position. (2) Put the wheel chocks in position at the main landing gear. (3) Put a warning notice in position in the cockpit to tell persons not to operate the systems. R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-17-010-050 C. Get Access (1) Open the main landing gear doors (Ref. TASK 32-12-00-010-801).
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(2) Put an adjustable access platform in position near the area you want to examine. (3) Install the safety devices on the landing gears (Ref. TASK 32-00-00481-801).
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(4) Open the fan cowls doors (Ref. TASK 71-13-00-010-802) FOR 4030EM1 415BL, 416BR FOR 4030EM2 425BL, 426BR.
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(5) Open the thrust reverser doors (Ref. TASK 78-30-00-010-801) FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR.
EFF : ALL 05-51-17 SROS
Page 604 Jul 01/05
**ON A/C 701-749, Subtask 05-51-17-010-050-A C. Get Access (1) Open the main landing gear doors (Ref. TASK 32-12-00-010-801). R R
(2) Put an adjustable access platform in position near the area you want to examine. (3) Install the safety devices on the landing gears (Ref. TASK 32-00-00481-801).
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(4) Open the fan cowls doors (Ref. TASK 71-13-00-010-805) FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR.
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(5) Open the thrust reverser doors (Ref. TASK 78-30-00-010-803) FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR. **ON A/C ALL Subtask 05-51-17-860-050 D. Aircraft Maintenance Configuration (1) Extend the flaps (Ref. TASK 27-50-00-866-801). (2) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (3) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803). (4) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802). (5) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
EFF : ALL 05-51-17 SROS
Page 605 Jul 01/05
4. Procedure _________ Subtask 05-51-17-210-050 A. Inspection of the Fuselage (Ref. TASK 53-35-11-000-802) NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the non-destructive testing manual (NTM) and use non-destructive test procedures.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Fuselage | | | | | | | | | | | | | | | | A.| | Remove the wing-to-fuselage fillets | | | | | | | | | (Ref. Task 53-35-11-000-802). | | | | | | | | | Examine the junction between the wing | X | | | | | | | | spar box, the rear spar splice, the | | | | | | | | | fuselage skin panels, the panel | | | | | | | | | splices for: | | | | | | | | | - distortion, cracks, pulled or torn | | | | | | | | | fasteners, damaged paintwork. | | | | | | | | | | | | | | | | B.| | Examine the fuselage between FR26 and | | | | | | | | | FR38, the skin panels, the splicing, | X | | | | | | | | the rivets for: | | | | | | | | | - distortion, cracks, pulled or torn | | | | | | | | | fasteners, damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the FWD cargo-compartment | | | | | | | | | panel and examine internally the | | | | | | | | | structure, the frames, the | | X | | | | | | | splices, the rivets, the | | | | | | | | | stringers for: | | | | | | | | | - distortion, cracks, pulled or | | | | | | | | | torn fasteners and damaged | | | | | | | | | paintwork. | | | | | | | | | | | | | | | | C.| | At FR38, examine the top of the joint | | | | | | | | | between STGR10L and 10R for: | | | | | | | | | - cracks, distortion, pulled or torn | | | | | | | | | fasteners, damaged paintwork. | X | | | | | | | | If you find damage: | | | | | | | | | (1) Examine internally the structure, | | | | | |
EFF : ALL 05-51-17 SROS
Page 606 Jul 01/06
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | the stringers, the frames for: | | | | | | | | | - cracks, distortion, pulled or | | X | | | | | | | torn fasteners. | | | | | | | | | | | | | | | | D.| | Examine the fuselage between FR38 and | | | | | | | | | FR91, the skin panels, the splicing, | | | | | | | | | the rivets for: | | | | | | | | | - distortion, cracks, pulled or torn | X | | | | | | | | fasteners, damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Examine internally the structure, | | | | | | | | | the stringers, the frames for: | | | | | | | | | - damage, distortion, pulled or | | X | | | | | | | torn fasteners. | | | | | | | | | | | | | | | | E.| | At FR54, examine the top of the joint | | | | | | | | | between STGR10 and 10R for: | | | | | | | | | - cracks, distortion, pulled or torn | X | | | | | | | | fasteners, damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Examine internally the structure, | | | | | | | | | the stringers, the frames for: | | | | | | | | | - damage, distortion, pulled or | | X | | | | | | | torn fasteners. | | | | | | | | | | | | | | | | F.| | Examine the cut-out corners and rivets| X | | | | | | | | of the door surround panels for: | | | | | | | | | - cracks, distortion, pulling and | | | | | | | | | tears and damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Examine internally the cut-out | | | | | | | | | corners of the door surround | | X | | | | | | | panels for: | | | | | | | | | - cracks, distortion, pulling, | | | | | | | | | tears and other damage. | | | | | | | | | | | | | | | | G.| | Examine the horizontal stabilizer | | | | | | | | | cut-out corners (FR87 to FR91) for: | X | | | | | | | | - cracks, distortion and other damage.| | | | | | | | | If you find damage: | | | | | | | | | (1) Internally examine the cut-out | | | | | | | | | edges of the top and bottom | | | | | | | | | stringers for: | | | | | |
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Page 607 Jul 01/06
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - cracks, damaged paintwork, | | X | | | | | | | pulled or torn fasteners. | | | | | | | | | | | | | | | |2. | | Inspection of the Belly Fairing | | | | | | | | | | | | | | | | A.| | Examine externally the belly fairing | | | | | | | | | panels for: | X | | | | | | | | - cracks, delamination, pulled or torn| | | | | | | | | fasteners and damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the damaged panel. | | X | | | | | | | (2) Examine internally the belly | | | | | | | | | fairing structure, all the | | | | | | | | | components, the pipes, the ducts, | | X | | | | | | | the electrical harnesses for: | | | | | | | | | - distortion, cracks, pulled or | | | | | | | | | torn fasteners and fluid | | | | | | | | | leakage. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-17-210-051 B. Inspection of the Vertical Stabilizer
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NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non-destructive Testing Manual (NTM) and use non-destructive procedures. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Vertical Stabilizer | | | | | | | | | | | | | | | | A.| | Examine the spar box for: | | | | | | | | | - cracks, pulled or torn fasteners, | X | | | | | | | | delamination, damaged paint | | | | | | | | | - wash. | | | | | | | | | If you find damage: | | | | | | | | | (1) Examine the attachment fittings | | | | | | | | | and their adjacent structure, the | | X | | | | | | | front and rear spar webs for: | | | | | |
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Page 608 Jul 01/05
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - damaged paintwork, cracks, | | | | | | | | | delamination, pulled or torn | | | | | | | | | fasteners. | | | | | | | | | (2) On the rear spar, examine the | | | | | | | | | hydraulic lines, the mechanical | | X | | | | | | | linkage, the electrical harnesses,| | | | | | | | | their brackets for: | | | | | | | | | - distortion, cracks, fluid | | | | | | | | | leakage. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-17-210-052 C. Inspection of the Horizontal Stabilizer NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non-destructive Testing Manual (NTM) and use non-destructive test procedures.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Horizontal | | | | | | | | | Stabilizer | | | | | | | | | | | | | | | | A.| | Examine the top and bottom skin | | | | | | | | | panels, the actuator fitting, the ribs| X | | | | | | | | for: | | | | | | | | | - cracks, distortion, pulled or torn | | | | | | | | | fasteners, damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Examine the rear spar web on each | | | | | | | | | side of the pivot bearing fitting | | X | | | | | | | for: | | | | | | | | | - cracks, distortion, pulled or | | | | | | | | | torn fasteners and damaged | | | | | | | | | paintwork. | | | | | | | | | (2) Examine the hydraulic pipes, the | | X | | | | | | | electrical harnesses, the | | | | | | | | | components for: | | | | | | | | | - rupture, cracks, distortion and | | | | | |
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Page 609 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | fluid leakage. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-17-210-053 D. Inspection of the Wing (Ref. TASK 28-10-00-910-802) NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non-destructive Testing Manual (NTM) and use non-destructive procedures.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Wing | | | | | | | | | | | | | | | | A.| | Examine the skin panels for: | | | | | | | | | - distortion, cracks, tears, fluid | X | | | | | | | | leakage or other damage. | | | | | | | | | If you find damage: | | | | | | | | | (1) Get access to the fuel tanks. | | X | | | | | | | (Ref. TASK 28-10-00-910-802) | | | | | | | | | (2) Examine the front spar and the | | X | | | | | | | rear spar, the stringers, the | | | | | | | | | internal structure of the wing, | | | | | | | | | the skin panels, the fasteners | | | | | | | | | for: | | | | | | | | | - cracks, distortion, pulled or | | | | | | | | | torn fasteners. | | | | | | | | | (3) Make sure that the sealant | | X | | | | | | | beads are in the correct | | | | | | | | | condition. | | | | | | | | | (4) Examine the ducts, lines, pipes, | | | | | | | | | the mechanical linkages and | | X | | | | | | | their support for: | | | | | | | | | - distortion, cracks, fluid | | | | | | | | | leakage, damage. | | | | | | | | | Make sure that the attachments | | | | | | | | | are correct. | | | | | | | | | (5) Examine the attachment fitting | | | | | |
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Page 610 Jul 01/05
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | of the engine pylon. | | X | | | | | | | | | | | | | |2. | | Inspection of the Aileron | | | | | | | | | | | | | | | | A.| | Examine the aileron for: | X | | | | | | | | - cracks, distortion, torn or pulled | | | | | | | | | fasteners. | | | | | | | | | If you find damage: | | | | | | | | | (1) Examine the aileron hinge and the | | | | | | | | | actuator for: | | X | | | | | | | - cracks, distortion, torn or | | | | | | | | | pulled fasteners. | | | | | | | | | | | | | | | |3. | | Inspection of the Flaps and Slats | | | | | | | | | | | | | | | | A.| | Examine the slats and flaps and their | X | | | | | | | | fairings for: | | | | | | | | | - cracks, distortion, torn or pulled | | | | | | | | | fasteners. | | | | | | | | | | | | | | | |4. | | Inspection of the Spoilers | | | | | | | | | | | | | | | | A.| | Examine the spoilers for: | | | | | | | | | - distortion, cracks, pulled or torn | X | | | | | | | | fasteners. | | | | | | | | | If you find damage: | | | | | | | | | (1) Examine the spoiler hinges and | | X | | | | | | | actuator for: | | | | | | | | | - cracks, distortion and other | | | | | | | | | damage. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-17-210-054 E. Inspection of the Pylons NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the non-destructive testing manual (NTM) and use non-destructive procedures.
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Page 611 Jul 01/05
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Pylon | | | | | | | | | | | | | | | | A.| | Examine the lateral panels around the | X | | | | | | | | access door cut-out for: | | | | | | | | | - cracks, distortion, damaged | | | | | | | | | paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Open the access door and remove | | X | | | | | | | the access panels. | | | | | | | | | (2) Examine the lower spar, the rib- | | X | | | | | | | to-panel attachments, the | | | | | | | | | structure for: | | | | | | | | | - distortion, cracks, rupture and | | | | | | | | | fluid leakage. | | | | | | | | | (3) Examine the components, the pipes,| | | | | | | | | the ducts, the electrical | | X | | | | | | | harnesses and their brackets for: | | | | | | | | | - distortion, cracks, rupture and | | | | | | | | | fluid leakage. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-17-210-055 F. Inspection of the Nacelle
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NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non-destructive Testing Manual (NTM) and use non-destructive test procedures. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Nacelle | | | | | | | | | | | | | | | | A.| | Examine the nacelle for: | | | | | | | | | - cracks, distortion, delamination, | X | | | | | | | | damaged paintwork, loose rivets and | | | | | | | | | signs of shearing. | | | | | | | | | If you find damage: | | | | | | | | | (1) Open the fan cowl doors. | | X | | | | | | | (2) Open the thrust reverser doors. | | X | | | |
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Page 612 Jul 01/05
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (3) Examine the doors internally for: | | X | | | | | | | - damage. | | | | | | | | | (4) Examine the attachments of the | | | | | | | | | air intake cowl to the fan case | | X | | | | | | | for: | | | | | | | | | - cracks, distortion, pulled or | | | | | | | | | torn fasteners. | | | | | | | | | Make sure that the attachments are| | | | | | | | | correct. | | | | | | | | | (5) Examine all the cowl hinges, | | | | | | | | | fittings and the cowl attachment | | X | | | | | | | points on the pylon for: | | | | | | | | | - damage. | | | | | | | | | (6) Examine the components, the pipes,| | | | | | | | | the ducts, the electrical | | | | | | | | | harnesses for: | | X | | | | | | | - damage | | | | | | | | | - fluid leakage. | | | | | | ------------------------------------------------------------------------------**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-17-410-050 G. Close Access (1) Close the main landing gear doors (Ref. TASK 32-12-00-410-801).
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(2) Close the fan cowl doors (Ref. TASK 71-13-00-410-802) FOR 4030EM1 415BL, 416BR FOR 4030EM2 425BL, 426BR.
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(3) Close the thrust reverser doors (Ref. TASK 78-30-00-410-801) FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR. (4) Close the main landing gear door (Ref. TASK 32-12-00-410-801).
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Page 613 Jul 01/05
**ON A/C 701-749, Subtask 05-51-17-410-050-A G. Close Access (1) Close the main landing gear doors (Ref. TASK 32-12-00-410-801).
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(2) Close the fan cowl doors (Ref. TASK 71-13-00-410-805) FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR.
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(3) Close the thrust reverser doors (Ref. TASK 78-30-00-410-803) FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR. (4) Close the main landing gear door (Ref. TASK 32-12-00-410-801). **ON A/C ALL Subtask 05-51-17-860-051 H. 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).
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(3) Pressurize the Yellow hydraulic system (Ref. TASK 29-00-00-863-803).
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(4) Pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-802).
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Page 614 Jul 01/05
Subtask 05-51-17-710-050 J. Do the flight system test NOTE : The tests below are necessary only if you find damage to the ____ structure adjacent to a flight control surface. (1) Operate the aileron system. Make sure that the travel is full and that the ailerons move freely (Ref. TASK 27-14-00-710-801). (2) Operate the flap system. Make sure that the travel is full and that the flaps move freely (Ref. TASK 27-54-00-710-801). (3) Operate the slat system. Make sure that the travel is full and that the slats move freely (Ref. TASK 27-84-00-710-801).
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(4) Operate the spoiler system. Make sure that the travel is full and that the spoilers move freely (Ref. TASK 27-64-00-710-801).
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(5) Operate the THS system. Make sure that the travel is full and that the THS moves freely.
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(6) Operate the elevator system. Make sure that the travel is full and that the elevators move freely (Ref. TASK 27-34-00-710-801).
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(7) Operate the rudder system. Make sure that the travel is full and that the rudder moves freely (Ref. TASK 27-24-00-710-801).
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**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-17-710-051 K. Do a test of the thrust reverser system. NOTE : The test below is necessary only if you find damage to the ____ structure adjacent to a cowl surface. (1) Operate the thrust reverser system (Ref. TASK 78-31-00-710-804). Make sure that the travel is full and that the thrust reverser moves freely.
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Page 615 Jul 01/05
**ON A/C 701-749, Subtask 05-51-17-710-051-A K. Do a test of the thrust reverser system. NOTE : The test below is necessary only if you find damage to the ____ structure adjacent to a cowl surface. (1) Operate the thrust reverser system (Ref. TASK 78-31-00-740-802). Make sure that the travel is full and that the thrust reverser moves freely. **ON A/C ALL 5. Close-up ________ Subtask 05-51-17-860-052 A. Put the Aircraft back to its Initial Configuration R
(1) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801).
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(2) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803).
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(3) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802).
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(4) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). Subtask 05-51-17-942-050 B. Put the Aircraft back to its Initial Configuration (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.
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Page 616 Jul 01/05
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INSPECTION AFTER LIGHTNING STRIKE - INSPECTION/CHECK ____________________________________________________ TASK 05-51-18-200-801 Inspection after Lightning Strike WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A _______ FALL CAN KILL OR INJURE YOU. 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 After a lightning strike, before the aircraft continues in service, you must: - do a general inspection of the total surface of the aircraft to find the strike areas, - do a careful inspection of the strike areas to find the type and quantity of possible damage. - if you find damage, make a decision about the necessary repair/action. NOTE : To do this inspection, you must have: ____ - a set of access platforms, 2 m (6.56 ft.) to 17 m (55.9 ft.) - or an adjustable access platform, 2 m (6.56 ft.) to 17 m (55.9 ft.) - or a manlift aerial boom, 2 m (6.56 ft.) to 17 m (55.9 ft.) 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
warning notices adjustable access platform 17 m (55 ft. 9 in.)
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Page 601 Apr 01/99
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------23-11-00-710-801 23-12-00-710-801 23-36-00-710-808 23-61-00-200-801 24-22-51-210-802 24-41-00-862-801 27-14-00-710-801 27-14-51-000-801 27-14-51-000-802 27-14-51-400-801 27-14-51-400-802 27-24-00-710-801 27-24-51-000-801 27-24-51-400-801 27-34-00-710-801 R R
27-34-51-000-801 27-34-51-400-801 27-44-00-710-801 27-50-00-866-801 27-50-00-866-802 27-54-00-710-801 27-60-00-866-801 27-60-00-866-802 27-64-00-710-801 27-84-00-710-801 29-00-00-864-804
Operational Test of the HF System Operational Test of the VHF System Operational Test of the Landscape-Camera System Check the Resistance from the Static Discharger to the Base (Retainer) and from the Base (Retainer) to the Aircraft Structure Visual Inspection of the Lightning Protection Module (19XU1,19XU2) De-energize the Aircraft Electrical Circuits from the External Power A Operational Test of the Aileron and Hydraulic Actuation Removal of the Inboard Aileron Servo-Control (7CS1,7CS2,8CS1,8CS2) Removal of the Outboard Aileron Servo-Control (9CS1,9CS2,10CS1,10CS2) Installation of the Inboard Aileron Servo-Control (7CS1,7CS2,8CS1,8CS2) Installation of the Outboard Aileron Servo-Control (9CS1,9CS2,10CS1,10CS2) Operational Test of the Rudder Servo Control with each Hydraulic System Removal of the Rudder Servo Control (5002CY1, 5002CY2, 5002CY3) Installation of the Rudder Servo Control (5002CY1, 5002CY2, 5002CY3) Operational Test of the Elevator and Hydraulic Actuation Removal of the Elevator Servo-Control Units Installation of the Elevator Servo-Control Units Operational Test of the Trimmable Horizontal Stabilizer (THS) Actuator Jamming Protection Device Extension of the Flaps/Slats on the Ground Retraction of the Flaps/Slats on the Ground Operational Test of the Flap System Extension of the Spoilers for Maintenance Retraction of the Spoilers after Maintenance Operational Test of the Spoilers Operational Test of the Slat System Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------30-31-00-710-801 30-42-00-710-801 R
30-71-00-740-801 30-81-00-710-801 32-00-00-481-801 32-11-00-220-801
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32-12-00-010-801 32-12-00-410-801 32-21-00-220-801 32-22-00-010-801 32-22-00-410-801 32-31-00-740-801 32-46-00-740-801 33-41-00-710-802 33-42-11-400-801 33-47-00-710-801 33-48-00-710-801 33-49-00-710-801 34-11-00-710-801 34-11-15-200-801 34-11-19-000-801 34-11-19-400-801 34-13-00-710-803 34-13-00-740-803 34-22-00-710-801 34-36-00-710-801 34-36-00-710-802 34-36-00-710-803 34-36-00-720-801 34-36-00-720-802
Operational Test of the Probe Ice Protection Operational Test of the Windshield Anti Icing and Defogging BITE Test of the Waste Water Ice Protection (via CIDS POWER-UP) Operational Test of the Ice Detection System Installation of the Safety Devices on the Landing Gears Detailed Inspection of Main Gear Structure comprising: Main Fittings, Sliding Piston, Bogie Beam, Pitch Trimmer, Sidestay Assy, Lock Pins Assembly ... Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Detailed Inspection of the Nose Gear Structure comprising : Main Fitting (Barrel), Sliding Member, Torque Links, Drag Stay Upper and Lower Arm .... Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance BITE Test of the Normal Extension and Retraction System BITE Test of the BSCU and its Related Systems Operational Test of the Navigation Lights Installation of the Landing Light (6LB1, 6LB2) Operational Test of the Logo Lights Operational Test of the Anti-Collision/Strobe Lighting Operational Test of the Wing and Engine Scan Lighting Operational Test of the AIR DATA Switching Inspection/Check of the Pitot Probe (9DA1, 9DA2, 9DA3) Removal of the Angle of Attack Sensor (3FP1, 3FP2, 3FP3) Installation of the Angle of Attack Sensor (3FP1, 3FP2, 3FP3) AOA SENSOR TEST SYSTEM TEST of the ADR Operational test of the Standby Compass Operational Test of the ILS Operational Test of the ILS Function Operational Test of the GPS Function Functional Test of the ILS Functional Test of the ILS Function
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Page 603 Jul 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------34-41-00-710-802 34-41-00-740-801 34-41-11-000-801 34-41-11-400-801
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34-42-00-740-801 34-43-00-740-801 34-48-00-740-801 34-51-00-740-801 34-52-00-740-801 34-53-00-710-801 34-55-00-710-801 49-00-00-710-801 53-15-11-200-801 55-32-11-000-801 55-34-11-000-801 56-11-11-200-801 56-11-12-200-801 56-12-11-200-801 73-21-00-710-803 73-21-00-710-812 78-31-00-710-804 78-31-00-740-802 05-51-18-991-004 05-51-18-991-005
Operational test of the Weather-Radar Antenna Scanning BITE test of the Weather Radar Removal of the Weather Radar Antenna Assembly (7SQ, 11SQ) Installation of the Weather Radar Antenna Assembly (7SQ, 11SQ) BITE Test of the Radio Altimeter BITE test of the TCAS Operational test of GPW Computer by BITE BITE Test of the DME BITE test of the ATC Operational Test of the ADF Operational Test of the VOR Operational Test of the APU Detailed Inspection of the Radome (110AL) Removal of the Vertical Stabilizer Leading-Edge Removal of the Vertical Stabilizer Tip Inspection of the Windshields (3DG1,3DG2). Inspection of the Fixed Windows (7DG1,7DG2) Inspection of the Sliding Windows (8DG1,8DG2). Full Authority Digital Engine Control (FADEC) System Static Test Test of the FADEC System Thrust Reverser Cycling Test (MCDU) Test of the Thrust Reverser Deployment and Stowage (Engine not Running) Fig. 601 Fig. 602
3. __________ Job Set-up Subtask 05-51-18-210-076 A. General (1) Lightning (a) Lightning always has two or more attachment points (one entry and one exit) on the aircraft skin. (b) Lightning moves back along the surface of the aircraft (swept stroke zone). This can cause a chain of scattered attachment points along a line in the direction of travel of the aircraft. (c) Lightning hits some areas more frequently than others.
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Page 604 Jan 01/06
(2) Aircraft zoning (Ref. Fig. 601/TASK 05-51-18-991-004) (a) The aircraft is divided into three zones related to the probability of lightning strike: 1 _
Zone 1: - surfaces where there is a high probability of initial lightning attachment (entry or exit).
2 _
Zone 2: - surfaces where there is a high probability of a swept stroke zone. The lightning strike has its initial point of attachment in Zone 1 and moves into Zone 2.
3 _
Zone 3: - this zone includes all of the aircraft surfaces that are not in Zone 1 and 2. In Zone 3 there is a low probability of attachment of a lightning strike. However, high lightning currents can go through Zone 3 by direct conduction between 2 attachment points. Zone 3 currents will also go into Zones 1 and 2.
(b) Zones 1 and 2 are divided into A and B areas related to the probability of continued attachment of the arc (hang on). The probability of arc hang on is low in A areas and high in B areas. 1 _
Zone 1A: - area where there is a high probability of initial attachment and low probability of arc hang on, such as the forward-mounted pitot probes, the radome diverter strips and the nacelle leading edges.
2 _
Zone 1B: - area where there is a high probability of initial attachment and high probability of arc hang on, such as the wing, stabilizers and fin tips and some trailing edge areas.
3 _
Zone 2A: - a swept stroke zone with low probability of arc hang on, such as mid-chord regions of the wing surface, aft of an engine and the total fuselage surface.
4 _
Zone 2B: - a swept stroke zone with high probability of arc hang on, such as the wing trailing edge aft of Zone 2A.
EFF : ALL 05-51-18 SROS
Page 605 Apr 01/98
Lightning Strike Inspection Areas Figure 601/TASK 05-51-18-991-004 EFF : ALL 05-51-18 SROS
Page 606 Apr 01/98
(3) Effects on the aircraft structure and systems. There are two types of possible risks to the aircraft: - indirect effects - direct effects. (a) Indirect effects. 1 _
Electromagnetic fields: - the electromagnetic fields related to the lightning attachment can cause unwanted transient voltages and currents in the aircraft wiring and systems. In some conditions (low intensity strike, high protection), the effect on the systems can be temporary and the systems can operate correctly again after the strike. In other conditions (low protection, no circuit protection devices), the damage can be permanent and it will be necessary to replace parts.
(b) Direct effects The direct effects are the physical damage related to signs such as: 1 _
Pitting/meltthrough: - this is the action of the electrical arc formed when a lightning stroke attaches to the aircraft (arc root damage at the attachment points or damage caused by current flow which can appear also far from the attachment points). - signs of a lightning attachment are pitting and scorch marks and paint discoloration. On composite components, in addition to paint discoloration and skin puncturing, some delamination of the fibers can occur. If there is skin puncturing, there can be damage to the grounded equipment below composite material fairings. - you must always compare the damage you find with the limits given in the Structural Repair Manual (SRM).
2 _
Magnetic force: - the damage usually occurs where a small area causes the density of the current to be high (e.g. a bonding lead installed at a control surface hinge).
3 _
Resistive heating: - when lightning currents flow through an aircraft structure, energy is changed to heat along its path. - resistive heating usually causes marks of the weld type, specially where the lightning current flows for some time.
EFF : ALL 05-51-18 SROS
Page 607 Apr 01/98
4 _
Acoustic shock wave: - When a lightning strike occurs, there is an acoustic shock wave. If the intensity of this shock wave is high, it can cause deformation of thin metal skins or rupture of thin composite skins.
(4) Inspection requirements: (a) Aircraft are designed to keep the effects of lightning to a minimum and make sure it can continue its flight and land safely after a lightning attachment. (b) It is not possible to accurately know where the attachment will occur but Zone 1 and Zone 2 show the most probable areas of lightning attachment. (c) Lightning strikes do not always give the same quantity of damage. The quantity of damage comes from the intensity of the lightning strike. (d) Therefore, it is necessary to do a full inspection after a lightning strike to make an estimate of the damage and make sure that the aircraft can, as a minimum, continue service in a Master Minimum Equipment List (MMEL) condition. The inspection after a lightning strike refers to: - the type of the system (critical/essential) to specify the tests that are necessary - the requirements of the MMEL NOTE : Critical function: ____ If a critical function fails, it can result in a failure condition that can prevent continued safe flight and landing of the aircraft. Essential function: If an essential function fails, it can result in a failure condition which can have an effect on : - the performance of the aircraft - or the ability of the flight crew to fly the aircraft in the adverse conditions.
EFF : ALL 05-51-18 SROS
Page 608 Apr 01/98
Subtask 05-51-18-210-077 B. Inspection Preparation (1) Before you start, we recommend that you get information from the crew about the flight condition. (2) Make sure that you have the related aircraft Post Flight Report (PFR). (3) All events reported by the crew or by the PFR must be checked in addition/ conjunction with this inspection. Subtask 05-51-18-481-051 C. Safety Precautions Make sure that the safety devices are installed on the landing gears (Ref. TASK 32-00-00-481-801). Subtask 05-51-18-866-051 D. Extension of the Flight Control Surfaces (1) Extend the flaps and the slats (Ref. TASK 27-50-00-866-801). (2) Extend the spoilers (Ref. TASK 27-60-00-866-801). Subtask 05-51-18-010-050 E. Get Access (1) Open the nose gear doors and install the safety devices (Ref. TASK 32-22-00-010-801). (2) Open the main gear doors and install the safety devices (Ref. TASK 32-12-00-010-801). Subtask 05-51-18-860-051 F. Aircraft Maintenance Configuration (1) Make sure that the electrical circuits are de-energized (Ref. TASK 24-41-00-862-801). (2) Make sure that the hydraulic systems are depressurized (Ref. TASK 2900-00-864-804).
EFF : ALL 05-51-18 SROS
Page 609 Apr 01/98
(3) Put warning notices in the cockpit to tell persons not to operate the systems. (4) Put the adjustable access platform in position. 4. Procedure _________ Subtask 05-51-18-210-050 A. Inspection of the total Surface of the Aircraft (Ref. Fig. 602/TASK 05-51-18-991-005) NOTE : All the necessary inspections are visual unless the text gives ____ other instructions. Operators can refer to the Non-destructive Testing Manual (NTM) and use non-destructive procedures. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Radome and the | | | | | | | | | Access Door 121AL (Glide/Slope | | | | | | | | | Antenna access. | | | | | | | | | | | | | | | | A.| | Examine visually the radome external | X | | | | | | | | skin and the lightning diverters for | | | | | | | | | burn marks, change of color, | | | | | | | | | puncturing and other damage. | | | | | | | | | | | | | | | | B.| | Examine the access door 121AL (glide/ | X | | | | | | | | slope antenna access) for burn marks, | | | | | | | | | puncturing and other damage. | | | | | | | | | | | | | | | |2. | | Inspection of the Windshield, Fixed | | | | | | | | | Windows, Sliding Windows and Window | | | | | | | | | Frames. | | | | | | | | | | | | | | | | A.| | Examine visually the windshield, | X | | | | | | | | fixed windows, sliding windows and the| | | | | | | | | window frames for burn marks, change | | | | | | | | | of color and other damage. | | | | | | | | | | | | | | | |3. | | inspection of the Landing Gear Doors | | | | | | | | | | | | | | | | A.| | Examine the skin of all landing gear | X | | | | | | | | doors for burn marks, change of color,| | | | | |
EFF : ALL 05-51-18 R SROS
Page 610 Apr 01/02
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | puncturing and delamination. | | | | | | | | | | | | | | | | B.| | Examine the electrical bonding leads | X | | | | | | | | for breakage and defective attachment.| | | | | | | | | | | | | | | |4. | | Inspection of the Landing Gears. | | | | | | | | | | | | | | | | | | NOTE: Do these checks if the lightning| | | | | | | | | strike occurred: | | | | | | | | | - when the LG was extended and locked | | | | | | | | | down, | | | | | | | | | - during the extension of the LG. | | | | | | | | | and when you find a through hole | | | | | | | | | during the inspection of the landing | | | | | | | | | gears doors. | | | | | | | | | | | | | | | | A.| | Examine all the landing gears. | X | | | | | | | | (1) Examine the LG structure and the | | | | | | | | | points where it is attached for | | | | | | | | | change of color, burn marks and | | | | | | | | | other damage. | | | | | | | | | (2) Examine the shock absorber for | | | | | | | | | change of color and burn marks. | | | | | | | | | (3) Examine all the components | | | | | | | | | attached to the landing gear and | | | | | | | | | fully examine the electrical looms| | | | | | | | | and components for a change of | | | | | | | | | color and burn marks. | | | | | | | | | | | | | | | |5. | | Inspection of the Belly Fairing | | | | | | | | | | | | | | | | A.| | Examine the belly fairing panels | X | | | | | | | | (including the wing-to-fuselage | | | | | | | | | fairings) for change of color, burn | | | | | | | | | marks, puncturing and delamination. | | | | | | | | | Examine fairing screws and fasteners | X | | | | | | | | for burn marks. | | | | | | | | | | | | | | | |6. | | Inspection of the Fuselage | | | | | | | | | | | | | | | | A.| | Externally examine all of the fuselage| X | | | | | | | | skin including rivets and screws for | | | | | | | | | change of color, burns marks and | | | | | |
EFF : ALL 05-51-18 R SROS
Page 611 Apr 01/02
R
Location of the Antennas, Probes and Sensors and Exterior Lights Figure 602/TASK 05-51-18-991-005- 12 (SHEET 1)
EFF : ALL 05-51-18 SROS
Page 612 Jan 01/00
R
Location of the Antennas, Probes and Sensors and Exterior Lights Figure 602/TASK 05-51-18-991-005- 22 (SHEET 2)
EFF : ALL 05-51-18 SROS
Page 613 Jan 01/00
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | small holes. | | | | | | | | | | | | | | | | B.| | Examine all the probes, sensors and | X | | | | | | | | drain masts and the adjacent area for | | | | | | | | | burn marks and change of color. | | | | | | | | | | | | | | | | C.| | Examine carefully all the | X | | | | | | | | communication and navigation antennas | | | | | | | | | and the adjacent area for burn marks, | | | | | | | | | change of color, puncturing and | | | | | | | | | delamination. | | | | | | | | | | | | | | | | D.| | Examine all exterior lights and | X | | | | | | | | adjacent area for burn marks and other| | | | | | | | | damage. | | | | | | | | | | | | | | | | E.| | Examine the APU exhaust for burn marks| X | | | | | | | | and change of color. | | | | | | | | | | | | | | | |7. | | Inspection of the Wings | | | | | | | | | | | | | | | | A.| | Examine the top and bottom skin of the| X | | | | | | | | wings and the leading and trailing | | | | | | | | | edges for burn marks, change of color | | | | | | | | | | | | | | | | B.| | Examine the slats for burn marks and | X | | | | | | | | damage. | | | | | | | | | | | | | | | | C.| | Examine the flap track fairings for | X | | | | | | | | burn marks, change of color, | | | | | | | | | puncturing and other damage. | | | | | | | | | | | | | | | | D.| | Examine the flaps for burn marks, | X | | | | | | | | change of color, puncturing and | | | | | | | | | delamination. | | | | | | | | | | | | | | | | E.| | Examine the spoilers for burn marks, | X | | | | | | | | change of color, puncturing and | | | | | | | | | delamination. | | | | | | | | | | | | | | | | F.| | Examine the ailerons for burn marks, | X | | | | | | | | change of color, puncturing and | | | | | | | | | delamination. | | | | | |
EFF : ALL 05-51-18 R SROS
Page 614 Apr 01/02
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | | | | | | | | G.| | Examine all the static dischargers for| X | | | | | | | | burn marks, damaged tip and breakage. | | | | | | | | | | | | | | | | H.| | Examine the wing tip for burn marks | X | | | | | | | | and burn holes. | | | | | | | | | | | | | | | | I.| | Examine the lights on the wing tip for| X | | | | | | | | burn marks and other damage. | | | | | | | | | | | | | | | |8. | | Inspection of the Engine Nacelles and | | | | | | | | | the Pylons. | | | | | | | | | | | | | | | | A.| | Examine each air intake, inlet cowl, | X | | | | | | | | fan cowl, thrust reverser, exhaust | | | | | | | | | nozzle and the pylon for burn marks, | | | | | | | | | change of color, puncturing and | | | | | | | | | delamination. | | | | | | | | | | | | | | | |9. | | Inspection of the Vertical Stabilizer | | | | | | | | | | | | | | | | A.| | Examine all the static dischargers for| X | | | | | | | | burn marks, damaged tip and breakage. | | | | | | | | | | | | | | | | B.| | Examine the skin of the vertical | X | | | | | | | | stabilizer and the rudder (specially | | | | | | | | | the leading and the trailing edges, | | | | | | | | | the rudder surface in the hinge area | | | | | | | | | and the antenna fairings), the fin | | | | | | | | | tip cap, the fin and rudder tip cap | | | | | | | | | lightning diverters for burn marks, | | | | | | | | | change of color, puncturing, | | | | | | | | | delamination and other damage. | | | | | | | | | | | | | | | |10. | | Inspection of the Horizontal | | | | | | | | | Stabilizer | | | | | | | | | | | | | | | | A.| | Examine all the static dischargers for| X | | | | | | | | burn marks, damaged tip and breakage. | | | | | | | | | | | | | | | | B.| | Examine the skin of the horizontal | X | | | | | | | | stabilizer and elevators (specially | | | | | | | | | the leading and the trailing edges, | | | | | |
EFF : ALL 05-51-18 R SROS
Page 615 Apr 01/02
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | the elevator surface in the hinge | | | | | | | | | area and the tip) for burn marks, | | | | | | | | | change of color, puncturing, | | | | | | | | | delamination and other damage. | | | | | | ------------------------------------------------------------------------------R R R
Subtask 05-51-18-710-056 B. Operational test of the HF system (Ref. TASK 23-11-00-710-801)
R R R R R R R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | Do the operational test of the HF | X | | | | | | | | system (Ref. TASK 23-11-00-710-801). | | | | | | -------------------------------------------------------------------------------
R R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 402-449, 451-499, 701-749, Subtask 05-51-18-210-051
R
C. Check after Damage on the Radome and/or the Access Door 121AL (Ref. TASK 53-15-11-200-801) (Ref. TASK 34-41-00-740-801) (Ref. TASK 3441-00-710-802) (Ref. TASK 34-36-00-710-802) (Ref. TASK 34-36-00-720-802) (Ref. TASK 34-41-11-000-801) (Ref. TASK 34-41-11-400-801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage on the radome | | | | | | | | | during the inspection: | | | | | | | | | (1) Do the detailed inspection of the | | X | | | | | | | radome | | | | | | | | | (Ref. TASK 53-15-11-200-801). | | | | | | | | | If you find a through hole: | | | | | | | | | (a) Examine the weather radar and | | | X | | | | | | the WR antenna drive for burn | | | | | | | | | marks, pitting and other | | | | | | | | | damage. | | | | | |
EFF : ALL 05-51-18 SROS
Page 616 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | If you find damage: | | | | | | | | | - if you find damage on the | | | X | | | | | | flat plate antenna, replace | | | | | | | | | it: | | | | | | | | | (Ref. TASK 34-41-11-000-801)| | | | | | | | | (Ref. TASK 34-41-11-400-801)| | | | | | | | | - do the BITE test of the | | | X | | | | | | weather radar: | | | | | | | | | (Ref. TASK 34-41-00-740-801)| | | | | | | | | - do the operational test of | | | X | | | | | | the weather-radar antenna | | | | | | | | | scanning. | | | | | | | | | (Ref. TASK 34-41-00-710-802)| | | | | | | | | (b) Examine the localizer antenna | | | X | | | | | | for burn marks, pitting and | | | | | | | | | other damage. | | | | | | | | | | | | | | | | B.| | If you find a through hole on the | | X | | | | | | | access door 121AL (glide/slope antenna| | | | | | | | | access): | | | | | | | | | (1) Examine the glide/slope antenna | | | X | | | | | | for sign of arc attachment. | | | | | | | | | | | | | | | | C.| | If you find damage on the localizer | | | | | | | | | antenna and/or the glide/slope | | | | | | | | | antenna: | | | | | | | | | (1) Do the functional test of the ILS | | | X | | | | | | function of the MMR: | | | | | | | | | (Ref. TASK 34-36-00-720-802) | | | | | | | | | NOTE: If an ILS ground test unit is | | | | | | | | | not available, do an operational| | | | | | | | | test of the ILS function of the | | | | | | | | | MMR: | | | | | | | | | (Ref. TASK 34-36-00-710-802) | | | | | | -------------------------------------------------------------------------------
R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-18 301-399, 402-449, 451-499, 701-749, SROS
Page 617 Jul 01/05
**ON A/C 401-401, Subtask 05-51-18-210-051-A R
C. Check after Damage on the Radome and/or the Access Door 121AL (Ref. TASK 53-15-11-200-801) (Ref. TASK 34-41-00-740-801) (Ref. TASK 3441-00-710-802) (Ref. TASK 34-36-00-710-801) (Ref. TASK 34-36-00-720-801) (Ref. TASK 34-41-11-000-801) (Ref. TASK 34-41-11-400-801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage on the radome | | | | | | | | | during the inspection: | | | | | | | | | (1) Do the detailed inspection of the | | X | | | | | | | radome | | | | | | | | | (Ref. TASK 53-15-11-200-801). | | | | | | | | | If you find a through hole: | | | | | | | | | (a) Examine the weather radar and | | | X | | | | | | the WR antenna drive for burn | | | | | | | | | marks, pitting and other | | | | | | | | | damage. | | | | | | | | | If you find damage: | | | | | | | | | - if you find damage on the | | | X | | | | | | flat plate antenna, replace | | | | | | | | | it: | | | | | | | | | (Ref. TASK 34-41-11-000-801)| | | | | | | | | (Ref. TASK 34-41-11-400-801)| | | | | | | | | - do the BITE test of the | | | X | | | | | | weather radar: | | | | | | | | | (Ref. TASK 34-41-00-740-801)| | | | | | | | | - do the operational test of | | | X | | | | | | the weather-radar antenna | | | | | | | | | scanning. | | | | | | | | | (Ref. TASK 34-41-00-710-802)| | | | | | | | | (b) Examine the localizer antenna | | | X | | | | | | for burn marks, pitting and | | | | | | | | | other damage. | | | | | | | | | | | | | | | | B.| | If you find a through hole on the | | X | | | | | | | access door 121AL (glide/slope antenna| | | | | | | | | access): | | | | | | | | | (1) Examine the glide/slope antenna | | | X | | | | | | for sign of arc attachment. | | | | | | | | | | | | | | |
EFF : 401-401, 05-51-18 SROS
Page 618 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | C.| | If you find damage on the localizer | | | | | | | | | antenna and/or the glide/slope | | | | | | | | | antenna: | | | | | | | | | (1) Do the functional test of the ILS:| | | X | | | | | | (Ref. TASK 34-36-00-720-801) | | | | | | | | | NOTE: If an ILS ground test unit is | | | | | | | | | not available, do an operational| | | | | | | | | test of the ILS | | | | | | | | | (Ref. TASK 34-36-00-710-801) | | | | | | ------------------------------------------------------------------------------**ON A/C ALL Subtask 05-51-18-210-053 R
D. Check after Damage on the Windshield, Fixed Windows, Sliding Windows and the Window Frames (Ref. TASK 56-11-11-200-801) (Ref. TASK 56-11-12-200-801) (Ref. TASK 5612-11-200-801) (Ref. TASK 30-42-00-710-801) (Ref. TASK 34-22-00-710-801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage during the | | | | | | | | | inspection: | | | | | | | | | (1) Do the inspection of the related | | X | | | | | | | component: | | | | | | | | | - for the windshield | | | | | | | | | (Ref. TASK 56-11-11-200-801) | | | | | | | | | - for the fixed windows | | | | | | | | | (Ref. TASK 56-11-12-200-801) | | | | | | | | | - for the sliding windows | | | | | | | | | (Ref. TASK 56-12-11-200-801) | | | | | | | | | (2) Do the operational test of the | | X | | | | | | | windshield anti icing and | | | | | | | | | defogging | | | | | | | | | (Ref. TASK 30-42-00-710-801) | | | | | | | | | (3) Do the operational test of the | | X | | | | | | | standby compass | | | | | | | | | (Ref. TASK 34-22-00-710-801) | | | | | | -------------------------------------------------------------------------------
EFF : ALL 05-51-18 SROS
Page 619 Jul 01/05
Subtask 05-51-18-210-078 R
E. Check after Damage on the Landing Gear Doors NOTE : If there is damage to the aircraft structure, refer to the ____ Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage during the | | | | | | | | | inspection: | | | | | | | | | (1) Refer to allowable damage and | | X | | | | | | | repair (Ref. SRM). | | | | | | | | | (2) If you find a through hole: | | X | | | | | | | - examine internally the adjacent | | | | | | | | | and underneath area including | | | | | | | | | all the components (pipes, items| | | | | | | | | of equipment, electrical | | | | | | | | | harnesses...) for damage. | | | | | | | | | if you find damage: | | | | | | | | | - replace or repair the | | | X | | | | | | the related component | | | | | | | | | | | | | | | | B.| | If you find damage on the electrical | | | | | | | | | bonding leads during the inspection: | | | | | | | | | (1) Replace the electrical bonding | | X | | | | | | | lead and/or the defective | | | | | | | | | attachment. | | | | | | -------------------------------------------------------------------------------
EFF : ALL 05-51-18 SROS
Page 620 Jul 01/05
Subtask 05-51-18-210-052 R
F. Check after Damage on the Nose and/or the Main Landing Gear (Ref. TASK 32-21-00-220-801) (Ref. TASK 32-11-00-220-801) (Ref. TASK 3231-00-740-801) (Ref. TASK 32-46-00-740-801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage on the nose and/or | | | | | | | | | the main landing gear during the | | | | | | | | | inspection: | | | | | | | | | (1) do the inspection of the LG: | | | | | | | | | (a) For the NLG: | | X | | | | | | | - (Ref. TASK 32-21-00-220-801)| | | | | | | | | (b) For the MLG: | | X | | | | | | | - (Ref. TASK 32-11-00-220-801)| | | | | | | | | (2) Do a BITE test of the landing gear| | X | | | | | | | (Ref. TASK 32-31-00-740-801) | | | | | | | | | (3) Do a BITE test of the BSCU | | X | | | | | | | (Ref. TASK 32-46-00-740-801) | | | | | | | | | | | | | | | | B.| | If you find damage on the components | | | | | | | | | attached to the landing gear: | | | | | | | | | (1) Examine the electrical components | | X | | | | | | | internally. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-18-210-079
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G. Check after Damage on the Belly Fairing NOTE : If there is damage to the aircraft structure, refer to the ____ Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures.
EFF : ALL 05-51-18 SROS
Page 621 Jul 01/05
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage during the | | | | | | | | | inspection: | | | | | | | | | (1) Refer to the allowable damage and | | X | | | | | | | repair (Ref. SRM). | | | | | | | | | (2) If you find a through hole: | | | | | | | | | (a) Get access internally and | | X | | | | | | | examine the adjacent and | | | | | | | | | underneath area to do a check | | | | | | | | | of all the components (pipes, | | | | | | | | | items of equipment, electrical| | | | | | | | | harnesses...) for damage. | | | | | | | | | If you find damage: | | | | | | | | | - replace or repair the | | | X | | | | | | related component. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-18-210-080 H. Check after damage on the ADIRS Probes and Sensors NOTE : If there is damage to the aircraft structure, refer to the ____ Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures. (Ref. TASK 34-11-15-200-801) (Ref. TASK 34-13-00-740-803) (Ref. TASK 3413-00-710-803) (Ref. TASK 34-11-19-000-801) (Ref. TASK 34-11-19-400-801) (Ref. TASK 30-31-00-710-801) (Ref. TASK 3411-00-710-801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | Pitot probes | | | | | | | | | (1) If you find damage during the | | | | | | | | | inspection: | | | | | | | | | (a) do the inspection/check of the| | X | | | | | | | pitot probes | | | | | | | | | (Ref. TASK 34-11-15-200-801). | | | | | | | | | (b) If you find damage on the | | | | | | | | | adjacent area: | | | | | | | | | - refer to the allowable | | X | | | | | | | damage and repair (Ref. SRM)| | | | | |
EFF : ALL 05-51-18 SROS
Page 622 Jan 01/07
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | | | | | | | | B.| | Static probes | | | | | | | | | (1) If you find damage during the | | | | | | | | | inspection: | | | | | | | | | (a) refer to allowable damage and | | X | | | | | | | repair (Ref. SRM) | | | | | | | | | | | | | | | | C.| | TAT sensors | | | | | | | | | (1) If you find damage during the | | | | | | | | | inspection: | | | | | | | | | (a) do the SYSTEM TEST of the ADR | | X | | | | | | | (Ref. TASK 34-13-00-740-803). | | | | | | | | | (b) If you find damage on the | | | | | | | | | adjacent area: | | | | | | | | | - refer to the allowable | | X | | | | | | | damage and repair (Ref. SRM)| | | | | | | | | | | | | | | | D.| | AOA sensors | | | | | | | | | (1) If you find damage during the | | | | | | | | | inspection: | | | | | | | | | (a) Do the AOA SENSOR TEST | | X | | | | | | | (Ref. TASK 34-13-00-710-803) | | | | | | | | | (b) Manually rotate the AOA | | X | | | | | | | sensors to the full up | | | | | | | | | position then to the full down| | | | | | | | | position and make sure that | | | | | | | | | there is no hard point. | | | | | | | | | If you find a hard point: | | | | | | | | | - replace the related AOA | | | X | | | | | | sensor | | | | | | | | | (Ref. TASK 34-11-19-000-801)| | | | | | | | | (Ref. TASK 34-11-19-400-801)| | | | | | | | | (c) If you find damage on the | | | | | | | | | adjacent area: | | | | | | | | | - refer to the allowable | | X | | | | | | | damage and repair (Ref. SRM)| | | | | | | | | | | | | | | | E.| | If you find damage on AOA, TAT, static| | | | | | | | | or pitot probes: | | | | | | | | | (1) Do the operational test of the | | X | | | | | | | probe ice protection system | | | | | | | | | (Ref. TASK 30-31-00-710-801). | | | | | | | | | (2) Do an operational test of the AIR | | X | | | |
EFF : ALL 05-51-18 R SROS
Page 623 Apr 01/02
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | DATA switching | | | | | | | | | (Ref. TASK 34-11-00-710-801) | | | | | | ------------------------------------------------------------------------------Subtask 05-51-18-210-081 R
J. Check after damage on the Ice Detection Probes (Ref. TASK 30-81-00-710-801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | Ice detection probes | | | | | | | | | (1) If you find damage during the | | | | | | | | | inspection: | | | | | | | | | (a) Do the operational test of the| | X | | | | | | | ice detection system | | | | | | | | | (Ref. TASK 30-81-00-710-801). | | | | | | ------------------------------------------------------------------------------Subtask 05-51-18-210-082
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K. Check after damage on the Drain Masts (Ref. TASK 30-71-00-740-801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | Drain masts | | | | | | | | | (1) If you find damage during the | | | | | | | | | inspection: | | | | | | | | | (a) Do the BITE test of the waste | | X | | | | | | | water ice-protection system | | | | | | | | | (Ref. TASK 30-71-00-740-801). | | | | | | -------------------------------------------------------------------------------
EFF : ALL 05-51-18 SROS
Page 624 Jul 01/05
Subtask 05-51-18-210-083 R
L. Check after Damage on the Exterior Lights (Ref. TASK 33-41-00-710-802) (Ref. TASK 33-42-11-400-801) (Ref. TASK 3347-00-710-801) (Ref. TASK 33-48-00-710-801) (Ref. TASK 33-49-00-710-801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage on exterior lights:| | | | | | | | | (1) Do the operational test of the | | X | | | | | | | related system: | | | | | | | | | (a) For the navigation lights: | | | | | | | | | - (Ref. TASK 33-41-00-710-802)| | | | | | | | | (b) For the landing lights: | | | | | | | | | - do the test given in the | | | | | | | | | installation of the landing | | | | | | | | | lights | | | | | | | | | (Ref. TASK 33-42-11-400-801)| | | | | | | | | (c) For the logo lights: | | | | | | | | | - (Ref. TASK 33-47-00-710-801)| | | | | | | | | (d) For the anti-collision/strobe | | | | | | | | | lightning: | | | | | | | | | - (Ref. TASK 33-48-00-710-801)| | | | | | | | | (e) For the wing and engine scan | | | | | | | | | lightning: | | | | | | | | | - (Ref. TASK 33-49-00-710-801)| | | | | | ------------------------------------------------------------------------------Subtask 05-51-18-210-084
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M. Not applicable. Subtask 05-51-18-210-085
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N. Check after Damage on the Communication Antennas NOTE : If there is damage to the aircraft structure, refer to the ____ Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures. (Ref. TASK 23-12-00-710-801) (Ref. TASK 23-11-00-710-801) (Ref. TASK 5532-11-000-801)
EFF : ALL 05-51-18 SROS
Page 625 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | VHF antennas | | | | | | | | | (1) If you find damage during the | | | | | | | | | inspection: | | | | | | | | | (a) Do the operational test of the| | X | | | | | | | VHF system | | | | | | | | | (Ref. TASK 23-12-00-710-801). | | | | | | | B.| | HF fairing | | | | | | | | | (1) If you find damage on the HF | | | | | | | | | fairing: | | | | | | | | | - refer to allowable damage and | | X | | | | | | | repair (Ref. SRM) | | | | | | | | | (2) If you find a through hole on the | | | | | | | | | HF fairing during the inspection: | | | | | | | | | (a) Remove the HF fairing | | X | | | | | | | (Ref. TASK 55-32-11-000-801) | | | | | | | | | (b) Examine the HF antenna for | | X | | | | | | | signs of arc attachment | | | | | | | | | (c) Do the operational test of the| | X | | | | | | | HF system | | | | | | | | | (Ref. TASK 23-11-00-710-801). | | | | | | ------------------------------------------------------------------------------R R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 402-449, 451-499, 701-749, Subtask 05-51-18-210-086
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P. Check after Damage on the Navigation Antennas NOTE : If there is damage to the aircraft structure, refer to the ____ Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures. (Ref. TASK 34-51-00-740-801) (Ref. TASK 34-42-00-740-801) (Ref. TASK 3443-00-740-801) (Ref. TASK 34-53-00-710-801) (Ref. TASK 34-52-00-740-801) (Ref. TASK 34-55-00-710-801) (Ref. TASK 3448-00-740-801) (Ref. TASK 55-34-11-000-801) (Ref. TASK 34-36-00-710-803)
EFF : ALL 05-51-18 SROS
Page 626 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | DME antennas | | | | | | | | | (1) If you find damage during the | | | | | | | | | inspection: | | | | | | | | | - do the BITE test of the DME | | X | | | | | | | (Ref. TASK 34-51-00-740-801). | | | | | | | | | | | | | | | | B.| | Radio altimeter antennas | | | | | | | | | (1) If you find damage during the | | | | | | | | | inspection: | | | | | | | | | - do the BITE test of the radio | | X | | | | | | | altimeter | | | | | | | | | (Ref. TASK 34-42-00-740-801). | | | | | | | | | | | | | | | | C.| | ADF antenna(s) | | | | | | | | | (1) If you find a through hole during | | | | | | | | | the inspection: | | | | | | | | | - do the operational test of the | | X | | | | | | | ADF | | | | | | | | | (Ref. TASK 34-53-00-710-801). | | | | | | | | | | | | | | | | D.| | ATC antenna(s) | | | | | | | | | (1) If you find damage during the | | | | | | | | | inspection: | | | | | | | | | - do the BITE test of the ATC | | X | | | | | | | (Ref. TASK 34-52-00-740-801). | | | | | | | | | | | | | | | | E.| | TCAS antennas | | | | | | | | | (1) If you find damage during the | | | | | | | | | inspection: | | | | | | | | | - do the BITE test of the TCAS | | X | | | | | | | (Ref. TASK 34-43-00-740-801). | | | | | | | | | | | | | | | | F.| | GPS antennas | | | | | | | | | (1) If you find a through hole during | | | | | | | | | the inspection: | | | | | | | | | - do the operational test of the | | X | | | | | | | GPS | | | | | | | | | (Ref. TASK 34-36-00-710-803) | | | | | | | | | | | | | | | | G.| | VOR/MKR antennas | | | | | | | | | (1) If you find damage on the fin tip | | | | | | | | | cap (VOR fairing): | | | | | | | | | - refer to allowable damage and | | X | | | |
R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-18 301-399, 402-449, 451-499, 701-749, SROS
Page 627 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | repair (Ref. SRM) | | | | | | | | | If you find a through hole on the | | | | | | | | | fin tip cap: | | | | | | | | | - remove the fin tip cap | | X | | | | | | | (Ref. TASK 55-34-11-000-801) | | | | | | | | | - examine the VOR antenna for | | X | | | | | | | signs of arc attachment | | | | | | | | | (2) If you find damage on the MKR | | | | | | | | | antenna and/or a through hole on | | | | | | | | | the fin tip cap: | | | | | | | | | - do the operational test of the | | X | | | | | | | VOR/MKR system | | | | | | | | | (Ref. TASK 34-55-00-710-801). | | | | | | | | | | | | | | | | H.| | GPWS system | | | | | | | | | (1) If you find damage on the radio | | | | | | | | | altimeter antennas and/or ILS | | | | | | | | | antennas (glide and/or localizer):| | | | | | | | | - do the BITE test of the GPWS | | X | | | | | | | (Ref. TASK 34-48-00-740-801). | | | | | | ------------------------------------------------------------------------------**ON A/C 401-401, Subtask 05-51-18-210-086-A R
P. Check after Damage on the Navigation Antennas NOTE : If there is damage to the aircraft structure, refer to the ____ Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures. (Ref. TASK 34-51-00-740-801) (Ref. TASK 34-42-00-740-801) (Ref. TASK 3443-00-740-801) (Ref. TASK 34-53-00-710-801) (Ref. TASK 34-52-00-740-801) (Ref. TASK 34-55-00-710-801) (Ref. TASK 3448-00-740-801) (Ref. TASK 55-34-11-000-801)
R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-18 301-399, 401-449, 451-499, 701-749, SROS
Page 628 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | DME antennas | | | | | | | | | (1) If you find damage during the | | | | | | | | | inspection: | | | | | | | | | - do the BITE test of the DME | | X | | | | | | | (Ref. TASK 34-51-00-740-801). | | | | | | | | | | | | | | | | B.| | Radio altimeter antennas | | | | | | | | | (1) If you find damage during the | | | | | | | | | inspection: | | | | | | | | | - do the BITE test of the radio | | X | | | | | | | altimeter | | | | | | | | | (Ref. TASK 34-42-00-740-801). | | | | | | | | | | | | | | | | C.| | ADF antenna(s) | | | | | | | | | (1) If you find a through hole during | | | | | | | | | the inspection: | | | | | | | | | - do the operational test of the | | X | | | | | | | ADF | | | | | | | | | (Ref. TASK 34-53-00-710-801). | | | | | | | | | | | | | | | | D.| | ATC antenna(s) | | | | | | | | | (1) If you find damage during the | | | | | | | | | inspection: | | | | | | | | | - do the BITE test of the ATC | | X | | | | | | | (Ref. TASK 34-52-00-740-801). | | | | | | | | | | | | | | | | E.| | TCAS antennas | | | | | | | | | (1) If you find damage during the | | | | | | | | | inspection: | | | | | | | | | - do the BITE test of the TCAS | | X | | | | | | | (Ref. TASK 34-43-00-740-801). | | | | | | | | | | | | | | | | F.| | VOR/MKR antennas | | | | | | | | | (1) If you find damage on the fin tip | | | | | | | | | cap (VOR fairing): | | | | | | | | | - refer to allowable damage and | | X | | | | | | | repair (Ref. SRM) | | | | | | | | | If you find a through hole on the | | | | | | | | | fin tip cap: | | | | | | | | | - remove the fin tip cap | | X | | | | | | | (Ref. TASK 55-34-11-000-801) | | | | | | | | | - examine the VOR antenna for | | X | | | | | | | signs of arc attachment | | | | | |
EFF : 401-401, 05-51-18 R SROS
Page 629 Apr 01/02
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (2) If you find damage on the MKR | | | | | | | | | antenna and/or a through hole on | | | | | | | | | the fin tip cap: | | | | | | | | | - do the operational test of the | | X | | | | | | | VOR/MKR system | | | | | | | | | (Ref. TASK 34-55-00-710-801). | | | | | | | | | | | | | | | | G.| | GPWS system | | | | | | | | | (1) If you find damage on the radio | | | | | | | | | altimeter antennas and/or ILS | | | | | | | | | antennas (glide and/or localizer):| | | | | | | | | - do the BITE test of the GPWS | | X | | | | | | | (Ref. TASK 34-48-00-740-801). | | | | | | ------------------------------------------------------------------------------**ON A/C ALL Subtask 05-51-18-210-087 R
Q. Check after Damage on the Fuselage Skin NOTE : If there is damage to the aircraft structure, refer to the ____ Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage during the | | | | | | | | | inspection: | | | | | | | | | (1) Refer to the flow chart for the | | X | | | | | | | allowable damage and repair | | | | | | | | | (Ref. SRM). | | | | | | | | | (2) If you find a through hole: | | X | | | | | | | (a) Examine internally the | | | | | | | | | adjacent area of the damage | | | | | | | | | specially the components, the | | | | | | | | | pipes and the electrical looms| | | | | | | | | for damage. | | | | | | | | | If you find damage: | | | | | | | | | - repair or replace the | | | X | | |
EFF : ALL 05-51-18 SROS
Page 630 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | related component. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-18-210-088 R
R. Check of the APU after Damage on the APU Exhaust (Ref. TASK 49-00-00-710801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage on the APU exhaust | | | | | | | | | during the inspection: | | | | | | | | | (1) Do the operational test of the | | X | | | | | | | APU | | | | | | | | | (Ref. TASK 49-00-00-710-801). | | | | | | ------------------------------------------------------------------------------Subtask 05-51-18-210-089
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S. Check after Damage on the Wings NOTE : If there is damage to the aircraft structure, refer to the ____ Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures. (Ref. TASK 27-84-00-710-801) (Ref. TASK 27-54-00-710-801) (Ref. TASK 2764-00-710-801) (Ref. TASK 27-14-51-000-801) (Ref. TASK 27-14-51-000-802) (Ref. TASK 27-14-51-400-801) (Ref. TASK 2714-51-400-802) (Ref. TASK 27-14-00-710-801)
EFF : ALL 05-51-18 SROS
Page 631 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage on the top or | | | | | | | | | bottom of the wings: | | | | | | | | | (1) Refer to allowable damage and | | X | | | | | | | repair (Ref. SRM) | | | | | | | | | | | | | | | | B.| | If you find damage on the slats: | | | | | | | | | (1) Refer to allowable damage and | | X | | | | | | | repair (Ref. SRM) | | | | | | | | | (2) Do the operational test of the | | X | | | | | | | slats | | | | | | | | | (Ref. TASK 27-84-00-710-801). | | | | | | | | | | | | | | | | C.| | If you find damage on the flap track | | | | | | | | | fairings: | | | | | | | | | (1) Refer to allowable damage and | | X | | | | | | | repair (Ref. SRM) | | | | | | | | | | | | | | | | D.| | If you find damage on the flaps: | | | | | | | | | (1) Refer to allowable damage and | | X | | | | | | | repair (Ref. SRM) | | | | | | | | | (2) Examine the bonding leads (on the | | X | | | | | | | hinges) of the related damaged | | | | | | | | | flap for breakage and defective | | | | | | | | | attachment. | | | | | | | | | If you find damage: | | | | | | | | | - replace the bonding lead and/or | | | X | | | | | | the defective attachment | | | | | | | | | (3) Do the operational test of the | | X | | | | | | | flaps | | | | | | | | | (Ref. TASK 27-54-00-710-801). | | | | | | | | | | | | | | | | E.| | If you find damage on the spoilers: | | | | | | | | | (1) Refer to allowable damage and | | X | | | | | | | repair (Ref. SRM) | | | | | | | | | (2) Examine the bonding leads (on the | | X | | | | | | | hinges) of the related damaged | | | | | | | | | spoiler for breakage and | | | | | | | | | defective attachment. | | | | | | | | | If you find damage: | | | | | | | | | - replace the bonding lead and/or | | | X | | | | | | the defective attachment | | | | | | | | | (3) Do the operational test of the | | X | | | | | | | spoilers | | | | | |
EFF : ALL 05-51-18 R SROS
Page 632 Apr 01/02
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (Ref. TASK 27-64-00-710-801). | | | | | | | | | | | | | | | | F.| | If you find damage on the ailerons: | | | | | | | | | (1) Refer to allowable damage and | | X | | | | | | | repair (Ref. SRM) | | | | | | | | | (2) Examine all the bonding leads of | | X | | | | | | | the aileron hinges and | | | | | | | | | servocontrols of the related | | | | | | | | | damaged aileron for breakage and | | | | | | | | | defective attachment. | | | | | | | | | If you find damage: | | | | | | | | | - replace the bonding lead and/or | | | X | | | | | | the defective attachment | | | | | | | | | (3) Examine the piston rod of each | | X | | | | | | | servocontrol (it must be fully | | | | | | | | | extended) of the related damaged | | | | | | | | | aileron for burn marks, damage and| | | | | | | | | leaks. | | | | | | | | | If you find a leak or damage: | | | | | | | | | (a) Replace the related aileron | | | X | | | | | | servocontrol | | | | | | | | | (Ref. TASK 27-14-51-000-801) | | | | | | | | | (Ref. TASK 27-14-51-400-801) | | | | | | | | | (Ref. TASK 27-14-51-000-802) | | | | | | | | | (Ref. TASK 27-14-51-400-802) | | | | | | | | |NOTE: If you are at a line station and | | | | | | | | | you cannot do the inspection of | | | | | | | | | the piston rod, do this check: | | | | | | | | | - operate the ailerons 10 times | | | | | | | | | fully in each direction then | | | | | | | | | make sure from the ground that | | | | | | | | | there are no leaks below the | | | | | | | | | aileron servocontrols. | | | | | | | | | You must do this check before | | | | | | | | | each flight until the return to| | | | | | | | | the main base. You can do the | | | | | | | | | check before each flight for a | | | | | | | | | maximum of 3 days or 10 flights| | | | | | | | | - At the first return to the main| | | | | | | | | base, you must do the | | | | | | | | | inspection of the piston rods. | | | | | | | | | (4) Do the operational test of the | | X | | | | | | | ailerons | | | | | |
EFF : ALL 05-51-18 R SROS
Page 633 Apr 01/02
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (Ref. TASK 27-14-00-710-801). | | | | | | ------------------------------------------------------------------------------**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-18-210-054 T. Check after Damage on the Engine Nacelles and Pylons NOTE : If there is damage to the aircraft structure, refer to the ____ Structural Repair Manual (SRM) and/or to the applicable Nacelle Structural Repair Manual. The SRM has the approved damage limits and repair procedures.
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(Ref. TASK 78-31-00-710-804) (Ref. TASK 73-21-00-710-803) (Ref. TASK 2422-51-210-802)
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage on the air intake, | | | | | | | | | inlet cowl, fan cowl, thrust reverser,| | | | | | | | | exhaust nozzle or the pylon: | | | | | | | | | (1) Refer to the allowable damage and | | X | | | | | | | repair (Ref. SRM and/or applicable| | | | | | | | | Nacelle SRM). | | | | | | | | | (2) At the first return to the main | | X | | | | | | | base, do the inspection of the | | | | | | | | | lightning protection module | | | | | | | | | (Ref. TASK 24-22-51-210-802) | | | | | | | | | (3) If you find damage on the thrust | | | | | | | | | reverser: | | | | | | | | | (a) Do an operational test of the | | X | | | | | | | thrust reverser system | | | | | | | | | (Ref. TASK 78-31-00-710-804). | | | | | | | | | (4) If you find a through hole | | | | | | | | | on the fan cowl: | | | | | | | | | (a) Do a ground test of the FADEC | | X | | | | | | | (Ref. TASK 73-21-00-710-803) | | | | | | -------------------------------------------------------------------------------
EFF : ALL 05-51-18 SROS
Page 634 Jan 01/06
**ON A/C 701-749, Subtask 05-51-18-210-054-A T. Check after Damage on the Engine Nacelles and Pylons NOTE : If there is damage to the aircraft structure, refer to the ____ Structural Repair Manual (SRM) and/or to the applicable Nacelle Structural Repair Manual. The SRM has the approved damage limits and repair procedures.
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(Ref. TASK 78-31-00-740-802) (Ref. TASK 73-21-00-710-812) (Ref. TASK 2422-51-210-802)
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage on the air intake, | | | | | | | | | inlet cowl, fan cowl, thrust reverser,| | | | | | | | | exhaust nozzle or the pylon: | | | | | | | | | (1) Refer to the allowable damage and | | X | | | | | | | repair (Ref. SRM and/or applicable| | | | | | | | | Nacelle SRM). | | | | | | | | | (2) At the first return to the main | | X | | | | | | | base, do the inspection of the | | | | | | | | | lightning protection module | | | | | | | | | (Ref. TASK 24-22-51-210-802) | | | | | | | | | (3) If you find damage on the thrust | | | | | | | | | reverser: | | | | | | | | | (a) Do an operational test of the | | X | | | | | | | thrust reverser system | | | | | | | | | (Ref. TASK 78-31-00-740-802). | | | | | | | | | (4) If you find a through hole | | | | | | | | | on the fan cowl: | | | | | | | | | (a) Do a ground test of the FADEC | | X | | | | | | | (Ref. TASK 73-21-00-710-812) | | | | | | -------------------------------------------------------------------------------
EFF : 701-749, 05-51-18 SROS
Page 635 Jan 01/06
**ON A/C ALL Subtask 05-51-18-210-090 R
U. Check after Damage on the Stabilizers NOTE : If there is damage to the aircraft structure, refer to the ____ Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures. (Ref. TASK 27-24-51-000-801) (Ref. TASK 27-24-51-400-801) (Ref. TASK 2724-00-710-801) (Ref. TASK 27-34-51-000-801) (Ref. TASK 27-34-51-400-801) (Ref. TASK 27-34-00-710-801) (Ref. TASK 2744-00-710-801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage during the | | | | | | | | | inspection on the skin of the vertical| X | | | | | | | | stabilizer and the rudder, the fin | | | | | | | | | tip cap, the fin and rudder tip cap | | | | | | | | | lightning diverters: | | | | | | | | | (1) Refer to allowable damage and | | X | | | | | | | repair (Ref. SRM) | | | | | | | | | (2) Examine all the electrical bonding| | X | | | | | | | leads of the rudder hinges and | | | | | | | | | servocontrols for breakage and | | | | | | | | | defective attachment. | | | | | | | | | If you find damage: | | | | | | | | | (a) replace the electrical bonding| | | X | | | | | | lead and/or the defective | | | | | | | | | attachment | | | | | | | | | (3) At the first return to the main | | X | | | | | | | base, examine the piston rod of | | | | | | | | | each rudder servocontrol (it must | | | | | | | | | be fully extended) for damage and | | | | | | | | | burn marks and make sure that | | | | | | | | | there are no leaks. | | | | | | | | | If you find a leak or damage: | | | | | | | | | - replace the related rudder | | | X | | | | | | servocontrol | | | | | | | | | (Ref. TASK 27-24-51-000-801) | | | | | | | | | (Ref. TASK 27-24-51-400-801). | | | | | | | | | (4) Do an operational test of the | | X | | | |
EFF : ALL 05-51-18 SROS
Page 636 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | rudder | | | | | | | | | (Ref. TASK 27-24-00-710-801). | | | | | | | | | | | | | | | | B.| | If you find damage during the | | | | | | | | | inspection of the horizontal | | | | | | | | | stabilizer and elevators: | | | | | | | | | (1) Refer to allowable damage and | | X | | | | | | | repair (Ref. SRM) | | | | | | | | | (2) Examine all the electrical bonding| | X | | | | | | | leads of the elevator hinges and | | | | | | | | | servocontrols of the related | | | | | | | | | damaged elevator for breakage and | | | | | | | | | defective attachment. | | | | | | | | | If you find damage: | | | | | | | | | (a) replace the electrical bonding| | | X | | | | | | lead and/or the defective | | | | | | | | | attachment. | | | | | | | | | (3) Examine the piston rod of each | | X | | | | | | | elevator servocontrol (it must be | | | | | | | | | fully extended) of the related | | | | | | | | | damaged elevator for burn marks, | | | | | | | | | damage and leaks. | | | | | | | | | If you find a leak or damage: | | | | | | | | | (a) Replace the related elevator | | | X | | | | | | servocontrol | | | | | | | | | (Ref. TASK 27-34-51-000-801) | | | | | | | | | (Ref. TASK 27-34-51-400-801) | | | | | | | | |NOTE: If you are at a line station and | | | | | | | | | you cannot do the inspection of | | | | | | | | | the piston rod, do this check: | | | | | | | | | - operate the elevators 10 times | | | | | | | | | fully in each direction then | | | | | | | | | make sure from the ground that | | | | | | | | | there are no leaks below the | | | | | | | | | elevator servocontrols. | | | | | | | | | You must do this check before | | | | | | | | | each flight until the return to| | | | | | | | | the main base. You can do the | | | | | | | | | check before each flight for a | | | | | | | | | maximum of 3 days or 10 flights| | | | | | | | | - At the first return to the main| | | | | | | | | base, you must do the | | | | | | | | | inspection of the piston rods. | | | | | |
EFF : ALL 05-51-18 R SROS
Page 637 Apr 01/02
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (4) Do an operational test of the | | X | | | | | | | elevators | | | | | | | | | (Ref. TASK 27-34-00-710-801). | | | | | | | | | (5) Do an operational test of the THS | | X | | | | | | | (Ref. TASK 27-44-00-710-801). | | | | | | ------------------------------------------------------------------------------Subtask 05-51-18-210-091 R
V. Check after Damage on the Static Dischargers (Ref. TASK 23-61-00-200-801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage on the static | | | | | | | | | dischargers of the wing or vertical | | | | | | | | | and horizontal stabilizer. | | | | | | | | | (1) Do a check of the related static | | X | | | | | | | discharger | | | | | | | | | (Ref. TASK 23-61-00-200-801). | | | | | | | | | NOTE: (Ref. CDL 6.01.23 P01): | | | | | | | | | - 2 static dischargers can be | | | | | | | | | missing on each wing. | | | | | | | | | - 2 static discharger can be | | | | | | | | | missing on each horizontal | | | | | | | | | stabilizer tip zone (including| | | | | | | | | the elevator). | | | | | | | | | - 2 static discharger can be | | | | | | | | | missing on the vertical | | | | | | | | | stabilizer tip zone (including| | | | | | | | | the rudder). | | | | | | -------------------------------------------------------------------------------
EFF : ALL 05-51-18 SROS
Page 638 Jul 01/05
**ON A/C 401-449, 451-499, Subtask 05-51-18-210-093 R
W. Check after Damage on the Exterior Video Systems (Ref. TASK 23-36-00-710-808) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| |If you find damage on the Landscape| | | | | | | | |Camera: | | | | | | | | |(1) Do the operational test of the | | X | | | | | | | Landscape- Camera System: | | | | | | | | | (Ref. TASK 23-36-00-710-808). | | | | | | -----------------------------------------------------------------------------**ON A/C ALL 5. Close-up ________ Subtask 05-51-18-866-052 A. Retraction of the Flight control surfaces (1) Retract the flaps and the slats (Ref. TASK 27-50-00-866-802). (2) Retract the spoilers (Ref. TASK 27-60-00-866-802). Subtask 05-51-18-410-050 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the NLG doors (Ref. TASK 32-22-00-410-801). (3) Close the MLG doors (Ref. TASK 32-12-00-410-801). (4) Close all the access doors, and the access panels opened during the inspection procedure. (5) Remove the access platform(s).
EFF : ALL 05-51-18 SROS
Page 639 Jul 01/05
(6) Remove the warning notice(s).
EFF : ALL 05-51-18 SROS
Page 640 Jul 01/02
INSPECTION AFTER ENGINE BIRD STRIKE OR SLUSH INGESTION - INSPECTION/CHECK _________________________________________________________________________ TASK 05-51-19-200-801 Inspection after Engine Bird Strike or Slush Ingestion 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. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------71-00-00-200-803 72-00-00-200-811
Inspection after a Birdstrike and Foreign Object Damage Inspection Procedure After Birdstrike (Foreign Object Damage)
3. __________ Job Set-up Subtask 05-51-19-941-050 A. Not Applicable.
EFF : ALL 05-51-19 SROS
Page 601 Jan 01/07
4. Procedure _________ **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-19-210-050 A. Inspection of the engine (Ref. TASK 72-00-00-200-811) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Do the inspection after Birdstrike: | X | | | | | | | | (Ref. TASK 72-00-00-200-81100) | | | | | | ------------------------------------------------------------------------------**ON A/C 701-749, Subtask 05-51-19-210-050-A A. Inspection of the engine (Ref. TASK 71-00-00-200-803) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Do the inspection after a Birdstrike: | X | | | | | | | | (Ref. TASK 71-00-00-200-80300) | | | | | | -------------------------------------------------------------------------------
R EFF : ALL 05-51-19 SROS
Page 602 Jan 01/07
INSPECTION AFTER TAIL RUNWAY IMPACT - INSPECTION/CHECK ______________________________________________________ TASK 05-51-21-200-801 Inspection after a Tail Runway Impact 1. __________________ Reason for the Job This inspection is applicable when the tail hits the runway during the take-off or the landing. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
adjustable access platform 7 m (22 ft. 12 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R
32-11-00-220-802 49-12-00-200-801 49-16-00-200-801 05-51-21-991-001
Check of Shock Absorber Nitrogen Charge Pressure Visual Check of APU Suspension System Including Shockmount Structure And Brackets Inspection of the Air Intake System Fig. 601
3. __________ Job Set-up Subtask 05-51-21-010-050 A. Get Access (1) Put an adjustable access platform in position at the tail cone. (2) Open the access panels 312AR, 313AL, 316AR and 315AL.
EFF : ALL 05-51-21 SROS
Page 601 Jan 01/07
4. Procedure _________ (Ref. Fig. 601/TASK 05-51-21-991-001) Subtask 05-51-21-210-050 A. Inspection of the Tail Cone (Ref. TASK 49-16-00-200-801), (Ref. TASK 4912-00-200-801)
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the Fuselage | | | | | | | | | | | | | | | | A.| |Externally examine the skin panels | X | | | | | | | |(FR75 thru FR78) for damaged paintwork | | | | | | | | |and any other type of damage. | | | | | | | | |If you find damage: | | | | | | | | |- internally examine the frames, the | | X | | | | | | | skin panels, the clips and the | | | | | | | | | stringers for damaged paintwork, | | | | | | | | | distortion, cracks, scratches, dents,| | | | | | | | | pulled or torn fasteners (Extend | | | | | | | | | inspection area as necessary). | | | | | | | | | | | | | | | |2. | |Inspection of the APU Air Intake and | | | | | | | | |the APU compartment | | | | | | | | | | | | | | | | A.| |Examine the APU diverter, intake flap, | X | | | | | | | |intake nose and drain mast for: | | | | | | | | |- damaged paintwork, distortion, | | | | | | | | | cracks, scratches, dents, pulled or | | | | | | | | | torn fasteners. | | | | | | | | |If you find damage: | | | | | | | | |- do the inspection of the Air Intake | | X | | | | | | | system: | | | | | | | | | (Ref. TASK 49-16-00-200-801) | | | | | | | | | | | | | | | | B.| |Examine the APU compartment for leakage| | | | | | | | |and damage: | | | | | | | | |if you find damage: | | | | | | | | |(1) make sure that the APU is correctly| | | | | | | | |installed. | | | | | | | | |(2) examine the mountings for damage, | | | | | | | | |distortion and signs of movement | | | | | | | | |(Ref. TASK 49-12-00-200-804). | | | | | |
EFF : ALL 05-51-21 SROS
Page 602 Oct 01/04
Location of APU Components to be Inspected Figure 601/TASK 05-51-21-991-001 EFF : ALL 05-51-21 SROS
Page 603 Apr 01/98
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| ------------------------------------------------------------------------------Subtask 05-51-21-210-051 B. Inspection of the Main Landing Gear (MLG) (Ref. TASK 32-11-00-220-802)
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the Shock Absorber | | | | | | | | |Pressure | | | | | | | | | | | | | | | | A.| |Do a check of the MLG shock-absorber | X | | | | | | | |pressure | | | | | | | | |(Ref. TASK 32-11-00-220-80200). | | | | | | | | | | | | | | | ------------------------------------------------------------------------------5. Close-up ________ Subtask 05-51-21-410-050 A. Close Access (1) Close the access panels 312AR, 313AL, 316AR and 315AL. Subtask 05-51-21-942-050 B. Put the Aircraft back to its Initial Configuration (1) Remove the access platform(s). (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-51-21 SROS
Page 604 Jan 01/07
INSPECTION AFTER NLG TOWING OVERLOAD OR OVERRUN - INSPECTION/CHECK __________________________________________________________________ TASK 05-51-22-200-801 Inspection after NLG Towing Overload or Overrun 1. __________________ Reason for the Job This procedure is necessary when unwanted movements have occurred after the shear pin of the tow bar has broken during towing. Do an inspection of the nose gear only: - if, after the shear pin has broken . the aircraft moves farther than the tow bar - or if, after a turn (aircraft pushed), the bar touches the tow vehicle. Do not do this inspection if you stopped towing when the shear pin broke. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No
specific specific specific specific
safety barriers warning notice wheel chocks adjustable access platform 2.5 m (8 ft. 2 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------05-56-00-200-801 24-41-00-861-801 24-41-00-862-801 24-42-00-861-801 24-42-00-862-801 29-00-00-863-801 29-00-00-864-801
Measurement of the Aircraft by Photogrammetry after Abnormal Operation of the Aircraft Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Energize the Ground Service Network De-energize the Ground Service Network Pressurize the Green Hydraulic System with the Ground Hydraulic Supply Depressurize the Green Hydraulic System (Pressurized with the Hydraulic Ground Supply)
EFF : ALL 05-51-22 SROS
Page 601 Apr 01/98
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-00-00-081-801 32-00-00-481-801
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32-22-00-010-801 32-22-00-410-801 32-30-00-867-801 32-30-00-867-802 32-31-00-720-802 32-31-22-000-801 05-51-22-991-001
Removal of the Safety Devices from the Landing Gears Installation of the Safety Devices on the Landing Gears Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance Retraction of the Landing Gear for Maintenance Extension of the Landing Gear After Maintenance Functional Check to Ensure that the Safety Valve Closes at 280 KTS Removal of the NLG Actuator (5201GA) Fig. 601
3. __________ Job Set-up Subtask 05-51-22-941-050 A. Safety Precautions (1) Put the safety barriers in position. (2) Put a warning notice in position in the cockpit, on the panel 312VU, to tell persons not to operate the nose landing gear and the NLG doors. (3) Put wheel chocks in position at the main landing gear. (4) Install the safety devices on the landing gear (Ref. TASK 32-00-00481-801). Subtask 05-51-22-860-052 B. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801) (2) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801) (3) Pressurize the Green hydraulic system (Ref. TASK 29-00-00-863-801)
EFF : ALL 05-51-22 SROS
Page 602 Jan 01/07
Subtask 05-51-22-010-050 C. Get Access (1) Open the NLG door (Ref. TASK 32-22-00-010-801). (2) Open the access door 811. (3) Put an adjustable access platform in position near the aircraft. Subtask 05-51-22-860-050 D. Aircraft Maintenance Configuration (1) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (2) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). 4. Procedure _________ (Ref. Fig. 601/TASK 05-51-22-991-001) Subtask 05-51-22-210-050 A. Inspection of the NLG well (Ref. TASK 05-56-00-200-801) (Ref. TASK 32-31-22-000-801) (Ref. Fig. 601/TASK 05-51-22-991-001) NOTE : All the necessary inspections are visual unless specified ____ differently on the test procedure. Operators can refer to the Non Destructive Testing Manual (NTM) and use non destructive procedure. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the NLG Well | | | | | | | | | (Ref. Fig. 601/TASK 05-51-22-991-001) | | | | | | | A.| | Examine the attachment fittings of the| | | | | | | | | drag stay assembly and the bearings | X | | | | | | | | for: | | | | | | | | | - distortion, cracks and damaged | | | | | | | | | paintwork | | | | | | | | | | | | | | |
EFF : ALL 05-51-22 R SROS
Page 603 Jan 01/02
Structure of the NLG Well Figure 601/TASK 05-51-22-991-001 EFF : ALL 05-51-22 SROS
Page 604 Apr 01/98
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | B.| | Examine the attachment fitting of the | | | | | | | | | lockstay assembly for: | X | | | | | | | | - distortion, damaged paintwork and | | | | | | | | | cracks. | | | | | | | | | | | | | | | | C.| | Examine the attach fitting of the NLG | X | | | | | | | | actuator for: | | | | | | | | | - cracks, distortion and damaged | | | | | | | | | paintwork. | | | | | | | | | | | | | | | | D.| | Examine the attach fittings of the | X | | | | | | | | NLG leg for crack, distortion and | | | | | | | | | - cracks, distortion and damaged | | | | | | | | | paintwork. | | | | | | | | | | | | | | | | E.| | Get access to the avionic compartment.| | | | | | | | | Examine the structure, the machined | X | | | | | | | | panels, the attach fittings, the | | | | | | | | | support strut for: | | | | | | | | | - cracks, distortion, damaged | | | | | | | | | paintwork, pulled or torn fasteners.| | | | | | | | | If you find damage: | | | | | | | | | (1) Do a check of the angles between | | X | | | | | | | the NLG and the aircraft | | | | | | | | | (Ref. TASK 05-56-00-200-801) | | | | | | | | | (2) Remove the NLG actuator for | | | | | | | | | inspection | | X | | | | | | | (Ref. TASK 32-31-22-000-801) | | | | | | ------------------------------------------------------------------------------Subtask 05-51-22-210-051 B. Inspection of the Nose Landing Gear NOTE : All the necessary inspections are visual unless specified ____ differently in the test procedure. Operators can refer to the Non Destructive Testing Manual (NTM) and use non destructive testing procedure.
EFF : ALL 05-51-22 SROS
Page 605 Jan 01/07
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection the nose landing gear. | | | | | | | | | | | | | | | | A.| | Examine the shock absorber, the | | | | | | | | | wheels, the tires, the towing lug for:| X | | | | | | | | - distortion, cracks, damage, torn or | | | | | | | | | pulled fasteners, and damaged | | | | | | | | | paintwork. | | | | | | ------------------------------------------------------------------------------| Subtask 05-51-22-860-053 C. 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) Subtask 05-51-22-410-050 D. Close Access (1) Close the NLG doors (Ref. TASK 32-22-00-410-801). (2) Close the access door 811. (3) Close all the access doors that you opened during the inspection. (4) Remove the access platform(s). (5) Remove the safety devices installed on the landing gear (Ref. TASK 32-00-00-081-801).
EFF : ALL 05-51-22 R SROS
Page 606 Jan 01/02
Subtask 05-51-22-710-050 E. Do the subsequent test. R R
NOTE : The test below is necessary only if you find damage on the ____ structure adjacent to the landing gear or on the attachments. (1) Extend and retract the landing gear 5 times. Make sure the nose landing gear moves freely. (Ref. TASK 32-30-00-867-801) (Ref. TASK 32-31-00-720-802) (Ref. TASK 32-30-00-867-802)
R Subtask 05-51-22-860-051 F. Put the system back to its operational configuration. (1) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). (2) De-energize the ground service network (Ref. TASK 24-42-00-862-801)> (3) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). 5. Close-up ________ Subtask 05-51-22-942-050 A. Put the Aircraft back to its Initial Configuration (1) Remove the warning notice(s). (2) Remove the ground support and maintenance equipment, the special and standard tools and all other items. (3) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-51-22 SROS
Page 607 Oct 01/00
INSPECTION AFTER NLG STEERING ANGLE EXCEEDED - INSPECTION/CHECK _______________________________________________________________ TASK 05-51-23-200-801 Inspection of the Nose Landing Gear after a NLG Steering Angle of more than 95⁰ 1. __________________ Reason for the Job
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NOTE : If the 95⁰ NLG steering angle was exceeded by a large value (a ____ maximum of 180⁰ for example when tow vehicle control is not kept in icy conditions), it is possible that damage occurred not only to the NLG but also to its attachment structure. If this occurs, do the NLG well inspection after NLG Towing Overload or Overrun (Ref. TASK 05-51-22-200-801). 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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32-21-00-220-805
Inspection of the NLG After the NLG Steering Angle is Exceeded
3. __________ Job Set-up Subtask 05-51-23-941-050 A. Not applicable. 4. Procedure _________ Subtask 05-51-23-210-050-A A. Inspection (1) Do the Inspection of the NLG after a NLG steering angle is exceeded (Ref. TASK 32-21-00-220-805).
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EFF : ALL 05-51-23 SROS
Page 601 Jan 01/07
INSPECTION AFTER LEAVING RUNWAY OR TAXIWAY - INSPECTION/CHECK _____________________________________________________________ TASK 05-51-24-200-801 Inspection after Leaving a Runway or a Taxiway 1. __________________ Reason for the Job A number of factors can possibly change the loads on the landing gear and the structure. They are, for example: - the speed and the weight of the aircraft - the condition of the ground (soft or hard) - the depth the landing gear goes into the ground. R R R
NOTE : Recovery must obey the ARM requirement. If recovery is different to ____ the ARM requirement or if no recovery report is available, refer to Airbus for special instructions. You must think of all these factors when you do this inspection. You must always do this inspection fully before the next flight of the aircraft. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific FOR FIN 4030EM2 No specific
safety barriers warning notice wheel chocks adjustable access platform 8.3 m (27 ft. 3 in.)
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Page 601 Jul 01/05
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------05-56-00-200-801 24-41-00-861-801 24-41-00-862-801 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 27-80-00-866-801 27-80-00-866-802 28-10-00-910-802 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 32-00-00-081-801 32-00-00-481-801 32-11-11-000-801 32-11-13-000-801 32-11-15-000-801 32-12-00-010-801 32-12-00-410-801 32-21-11-000-801 32-21-13-000-801 32-21-16-000-801 32-21-17-000-801 32-22-00-010-801
Measurement of the Aircraft by Photogrammetry after Abnormal Operation of the Aircraft Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power 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 Spoilers for Maintenance Retraction of the Spoilers after Maintenance Extension of the Slats on the Ground Retraction of the Slats on the Ground Access to Fuel Tanks and Work Areas 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) Removal of the Safety Devices from the Landing Gears Installation of the Safety Devices on the Landing Gears Removal of the MLG Leg Assembly Removal of the MLG Shock Absorber Removal of the MLG Bogie-Alignment Pitch Trimmer (Weight on Wheels) Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Removal of the NLG Leg Assy (5002GN) Removal of the NLG Shock Absorber Assembly Removal of the Upper Drag Stay Assembly Removal of the Lock Stay Assembly Open the NLG Doors for Maintenance
EFF : ALL 05-51-24 R SROS
Page 602 Jul 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-22-00-410-801 32-31-22-000-801 32-31-46-000-801 32-41-11-000-801 32-41-12-000-801 71-00-00-000-803 71-00-00-000-805 71-00-00-400-803 71-00-00-400-805 71-13-00-010-802 71-13-00-010-805 71-13-00-410-802 71-13-00-410-805 78-31-00-710-804 78-31-00-740-802 05-51-24-991-001 05-51-24-991-002 FOR FIN 4030EM2 53-35-13-000-801 53-35-13-000-802 78-30-00-010-801 78-30-00-010-803 78-30-00-410-801 78-30-00-410-803
Close the NLG Doors after Maintenance Removal of the NLG Actuator (5201GA) Removal of the MLG Actuator 5222GA(5223GA) Removal of the MLG Wheel Removal of the NLG Wheel Removal of the Engine Removal of the Demountable Power Plant Installation of the Engine Installation of the Demountable Power Plant Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Open the Fan Cowl Doors Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Close the Fan Cowl Doors Thrust Reverser Cycling Test (MCDU) Test of the Thrust Reverser Deployment and Stowage (Engine not Running) Fig. 601 Fig. 602 Removal of the Access Panels 191AB, 191BB, 192BB, 191DB, 197AB, 197AT, 198AT, 197BB, 198BB, 197EB, 198EB, 197FB, 197GB, 198GB, 198HB and 197HB. Removal of the Belly Fairing Access Panels Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Open the Thrust Reverser Cowl Doors Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Close the Thrust Reverser Cowl Doors
3. __________ Job Set-up Subtask 05-51-24-941-050 A. Safety Precautions (1) Put a warning notice in position in the cockpit to tell persons not to operate the systems. (2) Put wheel chocks in position at the main landing gear.
EFF : ALL 05-51-24 R SROS
Page 603 Jan 01/06
(3) Install the safety devices on the landing gear (Ref. TASK 32-00-00481-801). (4) Put the safety barriers in position. Subtask 05-51-24-860-052 B. Aircraft Maintenance Configuration R
(1) Energize the ground service network (Ref. TASK 24-42-00-861-801).
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(2) Pressurize the Green hydraulic system (Ref. TASK 29-00-00-863-801).
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(3) Pressurize the Yellow hydraulic system (Ref. TASK 29-00-00-863-803).
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(4) Pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-802). **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-24-010-050 C. Get Access (1) Open the NLG doors (Ref. TASK 32-22-00-010-801). (2) Open the MLG doors (Ref. TASK 32-12-00-010-801). (3) Open the access door 811. (4) Open the fan cowl doors (Ref. TASK 71-13-00-010-802) FOR 4030EM1 415BL, 416BR FOR 4030EM2 425BL, 426BR (5) Open the thrust reverser door (Ref. TASK 78-30-00-010-801) FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR
EFF : ALL 05-51-24 SROS
Page 604 Jan 01/06
(6) Open all the access doors and the access panels of the belly fairing (Ref. TASK 53-35-13-000-801) (Ref. TASK 53-35-13-000-802). (7) Put an adjustable access platform in position near the area where you must do the inspection. **ON A/C 701-749, Subtask 05-51-24-010-050-A C. Get Access (1) Open the NLG doors (Ref. TASK 32-22-00-010-801). (2) Open the MLG doors (Ref. TASK 32-12-00-010-801). (3) Open the access door 811. (4) Open the fan cowl doors (Ref. TASK 71-13-00-010-805) FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR (5) Open the thrust reverser door (Ref. TASK 78-30-00-010-803) FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR (6) Open all the access doors and the access panels of the belly fairing (Ref. TASK 53-35-13-000-801) (Ref. TASK 53-35-13-000-802). (7) Put an adjustable access platform in position near the area where you must do the inspection. **ON A/C ALL Subtask 05-51-24-860-050 D. Aircraft Maintenance Configuration (1) Extend the flaps to full position (Ref. TASK 27-50-00-866-801). (2) Extend the slats to full position (Ref. TASK 27-80-00-866-801).
EFF : ALL 05-51-24 R SROS
Page 605 Jan 01/06
(3) Extend the spoilers (Ref. TASK 27-60-00-866-801). (4) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (5) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803). (6) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802). (7) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). 4. Procedure _________ Subtask 05-51-24-210-050 A. Inspection of the Fuselage NOTE : All the inspections are visual unless specified differently in the ____ procedure. The inspection areas must be clean. Operators can refer to the Non-Destructive Testing Manual (NTM) and use non destructive procedures.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the bottom surface of | | | | | | | | | the fuselage. This includes the | | | | | | | | | cargo doors. | | | | | | | | | | | | | | | | A.| | Externally examine all the bottom | | | | | | | | | surface of the fuselage, the area | X | | | | | | | | around the door at FR17 below the | | | | | | | | | cabin floor, the skin panels | | | | | | | | | between FR17 and FR19 (bottom part | | | | | | | | | of the fuselage) | | | | | | | | | and between FR10 and FR13 and | | | | | | | | | stringers 37LH and 37RH and the NLG | | | | | | | | | doors and fairings for: | | | | | | | | | - dents, distortion, cracks, pulled or| | | | | | | | | torn fasteners and damaged | | | | | | | | | paintwork. | | | | | | | | | Internally examine all the parts that | | | | | |
EFF : ALL 05-51-24 SROS
Page 606 Jan 01/06
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | you can see of the area at FR17, | | | | | | | | | without removal of parts for | | | | | | | | | - dents, distortion, cracks, pulled or| | | | | | | | | torn fasteners and damaged | | | | | | | | | paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Get access and internally | | | | | | | | | examine: | | | | | | | | | - all the frames, stringers, | | | | | | | | | clips, fittings and component | | | | | | | | | mounts at and near the location | | X | | | | | | | of the damage for: | | | | | | | | | . distortion, cracks, dents, | | | | | | | | | pulled or torn fasteners and | | | | | | | | | damaged paintwork. | | | | | | | | | - all the components, pipes, | | | | | | | | | ducts, electrical harnesses, | | | | | | | | | cables, pulleys and mechanical | | X | | | | | | | linkages for: | | | | | | | | | . distortion, cracks, dents, | | | | | | | | | rupture, breaks and fluid | | | | | | | | | leakage. | | | | | | | | | | | | | | | | B.| | Examine the APU air intake for: | X | | | | | | | | - blockage and damage. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-24-210-051 B. Inspection of the Belly Fairing and the MLG Doors (Ref. Fig. 601/TASK 05-51-24-991-001) NOTE : All the inspections are visual unless specified differently in the ____ procedure. The inspection areas must be clean. Operators can refer to the Non-Destructive Testing manual (NTM) and use non destructive procedures.
EFF : ALL 05-51-24 SROS
Page 607 Jan 01/06
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Structure of the Belly Fairing Figure 601/TASK 05-51-24-991-001
EFF : ALL 05-51-24 SROS
Page 608 Jul 01/04
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Belly Fairing | | | | | | | | | | | | | | | | A.| | Examine externally and internally all | | | | | | | | | the panels, the leading edge fairing, | X | | | | | | | | the upper and lower fairings for: | | | | | | | | | - distortion, cracks, dents, pulled or| | | | | | | | | torn fasteners, damaged paintwork, | | | | | | | | | honeycomb and core damage and | | | | | | | | | delamination. | | | | | | | | | | | | | | | | B.| | Examine all the components, pipes, | | | | | | | | | ducts, electrical harnesses, mounts | X | | | | | | | | and supports for: | | | | | | | | | - distortion, cracks, breaks, and | | | | | | | | | fluid leakage. | | | | | | | | | | | | | | | | C.| | Make sure that the components are | X | | | | | | | | correctly installed. | | | | | | | | | | | | | | | | D.| | Examine externally the air| | | | | | | | | conditioning pack inlets for: | X | | | | | | | | - damage and blockage. | | | | | | | | | | | | | | | |2. | | Inspection of the Main Landing Gear | | | | | | | | | Doors | | | | | | | | | | | | | | | | A.| | Examine the honeycomb structure for: | X | | | | | | | | - delamination, core damage and | | | | | | | | | cracks. | | | | | | | | | | | | | | | | B.| | Examine the door hinge actuator | | | | | | | | | attachments, the proximity sensor | X | | | | | | | | attachments, the uplock roller | | | | | | | | | attachment for: | | | | | | | | | - distortion damage and separation. | | | | | | | | | | | | | | | | C.| | Examine the door actuator and its | | | | | | | | | hydraulic hoses, pipes for: | X | | | | | | | | - fluid leakage, distortion and | | | | | | | | | damage. | | | | | | -------------------------------------------------------------------------------
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Page 609 Jan 01/06
Subtask 05-51-24-210-052 C. Inspection of the Nose Landing Gear and the NLG Well (Ref. TASK 32-21-16-000-801) (Ref. TASK 05-56-00-200-801) (Ref. TASK 3221-17-000-801) (Ref. TASK 32-21-11-000-801) (Ref. TASK 32-31-22-000-801) (Ref. TASK 32-41-12-000-801) (Ref. TASK 32-21-13-000-801) (Ref. Fig. 602/TASK 05-51-24-991-002) NOTE : If the landing gear goes into soft ground, there is a risk of ____ damage to the primary structure of the landing gear. Airbus recommends that you replace the landing gear. NOTE : All the inspections are visual unless specified differently in the ____ procedure. The inspection areas must be clean. Operators can refer to the Non-Destructive Testing Manual (NTM) and use non destructive procedures. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Nose Landing Gear | | | | | | | | | | | | | | | | A.| | Examine externally the nose landing | | | | | | | | | gear and the components which are on | | | | | | | | | it, the attachment fittings and the | X | | | | | | | | bearing of the drag strut assembly | | | | | | | | | for: | | | | | | | | | - cracks, dents, scores, tears, | | | | | | | | | rupture, distortion, fluid leakage | | | | | | | | | and damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Do a measurement of the nose | | X | | | | | | | landing gear. | | | | | | | | | (Ref. TASK 05-56-00-200-801) | | | | | | | | | (2) Remove the drag strut assembly | | X | | | | | | | for inspection. | | | | | | | | | (Ref. TASK 32-21-16-000-801) | | | | | | | | | | | | | | | | B.| | Examine externally the NLG shock | | | | | | | | | absorber, the chrome-plated area for: | X | | | | | | | | - blue stains or bronze marks and | | | | | | | | | damage. | | | | | | | | | If you find damage: | | | | | |
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Page 610 Jan 01/06
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Location of the NLG Well Figure 602/TASK 05-51-24-991-002
EFF : ALL 05-51-24 SROS
Page 611 Jul 01/04
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (1) Remove the shock absorber for | | X | | | | | | | overhaul. | | | | | | | | | (Ref. TASK 32-21-13-000-801) | | | | | | | | | | | | | | | | C.| | Examine the NLG wheels for: | | | | | | | | | - distortion, damage, valve damage, | | | | | | | | | cracks, impacts, rim damage, and | | | | | | | | | examine the tires for: | X | | | | | | | | . tread separation, cuts, ply | | | | | | | | | delamination and bulges. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the NLG wheel for overhaul | | X | | | | | | | | | | | | | |2. | | Inspection of the NLG Well | | | | | | | | | (Ref. Fig. 602/TASK 05-51-24-991-002) | | | | | | | | | | | | | | | | A.| | Examine externally the attachment | | | | | | | | | fittings of the lockstay assembly | X | | | | | | | | for: | | | | | | | | | - distortion, cracks and damaged | | | | | | | | | paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the lockstay assembly | | X | | | | | | | for inspection. | | | | | | | | | (Ref. TASK 32-21-17-000-801). | | | | | | | | | | | | | | | | B.| | Examine the attachment fittings, the | | | | | | | | | components, the internal structure, | X | | | | | | | | the manifolds, the pipes, the | | | | | | | | | electrical harnesses, the mounts for: | | | | | | | | | - distortion, rupture, impacts, fluid | | | | | | | | | leakage and pulled or torn | | | | | | | | | fasteners. | | | | | | | | | | | | | | | | C.| | Examine the attachment of the NLG | | | | | | | | | actuating cylinder for: | | | | | | | | | - distortion, cracks, dents, pulled or| X | | | | | | | | torn fasteners and damaged | | | | | | | | | paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the actuating cylinder for | | X | | | | | | | inspection. | | | | | | | | | (Ref. TASK 32-31-22-000-801) | | | | | |
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Page 612 Jul 01/04
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | | | | | | | | D.| | Get access to the avionics compartment| | | | | | | | | and examine the NLG well roof and the | X | | | | | | | | lateral struts for: | | | | | | | | | - distortion, cracks, pulled or torn | | | | | | | | | fasteners and damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the nose landing gear for | | | | | | | | | strip-down inspection. | | X | | | | | | | (Ref. TASK 32-21-11-000-801) | | | | | | | | | (2) Examine the NLG attach fittings | | X | | | | | | | for: | | | | | | | | | - distortion , cracks pulled or | | | | | | | | | torn fasteners and damaged | | | | | | | | | paintwork. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-24-210-053 D. Inspection of the main landing gear and the MLG well (Ref. TASK 32-11-11-000-801) (Ref. TASK 32-31-46-000-801) (Ref. TASK 3241-11-000-801) (Ref. TASK 32-11-15-000-801) (Ref. TASK 32-11-13-000-801)
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NOTE : If the landing gear goes into soft ground, there is a risk of ____ damage to the primary structure of the landing gear. Airbus recommends that you replace the landing gear.
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NOTE : All the inspections are visual unless specified differently in the ____ procedure. The inspection areas must be clean. Operators can refer to the Non-Destructive Testing Manual (NTM) and use non destructive procedures.
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Page 613 Jul 01/04
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Main Landing Gear | | | | | | | | | | | | | | | | A.| | Examine the MLG leg in the rear | | | | | | | | | pintle area for: | X | | | | | | | | - shock damage. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the MLG for inspection | | X | | | | | | | (Ref. TASK 32-11-11-000-801) | | | | | | | | | - Contact Airbus for aircraft | | | | | | | | | structural inspection requirements. | | | | | | | | | | | | | | | | B.| | Examine the MLG shock absorber for: | | | | | | | | | - cracks, scores, rupture and leaks | | | | | | | | | distortion damage. | X | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the shock absorber and | | | | | | | | | examine the components | | X | | | | | | | (Ref. TASK 32-11-13-000-801) | | | | | | | C.| | Examine the MLG retraction actuator | X | | | | | | | | and the components attached to it for:| | | | | | | | | - distortion, cracks, damage. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove and examine the actuator | | X | | | | | | | (Ref. TASK 32-31-46-000-801). | | | | | | | | | | | | | | | | D.| | Examine the bogie alignment pitch| | | | | | | | | trimmer for: | | | | | | | | | - damage, leaks, rupture, cracks, | X | | | | | | | | distortion. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the bogie alignment | | X | | | | | | | pitch-trimmer for overhaul | | | | | | | | | (Ref. TASK 32-11-15-000-801). | | | | | | | | | | | | | | | | E.| | Examine the side stay and attachment | | | | | | | | | for: | X | | | | | | | | - cracks, damage and distortion. | | | | | | | | | | | | | | | | F.| | Examine the brake rods for: | X | | | | | | | | - damage, leaks, rupture, cracks, | | | | | | | | | distortion. | | | | | | | | | | | | | | | | G.| | Examine the MLG wheels for: | | | | | |
EFF : ALL 05-51-24 SROS
Page 614 Jul 01/04
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - distortion, damage, impacts, cracks,| X | | | | | | | | valve damage, rim damage and examine| | | | | | | | | the tires for bulges, tread | | | | | | | | | separation, cuts, ply delamination. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the wheels for overhaul | | | | | | | | | (Ref. TASK 32-41-11-000-801). | | | | | | | | | | | | | | | |2. | | Inspection of the MLG well | | | | | | | | | | | | | | | | A.| | Examine the protective panels, the | X | | | | | | | | internal structure for: | | | | | | | | | - distortion, cracks, dents, rupture, | | | | | | | | | breaks, honeycomb delamination and | | | | | | | | | core damage. | | | | | | | | | Make sure that the fasteners are not| | | | | | | | | pulled or torn and that the | | | | | | | | | paintwork is not damaged. | | | | | | | | | | | | | | | | B.| | Examine the pipes, ducts, electrical | | | | | | | | | looms and their supports for: | X | | | | | | | | - fluid leakage, distortion, rupture, | | | | | | | | | cracks, correct attachment and the | | | | | | | | | condition of the safety devices. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-24-210-055 E. Inspection of the Wing (Ref. TASK 28-10-00-910-802)
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NOTE : All the inspections are visual unless specified differently in the ____ procedure. The inspection areas must be clean. Operators can refer to the Non-Destructive Testing Manual (NTM) and use non destructive procedures.
EFF : ALL 05-51-24 SROS
Page 615 Jul 01/04
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Wing | | | | | | | | | | | | | | | | A.| | Examine externally the skin panels, | X | | | | | | | | the external structure of the wing | | | | | | | | | for: | | | | | | | | | - cracks, dents, distortion, impacts, | | | | | | | | | damaged paintwork, fluid leakage. | | | | | | | | | If you find damage: | | | | | | | | | (1) Get access to the fuel tanks. | | X | | | | | | | (Ref. TASK 28-10-00-910-802) | | | | | | | | | (2) Examine the front spar and the | | | | | | | | | rear spar, the stringers, the | | X | | | | | | | ribs, the internal structure of | | | | | | | | | the wing and the fasteners for: | | | | | | | | | - cracks, dents, distortion, | | | | | | | | | damaged, torn or pulled | | | | | | | | | fasteners. | | | | | | | | | (3) Make sure that the sealant beads | | | | | | | | | are in the correct condition. | | | | | | | | | (4) Examine the ducts, lines, pipes | | X | | | | | | | mechanical linkages and their | | | | | | | | | supports for: | | | | | | | | | - distortion, cracks, fluid, | | | | | | | | | leakage. | | | | | | | | | Make sure that the components are | | | | | | | | | not damaged and are correctly | | | | | | | | | attached. | | | | | | | | | | | | | | | | B.| | Examine the flap track attachments | | | | | | | | | and the adjacent structure for: | X | | | | | | | | - distortion, cracks, pulled fasteners| | | | | | | | | fluid leakage. | | | | | | | | | | | | | | | | C.| | Examine the wing internal structure | | | | | | | | | adjacent to the front and aft | X | | | | | | | | mountings of the flap beams for: | | | | | | | | | - distortion, cracks and damage to the| | | | | | | | | sealants. | | | | | | | | | | | | | | | | D.| | Examine the area where the MLG is | | | | | | | | | attached and the adjacent structure | X | | | | | | | | for: | | | | | | | | | - cracks or fuel leakage and | | | | | |
EFF : ALL 05-51-24 SROS
Page 616 Jul 01/04
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | distortion. | | | | | | | | | | | | | | | | E.| | Examine the internal structure of the | | | | | | | | | aft spar where the MLG and MLG | X | | | | | | | | sidestay are attached for: | | | | | | | | | - distortion, damage, pulled fasteners| | | | | | | | | and damage to the sealant bead. | | | | | | ------------------------------------------------------------------------------**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-24-210-056 F. Inspection of the Nacelles and the Engines (Ref. TASK 71-00-00-000-803) (Ref. TASK 71-00-00-400-803) (Ref. TASK 7831-00-710-804) NOTE : All the inspections are visual unless specified differently in the ____ procedure. The inspections areas must be clean. Operators can refer to the Non-Destructive Testing Manual (NTM) and use non destructive procedures. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Nacelles and the | | | | | | | | | Engines | | | | | | | | | | | | | | | | A.| | Examine the nacelles: | X | | | | | | | | - the fan cowl doors | | | | | | | | | - the thrust reverser doors | | | | | | | | | - the primary nozzle | | | | | | | | | - the attachments of the nose cowl to | | | | | | | | | the fan case | | | | | | | | | - all the cowl attachment points on | | | | | | | | | the pylon | | | | | | | | | - all the cowl hinge fittings | | | | | | | | | - the components | | | | | | | | | - the supports and brackets | | | | | | | | | - the ducts and pipes | | | | | |
EFF : ALL 05-51-24 SROS
Page 617 Jan 01/07
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - the cowl latches for: | | | | | | | | | . distortion, cracks, dents, pulled | | | | | | | | | or torn fasteners, correct | | | | | | | | | attachment, fluid leakage, damage,| | | | | | | | | loose rivets, signs of shearing | | | | | | | | | and damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Do an operational test of the | | X | | | | | | | thrust reverser system to make | | | | | | | | | sure that it operates freely | | | | | | | | | (Ref. TASK 73-31-00-710-804). | | X | | | | | | | | | | | | | | B.| | Examine the engines for foreign object| X | | | | | | | | damage: | | | | | | | | | (Ref. TASK 72-00-00-200-811) | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the engine | | | X | | | | | | (Ref. TASK 71-00-00-000-803). | | | | | | | | | (2) Examine the engine-to-pylon attach| | | X | | | | | | fittings for damage. | | | | | | ------------------------------------------------------------------------------**ON A/C 701-749, Subtask 05-51-24-210-056-A F. Inspection of the Nacelles and the Engines (Ref. TASK 71-00-00-000-805) (Ref. TASK 71-00-00-400-805) (Ref. TASK 7831-00-740-802) NOTE : All the inspections are visual unless specified differently in the ____ procedure. The inspection areas must be clean. Operators can refer to the Non-Destructive Testing Manual (NTM) and use non destructive procedures.
R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-24 301-399, 401-449, 451-499, 701-749, SROS
Page 618 Jul 01/05
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Nacelles and the | | | | | | | | | Engines | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | |
A.| | | | | | | | | | | | | | | | | | | | | | |
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Examine the nacelles: | - the fan cowl doors | - the thrust reverser doors | - the primary nozzle | - the attachments of the nose cowl to | the fan case | - all the cowl attachment points on | the pylon | - all the cowl hinge fittings | - the components | - the supports and brackets | - the ducts and pipes | - the cowl latches for: | . distortion, cracks, dents, pulled | or torn fasteners, correct | attachment, fluid leakage, damage,| loose rivets, signs of shearing | and damaged paintwork. | If you find damage: | (1) Do an operational test of the | thrust reverser system to make | sure that it operates freely | (Ref. TASK 78-31-00-740-802). |
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| Examine the engines for foreign object| damage: | (Ref. TASK 72-00-00-200-803) | If you find damage: | (1) Remove the engine | (REF. TASK 71-00-00-000-805). | (2) Examine the engine-to-pylon attach| fittings for damage. |
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EFF : 701-749, 05-51-24 SROS
Page 619 Jul 01/04
**ON A/C ALL Subtask 05-51-24-210-057 G. Inspection of the Pylon R R R R R
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NOTE : All the inspections are visual unless specified differently in the ____ procedure. The inspection areas must be clean. Operators can refer to the Non-Destructive Testing Manual (NTM) and use non destructive procedures. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Pylons | | | | | | | | | | | | | | | | A.| | Examine the pylons externally for: | | | | | | | | | - distortion, cracks, pulled or torn | X | | | | | | | | fasteners, and damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Examine the pylon internally for | | | | | | | | | distortion, cracks, pulled or torn| | X | | | | | | | fasteners, damaged paintwork. | | | | | | | | | (2) Examine the components, the pipes,| | | | | | | | | the ducts, the electrical | | | | | | | | | harnesses, the mounts for: | | X | | | | | | | - distortion, cracks, rupture and | | | | | | | | | fluid leakage. | | | | | | | | | (3) Examine the pylon-to-wing | | | | | | | | | attachment for distortion and | | X | | | | | | | cracks. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-24-860-051 H. 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).
EFF : ALL 05-51-24 SROS
Page 620 Jul 01/04
(3) Pressurize the Yellow hydraulic system (Ref. TASK 29-00-00-863-803). (4) Pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-802). (5) Retract the flaps (Ref. TASK 27-50-00-866-802). (6) Retract the slats (Ref. TASK 27-80-00-866-802). (7) Retract the spoilers (Ref. TASK 27-60-00-866-802). 5. Close-up ________ R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-24-410-050 A. Close Access (1) Close the NLG doors (Ref. TASK 32-22-00-410-801). (2) Close the MLG doors (Ref. TASK 32-12-00-410-801). (3) Close the access door 811. (4) Close the fan cowl doors (Ref. TASK 71-13-00-410-802).
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(a) FOR 4030EM1 415BL, 416BR
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(b) FOR 4030EM2 425BL, 426BR (5) Close the thrust reverser doors (Ref. TASK 78-30-00-410-801).
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(a) FOR 4030EM1 417AL, 418AR
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(b) FOR 4030EM2 427AL, 428AR (6) Close all the access doors and panels that you opened during the inspection.
EFF : ALL 05-51-24 SROS
Page 621 Jul 01/05
**ON A/C 701-749, Subtask 05-51-24-410-050-A A. Close Access (1) Close the NLG doors (Ref. TASK 32-22-00-410-801). (2) Close the MLG doors (Ref. TASK 32-12-00-410-801). (3) Close the access door 811. R
(4) Close the fan cowl doors (Ref. TASK 71-13-00-410-805). (a) FOR 4030EM1 415AL, 416AR (b) FOR 4030EM2 425AL, 426AR (5) Close the thrust reverser doors (Ref. TASK 78-30-00-410-803). (a) FOR 4030EM1 417AL, 418AR (b) FOR 4030EM2 427AL, 428AR (6) Close all the access doors and panels that you opened during the inspection. **ON A/C ALL Subtask 05-51-24-860-053 B. Put the system back to its operational configuration. (1) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801) (2) De-energize the ground service network (Ref. TASK 24-42-00-862-801) (3) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801)
EFF : ALL 05-51-24 SROS
Page 622 Jul 01/04
(4) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803) (5) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802) Subtask 05-51-24-942-050 C. Put the Aircraft back to its Initial Configuration (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. (4) Remove the safety devices that you installed on the landing gear (Ref. TASK 32-00-00-081-801). (5) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-51-24 SROS
Page 623 Oct 01/00
______________________________________________________________________________ INSPECTION AFTER FLIGHT THROUGH DUST STORM/VOLCANIC ASH OR SEVERE CONDITION ON GROUND - INSPECTION/CHECK _________________________ TASK 05-51-25-200-802 Inspection after Flight through Dust Storm or Dust contamination on Ground 1. __________________ Reason for the Job Do this inspection after flight in a severe dust storm or after dust contamination on ground. R R
NOTE : If the dust contamination occurred when the aircraft was on ground ____ with applicable protection by covers and blankets (ref. AMM 10-11-00), and if there is no dust behind the covers, the inspections specified in para. 4D.(Inspection of the probes and sensors) and in para.4F.(Inspection of the nacelles and engines) are not necessary. NOTE : This inspection specifies an adjustable access platform (2.5m to ____ 17m/8.2ft to 55.9ft) to get access to the different parts of the aircraft during the inspection. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 17M (56 FT) - ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-21-11-615-801 12-24-34-600-801 12-32-28-281-812 12-32-29-281-801 24-41-00-862-801 26-21-00-720-819
External Cleaning Draining of the Standby Static Pressure-Lines Sample Fuel for Microbiological Contamination Analysis Sampling for Analysis De-energize the Aircraft Electrical Circuits from the External Power A Functional Check of the Distribution Piping for Leakage and Obstruction
EFF : ALL 05-51-25 SROS
Page 601 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------26-22-00-200-801 27-50-00-866-801 27-50-00-866-802 27-60-00-866-801 27-60-00-866-802 27-80-00-866-801 28-12-00-210-802 29-00-00-864-801 29-00-00-864-802 29-00-00-864-803 R
29-10-00-200-803 30-11-00-710-801 30-11-51-000-802 30-11-51-400-802 32-00-00-481-801 32-12-00-010-801 32-12-00-410-801 32-16-00-010-801 32-22-00-010-801 32-22-00-410-801 34-11-00-170-801 34-11-00-170-802 34-11-00-170-803 35-12-41-100-802 49-16-00-100-801 49-16-00-200-801 49-20-00-290-809 49-20-00-290-810 49-91-44-000-801 49-91-44-400-801 53-15-11-200-801
Detailed Visual Inspection of the APU Fire-Extinguishing Distribution-Piping Extension of the Flaps on the Ground Retraction of the Flaps/Slats on the Ground Extension of the Spoilers for Maintenance Retraction of the Spoilers after Maintenance Extension of the Slats on the Ground Visual Check Of The Wing And Trim Vent Surge Tank Overpressure Protectors (5201QS1, 5201QS2, 5204QS) (Burst Discs) For Integrity 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) Check of the Clogging Indicators of High Pressure (HP), Return, Engine Driven Pump (EDP) Case drain, Reservoir Fill and Air Pressurization Unit Filters. Operational Test of the Wing Ice-Protection System Removal of the Wing Anti-ice Control Valve Filter Installation of the Wing Anti-ice Control Valve Filter Installation of the Safety Devices on the Landing Gears Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Open the CLG Doors for Maintenance Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance Flushing of the Principal Total Pressure Lines Flushing of the Principal Static Pressure Lines Draining and Flushing of the Standby Static and Standby Total Pressure Lines Cleaning of the mask full-face / Quick donning Cleaning of the Air Intake System Inspection of the Air Intake System Borescope Inspection of the Load Compressor - Access Through the LCIT-Sensor Bore Borescope Inspection of the APU Power Section Removal of the Oil Cooler (5100KT8) Installation of the Oil Cooler (5100KT8) Detailed Inspection of the Radome (110AL)
EFF : ALL 05-51-25 SROS
Page 602 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------56-11-11-200-801 56-11-12-200-801 56-12-11-200-801 56-21-15-200-801 71-00-00-200-802 71-00-00-200-813 71-13-00-200-803 71-13-00-220-801 R
71-61-00-220-801 71-61-41-200-802 78-30-00-210-802 78-32-00-200-802 AMM 122227 PB 301 AMM 122232 PB 301
Inspection of the Windshields (3DG1,3DG2). Inspection of the Fixed Windows (7DG1,7DG2) Inspection of the Sliding Windows (8DG1,8DG2). Detailed Visual Inspection of Passenger Cabin Window Panes including Passenger/ Crew Door and Emergency Exit Window Panes Inspection Procedures After the Ingestion of Volcanic Ash or Sand Examine the Power Plant after Contamination with Volcanic Ash Inspection of the Fan Cowl Doors Visual Inspection of Forward and Aft fan Cowls (5130EA) ,(5140EA), (5150EA), (5110EA) and (5120EA). Detailed Inspection of Intake Cowl Lip and Inner Skin Visual Check of the Airwashed Surfaces for Distortion and Security of Installation Visual Inspection of the Thrust Reverser (4120KS to 4130KS) (Thrust Reverser Closed) Inspection of the Thrust Reverser Structure (for corrective action) (for corrective action)
3. __________ Job Set-up Subtask 05-51-25-210-076 A. General (1) Inspection requirements (a) The dust particles can be of different sizes, they can enter all orifices and cause erosion, etching or shot peening on the surface. The dust can stay: - on all exposed lubricated surfaces - in all corners - in bottom places The dust can cause contamination on all filter elements. (b) All the necessary inspections are visual unless the text gives other instructions. Operators can refer to the Non-destructive Testing Manual (NTM) and use non-destructive procedures.
EFF : ALL 05-51-25 SROS
Page 603 Jan 01/07
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(c) If you find damage to the aircraft structure, refer to the Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures. (d) If you find damage to paint/protection, refer to the Structural Repair Manual (SRM). The SRM has the approved paint/protection repair procedures. (e) Examine the aircraft surfaces, structures, systems for contamination, erosion/abrasion, dents, etching, delamination or other damage. Subtask 05-51-25-210-078 B. Inspection Preparation
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(1) If contamination occurred in flight or during landing or take off: (a) Before you start, we recommend that you get information from the crew about the flight conditions. (b) Make sure that you have the related aircraft Post Flight Report (PFR). (c) Do a check of all the events reported by the crew or by the PFR in addition/conjunction with this inspection. (2) If contamination occurred with the aircraft in parking configuration, it is not necessary to do a check of the systems which are protected by the applicable protective covers/devices if you do not find dust behind them. Subtask 05-51-25-481-052 C. Safety Precautions (1) Make sure that the safety devices are installed on the landing gears (Ref. TASK 32-00-00-481-801). Subtask 05-51-25-866-056 D. Extension of the Flight Control Surfaces (1) Extend the flaps (Ref. TASK 27-50-00-866-801). (2) Extend the slats (Ref. TASK 27-80-00-866-801).
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(3) Extend the spoilers (Ref. TASK 27-60-00-866-801). Subtask 05-51-25-010-052 E. Get Access (1) Open the main gear doors and install the safety devices (Ref. TASK 32-12-00-010-801). (2) Open the nose gear doors and install the safety devices (Ref. TASK 32-22-00-010-801). (3) Open the center gear doors and install the safety devices (Ref. TASK 32-16-00-010-801). Subtask 05-51-25-860-052 F. Aircraft Maintenance Configuration (1) Make sure that the hydraulic systems are depressurized (2) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (3) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803). (4) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802). (5) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). (6) Put warning notices in the cockpit to tell persons not to operate the systems. (7) Put an ACCESS PLATFORM 17M (56 FT) - ADJUSTABLEin position near the area you must inspect.
EFF : ALL 05-51-25 R SROS
Page 605 Jan 01/07
4. Procedure _________ Subtask 05-51-25-160-052 A. Cleaning of the Aircraft CAUTION : DO NOT RUB THE SURFACE WHEN YOU REMOVE THE DUST FROM THE _______ AIRCRAFT. IF YOU RUB THE SURFACE, YOU CAN CAUSE EROSION/ ABRASION. CAUTION : DO NOT USE FLUIDS TO REMOVE THE DUST. IF THERE IS A LAYER OF _______ DUST ON THE AIRCRAFT SURFACES, REMOVE THE DUST WITH A VACUUM CLEANER (OR, IF YOU CANNOT USE A VACUUM CLEANER, USE AN AIR BLOWER, A SOFT CLOTH OR A HAND BRUSH). FLUIDS CAN MIX WITH THE DUST AND MAKE A PASTE THAT CAN CAUSE EROSION/ABRASION. THIS PASTE CAN GO INTO AREAS THAT ARE NOT EASY TO CLEAN. (1) If there is a layer of dust on the aircraft surfaces, remove the dust with a vacuum cleaner, an air blower, a soft cloth or a soft brush. (2) Clean the aircraft internally. (3) Clean the aircraft externally (Ref. TASK 12-21-11-615-801). Subtask 05-51-25-210-079 R
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B. Internal Inspection (Ref. TASK 35-12-41-100-802) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the cabin area | | | | | | | | | | | | | | | | A.| |Examine the cabin area for dust | X | | | | | | | |contamination. | | | | | | | | |If you find contamination: | | | | | | | | |(1) Clean all the contaminated surfaces| | X | | | | | | | | | | | | | | B.| |Examine the cockpit for dust | X | | | | | | | |contamination. | | | | | | | | |If you find contamination: | | | | | | | | |(1) Clean all the contaminated surfaces| | X | | | | | | |(2) Examine the oxygen full face masks | | X | | | | | | | for contamination. | | | | | | | | | If you find contamination: | | | | | | | | | (a) Clean the oxygen full face | | | X | | |
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Page 606 Jan 01/03
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | masks | | | | | | | | | (Ref. TASK 35-12-41-100-802). | | | | | | | C.| |Examine the avionics compartment (all | X | | | | | | | |the items you can see), specially: | | | | | | | | |- around the ventilated components | | | | | | | | |- the plugs | | | | | | | | |- the equipments | | | | | | | | |for dust contamination. | | | | | | | | |If you find contamination: | | | | | | | | |(1) Clean all the contaminated surfaces| | X | | | | | | | | | | | | | | D.| |Examine the cargo compartments for dust| X | | | | | | | |contamination. | | | | | | | | |If you find contamination: | | | | | | | | |(1) Clean all the contaminated surfaces| | X | | | | | | | (specially the PDU sensors). | | | | | | | | |(2) Examine the cargo drainage system | | X | | | | | | | (if installed) for dust | | | | | | | | | contamination. | | | | | | | | | If you find contamination: | | | | | | | | | (a) Replace the filters of the | | | X | | | | | | drain funnels. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-25-210-080 C. Inspection (Ref. TASK (Ref. TASK (Ref. TASK
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of the Fuselage, the Wings and the Stabilizers 53-15-11-200-801) (Ref. TASK 56-11-11-200-801) 56-11-12-200-801) (Ref. TASK 56-12-11-200-801) 56-21-15-200-801) (Ref. AMM 122227 PB 301)
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the fuselage | | | | | | | | | | | | | | | | A.| | Examine the radome skin for damage | X | | | | | | | | (Ref. TASK 53-15-11-200-801). | | | | | | | | | | | | | | | | B.| | Examine the windshield, the fixed | X | | | | | | | | windows and the sliding windows for | | | | | | | | | damage: | | | | | |
EFF : ALL 05-51-25 SROS
Page 607 Jan 01/03
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - for the windshield | | | | | | | | | (Ref. TASK 56-11-11-200-801) | | | | | | | | | - for the fixed windows | | | | | | | | | (Ref. TASK 56-11-12-200-801) | | | | | | | | | - for the sliding windows | | | | | | | | | (Ref. TASK 56-12-11-200-801). | | | | | | | | | | | | | | | | C.| | Examine the passenger cabin windows, | X | | | | | | | | the passenger/crew doors and the | | | | | | | | | emergency exit windows for damage | | | | | | | | | (Ref. TASK 56-21-15-200-801). | | | | | | | | | | | | | | | | D.| | Examine all of the fuselage skin, the | X | | | | | | | | belly fairing and the wing-to-fuselage| | | | | | | | | fairings for damage. | | | | | | | | | | | | | | | | E.| | Examine the ram air inlet and outlet, | X | | | | | | | | the air inlet and outlet flaps for | | | | | | | | | damage. | | | | | | | | | | | | | | | |2. | | Inspection of the Wings | | | | | | | | | | | | | | | | A.| | Examine all the static dischargers for| X | | | | | | | | damage. | | | | | | | | | | | | | | | | B.| | Examine the top and bottom skin of the| X | | | | | | | | wings for damage. | | | | | | | | | | | | | | | | C.| | Examine the flap track fairings for | X | | | | | | | | damage. | | | | | | | | | | | | | | | | D.| | Examine the skin of all the control | X | | | | | | | | surfaces ( slats, flaps, ailerons and | | | | | | | | | spoilers), specially the leading and | | | | | | | | | the trailing edges, for damage. | | | | | | | | | | | | |
| E.| | | | F.| |
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Examine the hinge areas of the spoilers and the ailerons for contamination. Examine the flap tracks, flap inter connecting strut, track 4 sensor,
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | roller mechanisms, steady bearings and| | | | | | | | | universal joints for contamination. | | | | | | | | | Make sure that there is no dust | | | | | | | | | deposit on the roller stops. | | | | | | | | | If you find contamination: | | | | | | | | | (1) Clean and lubricate the related | | X | | | | | | | components | | | | | | | | | (Ref. AMM 12-22-27 PB 301). | | | | | | | | | | | | | | | | G.| | Examine the piston rod of each | X | | | | | | | | servocontrol of the ailerons and the | | | | | | | | | spoilers for contamination. | | | | | | | | | If you find contamination: | | | | | | | | | (1) Clean the piston rod of the | | X | | | | | | | servocontrols. | | | | | | | | | | | | | | | |3. | | Inspection of the Vertical Stabilizer | | | | | | | | | | | | | | | | A.| | Examine all the static dischargers for| X | | | | | | | | damage. | | | | | | | | | | | | | | | | B.| | Examine the skin of the vertical | X | | | | | | | | stabilizer and the rudder, specially | | | | | | | | | the leading and the trailing edges, | | | | | | | | | for damage. | | | | | | | | | | | | | | | | C.| | Examine the hinge areas of the rudder | X | | | | | | | | for contamination. | | | | | | | | | | | | | | | | D.| | Examine the piston rod of each | X | | | | | | | | servocontrol of the rudder for | | | | | | | | | contamination. | | | | | | | | | If you find contamination: | | | | | | | | | (1) Clean the piston rod of the | | X | | | | | | | servocontrols. | | | | | | | | | | | | | | | |4. | | Inspection of the Horizontal | | | | | | | | | Stabilizers | | | | | | | | | | | | | | | | A.| | Examine all the static dischargers for| X | | | | | | | | damage. | | | | | | | | | | | | | | | | B.| | Examine the skin of the horizontal | X | | | | |
EFF : ALL 05-51-25 SROS
Page 609 Jan 01/03
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | stabilizers and the elevators, | | | | | | | | | specially the leading and the trailing| | | | | | | | | edges, for damage. | | | | | | | | | | | | | | | | C.| | Examine the hinge areas of the | X | | | | | | | | elevators for contamination. | | | | | | | | | | | | | | | | D.| | Examine the piston rod of each | X | | | | | | | | servocontrol of the elevators for | | | | | | | | | contamination. | | | | | | | | | If you find contamination: | | | | | | | | | (1) Clean the piston rod of the | | X | | | | | | | servocontrols. | | | | | | | | | | | | | | | |5. | | Inspection of the external lights | | | | | | | | | | | | | | | | A.| | Examine all the external lights for | X | | | | | | | | damage. | | | | | | | | | If you find damage: | | | | | | | | | (1) Replace the related component(s). | | X | | | | | | | | | | | | | |6. | | Inspection of the antennas and the | | | | | | | | | drain masts | | | | | | | | | | | | | | | | A.| | Examine all the antennas and the drain| X | | | | | | | | masts for damage. | | | | | | | | | If you find damage: | | | | | | | | | (1) Replace the related component(s). | | X | | | | ------------------------------------------------------------------------------Subtask 05-51-25-210-081 D. Inspection of the Probes and Sensors NOTE : If the aircraft was on the ground with the applicable protective ____ covers/devices installed (ref. AMM 10-11-00) when the dust contamination occurred, this inspection is not necessary if there is no dust behind the covers.
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NOTE : If the crew report shows an important dust storm. ____ If the maintenance crew reports an important dust storm with probe covers in position. If a general inspection shows evidence of an heavy contamination:
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Page 610 Jan 01/07
- you must flush of all the pressure lines. (Ref. TASK 12-24-34-600-801) (Ref. TASK 34-11-00-170-801) (Ref. TASK 34-11-00-170-802) (Ref. TASK 34-11-00-170-803)
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the sensors and probes | | | | | | | | | | | | | | | | A.| | Inspect all the probes and sensors. | X | | | | | | | | | | | | | | | | |(1) Examine all the probes and sensors | | | | | | | | | for damage and contamination (not | | | | | | | | | clogged): | | | | | | | | | - the pitot probes | | | | | | | | | - the static probes | | | | | | | | | - the TAT sensors | | | | | | | | | - the AOA sensors | | | | | | | | | - the ice detector probes | | | | | | | | | (if installed). | | | | | | | | |NOTE: Make sure that the AOA sensors | | | | | | | | | move freely and that the drain | | | | | | | | | holes of the pitot probes are not| | | | | | | | | clogged. | | | | | | | | | | | | | | | | | |(2) Drain the standby static pressure | X | | | | | | | | lines and make sure that there | | | | | | | | | are no signs of dust | | | | | | | | | (Ref. TASK 12-24-34-600-801). | | | | | | | | | If you find contamination: | | | | | | | | | (a) Flush all the pressure lines | | | X | | | | | | (Ref. TASK 34-11-00-170-801) | | | | | | | | | (Ref. TASK 34-11-00-170-802) | | | | | | | | | (Ref. TASK 34-11-00-170-803). | | | | | | -------------------------------------------------------------------------------
EFF : ALL 05-51-25 SROS
Page 611 Jan 01/03
Subtask 05-51-25-210-082 E. Inspection of the Landing Gear Doors, the Landing Gears and the Landing Gear Wells (Ref. AMM 122232 PB 301)
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the landing gear doors, | | | | | | | | |the landing gears and the landing gear | | | | | | | | |wells. | | | | | | | | |NOTE: If you find contamination, you | X | | | | | | | | must: | | | | | | | | | (a) Remove the contamination from | | X | | | | | | | surface, the moving joints | | | | | | | | | and the chromed areas of | | | | | | | | | shock absorbers and actuators | | | | | | | | | before the next flight. | | | | | | | | | (b) Do a full lubrication of | | | X | | | | | | the landing gears before a | | | | | | | | | maximum of 10 flight cycles | | | | | | | | | (Ref. AMM 12-22-32, PB 301). | | | | | | | | | | | | | | | | A.| |Inspection of the doors | | | | | | | | |(1) Examine all the doors for damage | X | | | | | | | | and/or contamination, specially on:| | | | | | | | | - the door skin | | | | | | | | | - the door hinges | | | | | | | | | - the proximity sensors | | | | | | | | | - the actuators bare rods. | | | | | | | | | | | | | | | | B.| |Inspection of the landing gears | | | | | | | | |(1) Examine all the landing gear | X | | | | | | | | structures and the components | | | | | | | | | installed on them for damage and/or| | | | | | | | | contamination, specially on: | | | | | | | | | - the attachment points of the | | | | | | | | | landing gears | | | | | | | | | - the proximity sensors | | | | | | | | | - the actuator rods | | | | | | | | | - the chromed area of the shock | | | | | | | | | absorbers | | | | | | | | | - the mechanical linkages and the | | | | | | | | | moving joints. | | | | | | | | | | | | | | | | C.| |Inspection of the landing gear wells. | | | | | |
EFF : ALL 05-51-25 SROS
Page 612 Jan 01/03
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | |(1) Examine all the landing gear wells | X | | | | | | | | and the components installed in | | | | | | | | | them for damage and/or | | | | | | | | | contamination. | | | | | | ------------------------------------------------------------------------------R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-25-210-083 F. Inspection of the Nacelles and the Engines NOTE : If the aircraft was on the ground with the applicable protective ____ covers/devices installed (Ref. AMM 10-11-00) when the dust contamination occurred, this inspection is not necessary if there is no dust behind the covers. NOTE : If the aircraft was on the ground without the applicable ____ protective covers/devices installed, we recommend that after you start the engines, you let the engines run a few minutes before you use the bleed air systems. This is to make sure that the engines blow out remaining particles. (Ref. TASK 71-61-00-220-801) (Ref. TASK 71-13-00-220-801) (Ref. TASK 78-30-00-210-802) (Ref. TASK 26-21-00-720-819) (Ref. TASK 71-00-00-200-802) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the nacelles and engines | | | | | | | | | | | | | | | | A.| |Inspection of the nacelles | | | | | | | | |(1) Examine the air intake cowl for | X | | | | | | | | damage | | | | | | | | | (Ref. TASK 71-61-00-220-801). | | | | | | | | |(2) Examine the fan cowl doors for | X | | | | | | | | damage | | | | | | | | | (Ref. TASK 71-13-00-220-801). | | | | | | | | |(3) Examine the thrust reversers for | X | | | | | | | | damage | | | | | |
EFF : ALL 05-51-25 SROS
Page 613 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (Ref. TASK 78-30-00-210-802). | | | | | | | | | | | | | | | | B.| |Inspection of the engines | | | | | | | | |(1) Examine the fire extinguisher | X | | | | | | | | outlets for contamination. | | | | | | | | | If you find contamination: | | | | | | | | | (a) Do a check of the | | X | | | | | | | distribution piping for | | | | | | | | | obstruction | | | | | | | | | (Ref. TASK 26-21-00-720-819). | | | | | | | | |(2) Do the inspection of the engines | X | | | | | | | | after dust ingestion | | | | | | | | | (Ref. TASK 71-00-00-200-802). | | | | | | ------------------------------------------------------------------------------**ON A/C 701-749, Subtask 05-51-25-210-083-A F. Inspection of the Nacelles and the Engines NOTE : If the aircraft was on the ground with the applicable protective ____ covers/devices installed (Ref. AMM 10-11-00) when the dust contamination occurred, this inspection is not necessary if there is no dust behind the covers. NOTE : If the aircraft was on the ground without the applicable ____ protective covers/devices installed, we recommend that after you start the engines, you let the engines run a few minutes before you start the bleed air systems. This is to make sure that the engines blow out remaining particles. (Ref. TASK 71-61-41-200-802) (Ref. TASK 71-13-00-200-803) (Ref. TASK 78-32-00-200-802) (Ref. TASK 26-21-00-720-819) (Ref. TASK 71-00-00-200-813)
R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-25 301-399, 401-449, 451-499, 701-749, SROS
Page 614 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the nacelles and engines | | | | | | | | | | | | | | | | A.| |Inspection of the nacelles | | | | | | | | |(1) Examine the air intake cowl for | X | | | | | | | | damage | | | | | | | | | (Ref. TASK 71-61-41-200-802). | | | | | | | | |(2) Examine the fan cowl doors for | X | | | | | | | | damage | | | | | | | | | (Ref. TASK 71-13-00-200-803). | | | | | | | | |(3) Examine the thrust reversers for | X | | | | | | | | damage | | | | | | | | | (Ref. TASK 78-32-00-200-802). | | | | | | | | | | | | | | | | B.| |Inspection of the engines | | | | | | | | |(1) Examine the fire extinguisher | X | | | | | | | | outlets for contamination. | | | | | | | | | If you find contamination: | | | | | | | | | (a) Do a check of the | | X | | | | | | | distribution piping for | | | | | | | | | obstruction | | | | | | | | | (Ref. TASK 26-21-00-720-819). | | | | | | | | |(2) Do inspection/check of the engine | X | | | | | | | | after dust ingestion | | | | | | | | | (Ref. TASK 71-00-00-200-813). | | | | | | ------------------------------------------------------------------------------**ON A/C ALL Subtask 05-51-25-210-084
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G. Inspection (Ref. TASK (Ref. TASK (Ref. TASK (Ref. TASK
of the APU 49-16-00-200-801) (Ref. TASK 49-16-00-100-801). 49-91-44-000-801) (Ref. TASK 49-91-44-400-801) 49-20-00-290-809) (Ref. TASK 49-20-00-290-810) 26-22-00-200-801)
EFF : ALL 05-51-25 SROS
Page 615 Jul 01/06
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the APU | | | | | | | | | | | | | | | | A.| |Examine the APU intake and exhaust for | X | | | | | | | |contamination and/or damage | | | | | | | | |(Ref. TASK 49-16-00-200-801). | | | | | | | | |If you find contamination: | | | | | | | | |(1) If the APU was not in operation | | | | | | | | | during the dust contamination: | | | | | | | | | (a) Clean the APU air intake and | | X | | | | | | | exhaust | | | | | | | | | (Ref. TASK 49-16-00-100-801). | | | | | | | | |(2) If the APU was in operation during | | | | | | | | | the dust contamination: | | | | | | | | | (a) Clean the APU air intake and | | X | | | | | | | exhaust | | | | | | | | | (Ref. TASK 49-16-00-100-801). | | | | | | | | | (b) Examine the oil cooler for | | X | | | | | | | contamination | | | | | | | | | (Ref. TASK 49-91-44-000-801) | | | | | | | | | (Ref. TASK 49-91-44-400-801). | | | | | | | | | If you find contamination: | | | | | | | | | - do an APU inspection/check | | | X | | | | | | (Ref. TASK 49-20-00-290-809) | | | | | | | | | (Ref. TASK 49-20-00-290-810).| | | | | | | | | NOTE: We recommend that you | | | | | | | | | replace the APU if you | | | | | | | | | find large contamination | | | | | | | | | in the oil cooler. | | | | | | | | | (c) Examine the fire extinguisher | | X | | | | | | | outlets for contamination | | | | | | | | | (Ref. TASK 26-22-00-200-801). | | | | | | -------------------------------------------------------------------------------
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Subtask 05-51-25-210-085 H. Inspection of the Hydraulic System (Ref. TASK 29-10-00-200-803) (Ref. TASK 12-32-29-281-801)
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the hydraulic system | | | | | | | | | | | | | | | | A.| |Examine the filters for contamination | X | | | | | | | |(clogging indicators and filter | | | | | | | | |elements) | | | | | | | | |(Ref. TASK 29-10-00-200-803). | | | | | | | | |If you find contamination: | | | | | | | | |(1) replace the filter elements. | | X | | | | | | |(2) get a sample of fluid and make | | X | | | | | | | sure that the contamination is in | | | | | | | | | the permitted limits | | | | | | | | | (Ref. TASK 12-32-29-281-801). | | | | | | | | | | | | | | | | B.| |Examine the RAT for contamination | X | | | | | | | |and/or damage. | | | | | | | | | | | | | | | | C.| |Examine the sliding unions for | X | | | | | | | |contamination. | | | | | | | | |If you find contamination: | | | | | | | | |(1) Clean the sliding unions. | | X | | | | -------------------------------------------------------------------------------
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Subtask 05-51-25-210-086 R
J. Inspection of the Fuel System (Ref. TASK 28-12-00-210-802) (Ref. TASK 12-32-28-281-812) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the fuel system | | | | | | | | | | | | | | | | A.| | Examine the NACA vent intakes for | X | | | | | | | | contamination | | | | | |
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| | | (Ref. TASK 28-12-00-210-802). | | | | | | | | | If you find contamination: | | | | | | | | | (1) Get a sample of fuel from the | | X | | | | | | | water drain valves and do a check | | | | | | | | | for particle contamination | | | | | | | | | (Ref. TASK 12-32-28-281-812). | | | | | | | | | If you find contamination: | | | | | | | | | (a) Clean the fuel tanks. | | X | | | | | | | | | | | | | ------------------------------------------------------------------------------Subtask 05-51-25-210-087 K. Inspection of the Anti-Ice System (Ref. TASK 30-11-00-710-801) (Ref. TASK 30-11-51-000-802) (Ref. TASK 3011-51-400-802) NOTE : If the anti-ice system was selected OFF in flight, this inspection ____ is not necessary. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the anti-ice system | | | | | | | | | | | | | | | | A.| | Do an operational test of the wing | X | | | | | | | | anti-ice system: | | | | | | | | | (ref. TASK 30-11-00-710-801). | | | | | | | | | If the valve response time is | | | | | | | | | incorrect: | | | | | | | | | (1) Clean the valve and replace the | | X | | | | | | | valve filter | | | | | |
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Page 618 Jan 01/06
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (Ref. TASK 30-11-51-000-802) | | | | | | | | | (Ref. TASK 30-11-51-400-802). | | | | | | ------------------------------------------------------------------------------5. Close-up ________ Subtask 05-51-25-866-054 A. Retraction of the Flight Control Surfaces (1) Retract the flaps and the slats (Ref. TASK 27-50-00-866-802). (2) Retract the spoilers (Ref. TASK 27-60-00-866-802). Subtask 05-51-25-410-052 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the NLG doors (Ref. TASK 32-22-00-410-801). (3) Close the MLG doors (Ref. TASK 32-12-00-410-801). (4) Close all the access doors, and the access panels opened during the inspection procedure. Subtask 05-51-25-860-053 C. Put the Aircraft back to its Initial Configuration (1) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862801). (2) Remove the access platform(s). (3) Remove the warning notice(s).
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Page 619 Jan 01/06
TASK 05-51-25-200-803 Inspection after Flight through Volcanic Ash or Volcanic Ash contamination on Ground 1. __________________ Reason for the Job Do this inspection after flight in volcanic ash or after volcanic ash contamination on ground. R R R R
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NOTE : If the volcanic ash contamination occurred when the aircraft was on ____ ground with applicable protection by covers and blankets (Ref. AMM 10-11-00), and if there is no ash behind the covers, this inspections specified in para. 4.D. (Inspection of the probes and sensors) and in para. 4.F. (Inspection of the nacelles and engines ) are not necessary. NOTE : This inspection specifies an adjustable access platform (2,5m to ____ 17m/8ft.2in/to55ft.9in) to get access to the different parts of the aircraft during this inspection. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 17M (56 FT) - ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-15-38-613-801 12-21-11-615-801 12-24-34-600-801 12-24-38-680-801 12-32-28-281-812 12-32-29-281-801 21-51-51-000-801
Fill the Potable Water System (Aircraft Electrical Power Available) External Cleaning Draining of the Standby Static Pressure-Lines Draining of the Potable Water System (with Electrical Power) Sample Fuel for Microbiological Contamination Analysis Sampling for Analysis Removal of the Pack Flow Control-Valve (511HB,512HB)
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Page 620 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------21-51-51-400-801 21-63-52-000-801 21-63-52-400-801 24-41-00-862-801 26-21-00-720-819 26-22-00-200-801 27-50-00-866-801 27-50-00-866-802 27-60-00-866-801 27-60-00-866-802 27-80-00-866-801 27-84-61-000-801 27-84-61-400-801 27-84-62-000-801 27-84-62-400-801 28-12-00-210-802 28-14-00-210-801 29-00-00-864-801 29-00-00-864-802 29-00-00-864-803 R
29-10-00-200-803 30-11-51-000-802 30-11-51-400-802 30-21-51-000-801 30-21-51-400-801 32-00-00-481-801
Installation of the Pack Flow Control-Valve (511HB,512HB) Removal of the Trim-Air Pressure-Regulating Valve (638HK, 639HK) Installation of the Trim-Air Pressure-Regulating Valve (638HK, 639HK) De-energize the Aircraft Electrical Circuits from the External Power A Functional Check of the Distribution Piping for Leakage and Obstruction Detailed Visual Inspection of the APU Fire-Extinguishing Distribution-Piping Extension of the Flaps on the Ground Retraction of the Flaps/Slats on the Ground Extension of the Spoilers for Maintenance Retraction of the Spoilers after Maintenance Extension of the Slats on the Ground Removal of the Slat 1 Installation of the Slat 1 Removal of the Slat 2, 3, 4, 5, 6, 7 Installation of the Slat 2, 3, 4, 5, 6, 7 Visual Check Of The Wing And Trim Vent Surge Tank Overpressure Protectors (5201QS1, 5201QS2, 5204QS) (Burst Discs) For Integrity Visual Check of Drain Mast Outlet for Blockage 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) Check of the Clogging Indicators of High Pressure (HP), Return, Engine Driven Pump (EDP) Case drain, Reservoir Fill and Air Pressurization Unit Filters. Removal of the Wing Anti-ice Control Valve Filter Installation of the Wing Anti-ice Control Valve Filter Removal of the Engine-Air-Intake Anti Ice Valve (4000DN) Installation of the Engine-Air-Intake Anti Ice Valve (4000DN) Installation of the Safety Devices on the Landing Gears
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Page 621 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-12-00-010-801 32-12-00-410-801 32-16-00-010-801 32-22-00-010-801 32-22-00-410-801 34-11-00-170-801 34-11-00-170-802 34-11-00-170-803 35-12-41-100-802 36-11-51-000-801 36-11-51-400-801 36-11-52-000-801 36-11-52-400-801 36-12-52-000-801 36-12-52-400-801 49-16-00-100-801 49-16-00-200-801 49-20-00-290-809 49-20-00-290-810 49-91-44-000-801 49-91-44-400-801 53-15-11-200-801 56-11-11-200-801 56-11-12-200-801 56-12-11-200-801 56-21-15-200-801 71-00-00-200-802 71-00-00-200-813 71-13-00-200-803 71-13-00-220-801 R
71-61-00-220-801 71-61-41-200-802 78-30-00-210-802 78-32-00-200-802
Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Open the CLG Doors for Maintenance Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance Flushing of the Principal Total Pressure Lines Flushing of the Principal Static Pressure Lines Draining and Flushing of the Standby Static and Standby Total Pressure Lines Cleaning of the mask full-face / Quick donning Removal of the HP Bleed Valve (4000HA) Installation of the HP Bleed Valve (4000HA) Removal of the Bleed Valve (4001HA) Installation of the Bleed Valve (4001HA) Removal of the Crossbleed Valve (6HV) Installation of the Crossbleed Valve (6HV) Cleaning of the Air Intake System Inspection of the Air Intake System Borescope Inspection of the Load Compressor - Access Through the LCIT-Sensor Bore Borescope Inspection of the APU Power Section Removal of the Oil Cooler (5100KT8) Installation of the Oil Cooler (5100KT8) Detailed Inspection of the Radome (110AL) Inspection of the Windshields (3DG1,3DG2). Inspection of the Fixed Windows (7DG1,7DG2) Inspection of the Sliding Windows (8DG1,8DG2). Detailed Visual Inspection of Passenger Cabin Window Panes including Passenger/ Crew Door and Emergency Exit Window Panes Inspection Procedures After the Ingestion of Volcanic Ash or Sand Examine the Power Plant after Contamination with Volcanic Ash Inspection of the Fan Cowl Doors Visual Inspection of Forward and Aft fan Cowls (5130EA) ,(5140EA), (5150EA), (5110EA) and (5120EA). Detailed Inspection of Intake Cowl Lip and Inner Skin Visual Check of the Airwashed Surfaces for Distortion and Security of Installation Visual Inspection of the Thrust Reverser (4120KS to 4130KS) (Thrust Reverser Closed) Inspection of the Thrust Reverser Structure
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Page 622 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------AMM AMM
122227 PB 301 122232 PB 301
(for corrective action) (for corrective action)
3. __________ Job Set-up Subtask 05-51-25-210-077 A. General WARNING : DO NOT BREATHE VOLCANIC ASH. DO NOT GET VOLCANIC ASH IN YOUR _______ EYES. PUT ON PROTECTIVE CLOTHES, EYE GOGGLES AND A RESPIRATOR MASK. MAKE SURE THAT THE RESPIRATOR MASK CAN REMOVE VOLCANIC ASH FROM THE AIR. VOLCANIC ASH CAN CAUSE EYE IRRITATION AND INJURY TO THE RESPIRATORY SYSTEM. (1) Volcanic ash (a) Volcanic ash is hard, very abrasive and acid (pH between 2 and neutral). It can cause erosion/abrasion, etching or shot-peening on the surfaces and can remove the finishes/protection and thus cause damage/corrosion. (b) The ash particles can be of different sizes but the texture of volcanic ash is almost the same as talcum powder and can enter all orifices and go through many seals. Volcanic ash will stay: - on bare and lubricated surfaces. - in all corners. - in bottom places. It can cause unusual wear and contamination of many aircraft systems and filter elements. (c) The volcanic ash will melt when it goes through the chamber of the engines. The melted ash has very high adhesive qualities and engine parts and thus decreases engine performance. obstruct the fuel injectors and can cause an engine
combustion bonds to It may shutdown.
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Page 623 Jan 01/07
(2) Inspection requirements (a) Volcanic ash can cause severe damage/contamination on the structure/systems of the aircraft. It is not possible to estimate the quantity and the type of damage after volcanic ash contamination. Therefore, it is necessary to do a full inspection of the aircraft to know the damage and make a decision about the necessary repair/action. (b) All the necessary inspections are visual unless the text gives other instructions. Operators can refer to the Non-destructive Testing Manual (NTM) and use non-destructive procedures. (c) If you find damage to the aircraft structure, refer to the Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures. (d) If you find damage to paint/protection, refer to the Structural Repair Manual (SRM). The SRM has the approved paint/protection repair procedures. (e) Examine the aircraft surfaces, structures, systems for contamination, erosion/abrasion, dents, etching, delamination or other damage. Subtask 05-51-25-210-088 B. Inspection Preparation R
(1) If contamination occurred in flight or during landing or take off: (a) Before you start, we recommend that you get information from the crew about the flight conditions. (b) Make sure that you have the related aircraft Post Flight Report (PFR). (c) Do a check of all the events reported by the crew or by the PFR in addition/conjunction with this inspection. (2) If contamination occurred with the aircraft in the parking configuration, it is not necessary to do a check of the systems which are protected by the applicable protective covers/devices if you do not find ash behind them.
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Subtask 05-51-25-481-053 C. Safety Precautions (1) Install the safety devices on the landing gears (Ref. TASK 32-00-00481-801). Subtask 05-51-25-866-057 D. Extension of the Flight Control Surfaces (1) Extend the flaps (Ref. TASK 27-50-00-866-801). (2) Extend the slats (Ref. TASK 27-80-00-866-801). (3) Extend the spoilers (Ref. TASK 27-60-00-866-801). Subtask 05-51-25-010-053 E. Get Access R
(1) Open the main gear doors and install the safety devices (Ref. TASK 32-12-00-010-801). (2) Open the nose gear doors and install the devices (Ref. TASK 32-22-00010-801). (3) Open the center gear doors and install the safety devices (Ref. TASK 32-16-00-010-801). Subtask 05-51-25-860-054 F. Aircraft Maintenance Configuration (1) Make sure that the hydraulic systems are depressurized (2) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (3) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803). (4) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802). (5) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
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Page 625 Jan 01/07
(6) Put warning notices in the cockpit to tell persons not to operate the systems. R R
(7) Put an ACCESS PLATFORM 17M (56 FT) - ADJUSTABLE in position near the area you must inspect. 4. Procedure _________ Subtask 05-51-25-160-053 A. Cleaning of the Aircraft CAUTION : DO NOT RUB THE SURFACE WHEN YOU REMOVE THE ASH FROM THE _______ AIRCRAFT. IF YOU RUB THE SURFACE, YOU CAN CAUSE EROSION/ ABRASION. CAUTION : DO NOT USE FLUIDS TO REMOVE THE ASH. IF THERE IS A LAYER OF ASH _______ ON THE AIRCRAFT SURFACES, REMOVE THE ASH WITH A VACUUM CLEANER (OR, IF YOU CANNOT USE A VACUUM CLEANER, USE AN AIR BLOWER, A SOFT CLOTH OR A HAND BRUSH). FLUIDS CAN MIX WITH THE ASH AND MAKE A PASTE THAT CAN CAUSE EROSION/ABRASION. THIS PASTE CAN GO INTO AREAS THAT ARE NOT EASY TO CLEAN. (1) If there is a layer of volcanic ash on the aircraft surfaces, remove the volcanic ash with a vacuum cleaner, an air blower, a soft cloth or a soft brush. (2) Clean the aircraft internally. (3) Clean the aircraft externally (Ref. TASK 12-21-11-615-801). Subtask 05-51-25-210-089
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B. Internal Inspection (Ref. TASK 35-12-41-100-802) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the cabin area | | | | | | | | | | | | | | | | A.| |Examine the cabin area for ash | X | | | | | | | |contamination. | | | | | | | | |If you find contamination: | | | | | | | | |(1) Clean all the contaminated surfaces| | X | | | | | | | | | | | | | | B.| |Examine the cockpit for ash | X | | | | |
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Page 626 Jan 01/03
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | |contamination. | | | | | | | | |If you find contamination: | | | | | | | | |(1) Clean all the contaminated surfaces| | X | | | | | | |(2) Examine the oxygen full face masks | | X | | | | | | | for contamination. | | | | | | | | | If you find contamination: | | | | | | | | | (a) Clean the oxygen full face | | | X | | | | | | masks | | | | | | | | | (Ref. TASK 35-12-41-100-802). | | | | | | | C.| |Examine the avionics compartment (all | X | | | | | | | |the items you can see), specially: | | | | | | | | |- around the ventilated components | | | | | | | | |- the plugs | | | | | | | | |- the equipments | | | | | | | | |for ash contamination. | | | | | | | | |If you find contamination: | | | | | | | | |(1) Clean all the contaminated surfaces| | X | | | | | | |NOTE: If the crew report shows a very | | | | | | | | | dense cloud of volcanic ashes, | | | | | | | | | clean the computers in the | | | | | | | | workshop. | | | | | | | | | | | | | | | | D.| |Examine the cargo compartments for ash | X | | | | | | | |contamination. | | | | | | | | |If you find contamination: | | | | | | | | |(1) Clean all the contaminated surfaces| | X | | | | | | | (specially the PDU sensors). | | | | | | | | |(2) Examine the cargo drainage system | | X | | | | | | | (if installed) for ash | | | | | | | | | contamination. | | | | | | | | | If you find contamination: | | | | | | | | | (a) Replace the filters of the | | | X | | | | | | drain funnels. | | | | | | -------------------------------------------------------------------------------
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Page 627 Jan 01/03
Subtask 05-51-25-210-090 C. Inspection (Ref. TASK (Ref. TASK (Ref. TASK
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of the Fuselage, the Wings and the Stabilizers 53-15-11-200-801) (Ref. TASK 56-11-11-200-801) 56-11-12-200-801) (Ref. TASK 56-12-11-200-801) 56-21-15-200-801) (Ref. AMM 122227 PB 301)
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the fuselage | | | | | | | | | | | | | | | | A.| | Examine the radome skin for damage | X | | | | | | | | (Ref. TASK 53-15-11-200-801). | | | | | | | | | | | | | | | | B.| | Examine the windshield, the fixed | X | | | | | | | | windows and the sliding windows for | | | | | | | | | damage: | | | | | | | | | - for the windshield | | | | | | | | | (Ref. TASK 56-11-11-200-801) | | | | | | | | | - for the fixed windows | | | | | | | | | (Ref. TASK 56-11-12-200-801) | | | | | | | | | - for the sliding windows | | | | | | | | | (Ref. TASK 56-12-11-200-801). | | | | | | | | | | | | | | | | C.| | Examine the passenger cabin windows, | X | | | | | | | | the passenger/crew doors and the | | | | | | | | | emergency exit windows for damage | | | | | | | | | (Ref. TASK 56-21-15-200-801). | | | | | | | | | | | | | | | | D.| | Examine all of the fuselage skin, the | X | | | | | | | | belly fairing and the wing-to-fuselage| | | | | | | | | fairings for damage. | | | | | | | | | | | | | | | | E.| | Examine the ram air inlet and outlet, | X | | | | | | | | the air inlet and outlet flaps for | | | | | | | | | damage. | | | | | | | | | | | | | | | |2. | | Inspection of the Wings | | | | | | | | | | | | | | | | A.| | Examine all the static dischargers for| X | | | | | | | | damage. | | | | | | | | | | | | | | | | B.| | Examine the top and bottom skin of the| X | | | | | | | | wings for damage. | | | | | | | | | | | | | | |
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Page 628 Jan 01/03
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | C.| | Examine the flap track fairings for | X | | | | | | | | damage. | | | | | | | | | | | | | | | | D.| | Examine the skin of all the control | X | | | | | | | | surfaces ( slats, flaps, ailerons | | | ||| | | | and the spoilers), specially the | | | | | | | | | leading and the trailing edges, | | | | | | | | | for damage. | | | | | | | | | | | | | | | | E.| | Examine the hinge areas of the | X | | | | | | | | spoilers and the ailerons for | | | | | | | | | contamination. | | | | | | | | | | | | | | | | F.| | Examine the flap tracks, flap inter | X | | | | | | | | connecting strut, track 4 sensor, | | | | | | | | | roller mechanisms, steady bearings and| | | | | | | | | universal joints for contamination. | | | | | | | | | Make sure that there is no ash deposit| | | | | | | | | on the roller stops. | | | | | | | | | If you find contamination: | | | | | | | | | (1) Clean and lubricate the related | | X | | | | | | | components | | | | | | | | | (Ref. AMM 12-22-27 PB 301). | | | | | | | | | | | | | | | | G.| | Examine the piston rod of each | X | | | | | | | | servocontrol of the ailerons and the | | | | | | | | | spoilers for contamination. | | | | | | | | | If you find contamination: | | | | | | | | | (1) Clean the piston rod of the | | X | | | | | | | servocontrols. | | | | | | | | | | | | | | | |3. | | Inspection of the Vertical Stabilizer | | | | | | | | | | | | | | | | A.| | Examine all the static dischargers for| X | | | | | | | | damage. | | | | | | | | | | | | | | | | B.| | Examine the skin of the vertical | X | | | | | | | | stabilizer and the rudder, specially | | | | | | | | | the leading and the trailing edges, | | | | | | | | | for damage. | | | | | | | | | | | | | | | | C.| | Examine the hinge areas of the rudder | X | | | | | | | | for contamination. | | | | | |
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Page 629 Jan 01/03
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | | | | | | | | D.| | Examine the piston rod of each | X | | | | | | | | servocontrol of the rudder for | | | | | | | | | contamination. | | | | | | | | | If you find contamination: | | | | | | | | | (1) Clean the piston rod of the | | X | | | | | | | servocontrols. | | | | | | | | | | | | | | | |4. | | Inspection of the Horizontal | | | | | | | | | Stabilizers | | | | | | | | | | | | | | | | A.| | Examine all the static dischargers for| X | | | | | | | | damage. | | | | | | | | | | | | | | | | B.| | Examine the skin of the horizontal | X | | | | | | | | stabilizers and the elevators, | | | | | | | | | specially the leading and the trailing| | | | | | | | | edges, for damage. | | | | | | | | | | | | | | | | C.| | Examine the hinge areas of the | X | | | | | | | | elevators for contamination. | | | | | | | | | | | | | | | | D.| | Examine the piston rod of each | X | | | | | | | | servocontrol of the elevators for | | | | | | | | | contamination. | | | | | | | | | If you find contamination: | | | | | | | | | (1) Clean the piston rod of the | | X | | | | | | | servocontrols. | | | | | | | | | | | | | | | |5. | | Inspection of the external lights | | | | | | | | | | | | | | | | A.| | Examine all the external lights for | X | | | | | | | | damage. | | | | | | | | | If you find damage: | | | | | | | | | (1) Replace the related component(s). | | X | | | | | | | | | | | | | |6. | | Inspection of the antennas and the | | | | | | | | | drain masts | | | | | | | | | | | | | | | | A.| | Examine all the antennas and the drain| X | | | | | | | | masts for damage. | | | | | | | | | If you find damage: | | | | | | | | | (1) Replace the related component(s). | | X | | | |
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Page 630 Jan 01/03
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| ------------------------------------------------------------------------------Subtask 05-51-25-210-091 D. Inspection of the Probes and Sensors NOTE : If the aircraft was on ground with the applicable protective ____ covers/devices installed (Ref.AMM 10-11-00) when the volcanic ash contamination occurred, this inspection is not necessary if there is no ash behind the covers.
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NOTE : If the crew report shows a very dense cloud of volcanic ashes, ____ If the maintenance reports a very dense cloud of volcanic ashes with probe covers not in position,. If a general inspection shows evidence of heavy contamination: - you must flush all the pressure lines: (Ref. TASK 12-24-34-600-801) (Ref. TASK 34-11-00-170-801) (Ref. TASK 34-11-00-170-802) (Ref. TASK 34-11-00-170-803) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the sensors and probes | | | | | | | | | | | | | | | | A.| | Inspect all the probes and sensors | X | | | | | | | | | | | | | | | | |(1) Examine all the probes and sensors | | | | | | | | | for damage and contamination (not | | | | | | | | | clogged): | | | | | | | | | - the pitot probes | | | | | | | | | - the static probes | | | | | | | | | - the TAT sensors | | | | | | | | | - the AOA sensors | | | | | | | | | - the ice detector probes | | | | | | | | | (if installed) | | | | | | | | |NOTE: Make sure that the AOA sensors | | | | | | | | | move freely and that the drain | | | | | | | | | holes of the pitot probes are not| | | | | | | | | clogged. | | | | | | | | | | | | | | | | | |(2) Drain the standby static pressure | X | | | | | | | | lines and make sure that there are | | | | | |
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Page 631 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | no signs of ash | | | | | | | | | (Ref. TASK 12-24-34-600-801). | | | | | | | | | If you find contamination: | | | | | | | B.| | Flush all the pressure lines | | X | | | | | | | (Ref. TASK 34-11-00-170-801) | | | | | | | | | (Ref. TASK 34-11-00-170-802) | | | | | | | | | (Ref. TASK 34-11-00-170-803). | | | | | | ------------------------------------------------------------------------------Subtask 05-51-25-210-092 E. Inspection of the Landing Gear Doors, the Landing Gears and the Landing Gear Wells (Ref. AMM 122232 PB 301)
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the landing gear doors, | | | | | | | | |the landing gears and the landing gear | | | | | | | | |wells. | | | | | | | | |NOTE: If you find contamination, you | | | | | | | | | must: | | | | | | | | | (a) Remove the contamination from| | | | | | | | | surface, the moving joints | | | | | | | | | and the chromed areas of | | | | | | | | | shock absorbers and actuators| | | | | | | | | before the next flight. | | | | | | | | | (b) Do a full lubrication of the | | | | | | | | | landing gears before a | | | | | | | | | maximum of 10 flight cycles | | | | | | | | | (Ref. AMM 12-22-32, PB 301). | | | | | | | | | | | | | | | | A.| |Inspection of the doors | | | | | | | | |(1) Examine all the doors for damage | X | | | | | | | | and/or contamination, specially on:| | | | | | | | | - the door skin | | | | | | | | | - the door hinges | | | | | | | | | - the proximity sensors | | | | | | | | | - the actuator bare rods. | | | | | | | | | | | | | | | | B.| |Inspection of the landing gears | | | | | | | | |(1) Examine all the landing gear | X | | | | |
EFF : ALL 05-51-25 SROS
Page 632 Jan 01/03
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | structures and the components | | | | | | | | | installed on them for damage and/or| | | | | | | | | contamination, specially on: | | | | | | | | | - the attachment points of the | | | | | | | | | landing gears | | | | | | | | | - the proximity sensors | | | | | | | | | - the actuator rods | | | | | | | | | - the chromed area of the shock | | | | | | | | | absorbers | | | | | | | | | - the mechanical linkages and the | | | | | | | | | moving joints. | | | | | | | | | | | | | | | | C.| |Inspection of the landing gear wells | | | | | | | | |(1) Examine all the landing gear wells | X | | | | | | | | and the components installed in | | | | | | | | | them for damage and/or | | | | | | | | | contamination. | | | | | | ------------------------------------------------------------------------------R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-25-210-100 F. Inspection of the Nacelles and the Engines NOTE : If the aircraft was on the ground with the applicable protective ____ covers/devices installed (Ref. AMM 10-11-00) when the volcanic ash contamination occurred, thisinspection is not necessary if there is no ash behind the covers. NOTE : If the aircraft was on the ground without the applicable ____ protective covers/devices installed, we recommend that after you start the engines, you let the engines run a few minutes before you use the bleed air systems. This is to make sure that the engines blow out remaining particles. (Ref. TASK 71-61-00-220-801) (Ref. TASK 71-13-00-220-801) (Ref. TASK 78-30-00-210-802) (Ref. TASK 26-21-00-720-819) (Ref. TASK 71-00-00-200-802)
EFF : ALL 05-51-25 SROS
Page 633 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the nacelles and engines | | | | | | | | | | | | | | | | A.| |Inspection of the nacelles | | | | | | | | |(1) Examine the air intake cowl for | X | | | | | | | | damage | | | | | | | | | (Ref. TASK 71-61-00-220-801). | | | | | | | | |(2) Examine the fan cowl doors for | X | | | | | | | | damage | | | | | | | | | (Ref. TASK 71-13-00-220-801). | | | | | | | | |(3) Examine the thrust reversers for | X | | | | | | | | damage | | | | | | | | | (Ref. TASK 78-30-00-210-802). | | | | | | | | | | | | | | | | B.| |Inspection of the engines | | | | | | | | |(1) Examine the fire extinguisher | X | | | | | | | | outlets for contamination. | | | | | | | | | If you find contamination: | | | | | | | | | (a) Do a check of the | | X | | | | | | | distribution piping for | | | | | | | | | obstruction | | | | | | | | | (Ref. TASK 26-21-00-720-819). | | | | | | | | |(2) Do the inspection of the engines | X | | | | | | | | after flight through volcanic ash | | | | | | | | | (Ref. TASK 71-00-00-200-802). | | | | | | ------------------------------------------------------------------------------**ON A/C 701-749, Subtask 05-51-25-210-100-A F. Inspection of the Nacelles and the Engines NOTE : If the aircraft was on the ground with the applicable protective ____ covers/devices installed (Ref. AMM 10-11-00) when the volcanic ash contamination occurred, thisinspection is not necessary if there is no ash behind the covers. NOTE : If the aircraft was on the ground without the applicable ____ protective covers/devices installed, we recommend that after you start the engines, you let the engines run a few minutes before you use the bleed air systems. This is to make sure that the engines blow out remaining particles.
R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-25 301-399, 401-449, 451-499, 701-749, SROS
Page 634 Jul 01/05
(Ref. TASK 71-61-41-200-802) (Ref. TASK 71-13-00-200-803) (Ref. TASK 78-32-00-200-802) (Ref. TASK 26-21-00-720-819) (Ref. TASK 71-00-00-200-813) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the nacelles and engines | | | | | | | | | | | | | | | | A.| |Inspection of the nacelles | | | | | | | | |(1) Examine the air intake cowl for | X | | | | | | | | damage | | | | | | | | | (Ref. TASK 71-61-41-200-802). | | | | | | | | |(2) Examine the fan cowl doors for | X | | | | | | | | damage | | | | | | | | | (Ref. TASK 71-13-00-200-803). | | | | | | | | |(3) Examine the thrust reversers for | X | | | | | | | | damage | | | | | | | | | (Ref. TASK 78-32-00-200-802). | | | | | | | | | | | | | | | | B.| |Inspection of the engines | | | | | | | | |(1) Examine the fire extinguisher | X | | | | | | | | outlets for contamination. | | | | | | | | | If you find contamination: | | | | | | | | | (a) Do a check of the | | X | | | | | | | distribution piping for | | | | | | | | | obstruction | | | | | | | | | (Ref. TASK 26-21-00-720-819). | | | | | | | | |(2) Do inspection/check of the engine | X | | | | | | | | after flight through volcanic ash | | | | | | | | | (Ref. TASK 71-00-00-200-813). | | | | | | ------------------------------------------------------------------------------**ON A/C ALL Subtask 05-51-25-210-094
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G. Inspection (Ref. TASK (Ref. TASK (Ref. TASK (Ref. TASK
of the APU 49-16-00-200-801) (Ref. TASK 49-16-00-100-801) 49-91-44-000-801) (Ref. TASK 49-91-44-400-801) 49-20-00-290-809) (Ref. TASK 49-20-00-290-810) 26-22-00-200-801)
EFF : ALL 05-51-25 SROS
Page 635 Jul 01/06
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the APU | | | | | | | | | | | | | | | | A.| |Examine the APU intake and exhaust for | X | | | | | | | |contamination and/or damage | | | | | | | | |(Ref. TASK 49-16-00-200-801). | | | | | | | | |If you find contamination: | | | | | | | | |(1) If the APU was not in operation | | | | | | | | | during volcanic ash contamination: | | | | | | | | | (a) Clean the APU air intake and | | X | | | | | | | exhaust | | | | | | | | | (Ref. TASK 49-16-00-100-801). | | | | | | | | |(2) If the APU was in operation during | | | | | | | | | volcanic ash contamination: | | | | | | | | | (a) Clean the APU air intake and | | X | | | | | | | exhaust | | | | | | | | | (Ref. TASK 49-16-00-100-801). | | | | | | | | | (b) Examine the oil cooler for | | X | | | | | | | contamination | | | | | | | | | (Ref. TASK 49-91-44-000-801) | | | | | | | | | (Ref. TASK 49-91-44-400-801). | | | | | | | | | If you find contamination: | | | | | | | | | - do an APU inspection/check | | | X | | | | | | (Ref. TASK 49-20-00-290-809) | | | | | | | | | (Ref. TASK 49-20-00-290-810).| | | | | | | | | NOTE: We recommend that you | | | | | | | | | replace the APU if you | | | | | | | | | find large contamination | | | | | | | | | in the oil cooler. | | | | | | | | | (c) Examine the fire extinguisher | | X | | | | | | | outlets for contamination | | | | | | | | | (Ref. TASK 26-22-00-200-801). | | | | | | -------------------------------------------------------------------------------
EFF : ALL 05-51-25 SROS
Page 636 Jul 01/06
Subtask 05-51-25-210-095 R
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H. Inspection of the Fuel System (Ref. TASK 28-12-00-210-802) (Ref. TASK 12-32-28-281-812) (Ref. TASK 2814-00-210-801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the fuel system | | | | | | | | | | | | | | | | A.| | Examine the NACA vent intakes for | X | | | | | | | | contamination | | | | | | | | | (Ref. TASK 28-12-00-210-802). | | | | | | | | | If you find contamination: | | | | | | | | | (1) Get a sample of fuel from the | | X | | | | | | | water drain valves and do a check | | | | | | | | | for particle contamination | | | | | | | | | (Ref. TASK 12-32-28-281-812). | | | | | | | | | If you find contamination: | | | | | | | | | (a) Clean the fuel tanks. | | X | | | | | | | | | | | | | | B.| |Examine the Refuel/Defuel control | X | | | | | | | |panel for contamination. | | | | | | | | |If you find contamination: | | | | | | | | |(1) Clean the panel. | | X | | | | | | | | | | | | | | C.| |Examine the refuel/defuel coupling and | X | | | | | | | |the refuel/defuel coupling cap for | | | | | | | | |contamination. | | | | | | | | |If you find contamination. | | | | | | | | |(1) Clean the refuel/defuel coupling | | X | | | | | | | and the refuel/defuel coupling cap.| | | | | | | | | | | | | | | | D.| |Examine the overwing refuel adaptor/ | X | | | | | | | |cap for contamination. | | | | | | | | |If you find contamination: | | | | | | | | |(1) Clean the adaptor/cap. | | X | | | | | | | | | | | | | | E.| |Examine the fuel drain mast for | X | | | | | | | |contamination | | | | | | | | |(Ref. TASK 28-14-00-210-801). | | | | | | | | |If you find contamination: | | | | | | | | |(1) Clean the fuel drain mast. | | X | | | | -------------------------------------------------------------------------------
EFF : ALL 05-51-25 SROS
Page 637 Jan 01/06
Subtask 05-51-25-210-096 J. Inspection of the Anti-Ice System NOTE : If the anti-ice system was selected OFF ____ is not necessary. (Ref. TASK 27-84-61-000-801) (Ref. TASK (Ref. TASK 27-84-62-000-801) (Ref. TASK (Ref. TASK 30-11-51-000-802) (Ref. TASK (Ref. TASK 30-21-51-000-801) (Ref. TASK
in flight, this inspection 27-84-61-400-801) 27-84-62-400-801) 30-11-51-400-802) 30-21-51-400-801)
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the anti-ice system | | | | | | | | | | | | | | | | A.| |Examine the air inlet and the outlet | X | | | | | | | |of the pre-cooler for contamination. | | | | | | | | | | | | | | | | | |If you find contamination: | | | | | | | | |(1) If the anti-ice system was not in | | | | | | | | | operation during or after volcanic | | | | | | | | | ash contamination: | | | | | | | | | (a) Disconnect and remove the duct | | X | | | | | | | immediately upstream of the | | | | | | | | | wing anti-ice valve. | | | | | | | | | (b) Examine the valve for | | X | | | | | | | contamination. | | | | | | | | | If you find contamination: | | | | | | | | | - Clean the ducts upstream of | | | X | | | | | | the wing anti-ice valve. | | | | | | | | | - Clean the valve and replace | | | X | | | | | | the valve filter | | | | | | | | | (Ref. TASK 30-11-51-000-802) | | | | | | | | | (Ref. TASK 30-11-51-400-802).| | | | | | | | |(2) If the anti-ice system was in | | | | | | | | | operation during or immediately | | | | | | | | | after volcanic ash contamination: | | | | | | | | | (a) Remove the valve filter and | X | | | | | | | | install a clean filter | | | | | | | | | (Ref. TASK 30-11-51-000-802) | | | | | | | | | (Ref. TASK 30-11-51-400-802). | | | | | | | | | (b) Disconnect the anti-ice duct | X | | | | | | | | from the telescopic duct and do| | | | | | | | | a check for contamination. | | | | | |
EFF : ALL 05-51-25 R SROS
Page 638 Jul 01/03
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | If you find contamination: | | | | | | | | | - Clean all the anti-ice ducts | | X | | | | | | | from the pylon interface to | | | | | | | | | the telescopic duct outlet. | | | | | | | | | - Clean the wing anti-ice valve| | X | | | | | | | - Do a check for contamination | | X | | | | | | | at the slat anti-ice duct | | | | | | | | | outlets. Clean them if | | | | | | | | | necessary. | | | | | | | | | (c) Disconnect the slat inter| X | | | | | | | | connecting ducts and do a check| | | | | | | | | for contamination. | | | | | | | | | If you find contamination: | | | | | | | | | - Remove the slats for | | X | | | | | | | component maintenance | | | | | | | | | (Ref. TASK 27-84-61-000-801) | | | | | | | | | (Ref. TASK 27-84-61-400-801) | | | | | | | | | (Ref. TASK 27-84-62-000-801) | | | | | | | | | (Ref. TASK 27-84-62-400-801).| | | | | | | | | (d) Make sure that the telescopic | X | | | | | | | | duct operates correctly and | | | | | | | | | do a check for contamination. | | | | | | | | | If you find contamination: | | | | | | | | | - Remove the telescopic duct | | X | | | | | | | for component maintenance | | | | | | | | | (Ref. TASK 30-11-41-000-801) | | | | | | | | | (Ref. TASK 30-11-41-400-801).| | | | | | | | | | | | | | | | B.| |Examine the nacelle anti-ice valves for| X | | | | | | | |contamination | | | | | | | | |(Ref. TASK 30-21-51-000-801) | | | | | | | | |(Ref. TASK 30-21-51-400-801). | | | | | | | | |If you find contamination: | | | | | | | | |(1) Clean the ducts. | | X | | | | -------------------------------------------------------------------------------
EFF : ALL 05-51-25 SROS
Page 639 Jan 01/03
Subtask 05-51-25-210-097 K. Inspection (Ref. TASK (Ref. TASK (Ref. TASK (Ref. TASK (Ref. TASK
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of the Air Conditioning 36-11-52-000-801) (Ref. 36-12-52-000-801) (Ref. 21-51-51-000-801) (Ref. 21-63-52-000-801) (Ref. 36-11-51-000-801) (Ref.
System TASK 36-11-52-400-801) TASK 36-12-52-400-801) TASK 21-51-51-400-801) TASK 21-63-52-400-801) TASK 36-11-51-400-801)
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the air conditioning | | | | | | | | |system | | | | | | | | | | | | | | | | A.| |Examine the high pressure bleed valves | X | | | | | | | |for contamination | | | | | | | | |(Ref. TASK 36-11-51-000-801) | | | | | | | | |(Ref. TASK 36-11-51-400-801). | | | | | | | | |If you find contamination : | | | | | | | | |(1) Clean the ducts. | | X | | | | | | | | | | | | | | B.| |Examine the bleed valves for | X | | | | | | | |contamination | | | | | | | | |(Ref. TASK 36-11-52-000-801) | | | | | | | | |(Ref. TASK 36-11-52-400-801). | | | | | | | | |If you find contamination : | | | | | | | | |(1) Clean the ducts. | | X | | | | | | | | | | | | | | C.| |Examine the cross-bleed valves for | X | | | | | | | |contamination | | | | | | | | |(Ref. TASK 36-12-52-000-801) | | | | | | | | |(Ref. TASK 36-12-52-400-801). | | | | | | | | |If you find contamination : | | | | | | | | |(1) Clean the ducts. | | X | | | | | | |(2) Replace the cross-bleed valve. | | X | | | | | | | | | | | | | | D.| |Examine the flow control valves for | X | | | | | | | |contamination. | | | | | | | | |(Ref. TASK 21-51-51-000-801) | | | | | | | | |(Ref. TASK 21-51-51-400-801). | | | | | | | | |If you find contamination : | | | | | | | | |(1) Clean the ducts. | | X | | | | | | |(2) Replace the filter. | | X | | | | | | | | | | | | | | E.| |Examine the primary heat exchangers, | X | | | | |
EFF : ALL 05-51-25 SROS
Page 640 Jan 01/03
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | |main heat exchangers, condensers, | | | | | | | | |reheaters and water extractors for | | | | | | | | |contamination. | | | | | | | | |If you find contamination : | | | | | | | | |(1) Clean the related component (refer | | X | | | | | | | to the manufacturers instructions | | | | | | | | | for the cleaning procedure). | | | | | | | | | | | | | | | | F.| |Examine the trim air pressure | X | | | | | | | |regulating valves for contamination | | | | | | | | |(Ref. TASK 21-63-52-000-801) | | | | | | | | |(Ref. TASK 21-63-52-400-801). | | | | | | | | |If you find contamination : | | | | | | | | |(1) Clean the ducts. | | X | | | | | | |(2) Replace the filter. | | X | | | | | | | | | | | | | | G.| |Examine the water extractor drain lines| X | | | | | | | |for contamination and blockage. | | | | | | | | | | | | | | | | H.| |Examine the air cycle machine for | X | | | | | | | |contamination. | | | | | | | | |If you find contamination: | | | | | | | | |(1) Replace the filter. | | X | | | | ------------------------------------------------------------------------------Subtask 05-51-25-210-098 L. Inspection of the Hydraulic System (Ref. TASK 29-10-00-200-803) (Ref. TASK 12-32-29-281-801)
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the hydraulic system | | | | | | | | | | | | | | | | A.| |Examine the filters for contamination | X | | | | | | | |(clogging indicators and filter | | | | | | | | |elements) | | | | | | | | |(Ref. TASK 29-10-00-200-803). | | | | | | | | |If you find contamination: | | | | | | | | |(1) replace the filter elements. | | X | | | | | | |(2) get a sample of fluid and make | | X | | | |
EFF : ALL 05-51-25 SROS
Page 641 Jan 01/03
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | sure that contamination is in | | | | | | | | | the permitted limits | | | | | | | | | (Ref. TASK 12-32-29-281-801). | | | | | | | | | | | | | | | | B.| |Examine the RAT for contamination | X | | | | | | | |and/or damage. | | | | | | | | | | | | | | | | C.| |Examine the sliding unions for | X | | | | | | | |contamination. | | | | | | | | |If you find contamination: | | | | | | | | |(1) Clean the sliding unions. | | X | | | | ------------------------------------------------------------------------------Subtask 05-51-25-210-099 M. Inspection of the Potable Water System (Ref. TASK 12-24-38-680-801) (Ref. TASK 12-15-38-613-801).
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the potable water system | | | | | | | | | | | | | | | | A.| |Drain the potable water system, flush | X | | | | | | | |and refill with potable water | | | | | | | | |(Ref. TASK 12-24-38-680-801) | | | | | | | | |(Ref. TASK 12-15-38-613-801). | | | | | | ------------------------------------------------------------------------------5. Close-up ________ Subtask 05-51-25-866-055 A. Retraction of the Flight control surfaces (1) Retract the flaps and the slats (Ref. TASK 27-50-00-866-802). (2) Retract the spoilers (Ref. TASK 27-60-00-866-802).
EFF : ALL 05-51-25 SROS
Page 642 Jan 01/03
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Subtask 05-51-25-410-053 B. Close Access
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(1) Make sure that the work area is clean and clear of tools and other items.
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(2) Close the NLG doors (Ref. TASK 32-22-00-410-801).
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(3) Close the MLG doors (Ref. TASK 32-12-00-410-801).
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(4) Close all the access doors, and the access panels opened during the inspection procedure.
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Subtask 05-51-25-860-055
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C. Put the Aircraft back to its Initial Configuration
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(1) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801)
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(2) Remove the access platform(s).
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(3) Remove the warning notice(s).
EFF : ALL 05-51-25 SROS
Page 643 Jul 01/02
INSPECTION AFTER ENGINE FAILURE - INSPECTION/CHECK __________________________________________________ TASK 05-51-26-200-801 Inspection of the Aircraft after Engine Failure 1. __________________ Reason for the Job You must do this inspection after an engine failure if: - the engine is not balanced after one or several blades (fan or other blades) is /are damaged/missing. - the engine is seized. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
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No No No No
specific specific specific specific
safety barriers warning notices wheel chocks adjustable access platform 5.0 m (16 ft. 5 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------05-56-00-200-801 32-00-00-481-801 71-00-00-000-803 71-00-00-000-805 71-00-00-400-803 71-13-00-010-802 71-13-00-010-805 71-13-00-410-802 71-13-00-410-805 78-30-00-010-801
Measurement of the Aircraft by Photogrammetry after Abnormal Operation of the Aircraft Installation of the Safety Devices on the Landing Gears Removal of the Engine Removal of the Demountable Power Plant Installation of the Engine Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Open the Fan Cowl Doors Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Close the Fan Cowl Doors Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS)
EFF : ALL 05-51-26 SROS
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------78-30-00-010-803 78-30-00-410-801 78-30-00-410-803
Open the Thrust Reverser Cowl Doors Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Close the Thrust Reverser Cowl Doors
3. __________ Job Set-up Subtask 05-51-26-941-050 A. Safety Precautions (1) Put the safety barriers in position. (2) Put warning notices in position in the cockpit to tell persons not to operate the systems. (3) Put wheel chocks in position at the main gears. (4) Install the safety devices on the landing gear (Ref. TASK 32-00-00481-801). R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-26-010-050 B. Get Access (1) Open the fan cowls doors (Ref. TASK 71-13-00-010-802).
R
(a) FOR 4030EM1 415BL, 416BR
R
(b) FOR 4030EM2 425BL, 426BR (2) Open the thrust reverser doors (Ref. TASK 78-30-00-010-801).
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(a) FOR 4030EM1 417AL, 418AR
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(b) FOR 4030EM2 427AL, 428AR
EFF : ALL 05-51-26 SROS
Page 602 Jul 01/05
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(3) Put an adjustable access platform in position near the damaged engine. **ON A/C 701-749, Subtask 05-51-26-010-050-A B. Get Access (1) Open the fan cowls doors (Ref. TASK 71-13-00-010-805). (a) FOR 4030EM1 415AL, 416AR (b) FOR 4030EM2 425AL, 426AR (2) Open the thrust reverser doors (Ref. TASK 78-30-00-010-803). (a) FOR 4030EM1 417AL, 418AR (b) FOR 4030EM2 427AL, 428AR
R
(3) Put an adjustable access platform in position near the damaged engine. **ON A/C ALL Subtask 05-51-26-860-050 C. Aircraft Maintenance Configuration (1) Make sure that the hydraulic systems are depressurized **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-26-010-051 D. Engine Removal (1) Remove the engine (Ref. TASK 71-00-00-000-803).
EFF : ALL 05-51-26 SROS
Page 603 Jan 01/07
**ON A/C 701-749, Subtask 05-51-26-010-051-A D. Engine Removal (1) Remove the engine (Ref. TASK 71-00-00-000-805). **ON A/C ALL 4. Procedure _________ R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-26-210-050 A. Inspection of the Pylon and the Nacelle (Ref. TASK 05-56-00-200-801) NOTE : All the necessary inspections are visual unless specified ____ differently in the text procedure. Operators can refer to the Non Destructive Testing Manual (NTM) and use non destructive procedure. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of Outboard and Inboard | | | | | | | | | Pylons | | | | | | | | | | | | | | | | A.| | Examine the items below for cracks, | | | | | | | | | signs of shear, damaged or missing | X | | | | | | | | fasteners, cracked paint: | | | | | | | | | - external panels | | | | | | | | | - the plates you find in: | | | | | | | | | . the visor | | | | | | | | | . the forward secondary structure | | | | | | | | | . the primary structure | | | | | | | | | . the pylon-to-wing fillet | | | | | | | | | . the aft secondary structure | | | | | | | | | . the aft bottom fairing | | | | | | | | | . the center bottom fairing | | | | | | | | | . all access doors and panels. | | | | | |
EFF : ALL 05-51-26 SROS
Page 604 Jul 01/05
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | If you find damage: | | | | | | | | | (1) Open the doors and panels to get | | X | | | | | | | access to the structure. | | | | | | | | | (2) Examine the adjacent structure for| | X | | | | | | | distortion and the plates for | | | | | | | | | - buckles or warps, wrinkles or | | | | | | | | | tears. | | | | | | | | | (3) Examine the items below for | | X | | | | | | | - distortion, pulled or missing | | | | | | | | | fasteners, tears or cracked | | | | | | | | | paint: | | | | | | | | | . the primary structure | | | | | | | | | . the fasteners | | | | | | | | | . the longerons | | | | | | | | | . the lateral plates | | | | | | | | | . the main ribs | | | | | | | | | . the lateral panels. | | | | | | | | | (4) Examine the fire protection system| | | | | | | | | and specially the items below for | | | | | | | | | - distortion, fluid leaks and | | | | | | | | | other damage: | | X | | | | | | | . the attachments of the fire | | | | | | | | | extinguishing bottles | | | | | | | | | . the attachment of the pipes | | | | | | | | | . the electrical wiring | | | | | | | | | . the hydraulic pipes | | | | | | | | | . the fuel pipes | | | | | | | | | . the air conditioning pipes and| | | | | | | | | components | | | | | | | | | . the components that are in the| | | | | | | | | engine pylon. | | | | | | | | | | | | | | | | B.| | Examine externally the hinge fittings | | | | | | | | | of: | X | | | | | | | | - the fan cowls | | | | | | | | | - the thrust reverser cowls. | | | | | | | | | | | | | | | |2. | | Inspection of the Nacelles | | | | | | | | | | | | | | | | A.| | Examine the fan cowls. | X | | | | | | | | | | | | | | | B.| | Examine the thrust reverser cowls | X | | | | | | | | | | | | | |
EFF : 001-049, 201-249, 251-252, 255-299, 05-51-26 301-399, 401-449, 451-499, SROS
Page 605 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | If you find damage: | | | | | | | | | (1) Examine externally the engine-to- | | X | | | | | | | pylon attach fittings below the | | | | | | | | | main ribs for: | | | | | | | | | - damage, rupture, signs of burns | | | | | | | | | oxidation, cracks, distortion. | | | | | | | | | (2) Remove the fillets from the | | X | | | | | | | outboard and inboard pylons. | | | | | | | | | (3) Examine | | | | | | | | | - the forward pylon-to-wing attach| | | | | | | | | fitting | | | | | | | | | - the aft pylon-to-wing attach | | | | | | | | | fitting. | | | | | | | | | If you find damage: | | | | | | | | | (a) Examine the area adjacent to | | | | | | | | | the forward and aft | | | | | | | | | attachments of the pylon for: | | | X | | | | | | - the correct condition of all| | | | | | | | | fasteners and safety | | | | | | | | | devices, cracks and damage. | | | | | | | | | (b) Examine the wing bottom skin | | | | | | | | | adjacent to the forward and | | | | | | | | | aft attachments of the pylon | | | X | | | | | | for : | | | | | | | | | - cracks, fluid leaks, damage,| | | | | | | | | the correct condition of all| | | | | | | | | fasteners and safety | | | | | | | | | devices. | | | | | | | | | If you find damage: | | | | | | | | | (1) Defuel the wing and get access | | | X | | | | | | into it. | | | | | | | | | (2) Examine: | | | | | | | | | - the internal structure | | | | | | | | | - the rear and front spars | | | X | | | | | | - the ribs | | | | | | | | | - the stringers | | | | | | | | | - the pylon attachments | | | | | | | | | - the brackets | | | | | | | | | - the structure adjacent to the | | | | | | | | | outboard and inboard pylons. | | | | | | | | | If you find damage: | | | | | | | | | (1) Do a measurement of the aircraft. | | | X | | | | | | (Ref. TASK 05-56-00-200-801) | | | | | |
EFF : 001-049, 201-249, 251-252, 255-299, 05-51-26 301-399, 401-449, 451-499, SROS
Page 606 Jan 01/07
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| ------------------------------------------------------------------------------**ON A/C 701-749, Subtask 05-51-26-210-050-A A. Inspection of the Pylon and the Nacelle (Ref. TASK 05-56-00-200-801) NOTE : All the necessary inspections are visual unless specified ____ differently in the text procedure. Operators can refer to the Non Destructive Testing Manual (NTM) and use non destructive procedure. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of Outboard and Inboard | | | | | | | | | Pylons | | | | | | | | | | | | | | | | A.| | Examine the items below for cracks, | | | | | | | | | signs of shear, damaged or missing | X | | | | | | | | fasteners, cracked paint: | | | | | | | | | - external panels | | | | | | | | | - the plates you find in: | | | | | | | | | . the visor | | | | | | | | | . the forward secondary structure | | | | | | | | | . the primary structure | | | | | | | | | . the pylon-to-wing fillet | | | | | | | | | . the aft secondary structure | | | | | | | | | . the aft bottom fairing | | | | | | | | | . the center bottom fairing | | | | | | | | | . all access doors and panels. | | | | | | | | | If you find damage: | | | | | | | | | (1) Open the doors and panels to get | | X | | | | | | | access to the structure. | | | | | | | | | (2) Examine the adjacent structure for| | X | | | | | | | distortion and the plates for | | | | | | | | | - buckles or warps, wrinkles or | | | | | | | | | tears. | | | | | | | | | (3) Examine the items below for | | X | | | |
R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-26 301-399, 401-449, 451-499, 701-749, SROS
Page 607 Jul 01/05
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R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - distortion, pulled or missing | | | | | | | | | fasteners, tears or cracked | | | | | | | | | paint: | | | | | | | | | . the primary structure | | | | | | | | | . the fasteners | | | | | | | | | . the longerons | | | | | | | | | . the lateral plates | | | | | | | | | . the main ribs | | | | | | | | | . the lateral panels. | | | | | | | | | (4) Examine the fire protection system| | | | | | | | | and specially the items below for | | | | | | | | | - distortion, fluid leaks and | | | | | | | | | other damage: | | X | | | | | | | . the attachments of the fire | | | | | | | | | extinguishing bottles | | | | | | | | | . the attachment of the pipes | | | | | | | | | . the electrical wiring | | | | | | | | | . the hydraulic pipes | | | | | | | | | . the fuel pipes | | | | | | | | | . the air conditioning pipes and| | | | | | | | | components | | | | | | | | | . the components that are in the| | | | | | | | | engine pylon. | | | | | | | | | | | | | | | | B.| | Examine externally the hinge fittings | | | | | | | | | of: | X | | | | | | | | - the fan cowls | | | | | | | | | - the thrust reverser cowls. | | | | | | | | | | | | | | | |2. | | Inspection of the Nacelles | | | | | | | | | | | | | | | | A.| | Examine the fan cowls. | X | | | | | | | | | | | | | | | B.| | Examine the thrust reverser cowls | X | | | | | | | | If you find damage: | | | | | | | | | (1) Examine externally the engine-to- | | X | | | | | | | pylon attach fittings below the | | | | | | | | | main ribs for: | | | | | | | | | - damage, rupture, signs of burns | | | | | | | | | oxidation, cracks, distortion. | | | | | | | | | (2) Remove the fillets from the | | X | | | | | | | outboard and inboard pylons. | | | | | | | | | (3) Examine | | | | | |
EFF : 701-749, 05-51-26 SROS
Page 608 Jan 01/07
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - the forward pylon-to-wing attach| | | | | | | | | fitting | | | | | | | | | - the aft pylon-to-wing attach | | | | | | | | | fitting. | | | | | | | | | If you find damage: | | | | | | | | | (a) Examine the area adjacent to | | | | | | | | | the forward and aft | | | | | | | | | attachments of the pylon for: | | | X | | | | | | - the correct condition of all| | | | | | | | | fasteners and safety | | | | | | | | | devices, cracks and damage. | | | | | | | | | (b) Examine the wing bottom skin | | | | | | | | | adjacent to the forward and | | | | | | | | | aft attachments of the pylon | | | X | | | | | | for : | | | | | | | | | - cracks, fluid leaks, damage,| | | | | | | | | the correct condition of all| | | | | | | | | fasteners and safety | | | | | | | | | devices. | | | | | | | | | If you find damage: | | | | | | | | | (1) Defuel the wing and get access | | | X | | | | | | into it. | | | | | | | | | (2) Examine: | | | | | | | | | - the internal structure | | | | | | | | | - the rear and front spars | | | X | | | | | | - the ribs | | | | | | | | | - the stringers | | | | | | | | | - the pylon attachments | | | | | | | | | - the brackets | | | | | | | | | - the structure adjacent to the | | | | | | | | | outboard and inboard pylons. | | | | | | | | | If you find damage: | | | | | | | | | (1) Do a measurement of the aircraft. | | | X | | | | | | (Ref. TASK 05-56-00-200-801) | | | | | | -------------------------------------------------------------------------------
EFF : 701-749, 05-51-26 R SROS
Page 609 Apr 01/02
**ON A/C ALL 5. Close-up ________ R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-26-410-051 A. Engine Installation (1) Install the engine (Ref. TASK 71-00-00-400-803). Subtask 05-51-26-410-050 B. Close Access (1) Close the fan cowls doors (Ref. TASK 71-13-00-410-802).
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(a) FOR 4030EM1 415BL, 416BR
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(b) FOR 4030EM2 425BL, 426BR (2) Close the thrust reverser doors (Ref. TASK 78-30-00-410-801).
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(a) FOR 4030EM1 417AL, 418AR
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(b) FOR 4030EM2 427AL, 428AR (3) Close all the access panels that you opened during the inspection. **ON A/C 701-749, Subtask 05-51-26-410-051-A A. Engine Installation (1) Install the engine
EFF : ALL 05-51-26 SROS
Page 610 Jul 01/05
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Subtask 05-51-26-410-050-A B. Close Access
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(1) Close the fan cowls doors (Ref. TASK 71-13-00-410-805).
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(a) FOR 4030EM1 415AL, 416AR
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(b) FOR 4030EM2 425AL, 426AR
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(2) Close the thrust reverser doors (Ref. TASK 78-30-00-410-803).
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(a) FOR 4030EM1 417AL, 418AR
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(b) FOR 4030EM2 427AL, 428AR
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**ON A/C ALL Subtask 05-51-26-942-050 C. Put the Aircraft back to its Initial Configuration (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. (4) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-51-26 SROS
Page 611 Oct 01/00
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INSPECTION AFTER IMPACT ON ENGINE COWLS - INSPECTION/CHECK __________________________________________________________ TASK 05-51-27-200-801
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Inspection after Impact on Engine Cowls 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 FOR FIN 4000EM2 No specific
safety barriers warning notice adjustable access platform 5.0 m (16 ft. 5 in.) adjustable access platform 5.0 m (16 ft. 5 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------71-00-00-000-803 71-00-00-000-805 71-00-00-400-803 71-00-00-400-805 71-13-00-010-802 71-13-00-010-805 71-13-00-410-802 71-13-00-410-805 78-30-00-010-801 78-30-00-410-801 78-30-00-410-803 FOR FIN 4030EM2 78-30-00-010-803
Removal of the Engine Removal of the Demountable Power Plant Installation of the Engine Installation of the Demountable Power Plant Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Open the Fan Cowl Doors Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Close the Fan Cowl Doors Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Close the Thrust Reverser Cowl Doors Open the Thrust Reverser Cowl Doors
EFF : ALL 05-51-27 SROS
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3. __________ Job Set-up Subtask 05-51-27-941-050 A. Safety Precautions (1) Put the safety barriers in position. (2) On the panel 145VU: - put a warning notice to tell persons not to start the engine. R R
(3) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure. (4) On the panel 285VU: - make sure that the ON legend of the ENG/FADEC GND PWR/1, (2), pushbutton switch is off - put a warning notice to tell persons not to energize the FADEC system. (5) On the panel 125VU: - make sure that the ENG MASTER switch 1, (2), is in the OFF position - put a warning notice to tell persons not to energize the ECU.
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**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-27-010-050 B. Get Access
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(1) Open the fan cowl doors (Ref. TASK 71-13-00-010-802).
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(a) FOR 4030EM1 415BL, 416BR
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(b) FOR 4030EM2 425BL, 426BR (2) Open the thrust reverser doors (Ref. TASK 78-30-00-010-801).
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(a) FOR 4030EM1 417AL, 418AR
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(b) FOR 4030EM2 427AL, 428AR
EFF : ALL 05-51-27 SROS
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(3) Put an adjustable access platform in position near the damaged engine. **ON A/C 701-749, Subtask 05-51-27-010-050-A B. Get Access R
(1) Open the fan cowl doors (Ref. TASK 71-13-00-010-805). (a) FOR 4030EM1 415AL, 416AR (b) FOR 4030EM2 425AL, 426AR (2) Open the thrust reverser doors (Ref. TASK 78-30-00-010-803). (a) FOR 4000EM1 417AL, 418AR (b) FOR 4000EM2 427AL, 428AR (3) Put an adjustable access platform in position near the damaged engine.
R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-27 301-399, 401-449, 451-499, 701-749, SROS
Page 603 Jul 01/05
**ON A/C ALL 4. Procedure _________ R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-27-210-050 A. Inspection of the Engine (Ref. TASK 71-00-00-000-803) (Ref. TASK 71-00-00-400-803)
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R R R R R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Examine the cowl after a side impact | | | | | | | | |and damage only to the cowl. | | | | | | | | | | | | | | | | A.| |Externally examine the cowl fittings | X | | | | | | | |and the adjacent area of the pylon: | | | | | | | | |(1) Pylon side panels when damage on | | | | | | | | | thrust reverser or core cowl. | | | | | | | | |(2) Cantilever structure when damage on| | | | | | | | | inlet cowl, fan cowl or thrust | | | | | | | | | reverser for: | | | | | | | | | - damage. | | | | | | | | | | | | | | | |2. | |Examine the cowl after a side impact | | | | | | | | |and subsequent damage to the engine or | | | | | | | | |the equipment/accessories attached to | | | | | | | | |it for: | | | | | | | | |- damage. | | | | | | | | | | | | | | | | A.| |Examine pylon panels, doors and auxi- | X | | | | | | | |liary structure for distortion, | | | | | | | | |wrinkles, buckles, tearing of plates at| | | | | | | | |the rivets and stringers attached to | | | | | | | | |panels. | | | | | | | | | | | | | | | | B.| |Examine pylon main frame for: | X | | | | | | | |- cracks, cracked or flaking paint, | | | | | | | | | loose rivets and signs of shearing | | | | | | | | | and distorsion. | | | | | | | | |If you find damage: | | | | | | | | |(1) Examine panels and adjacent | | X | | | |
EFF : ALL 05-51-27 SROS
Page 604 Jul 01/05
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | structure for: | | | | | | | | | - buckles, tearing of plates at the| | | | | | | | | rivets, stringers attached to | | | | | | | | | panels, distorsion and wrinkles. | | | | | | | | |(2) Examine pylon main frame for: | | X | | | | | | | - distortion and condition of spars| | | | | | | | | and ribs attached to the side | | | | | | | | | panels. | | | | | | | | | If you find damage: | | | | | | | | | (a) Remove the engine | | | X | | | | | | (Ref. TASK 71-00-00-000-803). | | | | | | | | | (b) Examine the FWD and AFT | | | X | | | | | | attachments of the engine pylon| | | | | | | | | for: | | | | | | | | | - distortion and cracks. | | | | | | | | | (c) Remove the center panels of the| | | x | | | | | | pylon-to-wing fillet. | | | | | | | | | (d) Examine the pylon-to-wing | | | X | | | | | | attach fittings for: | | | | | | | | | - distortion and cracks. | | | | | | | | | (e) Install the engine | | | x | | | | | | (Ref. TASK 71-00-00-400-803). | | | | | | -------------------------------------------------------------------------------
R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-27 301-399, 401-449, 451-499, SROS
Page 605 Jul 01/05
**ON A/C 701-749, Subtask 05-51-27-210-050-A A. Inspection of the Engine (Ref. TASK 71-00-00-000-805) (Ref. TASK 71-00-00-400-805)
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R R R R R R R R R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Examine the cowl after a side impact | | | | | | | | |and damage only to the cowl. | | | | | | | | | | | | | | | | A.| |Externally examine the cowl fittings | X | | | | | | | |and the adjacent area of the pylon: | | | | | | | | |(1) Pylon side panels when damage on | | | | | | | | | thrust reverser or core cowl. | | | | | | | | |(2) Cantilever structure when damage on| | | | | | | | | inlet cowl, fan cowl or thrust | | | | | | | | | reverser for: | | | | | | | | | - damage. | | | | | | | | | | | | | | | |2. | |Examine the cowl after a side impact | | | | | | | | |and subsequent damage to the engine or | | | | | | | | |the equipment/accessories attached to | | | | | | | | |it for: | | | | | | | | |- damage. | | | | | | | | | | | | | | | | A.| |Examine pylon panels, doors and auxi- | X | | | | | | | |liary structure for distortion, | | | | | | | | |wrinkles, buckles, tearing of plates at| | | | | | | | |the rivets and stringers attached to | | | | | | | | |panels. | | | | | | | | | | | | | | | | B.| |Examine pylon main frame for: | X | | | | | | | |- cracks, cracked or flaking paint, | | | | | | | | | loose rivets and signs of shearing | | | | | | | | | and distortion. | | | | | | | | |If you find damage: | | | | | | | | |(1) Examine panels and adjacent | | X | | | | | | | structure for: | | | | | | | | | - buckles, tearing of plates at the| | | | | | | | | rivets, stringers attached to | | | | | | | | | panels, distortion and wrinkles. | | | | | | | | |(2) Examine pylon main frame for: | | X | | | |
EFF : 701-749, 05-51-27 SROS
Page 606 Jul 01/05
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - distortion and condition of spars| | | | | | | | | and ribs attached to the side | | | | | | | | | panels. | | | | | | | | | If you find damage: | | | | | | | | | (a) Remove the engine | | | X | | | | | | (Ref. TASK 71-00-00-000-805). | | | | | | | | | (b) Examine the FWD and AFT | | | X | | | | | | attachments of the engine pylon| | | | | | | | | for: | | | | | | | | | - distortion and cracks. | | | | | | | | | (c) Remove the center panels of the| | | x | | | | | | pylon-to-wing fillet. | | | | | | | | | (d) Examine the pylon-to-wing | | | X | | | | | | attach fittings for: | | | | | | | | | - distortion and cracks. | | | | | | | | | (e) Install the engine | | | x | | | | | | (Ref. TASK 71-00-00-400-805). | | | | | | ------------------------------------------------------------------------------**ON A/C ALL 5. Close-up ________
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**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-27-410-050 A. Close Access (1) Close the thrust reverser door (Ref. TASK 78-30-00-410-801).
R
(a) FOR 4030EM1 417AL, 418AR
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(b) FOR 4030EM2 427AL, 428AR
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(2) Close the fan cowl doors (Ref. TASK 71-13-00-410-802).
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(a) FOR 4030EM1 415BL, 416BR
EFF : ALL 05-51-27 SROS
Page 607 Jul 01/05
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(b) FOR 4030EM2 425BL, 426BR (3) Close all the access panels opened during the inspection. **ON A/C 701-749, Subtask 05-51-27-410-050-A A. Close Access (1) Close the thrust reverser door (Ref. TASK 78-30-00-410-803). (a) FOR 4030EM1 417AL, 418AR (b) FOR 4030EM2 427AL, 428AR
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(2) Close the fan cowl doors (Ref. TASK 71-13-00-410-805). (a) FOR 4030EM1 415AL, 416AR (b) FOR 4030EM2 425AL, 426AR (3) Close all the access panels opened during the inspection. **ON A/C ALL Subtask 05-51-27-942-050 B. Put the Aircraft back to its Initial Configuration (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. (4) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-51-27 SROS
Page 608 Jul 01/05
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INSPECTION AFTER SPILLAGE - INSPECTION/CHECK ____________________________________________ TASK 05-51-28-200-801
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Inspection after Spillage 1. __________________ Reason for the Job
R Self Explanatory 2. ______________________ Job Set-up Information R R
A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R R R R
51-78-00-200-801 51-78-00-615-801 51-78-00-615-802 51-78-00-615-803 51-78-00-615-804
Inspection after Mercury Contamination Aircraft Cleaning after a Sewage Leakage Aircraft Cleaning after a Hydraulic Fluid Leakage Aircraft Cleaning after a Fish Shipment Aircraft Cleaning after an Acid or Alkali Leakage
3. __________ Job Set-up R Subtask 05-51-28-869-050 R R
A. Not applicable.
EFF : ALL 05-51-28 SROS
Page 601 Jul 01/05
4. Procedure _________ Subtask 05-51-28-210-050 R R R R R R R R R R R
A. Refer to the applicable procedure(s): - For aircraft cleaning after a sewage leakage (Ref. TASK 51-78-00-615801). - For aircraft cleaning after a hydraulic fluid leakage (Ref. TASK 51-7800-615-802). - For aircraft cleaning after leakage from a fish shipment (Ref. TASK 5178-00-615-803). - For aircraft cleaning after an acid or alkali leakage (Ref. TASK 51-7800-615-804). - For inspection after mercury spillage (Ref. TASK 51-78-00-200-801).
EFF : ALL 05-51-28 SROS
Page 602 Jul 01/05
INSPECTION AFTER ABNORMAL PAX/CREW DOOR MOVEMENT - INSPECTION/CHECK ___________________________________________________________________ TASK 05-51-29-200-801 Inspection after Abnormal Pax/Crew Door Movement. WARNING : BEFORE YOU START WORK ON THE DOOR MAKE SURE THAT: _______ - THE EMERGENCY CONTROL HANDLE IS IN THE DISARMED POSITION WITH THE SAFETY PIN INSTALLED. - THE PERCUSSION LEVER OF THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER IS IN THE DISARMED POSITION WITH THE SAFETY PIN INSTALLED. THIS MAKES SURE THAT THE DOOR DOES NOT OPEN SUDDENLY. IF THE DOOR OPENS SUDDENLY IT CAN CAUSE INJURY AND/OR DAMAGE. 1. __________________ Reason for the Job You must do this inspection in case of abnormal pax/crew door movement like lifting or pushing down by a loader or a jetway. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
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No specific No specific 98A52108008001 98F52108431000
circuit breaker(s) safety clip(s) adjustable access platform 5.50 m (18 ft. 1 in.) 1 SUPPORT FRAME - BALLAST WEIGHT, DOORS 1 BALLAST WEIGHT - SLIDE RAFT
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 25-23-45-000-801 25-23-45-400-801 25-23-46-000-801
Energize the Ground Service Network De-energize the Ground Service Network Removal of the Door Frame Linings of the FWD Passenger/Crew Door Installation of the Door Frame Linings of the FWD Passenger/Crew Door Removal of the Door Frame Linings of the MID Passenger/Crew Door
EFF : ALL 05-51-29 SROS
Page 601 Oct 01/03
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------25-23-46-400-801 25-23-47-000-801 25-23-47-400-801 R R
25-23-49-000-801 25-23-49-400-801
R R R
25-23-51-000-801 25-23-51-400-801
R 25-23-52-000-802 25-23-52-400-802 R R
25-62-41-000-801 25-62-41-400-801 52-10-00-010-801 52-10-00-410-801 52-10-00-860-801 52-10-00-860-802 52-11-12-000-801 52-11-12-000-802 52-11-12-400-801 52-11-12-400-802 52-11-22-000-801 52-11-22-400-801 52-11-31-000-801 52-11-31-400-801
R R
52-12-00-720-801
Installation of the Door Frame Linings of the MID Passenger/Crew Door Removal of the Door Frame Linings of the AFT Passenger/Crew Door Installation of the Door Frame Linings of the AFT Passenger/Crew Door Removal of the Lining of the FWD Passenger/Crew Door(s) Installation of the Lining of the FWD Passenger/Crew Door(s) Removal of the Lining of the MID Passenger/Crew Door(s) Installation of the Lining of the MID Passenger/Crew Door(s) Removal of the Lining of the AFT Passenger/Crew Door Installation of the Lining of the AFT Passenger/Crew Door Escape Facilities - Removal Escape Facilities - Installation Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door Special Precautions before Work on the Passenger/Crew Door Special Precautions after Work on the Passenger/Crew Door Removal of the Door Support Arm, Door Buffer and Door Stay Mechanism. Removal of the Upper and Lower Guide Arms and the Guide Arm Hinge-Fittings. Installation of the Door Support Arm, Door buffer and Door Stay Mechanism. Installation of the Upper and Lower Guide Arms and the Guide Arm Hinge-Fittings. Removal of the Emergency Escape Slide Release Mechanism- FWD Passenger/Crew Door (831) (841) Installation of the Emergency Escape Slide MechanismFWD Passenger/Crew Door (831) (841) Removal of the Forward Passenger/Crew Door Latch and Stop Fittings Installation of the Forward Passenger/Crew Door Latch and Stop Fittings Functional Test of the MID Passenger/Crew Door (Door 2L/2R)
EFF : ALL 05-51-29 SROS
Page 602 Oct 01/03
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R
52-12-00-820-801 52-12-12-000-801
R 52-12-12-400-801 R 52-12-21-000-801 R 52-12-21-400-801 R 52-12-22-000-801 R 52-12-22-400-801 R R R
52-12-31-000-801 52-12-31-400-801
R R R R R
52-13-00-720-801 52-13-00-820-801 52-13-12-000-801
R 52-13-12-400-801 R 52-13-21-000-801 R 52-13-21-400-801 R 52-13-22-000-801 R 52-13-22-400-801 R R R
52-13-31-000-801 52-13-31-400-801
R SRM
Adjustment of the MID Passenger/Crew Door (Door 2L/2R) Removal of the Suspension of the MID Passenger/Crew Door (Door 2L/2R) Installation of the Suspension of the MID Passenger/Crew Door (Door 2L/2R) Removal of the Door Locking Mechanism from the MID Passenger/Crew Door (Door 2L/2R) Installation of the Door Locking Mechanism in the MID Passenger/Crew Door (Door 2L/2R) Removal of the Emergency Escape-Slide Release-Mechanism from the MID Passenger/Crew Door (Door 2L/2R) Installation of the Emergency Escape-Slide Release-Mechanism in the MID Passenger/Crew Door (Door 2L/2R) Removal of the Door, Latch and Stop Fittings (Door 2L/2R) Installation of the Door, Latch and Stop Fittings (Door 2L/2R) Functional Test of the AFT Passenger/Crew Door (Door 4L/4R) Adjustment of the AFT Passenger/Crew Door (Door 4L/4R) Removal of the Suspension of the AFT Passenger/Crew Door (Door 4L/4R) Installation of the Suspension of the AFT Passenger/Crew Door (Door 4L/4R) Removal of the Door Locking Mechanism from the AFT Passenger/Crew Door (Door 4L/4R) Installation of the Door Locking Mechanism in the AFT Passenger/Crew Door (Door 4L/4R) Removal of the Emergency Escape-Slide Release-Mechanism from the AFT Passenger/Crew Door (Door 4L/4R) Installation of the Emergency Escape-Slide Release-Mechanism in the AFT Passenger/Crew Door (Door 4L/4R) Removal of the Door Latch and Stop Fittings (Door 4L/4R) Installation of the Door Latch and Stop Fittings (Door 4L/4R)
521000
EFF : ALL 05-51-29 SROS
Page 603 Oct 01/03
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------SRM 530000 05-51-29-991-001 05-51-29-991-002 05-51-29-991-003
Fig. 601 Fig. 602 Fig. 603
3. __________ Job Set-up Subtask 05-51-29-010-050 A. Get Access (1) Energize the aircraft electrical circuits (Ref. TASK 24-42-00-861-801). (2) Put an adjustable access platform in position at the doors 831, 841, 832, 842, 833, 843. (3) Open the passenger/crew doors 831, 841, 832, 842, 833, 843, (Ref. TASK 52-10-00-010-801). Subtask 05-51-29-010-051 B. Get Access to the Avionics Compartment (1) Open the access door 211FF. (2) Set the AVNCS LT switch 1LS to ON. Subtask 05-51-29-865-050 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU DOORS & SLIDES CTL 3MJ N09 722VU DOORS & SLIDES CTL 2MJ P41
EFF : ALL 05-51-29 R SROS
Page 604 Oct 01/03
Subtask 05-51-29-860-050 D. Aircraft Maintenance Configuration (1) Observe the special precautions before you start work on the door (Ref. TASK 52-10-00-860-801). (2) Remove the escape slide/raft container (Ref. TASK 25-62-41-000-801). (3) Remove the door frame linings (Ref. TASK 25-23-45-000-801), (Ref. TASK 25-23-46-000-801), (Ref. TASK 25-23-47-000-801). (4) Remove the door lining and insulation (Ref. TASK 25-23-49-000-801), (Ref. TASK 25-23-51-000-801), (Ref. TASK 25-23-52-000-802). (5) Install the SUPPORT FRAME - BALLAST WEIGHT, DOORS (98A52108008001) together with the BALLAST WEIGHT - SLIDE RAFT (98F52108431000) to replace the escape slide and the lining.
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4. Procedure _________ Subtask 05-51-29-210-050 A. Inspection of the Doors (Ref. TASK 52-11-12-000-801), (Ref. TASK 52-1112-400-801) (Ref. TASK 52-11-12-000-802), (Ref. TASK 52-11-12-400-802), (Ref. TASK 52-12-12-000-801), (Ref. TASK 52-12-12-400-801), (Ref. TASK 52-13-12-000801), (Ref. TASK 52-13-12-400-801). (Ref. TASK 52-11-22-000-801) (Ref. TASK 52-11-22-400-801) (Ref. TASK 5212-22-000-801), (Ref. TASK 52-12-22-400-801), (Ref. TASK 52-13-22-000801), (Ref. TASK 52-13-22-400-801). (Ref. TASK 52-12-21-000-801), (Ref. TASK 52-12-21-400-801), (Ref. TASK 52-13-21-000-801), (Ref. TASK 52-13-21-400-801), (Ref. TASK 52-11-31-000801), (Ref. TASK 52-11-31-400-801). (Ref. TASK 52-12-31-000-801), (Ref. TASK 52-12-31-400-801), (Ref. TASK 52-13-31-000-801), (Ref. TASK 52-13-31-400-801), (Ref. SRM 521000), (Ref. SRM 530000). (Ref. Fig. 601/TASK 05-51-29-991-001, 602/TASK 05-51-29-991-002, 603/TASK 05-51-29-991-003) NOTE : All the necessary inspections are visual unless specified ____ differently in the text. Operators can refer to the Non-destructive Testing Manual (NTM) and use non-destructive test procedures.
EFF : ALL 05-51-29 SROS
Page 605 Oct 01/03
Fwd Passenger/Crew Doors Figure 601/TASK 05-51-29-991-001 EFF : ALL 05-51-29 SROS
Page 606 Apr 01/98
Mid Passenger/Crew Doors Figure 602/TASK 05-51-29-991-002 EFF : ALL 05-51-29 SROS
Page 607 Apr 01/98
Aft Passenger/Crew Doors Figure 603/TASK 05-51-29-991-003 EFF : ALL 05-51-29 SROS
Page 608 Apr 01/98
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Pax/Crew Door Open | | | | | | | | | (Ref. Fig. 601/TASK 05-51-29-991-001) | | | | | | | | | (Ref. Fig. 602/TASK 05-51-29-991-002) | | | | | | | | | (Ref. Fig. 603/TASK 05-51-29-991-003) | | | | | | | A.| | Examine the door skin, door structure | X | | | | | | | | and the fuselage structure for | | | | | | | | | distortion, cracks, tears and loose or| | | | | | | | | missing rivets. | | | | | | | | | If you find damage: | | X | | | | | | | (1) Do a structural repair at the | | | | | | | | | door and (or) the fuselage | | | | | | | | | structure | | | | | | | | | (Ref. SRM 52-10-00). | | | | | | | | | | | | | | | | B.| | Examine the door suspension for | X | | | | | | | | damage. | | | | | | | | | If you find damage: | | X | | | | | | | (1) Remove the damaged components | | | | | | | | | (Ref. TASK 52-11-12-000-801) | | | | | | | | | (Ref. TASK 52-11-12-000-802) | | | | | | | | | (Ref. TASK 52-12-12-000-801) | | | | | | | | | (Ref. TASK 52-13-12-000-801) | | | | | | | | | and install a new component | | | | | | | | | (Ref. TASK 52-11-12-400-801) | | | | | | | | | (Ref. TASK 52-11-12-400-802) | | | | | | | | | (Ref. TASK 52-12-12-400-801) | | | | | | | | | (Ref. TASK 52-13-12-400-801). | | | | | | | | | | | | | | | |2. | | Inspection of the Pax/Crew Door in | | | | | | | | | the Up and Closed Position | | | | | | | | | | | | | | | | A.| | Examine the door skin, door structure | X | | | | | | | | and the fuselage structure for | | | | | | | | | distortion, cracks, tears and loose or| | | | | | | | | missing rivets. | | | | | | | | | If you find damage: | | X | | | | | | | (1) Do a structural repair of the | | | | | | | | | door and (or) the fuselage | | | | | | | | | structure | | | | | | | | | (Ref. SRM 52-10-00) | | | | | | | | | (Ref. SRM 53-00-00). | | | | | | | | | | | | | | | | B.| | Examine the locking mechanism for | X | | | | |
EFF : ALL 05-51-29 R SROS
Page 609 Oct 01/03
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | damage. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the damaged component | | X | | | | | | | (Ref. TASK 52-12-21-000-801) | | | | | | | | | (Ref. TASK 52-13-21-000-801) | | | | | | | | | and install a new component | | | | | | | | | (Ref. TASK 52-12-21-400-801) | | | | | | | | | (Ref. TASK 52-13-21-400-801). | | | | | | | | | | | | | | | | C.| | Examine the emergency escape slide | X | | | | | | | | release mechanism for damage. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the damaged component | | X | | | | | | | (Ref. TASK 52-11-22-000-801) | | | | | | | | | (Ref. TASK 52-12-22-000-801) | | | | | | | | | (Ref. TASK 52-13-22-000-801) | | | | | | | | | and install a new component | | | | | | | | | (Ref. TASK 52-11-22-400-801) | | | | | | | | | (Ref. TASK 52-12-22-400-801) | | | | | | | | | (Ref. TASK 52-13-22-400-801). | | | | | | | | | | | | | | | | D.| | Examine the door support mechanism | X | | | | | | | | for damage. | | | | | | | | | If you find damage: | X | | | | | | | | (1) Remove the damaged component | | | | | | | | | (Ref. TASK 52-11-12-000-801) | | | | | | | | | (Ref. TASK 52-12-12-000-801) | | | | | | | | | (Ref. TASK 52-13-12-000-801) | | | | | | | | | and install a new component | | | | | | | | | (Ref. TASK 52-11-12-400-801) | | | | | | | | | (Ref. TASK 52-12-12-400-801) | | | | | | | | | (Ref. TASK 52-13-12-400-801). | | | | | | | | | | | | | | | | E.| | Examine the fittings for damage. | X | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the damaged component | | | | | | | | | (Ref. TASK 52-11-31-000-801) | | | | | | | | | (Ref. TASK 52-12-31-000-801) | | | | | | | | | (Ref. TASK 52-13-31-000-801) | | | | | | | | | and install a new component | | | | | | | | | (Ref. TASK 52-11-31-400-801) | | | | | | | | | (Ref. TASK 52-12-31-400-801) | | | | | | | | | (Ref. TASK 52-13-31-400-801). | | | | | |
EFF : ALL 05-51-29 R SROS
Page 610 Oct 01/03
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| ------------------------------------------------------------------------------Subtask 05-51-29-710-050 B. Adjustment/Test of the Doors (Ref. TASK 52-12-00-720-801) (Ref. TASK 5212-00-820-801) (Ref. TASK 52-13-00-720-801) (Ref. TASK 52-13-00-820-801) (1) Make sure that the work area is clean and clear of tools and other items. (2) Do the test below: ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Do the adjustment/test of the pax/crew| | X | | | | | | | door | | | | | | | | | (Ref. TASK 52-12-00-720-801) | | | | | | | | | (Ref. TASK 52-12-00-820-801) | | | | | | | | | (Ref. TASK 52-13-00-720-801) | | | | | | | | | (Ref. TASK 52-13-00-820-801). | | | | | | ------------------------------------------------------------------------------5. Close-up ________ Subtask 05-51-29-860-051 A. Put the Aircraft back to its Initial Configuration R
(1) Remove the BALLAST WEIGHT - SLIDE RAFT (98F52108431000) and the SUPPORT FRAME - BALLAST WEIGHT, DOORS (98A52108008001). (2) Install the door lining and insulation (Ref. TASK 25-23-49-400-801), (Ref. TASK 25-23-51-400-801), (Ref. TASK 25-23-52-400-802). (3) Install the door frame linings (Ref. TASK 25-23-45-400-801), (Ref. TASK 25-23-46-400-801), (Ref. TASK 25-23-47-400-801). (4) Install the escape slide (escape slide raft) container (Ref. TASK 2562-41-400-801).
EFF : ALL 05-51-29 SROS
Page 611 Oct 01/03
(5) Observe the special precautions after work on the door (Ref. TASK 5210-00-860-802). Subtask 05-51-29-865-051 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 2MJ, 3MJ Subtask 05-51-29-862-050 C. De-energize the ground service network (Ref. TASK 24-42-00-862-801). Subtask 05-51-29-942-050 D. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Set the AVNCS LT switch 1LS to off. (3) Close the access door 211FF. (4) Close the passenger/crew doors. (Ref. TASK 52-10-00-410-801) (5) Remove the access platform(s).
EFF : ALL 05-51-29 R SROS
Page 612 Oct 01/03
______________________________________________________________________ INSPECTION AFTER ENGINE WINDMILLING (AFTER ENGINE IN-FLIGHT SHUT-DOWN) ________________ INSPECTION/CHECK TASK 05-51-34-200-802 Inspection after Engine Windmilling (after Engine In-Flight Shut-Down) 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------71-00-00-200-812 72-00-00-200-810
Examine the Power Plant after it has been stopped in Flight Inspection After Windmilling
3. __________ Job Set-up Subtask 05-51-34-860-051 A. Not applicable. 4. Procedure _________ R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-34-210-051 A. Do the inspection after windmilling (Ref. TASK 72-00-00-200-810) **ON A/C 701-749, Subtask 05-51-34-210-051-A A. Do the procedure to examine the power plant after it has been stopped in flight (Ref. TASK 71-00-00-200-812)
EFF : ALL 05-51-34 SROS
Page 601 Jul 01/05
INSPECTION AFTER VERY HIGH WINDS ON GROUND - INSPECTION/CHECK _____________________________________________________________ TASK 05-51-42-200-801 Inspection after Very High Winds on Ground WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A _______ FALL CAN KILL OR INJURE YOU. 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
warning notices adjustable access platform 11 m (36 ft. 1 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-862-801 27-24-00-710-802 27-34-00-710-801 27-50-00-866-801 27-54-00-710-801 27-60-00-866-801 27-64-00-710-801
De-energize the Aircraft Electrical Circuits from the External Power A Operational Test of the Rudder Hydraulic Actuation Operational Test of the Elevator and Hydraulic Actuation Extension of the Flaps on the Ground Operational Test of the Flap System Extension of the Spoilers for Maintenance Operational Test of the Spoilers
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
27-80-00-866-801 27-80-00-866-801 27-84-00-710-801 29-00-00-864-804 32-00-00-481-801 32-12-00-010-801 32-12-00-410-801 32-22-00-010-801 32-22-00-410-801 55-16-00-200-803 55-26-00-200-801 55-26-00-200-802 55-30-00-210-806
Extension of the Slats on the Ground Extension of the Slats on the Ground Operational Test of the Slat System 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 Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance Detailed Inspection of Horizontal Stabilizer Hinge Fittings No 1, 4, 5, 6 and 7 and Support Ribs Detailed Inspection of Elevator Hinge Fittings No 2 and 3 and Actuator Fittings, LH and RH Detailed Inspection of Elevator Hinge Fittings No 1, 4, 5, 6 and 7 Detailed Visual Inspection of the Rudder Hinge Arms and Actuator Support Fittings
3. __________ Job Set-up Subtask 05-51-42-941-050 A. General (1) You must do this inspection if the aircraft was in very high winds on the ground (wind speed of more than 80 knots (150 KM/H)). NOTE : This procedure is for an aircraft that was in the moored ____ configuration before it was in very high winds. Subtask 05-51-42-481-050 B. Safety Precautions Make sure that the safety devices are installed on the landing gears (Ref. TASK 32-00-00-481-801).
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R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-42-866-050 C. Extension of the Flight Control Surfaces (1) Extend the flaps (Ref. TASK 27-50-00-866-801). (2) Extend the slats (Ref. TASK 27-80-00-866-801). (3) Extend the spoilers (Ref. TASK 27-60-00-866-801).
R
**ON A/C 701-749,
R
Subtask 05-51-42-866-050-A
R
C. Extension of the Flight Control Surfaces
R
(1) Extend the flaps (Ref. TASK 27-50-00-866-801).
R
(2) Extend the slats (Ref. TASK 27-80-00-866-801).
R
(3) Extend the spoilers (Ref. TASK 27-60-00-866-801).
R
**ON A/C ALL Subtask 05-51-42-010-050 D. Get Access (1) Open the main gear doors and install the safety devices (Ref. TASK 32-12-00-010-801). (2) Open the nose gear doors and install the safety devices (Ref. TASK 32-22-00-010-801). Subtask 05-51-42-860-050 E. Aircraft Maintenance Configuration (1) Make sure that the electrical circuits are de-energized (Ref. TASK 24-41-00-862-801). (2) Make sure that the hydraulic systems are depressurized (Ref. TASK 2900-00-864-804). (3) Put warning notices in the cockpit to tell persons not to operate the flight control surfaces.
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Page 603 Jan 01/07
(4) Put the adjustable access platform in position near the area you must examine. 4. Procedure _________ Subtask 05-51-42-210-050 A. General External Inspection ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | General External Inspection | | | | | | | | | | | | | | | | A.| | Do a general visual inspection of the | X | | | | | | | | aircraft from the ground for | | | | | | | | | distortion, damage and fluid leakage | | | | | | ------------------------------------------------------------------------------Subtask 05-51-42-210-051 B. Inspection of the Landing Gear ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Landing Gear | | | | | | | | | | | | | | | | A.| | Nose Landing Gear | | | | | | | | | | | | | | | | | | (1) Examine the NLG, its attachment | X | | | | | | | | fittings on the structure and all | | | | | | | | | the components installed on the | | | | | | | | | NLG for: | | | | | | | | | - distortion, | | | | | | | | | - leakage, | | | | | | | | | - defective attachment, | | | | | | | | | - other damage. | | | | | | | | | NOTE: Carefully examine the | | | | | | | | | hydraulic and electrical | | | | | | | | | connections and the mooring | | | | | | | | | fitting. | | | | | | | | | | | | | | | | B.| | Main Landing Gear | | | | | | | | | | | | | | | | | | (1) Examine the MLG, its attachment | X | | | | | | | | fittings on structure, the side | | | | | | | | | stay, the forward and aft pintle | | | | | |
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | fittings and all the components | | | | | | | | | installed on the MLG for: | | | | | | | | | - distortion, | | | | | | | | | - leakage, | | | | | | | | | - defective attachment, | | | | | | | | | - other damage. | | | | | | | | | NOTE: Carefully examine the | | | | | | | | | hydraulic and electrical | | | | | | | | | connections. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-42-210-052
R
C. Inspection (Ref. TASK (Ref. TASK (Ref. TASK (Ref. TASK
of the Flight Control Surfaces (Ref. TASK 55-16-00-200-803) 55-26-00-200-801) (Ref. TASK 55-26-00-200-802) 55-30-00-210-806) (Ref. TASK 27-24-00-710-802) 27-34-00-710-801) (Ref. TASK 27-54-00-710-801) 27-64-00-710-801) (Ref. TASK 27-84-00-710-801)
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Flight Control | | | | | | | | | Surfaces | | | | | | | | | | | | | | | | A.| | Rudder | | | | | | | | | | | | | | | | | | (1) Examine the rudder external | X | | | | | | | | surface for distortion and damage | | | | | | | | | | | | | | | | | | (2) Do a detailed visual inspection | X | | | | | | | | (Ref. TASK 55-30-00-210-806) | | | | | | | | | of the actuator fittings 1, 2 and | | | | | | | | | 3 at: | | | | | | | | | - the vertical stabilizer | | | | | | | | | center-box, | | | | | | | | | - the rudder front spar. | | | | | | | | | NOTE: Carefully examine the | | | | | | | | | actuator fitting lugs and | | | | | | | | | the areas of the fitting | | | | | | | | | around the fasteners. | | | | | | | | | | | | | | |
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | B.| | Elevators | | | | | | | | | | | | | | | | | | (1) Examine the elevator external | X | | | | | | | | surface for distortion and damage | | | | | | | | | | | | | | | | | | (2) Do a detailed visual inspection | X | | | | | | | | (Ref. TASK 55-16-00-200-803) | | | | | | | | | (Ref. TASK 55-26-00-200-801) | | | | | | | | | (Ref. TASK 55-26-00-200-802) of | | | | | | | | | these parts in the actuator areas:| | | | | | | | | - the actuator fittings 1 and 2 | | | | | | | | | and their attachments, | | | | | | | | | - the hinge fittings 2, 3 and 4 | | | | | | | | | and their attachments, | | | | | | | | | - the hinge arms 2, 3 and 4 and | | | | | | | | | their attachments | | | | | | | | | at the horizontal stabilizer | | | | | | | | | rear-spar and at the elevator | | | | | | | | | front spar. | | | | | | | | | | | | | | | | C.| | Flaps | | | | | | | | | | | | | | | | | | (1) Do a general visual inspection of | X | | | | | | | | each control surface and its | | | | | | | | | attachments for distortion and | | | | | | | | | damage. | | | | | | | | | | | | | | | | | | (2) Do a visual inspection of: | X | | | | | | | | - the flap track fairings, | | | | | | | | | for distortion and damage. | | | | | | | | | | | | | | | | | | (1) Examine the external surface and | X | | | | | | | | the attachments of each control | | | | | | | | | surface for distortion and damage.| | | | | | | | | | | | | | | |2. | | Operational Test of the Flight Control| | | | | | | | | Surfaces | | | | | | | | | | | | | | | | A.| | Make sure that the work area is clean | X | | | | | | | | and clear of tool(s) and other items. | | | | | | | | | | | | | | | | B.| | Do an operational test of each control| X | | | | | | | | surface and make sure that the related| | | | | |
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | surface(s) move(s) smoothly and freely| | | | | | | | | | | | | | | | | | (1) For the rudder: | | | | | | | | | (Ref. TASK 27-24-00-710-802) | | | | | | | | | | | | | | | | | | (2) For the elevators: | | | | | | | | | (Ref. TASK 27-34-00-710-801) | | | | | | | | | | | | | | | | | | (3) For the flaps: | | | | | | | | | (Ref. TASK 27-54-00-710-801) | | | | | | | | | | | | | | | | | | (4) For the slats: | | | | | | | | | (Ref. TASK 27-84-00-710-801) | | | | | | | | | | | | | | | | | | (5) For the spoilers: | | | | | | | | | (Ref. TASK 27-64-00-710-801) | | | | | | ------------------------------------------------------------------------------5. Close-up ________ Subtask 05-51-42-410-050 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the nose gear doors (Ref. TASK 32-22-00-410-801). (3) Close the main gear doors (Ref. TASK 32-12-00-410-801). (4) Remove the access platform(s). (5) Remove the warning notice(s).
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INSPECTIONS AFTER WORK ON SYSTEM ELECTRICAL INSTALLATION - ADJUSTMENT/TEST __________________________________________________________________________ TASK 05-51-43-700-801 Inspection after Work on System Electrical Installation 1. __________________ Reason for the Job R
To give the list of all the inspections to do after work on the aircraft electrical installation (wiring, connectors, etc.). The purpose of this integrity inspection is not to do a check of all the aircraft functions but to make sure that: - basic functions of the aircraft systems operate correctly - there are no unwanted effects on the main functions of systems not directly related to the work done. 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------22-10-00-710-803 22-30-00-710-801 22-96-00-740-801 22-97-00-740-801 24-00-00-710-801 24-24-00-710-801 24-29-00-740-801 24-38-00-740-801 24-41-00-740-803 24-41-00-861-801 26-12-00-710-812 27-54-00-710-802 27-96-00-710-818 29-00-00-710-802 34-13-00-710-803 34-13-00-740-801 34-13-00-740-802 34-13-00-740-803
Operational Test of Autopilot Engagement and Locking Devices of The Side Stick Controller and Rudder Pedals Operational Test of the Autothrust Isolation from Engine Control BITE Test of the Auto Flight System (SYSTEM TEST) Test of the LAND CAT III Capability Integrity Test of the Electrical Power Operational Test of the Emergency Generation System BITE Test of the ECMU (1XM1, 1XM2) BITE Test of the BCL (1PB1, 1PB2, 1PB3) Ground Report of the EPGS Energize the Aircraft Electrical Circuits from the External Power A Operational Test of the Engine Fire and Overheat Detection (Loop/Squib) Operational Test of the Flap and Slat System Integrity Test of the Flight Control System Integrity Test of the Hydraulic Power AOA SENSOR TEST INTERFACE TEST of the ADR Read the CMC for the ADR CURRENT STATUS SYSTEM TEST of the ADR
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------34-13-00-740-804 34-14-00-740-801 34-14-00-740-802 34-14-00-740-803 34-14-00-740-804 71-00-00-720-817 71-00-00-720-827 73-21-00-710-803 73-21-00-710-812 73-25-34-740-820 73-25-34-740-823 74-00-00-710-803 74-00-00-710-804 78-31-00-710-804 78-31-00-740-802
Read the CMC for the ADR INPUT STATUS INTERFACE TEST of the IR Read the CMC for the IR CURRENT STATUS SYSTEM TEST of the IR Read the CMC for the IR INPUT STATUS Test No. 2A - Engine Motor Leak Test (Wet Method) Thrust Reverser Cowl Doors Open Wet Motoring Engine Full Authority Digital Engine Control (FADEC) System Static Test Test of the FADEC System Bite Test of the EIVMU BITE Test of the EIVMU Operational Test of the Ignition System (Audible Check) Audible Test of the Igniters Thrust Reverser Cycling Test (MCDU) Test of the Thrust Reverser Deployment and Stowage (Engine not Running)
3. __________ Job Set-up Subtask 05-51-43-200-050 A. Not applicable. 4. Procedure _________ Subtask 05-51-43-710-050 R
A. Inspections of the basic Functions of the Aircraft Systems
R R
(1) Do these inspections to make sure that the basic functions of the auto flight system operate correctly: (a) Operational test of autopilot engagement and locking devices of the side stick controller and rudder (Ref. TASK 22-10-00-710803). (b) Operational test of the autothrust isolation from engine control (Ref. TASK 22-30-00-710-801).
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Page 502 Oct 01/04
(c) BITE test of the auto flight system (SYSTEM TEST) (Ref. TASK 2296-00-740-801). (d) Test of the LAND CAT III capability (Ref. TASK 22-97-00-740-801). R R
(2) Do these inspections to make sure that the basic functions of the electrical power system operate correctly: (a) Integrity test of the electrical power (Ref. TASK 24-00-00-710801). (b) Operational test of the emergency generation system (Ref. TASK 24-24-00-710-801). (c) BITE test of the ECMU (1XM1, 1XM2) (Ref. TASK 24-29-00-740-801). (d) BITE test of the BCL (1PB1, 1PB2, 1PB3) (Ref. TASK 24-38-00-740801). (e) Ground report of the EPGS (Ref. TASK 24-41-00-740-803). (f) Energize the aircraft electrical circuits from the external power A (Ref. TASK 24-41-00-861-801).
R R
(3) Do this inspection to make sure that the basic functions of the fire protection system operate correctly: (a) Operational test of the engine fire and overheat detection (Loop/Squib) (Ref. TASK 26-12-00-710-812).
R R
(4) Do these inspections to make sure that the basic functions of the flight controls system operate correctly: (a) Integrity test of the flight control system (Ref. TASK 27-96-00710-818). (b) Operational test of the flap and slat system (Ref. TASK 27-54-00710-802).
R R
(5) Do this inspection to make sure that the basic functions of the hydraulic power operate correctly: (a) Integrity test of the hydraulic power (Ref. TASK 29-00-00-710802).
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(6) Do these inspections to make sure that the basic functions of the navigation system operate correctly: (a) AOA sensor test (Ref. TASK 34-13-00-710-803). (b) Interface test of the ADR (Ref. TASK 34-13-00-740-801). (c) Read the CMC for the ADR CURRENT STATUS (for Litton ADIRU) (Ref. TASK 34-13-00-740-802). (d) System test of the ADR (Ref. TASK 34-13-00-740-803). (e) Read the CMC for the ADR INPUT STATUS (for Honeywell ADIRU) (Ref. TASK 34-13-00-740-804). (f) Interface test of the IR (Ref. TASK 34-14-00-740-801). (g) Read the CMC for the IR CURRENT STATUS (for Litton ADIRU) (Ref. TASK 34-14-00-740-802). (h) System test of the IR (Ref. TASK 34-14-00-740-803). (i) Read the CMC for the IR INPUT STATUS (for Honeywell ADIRU) (Ref. TASK 34-14-00-740-804). R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-43-710-051 B. Inspections of the basic Engine Functions (1) Thrust reverser cycling test (MCDU) (Ref. TASK 78-31-00-710-804). (2) Operational test of the ignition system (Audible Check) (Ref. TASK 74-00-00-710-803). (3) Engine motor leak test (Wet Method) - Thrust reverser cowl doors open (Ref. TASK 71-00-00-720-817). (4) BITE test of the EIVMU (Ref. TASK 73-25-34-740-823). (5) Full Authority Digital Engine Control (FADEC) system static test (Ref. TASK 73-21-00-710-803).
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**ON A/C 701-749, Subtask 05-51-43-710-051-A R
B. Inspections of the basic Engine Functions (1) Test of the thrust reverser deployment and stowage (engine not running) (Ref. TASK 78-31-00-740-802). (2) Audible test of the igniters (Ref. TASK 74-00-00-710-804). (3) Wet motoring engine (Ref. TASK 71-00-00-720-827). (4) BITE test of the EIVMU (Ref. TASK 73-25-34-740-820). (5) Test of the FADEC system (Ref. TASK 73-21-00-710-812).
EFF : 701-749, 05-51-43 SROS
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INSPECTION AFTER FLIGHT WITH HIGH LATERAL LOADS - INSPECTION/CHECK __________________________________________________________________ TASK 05-51-44-200-801 INSPECTION AFTER FLIGHT WITH HIGH LATERAL LOADS 1. __________________ Reason for the Job To do an inspection of the aircraft for structural damage after a flight during which high lateral loads occurred. NOTE : Typical examples of conditions that can cause high lateral load ____ factors are: - loss of control involving yaw and/or roll maneuvers, - severe turbulence with A.P. disconnection or in manual mode, - system failures such as rudder trim runaway with crew take over, - etc. NOTE : If the lateral acceleration occurred when the aircraft was on the ____ ground (landing, taxiing, etc.), it is not necessary to do this procedure. To know if the inspection is necessary, refer to Para. 3.A. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No
specific specific specific specific
safety barriers warning notices wheel chocks 1 ACCESS PLATFORM 17M (56 FT) - ADJUSTABLE
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B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------05-23-20-200-804 05-51-17-200-801 24-41-00-861-801 24-41-00-862-801 27-14-00-710-801 27-14-00-820-801 27-24-00-710-801 27-34-00-710-801 27-50-00-866-801 27-54-00-710-801 27-64-00-710-801 27-84-00-710-801 28-25-00-650-803 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 32-00-00-481-801 32-12-00-010-801 32-12-00-410-801 53-15-11-010-801 53-15-11-400-801 53-15-11-700-801 55-34-11-000-801 55-34-11-400-801 71-00-51-000-801
Zonal Inspection of Vertical Stabilizer Spar Box Inspection after Flight in Excessive Turbulence or in Excess of VMO/MMO Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Operational Test of the Aileron and Hydraulic Actuation Adjustment of the Aileron Operational Test of the Rudder Servo Control with each Hydraulic System Operational Test of the Elevator and Hydraulic Actuation Extension of the Flaps on the Ground Operational Test of the Flap System Operational Test of the Spoilers Operational Test of the Slat System To Drain the Remaining Fuel (Wing Tanks) 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) Installation of the Safety Devices on the Landing Gears Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Opening of the Radome Installation of the Radome Tap Test of the Radome Removal of the Vertical Stabilizer Tip Installation of the Vertical Stabilizer Tip Removal of the Demountable Power Plant
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------71-13-00-010-802 71-13-00-010-805 71-13-00-410-802 71-13-00-410-805 78-30-00-010-801 78-30-00-010-803 78-30-00-410-801 78-30-00-410-803 78-31-00-710-804 78-31-00-740-802 05-51-44-991-001 05-51-44-991-002 05-51-44-991-003
Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Open the Fan Cowl Doors Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Close the Fan Cowl Doors Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Open the Thrust Reverser Cowl Doors Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Close the Thrust Reverser Cowl Doors Thrust Reverser Cycling Test (MCDU) Test of the Thrust Reverser Deployment and Stowage (Engine not Running) Fig. 601 Fig. 602 Fig. 603
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 05-51-44-991-004
Fig. 604
**ON A/C 701-749, 05-51-44-991-004-A
Fig. 604A
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 05-51-44-991-006
Fig. 605
**ON A/C 701-749, 05-51-44-991-006-A
Fig. 605A
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 05-51-44-991-008
Fig. 606
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------**ON A/C 701-749, 05-51-44-991-008-A
Fig. 606A
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 05-51-44-991-009
Fig. 607
**ON A/C 701-749, 05-51-44-991-009-A
Fig. 607A
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 05-51-44-991-010
Fig. 608
**ON A/C 701-749, 05-51-44-991-010-A
Fig. 608A
**ON A/C ALL 3. __________ Job Set-up Subtask 05-51-44-210-052 A. Inspection Requirements (1) Definitions If there is a flight crew report of high lateral acceleration, you must get the data from the DFDR or any other device available to know the lateral load factor before the aircraft is released for flight. NOTE : If excessive turbulence caused the high vertical lateral ____ loads, it is possible that there were also high vertical loads. For high vertical loads, do the inspection after Flight
EFF : ALL 05-51-44 SROS
Page 604 Jul 01/06
in Excessive Turbulence or in Excess of VMO/MMO (Ref. TASK 0551-17-200-801). NOTE : If there is a flight crew report of high lateral acceleration ____ and if the data from the DFDR or any other device available cannot be used to know the lateral load factor, contact AIRBUS before the subsequent flight for more information. (2) Confirmation that inspection is necessary: (a) If the value of the lateral load factor is less than 0.28 g on the two sides of the aircraft: - this inspection is not necessary and the aircraft can return to service. (b) If the value of the lateral load factor is equal to or more than 0.28 g but less than 0.33 g: - do the inspection given in Para. 4. of this procedure, - send the DFDR recording (or equivalent) for the section of the flight during which the event occurred to AIRBUS for analysis. NOTE : Until the results of the AIRBUS analysis are available and ____ on the condition that no damage is found during the visual inspection given in Para. 4., the aircraft can return to service for a period of 30 days/100 Flight Cycles maximum (the one that occurs first). AIRBUS will make an analysis of the event for final clearance or more instructions. (c) If the value of the lateral load factor is equal to or more than 0.33 g: - the aircraft is not permitted to return to flight, - do the inspection given in Para. 4. of this procedure, - send the DFDR recording (or equivalent) for the section of the flight during which the event occurred to AIRBUS for analysis, - get instructions from AIRBUS for preparation of the aircraft for detailed information, - AIRBUS will make an analysis of the event to find if the aircraft can return to service. (3) Inspection Preparation NOTE : All inspections are visual unless specified differently in the ____ text. Operators can refer to the non-destructive testing manual (NTM) and use non-destructive test procedures.
EFF : ALL 05-51-44 SROS
Page 605 Jul 01/06
Subtask 05-51-44-941-050 B. Safety Precautions (1) Put the safety barriers in position. (2) Put the wheel chocks in position at the main landing gear. (3) Put warning notices in position in the cockpit to tell persons not to operate the systems. **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-44-010-050 C. Get Access (1) Open the main-landing-gear doors (Ref. TASK 32-12-00-010-801). (2) Put an ACCESS PLATFORM 17M (56 FT) - ADJUSTABLE in position near the area you must examine. (3) Install the safety devices on the landing gears (Ref. TASK 32-00-00481-801). (4) Open the fan cowl doors (Ref. TASK 71-13-00-010-802): FOR 4030EM1 415BL, 416BR FOR 4030EM2 425BL, 426BR (5) Open the thrust reverser doors (Ref. TASK 78-30-00-010-801): FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR
EFF : ALL 05-51-44 SROS
Page 606 Jul 01/06
**ON A/C 701-749, Subtask 05-51-44-010-050-A C. Get Access (1) Open the main-landing-gear doors (Ref. TASK 32-12-00-010-801). (2) Put an ACCESS PLATFORM 17M (56 FT) - ADJUSTABLE in position near the area you must examine. (3) Install the safety devices on the landing gears (Ref. TASK 32-00-00481-801). (4) Open the fan cowl doors (Ref. TASK 71-13-00-010-805): FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR (5) Open the thrust reverser doors (Ref. TASK 78-30-00-010-803): FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR **ON A/C ALL Subtask 05-51-44-860-050 D. Aircraft Maintenance Configuration (1) Extend the flaps (Ref. TASK 27-50-00-866-801). (2) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (3) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803). (4) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802). (5) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
EFF : ALL 05-51-44 SROS
Page 607 Jul 01/06
4. Procedure _________ Subtask 05-51-44-210-051 A. Inspection of the Fuselage (Ref. Fig. 601/TASK 05-51-44-991-001, 602/TASK 05-51-44-991-002) (Ref. TASK 53-15-11-400-801), (Ref. TASK 53-15-11-010-801), (Ref. TASK 53-15-11-700-801), (Ref. TASK 05-51-17-200-801), (Ref. TASK 05-23-20-200804). ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Radome | | | | | | | | | | | | | | | | A.| | Examine the radome shell (Ref.TASK | | | | | | | | | 53-15-11-400-801) for: | | | | | | | | | - gap and mismatch. | X | | | | | | | | If out of tolerances: | | | | | | | | | Open the radome (Ref. TASK 53-15-11- | | | | | | | | | 010-801) and do a check of | | | | | | | | | the metallic parts and arrestor | | | | | | | | | pick-up fitting for: | | | | | | | | | - deformation, bending and twist. | | X | | | | | | | If you find a defect, replace the | | | | | | | | | defective part and do a check of the | | | | | | | | | metallic frame. | | | | | | | | | Do a tap test around fitting areas | | | | | | | | | (hinges and latches) | | | | | | | | | (Ref. TASK 53-15-11-700-801). | | | | | | | | | | | | | | | |2. | | Inspection of the FWD/AFT Fuselage | | | | | | | | | | | | | | | | A.| | Do the inspection after Flight in | X | | | | | | | | Excessive Turbulence or in Excess of | | | | | | | | | VMO/MMO (Ref. TASK 05-51-17-200-801) | | | | | | | | | and add these inspections: | | | | | | | | | | | | | | | | B.| | Examine the fuselage externally | | | | | | | | | between FR78 and FR80 above STGR25, | | | | | | | | | the skin panels, the splicing and the | | | | | | | | | rivets for: | | | | | | | | | - distortion, cracks, pulled or torn | X | | | | | | | | fasteners and damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | Examine the internal structure, the | | | | | |
EFF : ALL 05-51-44 SROS
Page 608 Jul 01/06
Center Fuselage Figure 601/TASK 05-51-44-991-001 EFF : ALL 05-51-44 SROS
Page 609 Jul 01/06
Rear Fuselage and Tail Section Figure 602/TASK 05-51-44-991-002 EFF : ALL 05-51-44 SROS
Page 610 Jul 01/06
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | stringers and the frames for: | | | | | | | | | - distortion, cracks, pulled or torn | | X | | | | | | | fasteners and damaged paintwork. | | | | | | | | | | | | | | | | C.| | Examine the fuselage internally | | | | | | | | | between FR83 to FR88 above STGR27 and | | | | | | | | | FR87 and FR91 at all areas for: | | | | | | | | | - distortion, cracks, pulled or torn | X | | | | | | | | fasteners and damaged paintwork. | | | | | | | | | | | | | | | | D.| | Do a detailed visual inspection of the| X | | | | | | | | fuselage external surface below the | | | | | | | | | fin-to-fuselage fairing, | | | | | | | | | fin-to-fuselage attach fittings | | | | | | | | | with side load fittings and lower | | | | | | | | | surface of the vertical RIB1 | | | | | | | | | (Ref. TASK 05-23-20-200-804). | | | | | | | | | | | | | | | |3. | | Inspection of the center fuselage | | | | | | | | | | | | | | | | A.| | Examine attachment of FR40 to skin | | | | | | | | | fuselage between STGR18 and STGR30 | | | | | | | | | for: | | | | | | | | | - damaged paintwork and damaged | X | | | | | | | | fasteners. | | | | | | | | | | | | | | | | B.| | At FR40, examine upper skin of wing | | | | | | | | | box attachment to STGR27 for: | | | | | | | | | - damaged fasteners. | X | | | | | | | | | | | | | | | C.| | Examine FR40 between upper skin of | | | | | | | | | wing box and STGR18 for: | | | | | | | | | - buckling, distortion and damaged | X | | | | | | | | fasteners. | | | | | | | | | | | | | | | | D.| | At aft FR40 area, examine joint | | | | | | | | | fitting of STGR41 to STGR44 for: | | | | | | | | | - damaged paintwork, damaged fasteners| X | | | | | | | | and cracks in flanges. | | | | | | | | | | | | | | | | E.| | Examine attachment of FR46 to FR53.2 | | | | | | | | | between STGR17 and STGR20 for: | | | | | | | | | - damaged fasteners. | X | | | | |
EFF : ALL 05-51-44 SROS
Page 611 Jul 01/06
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | | | | | | | | F.| | Examine lower fitting of forward | | | | | | | | | canted longeron attachment to FR47 | | | | | | | | | for: | | | | | | | | | - damaged fasteners. | X | | | | | | | | | | | | | | | G.| | Examine FR39.2 between STGR24 and | | | | | | | | | STGR26 above the floor, FR39.2 between| | | | | | | | | STGR26 and STGR28 below the floor, | | | | | | | | | FR47 between STGR20 and STGR24, FR48 | | | | | | | | | and FR49 between STGR18 and STGR21 | | | | | | | | | for: | | | | | | | | | - buckling, distortion and damaged | X | | | | | | | | fasteners. | | | | | | | | | | | | | | | | H.| | Examine stiffener at Y2565 below | | | | | | | | | lateral pressurized floor between FR48| | | | | | | | | and FR53.2 for: | | | | | | | | | - buckling, distortion and damaged | X | | | | | | | | fasteners. | | | | | | | | | | | | | | | | J.| | Examine attachment of FR49 and FR48 | | | | | | | | | mid frame to lateral pressurized floor| | | | | | | | | at Z-700 for: | | | | | | | | | - damaged fasteners and cracks in | X | | | | | | | | angles. | | | | | | | | | | | | | | | | K.| | Examine lateral FR52 in door stop | | | | | | | | | and fairing area for: | | | | | | | | | - damaged paintwork, damaged | X | | | | | | | | fasteners and cracks in flanges. | | | | | | | | | | | | | | | | L.| | Examine main longeron between FR52 | | | | | | | | | and FR53 for: | | | | | | | | | - buckling and distortion of web and | X | | | | | | | | flanges. | | | | | | | | | | | | | | | | M.| | Examine main longeron attachment to | | | | | | | | | aft extension longeron at Z-1080.2 | | | | | | | | | across FR53.2 for: | | | | | | | | | - damaged fasteners. | X | | | | | | | | | | | | | | | N.| | Examine Z-700 Horizontal Tee | | | | | |
EFF : ALL 05-51-44 SROS
Page 612 Jul 01/06
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | attachment to lateral pressurized | | | | | | | | | floor between FR53 and FR53.2 and | | | | | | | | | between FR48 and FR50 for: | | | | | | | | | - damaged fasteners. | X | | | | | | | | | | | | | | | P.| | Examine joint fitting of STGR28 | | | | | | | | | attachment to FR53.2 for: | | | | | | | | | - damaged fasteners. | X | | | | | | | | | | | | | | | Q.| | Examine lower skin of wing box | | | | | | | | | attachment to the keel beam fitting: | | | | | | | | | - damaged fasteners. | X | | | | | | | | | | | | | | | R.| | Examine lateral FR53.1 for: | | | | | | | | | - bolting paintwork, damaged | X | | | | | | | | fasteners and cracks. | | | | | | | | | | | | | | | | S.| | Examine external STGR31 attachment | | | | | | | | | to skin panel between FR53.2 and | | | | | | | | | FR53.4 for: | | | | | | | | | - damaged fasteners. | X | | | | | | | | | | | | | | | T.| | Examine attachment of FR53.3 to skin | | | | | | | | | fuselage between STGR30 and STGR35 | | | | | | | | | for: | | | | | | | | | - damaged fasteners. | X | | | | | | | | | | | | | | | U.| | Examine STGR26 between FR53.1 and | | | | | | | | | FR53.3, STGR28 between FR53.2 and | | | | | | | | | FR53.3, STGR30 between FR52 and FR53, | | | | | | | | | the panels, the web and the flange of | | | | | | | | | of the stringer and the stiffener for:| | | | | | | | | - buckling, distortion and damaged | X | | | | | | | | fasteners. | | | | | | -------------------------------------------------------------------------------
EFF : ALL 05-51-44 SROS
Page 613 Jul 01/06
Subtask 05-51-44-210-053 B. Inspection of the Vertical Stabilizer (Ref. TASK 05-51-17-200-801), (Ref. TASK 55-34-11-000-801), (Ref. TASK 55-34-11-400-801). ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Vertical Stabilizer | | | | | | | | | and Rudder | | | | | | | | | | | | | | | | A.| | Do the inspection after Flight in | X | | | | | | | | Excessive Turbulence or in Excess of | | | | | | | | | VMO/MMO (Ref. TASK 05-51-17-200-801) | | | | | | | | | and add these inspections: | | | | | | | | | | | | | | | | B.| | Do a detailed visual inspection of | | X | | | | | | | the Fin box RIB13. To do this, remove | | | | | | | | | the fin tip (access as per Ref TASk | | | | | | | | | 55-34-11-000-801), (installation | | | | | | | | | as per Ref. TASK 55-34-11-400-801). | | | | | | ------------------------------------------------------------------------------Subtask 05-51-44-210-054 C. Inspection of the Horizontal Stabilizer ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Trimmable Horizontal| | | | | | | | | Stabilizer (THS) and Elevator | | | | | | | | | | | | | | | | A.| | Do a general visual inspection of: | X | | | | | | | | - the upper and lower skins of the | | | | | | | | | THS center and lateral spar boxes, | | | | | | | | | - the front and rear spars of the THS | | | | | | | | | center and lateral spar boxes, | | | | | | | | | - the top and the bottom trailing | | | | | | | | | edges of the THS access panels, | | | | | | | | | - the THS leading-edge skin on the two| | | | | | | | | sides, | | | | | | | | | - the THS tip skin on the two sides, | | | | | | | | | - the lower and upper elevator skins | | | | | | | | | on the two sides, | | | | | |
EFF : ALL 05-51-44 SROS
Page 614 Jul 01/06
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - the elevator front spar on the two | | | | | | | | | sides. | | | | | | | | | | | | | | | | B.| | If you find damage on the skins of | | | | | | | | | the lateral boxes: | | | | | | | | | (1) Examine the inner side at the | | X | | | | | | | damage location to do a check of | | | | | | | | | STGR and rib conditions. | | | | | | | | | | | | | | | | C.| | Do a detailed visual inspection of: | X | | | | | | | | - the attachment areas, the screw | | | | | | | | | jacks, the two rear supports (and | | | | | | | | | the fittings) and the two side load | | | | | | | | | fittings (Rib 4 at rear spar) of the| | | | | | | | | THS, | | | | | | | | | - all hinge arms, actuator fittings, | | | | | | | | | elevator side-load fittings and | | | | | | | | | their attachments on the two sides, | | | | | | | | | - the skin joints between the THS | | | | | | | | | lateral and central spar boxes, | | | | | | | | | - the spar joints between the THS | | | | | | | | | lateral and central spar boxes, | | | | | | | | | - the THS trailing-edge ribs and | | | | | | | | | their attachments, | | | | | | | | | - the elevator fittings and their | | | | | | | | | attachments to the THS for leakage. | | | | | | | | | | | | | | | | D.| | If you find damage: | | | | | | | | | (1) Do a special detailed inspection | | | | | | | | | of the carbon component for: | | | | | | | | | - exact location of damage and | | X | | | | | | | damage length width and depth. | | | | | | | | | (2) Do a special detailed inspection | | | | | | | | | of the metallic component for: | | | | | | | | | - cracks. | | X | | | | | | | | | | | | | | E.| | Do a functional test of the elevator | X | | | | | | | | movement. | | | | | | -------------------------------------------------------------------------------
EFF : ALL 05-51-44 SROS
Page 615 Jul 01/06
Subtask 05-51-44-210-055 D. Inspection of the Wing (Ref. Fig. 603/TASK 05-51-44-991-003) (Ref. TASK 05-51-17-200-801), (Ref. TASK 27-14-00-820-801). ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Wing | | | | | | | | | | | | | | | | A.| | Do the inspection after Flight in | X | | | | | | | | Excessive Turbulence or in Excess of | | | | | | | | | VMO/MMO (Ref.TASK 05-51-17-200-801). | | | | | | | | | | | | | | | |2. | | Inspection of the Outer-Wing Wingtip | | | | | | | | | to Main Wingbox joint | | | | | | | | | | | | | | | | A.| | At RIB39, examine the upper and lower | | | | | | | | | skin panel joints for: | | | | | | | | | - cracks, distortion and pulled or | X | | | | | | | | torn fasteners. | | | | | | | | | Make sure that the sealant beads are | X | | | | | | | | in the correct condition. | | | | | | | | | | | | | | | |3. | | Inspection of Fixed Leading-Edge | | | | | | | | | D-Nose Skins | | | | | | | | | | | | | | | | A.| | Examine the D-nose skin-panel joint | | | | | | | | | at slat track center-lines, from slat | | | | | | | | | track 9 and outboard for: | | | | | | | | | - cracks, distortion and pulled or | X | | | | | | | | torn fasteners. | | | | | | | | | Make sure that the sealant beads are | X | | | | | | | | in the correct condition. | | | | | | | | | | | | | | | |4. | | Inspection of the Aileron | | | | | | | | | | | | | | | | A.| | Examine the upper and lower skin | | | | | | | | | panels, the hinges and the spar | | | | | | | | | fasteners for: | | | | | | | | | - damaged paintwork and damaged | X | | | | | | | | filler. | | | | | | | | | | | | | | | | B.| | Examine the fittings for: | | | | | | | | | - damage. | X | | | | |
EFF : ALL 05-51-44 SROS
Page 616 Jul 01/06
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | | | | | | | | C.| | Do the inspection of the aileron | X | | | | | | | | adjustment | | | | | | | | | (Ref. TASK 27-14-00-820-801). | | | | | | | | | | | | | | | |5. | | Inspection of the Flaps and Slats | | | | | | | | | | | | | | | | A.| | At flap track 2, examine aft | X | | | | | | | | attachment (spigot) and flap-to| | | | | | | | | carriage attachment of inboard flap. | | | | | | | | | | | | | | | | B.| | At flap track 4, examine aft | X | | | | | | | | attachment (spigot), flap-to| | | | | | | | | carriage and flap-to-I/M beam | | | | | | | | | attachment of outboard flap. | | | | | | | | | | | | | | | | C.| | Examine attachment-points of movable | X | | | | | | | | flap track fairings 2 to 5. | | | | | | | | | | | | | | | | D.| | Examine the slats and their fairings | | | | | | | | | for: | | | | | | | | | - cracks, distortion and pulled or | X | | | | | | | | torn fasteners. | | | | | | | | | | | | | | | |6. | | Inspection of spoiler | | | | | | | | | | | | | | | | A.| | Examine the center hinge lugs of | | | | | | | | | spoilers 1 to 6 for: | | | | | | | | |- cracks, distortion and other damage. | X | | | | | ------------------------------------------------------------------------------Subtask 05-51-44-210-056 E. Inspection of the Pylons **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, (Ref. Fig. 604/TASK 05-51-44-991-004)
EFF : ALL 05-51-44 SROS
Page 617 Jul 01/06
Structure of the Wing Figure 603/TASK 05-51-44-991-003- 12 (SHEET 1) EFF : ALL 05-51-44 SROS
Page 618 Jul 01/06
Structure of the Wing Figure 603/TASK 05-51-44-991-003- 22 (SHEET 2) EFF : ALL 05-51-44 SROS
Page 619 Jul 01/06
Engine-Pylon Station Figure 604/TASK 05-51-44-991-004 EFF : 001-049, 201-249, 251-252, 255-299, 05-51-44 301-399, 401-449, 451-499, SROS
Page 620 Jul 01/06
**ON A/C 701-749, (Ref. Fig. 604A/TASK 05-51-44-991-004-A) **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, (Ref. Fig. 605/TASK 05-51-44-991-006) **ON A/C 701-749, (Ref. Fig. 605A/TASK 05-51-44-991-006-A) **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, (Ref. Fig. 606/TASK 05-51-44-991-008) **ON A/C 701-749, (Ref. Fig. 606A/TASK 05-51-44-991-008-A) **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, (Ref. Fig. 607/TASK 05-51-44-991-009) **ON A/C 701-749, (Ref. Fig. 607A/TASK 05-51-44-991-009-A) **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, (Ref. Fig. 608/TASK 05-51-44-991-010) **ON A/C 701-749, (Ref. Fig. 608A/TASK 05-51-44-991-010-A)
EFF : 001-049, 201-249, 251-252, 255-299, 05-51-44 301-399, 401-449, 451-499, 701-749, SROS
Page 621 Jul 01/06
Engine-Pylon Station Figure 604A/TASK 05-51-44-991-004-A EFF : 701-749, 05-51-44 SROS
Page 622 Jul 01/06
Engine-Pylon Box Figure 605/TASK 05-51-44-991-006 EFF : 001-049, 201-249, 251-252, 255-299, 05-51-44 301-399, 401-449, 451-499, SROS
Page 623 Jul 01/06
Engine-Pylon Box Figure 605A/TASK 05-51-44-991-006-A EFF : 701-749, 05-51-44 SROS
Page 624 Jul 01/06
Engine-to-Pylon Attach Fittings Figure 606/TASK 05-51-44-991-008 EFF : 001-049, 201-249, 251-252, 255-299, 05-51-44 301-399, 401-449, 451-499, SROS
Page 625 Jul 01/06
Engine-to-Pylon Attach Fittings Figure 606A/TASK 05-51-44-991-008-A EFF : 701-749, 05-51-44 SROS
Page 626 Jul 01/06
Pylon-to-Wing Forward Attach-Fittings Figure 607/TASK 05-51-44-991-009 EFF : 001-049, 201-249, 251-252, 255-299, 05-51-44 301-399, 401-449, 451-499, SROS
Page 627 Jul 01/06
Pylon-to-Wing Forward Attach-Fittings Figure 607A/TASK 05-51-44-991-009-A EFF : 701-749, 05-51-44 SROS
Page 628 Jul 01/06
Pylon-to-Wing Aft Attach-Fittings Figure 608/TASK 05-51-44-991-010 EFF : 001-049, 201-249, 251-252, 255-299, 05-51-44 301-399, 401-449, 451-499, SROS
Page 629 Jul 01/06
Pylon-to-Wing Aft Attach-Fittings Figure 608A/TASK 05-51-44-991-010-A EFF : 701-749, 05-51-44 SROS
Page 630 Jul 01/06
**ON A/C ALL (Ref. TASK 28-25-00-650-803), (Ref. TASK 71-00-51-000-801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Pylons | | | | | | | | | | | | | | | | A.| | Examine pylon panels, doors, auxiliary| | | | | | | | | structure, the rivets and the | | | | | | | | | stiffeners for: | | | | | | | | | - distortion, buckling and tearing of | X | | | | | | | | plates at rivet locations. | | | | | | | | | | | | | | | | B.| | Examine the pylon forward secondary | | | | | | | | | structure for: | | | | | | | | | - buckling and missing rivets. | X | | | | | | | | If you find damage: | | | | | | | | | Examine adjacent external and internal| | | | | | | | | area of pylon forward secondary | | | | | | | | | structure for: | | | | | | | | | - distortion, cracks, rupture and | | X | | | | | | | fluid leakage and sheared or slack | | | | | | | | | or missing fasteners. | | | | | | | | | | | | | | | | C.| | Examine the pylon panels between | | | | | | | | | forward and aft pylon-to-wing | | | | | | | | | attachment for: | | | | | | | | | - distortion, wrinkles, buckles, | X | | | | | | | | sheared or slack or missing | | | | | | | | | fasteners and tearing of plates | | | | | | | | | at rivet locations. | | | | | | | | | | | | | | | | D.| | Examine upper spar between spigot | | | | | | | | | hole and aft attachment and around | | | | | | | | | access door for: | | | | | | | | | - distortion, wrinkles, buckles, | X | | | | | | | | sheared or slack or missing | | | | | | | | | fasteners and tearing of plates | | | | | | | | | at rivet locations. | | | | | | | | | If you find damage: | | | | | | | | | Examine pylon main frame (lower spar, | | | | | | | | | upper spar, panels, ribs, rib-to-panel| | | | | | | | | attachments, spar-to-panel | | | | | |
EFF : ALL 05-51-44 SROS
Page 631 Jul 01/06
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | attachments, structure) for: | | | | | | | | | - distortion, cracks, rupture and | | X | | | | | | | fluid leakage. | | | | | | | | | | | | | | | | E.| | Examine the Fan Cowl and Thrust | | | | | | | | | Reverser attachments for: | | | | | | | | | - cracks, distortion and pulled or | X | | | | | | | | torn fasteners. | | | | | | | | | Make sure the Cowl closes correctly. | | | | | | | | | | | | | | | | F.| | Examine the engine-to-pylon | | | | | | | | | attachments for: | | | | | | | | | - distortion and cracks. | X | | | | | | | | If you find damage: | | | | | | | | | (1) Examine the Thrust-Reverser spigot| | | | | | | | | Fitting for: | | | | | | | | | - cracks in the protective | | X | | | | | | | sealant at the most inboard and | | | | | | | | | outboard edges of the spigot | | | | | | | | | attachment flange with the wing | | | | | | | | | surface, | | | | | | | | | - distortion, gapping between | | X | | | | | | | attachment flange and wing | | | | | | | | | surface, | | | | | | | | | - distortion of fasteners, | | X | | | | | | | - cracks. | | X | | | | | | | (2) Examine the Rear Pick-up for: | | | | | | | | | - cracks in the protective | | X | | | | | | | treatment/sealant around the | | | | | | | | | attachment to the wing surface, | | | | | | | | | - distortion, gapping between | | X | | | | | | | attachment flange and wing | | | | | | | | | surface, | | | | | | | | | - distortion of fasteners, | | X | | | | | | | - cracks. | | X | | | | | | | | | | | | | | G.| | Examine the pylon-to-wing fittings | | | | | | | | | for: | | | | | | | | | - distortion and cracks. | X | | | | | | | | If you find damage: | | | | | | | | | Examine the pylon-to-wing attach | | | | | | | | | fitting for: | | | | | | | | | - distortion and cracks. | | X | | | |
EFF : ALL 05-51-44 SROS
Page 632 Jul 01/06
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| ------------------------------------------------------------------------------Subtask 05-51-44-210-057 F. Inspection of the Nacelles ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Nacelles | | | | | | | | | | | | | | | | A.| | Examine the Fan Cowl and Thrust| | | | | | | | | Reverser hinge fitting and latches | | | | | | | | | for: | | | | | | | | | - cracks, distortion and pulled or | X | | | | | | | | torn fasteners. | | | | | | | | | Make sure the Fan Cowl and the Thrust | | | | | | | | | Reverser close correctly. | | | | | | | | | If you find damage: | | | | | | | | | (1) Examine the thrust-reverser | | | | | | | | | fitting adjacent area of the | | | | | | | | | pylon (lateral panel, rib) for: | | | | | | | | | - distortion, cracks and sheared | | X | | | | | | | or slack or missing fasteners. | | | | | | | | | (2) Examine the fan-cowl fitting | | | | | | | | | adjacent internal and external | | | | | | | | | areas of the secondary structure | | | | | | | | | for: | | | | | | | | | - cracks, distortion, dents and | | X | | | | | | | sheared or slack or missing | | | | | | | | | rivets and fasteners. | | | | | | -------------------------------------------------------------------------------
EFF : ALL 05-51-44 SROS
Page 633 Jul 01/06
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-44-410-050 G. Close Access (1) Close the main-landing-gear doors (Ref. TASK 32-12-00-410-801). (2) Close the fan cowl doors (Ref. TASK 71-13-00-410-802): FOR 4030EM1 415BL, 416BR FOR 4030EM2 425BL, 426BR (3) Close the thrust reverser doors (Ref. TASK 78-30-00-410-801): FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR **ON A/C 701-749, Subtask 05-51-44-410-050-A G. Close Access (1) Close the main-landing-gear doors (Ref. TASK 32-12-00-410-801). (2) Close the fan cowl doors (Ref. TASK 71-13-00-410-805): FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR (3) Close the thrust reverser doors (Ref. TASK 78-30-00-410-803): FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR
EFF : 001-049, 201-249, 251-252, 255-299, 05-51-44 301-399, 401-449, 451-499, 701-749, SROS
Page 634 Jul 01/06
**ON A/C ALL Subtask 05-51-44-866-050 H. 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) Pressurize the Yellow hydraulic system (Ref. TASK 29-00-00-863-803). (4) Pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-802). Subtask 05-51-44-200-050 J. Do The Flight System Test NOTE : The tests below are necessary only if you find damage to the ____ structure adjacent to a flight control surface. (1) Operate the aileron system. Make sure that the travel is full and that the aileron moves freely (Ref. TASK 27-14-00-710-801). (2) Operate the flap system. Make sure that the travel is full and that the flap moves freely (Ref. TASK 27-54-00-710-801). (3) Operate the slat system. Make sure that the travel is full and that the slat moves freely (Ref. TASK 27-84-00-710-801). (4) Operate the spoiler system. Make sure that the travel is full and that the spoiler moves freely (Ref. TASK 27-64-00-710-801). (5) Operate the THS system. Make sure that the travel is full and that the THS moves freely.
EFF : ALL 05-51-44 SROS
Page 635 Jul 01/06
(6) Operate the elevator system. Make sure that the travel is full and that the elevator moves freely (Ref. TASK 27-34-00-710-801). (7) Operate the rudder system. Make sure that the travel is full and that the rudder moves freely (Ref. TASK 27-24-00-710-801). **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-44-200-051 K. Do a test of the Thrust Reverser System NOTE : The test below is necessary only if you find damage to the ____ structure adjacent to a cowl surface. (1) Operate the thrust reverser system. Make sure that the travel is full and that the thrust reverser moves freely (Ref. TASK 78-31-00-710-804). **ON A/C 701-749, Subtask 05-51-44-200-051-A K. Do a test of the Thrust Reverser System NOTE : The test below is necessary only if you find damage to the ____ structure adjacent to a cowl surface. (1) Operate the thrust reverser system. Make sure that the travel is full and that the thrust reverser moves freely (Ref. TASK 78-31-00-740-802).
EFF : ALL 05-51-44 SROS
Page 636 Jul 01/06
**ON A/C ALL 5. Close-up ________ Subtask 05-51-44-866-051 A. Aircraft Maintenance Configuration (1) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (2) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803). (3) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802). (4) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). Subtask 05-51-44-860-051 B. Put the Aircraft back to its Initial Configuration (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.
EFF : ALL 05-51-44 SROS
Page 637 Jul 01/06
_____________________________________________________________________________ PRESSURIZATION TEST OF FUSELAGE (LEAKAGE CHECKS) AFTER A/C ABNORMAL OPERATION OR REPAIR - ADJUSTMENT/TEST ___________________________ TASK 05-53-00-780-803 Pressurization Retest and Leakage Rate Measurement WARNING : MAKE SURE THAT: _______ - ONLY THE PERSONS NECESSARY FOR THE PRESSURIZATION TEST ARE IN THE AIRCRAFT DURING THE TEST. - THE PERSONS IN THE AIRCRAFT HAVE MEDICAL CLEARANCE TO DO THIS TYPE OF TEST. BE CAREFUL WHEN YOU CONTROL THE PRESSURE. SUDDEN CHANGES IN PRESSURE CAN CAUSE PAIN AND INJURY. WARNING : THERE MUST BE TWO PERSONS IN THE COCKPIT DURING THE PRESSURIZATION _______ TEST. IF A CHANGE IN PRESSURE HAS AN UNWANTED EFFECT (PAIN, NOISE IN THE EARS, HEADACHE OR OTHER) ON ONE PERSON, THE OTHER PERSON CAN ADJUST THE PRESSURE TO AVOID INJURY. 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. 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. 1. __________________ Reason for the Job To measure the structural leakage.
EFF : ALL 05-53-00 R SROS
Page 501 Jan 01/07
2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific R
No No No No No No No No
specific specific specific specific specific specific specific specific
absolute pressure indicator/digital indication/sensitivity 1mbar(0.01psi) circuit breaker(s) safety clip(s) safety barriers safety plug - ref MS21913-4 safety streamer stop-watch vertical speed indicator warning notices O-ring - ref NAS1612-4
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-33-21-618-801 12-33-21-618-801 23-44-00-860-801 24-41-00-861-801 24-41-00-862-801 31-60-00-860-801 31-60-00-860-802 35-12-41-000-802 35-12-41-400-802 52-51-00-710-801
Pre-conditioning through the High-Pressure Ground Connection Pre-conditioning with the APU Operation of the Service Interphone System 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 Removal of the Full-Face/Quick-Donning Oxygen Mask (8RN1,2,3,4) Installation of the Full-Face/Quick-Donning Oxygen Mask (8RN1,2,3,4) Operational Test of the Cockpit-Door Lock System (CDLS)
EFF : ALL 05-53-00 SROS
Page 502 Jan 01/07
3. __________ Job Set-up R R R R R
Subtask 05-53-00-865-050 A. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------C/B NOT APPLICABLE Subtask 05-53-00-860-064-A
R
B. Aircraft Maintenance Configuration (1) Put the safety barriers and the warning notices in position to keep persons out of the work area. (2) Put the vertical speed indicator, absolute pressure indicator/digital indication/sensitivity 1mbar(0.01psi) and the stop-watch in position in the cockpit. (3) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861801). (4) Make sure that the avionics equipment ventilation operates correctly. NOTE : If during this test, the avionics equipment ventilation stops, ____ you must stop the test. (5) In the left side of the avionics compartment at frame 14: - put the safety plug - ref MS21913-4 with its O-ring - ref NAS1612-4 on the air inlet of the pressure switch 16WR. - put a safety streamer on the safety plug. (6) On the panel 722VU, open the circuit breaker 1MQ Cockpit Door Lock System (CDLS). (7) We recommend that you remove the crew oxygen masks (Ref. TASK 35-1241-000-802) NOTE : This test requires an absolute pressure higher than the cabin ____ pressures you get during usual aircraft operations. The crew masks have an aneroid capsule that is usually resistant to the absolute pressures you can get during this test.
EFF : ALL 05-53-00 SROS
Page 503 Jan 01/07
But, to prevent high stress on the aneroid capsule, we recommend the removal of the crew oxygen masks. (8) On the AIR section of the panel 225VU: - make sure that the PACK 1 and PACK 2 pushbutton switches are pushed (the FAULT legends are on). (9) On the CABIN PRESS section of the panel 225VU: - release the MOD SEL pushbutton switch (the MAN legend is on) - make sure that the MAN/VALVE SEL switch is in the BOTH position. (10) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00860-801). (11) On the SD on the CAB PRESS page: - make sure that the outflow valves 313HL and 315HL are in the fully open position. (12) On the CARGO AIR COND section of the panel 212VU: - make sure that the BULK (FWD, AFT) ISOL VALVES pushbutton switch is released (the OFF legend is on). (13) On the VENTILATION section of the panel 212VU: - push the EXTRACT pushbutton switch (the OVRD legend is on). (14) On the overboard extract valve (13HQ): (a) Push the latch to release the handle. (b) Pull out the handle to engage the mechanism. (c) Fold out the handle. (d) Set the deactivation switch to the OFF position. (e) Turn the handle counterclockwise until the main and auxiliary flaps of the valve are fully closed. (f) Fold and latch the handle. (15) On the SD, on the CAB PRESS page: - make sure that the VENT EXTRACT ventilation valve is closed. After 30 seconds approximately, the horn in the nose gear well sounds. On the panel 925VU: - push the HORN RESET pushbutton switch.
EFF : ALL 05-53-00 R SROS
Page 504 Jan 01/07
(16) Close and lock the sliding windows and all access doors to the pressurized area. (17) For aircraft on which the optional LDMCR is installed, make sure that the access panel to the staircase is open. (18) on the EXT LT section of the panel 215VU: - set the BEACON switch to ON. (19) Do an interphone communication test between the cockpit and the ground service personnel out of the closed area .(Ref. TASK 23-44-00860-801) (20) Pressurize the pneumatic system: - with the APU (Ref. TASK 12-33-21-618-801) or with the HP ground-supply unit (Ref. TASK 12-33-21-618-801) NOTE : You must shut the access door 811 for this procedure. ____ Subtask 05-53-00-860-071 R
C. Not applicable. Subtask 05-53-00-970-052
R
D. Calculation of the Pressure. (1) Use the pressure indicator to measure the ambient pressure (Pamb). (2) Calculate and write these values: - Value A = Pamb + 400 mbar (5.80 psi) - Value B = Pamb + 610 +7 -7 mbar (8.84 +0.10 -0.10 psi) - Value C = Pamb + 578 mbar (8.38 psi) - Value D = Pamb + 570 mbar (8.26 psi) The values A and B are necessary to monitor the system. The values C and D are necessary to mesure the leakage rate.
EFF : ALL 05-53-00 SROS
Page 505 Jan 01/07
4. Procedure _________ Subtask 05-53-00-780-054 A. Procedure to measure the leakage rate. WARNING : DO NOT LET THE CABIN ALTITUDE CHANGE TOO FAST. SUDDEN CHANGES _______ IN PRESSURE CAN CAUSE INJURY TO PERSONS. WARNING : MAKE SURE THAT THE DIFFERENTIAL PRESSURE IS NOT MORE THAN THE _______ VALUE SPECIFIED FOR THIS TEST. WARNING : DO NOT USE THE ECAM DISPLAYS TO READ THE CABIN PRESSURE _______ PARAMETERS (CABIN DIFFERENTIAL PRESSURE, CABIN ALTITUDE, CABIN VERTICAL- SPEED) DURING THIS TEST. THE PRESSURES USED IN THIS TEST ARE MORE THAN THE MAXIMUM LIMIT OF THE RELATED PRESSURE SENSOR. WHEN THESE PRESSURES BECOME MORE THAN THE PRESSURE SENSOR LIMIT, ON THE ECAM DISPLAY: - THE CABIN DIFFERENTIAL PRESSURE INDICATION AND THE CABIN ALTITUDE INDICATION WILL CONTINUE TO SHOW THESE LIMIT VALUES. - THE CABIN VERTICAL-SPEED INDICATION IS NO LONGER CORRECT. IF YOU DO NOT KNOW THE CORRECT CABIN PRESSURE VALUES, YOU CAN MAKE UNWANTED CHANGES IN PRESSURE THAT CAN CAUSE INJURY.
R R R
NOTE : This procedure uses the MAN V/S CTL switch on the CABIN PRESS ____ section of the panel 225VU to control the cabin pressure. This switch, spring loaded to neutral, controls the outflow valves position: - UP: the outflow valves move to the open position (the cabin pressure decreases) - DN: the outflow valves move to the closed position (the cabin pressure increases) We recommend: - short action on this switch (do not hold the switch in the UP or DN position) - that you monitor the cabin vertical speed indication to prevent sudden changes in cabin pressure.
EFF : ALL 05-53-00 SROS
Page 506 Jan 01/07
------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------1. On the AIR section of the panel 225VU: - adjust the cabin temperature control as necessary.
On the AIR section of the panel 225VU: - make sure that the FAULT legend of the PACK 1 and PACK 2 pushbutton switches is off. Air blows into the fuselage.
2. On the CABIN PRESS section of the panel 225VU: - set the MAN V/S CTL switch to DN and release, the switch moves to the neutral position. Do this operation several times. This closes the outflow valves.
On the vertical speed indicator: - the cabin vertical speed must not be more than 500 ft.min (152.39 m.min). On the pressure indicator: - the cabin pressure increases up to value A (Pamb + 400 mbar (5.80 psi)).
NOTE : The cabin vertical speed ____ must not be more than 500 ft.min (152.39 m.min). - stop when you get a cabin pressure of value A (Pamb + 400 mbar (5.80 psi)). 3. With the MAN/V/S CTL switch in the UP or DN position, keep the pressure stable at value A (Pamb + 400 mbar (5.80 psi)) for 5 minutes.
Tell ground personnel to walk around the aircraft and to do a check for leakage. On the vertical speed indicator: - the cabin vertical speed is 0. On the pressure indicator: - the cabin pressure is value A (Pamb + 400 mbar (5.80 psi)).
4. Use the same method as in step 2 to increase cabin pressure up to value B (Pamb + 610 +7 -7 mbar (8.84 +0.10 -0.10 psi)).
On the pressure indicator: - the cabin pressure increases up to value B (Pamb + 610 +7 -7 mbar (8.84 +0.10 -0.10 psi)). On the vertical speed indicator: - the cabin vertical speed must not be more than 500 ft.min (152.39 m.min).
NOTE : the cabin vertical speed ____ must not be more than 500 ft.min (152.39 m.min). 5. With the MAN/V/S CTL switch in the UP or DN position, keep the
On the vertical speed indicator: - the cabin vertical speed is 0.
EFF : ALL 05-53-00 R SROS
Page 507 Jan 01/07
------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------pressure stable at value B (Pamb On the pressure indicator: + 610 +7 -7 mbar (8.84 +0.10 - the cabin pressure is value B (Pamb + 0.10 psi)). 610 +7 -7 mbar (8.84 +0.10 -0.10 psi)). 6. On the AIR section of the panel 225VU: - release the PACK 1 pushbutton switch. On the CABIN PRESS section of the panel 225VU: - with the MAN/V/S CTL switch, stabilize the pressure at value B (Pamb + 610 +7 -7 mbar (8.84 +0.10 -0.10 psi)).
On the AIR section of the panel 225VU: - the OFF legend of the PACK 1 pushbutton switch comes on. On the vertical speed indicator: - the cabin vertical speed is 0. On the pressure indicator: - the cabin pressure is value B (Pamb + 610 +7 -7 mbar (8.84 +0.10 -0.10 psi)).
7. On the CABIN PRESS section of the panel 225VU: - with the MAN/V/S CTL switch in DN position, fully close the outflow valves. On the AIR section of the panel 225VU: - release the PACK 2 pushbutton switch when the outflow valves are closed.
On the SD, on the CAB PRESS page: - the outflow valves are in the fully closed position. On the AIR section of the panel 225VU: - the OFF legend of the PACK 2 pushbutton switch comes on. On the pressure indicator: - the cabin pressure indication decreases.
8. Monitor the decrease of the pressure: - at value C (Pamb + 578 mbar (8.38 psi)), start the stop-watch. - at value D (Pamb + 570 mbar (8.26 psi)), stop the stop-watch and write the time. 9. Calculate the leakage rate: - leakage rate = (value C) (value D) / time The leakage rate is permitted if below 0.64 mbar/s (0.56 psi/min) On the AIR section of the panel
On the vertical speed indicator:
EFF : ALL 05-53-00 R SROS
Page 508 Jan 01/07
R R R
------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------225VU: - the cabin vertical speed must not be - push the PACK 1 and PACK 2 more than 500 ft.min (152.39 m.min). pushbutton switches (the OFF On the pressure indicator: legend is off). - the cabin pressure indication On the CABIN PRESS section of the decreases down to the external panel 225VU: ambient pressure. - with the MAN V/S CTL switch, decrease the cabin pressure until you get a differential pressure of 0 psi. NOTE : The cabin vertical speed ____ must not be more than 500 ft.min (152.39 m.min). 10. Wait until the cabin has completely depressurized and then fully open the outflow valves. 5. Close-up ________
R
Subtask 05-53-00-865-051
R R
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
R R R
------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------C/B NOT APPLICABLE Subtask 05-53-00-860-065-A
R
B. Put the Aircraft back to its Initial Configuration (1) Shut down the APU (Ref. TASK 12-33-21-618-801) or stop the HP ground-air supply unit (Ref. TASK 12-33-21-618-801). (2) On the EXT LT section of the panel 215VU: - set the BEACON switch to OFF.
EFF : ALL 05-53-00 SROS
Page 509 Jan 01/07
(3) In the left side of the avionics compartment at frame 14: - remove the safety streamer from the safety plug. - remove the safety plug with its O-ring from the air inlet of the pressure switch 16WR. (4) If you removed the crew oxygen masks, install them (Ref. TASK 35-1241-400-802) (5) Remove the pressure indicator, the vertical speed indicator and the stop-watch from the cockpit. (6) On the VENTILATION section of the panel 212VU: - release the EXTRACT pushbutton switch (the FAULT legend comes on) (7) On the panel 722VU, close the circuit breaker 1MQ and do a CDLS test (Ref. TASK 52-51-00-710-801). (8) On the overboard extract valve (13HQ): (a) Push the latch to release the handle. (b) Pull the handle. (c) Set the deactivation switch to ON, and make sure that the two flaps open. (d) Fold and latch the handle. (9) On the VENTILATION section of the panel 212VU: - the FAULT legend of the EXTRACT pushbutton switch goes off (10) Put the system and the aircraft back to the serviceable configuration. (11) Do the EIS stop procedure: (Ref. TASK 31-60-00-860-802) (12) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862801). (13) Remove the warning notices and the safety barriers.
EFF : ALL 05-53-00 R SROS
Page 510 Jan 01/07
TASK 05-53-00-780-803- 01 Pressurization Retest and Leakage Rate Measurement (with ACMS) WARNING : MAKE SURE THAT: _______ - ONLY THE PERSONS NECESSARY FOR THE PRESSURIZATION TEST ARE IN THE AIRCRAFT DURING THE TEST. - THE PERSONS IN THE AIRCRAFT HAVE MEDICAL CLEARANCE TO DO THIS TYPE OF TEST. BE CAREFUL WHEN YOU CONTROL THE PRESSURE. SUDDEN CHANGES IN PRESSURE CAN CAUSE PAIN AND INJURY. WARNING : THERE MUST BE TWO PERSONS IN THE COCKPIT DURING THE PRESSURIZATION _______ TEST. IF A CHANGE IN PRESSURE HAS AN UNWANTED EFFECT (PAIN, NOISE IN THE EARS, HEADACHE OR OTHER) ON ONE PERSON, THE OTHER PERSON CAN ADJUST THE PRESSURE TO AVOID INJURY. 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. 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. 1. __________________ Reason for the Job To measure the structural leakage.
EFF : ALL 05-53-00 R SROS
Page 511 Jul 01/05
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
safety barriers safety plug - ref MS21913-4 safety streamer stop-watch warning notices O-ring - ref NAS1612-4
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-33-21-618-801 12-33-21-618-801 23-44-00-860-801 24-41-00-861-801 24-41-00-862-801 31-36-00-740-805 31-60-00-860-801 31-60-00-860-802 34-10-00-860-801 34-10-00-860-803 35-12-41-000-802 35-12-41-400-802 52-51-00-710-801
Pre-conditioning through the High-Pressure Ground Connection Pre-conditioning with the APU Operation of the Service Interphone System Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Access to the Parameter call-up menus. EIS Start Procedure EIS Stop Procedure ADIRS Start Procedure ADIRS Stop Procedure Removal of the Full-Face/Quick-Donning Oxygen Mask (8RN1,2,3,4) Installation of the Full-Face/Quick-Donning Oxygen Mask (8RN1,2,3,4) Operational Test of the Cockpit-Door Lock System (CDLS)
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Page 512 Jul 01/05
3. __________ Job Set-up R Subtask 05-53-00-860-066-A A. Aircraft Maintenance Configuration (1) Put the safety barriers and the warning notices in position to keep persons out of the work area. (2) Make sure that the static probe covers are not installed. (3) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861801). (4) Make sure that the avionics equipment ventilation operates correctly. NOTE : If during this test, the avionics equipment ventilation stops, ____ you must stop the test. (5) In the left side of the avionics compartment at frame 14: - put the safety plug - ref MS21913-4 with its O-ring - ref NAS1612-4 on the air inlet of the pressure switch 16WR. - put a safety streamer on the safety plug. (6) We recommend that you remove the crew oxygen masks (Ref. TASK 35-1241-000-802) NOTE : This test requires an absolute pressure higher than the cabin ____ pressures you get during usual aircraft operations. The crew masks have an aneroid capsule that is usually resistant to the absolute pressures you can get during this test. But, to prevent high stress on the aneroid capsule, we recommend the removal of the crew oxygen masks. (7) On the AIR section of the panel 225VU: - make sure that the PACK 1 and PACK 2 pushbutton switches are pushed (the FAULT legends is on). (8) On the CABIN PRESS section of the panel 225VU: - release the MOD SEL pushbutton switch (the MAN legend is on) - make sure that the MAN/VALVE SEL switch is in the BOTH position. (9) On the panel 722VU, open the circuit breaker 1MQ Cockpit Door Lock System (CDLS).
EFF : ALL 05-53-00 SROS
Page 513 Jul 01/05
(10) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00860-801). (11) On the SD on the CAB PRESS page: - make sure that the outflow valves 313HL and 315HL are in the fully open position. (12) On the CARGO AIR COND section of the panel 212VU: - make sure that the BULK (FWD, AFT) ISOL VALVES pushbutton switch is released (the OFF legend is on). (13) On the VENTILATION section of the panel 212VU: - push the EXTRACT pushbutton switch (the OVRD legend is on). (14) On the overboard extract valve (13HQ): (a) Push the latch to release the handle. (b) Pull out the handle to engage the mechanism. (c) Fold out the handle. (d) Set the deactivation switch to the OFF position. (e) Turn the handle counterclockwise until the main and auxiliary flaps of the valve are fully closed. (f) Fold and latch the handle. (15) On the SD, on the CAB PRESS page: - make sure that the VENT EXTRACT ventilation valve is closed. After 30 seconds approximately, the horn in the nose gear well sounds. On the panel 925VU: - push the HORN RESET pushbutton switch. (16) Do the ADIRS start procedure (Ref. TASK 34-10-00-860-801). (17) On the MCDU, get access to the ACMS : PARAM ALPHA CALL-UP page. Enter the alpha codes: (Ref. TASK 31-36-00-740-805) - PDC to show the cabin differential pressure - VSCB to show the cabin vertical speed - AOV to show the aft outflow valve position - FOV to show the forward outflow valve position (18) Close and lock the sliding windows and all access doors to the pressurized area.
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Page 514 Jul 01/05
(19) on the EXT LT section of the panel 215VU: - set the BEACON switch to ON. (20) Do an interphone communication test between the cockpit and the ground service personnel out of the closed area.(Ref. TASK 23-44-00860-801) (21) Pressurize the pneumatic system: - with the APU (Ref. TASK 12-33-21-618-801) or with the HP ground-supply unit (Ref. TASK 12-33-21-618-801) NOTE : You must shut the access door 811 for this procedure. ____ Subtask 05-53-00-860-072 B. Not applicable. 4. Procedure _________ Subtask 05-53-00-780-055 A. Procedure to measure the leakage rate. WARNING : DO NOT LET THE CABIN ALTITUDE CHANGE TOO FAST. SUDDEN CHANGES _______ IN PRESSURE CAN CAUSE INJURY TO PERSONS. WARNING : MAKE SURE THAT THE DIFFERENTIAL PRESSURE IS NOT MORE THAN THE _______ VALUE SPECIFIED FOR THIS TEST. WARNING : DO NOT USE THE ECAM DISPLAYS TO READ THE CABIN PRESSURE _______ PARAMETERS (CABIN DIFFERENTIAL PRESSURE, CABIN ALTITUDE, CABIN VERTICAL- SPEED) DURING THIS TEST. THE PRESSURES USED IN THIS TEST ARE MORE THAN THE MAXIMUM LIMIT OF THE RELATED PRESSURE SENSOR. WHEN THESE PRESSURES BECOME MORE THAN THE PRESSURE SENSOR LIMIT, ON THE ECAM DISPLAY: - THE CABIN DIFFERENTIAL PRESSURE INDICATION AND THE CABIN ALTITUDE INDICATION WILL CONTINUE TO SHOW THESE LIMIT VALUES. - THE CABIN VERTICAL-SPEED INDICATION IS NO LONGER CORRECT. IF YOU DO NOT KNOW THE CORRECT CABIN PRESSURE VALUES, YOU CAN MAKE UNWANTED CHANGES IN PRESSURE THAT CAN CAUSE INJURY.
R R R
NOTE : This procedure uses the MAN V/S CTL switch on the CABIN PRESS ____ section of the panel 225VU to control the cabin pressure. This switch, spring loaded to neutral, controls the outflow valves position:
EFF : ALL 05-53-00 SROS
Page 515 Jan 01/07
- UP: the outflow valves move to the open position (the cabin pressure decreases) - DN: the outflow valves move to the closed position (the cabin pressure increases) We recommend: - short action on this switch (do not hold the switch in the UP or DN position) - that you monitor the cabin vertical speed indication to prevent sudden changes in cabin pressure. ------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------1. On the AIR section of the panel 225VU: - adjust the cabin temperature control as necessary.
On the AIR section of the panel 225VU: - make sure that the FAULT legend of the PACK 1 and PACK 2 pushbutton switches is off. Air blows into the fuselage.
2. On the CABIN PRESS section of the panel 225VU: - set the MAN V/S CTL switch to DN and release, the switch moves to the neutral position. Do this operation several times. This closes the outflow valves (AOV and FOV indication on MCDU).
On the MCDU - the cabin more than On the MCDU - the cabin increases
(VSCB indication): vertical speed must not be 500 ft.min (152.39 m.min). (PDC indication): differential pressure up to 400 mbar (5.80 psi).
NOTE : The cabin vertical speed ____ must not be more than 500 ft.min (152.39 m.min) (VSCB indication on MCDU). - stop when you get a cabin differential pressure of 400 mbar (5.80 psi) (PDC indication on MCDU). 3. With the MAN/V/S CTL switch in the UP or DN position, keep the differential pressure stable at 400 mbar (5.80 psi) for 5 minutes.
tell ground personnel to walk around the aircraft and do a check for leakage. On the MCDU (VSCB indication): - the cabin vertical speed is 0.
EFF : ALL 05-53-00 R SROS
Page 516 Jan 01/07
------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------On the MCDU (PDC indication): - the cabin differential pressure is 400 mbar (5.80 psi). 4. Use the same method as in step 2 to increase cabin differential pressure up to 610 +7 -7 mbar (8.84 +0.10 -0.10 psi). NOTE : the cabin vertical speed ____ must not be more than 500 ft.min (152.39 m.min) (VSCB indication on MCDU).
On the MCDU (PDC indication): - the cabin differential pressure increases up to 610 +7 -7 mbar (8.84 +0.10 -0.10 psi). On the MCDU (VSCB indication): - the cabin vertical speed must not be more than 500 ft.min (152.39 m.min).
5. With the MAN/V/S CTL switch in the UP or DN position, keep the differential pressure stable at 610 +7 -7 mbar (8.84 +0.10 -0.10 psi).
On the MCDU - the cabin On the MCDU - the cabin 610 +7 -7 psi).
(VSCB indication): vertical speed is 0. (PDC indication): differential pressure is mbar (8.84 +0.10 -0.10
6. On the AIR section of the panel 225VU: - Release the PACK 1 pushbutton switch. On the CABIN PRESS panel 25VU: - with the MAN/V/S CTL switch, stabilize the differential pressure at 610 +7 -7 mbar (8.84 +0.10 -0.10 psi).
On the AIR section of the panel 225VU: - the OFF legend of the PACK 1 pushbutton switch comes on. On the MCDU (VSCB indication): - the cabin vertical speed is 0. On the MCDU (PDC indication): - the cabin differential pressure is 610 +7 -7 mbar (8.84 +0.10 -0.10 psi).
7. On the CABIN PRESS section of the panel 225VU: - with the MAN/V/S CTL switch in DN position, fully close the outflow valves (AOV and FOV indication on MCDU). On the AIR section of the panel 225VU: - release the PACK 2 pushbutton switch when the outflow valves are closed.
On the SD, on the CAB PRESS page: - the outflow valves are in the fully closed position. On the AIR section of the panel 225VU: - the OFF legend of the PACK 2 pushbutton switch comes on. On the MCDU (PDC indication): - the cabin differential pressure indication decreases.
R EFF : ALL 05-53-00 SROS
Page 517 Jul 01/05
------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------8. Monitor the differential pressure decrease on the MCDU (PDC indication): - at 578 mbar (8.38 psi), start the stop-watch. - at 570 mbar (8.26 psi), stop the stop-watch and write the time. 9. Calculate the leakage rate: - leakage rate = 578 mbar (8.38 psi) - 570 mbar (8.26 psi) / time. The leakage rate is permitted if below 0.64 mbar/s (0.56 psi/min). On the AIR section of the panel 225VU: - push the PACK 1 and PACK 2 pushbutton switches (the OFF legend is off). On the CABIN PRESS section of the panel 225VU: - with the MAN V/S CTL switch, decrease the cabin differential pressure until you get a differential pressure of 0 psi.
On the MCDU - the cabin more than On the MCDU - the cabin decreases
(VSCB indication): vertical speed must not be 500 ft.min (152.39 m.min). (PDC indication): differential pressure down to 0.
NOTE : The cabin vertical speed ____ must not be more than 500 ft.min (152.39 m.min) (VSCB indication on MCDU). 10. Wait until the cabin has completely depressurized and then fully open the outflow valves (AOV and FOV indication on MCDU).
EFF : ALL 05-53-00 R SROS
Page 518 Jul 01/05
5. Close-up ________ R Subtask 05-53-00-860-067-A A. Put the Aircraft back to its Initial Configuration (1) Shut down the APU (Ref. TASK 12-33-21-618-801) or stop the HP ground-air supply unit (Ref. TASK 12-33-21-618-801). (2) On the EXT LT section of the panel 215VU: - set the BEACON switch to OFF. (3) In the left side of the avionics compartment at frame 14: - remove the safety streamer from the safety plug. - remove the safety plug with its O-ring from the air inlet of the pressure switch 16WR. (4) If you removed the crew oxygen masks, install them (Ref. TASK 35-1241-400-802) (5) On the VENTILATION section of the panel 212VU: - release the EXTRACT pushbutton switch (the FAULT legend comes on) (6) On the panel 722VU, close the circuit breaker 1MQ and do a CDLS test (Ref. TASK 52-51-00-710-801). (7) On the overboard extract valve (13HQ): (a) Push the latch to release the handle. (b) Pull the handle. (c) Set the deactivation switch to ON, and make sure that the two flaps open. (d) Fold and latch the handle. (8) On the VENTILATION section of the panel 212VU: - the FAULT legend of the EXTRACT pushbutton switch goes off (9) Put the system and the aircraft back to the serviceable configuration. (10) Do the ADIRS stop procedure: (Ref. TASK 34-10-00-860-803)
EFF : ALL 05-53-00 SROS
Page 519 Jul 01/05
(11) Do the EIS stop procedure: (Ref. TASK 31-60-00-860-802) (12) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862801). (13) Remove the warning notices and the safety barriers. R
EFF : ALL 05-53-00 SROS
Page 520 Jul 01/05
DEMAGNETIZATION - MAINTENANCE PRACTICES _______________________________________ TASK 05-54-00-860-801 Demagnetization of the External Parts of the Frames of the Windshield and Sliding Windows 1. __________________ Reason for the Job The demagnetization procedure is applicable to the external parts of the frames of the windshield and sliding windows. R
Use this procedure if you are sure that incorrect deviation of the standby compass occurs after adjustment on the compensation base. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------DM05275A DM05275B MGM50 SAV890-71
1 1 1 1
DEMAGNETIZER - 110V/60HZ DEMAGNETIZER - 220V/50HZ GAUSSMETER DEMAGNETIZER - 230V/50HZ
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------34-22-00-730-801 34-22-23-000-801 34-22-23-400-801
Adjustment test of the standby compass Removal of the Standby Compass (3FC) Installation of the Standby Compass (3FC)
3. __________ Job Set-up Subtask 05-54-00-860-050 A. Aircraft Configuration (1) Make sure that the A/C is not energized (batteries, engines or external power supply).
EFF : ALL 05-54-00 SROS
Page 201 Jan 01/07
Subtask 05-54-00-020-050 B. Removal of the Standby Compass (1) Remove the standby compass (Ref. TASK 34-22-23-000-801) from the cockpit and keep it away from magnetic sources. 4. Procedure _________ Subtask 05-54-00-280-050 A. Find the Magnetic Zones: (1) Obey the instructions from the manufacturer for the GAUSSMETER (MGM50). (2) Make sure that the Gaussmeter operates correctly: - the pointer must move when you put the instrument near the shaft of the windshield wiper motors. (3) With the Gaussmeter, find the magnetic zones of the external parts of the frames of the windshield and sliding windows. Record the value for each zone. NOTE : Ignore the magnetization on the shaft of the windshield wiper ____ motors. Subtask 05-54-00-869-050 B. Demagnetize: R R R
(1) Obey the instructions from the manufacturer for the DEMAGNETIZER 110V/60HZ (DM05275A), DEMAGNETIZER - 220V/50HZ (DM05275B) or the DEMAGNETIZER - 230V/50HZ (SAV890-71) (2) Energize the demagnetizer. (3) Put the demagnetizer at a very small distance (1 cm approx.) from the part it is necessary to demagnetize. This position gives the reference plane. (4) Push the power supply button (indicator light on) and keep the demagnetizer above the magnetic zone during 2 to 3 seconds. Then move the demagnetizer away slowly at a constant speed and at right angles to the reference plane. You must move the demagnetizer to a minimum distance of 50 cm approx. before you release the button. (5) Do the step (4) again for each zone that you must demagnetize.
EFF : ALL 05-54-00 SROS
Page 202 Jul 01/02
(6) De-energize the demagnetizer. (7) For each demagnetized zone, read the value shown on the Gaussmeter. Make sure that this value is near zero. (8) If you find zones that are not fully demagnetized, do again the step (4) until the value read on the Gaussmeter is near zero. 5. Close-up ________ Subtask 05-54-00-420-050 A. Installation of the Standby Compass (1) Install the standby compass (Ref. TASK 34-22-23-400-801). Subtask 05-54-00-730-050 B. Compensation of the Standby Compass (1) Do the compensation of the standby compass (Ref. TASK 34-22-00-730801).
EFF : ALL 05-54-00 SROS
Page 203 Apr 01/98
MEASUREMENT AFTER ABNORMAL OPERATION OF THE AIRCRAFT - INSPECTION/CHECK _______________________________________________________________________ TASK 05-56-00-200-801 Measurement of the Aircraft by Photogrammetry after Abnormal Operation of the Aircraft 1. __________________ Reason for the Job This procedure gives instructions to put the aircraft in the configuration necessary to measure it by photogrammetry. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific No specific No specific No specific 97F08001000000 98F05003000002
safety barriers warning notices wheel chocks adjustable access platform 16.8 m (55 ft. 1 in.) 1 MEASUREMENT TARGET 1 TARGET - MEASUREMENT
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------08-10-00-200-801 28-25-00-650-803 32-00-00-481-801 32-12-00-410-801 32-22-00-410-801 05-56-00-991-001 05-56-00-991-002 05-56-00-991-003 05-56-00-991-004 05-56-00-991-005 05-56-00-991-006 05-56-00-991-007
Weighing and Balancing To Drain the Remaining Fuel (Wing Tanks) Installation of the Safety Devices on the Landing Gears Close the MLG Doors after Maintenance Close the NLG Doors after Maintenance Fig. 601 Fig. 602 Fig. 603 Fig. 604 Fig. 605 Fig. 606 Fig. 607
EFF : ALL 05-56-00 SROS
Page 601 Jul 01/03
3. __________ Job Set-up Subtask 05-56-00-941-050 A. Towing of the Aircraft to the Work Area (1) Tow the aircraft to a place where there is no air movement and a constant temperature or into a hangar. NOTE : Tow the aircraft in a straight line over 10 meters to prevent ____ any lateral stress on the landing gears. Subtask 05-56-00-941-051 B. Safety Precautions (1) Put safety barriers in position around the aircraft. (2) Install the safety devices on the landing gears (Ref. TASK 32-00-00481-801). (3) Put an adjustable access platform in position near the aircraft. (4) Put wheel chocks in position at the main landing gear. Subtask 05-56-00-860-050 C. Aircraft Maintenance Configuration (1) Close the MLG doors (Ref. TASK 32-12-00-410-801). (2) Close the NLG doors (Ref. TASK 32-22-00-410-801). (3) Fully defuel the aircraft (Ref. TASK 28-25-00-650-803). (4) Make sure that: - flight control surfaces are in the neutral position - all doors and panels are closed. (5) Weigh the aircraft, if necessary (Ref. TASK 08-10-00-200-801).
EFF : ALL 05-56-00 SROS
Page 602 Apr 01/98
Subtask 05-56-00-210-050 D. Safety Precautions (1) Make sure that the area around the aircraft is clear. (2) Put warning notices on the passenger/crew doors to prevent access into the aircraft while you measure the aircraft. Subtask 05-56-00-010-050 E. Installation of the Targets on the Aircraft R R
(1) Use MEASUREMENT TARGET (97F08001000000) or TARGET - MEASUREMENT (98F05003000002) to install the targets. (2) Installation of the targets on the wing (Ref. Fig. 601/TASK 05-56-00-991-001) (a) Install 10 targets on the upper surface of each wing, on the sighting reference rivets that you use to adjust flap tracks (points 1R to 10R and 1L to 10L). (b) Install 2 targets at the end of each wing, at the farthest screws of the wing box (points 11R, 12R, 11L and 12L). (c) Install 3 targets on each wing tip (points 13L to 15L and 13R to 15R). (3) Installation of the targets on the fuselage (Ref. Fig. 602/TASK 05-56-00-991-002) (a) Install 10 targets on each side of the fuselage at the leveling points (red triangles) (points 20R to 24R and 20L to 24L). (b) Install 1 target on each side of the fuselage on the aft lower hole used to attach the hoist fitting at FR39-1 (points 25L and 25R). (c) Install 4 targets below the fuselage on the centerline. Put them on indexed tools installed in the measurement receptacles (points 16 to 19). (d) Install 2 targets on the centerline of the center post of the windshield (points 26 and 27). (e) Install 1 target on the centerline of the blanking plug of the shoring hole, at FR85 (point 28).
EFF : ALL 05-56-00 SROS
Page 603 Jul 01/03
Location of the Measurement Points on the Wing Figure 601/TASK 05-56-00-991-001 EFF : ALL 05-56-00 SROS
Page 604 Apr 01/98
Location of the Measurement Points on the Fuselage Figure 602/TASK 05-56-00-991-002 EFF : ALL 05-56-00 SROS
Page 605 Apr 01/98
(4) Installation of the targets on the THS (Ref. Fig. 603/TASK 05-56-00-991-003) (a) Install 4 targets on the THS at the hoisting points (points 30L to 33L and 30R to 33R). (5) Installation of the targets on the vertical stabilizer (Ref. Fig. 603/TASK 05-56-00-991-003) (a) Install 4 targets on the left side at the measurement receptacles (points 34 to 37). (6) Installation of the targets on the engine pylons (Ref. Fig. 604/TASK 05-56-00-991-004) (a) Install 2 targets on the outboard side of the pylons at the measurement receptacles (points 41L, 42L, 41R, and 42R). (b) Install 2 targets on the outboard side of the nacelle air intakes, at the measurement receptacles (points 40L (A,B), 40R (A,B)). NOTE : Install all the targets directly on the external surface ____ of the aircraft except at points 16 to 19 where you must use indexed tools. (7) Installation of the targets on the main landing gear (Ref. Fig. 605/TASK 05-56-00-991-005) (a) Install 1 target on the center of the hub of each outboard wheel (L and R) (points 50L, 50R, 53L and 53R). (b) Install 2 targets in an opposite position on the rim of these outboard wheels (L and R) (points 51L, 52L, 54L, 55L, 51R, 52R, 54R, 55R). (8) Installation of the targets on the nose landing gear. (a) Install 1 target on the center of the hub of the left wheel (point 59). (b) Install 2 targets in an opposite position on the rim of this left wheel (points 60 and 61).
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Page 606 Apr 01/98
Location of the Measurement Points on the Vertical Stabilizer and THS Figure 603/TASK 05-56-00-991-003 EFF : ALL 05-56-00 SROS
Page 607 Apr 01/98
Location of the Measurement Points on the Engine Pylons Figure 604/TASK 05-56-00-991-004 EFF : ALL 05-56-00 SROS
Page 608 Apr 01/98
Location of the Measurement Points on the Landing Gear Figure 605/TASK 05-56-00-991-005 EFF : ALL 05-56-00 SROS
Page 609 Apr 01/98
(9) Installation of ground targets (Ref. Fig. 606/TASK 05-56-00-991-006) (a) Install at least 8 ground targets that you will use to give the scale and for calibration. Make a record of the distance between the targets. 4. Procedure _________ Subtask 05-56-00-220-050 A. Aircraft measurement (1) Take the pictures (Ref. Fig. 607/TASK 05-56-00-991-007) (a) Take at least 9 shots from above the aircraft to have pictures which show all the targets that you can see on the wing. Each shot must include at least 2 ground points. (b) Take at least 7 shots from the ground to have pictures which show all the points that you can see from the ground. Each shot must include at least 2 ground points. (2) Use the photogrammetry principle when you: - take photographs - make a note of measures - make the restitution - make the analysis of the results. 5. Close-up ________ Subtask 05-56-00-410-050 A. Removal of the Targets (1) Remove all the targets and indexed tools that you have installed. Subtask 05-56-00-942-050 B. Put the Aircraft back to its Initial Configuration (1) Remove the safety devices installed on the landing gears. (2) Remove the access platform(s).
EFF : ALL 05-56-00 SROS
Page 610 Apr 01/98
Location of the Measurement Points on the Ground Figure 606/TASK 05-56-00-991-006 EFF : ALL 05-56-00 SROS
Page 611 Apr 01/98
Location of Shooting Positions Figure 607/TASK 05-56-00-991-007 EFF : ALL 05-56-00 SROS
Page 612 Apr 01/98
(3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
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Page 613 Apr 01/98
AIRCRAFT STABILITY - MAINTENANCE PRACTICES __________________________________________ TASK 05-57-00-200-801 Aircraft Stability 1. __________________ Reason for the Job The method given below is used to do graphical checks of the aircraft stability. NOTE : The stability graphs for aircraft on wheels (on dry or wet ground) ____ given in this procedure are applicable to a parked or towed aircraft.
R
NOTE : With the stability graphs (A/C on wheels) given in this procedure, ____ you can do a check of shifting or tipping stability limits, if you need to know only one such limit (when towing for example). It is also used to calculate the ballast necessary for aircraft stability under unfavorable conditions in the following configurations: - aircraft with engines - engines removed - engine re-installation 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------WBM 1-10-00 05-57-00-991-004 05-57-00-991-005 05-57-00-991-006 05-57-00-991-007 05-57-00-991-008 05-57-00-991-009
Fig. Fig. Fig. Fig. Fig. Fig.
201 202 203 204 205 206
EFF : ALL 05-57-00 SROS
Page 201 Jan 01/07
3. __________ Job Set-up Subtask 05-57-00-869-050 A. Aircraft Maintenance Configuration (1) Make sure that the flaps, the slats, the spoilers, the speed brakes and the thrust reverser are retracted. (2) Make sure that the THS is set to neutral. 4. Procedure _________ Subtask 05-57-00-210-050 A. Stability of the aircraft (1) If necessary, the ballast will be installed: - in the forward cargo compartment (at position 11P and 12P), - in the cabin at level of the FR18. NOTE : Before ballasts are put on the aircraft, make sure that the ____ limits below are not exceeded (Ref. WBM 1-10-00) - maximum weight of section 11P and 12P, - maximum loads on cabin floor, - maximum load on jacking points. (2) Refuelling wing tanks can also be a method to put the aircraft back into balance. In this case, the weight of the fuel must be added to the aircraft weight. (3) This method is applicable to these aircraft configurations for each of which a diagram is given: - diagram for aircraft on wheels, on dry ground, (Ref. Fig. 201/TASK 05-57-00-991-004) - diagram for aircraft on wheels, on wet ground, (Ref. Fig. 202/TASK 05-57-00-991-005) - diagram for aircraft on jacks, (Ref. Fig. 203/TASK 05-57-00-991-006) - diagram for aircraft on nose jack or on NLG wheel jack, (Ref. Fig. 204/TASK 05-57-00-991-007) - diagram for aircraft on one MLG wheel jack, (Ref. Fig. 205/TASK 05-57-00-991-008) - diagram for aircraft on MLG and NLG wheel jacks (Ref. Fig. 206/TASK 05-57-00-991-009)
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Page 202 Apr 01/98
Stability, Aircraft on wheels on dry ground (applicable to a parked or towed aircraft) Figure 201/TASK 05-57-00-991-004 EFF : ALL SROS
05-57-00
Page 203 Apr 01/98
Stability, Aircraft on wheels on wet ground (applicable to a parked or towed aircraft) Figure 202/TASK 05-57-00-991-005 EFF : ALL SROS
05-57-00
Page 204 Apr 01/98
Stability, Aircraft on jacks Figure 203/TASK 05-57-00-991-006 EFF : ALL 05-57-00 SROS
Page 205 Apr 01/98
Stability, Aircraft on forward jack or on nose wheel jack Figure 204/TASK 05-57-00-991-007 EFF : ALL 05-57-00 SROS
Page 206 Apr 01/98
Stability, aircraft on one main gear wheel jack Figure 205/TASK 05-57-00-991-008 EFF : ALL 05-57-00 SROS
Page 207 Apr 01/98
Stability, aircraft jacked at main and nose gears for wheel change Figure 206/TASK 05-57-00-991-009 EFF : ALL 05-57-00 SROS
Page 208 Apr 01/98
Subtask 05-57-00-210-052 B. Check of the aircraft stability NOTE : As the same procedure is applicable in any of the above ____ configurations, the diagram related to aircraft on wheels on dry ground is taken as an example. (Ref. Fig. 201/TASK 05-57-00-991-004) (1) Check of aircraft stability: - without crew, - without galleys, - without pallets and containers. For instance, plot point A on the chart from these coordonates: - weight: 160000 kg (352739.5200 lb) - CG: 23% NOTE : Under these conditions, the aircraft will be safe in winds up ____ to 54 kts (100 km/h) (2) Stability of the aircraft when both engines are removed. (a) From point A, make a horizontal line: it cuts across the weight axis at point B (b) From point B, substract the weight of two removed engines 14000 kg (30864.7080 lb) approx., to get point B. (c) From point A, make a vertical line: it cuts across one division of the removed engine scale at point C. (d) Make a line across two divisions on this scale (1 division per engine) to get point C. (e) From this point C, make a vertical line and from point B, make a horizontal line: These two lines cut at point D. For this point, the diagram gives these values: - aircraft weight: 146000 kg (321874.8120 lb) - CG: 29.5% - permissible wind: 38 kts (70 km/h) (3) Calculation of the amount of ballast necessary for engine installation It is considered that engines are installed in the open air, with peak windspeed of 49 kts (90 km/h). The ballast, if necessary shall be installed in the forward cargo-compartment at position 11P.
EFF : ALL 05-57-00 SROS
Page 209 Apr 01/98
(a) continue line BD until it cuts across the 49 kts (90 km/h) average windspeed line at point G. (b) continue line DC until it cuts across the ballast on pallet 11P scale at point E. (c) from point G, make a vertical line until it cross the ballast on pallet 11P scale at point E. (d) Count the number of divisions on the scale between point E and E(in the example 2.3 division). Thus, weight of ballast necessary: 2.3 x 1000 kg (2204.6220 lb) = 2300 kg (5070.6306 lb) NOTE : As the ballast causes only a small increase in the ____ aircraft weight, this weight has been ignored.
EFF : ALL 05-57-00 SROS
Page 210 Apr 01/98
_______________________________________________________________ NON-REVENUE FLIGHT - REQUIREMENTS FOLLOWING MAINTENANCE ACTIONS DESCRIPTION AND OPERATION _________________________ 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
1. _______ General Non-revenue flight following maintenance actions are not required by AIRBUS except for actions involving items that cannot be properly ground tested to verify that the aircrafts operational characteristics have not been adversly affected. Service experience has shown that a non-revenue flight is good practice following actions or repairs which could affect the aircrafts inherent aerodynamic characteristics. NOTE : Operators Regulatory Authority may require non-revenue flights ____ following certain maintenance actions. 2. Engine _________________________________________________________________________ Replacement Replacement or reinstallation of both engines does not require a non-revenue flight providing the engines have been successfully shop tested prior to installation, properly installed and successfully ground tested in accordance with all applicable maintenance instructions. However, owing to the number of different interfaces concerned, AIRBUS recommends that a non-revenue flight be carried out after changing or installing both engines to check that no double maintenance induced faults have been introduced. NOTE : It is recommended that operators avoid performing maintenance on ____ multiple engines installed on the same aircraft at the same time if at all possible. If it is not possible to avoid maintenance on more than one engine at the same time, it is recommended that different maintenance teams service each engine.
EFF : ALL 05-59-00 SROS
Page 1 Jul 01/06
FERRY FLIGHT WITH GEAR DOWN - MAINTENANCE PRACTICES ___________________________________________________ TASK 05-59-32-869-801 Preparation For Ferry Flight with Gear Down 1. __________________ Reason for the Job To prepare the aircraft for a ferry flight with gear down. R 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
access platform 2.5 m (8 ft. 2 in.)
3. __________ Job Set-up Subtask 05-59-32-941-050 A. General (1) You must put the aircraft systems in the ferry flight with gear down configuration before you can do such a flight. 4. Procedure _________ Subtask 05-59-32-020-050 A. Not applicable. Subtask 05-59-32-860-050 B. Put the Aircraft Systems in the Ferry Flight with Gear Down Configuration (1) Get Access to the Avionics Compartment (a) Put an access platform in position at the access door 811. (b) Open the access door 811.
EFF : ALL 05-59-32 SROS
Page 201 Jul 01/06
(2) In the avionics compartment, on the panel 808VU: (a) Lift the safety cover of the L/G DOWN VMO/MMO SELECTION switch. (b) Set the L/G DOWN VMO/MMO SELECTION switch to L/G ON. 5. Close-up ________ Subtask 05-59-32-942-050 A. Close-up (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. (4) Make an entry in the log book to tell the crew that: - the L/G DOWN VMO/MMO SELECTION switch is at L/G ON.
EFF : ALL 05-59-32 R SROS
Page 202 Jul 01/06
TASK 05-59-32-869-802 Return in Normal Operation after a Ferry flight with Gear Down 1. __________________ Reason for the Job You must put the aircraft in the normal configuration after a ferry flight. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
access platform 2.5 m (8 ft. 2 in.)
3. __________ Job Set-up Subtask 05-59-32-941-051 A. Not applicable. 4. Procedure _________ Subtask 05-59-32-860-051 A. Put the Aircraft Systems in the Normal Configuration after a Ferry Flight with Gear Down (1) Get Access to the Avionics Compartment (a) Put an access platform in position at the access door 811. (b) Open the access door 811. (2) In the avionics compartment, on the panel 808VU: (a) Set the L/G DOWN VMO/MMO SELECTION switch to NORM. (b) Lock the safety cover of the L/G DOWN VMO/MMO SELECTION switch. Subtask 05-59-32-420-050 B. Not applicable.
EFF : ALL 05-59-32 SROS
Page 203 Jan 01/05
5. Close-up ________ Subtask 05-59-32-942-051 A. Close-up (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. (4) Write in the log book that: - the L/G DOWN VMO/MMO SELECTION switch is set at NORM.
EFF : ALL 05-59-32 SROS
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CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS 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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601 601 602 603 604 605 606 607 608 601 602 603 604 605 606 607 608 609
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601 602 603 601 602 603 601 602 603 604 605 606 607 608
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05-28-20 05-28-20 05-28-20 05-28-20 05-28-20 05-28-20 05-28-20 05-28-20 05-28-20 05-28-20 05-28-20 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30 05-28-30
609 610 611 612 613 614 615 616 617 618 619 601 602 603 604 605 606 607 608 609 610 611 612 613 614 615 616 617 618 619 620 621 622 623
DATE Jul01/04 Apr01/04 Jul01/04 Jul01/04 Jul01/04 Apr01/04 Apr01/04 Apr01/04 Apr01/04 Apr01/04 Apr01/04 Apr01/04 Apr01/04 Jan01/06 Apr01/04 Jan01/04 Apr01/04 Jul01/05 Jul01/06 Jul01/06 Jul01/06 Apr01/04 Apr01/04 Jan01/05 Jan01/06 Jan01/06 Jan01/06 Jul01/04 Apr01/04 Jan01/06 Jan01/06 Jan01/06 Jul01/04 Jul01/04
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Jan01/07 Jan01/07 Apr01/98 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jul01/04 Jan01/07
CH/SE/SU 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11
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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 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-11 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-12 05-51-13 05-51-13 05-51-13 05-51-13 05-51-13 05-51-13 05-51-13 05-51-13 05-51-13 05-51-13 05-51-13 05-51-14 05-51-14 05-51-14
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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
Apr01/98 Jul01/05 Jan01/06 Jan01/02 Jan01/02 Jan01/02 Jan01/02 Apr01/98 Apr01/98 Apr01/98 Jan01/02 Jan01/02 Jan01/02 Jan01/06 Jul01/05 Jul01/05 Apr01/98 Apr01/98 Jul01/05 Jan01/02 Jul01/05 Oct01/03 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Oct01/03 Jan01/07 Jan01/07 Jan01/07
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DATE Jan01/07 Jul01/02 Apr01/02 Jan01/07 Jan01/07 Apr01/02 Jul01/05 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Apr01/98 Apr01/02 Jul01/05 Jul01/05 Apr01/98 Jul01/05 Apr01/02 Jan01/06 Jan01/06 Jan01/06 Jan01/02 Jan01/02 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jan01/02 Jul01/05 Oct01/00 Oct01/00 Jan01/07 Jul01/05 Jul01/05 Jul01/06 Jul01/06 Jul01/05 Jul01/05 Jul01/06 Jul01/06 Jul01/05 Jul01/05 Jul01/06 Jul01/06 Jul01/05 Jul01/05 Jul01/05 Jul01/05
CH/SE/SU 05-51-17 05-51-17 05-51-17 05-51-17 05-51-17 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-18 05-51-19 05-51-19 05-51-21 05-51-21 05-51-21 05-51-21
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DATE Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Apr01/99 Jul01/05 Jul01/05 Jan01/06 Apr01/98 Apr01/98 Apr01/98 Apr01/98 Apr01/98 Apr01/02 Apr01/02 Jan01/00 Jan01/00 Apr01/02 Apr01/02 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jan01/07 Apr01/02 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Apr01/02 Jul01/05 Jul01/05 Apr01/02 Apr01/02 Jan01/06 Jan01/06 Jul01/05 Apr01/02 Jul01/05 Jul01/05 Jul01/02 Jan01/07 Jan01/07 Jan01/07 Oct01/04 Apr01/98 Jan01/07
CH/SE/SU 05-51-22 05-51-22 05-51-22 05-51-22 05-51-22 05-51-22 05-51-22 05-51-23 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-24 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25
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DATE Apr01/98 Jan01/07 Jan01/02 Apr01/98 Jan01/07 Jan01/02 Oct01/00 Jan01/07 Jul01/05 Jul01/05 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jan01/06 Jul01/04 Jan01/06 Jan01/06 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jul01/04 Jan01/07 Jul01/05 Jul01/04 Jul01/04 Jul01/05 Jul01/04 Oct01/00 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/03 Jan01/03 Jan01/03 Jan01/03 Jan01/07 Jan01/03 Jan01/03 Jul01/05 Jul01/05 Jul01/06 Jul01/06 Jan01/03 Jan01/06 Jan01/06 Jan01/07
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CH/SE/SU 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-25 05-51-26 05-51-26 05-51-26 05-51-26 05-51-26 05-51-26 05-51-26 05-51-26 05-51-26 05-51-26 05-51-26 05-51-27 05-51-27 05-51-27 05-51-27 05-51-27 05-51-27 05-51-27 05-51-27 05-51-28 05-51-28 05-51-29 05-51-29 05-51-29 05-51-29 05-51-29 05-51-29 05-51-29
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DATE Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/07 Jan01/03 Jan01/03 Jan01/03 Jan01/03 Jan01/03 Jan01/07 Jan01/03 Jul01/05 Jul01/05 Jul01/06 Jul01/06 Jan01/06 Jul01/03 Jan01/03 Jan01/03 Jan01/03 Jan01/03 Jul01/02 Jan01/07 Jul01/05 Jan01/07 Jul01/05 Jan01/07 Jan01/07 Jul01/05 Jan01/07 Apr01/02 Jul01/05 Oct01/00 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Jul01/05 Oct01/03 Oct01/03 Oct01/03 Oct01/03 Oct01/03 Apr01/98 Apr01/98
CH/SE/SU 05-51-29 05-51-29 05-51-29 05-51-29 05-51-29 05-51-34 05-51-42 05-51-42 05-51-42 05-51-42 05-51-42 05-51-42 05-51-42 05-51-43 05-51-43 05-51-43 05-51-43 05-51-43 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44 05-51-44
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DATE Apr01/98 Oct01/03 Oct01/03 Oct01/03 Oct01/03 Jul01/05 Apr01/01 Jan01/07 Jan01/07 Jan01/07 Jul01/06 Apr01/01 Apr01/01 Jan01/06 Oct01/04 Oct01/04 Jul01/05 Oct01/04 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 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
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05-51-44 05-51-44 05-51-44 05-51-44 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00 05-53-00
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201 Jan01/07 202 Jul01/02 203 Apr01/98 601 602 603 604 605 606 607 608 609 610 611 612 613
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Jan01/07 Apr01/98 Apr01/98 Apr01/98 Apr01/98 Apr01/98 Apr01/98
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208 Apr01/98 209 Apr01/98 210 Apr01/98
05-59-00 05-59-32 05-59-32 05-59-32 05-59-32
1 201 202 203 204
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05-L.E.P. Page 7 Jan 01/07 SROS
CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS TABLE OF CONTENTS _________________ _______ SUBJECT TIME LIMITS - MAINTENANCE CHECKS __________________________________ _______ GENERAL DESCRIPTION AND OPERATION General Scheduled Maintenance Checks (05-20-00) Unscheduled Maintenance Checks (05-50-00) Time Limits And Maintenance Checks
________ CH/SE/SU 05-00-00
______________________________ SCHEDULED MAINTENANCE CHECKS MAINTENANCE MANUAL PROCEDURE ____________________________ DESCRIPTION AND OPERATION General Task Numbering Procedure Content
05-20-00
ZONAL INSPECTION : LOWER HALF OF FUSELAGE INSPECTION/CHECK General Visual Inspection as far as Visible from Ground of the Lower Half of the Fuselage Zonal Inspection of Lower Half of Fuselage General Visual Inspection of the Lower Half of the Fuselage ZONAL INSPECTION : RADOME INSPECTION/CHECK Zonal Inspection of Radome ZONAL INSPECTION : AVIONICS COMPARTMENT AND NOSE GEAR WELL INSPECTION/CHECK Zonal Inspection of Avionics Compartment Zonal Inspection of Avionics Compartment Zonal inspection of Nose Gear Well Zonal Inspection of the Nose Gear Well (zones 123 and 124). ZONAL INSPECTION : LOWER DECK FORWARD CARGO COMPARTMENT INSPECTION/CHECK Zonal Inspection of Forward Cargo Compartment Zonal Inspection of Forward Cargo
05-21-00
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05-21-10 05-21-20
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Page 1 Jan 01/07
CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS TABLE OF CONTENTS _________________ _______ SUBJECT Compartment Zonal Inspection of the Forward Cargo Compartment Zonal Inspection of Bay Under FWD Cargo Compartment Zonal Inspection of Bay behind FWD Cargo Compartment ZONAL INSPECTION : WING CENTER BOX, AIR CONDITIONING AND HYDRAULICS COMPARTMENTS INSPECTION/CHECK Zonal Inspection of Wing Center Box Zonal Inspection of Area Between Keel Beams Zonal Inspection of Zone Under Cabin Floor Zonal Inspection of MLG Well and Hydraulic Compartment General Visual Inspection of Centerline Gear Well ZONAL INSPECTION : LOWER DECK AFT CARGO COMPARTMENT INSPECTION/CHECK Zonal Inspection of Aft Cargo Compartment (if LD-MCR or LDF and/or DCR and/or ACT(s) installed, as far as visible) Zonal Inspection of Aft Cargo Compartment Zonal Inspection of Aft Cargo Compartment Zonal Inspection of Bay Under Aft Cargo Compartment ZONAL INSPECTION : LOWER DECK BULK CARGO COMPARTMENT INSPECTION/CHECK Zonal Inspection of Bulk Cargo Compartment Zonal Inspection of Bulk Cargo Compartment Zonal Inspection of Bulk Cargo Compartment Zonal Inspection of Bay Under Bulk Cargo Compartment ZONAL INSPECTION : AFT CABIN UNDERFLOOR COMPARTMENT
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05-21-40
05-21-50
05-21-60
05-21-70 05-CONTENTS
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Page 2 Oct 01/04
CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS TABLE OF CONTENTS _________________ _______ SUBJECT INSPECTION/CHECK Zonal Inspection of Aft Cabin Underfloor Compartment Zonal Inspection of Aft Cabin Underfloor Compartment ZONAL INSPECTION: AIR CONDITIONING, HYDRAULICS COMPARTMENTS AND FAIRINGS INSPECTION/CHECK Zonal Inspection of Air Conditioning Compt and Fairing Zonal Inspection of Air Conditioning Compt and Fairing Zonal Inspection of Hydraulic Compartment and Fairings Zonal Inspection of Hydraulics Compartment and Fairings Zonal Inspection of Rear Fairings Zonal Inspection of Rear Fairings Zonal Inspection of Air Conditioning Compartment and Fairing Zonal Inspection of Air Conditioning Compartment and Fairing
CH/SE/SU ________
ZONAL INSPECTION : UPPER HALF OF FUSELAGE INSPECTION/CHECK Zonal Inspection of the Upper Half of the fuselage (Zone 200). Zonal Inspection of Upper Half of Fuselage ZONAL INSPECTION : COCKPIT INSPECTION/CHECK Zonal Inspection of Cockpit Zonal Inspection of Cockpit ZONAL INSPECTION : FORWARD CABIN UTILITY AREAS INSPECTION/CHECK Zonal Inspection of FWD Cabin Utility Area Zonal Inspection of FWD Cabin Utility-Area Overhead-Compartment ZONAL INSPECTION: FORWARD CABIN AFT INSPECTION/CHECK Zonal Inspection of FWD Cabin
05-22-00
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05-21-90
05-22-10
05-22-20
05-22-30
05-CONTENTS R SROS
Page 3 Jan 01/06
CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS TABLE OF CONTENTS _________________ _______ SUBJECT Zonal Inspection of FWD Cabin Overhead Compartment ZONAL INSPECTION : MID CABIN UTILITY AREA AFT INSPECTION/CHECK Zonal Inspection of Mid Cabin Utility Area Zonal Inspection of Mid Cabin Utility Area Overhead Compt ZONAL INSPECTION : MID CABIN AFT OF MID CABIN UTILITY AREA TO FRONT OF AFT CABIN INSPECTION/CHECK Zonal Inspection of MID Cabin Zonal Inspection of MID Cabin Overhead Compartment ZONAL INSPECTION : AFT CABIN AFT OF MID CABIN TO FRONT OF AFT CABIN UTILITY AREA INSPECTION/CHECK Zonal Inspection of Aft Cabin Zonal Inspection of Aft Cabin Overhead Compartment ZONAL INSPECTION : AFT CABIN UTILITY AREA INSPECTION/CHECK Zonal Inspection of Aft Cabin Utility Area Zonal Inspection of Aft Cabin Utility Area Overhead Compt
CH/SE/SU ________
ZONAL INSPECTION : STABILIZERS AND FUSELAGE REAR SECTION INSPECTION/CHECK Zonal Inspection of the Stabilizers and the Fuselage Tail (zone 300). Zonal Inspection of Empennage and Rear Fuselage ZONAL INSPECTION : FUSELAGE REAR SECTION AFT OF AFT PRESSURE BULKHEAD INSPECTION/CHECK Zonal Inspection of Rear Fuselage Section Zonal Inspection of Tail Cone APU Air Intake Area Zonal Inspection of Tail Cone APU and Accessory Compt
05-23-00
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05-22-50
05-22-60
05-22-70
05-23-10
05-CONTENTS R SROS
Page 4 Oct 01/04
CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS TABLE OF CONTENTS _________________ _______ SUBJECT Zonal Inspection of Tail Cone APU Exhaust Area Zonal Inspection of Horizontal Stabilizer Center Box (Internal) ZONAL INSPECTION : VERTICAL STABILIZER AND RUDDER INSPECTION/CHECK Zonal Inspection of Dorsal Fin Zonal Inspection of Vertical Stabilizer Leading Edge Zonal Inspection of Vertical Stabilizer Spar Box Zonal Inspection of Vertical Stabilizer Spar Box Zonal Inspection of Vertical Stabilizer Tip Zonal Inspection of Vertical Stabilizer Trailing Edge Zonal Inspection of Vertical Stabilizer Trailing Edge Zonal Inspection of Rudder Zonal Inspection of Rudder Zonal Inspection of Rudder (Front Spar FWD Face and Internal Structure as far as visible) ZONAL INSPECTION : TRIMMABLE HORIZONTAL STABILIZER LEFT SIDE AND LEFT ELEVATOR INSPECTION/CHECK Zonal Inspection of Horizontal Stabilizer Leading Edge Zonal Inspection of Horizontal Stabilizer Tip Zonal Inspection of Horizontal Stabilizer Lateral Box Zonal Inspection of Horizontal Stabilizer Trailing Edge (From Fuselage Fairing to Rib 10) Zonal Inspection of Horizontal Stabilizer Trailing Edge (From Fuselage Fairing to Rib 21) Zonal Inspection of Elevator (Area between Ribs 8 and 9) Zonal Inspection of Elevator (Leading Edge as far as Visible)
CH/SE/SU ________
ZONAL INSPECTION : POWER PLANT, NACELLES
05-24-00
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604
ALL
607
ALL
610
ALL
613
ALL
616
ALL
619
ALL
05-23-20
05-23-30
05-CONTENTS R SROS
Page 5 Jul 01/06
CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS TABLE OF CONTENTS _________________ _______ SUBJECT AND PYLONS INSPECTION/CHECK Zonal Inspection as far as visible from the ground of the Power Plant, the Nacelles and the Pylons (zone 400). Zonal Inspection of Power Plants, Nacelles and Pylons. ZONAL INSPECTION : ENGINE INSPECTION/CHECK
CH/SE/SU ________
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PAGE ___________ ____ EFFECTIVITY 601 601
ALL ALL
602
ALL
601
601 601
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, 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,
609
701-749,
05-24-10 2
General Visual Inspection of the Engine Air Intake and Intake Lip
601
General Visual Inspection of the Engine Air Intake and Intake Lip
609
General Visual Inspection of the Fan Frame and Accessory Gear Box
614
General Visual Inspection of the Hot Section
618
General Visual Inspection of the Exhaust Nozzle
623
General Visual Inspection of the Fan Cowl
627
General Visual Inspection of the Thrust Reverser
632
INSPECTION/CHECK General Visual Inspection of Engine Air Intake and Intake General Visual Inspection of Engine Air Intake and Intake
3 the Lip the Lip
05-CONTENTS R SROS
201-249 255-299 401-449 201-249 255-299 401-449 201-249 255-299 401-449 201-249 255-299 401-449 201-249 255-299 401-449 201-249 255-299 401-449 201-249 255-299 401-449 201-249 255-299 401-449
Page 6 Jul 01/05
CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS TABLE OF CONTENTS _________________ _______ SUBJECT General Visual Inspection of Fan Frame and Accessory Gear General Visual Inspection of Hot Section General Visual Inspection of Exhaust Nozzle General Visual Inspection of Fan Cowl General Visual Inspection of Thrust Reverser ZONAL INSPECTION : ENGINE PYLON INSPECTION/CHECK
CH/SE/SU ________
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the Box the
____ ___________ PAGE EFFECTIVITY 614 701-749, 618
701-749,
the
623
701-749,
the
627
701-749,
the
632
701-749,
601
05-24-50 2
Pylon
601 601
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, 001-049, 251-252, 301-399, 451-499, 701-749, 701-749,
Upper
608
701-749,
Lower of
612
701-749,
Lower and
616
701-749,
Lower and
620
701-749,
Zonal Inspection of the Pylon Leading Edge
601
Zonal Inspection of the Upper Forward of the Pylon
607
Zonal Inspection of the Lower of the Pylon
611
Zonal Inspection of the Lower and Rear Pylon Fairings
615
Zonal Inspection of the Lower and Rear Pylon Fairings
619
INSPECTION/CHECK Zonal Inspection of the Leading Edge Zonal Inspection of the Forward of the Pylon Zonal Inspection of the the Pylon Zonal Inspection of the Rear Pylon Fairings Zonal Inspection of the Rear Pylon Fairings
3
05-CONTENTS R SROS
201-249 255-299 401-449 201-249 255-299 401-449 201-249 255-299 401-449 201-249 255-299 401-449 201-249 255-299 401-449 201-249 255-299 401-449
Page 7 Jul 01/05
CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS TABLE OF CONTENTS _________________ SUBJECT _______
CH/SE/SU ________
ZONAL INSPECTION : WING INSPECTION/CHECK Zonal Inspection as far as visible from the Ground of the Left and Right Wings (zone 500 and 600). Zonal Inspection of Wing Lower Surface Including Slats and Flaps Zonal Inspection of Wing Upper Surface (Including Slats, Flaps and Spoilers) ZONAL INSPECTION : WING FIXED LEADING EDGE INSPECTION/CHECK Zonal Inspection of Inboard Fixed Leading Edge Structure Zonal Inspection of Center Fixed Leading Edge Structure Zonal Inspection of Outer Fixed Leading Edge Structure ZONAL INSPECTION : WING FLAP TRACK FAIRINGS AND WING TIP INSPECTION/CHECK Zonal Inspection of Flap Tracks and Flap Track Fairings (Including RAT Attachment Points, as far as visible) Zonal inspection of Flap Tracks and Flap Track Fairings Zonal Inspection of Wing Tip. ZONAL INSPECTION : WING FUEL TANK INSPECTION/CHECK Zonal Inspection of Inner Fuel Tank. Zonal Inspection of Inner Fuel Tank (Rib 1 to Rib 23). Zonal Inspection of Outer Fuel Tank (Rib 23 to Rib 33). ZONAL INSPECTION : WING VENT SURGE TANK INSPECTION/CHECK Zonal Inspection of Vent Surge Tank ZONAL INSPECTION : AFT SECTION OF WING AND TRAILING EDGE FIXED STRUCTURE INSPECTION/CHECK Zonal Inspection of Main Landing
05-25-00
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PAGE ___________ ____ EFFECTIVITY 601 601
ALL ALL
602
ALL
605
ALL
601 601
ALL ALL
603
ALL
606
ALL
601 601
ALL ALL
604
ALL
607
ALL
601 601
ALL ALL
605
ALL
609
ALL
601 601
ALL ALL
601 601
ALL ALL
05-25-20
05-25-30
05-25-40
05-25-50
05-25-70
05-CONTENTS R SROS
Page 8 Jul 01/05
CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS TABLE OF CONTENTS _________________ _______ SUBJECT Gear Well. Zonal Inspection of Shroud Box. Zonal Inspection of Inner Trailing Edge Fixed Structure (RIB 6 to RIB 12) Zonal Inspection of Center Trailing Edge Fixed Structure (RIB 12 to RIB 27) Zonal Inspection of Outer Trailing Edge Fixed Structure (RIB 27 to RIB 39) ZONAL INSPECTION : WING AILERON INSPECTION/CHECK Zonal Inspection of Inboard Aileron. Zonal Inspection of Outboard Aileron.
CH/SE/SU ________
ZONAL INSPECTION : LANDING GEAR AND LANDING GEAR DOORS INSPECTION/CHECK Zonal inspection of Landing Gear and Landing Gear Doors. ZONAL INSPECTION : NOSE GEAR AND DOORS INSPECTION/CHECK Zonal Inspection of Nose Landing Gear. Zonal Inspection of the Nose Landing Gear (Zones 710) Zonal Inspection of Nose Landing Gear Main Doors. Zonal Inspection of Nose Landing Gear Aft Doors. ZONAL INSPECTION : MAIN LANDING GEAR AND DOORS INSPECTION/CHECK Zonal Inspection of LH and RH Main Landing Gear. Zonal Inspection of the Main Landing Gear (Zones 730 and 740). Zonal Inspection of Main Landing Gear Leg Doors. Zonal Inspection of Main Landing Gear Hinge Door. Zonal Inspection of Main Landing Gear Main Doors.
05-27-00
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PAGE ___________ ____ EFFECTIVITY 603 606
ALL ALL
609
ALL
612
ALL
601 601
ALL ALL
603
ALL
601 601
ALL ALL
601 601
ALL ALL
603
ALL
605
ALL
607
ALL
601 601
ALL ALL
603
ALL
604
ALL
606
ALL
608
ALL
05-25-90
05-27-10
05-27-30
05-CONTENTS R SROS
Page 9 Jul 01/06
CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS TABLE OF CONTENTS _________________ SUBJECT _______
CH/SE/SU ________
ZONAL INSPECTION : PASSENGER/CREW DOORS, CARGO COMPARTMENT DOORS AND EMERGENCY EXITS INSPECTION/CHECK Zonal Inspection as far as visible from the ground of the Doors (zone 800) Zonal Inspection of Doors ZONAL INSPECTION : FORWARD AVIONICS COMPARTMENT INSPECTION/CHECK Zonal Inspection of Forward Avionics Compartment Door ZONAL INSPECTION : LOWER DECK FORWARD AFT AND BULK CARGO COMPARTMENT DOORS INSPECTION/CHECK Zonal Inspection of Forward Cargo Compartment Door Zonal Inspection of Forward Cargo Compartment Door (Including Door Hinge Arms Attachment Area) Zonal Inspection of Aft Cargo Compartment Door Zonal Inspection of Aft Cargo Compartment Door (Including Door Hinge Arms Attachment Area) Zonal Inspection of Bulk Cargo Compartment Door (Including Fuselage Frames, Stop Fittings at Fuselage Frames, Door Seals, and Visible Part of Door Sill). Zonal Inspection of Bulk Cargo Compartment Door. Zonal Inspection of Forward Cargo Compartment Door Zonal Inspection of AFT Cargo Compartment Door. ZONAL INSPECTION : LEFT PASSENGER/ CREW DOORS AND EMERGENCY EXITS INSPECTION/CHECK Zonal Inspection of FWD Passenger/Crew Door (Including Door Stops on Fuselage Side, Door Seals and Scuff Plates) Zonal Inspection of FWD
05-28-00
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PAGE ___________ ____ EFFECTIVITY
601 601
ALL ALL
602
ALL
601 601
ALL ALL
601 601
ALL ALL
604
ALL
607
ALL
609
ALL
612
ALL
614
ALL
616
ALL
618
ALL
601 601
ALL ALL
603
ALL
05-28-10
05-28-20
05-28-30
05-CONTENTS R SROS
Page 10 Jul 01/05
CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS TABLE OF CONTENTS _________________ _______ SUBJECT Passenger/Crew Door Zonal Inspection of Emergency Exit (Including Door Stops on Fuselage Side, Door Seals and Scuff Plates) Zonal Inspection of Emergency Exit Zonal Inspection of Emergency Exit (Doors 3) Zonal Inspection of MID Passenger/Crew Doors Zonal Inspection of MID Passenger/Crew Door Zonal Inspection of AFT Passenger/Crew Doors Zonal Inspection of AFT Passenger/Crew Door
CH/SE/SU ________
______________________________ UNSCHEDULED MAINTENANCE CHECKS DESCRIPTION AND OPERATION General
05-50-00
_______________________________ UNSCHEDULED MAINTENANCE CHECKS MAINTENANCE PRACTICES Leaks - Permitted Values INSPECTIONS DESCRIPTION AND OPERATION General Inspection Coverage Inspection Sequence Inspection Presentation INSPECTION AFTER HARD/OVERWEIGHT LANDING INSPECTION/CHECK Inspection after Hard/Overweight Landing INSPECTION AFTER LANDING GEAR DOWN LIMITING SPEED EXCEEDED INSPECTION/CHECK Inspection After Landing Gear Extension at More than the Gear Down Limiting Speed. INSPECTION AFTER FLAP/SLAT LIMITING SPEED EXCEEDED INSPECTION/CHECK Inspection after Flap/Slat
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PAGE ___________ ____ EFFECTIVITY 606
ALL
608 611
ALL ALL
614
ALL
616
ALL
619
ALL
621
ALL
1 1
ALL ALL
201 201
ALL ALL
1 1 1 1 2
ALL ALL ALL ALL ALL
601 601
ALL ALL
601 601
ALL ALL
601 601
ALL ALL
05-50-00
05-51-00
05-51-11
05-51-12
05-51-13
05-CONTENTS R SROS
Page 11 Jul 01/05
CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS TABLE OF CONTENTS _________________ _______ SUBJECT Extension at more than the Flap/Slat Limiting Speed INSPECTION OF AIRFRAME AFTER BIRD OR HAIL STRIKE INSPECTION/CHECK Inspection of the Aircraft after a Bird or a Hail Strike INSPECTION AFTER A TIRE BURST OR TREAD THROW OR WHEEL FAILURE INSPECTION/CHECK Inspection of the Aircraft after a Tire Burst or Tread Throw or Wheel Failure INSPECTION AFTER BRAKE EMERGENCY APPLICATION OR OVERHEAT INSPECTION/CHECK Inspection After Brake Overheat INSPECTION AFTER FLIGHT IN EXCESSIVE TURBULENCE OR IN EXCESS OF VMO INSPECTION/CHECK Inspection after Flight in Excessive Turbulence or in Excess of VMO/MMO INSPECTION AFTER LIGHTNING STRIKE INSPECTION/CHECK Inspection after Lightning Strike INSPECTION AFTER ENGINE BIRD STRIKE OR SLUSH INGESTION INSPECTION/CHECK Inspection after Engine Bird Strike or Slush Ingestion INSPECTION AFTER TAIL RUNWAY IMPACT INSPECTION/CHECK Inspection after a Tail Runway Impact INSPECTION AFTER NLG TOWING OVERLOAD OR OVERRUN INSPECTION/CHECK Inspection after NLG Towing Overload or Overrun INSPECTION AFTER NLG STEERING ANGLE EXCEEDED INSPECTION/CHECK Inspection of the Nose Landing Gear after a NLG Steering Angle of more than 95⁰
CH/SE/SU ________
C _
PAGE ___________ ____ EFFECTIVITY
05-51-14 601 601
ALL ALL
601 601
ALL ALL
601 601
ALL ALL
601 601
ALL ALL
601 601
ALL ALL
601 601
ALL ALL
601 601
ALL ALL
601 601
ALL ALL
601 601
ALL ALL
05-51-15
05-51-16
05-51-17
05-51-18 05-51-19
05-51-21
05-51-22
05-51-23
05-CONTENTS R SROS
Page 12 Jul 01/05
CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS TABLE OF CONTENTS _________________ _______ SUBJECT INSPECTION AFTER LEAVING RUNWAY OR TAXIWAY INSPECTION/CHECK Inspection after Leaving a Runway or a Taxiway INSPECTION AFTER FLIGHT THROUGH DUST STORM/VOLCANIC ASH OR SEVERE CONDITION ON GROUND INSPECTION/CHECK Inspection after Flight through Dust Storm or Dust contamination on Ground Inspection after Flight through Volcanic Ash or Volcanic Ash contamination on Ground INSPECTION AFTER ENGINE FAILURE INSPECTION/CHECK Inspection of the Aircraft after Engine Failure INSPECTION AFTER IMPACT ON ENGINE COWLS INSPECTION/CHECK Inspection after Impact on Engine Cowls INSPECTION AFTER SPILLAGE INSPECTION/CHECK Inspection after Spillage INSPECTION AFTER ABNORMAL PAX/CREW DOOR MOVEMENT INSPECTION/CHECK Inspection after Abnormal Pax/Crew Door Movement. INSPECTION AFTER ENGINE WINDMILLING (AFTER ENGINE IN-FLIGHT SHUT-DOWN) INSPECTION/CHECK Inspection after Engine Windmilling (after Engine In-Flight Shut-Down) INSPECTION AFTER VERY HIGH WINDS ON GROUND INSPECTION/CHECK Inspection after Very High Winds on Ground INSPECTIONS AFTER WORK ON SYSTEM ELECTRICAL INSTALLATION ADJUSTMENT/TEST
________ CH/SE/SU 05-51-24
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PAGE ___________ ____ EFFECTIVITY 601 601
ALL ALL
601 601
ALL ALL
620
ALL
601 601
ALL ALL
601 601
ALL ALL
601 601
ALL ALL
601 601
ALL ALL
601 601
ALL ALL
601 601
ALL ALL
501
ALL
05-51-25
05-51-26
05-51-27
05-51-28 05-51-29
05-51-34
05-51-42
05-51-43
05-CONTENTS R SROS
Page 13 Jul 01/05
CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS TABLE OF CONTENTS _________________ _______ SUBJECT Inspection after Work on System Electrical Installation INSPECTION AFTER FLIGHT WITH HIGH LATERAL LOADS INSPECTION/CHECK INSPECTION AFTER FLIGHT WITH HIGH LATERAL LOADS
CH/SE/SU ________
PRESSURIZATION TEST OF FUSELAGE (LEAKAGE CHECKS) AFTER A/C ABNORMAL OPERATION OR REPAIR ADJUSTMENT/TEST Pressurization Retest and Leakage Rate Measurement Pressurization Retest and Leakage Rate Measurement (with ACMS)
05-53-00
DEMAGNETIZATION MAINTENANCE PRACTICES Demagnetization of the External Parts of the Frames of the Windshield and Sliding Windows
05-54-00
MEASUREMENT AFTER ABNORMAL OPERATION OF THE AIRCRAFT INSPECTION/CHECK Measurement of the Aircraft by Photogrammetry after Abnormal Operation of the Aircraft
05-56-00
AIRCRAFT STABILITY MAINTENANCE PRACTICES Aircraft Stability
05-57-00
NON-REVENUE FLIGHT - REQUIREMENTS FOLLOWING MAINTENANCE ACTIONS DESCRIPTION AND OPERATION General Engine Replacement Replacement or reinstallation of both engines does not require a non-revenue flight providing the engines have been successfully FERRY FLIGHT WITH GEAR DOWN MAINTENANCE PRACTICES Preparation For Ferry Flight with
05-59-00
C _
____ ___________ PAGE EFFECTIVITY 501 ALL
05-51-44 601 601
ALL ALL
501 501
ALL ALL
511
ALL
201 201
ALL ALL
601 601
ALL ALL
201 201
ALL ALL
1 1 1
ALL ALL ALL
201 201
ALL ALL
05-59-32
05-CONTENTS R SROS
Page 14 Jul 01/06
CHAPTER 05 __________ TIME LIMITS/MAINTENANCE CHECKS TABLE OF CONTENTS _________________ _______ SUBJECT Gear Down Return in Normal Operation after a Ferry flight with Gear Down
CH/SE/SU ________
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PAGE ___________ ____ EFFECTIVITY 203
ALL
05-CONTENTS SROS
Page 15 Jul 01/06
TIME LIMITS - MAINTENANCE CHECKS - GENERAL - DESCRIPTION AND OPERATION ______________________________________________________________________ R R R
1. _______ General This chapter includes the following sections: 05-20-00: SCHEDULED MAINTENANCE CHECKS 05-50-00: UNSCHEDULED MAINTENANCE CHECKS
R R R
A. Scheduled Maintenance Checks (05-20-00) This section includes all the zonal inspections that you must do on the aircraft.
R R R R R R
B. Unscheduled Maintenance Checks (05-50-00) This section includes the maintenance checks that you must do when a flight crew report shows abnormal flight conditions. This section is divided into two categories of information: - inspections - checks.
R R R R R R R R R R R
2. Time __________________________________ Limits And Maintenance Checks The part of the Aircraft Maintenance Manual (AMM) was previously issued in a separate Manual to this AMM with the title: ------------------------------------------------------------------------------Aircraft Maintenance Manual CHAPTER 05 Time Limits and Maintenance Checks ------------------------------------------------------------------------------The content of this manual, since revision 09 approved on NOV 13, 2001, is into the Maintenance Planning Document(MPD) - Section 9.1 : Life Limits/Monitored Parts.
EFF : ALL 05-00-00 SROS
Page 1 Jan 01/07
___________________________________________________________ SCHEDULED MAINTENANCE CHECKS - MAINTENANCE MANUAL PROCEDURE DESCRIPTION AND OPERATION _________________________ 1. General _______ A. Task Numbering This section gives the accomplishment instructions for zonal inspection tasks; - related to the requirements of the Maintenance Planning Document (MPD), a specific AMTOSS zonal task number which combines the ATA 05-20 and the concerned A/C zone is used as follows: Task Numbering System for Zonal Inspection Tasks. ATA Reference Number II TASK No. 0 5 - 2 2 - 6 0 - 2 0 0 - 0 0 1 I__I I I________I I_____I I_____I 1 2 3 4 5 1 : ATA 2 : Relates to ATA section 20 scheduled maintenance checks 3 : Zone 4 : Function code, e.g. 200 : INSPECTION CHECK 5 : Unique identification of discrete tasks B. Procedure Content (1) It is thought that people who do the zonal tasks have an adequate knowledge of the aircraft construction and systems installations; thus a list of all the items contained in the zones to be inspected is not given. (2) If you find damage, corrosion, leaks, it is recommended to refer to the related structure/system inspection ATA-chapter for detailed inspection and corrective action (3) During the zonal inspection, you must also examine any fairing, access panel, access door, etc. which you remove or open to gain access to zones. This requirement is not given in each individual procedure because it is a standard maintenance practice.
EFF : ALL 05-20-00 SROS
Page 1 Apr 01/98
ZONAL INSPECTION : LOWER HALF OF FUSELAGE - INSPECTION/CHECK ____________________________________________________________ TASK 05-21-00-200-801 General Visual Inspection as far as Visible from Ground of the Lower Half of the Fuselage 1. __________________ Reason for the Job R
NOTE : This task can contribute to fuel savings. ____ 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------53-35-00-200-801
Inspection of the Wing-to-Fuselage Fairings and Belly Fairing Access Panels for Missing Fasteners
3. __________ Job Set-up Subtask 05-21-00-869-050 A. Not applicable. 4. Procedure _________ Subtask 05-21-00-210-050 A. Inspection. (1) Do a general visual inspection of the lower half of the fuselage from the ground during the aircraft walkaround. (2) Inspect the belly fairing access panels and the wing-to-fuselage fairings for missing fasteners (Ref. TASK 53-35-00-200-801).
EFF : ALL 05-21-00 SROS
Page 601 Jan 01/07
TASK 05-21-00-200-802 Zonal Inspection of Lower Half of Fuselage 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-100-01 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
1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------53-35-00-200-801
Inspection of the Wing-to-Fuselage Fairings and Belly Fairing Access Panels for Missing Fasteners
3. __________ Job Set-up Subtask 05-21-00-010-050 A. Get Access R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at zone 100.
EFF : ALL 05-21-00 SROS
Page 602 Jan 01/07
4. Procedure _________ Subtask 05-21-00-210-051 A. Inspection R R
(1) Do a general visual inspection of the bottom half of the fuselage at zone 100 (below cabin floor). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see.
R R
(2) Inspect the belly-fairing access panels and the wing-to-fuselage fairings for missing fasteners (Ref. TASK 53-35-00-200-801).
R
5. Close-up ________
R
Subtask 05-21-00-860-051
R
A. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-00 SROS
Page 603 Jan 01/04
TASK 05-21-00-200-803 General Visual Inspection of the Lower Half of the Fuselage 1. __________________ Reason for the Job R R
Self Explanatory 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
access platform 2.5 m (8 ft. 2 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------53-35-00-200-801
Inspection of the Wing-to-Fuselage Fairings and Belly Fairing Access Panels for Missing Fasteners
3. __________ Job Set-up Subtask 05-21-00-010-051 A. Get Access (1) Put an access platform in position in the lower half of the fuselage. 4. Procedure _________ Subtask 05-21-00-210-052 A. Inspection of the Lower Half of the Fuselage (1) Do a general visual inspection of the lower half of the fuselage zone 100 (below cabin floor). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see.
EFF : ALL 05-21-00 SROS
Page 604 Jan 01/06
R R
(2) Inspect the belly fairing access panels and the wing-to-fuselage fairings for missing fasteners (Ref. TASK 53-35-00-200-801). 5. Close-up ________ Subtask 05-21-00-410-051 A. Close Access (1) Remove the access platform(s).
EFF : ALL 05-21-00 SROS
Page 605 Oct 01/02
ZONAL INSPECTION : RADOME - INSPECTION/CHECK ____________________________________________ TASK 05-21-10-200-801 R
Zonal Inspection of Radome 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-110-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 4M (13 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R
53-15-11-010-801 53-15-11-410-801
Opening of the Radome Closing of the Radome
3. __________ Job Set-up Subtask 05-21-10-010-050 A. Get Access R R
(1) Put an ACCESS PLATFORM 4M (13 FT) in position at zone 110.
R
(2) Open the radome 110AL (Ref. TASK 53-15-11-010-801).
EFF : ALL 05-21-10 SROS
Page 601 Jan 01/04
4. Procedure _________ Subtask 05-21-10-210-050 A. Do a general visual inspection of the radome. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-21-10-410-050 A. Close Access (1) Close the radome 110AL (Ref. TASK 53-15-11-410-801). R R R
Subtask 05-21-10-860-050 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-10 SROS
Page 602 Jan 01/04
ZONAL INSPECTION : AVIONICS COMPARTMENT AND NOSE GEAR WELL - INSPECTION/CHECK _____________________________________________________________________________ TASK 05-21-20-200-801 R
Zonal Inspection of Avionics Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-121-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------52-30-00-010-801 52-30-00-410-801 R
05-21-20-991-002
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 Fig. 601
3. __________ Job Set-up Subtask 05-21-20-010-050 A. Get Access R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at zone 821. (2) Open the forward cargo-compartment door 821 (Ref. TASK 52-30-00-010801).
R R
(3) Open the access door 132AZ (Ref. Fig. 601/TASK 05-21-20-991-002)
EFF : ALL 05-21-20 SROS
Page 601 Jan 01/04
R R
Forward Cargo-Compartment Partition Panels, FR20 Figure 601/TASK 05-21-20-991-002
EFF : ALL 05-21-20 SROS
Page 602 Jan 01/04
4. Procedure _________ Subtask 05-21-20-210-050 A. Inspection (1) Do a general visual inspection of the forward avionics compartment (zones 121 and 122). (2) Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. (3) Make sure that all the installations (wiring, ducting, piping) are attached correctly. 5. Close-up ________ Subtask 05-21-20-410-050 A. Close Access (1) Close the access door 132AZ. (2) Close the forward cargo-compartment door 821 (Ref. TASK 52-30-00-410801). (3) Remove the access platform(s). R R
Subtask 05-21-20-860-050 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-20 SROS
Page 603 Jan 01/04
TASK 05-21-20-200-802 Zonal Inspection of Avionics Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-121-02 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 ------------------------------------------------------------------------------R R R R R
25-52-00-000-801 25-52-00-400-801 52-30-00-010-801 52-30-00-410-801
R
53-12-13-000-801 53-12-13-400-801 05-21-20-991-001-A
Removal of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the FWD Cargo Compartment Installation of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the FWD Cargo Compartment 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 Removal of the Avionics-Compartment Floor Panels Installation of the Avionics-Compartment Floor Panels Fig. 602
EFF : ALL 05-21-20 SROS
Page 604 Jan 01/07
3. __________ Job Set-up R R R
(Ref. Fig. 602/TASK 05-21-20-991-001-A) Subtask 05-21-20-010-051-A A. Get Access
R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at zone 821.
R R
(2) Open the forward cargo-compartment door 821 (Ref. TASK 52-30-00-010801).
R
(3) Open the access door 132AZ.
R R
(4) Remove the partition panels 131AW, 131BW and 132CW at FR20 (Ref. TASK 25-52-00-000-801).
R R R R
(5) Remove the floor panels: 121AF, 121BF, 121CF, 121DF, 121EF, 121FF, 121GF, 121HF, 121KF, 122CF, 122DF, 122FF, 122GF, 122HF, 122LF, 122KF, 122JF, 122NF and 122PF from the forward cabin utility-area (Ref. TASK 53-12-13-000-801). 4. Procedure _________ Subtask 05-21-20-210-051 A. Inspection (1) Do a general visual inspection of the forward avionics compartment (zones 121 and 122). (2) Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. (3) Make sure that all the installations (wiring, ducting, piping) are attached.
EFF : ALL 05-21-20 SROS
Page 605 Jan 01/07
R R
Floor Panels of the Avionics Compartment Figure 602/TASK 05-21-20-991-001-A
R EFF : ALL 05-21-20 SROS
Page 606 Jan 01/07
5. Close-up ________ R R
Subtask 05-21-20-410-051-A A. Close Access
R R R
(1) Install the floor panels: 121AF, 121BF, 121CF, 121DF, 121EF, 121FF, 121GF, 121HF, 121KF, 122CF, 122DF, 122FF, 122GF, 122HF, 122LF, 122KF, 122JF, 122NF and 122PF (Ref. TASK 53-12-13-400-801).
R R
(2) Install the partition panels 131AW, 131BW and 132CW at FR20 (Ref. TASK 25-52-00-400-801).
R
(3) Close the access door 132AZ.
R R
(4) Close the forward cargo-compartment door 821 (Ref. TASK 52-30-00-410801). Subtask 05-21-20-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-20 SROS
Page 607 Jan 01/07
TASK 05-21-20-200-803 Zonal inspection of Nose Gear Well 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 Refer to the MPD TASK: ZL-123-01 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 ------------------------------------------------------------------------------32-22-00-010-801 32-22-00-410-801
Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-21-20-010-052 A. Get Access (1) Open the nose landing gear doors 713, 714 (Ref. TASK 32-22-00-010801). (2) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at zone 713 (714).
EFF : ALL 05-21-20 R SROS
Page 608 Jan 01/07
4. Procedure _________ Subtask 05-21-20-210-052 A. Inspection (1) Do a general visual inspection of the nose gear well (zone 123). (2) Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. (3) Make sure that all the installations (wiring, ducting, piping) are attached correctly. 5. Close-up ________ Subtask 05-21-20-410-052 A. Close Access (1) Close the nose-landing-gear doors 713, 714 (Ref. TASK 32-22-00-410801). Subtask 05-21-20-860-052 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-20 R SROS
Page 609 Jan 01/07
TASK 05-21-20-200-804 Zonal Inspection of the Nose Gear Well (zones 123 and 124). 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-22-00-010-801 32-22-00-410-801
Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-21-20-010-053 A. Get Access (1) Open the nose landing gear doors 713, 714 (Ref. TASK 32-22-00-010801). 4. Procedure _________ Subtask 05-21-20-210-053 A. Inspection (1) Do a general visual inspection of the nose gear well, from the ground, as far as visible (zones 123 and 124). (2) Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. (3) Make sure that all the installations (wiring, ducting, piping) are attached correctly.
EFF : ALL 05-21-20 R SROS
Page 610 Jan 01/07
5. Close-up ________ Subtask 05-21-20-410-053 A. Close Access (1) Close the nose landing gear doors 713, 714 (Ref. TASK 32-22-00-410801).
EFF : ALL 05-21-20 R SROS
Page 611 Jan 01/07
ZONAL INSPECTION : LOWER DECK FORWARD CARGO COMPARTMENT - INSPECTION/CHECK __________________________________________________________________________ TASK 05-21-30-200-801 R
Zonal Inspection of Forward Cargo Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-131-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------52-30-00-010-801 52-30-00-410-801
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 05-21-30-010-050 A. Get Access R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at zone 821. (2) Open the forward cargo-compartment door 821 (Ref. TASK 52-30-00-010801).
EFF : ALL 05-21-30 SROS
Page 601 Jan 01/04
4. Procedure _________ Subtask 05-21-30-210-050 A. Do a general visual inspection of the forward cargo compartment (zones 131 and 132). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (wiring, ducting, piping) are attached correctly. 5. Close-up ________ Subtask 05-21-30-410-050 A. Close Access (1) Close the forward cargo door 821 (Ref. TASK 52-30-00-410-801). R R R
Subtask 05-21-30-860-050 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-30 SROS
Page 602 Jan 01/04
TASK 05-21-30-200-802 R
Zonal Inspection of Forward Cargo Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-131-02 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 ------------------------------------------------------------------------------25-52-00-000-801 25-52-00-400-801
Removal of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the FWD Cargo Compartment Installation of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the FWD Cargo Compartment 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
52-30-00-010-801 52-30-00-410-801 3. __________ Job Set-up Subtask 05-21-30-010-051-A A. Get Access
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at access door 821. (2) Open the forward cargo-compartment door 821 (Ref. TASK 52-30-00-010801).
EFF : ALL 05-21-30 SROS
Page 603 Jul 01/06
R R
(3) Remove the sidewall panels: 131FX, 131KW, 132UW, 132WW, 132FX (Ref. TASK 25-52-00-000-801).
R
(4) Remove the ceiling panels: 131BC, 131FC, 131XC, 131PC, 131RC, 131TC, 131VC (Ref. TASK 25-52-00-000-801). 4. Procedure _________ Subtask 05-21-30-210-051
R
A. Do a general visual inspection of the forward cargo compartment. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting, piping) are attached correctly. 5. Close-up ________ Subtask 05-21-30-410-051-A A. Close Access
R R
(1) Install the ceiling panels: 131BC, 131FC, 131XC, 131PC, 131RC, 131TC, 131VC (Ref. TASK 25-52-00-400-801).
R R
(2) Install the sidewall panels: 131FX, 131KW, 132UW, 132WW, 132FX (Ref. TASK 25-52-00-400-801). (3) Make sure that the work area is clean and clear of tools and other items. (4) Close the forward cargo-compartment door 821 (Ref. TASK 52-30-00-410801). Subtask 05-21-30-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-21-30 SROS
Page 604 Jul 01/06
TASK 05-21-30-200-803 R
Zonal Inspection of the Forward Cargo Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-131-03 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------25-52-00-000-801 25-52-00-400-801 52-30-00-010-801 52-30-00-410-801
Removal of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the FWD Cargo Compartment Installation of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the FWD Cargo Compartment 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 05-21-30-010-052 A. Get Access R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at access door 821. (2) Open the forward cargo door 821 (Ref. TASK 52-30-00-010-801). (3) Remove the sidewall and ceiling panels from FR20 to FR39.2 (Ref. TASK 25-52-00-000-801).
EFF : ALL 05-21-30 SROS
Page 605 Jan 01/04
4. Procedure _________ Subtask 05-21-30-210-052
R
A. Do a general visual inspection of the forward cargo compartment. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping) are attached correctly. NOTE : Lift the insulation sufficiently to make sure that there is no ____ corrosion or signs of leaks. 5. Close-up ________ Subtask 05-21-30-410-052 A. Close Access
R R
(1) Install the sidewall and ceiling panels from FR20 to FR39.2 (Ref. TASK 25-52-00-400-801).
R
(2) Make sure that the work area is clean and clear of tools and other items.
R R
(3) Close the forward cargo door (Ref. TASK 52-30-00-410-801).
R R
Subtask 05-21-30-860-052 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-30 SROS
Page 606 Jan 01/04
TASK 05-21-30-200-804 R
Zonal Inspection of Bay Under FWD Cargo Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-133-01 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 ------------------------------------------------------------------------------52-30-00-010-801 52-30-00-410-801 53-00-00-000-802 53-00-00-400-802 R
05-21-30-991-007
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 Removal of the Floor Panels in the FWD Cargo-Compartment Installation of the Floor Panels in the FWD Cargo-Compartment Fig. 601
3. __________ Job Set-up Subtask 05-21-30-010-053 A. Get Access R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at access door 821. (2) Open the forward cargo door 821 (Ref. TASK 52-30-00-010-801). (3) Remove the floor panels from FR20 to FR39 (Ref. TASK 53-00-00-000802).
EFF : ALL 05-21-30 SROS
Page 607 Jul 01/04
R
(4) Lift the insulation.
R R
(5) Remove the access panels 133AL, 133BL. (Ref. Fig. 601/TASK 05-21-30-991-007) 4. Procedure _________ Subtask 05-21-30-210-053
R R R
A. Do a general visual inspection of the bay below the forward cargo-compartment floor (Zones 133 and 134).
R
(1) Make sure that: (a) there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. (b) all the installations (wiring, ducting, piping) are attached correctly. 5. Close-up ________ Subtask 05-21-30-410-053 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Put the insulation back in position.
R
(3) Install the access panels 133AL, 133BL.
R
(4) Install the floor panels from FR20 to FR39 (Ref. TASK 53-00-00-400802).
R
(5) Close the forward cargo door 821 (Ref. TASK 52-30-00-410-801). Subtask 05-21-30-860-053 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-21-30 SROS
Page 608 Jul 01/04
R R
Access Panels of the Forward-Fuselage Lower Section Figure 601/TASK 05-21-30-991-007
EFF : ALL 05-21-30 SROS
Page 609 Jul 01/04
TASK 05-21-30-200-806 R
Zonal Inspection of Bay behind FWD Cargo Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-137-01 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 ------------------------------------------------------------------------------25-52-00-000-801 25-52-00-400-801 52-30-00-010-801 52-30-00-410-801 53-00-00-000-802 53-00-00-400-802
Removal of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the FWD Cargo Compartment Installation of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the FWD Cargo Compartment 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 Removal of the Floor Panels in the FWD Cargo-Compartment Installation of the Floor Panels in the FWD Cargo-Compartment
EFF : ALL 05-21-30 SROS
Page 610 Jul 01/04
3. __________ Job Set-up Subtask 05-21-30-010-055 A. Get Access R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at access door 821. (2) Open the forward cargo-compartment door 821 (Ref. TASK 52-30-00-010801).
R R
(3) Remove the partition panels: 132DX, 132CX, 131BX, 131CX, 131DX (Ref. TASK 25-52-00-000-801).
R
(4) Remove the floor panels: 131DG, 132CG, 132DG, 131CG (Ref. TASK 53-0000-000-802). 4. Procedure _________ Subtask 05-21-30-210-055 A. Do a general visual inspection of the bay behind the forward cargo compartment (zones 137 and 138). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping) are attached correctly. 5. Close-up ________ Subtask 05-21-30-410-055 A. Close Access
R
(1) Install the floor panels: 131DG, 131CG, 132DG, 132CG (Ref. TASK 5300-00-400-802).
R R
(2) Install the partition panels: 132DX, 132CX, 131BX, 131CX, 131DX (Ref. TASK 25-52-00-400-801). (3) Close the forward cargo door (Ref. TASK 52-30-00-410-801). (4) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-30 SROS
Page 611 Jul 01/04
Subtask 05-21-30-860-054 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-21-30 SROS
Page 612 Jul 01/04
___________________________________________________________________ ZONAL INSPECTION : WING CENTER BOX, AIR CONDITIONING AND HYDRAULICS COMPARTMENTS - INSPECTION/CHECK _______________________________ TASK 05-21-40-200-801 R
Zonal Inspection of Wing Center Box WARNING : OBEY THE SAFETY PROCEDURES WHEN YOU DO WORK IN A FUEL TANK. _______ THIS WILL PREVENT INJURY OR DAMAGE. WARNING : DO NOT GET AIRCRAFT FUEL: _______ - IN YOUR MOUTH - IN YOUR EYES - ON YOUR SKIN FOR A LONG TIME. 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 Refer to the MPD TASK: ZL-141-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-12-00-010-801 32-12-00-410-801 57-17-11-000-801 57-17-11-400-801
Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Removal of the Covers 147AZ (148AZ) Installation of the Covers 147AZ (148AZ)
EFF : ALL 05-21-40 SROS
Page 601 Jan 01/04
3. __________ Job Set-up Subtask 05-21-40-010-050 A. Get Access R
(1) Open the main-landing-gear doors: 734 and 744.(Ref. TASK 32-12-00010-801)
R R
(2) Put an ACCESS PLATFORM 2M (6 FT) in position at the access doors 734 and 744. (3) Remove the cover panels 147AZ, 148AZ (Ref. TASK 57-17-11-000-801). 4. Procedure _________ Subtask 05-21-40-210-050
R R
A. Do a general visual inspection of the wing center box (zones 141 and 142). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting) are attached correctly. 5. Close-up ________ Subtask 05-21-40-410-050 A. Close Access (1) Install the cover panels 147AZ, 148AZ, (Ref. TASK 57-17-11-400-801).
R R
(2) Close the main-landing gear doors 734 and 744. (Ref. TASK 32-12-00410-801)
EFF : ALL 05-21-40 SROS
Page 602 Jan 01/04
TASK 05-21-40-200-802 R R
Zonal Inspection of Area Between Keel Beams 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 Refer to the MPD TASK: ZL-143-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-12-00-010-801 32-12-00-410-801
Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-21-40-010-052 A. Get Access R
(1) Open the main-landing-gear doors 734, 744 (Ref. TASK 32-12-00-010801).
R
(2) Put an ACCESS PLATFORM 2M (6 FT) in position at the access doors 734 and 744.
EFF : ALL 05-21-40 SROS
Page 603 Jan 01/04
4. Procedure _________ Subtask 05-21-40-210-052 R R R
A. Do a general visual inspection of the area between the keel beams (zone 143). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping) are attached correctly. 5. Close-up ________ Subtask 05-21-40-410-052 A. Close Access
R R R R
(1) Close the main-landing-gear doors 734, 744 (Ref. TASK 32-12-00-410801). Subtask 05-21-40-860-051 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-40 SROS
Page 604 Jan 01/04
TASK 05-21-40-200-803 R R
Zonal Inspection of Zone Under Cabin Floor 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-145-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R R
52-10-00-010-801 52-10-00-410-801 53-00-00-000-801 53-00-00-400-801
Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door Removal of the Floor Panels in the Cabin from FR17 to FR80 Installation of the Floor Panels in the Cabin from FR17 to FR80
3. __________ Job Set-up Subtask 05-21-40-010-053 A. Get Access R R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the access doors 834 and 844. (2) Open the Mid passenger/crew door (Ref. TASK 52-10-00-010-801).
R R
(3) Remove the floor panels in the cabin from FR40 to FR53.2 (Ref. TASK 53-00-00-000-801).
EFF : ALL 05-21-40 SROS
Page 605 Jan 01/04
4. Procedure _________ Subtask 05-21-40-210-053
R
A. Do a general visual inspection of the pressurized zone under the cabin floor. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping) are attached correctly. 5. Close-up ________ Subtask 05-21-40-410-053 A. Close Access
R R
(1) Install the floor panels in the cabin from FR40 to FR53.2 (Ref. TASK 53-00-00-400-801). (2) Close the Mid Passenger/crew door (Ref. TASK 52-10-00-410-801).
R R R
Subtask 05-21-40-860-052 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-40 SROS
Page 606 Jan 01/04
TASK 05-21-40-200-804 Zonal Inspection of MLG Well and Hydraulic Compartment 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 Refer to the MPD TASK: ZL-147-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-12-00-010-801 32-12-00-410-801
Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-21-40-010-054 A. Get Access (1) Open the main-landing-gear doors 734, 744 (Ref. TASK 32-12-00-010801). (2) Put ACCESS PLATFORM 2M (6 FT) in position at the access doors 734 and 744.
EFF : ALL 05-21-40 R SROS
Page 607 Jul 01/06
4. Procedure _________ Subtask 05-21-40-210-054 R
A. Do a general visual inspection of the main-landing-gear well and the hydraulics compartment (zones 147 and 148). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts. - all the installations (ducting) are attached correctly. 5. Close-up ________ Subtask 05-21-40-410-054 A. Close Access (1) Close the main-landing-gear doors 734, 744 (Ref. TASK 32-12-00-410801). Subtask 05-21-40-860-054 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-40 SROS
Page 608 Jul 01/06
R
TASK 05-21-40-200-809
R
General Visual Inspection of Centerline Gear Well
R
1. __________________ Reason for the Job
R R R
Refer to the MPD TASK: ZL-149-05 2. ______________________ Job Set-up Information A. Referenced Information
R R R
------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R
32-12-00-010-801 32-12-00-410-801
R
3. __________ Job Set-up
R
Subtask 05-21-40-010-058
R
Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance
A. Get Access
R
(1) Open the ground opening-handle access-doors 149AB, 149CB.
R R
(2) Open the main landing gear doors 734, 744 (Ref. TASK 32-12-00-010801).
R
4. Procedure _________
R
Subtask 05-21-40-210-058
R
A. Visual Inspection
R
(1) Do a general visual inspection of the centerline gear well.
EFF : ALL 05-21-40 SROS
Page 609 Oct 01/04
R
5. Close-up ________
R
Subtask 05-21-40-410-058
R
A. Close Access
R R
(1) Close the main landing gear doors 734, 744 (Ref. TASK 32-12-00-410801).
R
(2) Close the ground opening-handle access-doors 149AB, 149CB.
EFF : ALL 05-21-40 SROS
Page 610 Oct 01/04
ZONAL INSPECTION : LOWER DECK AFT CARGO COMPARTMENT - INSPECTION/CHECK ______________________________________________________________________ TASK 05-21-50-200-801 R R
Zonal Inspection of Aft Cargo Compartment (if LD-MCR or LDF and/or DCR and/or ACT(s) installed, as far as visible) 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-151-01 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 ------------------------------------------------------------------------------52-30-00-010-801 52-30-00-410-801
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 05-21-50-010-050 A. Get Access R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at access door 822. (2) Open the aft cargo-compartment door 822 (Ref. TASK 52-30-00-010-801).
EFF : ALL 05-21-50 SROS
Page 601 Jul 01/04
4. Procedure _________ Subtask 05-21-50-210-050 R R
A. Do a general visual inspection of the aft cargo compartment at zones 151 and 152 (as far as you can see if LD-MCR or LDF and/or DCR and/or ACT(s) installed). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring, ducting) are attached correctly. 5. Close-up ________ Subtask 05-21-50-410-050 A. Close Access (1) Close the aft cargo-compartment door 822 (Ref. TASK 52-30-00-410801). Subtask 05-21-50-860-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-50 SROS
Page 602 Jul 01/04
TASK 05-21-50-200-802 Zonal Inspection of Aft Cargo Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-151-02 2. ______________________ Job Set-up Information R
A. Fixtures, Tools, Test and Support Equipment
R R R
------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
R
1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
B. Referenced Information
R R R
------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R R R R R R R R
25-53-00-000-801
R
3. __________ Job Set-up
R
Subtask 05-21-50-010-051-A
R
25-53-00-400-801
Removal of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the AFT Cargo Compartment Installation of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the AFT Cargo Compartment Removal of the Lower-Deck Mobile Crew-Rest (LD-MCR) 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
25-75-41-000-801 52-30-00-010-801 52-30-00-410-801
A. Get Access
R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at access door 822.
R
(2) Open the aft cargo compartment door 822 (Ref. TASK 52-30-00-010-801).
EFF : ALL 05-21-50 SROS
Page 603 Apr 01/04
(3) For aircraft that have the Lower Deck-Mobile Crew Rest: (a) Remove the LD-MCR (Ref. TASK 25-75-41-000-801). (b) Remove the panels that follow (Ref. TASK 25-53-00-000-801). - Ceiling panels 151FC, 151KC, 151PC, 151BY, 151HC. - Partition panels 151BW, 152BW. - Sidewall panels 151TW, 152DW, 152JW, 152AX, 152BX, 151JW. (4) For aircraft without the LD-MCR and without the Lower Deck Lavatories: (a) Remove the panels that follow (Ref. TASK 25-53-00-000-801): - Ceiling panels 151BC, 151FC. - Partition panels 151BW, 152BW. - Sidewall panels 151JW, 151TW, 152DW, 152EW, 152GW, 152JW. (5) For aircraft that have the Lower Deck Lavatories: (a) Remove the panels that follow (Ref. TASK 25-53-00-000-801): - Ceiling panels 151NC, 151EC. - Sidewall panels 151HX, 151LX, 152HX, 152FX, 152LX, 151FX. 4. Procedure _________ Subtask 05-21-50-210-051 R R
A. Do a general visual inspection of the aft cargo compartment. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring, ducting) are attached correctly. 5. Close-up ________ Subtask 05-21-50-410-051-A A. Close Access (1) For aircraft that have the Lower Deck-Mobile Crew Rest: (a) Install the panels that follow (Ref. TASK 25-53-00-400-801). - Ceiling panels 151FC, 151KC, 151PC, 151BY, 151HC. - Partition panels 151BW, 152BW. - Sidewall panels 151TW, 152DW, 152JW, 152AX, 152BX, 151JW.
EFF : ALL 05-21-50 SROS
Page 604 Jul 01/05
(2) For aircraft without the LD-MCR and without the Lower Deck Lavatories: (a) Install the panels that follow (Ref. TASK 25-53-00-400-801): - Ceiling panels 151BC, 151FC. - Partition panels 151BW, 152BW. - Sidewall panels 151JW, 151TW, 152DW, 152EW, 152GW, 152JW. (3) For aircraft that have the Lower Deck Lavatories: (a) Install the panels that follow (Ref. TASK 25-53-00-400-801): - Ceiling panels 151NC, 151EC. - Sidewall panels 151HX, 151LX, 152HX, 152FX, 152LX, 151FX. (4) Close the AFT cargo-compartment door (Ref. TASK 52-30-00-410-801) Subtask 05-21-50-860-052 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-50 R SROS
Page 605 Oct 01/04
TASK 05-21-50-200-803 Zonal Inspection of Aft Cargo Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-151-03 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 ------------------------------------------------------------------------------25-53-00-000-801 25-53-00-400-801 R R
25-75-41-000-801 25-75-41-400-801 28-11-27-000-801 28-11-27-400-801 52-30-00-010-801 52-30-00-410-801
Removal of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the AFT Cargo Compartment Installation of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the AFT Cargo Compartment Removal of the Lower-Deck Mobile Crew-Rest (LD-MCR) Installation of the Lower-Deck Mobile Crew-Rest (LD-MCR) Removal of the Additional Center Tank Installation of the Additional Center Tank 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 05-21-50 SROS
Page 606 Apr 01/04
3. __________ Job Set-up Subtask 05-21-50-010-052 A. Get Access (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at zone 822. (2) Open the aft cargo-compartment door 822 (Ref. TASK 52-30-00-010-801). (3) Remove the ACTs, if installed (Ref. TASK 28-11-27-000-801). R
(4) Remove the LDMCR, if installed (Ref. TASK 25-75-41-000-801).
R R
(5) Remove the sidewall panels and the ceiling panels from FR53.2 to FR66 (Ref. TASK 25-53-00-000-801).
R
(6) Lift the insulation. 4. Procedure _________ Subtask 05-21-50-210-052 A. Do a general visual inspection of the aft cargo compartment. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring, piping) are attached correctly. 5. Close-up ________ Subtask 05-21-50-410-052 A. Close Access
R
(1) Put the insulation back in position.
R R
(2) Install the sidewall panels and the ceiling panels from FR53.2 to FR66 (Ref. TASK 25-53-00-400-801).
R
(3) Install the ACTs, if removed (Ref. TASK 28-11-27-400-801).
R
(4) Install the LDMCR, if removed (Ref. TASK 25-75-41-400-801).
R
(5) Close the aft cargo-compartment door (Ref. TASK 52-30-00-410-801).
EFF : ALL 05-21-50 SROS
Page 607 Jul 01/06
Subtask 05-21-50-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-50 R SROS
Page 608 Apr 01/04
TASK 05-21-50-200-805 Zonal Inspection of Bay Under Aft Cargo Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-153-01 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 ------------------------------------------------------------------------------52-30-00-010-801 52-30-00-410-801
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 Removal of the Floor Panels in the AFT Cargo-Compartment Installation of the Floor Panels in the AFT Cargo-Compartment Fig. 601
53-00-00-000-803 53-00-00-400-803 05-21-50-991-006 3. __________ Job Set-up Subtask 05-21-50-010-054-A A. Get Access
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at zone 822. (2) Open the aft cargo-compartment door 822 (Ref. TASK 52-30-00-010-801). (3) Open the AFT potable-water drain door 154AR. (Ref. Fig. 601/TASK 05-21-50-991-006)
EFF : ALL 05-21-50 R SROS
Page 609 Apr 01/04
R
Aft Fuselage, Lower Deck, Access Panels Zones 152, 154, 164 and 171 Figure 601/TASK 05-21-50-991-006
EFF : ALL 05-21-50 SROS
Page 610 Jan 01/06
(4) Remove the floor panels from FR53.2 to FR66 (Ref. TASK 53-00-00-000803). (5) For aircraft equipped with the Lower Deck Lavatories: (a) Remove the access panels 152AR, 152BR, 152CR, 152DR, 152ER, 152FR, 152GR, 152HR, 152JR, 152KR, 152LR. R
(6) Lift the insulation. 4. Procedure _________ Subtask 05-21-50-210-054 A. Do a general visual inspection of the underfloor bay of the aft cargo compartment. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring, ducting) are attached correctly. 5. Close-up ________ Subtask 05-21-50-410-054-A A. Close Access (1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Put the insulation back in position.
R
(3) Install the floor panels from FR53.2 to FR66 (Ref. TASK 53-00-00-400803).
R
(4) For aircraft equipped with the Lower Deck Lavatories: (a) Close the access panels 152AR, 152BR, 152CR, 152DR, 152ER, 152FR, 152GR, 152HR, 152JR, 152KR, 152LR.
R
(5) Close the AFT potable-water drain door 154AR.
R
(6) Close the AFT cargo-compartment door (Ref. TASK 52-30-00-410-801).
EFF : ALL 05-21-50 SROS
Page 611 Jul 01/06
Subtask 05-21-50-860-053 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-21-50 SROS
Page 612 Jul 01/06
ZONAL INSPECTION : LOWER DECK BULK CARGO COMPARTMENT - INSPECTION/CHECK _______________________________________________________________________ TASK 05-21-60-200-801 R
Zonal Inspection of Bulk Cargo Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-161-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------52-30-00-010-801 52-30-00-410-801
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 05-21-60-010-050 A. Get Access R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at access door 822.
R
(2) Open the aft cargo-compartment door 822 (Ref. TASK 52-30-00-010-801).
EFF : ALL 05-21-60 SROS
Page 601 Jan 01/04
4. Procedure _________ Subtask 05-21-60-210-050 A. Do a general visual inspection of the bulk cargo compartment (zones 161 and 162), (if BCRC or waste chute container installed, as far as you can see). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-21-60-410-050 A. Close Access R R
(1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Close the aft cargo-compartment door 822 (Ref. TASK 52-30-00-410801). Subtask 05-21-60-860-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R
EFF : ALL 05-21-60 SROS
Page 602 Jan 01/06
TASK 05-21-60-200-802 R
Zonal Inspection of Bulk Cargo Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-161-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------25-54-00-000-801 25-54-00-400-801 R R R R
52-30-00-010-801 52-30-00-410-801
Removal of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the BULK Cargo-Compartment Installation of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the BULK Cargo-Compartment 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 05-21-60-010-051 A. Get Access R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at access door 822.
R
(2) Open the aft cargo-compartment door 822 (Ref. TASK 52-30-00-010-801). (3) Remove the ceiling panels: 161AC, 161BC, 161EC. (Ref. TASK 25-54-00000-801)
EFF : ALL 05-21-60 SROS
Page 603 Jan 01/04
(4) Remove the sidewall panels: 161CW, 162LW, 162RW, 162SW, 162TW, 162WW. (Ref. TASK 25-54-00-000-801) 4. Procedure _________ Subtask 05-21-60-210-051
R
A. Do a general visual inspection of the bulk cargo compartment (zones 161 and 162). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-21-60-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the ceiling panels: 161AC, 161BC, 161EC. (Ref. TASK 25-54-00400-801) (3) Install the access panels: 161CW, 162LW, 162RW, 162SW, 162TW, 162WW. (Ref. TASK 25-54-00-400-801) (4) Close the aft cargo-compartment door 822 (Ref. TASK 52-30-00-410801). Subtask 05-21-60-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-21-60 SROS
Page 604 Jan 01/06
TASK 05-21-60-200-803 Zonal Inspection of Bulk Cargo Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-161-03 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 ------------------------------------------------------------------------------25-54-00-000-801 25-54-00-400-801 R R
52-30-00-010-803 52-30-00-410-803
Removal of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the BULK Cargo-Compartment Installation of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the BULK Cargo-Compartment Opening of the BULK Cargo-Compartment Door Closing of the BULK Cargo-Compartment Door
3. __________ Job Set-up Subtask 05-21-60-010-052 A. Get Access R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at access door 823.
R R
(2) Open the BULK cargo-compartment door 823 (Ref. TASK 52-30-00-010803).
R
(3) Remove the sidewall and ceiling panels from FR65 to FR73. (Ref. TASK 25-54-00-000-801)
EFF : ALL 05-21-60 SROS
Page 605 Jul 01/06
4. Procedure _________ Subtask 05-21-60-210-052 A. Do a general visual inspection of the bulk cargo compartment (zones 161). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-21-60-410-052 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the sidewall and ceiling panels from FR65 to FR73. (Ref. TASK 25-54-00-400-801) R R
(3) Close the BULK cargo-compartment door 823 (Ref. TASK 52-30-00-410803). Subtask 05-21-60-860-052 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-21-60 SROS
Page 606 Jul 01/06
TASK 05-21-60-200-804 Zonal Inspection of Bay Under Bulk Cargo Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-163-01 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 ------------------------------------------------------------------------------25-54-00-000-801 25-54-00-400-801 52-30-00-010-801 52-30-00-410-801 05-21-60-991-005
Removal of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the BULK Cargo-Compartment Installation of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the BULK Cargo-Compartment 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 Fig. 601
3. __________ Job Set-up Subtask 05-21-60-010-053 A. Get Access (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the AFT cargo-compartment door. R
(2) Open the AFT cargo-compartment door 822 (Ref. TASK 52-30-00-010-801).
EFF : ALL 05-21-60 SROS
Page 607 Jan 01/06
(3) Open the potable-water service-panel door 164AR. (Ref. Fig. 601/TASK 05-21-60-991-005) R
(4) Remove the floor panels from FR65 to FR73 (Ref. TASK 25-54-00-000801). 4. Procedure _________ Subtask 05-21-60-210-053 A. Do a general visual inspection of the underfloor bay of the bulk cargo compartment (zones 163 and 164). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-21-60-410-053 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the floor panels from FR65 to FR73. (Ref. TASK 25-54-00-400801)
R
(3) Close the potable-water service-panel door 164AR. (4) Close the AFT cargo compartment door. (Ref. TASK 52-30-00-410-801) (5) Remove the access platform(s). Subtask 05-21-60-860-053 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-21-60 SROS
Page 608 Jan 01/06
R
Aft Fuselage, Lower Section, Access Panels Figure 601/TASK 05-21-60-991-005
EFF : ALL 05-21-60 SROS
Page 609 Jan 01/06
ZONAL INSPECTION : AFT CABIN UNDERFLOOR COMPARTMENT - INSPECTION/CHECK ______________________________________________________________________ TASK 05-21-70-200-801 Zonal Inspection of Aft Cabin Underfloor Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-171-01 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 ------------------------------------------------------------------------------25-54-00-000-801 25-54-00-400-801 52-30-00-010-801 52-30-00-410-801 05-21-70-991-003
Removal of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the BULK Cargo-Compartment Installation of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the BULK Cargo-Compartment 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 Fig. 601
3. __________ Job Set-up Subtask 05-21-70-010-050 A. Get Access R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the aft cargo-compartment door.
R
(2) Open the aft cargo-compartment door 822 (Ref. TASK 52-30-00-010-801).
EFF : ALL 05-21-70 SROS
Page 601 Jul 01/04
(3) Open the access door 171AL. (Ref. Fig. 601/TASK 05-21-70-991-003) R
(4) Remove the partition panel 162ZW (Ref. TASK 25-54-00-000-801). 4. Procedure _________ Subtask 05-21-70-210-050 A. Do a general visual inspection of the aft-cabin underfloor compartment (Zones 171 and 172). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (ducting, piping) are attached correctly. 5. Close-up ________ Subtask 05-21-70-410-050 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the partition panel 162ZW. (Ref. TASK 25-54-00-400-801) (3) Close the access door 171AL.
R
(4) Close the aft cargo-compartment door 822 (Ref. TASK 52-30-00-410801). Subtask 05-21-70-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-21-70 SROS
Page 602 Jul 01/04
R
Aft Fuselage, Lower Section, Access Panels Figure 601/TASK 05-21-70-991-003
EFF : ALL 05-21-70 SROS
Page 603 Jan 01/06
TASK 05-21-70-200-802 Zonal Inspection of Aft Cabin Underfloor Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-171-02 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 ------------------------------------------------------------------------------25-54-00-000-801 25-54-00-400-801 52-30-00-010-801 52-30-00-410-801 R R R
53-42-17-000-801 53-42-17-400-801 05-21-70-991-003
Removal of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the BULK Cargo-Compartment Installation of the Ceiling Panels, the Partition Panels and the Sidewall Panels in the BULK Cargo-Compartment 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 Removal of the Floor Panels Between FR73 and FR79 Installation of the Floor Panels Between FR73 and FR79 Fig. 601
EFF : ALL 05-21-70 SROS
Page 604 Jul 01/05
3. __________ Job Set-up Subtask 05-21-70-010-051 A. Get Access (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the aft cargo-compartment door. (2) Open the aft cargo-compartment door 822 (Ref. TASK 52-30-00-010-801). (3) Open the access door 171AL. (Ref. Fig. 601/TASK 05-21-70-991-003) (4) Remove the partition panel 162ZW (Ref. TASK 25-54-00-000-801). R R
(5) Remove the floor panels from FR73 to FR80 (Ref. TASK 53-42-17-000801). (6) Lift the insulation. 4. Procedure _________ Subtask 05-21-70-210-051 A. Do a general visual inspection of the aft-cabin underfloor compartment (zones 171 and 172). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-21-70-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Put the insulation back in position.
R R
(3) Install the floor panels from FR73 to FR80 (Ref. TASK 53-42-17-400801). (4) Install the partition panel 162ZW (Ref. TASK 25-54-00-400-801).
EFF : ALL 05-21-70 SROS
Page 605 Jul 01/05
R
(5) Close the access door 171AL.
R R
(6) Close the aft cargo-compartment door 822 (Ref. TASK 52-30-00-410801). Subtask 05-21-70-860-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-21-70 SROS
Page 606 Jul 01/04
________________________________________________________________________ ZONAL INSPECTION: AIR CONDITIONING, HYDRAULICS COMPARTMENTS AND FAIRINGS ________________ INSPECTION/CHECK TASK 05-21-90-200-801 R R
Zonal Inspection of Air Conditioning Compt and Fairing 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-191-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------53-35-13-000-802 53-35-13-400-802
Removal of the Belly Fairing Access Panels Installation of the Belly Fairing Access Panels
3. __________ Job Set-up Subtask 05-21-90-010-050 A. Get Access R R
(1) Put an ACCESS PLATFORM 2M (6 FT) in position at the air conditioning compartment and fairings. (2) For the right side, zone 192: (a) Remove the access panels 192JB, 192PB (Ref. TASK 53-35-13-000802).
EFF : ALL 05-21-90 SROS
Page 601 Jan 01/04
(3) For left side, zone 191: (a) Remove the access panels 191FB, 191KB (Ref. TASK 53-35-13-000802). 4. Procedure _________ Subtask 05-21-90-210-050
R
A. Do a general visual inspection of the air conditioning compartment and fairings. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring, piping) are attached correctly. 5. Close-up ________ Subtask 05-21-90-410-050 A. Close Access
R R
(1) Make sure that the work area is clean and clear of tools and other items.
R
(2) For the right side zone 192: (a) Install the access panel 192JB, 192PB (Ref. TASK 53-35-13-400802).
R
(3) For the left side zone 191: (a) Install the access panels 191FB, 191KB (Ref. TASK 53-35-13-400802).
R R R
(4) Remove the access platform(s). Subtask 05-21-90-860-051 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-21-90 SROS
Page 602 Jan 01/04
TASK 05-21-90-200-802 R R
Zonal Inspection of Air Conditioning Compt and Fairing 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-191-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------53-35-11-000-801 53-35-11-400-801 53-35-13-000-801 53-35-13-000-802 53-35-13-400-801 53-35-13-400-802
Removal of the Wing-to-Fuselage Fairings Installation of the Wing-to-Fuselage Fairings Removal of the Access Panels 191AB, 191BB, 192BB, 191DB, 197AB, 197AT, 198AT, 197BB, 198BB, 197EB, 198EB, 197FB, 197GB, 198GB, 198HB and 197HB. Removal of the Belly Fairing Access Panels Installation of the Access Panels 191AB, 191BB, 192BB, 191DB, 197AB, 197AT, 198AT, 197BB, 198BB, 197EB, 198EB, 197FB, 197GB, 198GB, 198HB and 197HB. Installation of the Belly Fairing Access Panels
EFF : ALL 05-21-90 SROS
Page 603 Jan 01/04
3. __________ Job Set-up Subtask 05-21-90-010-051 A. Get Access R R
(1) Put an ACCESS PLATFORM 2M (6 FT)in position at the air conditioning compartment and fairings. (2) For the left side zone 191:
R R R R
(a) Remove the access panels 191AB, 191BB, 191CB, 191DB, 191FB, 191HB, 191KB, 191QB, 191AT, 191BT, 191CT 191EB (Ref. TASK 53-3511-000-801) (Ref. TASK 53-35-13-000-802) (Ref. TASK 53-35-13-000801). (3) For the right side zone 192:
R R R
(a) Remove the access panels: 192BB, 192CB, 192GB, 192HB, 192JB, 192MB, 192NB, 192PB, 192QB, 192AT, 192BT, 192CT (Ref. TASK 53-3513-000-801). (Ref. TASK 53-35-13-000-802) 4. Procedure _________ Subtask 05-21-90-210-051
R
A. Do a general visual inspection of the air conditioning compartment and fairings. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring, piping) are attached correctly.
EFF : ALL 05-21-90 SROS
Page 604 Jan 01/04
5. Close-up ________ Subtask 05-21-90-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) For the left side zone 191: (a) Install the access panels 191AB, 191BB, 191CB, 191DB, 191FB, 191HB, 191KB, 191QB, 191AT, 191BT, 191CT 191EB (Ref. TASK 53-3511-400-801) (Ref. TASK 53-35-13-400-801) (Ref. TASK 53-35-13-400802) (3) For the right side zone 192: (a) Install the access panels 192BB, 192CB, 192GB, 192HB, 192JB, 192MB, 192NB, 192PB, 192QB, 192AT, 192BT, 192CT, (Ref. TASK 5335-13-400-801), (Ref. TASK 53-35-13-400-802). (Ref. TASK 53-3511-400-801) Subtask 05-21-90-860-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-21-90 R SROS
Page 605 Jan 01/06
TASK 05-21-90-200-805 Zonal Inspection of Hydraulic Compartment and Fairings 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 Refer to the MPD TASK: ZL-195-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-12-00-010-801 32-12-00-410-801
Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-21-90-010-054 A. Get Access R R
(1) For the left side zone 147:
R
(a) Open the main landing-gear access door 734 (Ref. TASK 32-12-00010-801).
R
(2) For the right side zone 148:
R
(a) Open the main landing-gear access door 744 (Ref. TASK 32-12-00010-801).
EFF : ALL 05-21-90 SROS
Page 606 Jan 01/06
R R
(3) Put an ACCESS PLATFORM 2M (6 FT) in position at the hydraulic compartment and fairings. 4. Procedure _________ Subtask 05-21-90-210-054 A. Do a general visual inspection of the hydraulics compartment and fairings. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-21-90-410-054 A. Close Access
R
(1) For the left side zone 147:
R
(a) Close the access door 734 (Ref. TASK 32-12-00-410-801).
R
(2) For the right side zone 148:
R
(a) Close the access door 744 (Ref. TASK 32-12-00-410-801). Subtask 05-21-90-860-054 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-90 SROS
Page 607 Jan 01/06
TASK 05-21-90-200-806 R
Zonal Inspection of Hydraulics Compartment and Fairings 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-195-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------53-35-13-000-802 53-35-13-400-802
Removal of the Belly Fairing Access Panels Installation of the Belly Fairing Access Panels
3. __________ Job Set-up Subtask 05-21-90-010-055-A A. Get Access (1) Put an ACCESS PLATFORM 2M (6 FT) in position at the hydraulics compartment and fairings. (2) For the left side zone 195: (a) Open the blue ground service panel: 195BB. (b) Remove the access panels: 195CB, 195DB (Ref. TASK 53-35-13-000802).
EFF : ALL 05-21-90 SROS
Page 608 Jan 01/06
(3) For the right side zone 196: (a) Open the yellow ground service panel: 196BB. 4. Procedure _________ Subtask 05-21-90-210-055 A. Do a general visual inspection of the hydraulics compartment and fairings. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-21-90-410-055-A A. Close Access (1) For the left side zone 195: (a) Install the access panels: 195CB, 195DB (Ref. TASK 53-35-13-400802). (b) Close the blue ground service panel: 195BB. (2) For the right side zone 196: (a) Close the yellow ground service panel: 196BB. Subtask 05-21-90-860-055 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-90 R SROS
Page 609 Jan 01/07
TASK 05-21-90-200-807 Zonal Inspection of Rear Fairings 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-197-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-12-00-010-801 32-12-00-410-801
Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-21-90-010-056 A. Get Access R
(1) Put an ACCESS PLATFORM 2M (6 FT) in position at the rear fairing. (2) For the left side zone 197: (a) Open the access door 734. (Ref. TASK 32-12-00-010-801) (3) For the right side zone 198: (a) Open the access door 744. (Ref. TASK 32-12-00-010-801)
EFF : ALL 05-21-90 SROS
Page 610 Jan 01/07
4. Procedure _________ Subtask 05-21-90-210-056 A. Do a general visual inspection of the rear fairing. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-21-90-410-056 A. Close Access (1) For the left side zone 197: (a) Close the access door 734. (Ref. TASK 32-12-00-410-801) (2) For the right side zone 198: (a) Close the access door 744. (Ref. TASK 32-12-00-410-801) Subtask 05-21-90-860-056 B. Put the Aircraft back to its Initial Configuration R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-21-90 SROS
Page 611 Jan 01/06
TASK 05-21-90-200-808 Zonal Inspection of Rear Fairings 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-197-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------53-35-13-000-801 53-35-13-400-801
Removal of the Access Panels 191AB, 191BB, 192BB, 191DB, 197AB, 197AT, 198AT, 197BB, 198BB, 197EB, 198EB, 197FB, 197GB, 198GB, 198HB and 197HB. Installation of the Access Panels 191AB, 191BB, 192BB, 191DB, 197AB, 197AT, 198AT, 197BB, 198BB, 197EB, 198EB, 197FB, 197GB, 198GB, 198HB and 197HB.
3. __________ Job Set-up Subtask 05-21-90-010-057 A. Get Access (1) Put an ACCESS PLATFORM 2M (6 FT) in position at the rear fairing. (2) For the left side zone 197: (a) Remove the access panel 197EB. (Ref. TASK 53-35-13-000-801) (3) For the right side zone 198: (a) Remove the access panel 198EB. (Ref. TASK 53-35-13-000-801)
EFF : ALL 05-21-90 R SROS
Page 612 Jan 01/06
4. Procedure _________ Subtask 05-21-90-210-057 A. Do a general visual inspection of the rear fairing. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-21-90-410-057 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) For the left side zone 197: (a) Install the access panel 197EB. (Ref. TASK 53-35-13-400-801) (3) For the right side zone 198: (a) Install the access panel 198EB. (Ref. TASK 53-35-13-400-801) Subtask 05-21-90-860-057 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-21-90 R SROS
Page 613 Jan 01/06
TASK 05-21-90-200-810 Zonal Inspection of Air Conditioning Compartment and Fairing 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-193-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R
52-42-29-000-801 52-42-29-400-801 53-35-13-000-802 53-35-13-400-802
Removal of the Overpressure Door of the Panel 193DB Installation of the Overpressure Door of the Panel 193DB Removal of the Belly Fairing Access Panels Installation of the Belly Fairing Access Panels
3. __________ Job Set-up Subtask 05-21-90-010-059 A. Get Access (1) Put an ACCESS PLATFORM 2M (6 FT) in position at the air conditioning compartment and fairings. (a) Open the access panels 193BB, 193DB (Ref. TASK 53-35-13-000-802) (Ref. TASK 52-42-29-000-801).
EFF : ALL 05-21-90 SROS
Page 614 Jan 01/06
4. Procedure _________ Subtask 05-21-90-210-059 A. Do a general visual inspection of the air conditioning compartment and fairings. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring, piping) are attached correctly. 5. Close-up ________ Subtask 05-21-90-410-059 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels 193BB, 193DB (Ref. TASK 53-35-13-400-802) (Ref. TASK 52-42-29-400-801). Subtask 05-21-90-860-052 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-21-90 R SROS
Page 615 Jan 01/06
TASK 05-21-90-200-811 Zonal Inspection of Air Conditioning Compartment and Fairing 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-193-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R
52-42-29-000-801 52-42-29-400-801 53-35-13-000-802 53-35-13-400-802
Removal of the Overpressure Door of the Panel 193DB Installation of the Overpressure Door of the Panel 193DB Removal of the Belly Fairing Access Panels Installation of the Belly Fairing Access Panels
3. __________ Job Set-up Subtask 05-21-90-010-060 A. Get Access (1) Put an ACCESS PLATFORM 2M (6 FT) in position at the air conditioning compartment and fairings. (a) Remove the access panels 193AB, 193BB, 193DB (Ref. TASK 53-35-13000-802) (Ref. TASK 52-42-29-000-801). (b) Open the access door 193CB.
EFF : ALL 05-21-90 SROS
Page 616 Jan 01/06
4. Procedure _________ Subtask 05-21-90-210-060
R
A. Do a general visual inspection of the air conditioning compartment and fairings. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring, piping) are attached correctly. 5. Close-up ________ Subtask 05-21-90-410-060 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items.
R R
(2) Install the access panels 193AB, 193BB, 193DB (Ref. TASK 53-35-13400-802) (Ref. TASK 52-42-29-400-801). (3) Close the access door 193CB.
R R R
Subtask 05-21-90-860-053 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-21-90 SROS
Page 617 Jan 01/04
ZONAL INSPECTION : UPPER HALF OF FUSELAGE - INSPECTION/CHECK ____________________________________________________________ TASK 05-22-00-200-801 Zonal Inspection of the Upper Half of the fuselage (Zone 200). 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information Not Applicable 3. __________ Job Set-up Subtask 05-22-00-869-050 A. Not applicable. 4. Procedure _________ Subtask 05-22-00-210-050 A. Visual inspection. (1) Do a general visual inspection of the upper half of the fuselage from the ground.
EFF : ALL 05-22-00 R SROS
Page 601 Jan 01/04
TASK 05-22-00-200-802 R
Zonal Inspection of Upper Half of Fuselage 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-200-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R
No specific
1 ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE
3. __________ Job Set-up Subtask 05-22-00-010-051 A. Get Access R
(1) Put an ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE in position in the upper half of the fuselage. 4. Procedure _________ Subtask 05-22-00-210-051 A. Inspection (1) Do a general visual inspection of the upper half of the fuselage up to the stringer 26LH and RH (zone 200) and around the doors. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see.
R
R
EFF : ALL 05-22-00 SROS
Page 602 Jan 01/04
R
5. Close-up ________
R
Subtask 05-22-00-860-050
R
A. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-22-00 SROS
Page 603 Jan 01/04
ZONAL INSPECTION : COCKPIT - INSPECTION/CHECK _____________________________________________ TASK 05-22-10-200-801 Zonal Inspection of Cockpit 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-211-01 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
25-13-44-000-802 25-13-44-400-802 52-10-00-010-801 52-10-00-410-801 05-22-10-991-001
Removal of the Sidewall Panels Installation of the Sidewall Panels Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door Fig. 601
3. __________ Job Set-up Subtask 05-22-10-010-050 A. Get Access (Ref. Fig. 601/TASK 05-22-10-991-001) (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the access door 831 or 841. (2) Open the passenger/crew door (Ref. TASK 52-10-00-010-801). R
(3) Remove the sidewall panels (Ref. TASK 25-13-44-000-802): For the left side: 211JW, 211KW. For the right side: 212JW, 212KW.
EFF : ALL 05-22-10 SROS
Page 601 Jan 01/06
Ceiling and Sidewall Panels of the Cockpit Figure 601/TASK 05-22-10-991-001 EFF : ALL 05-22-10 SROS
Page 602 Apr 01/98
4. Procedure _________ Subtask 05-22-10-210-050 A. Do a general visual inspection of the cockpit. Make sure that: - there is no damage, corrosion, leaks or cracks on all the parts of the components and the structure you can see. - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-22-10-410-050 A. Close Access R R
(1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Install the sidewall panels (Ref. TASK 25-13-44-400-802): For the left side: 211JW, 211KW. For the right side: 212JW, 212KW.
R
(3) Close the passenger/crew door (Ref. TASK 52-10-00-410-801). Subtask 05-22-10-860-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R
EFF : ALL 05-22-10 SROS
Page 603 Jan 01/06
TASK 05-22-10-200-802 Zonal Inspection of Cockpit 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-211-02 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 ------------------------------------------------------------------------------25-13-44-000-801 25-13-44-000-802 25-13-44-400-801 25-13-44-400-802 52-10-00-010-801 52-10-00-410-801 53-12-11-000-801 53-12-11-400-801 05-22-10-991-001
Removal of the Ceiling Panels Removal of the Sidewall Panels Installation of the Ceiling Panels Installation of the Sidewall Panels Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door Removal of the Cockpit Floor Panels from FR1 thru FR11 Installation of the Cockpit Floor Panels from FR1 thru FR11 Fig. 601
3. __________ Job Set-up Subtask 05-22-10-010-051 A. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the access door 831 or 841. R
(2) Open the passenger/crew door 831 or 841 (Ref. TASK 52-10-00-010-801).
EFF : ALL 05-22-10 SROS
Page 604 Jul 01/06
(3) Remove the sidewall panels (Ref. TASK 25-13-44-000-802): (Ref. Fig. 601/TASK 05-22-10-991-001) For the left side: 211AW, 211BW, 211CW, 211DW, 211EW, 211FW, 211GW, 211HW, 211JW, 211KW, 211LW, 211MW, 211PW. For the right side: 212CW, 212DW, 212EW, 212FW, 212GW, 212HW, 212JW, 212KW, 212LW, 212MW, 212NW, 212QW.
R R
(4) Remove the ceiling panels (Ref. TASK 25-13-44-000-801): For the left side: 211AC, 211BC, 211CC, 211DC, 211EC, 211GC, 211HC, 211JC, 211KC, 211LC, 211MC. For the right side: 212BC, 212CC, 212DC, 212FC, 212GC, 212HC, 212JC, 212NC. (5) Remove the floor panels from FR1 to FR11 (Ref. TASK 53-12-11-000801). 4. Procedure _________ Subtask 05-22-10-210-051 A. Do a general visual inspection of the cockpit. Make sure that: - there is no damage, corrosion, leaks or cracks on all the parts of the components and the structure you can see. - all the installations (wiring, ducting) are attached correctly. NOTE : Lift the insulation sufficiently to make sure that there is no ____ corrosion or signs of leaks. 5. Close-up ________ Subtask 05-22-10-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the floor panels from FR1 to FR11 (Ref. TASK 53-12-11-400801).
EFF : ALL 05-22-10 SROS
Page 605 Jul 01/06
(3) Install the ceiling panels (Ref. TASK 25-13-44-400-801): For the left side: 211AC, 211BC, 211CC, 211DC, 211EC, 211GC, 211HC, 211JC, 211KC, 211LC, 211MC. For the right side: 212BC, 212CC, 212DC, 212FC, 212GC, 212HC, 212JC, 212NC. (4) Install the sidewall panels (Ref. TASK 25-13-44-400-802): For the left side: 211AW, 211BW, 211CW, 211DW, 211EW, 211FW, 211GW, 211HW, 211JW, 211KW, 211LW, 211MW, 211PW. For the right side: 212CW, 212DW, 212EW, 212FW, 212GW, 212HW, 212JW, 212KW, 212LW, 212MW, 212NW, 212QW. R
(5) Close the passenger/crew door 831 or 841 (Ref. TASK 52-10-00-410801). Subtask 05-22-10-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-22-10 SROS
Page 606 Jul 01/06
ZONAL INSPECTION : FORWARD CABIN UTILITY AREAS - INSPECTION/CHECK _________________________________________________________________ TASK 05-22-20-200-802 Zonal Inspection of FWD Cabin Utility Area 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-221-02 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 ------------------------------------------------------------------------------25-22-41-000-801 25-22-41-400-801 25-22-44-000-801 25-22-44-400-801 R
25-23-45-000-801
R
25-23-45-400-801 25-26-41-000-801 25-26-41-400-801 25-26-42-000-801 25-26-42-400-801 25-27-15-000-801 25-27-15-400-801 25-27-41-000-801 25-27-41-400-801 25-31-41-000-801 25-31-41-400-801 25-31-43-000-801
Removal of the Wall-Mounted Cabin-Attendant Seat Installation of the Wall-Mounted Cabin-Attendant Seat Removal of the Free-Standing Cabin-Attendant Seat, Seat Rail Mounted Installation of the Free-Standing Cabin-Attendant Seat, Seat Rail Mounted Removal of the Door Frame Linings of the Forward Passenger/Crew Door Installation of the Door Frame Linings of the Forward Passenger/Crew Door Removal of the Curtains and the Curtain Rails Installation of the Curtains and the Curtain Rails Removal of the Partitions Installation of the Partitions Removal of the Emergency Equipment Stowage Installation of the Emergency Equipment Stowage Removal of the Stowages Installation of the Stowages Removal of the FWD RH Galley Unit (6479ML) Installation of the FWD RH Galley Unit (6479ML) Removal of the FWD Center-Galley Unit 6477ML
EFF : ALL 05-22-20 SROS
Page 601 Jan 01/06
------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R
25-31-43-000-802 25-31-43-400-801 25-31-43-400-802 25-31-51-000-801 25-31-51-400-801 25-31-52-000-801 25-31-52-400-801 25-31-59-000-801 25-31-59-400-801 25-41-41-000-801 25-41-41-400-801 25-41-44-000-801 25-41-44-400-801 25-41-45-000-801 25-41-45-400-801 25-74-41-000-801 25-74-41-400-801
Removal of the FWD Center-Galley Unit 6477ML01 Installation of the FWD Center-Galley Unit 6477ML Installation of the FWD Center-Galley Unit 6477ML01 Removal of the FWD Galley Unit (6491ML) Installation of the FWD Galley Unit (6491ML) Removal of the FWD Galley Unit (6492ML) Installation of the FWD Galley Unit (6492ML) Removal of the Galley Unit (6489ML) Installation of the Galley Unit (6489ML) Removal of Lavatory A Installation of Lavatory A Removal of the Lavatory J Installation of the Lavatory J Removal of the Lavatory N Installation of the Lavatory N Removal of the Flight Crew Rest Compartment (FCRC) Installation of the Flight Crew Rest Compartment (FCRC) Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door Removal of the Cabin Floor Panels from FR11 thru FR17. Installation of the Cabin Floor Panels from FR11 thru FR17.
52-10-00-010-801 52-10-00-410-801 53-12-12-000-801 53-12-12-400-801 3. __________ Job Set-up Subtask 05-22-20-010-051 A. Get Access
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the FWD passenger/crew door. (2) Open the FWD passenger/crew door 831, 841 (Ref. TASK 52-10-00-010801). (3) Remove the (Ref. TASK (Ref. TASK (Ref. TASK (Ref. TASK
galleys, if installed 25-31-41-000-801), 25-31-43-000-801) or (Ref. TASK 25-31-43-000-802), 25-31-51-000-801), (Ref. TASK 25-31-52-000-801), 25-31-59-000-801).
EFF : ALL 05-22-20 SROS
Page 602 Jul 01/06
(4) Remove the (Ref. TASK (Ref. TASK (Ref. TASK
lavatories, if installed 25-41-41-000-801), 25-41-44-000-801), 25-41-45-000-801).
(5) Remove the (Ref. TASK (Ref. TASK (Ref. TASK
seats and the furnishings, if installed 25-22-41-000-801), (Ref. TASK 25-22-44-000-801), 25-26-41-000-801), (Ref. TASK 25-26-42-000-801), 25-27-15-000-801) or (Ref. TASK 25-27-41-000-801).
R R
(6) Remove the flight crew rest compartment, if installed (Ref. TASK 2574-41-000-801).
R
(7) Remove the floor panels around and below the galleys and the toilets (Ref. TASK 53-12-12-000-801).
R
(8) Remove the door frame linings (Ref. TASK 25-23-45-000-801).
R
(9) Lift the insulation sufficiently to do the inspection. 4. Procedure _________ Subtask 05-22-20-210-051 A. Do a general visual inspection of the forward cabin utility-area (zones 221 and 222). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, wiring) are attached correctly. 5. Close-up ________ Subtask 05-22-20-410-051 A. Close Access (1) Put the insulation back in position. (2) Install the door frame linings (Ref. TASK 25-23-45-400-801). (3) Install the floor panels (Ref. TASK 53-12-12-400-801).
R R
(4) Install the flight crew rest compartment, if removed (Ref. TASK 2574-41-400-801).
EFF : ALL 05-22-20 SROS
Page 603 Jul 01/06
R
(5) Install the seats and the furnishings, if removed (Ref. TASK 25-22-41-400-801), (Ref. TASK 25-22-44-400-801), (Ref. TASK 25-26-41-400-801), (Ref. TASK 25-26-42-400-801), (Ref. TASK 25-27-15-400-801) or (Ref. TASK 25-27-41-400-801).
R
(6) Install the galleys, if removed (Ref. TASK 25-31-41-400-801), (Ref. TASK 25-31-43-400-801) or (Ref. TASK 25-31-43-400-802), (Ref. TASK 25-31-51-400-801), (Ref. TASK 25-31-52-400-801), (Ref. TASK 25-31-59-400-801).
R
(7) Install the lavatories, if removed (Ref. TASK 25-41-41-400-801), (Ref. TASK 25-41-44-400-801), (Ref. TASK 25-41-45-400-801).
R
(8) Close the FWD passenger/crew door 831, 841 (Ref. TASK 52-10-00-410801). Subtask 05-22-20-860-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-22-20 SROS
Page 604 Jul 01/06
TASK 05-22-20-200-804 R
Zonal Inspection of FWD Cabin Utility-Area Overhead-Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-223-01 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
25-23-42-000-801 25-23-42-400-801 25-31-41-000-801 25-31-41-400-801 25-31-43-000-801 25-31-43-000-802 25-31-43-400-801 25-31-51-000-801 25-31-51-400-801 25-31-52-000-801 25-31-52-400-801 25-41-41-000-801 25-41-41-400-801 25-41-44-000-801 25-41-44-400-801 25-41-44-400-802 25-41-45-000-801 25-41-45-400-801 25-41-45-400-802 25-74-41-000-801 25-74-41-400-801 52-10-00-010-801
Removal of the FWD and AFT Exit Ceiling-Panels Installation of the FWD and AFT Exit Ceiling-Panels Removal of the FWD RH Galley Unit (6479ML) Installation of the FWD RH Galley Unit (6479ML) Removal of the FWD Center-Galley Unit 6477ML Removal of the FWD Center-Galley Unit 6477ML01 Installation of the FWD Center-Galley Unit 6477ML Removal of the FWD Galley Unit (6491ML) Installation of the FWD Galley Unit (6491ML) Removal of the FWD Galley Unit (6492ML) Installation of the FWD Galley Unit (6492ML) Removal of Lavatory A Installation of Lavatory A Removal of the Lavatory J Installation of the Lavatory J SPARE TASK FOR LATER USE Removal of the Lavatory N Installation of the Lavatory N SPARE TASK FOR LATER USE Removal of the Flight Crew Rest Compartment (FCRC) Installation of the Flight Crew Rest Compartment (FCRC) Opening of the Passenger/Crew Door
EFF : ALL 05-22-20 SROS
Page 605 Jan 01/06
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------52-10-00-410-801
Closing of the Passenger/Crew Door
3. __________ Job Set-up Subtask 05-22-20-010-053 A. Get Access R R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the FWD passenger/crew door. (2) Open the FWD passenger/crew door 831, 841 (Ref. TASK 52-10-00-010801). (3) Remove the (Ref. TASK (Ref. TASK (Ref. TASK
galleys, if installed 25-31-41-000-801), 25-31-43-000-801) or (Ref. TASK 25-31-43-000-802), 25-31-51-000-801), (Ref. TASK 25-31-52-000-801).
(4) Remove the (Ref. TASK (Ref. TASK (Ref. TASK
lavatories, if installed 25-41-41-000-801), 25-41-44-000-801), 25-41-45-000-801).
(5) Remove the rest room container, if installed (Ref. TASK 25-74-41-000-801). (6) Remove the ceiling panels 221AZ, 221BZ, 222AZ, 222BZ (Ref. TASK 25-23-42-000-801). R
(7) Lift the insulation sufficiently to do the inspection. 4. Procedure _________ Subtask 05-22-20-210-053 A. Do a general visual inspection of the forward cabin overhead-compartment (zones 223 and 224). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping, wiring) are attached correctly.
EFF : ALL 05-22-20 SROS
Page 606 Jul 01/06
5. Close-up ________ Subtask 05-22-20-410-053 A. Close Access (1) Put the insulation back in position. (2) Install the ceiling panels 221AZ, 221BZ, 222AZ, 222BZ (Ref. TASK 25-23-42-400-801). (3) Install the rest room container, if removed (Ref. TASK 25-74-41-400-801). (4) Install the lavatories, if removed (Ref. TASK 25-41-41-400-801), (Ref. TASK 25-41-44-400-801) or (Ref. TASK 25-41-44-400-802), (Ref. TASK 25-41-45-400-801) or (Ref. TASK 25-41-45-400-802). (5) Install the galleys, if removed (Ref. TASK 25-31-41-400-801), (Ref. TASK 25-31-43-400-801) or (Ref. TASK 25-31-43-000-802), (Ref. TASK 25-31-51-400-801) or (Ref. TASK 25-31-52-400-801).
R
(6) Close the FWD passenger/crew door 831, 841 (Ref. TASK 52-10-00-410801). Subtask 05-22-20-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-22-20 SROS
Page 607 Jul 01/06
ZONAL INSPECTION: FORWARD CABIN AFT - INSPECTION/CHECK ______________________________________________________ TASK 05-22-30-200-803 R
Zonal Inspection of FWD Cabin 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-231-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R R
25-21-41-000-801 25-21-41-400-801 25-23-43-000-802 25-23-43-400-802 25-32-41-000-801 25-32-41-400-801 25-32-42-000-801 25-32-42-000-802 25-32-42-400-801 25-32-42-400-802 25-32-43-000-801 25-32-43-000-802 25-32-43-400-801 25-32-43-400-802 25-32-44-000-801 25-32-44-400-801 25-32-46-000-801 25-32-46-400-801 25-32-47-000-801 25-32-47-400-801 25-32-48-000-801
Removal of the Passenger Seats Installation of the Passenger Seats Removal of the Sidewall Panel(s) Installation of the Sidewall Panel(s) Removal of the MID Galley Unit (7000ML) Installation of the MID Galley Unit (7000ML) Removal of the MID Galley Unit (7001ML) Removal of the MID Galley Unit (7001ML-01) Installation of the MID Galley Unit (7001ML) Installation of the MID Galley Unit (7001ML-01) Removal of the MID Galley Unit (7002ML) Removal of the MID Galley Unit (7002ML-01) Installation of the MID Galley Unit (7002ML) Installation of the MID Galley Unit (7002ML-01) Removal of the MID Galley Unit 7003ML Installation of the MID Galley Unit 7003ML Removal of the MID Galley Unit 7006ML Installation of the MID Galley Unit 7006ML Removal of the MID Galley Unit (7009ML) Installation of the MID Galley Unit (7009ML) Removal of the MID Galley Unit (7011ML)
EFF : ALL 05-22-30 SROS
Page 601 Jan 01/04
------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R R
25-32-48-400-801 25-32-52-000-801 25-32-52-400-801 25-32-61-000-801 25-32-61-400-801 25-32-62-000-801 25-32-62-400-801 25-32-69-000-801 25-32-69-400-801 25-32-73-000-801 25-32-73-400-801 25-42-41-000-801 25-42-41-000-802 25-42-41-400-801 25-42-41-400-802 25-42-42-000-801 25-42-42-400-801 25-46-41-000-801 25-46-41-400-801 25-46-42-000-801 25-46-42-400-801 52-10-00-010-801 52-10-00-410-801 53-00-00-000-801 53-00-00-400-801
Installation of the MID Galley Unit (7011ML) Removal of the MID Galley Unit (7010ML) Installation of the MID Galley Unit (7010ML) Removal of the MID Galley (6505ML) Installation of the MID Galley (6505ML) Removal of the MID Galley Unit (6506ML) Installation of the MID Galley Unit (6506ML) Removal of the MID Galley Unit (6507ML) Installation of the MID Galley Unit (6507ML) Removal of the MID Galley Unit (6511ML) Installation of the MID Galley Unit (6511ML) Removal of the Lavatory H SPARE TASK FOR LATER USE Installation of the Lavatory H SPARE TASK FOR LATER USE Removal of the Lavatory K Installation of the Lavatory K Removal of the Lavatory Block O/P Installation of the Lavatory Block O/P Removal of the Lavatory Block U/V Installation of the Lavatory Block U/V Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door Removal of the Floor Panels in the Cabin from FR17 to FR80 Installation of the Floor Panels in the Cabin from FR17 to FR80
3. __________ Job Set-up Subtask 05-22-30-010-052 A. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the FWD passenger/crew door. (2) Open the FWD passenger/crew door 831, 841 (Ref. TASK 52-10-00-010801). (3) Remove the seats and the furnishings (Ref. TASK 25-21-41-000-801).
EFF : ALL 05-22-30 SROS
Page 602 Jul 01/06
R
(4) Remove the (Ref. TASK (Ref. TASK (Ref. TASK (Ref. TASK (Ref. TASK (Ref. TASK (Ref. TASK (Ref. TASK
galleys, if installed 25-32-41-000-801), 25-32-42-000-801), (Ref. 25-32-43-000-801), (Ref. 25-32-44-000-801), (Ref. 25-32-47-000-801), (Ref. 25-32-52-000-801), (Ref. 25-32-62-000-801), (Ref. 25-32-73-000-801).
R
(5) Remove the (Ref. TASK (Ref. TASK (Ref. TASK
lavatories, if installed 25-42-41-000-801), (Ref. TASK 25-42-41-000-802), 25-42-42-000-801), (Ref. TASK 25-46-41-000-801), 25-46-42-000-801).
R R R
(6) Remove the sidewall panels and the floor panels from FR17 to FR31 (Ref. TASK 25-23-43-000-802) (Ref. TASK 53-00-00-000-801).
R R
TASK TASK TASK TASK TASK TASK
25-32-42-000-802), 25-32-43-000-802), 25-32-46-000-801), 25-32-48-000-801), 25-32-61-000-801), 25-32-69-000-801),
(7) Lift the insulation sufficiently to do the inspection. 4. Procedure _________ Subtask 05-22-30-210-052 A. Do a general visual inspection of the forward cabin (zones 231 and 232). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-22-30-410-052 A. Close Access (1) Put the insulation back in position. (2) Install all the floor panels and the sidewall panels from FR17 to FR31 (Ref. TASK 53-00-00-400-801) (Ref. TASK 25-23-43-400-802).
R R
(3) Install the lavatories, if removed (Ref. TASK 25-42-41-400-801), (Ref. TASK 25-42-41-400-802), (Ref. TASK 25-42-42-400-801), (Ref. TASK 25-46-41-400-801), (Ref. TASK 25-46-42-400-801).
EFF : ALL 05-22-30 SROS
Page 603 Jul 01/06
R
(4) Install the galleys, if removed (Ref. TASK 25-32-41-400-801), (Ref. TASK 25-32-42-400-801), (Ref. (Ref. TASK 25-32-43-400-801), (Ref. (Ref. TASK 25-32-44-400-801), (Ref. (Ref. TASK 25-32-47-400-801), (Ref. (Ref. TASK 25-32-52-400-801), (Ref. (Ref. TASK 25-32-62-400-801), (Ref. (Ref. TASK 25-32-73-400-801).
R R
TASK TASK TASK TASK TASK TASK
25-32-42-400-802), 25-32-43-400-802), 25-32-46-400-801), 25-32-48-400-801), 25-32-61-400-801), 25-32-69-400-801),
(5) Install the seats and furnishings (Ref. TASK 25-21-41-400-801). (6) Close the FWD passenger/crew door 831, 841 (Ref. TASK 52-10-00-410801). Subtask 05-22-30-860-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-22-30 SROS
Page 604 Jul 01/06
TASK 05-22-30-200-805 Zonal Inspection of FWD Cabin Overhead Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-233-01 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 ------------------------------------------------------------------------------25-23-41-000-801 25-23-41-400-801 25-24-51-000-801 25-24-51-400-801 25-24-61-000-801 25-24-61-400-801 52-10-00-010-801 52-10-00-410-801
Removal of the Ceiling Panels Installation of the Ceiling Panels Removal of the Lateral (Sidewall) Overhead Stowage-Compartment Installation of the Lateral (Sidewall) Overhead Stowage-Compartment Removal of the Center Overhead Stowage-Compartments Installation of the Center Overhead Stowage-Compartments Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door
3. __________ Job Set-up Subtask 05-22-30-010-054 A. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the passenger/crew door. (2) Open the FWD passenger/crew door 831, 841 (Ref. TASK 52-10-00-010801).
EFF : ALL 05-22-30 R SROS
Page 605 Jul 01/06
(3) Remove the galleys, if installed. (4) Remove the lavatories, if installed. (5) Remove the overhead stowage bins from FR17 to FR31 (Ref. TASK 25-24-51-000-801) and (Ref. TASK 25-24-61-000-801). (6) Remove the ceiling panels from FR17 to FR31 (Ref. TASK 25-23-41-000801). R R
(7) Lift the insulation sufficiently to do the inspection without removal of the wiring and ducting. 4. Procedure _________ Subtask 05-22-30-210-054 A. Do a general visual inspection of the forward cabin overhead-compartment (zones 233 and 234). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-22-30-410-054 A. Close Access (1) Put the insulation back in position. (2) Install all the ceiling panels from FR17 to FR31 (Ref. TASK 25-23-41400-801). (3) Install the overhead stowage bins from FR17 to FR31 (Ref. TASK 25-24-51-400-801) and (Ref. TASK 25-24-61-400-801). (4) Install the lavatories, if removed. (5) Install the galleys, if removed. (6) Close the FWD passenger/crew door 831, 841 (Ref. TASK 52-10-00-410801).
EFF : ALL 05-22-30 SROS
Page 606 Jul 01/06
Subtask 05-22-30-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-22-30 R SROS
Page 607 Jul 01/06
ZONAL INSPECTION : MID CABIN UTILITY AREA AFT - INSPECTION/CHECK ________________________________________________________________ TASK 05-22-40-200-802 Zonal Inspection of Mid Cabin Utility Area 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-241-02 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 ------------------------------------------------------------------------------25-22-41-000-801 25-22-41-400-801 25-22-44-000-801 25-22-44-400-801 R
25-23-46-000-801
R
25-23-46-400-801 25-26-41-000-801 25-26-41-400-801 25-26-42-000-801 25-26-42-400-801 25-27-41-000-801 25-27-41-400-801 52-10-00-010-801 52-10-00-410-801 53-00-00-000-801
Removal of the Wall-Mounted Cabin-Attendant Seat Installation of the Wall-Mounted Cabin-Attendant Seat Removal of the Free-Standing Cabin-Attendant Seat, Seat Rail Mounted Installation of the Free-Standing Cabin-Attendant Seat, Seat Rail Mounted Removal of the Door Frame Linings of the Middle Passenger/Crew Door Installation of the Door Frame Linings of the Middle Passenger/Crew Door Removal of the Curtains and the Curtain Rails Installation of the Curtains and the Curtain Rails Removal of the Partitions Installation of the Partitions Removal of the Stowages Installation of the Stowages Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door Removal of the Floor Panels in the Cabin from FR17 to FR80
EFF : ALL 05-22-40 SROS
Page 601 Jul 01/06
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------53-00-00-400-801
Installation of the Floor Panels in the Cabin from FR17 to FR80
3. __________ Job Set-up Subtask 05-22-40-010-051 A. Get Access R R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the MID passenger/crew door. (2) Open the Mid passenger/crew door (Ref. TASK 52-10-00-010-801). (3) Remove the (Ref. TASK (Ref. TASK (Ref. TASK
seats and the furnishings, if installed: 25-27-41-000-801), 25-22-41-000-801), (Ref. TASK 25-22-44-000-801), 25-26-41-000-801), (Ref. TASK 25-26-42-000-801).
(4) Remove the galleys, if installed. (5) Remove the lavatories, if installed. R R
(6) Remove the door frame linings and the floor panels from FR31 to FR36 (Ref. TASK 25-23-46-000-801), (Ref. TASK 53-00-00-000-801). (7) Lift the insulation sufficiently to do the inspection. 4. Procedure _________ Subtask 05-22-40-210-051 A. Do a general visual inspection of the MID cabin utility-area (zones 241 and 242). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping, wiring) are attached correctly.
EFF : ALL 05-22-40 SROS
Page 602 Jul 01/06
5. Close-up ________ Subtask 05-22-40-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. R
(2) Put the insulation back in position.
R
(3) Install the floor panels and the door frame linings from FR31 to FR36 (Ref. TASK 53-00-00-400-801), (Ref. TASK 25-23-46-400-801).
R
(4) Install the lavatories, if removed.
R
(5) Install the galleys, if removed.
R
(6) Install the seats and the furnishings, if removed: (Ref. TASK 25-27-41-400-801), (Ref. TASK 25-22-41-400-801), (Ref. TASK 25-22-44-400-801), (Ref. TASK 25-26-41-400-801), (Ref. TASK 25-26-42-400-801).
R
(7) Make sure that the work area is clean and clear of tools and other items.
R
(8) Close the MID passenger/crew door (Ref. TASK 52-10-00-410-801). Subtask 05-22-40-860-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-22-40 SROS
Page 603 Jul 01/06
TASK 05-22-40-200-804 Zonal Inspection of Mid Cabin Utility Area Overhead Compt 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-243-01 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 ------------------------------------------------------------------------------25-23-41-000-801 25-23-41-400-801 52-10-00-010-801 52-10-00-410-801
Removal of the Ceiling Panels Installation of the Ceiling Panels Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door
3. __________ Job Set-up Subtask 05-22-40-010-053 A. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the MID passenger/crew door. (2) Open the MID passenger/crew door (Ref. TASK 52-10-00-010-801). (3) Remove the galleys, if installed. (4) Remove the lavatories, if installed. (5) Remove the ceiling panels from FR31 to FR36 (Ref. TASK 25-23-41-000801).
EFF : ALL 05-22-40 R SROS
Page 604 Jul 01/06
(6) Lift the insulation sufficiently to do the inspection. 4. Procedure _________ Subtask 05-22-40-210-053 A. Do a general visual inspection of the MID cabin overhead-compartment (zones 243 and 244). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-22-40-410-053 A. Close Access R R
(1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Put the insulation back in position.
R
(3) Install the ceiling panels from FR31 to FR36 (Ref. TASK 25-23-41-400801).
R
(4) Install the lavatories, if removed.
R
(5) Install the galleys, if removed.
R
(6) Close the MID passenger/crew door (Ref. TASK 52-10-00-410-801). Subtask 05-22-40-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-22-40 SROS
Page 605 Jan 01/07
__________________________________________________________________________ ZONAL INSPECTION : MID CABIN AFT OF MID CABIN UTILITY AREA TO FRONT OF AFT CABIN - INSPECTION/CHECK ________________________ TASK 05-22-50-200-802 R
Zonal Inspection of MID Cabin 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-251-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
25-21-41-000-801 25-21-41-400-801 25-23-43-000-802 25-23-43-400-802
Removal of the Passenger Seats Installation of the Passenger Seats Removal of the Sidewall Panel(s) Installation of the Sidewall Panel(s)
52-10-00-010-801 52-10-00-410-801 53-00-00-000-801
Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door Removal of the Floor Panels in the Cabin from FR17 to FR80 Installation of the Floor Panels in the Cabin from FR17 to FR80
R
53-00-00-400-801
EFF : ALL 05-22-50 SROS
Page 601 Jan 01/04
3. __________ Job Set-up Subtask 05-22-50-010-051 A. Get Access R R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the MID passenger/crew door (2) Open the MID passenger/crew door (Ref. TASK 52-10-00-010-801). (3) Remove the galleys, if installed.
R (4) Remove the lavatories, if installed. R R R
(5) Remove the seats (Ref. TASK 25-21-41-000-801).
R R
(6) Remove the sidewall panels and the floor panels from FR36 to FR53.5 (Ref. TASK 25-23-43-000-802), (Ref. TASK 53-00-00-000-801). NOTE : Lift the insulation to do the inspection. ____ 4. Procedure _________ Subtask 05-22-50-210-051
R
A. Do a general visual inspection of the MID cabin (zones 251 and 252). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-22-50-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the floor panels and the sidewall panels from FR36 to FR53.5 (Ref. TASK 53-00-00-400-801), (Ref. TASK 25-23-43-400-802).
EFF : ALL 05-22-50 SROS
Page 602 Jan 01/04
R R
(3) Install the seat (Ref. TASK 25-21-41-400-801). (4) Install the lavatories, if removed.
R R R
(5) Install the galleys, if removed.
R R
(6) Close the MID passenger/crew door (Ref. TASK 52-10-00-410-801).
R R
Subtask 05-22-50-860-050 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-22-50 SROS
Page 603 Jan 01/04
TASK 05-22-50-200-804 R
Zonal Inspection of MID Cabin Overhead Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-253-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R
No specific No specific
1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 STEPLADDER 1.0 M (3.3 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------25-23-41-000-801 25-23-41-400-801 25-24-51-000-801 25-24-51-400-801 25-24-61-000-801 25-24-61-400-801
Removal of the Ceiling Panels Installation of the Ceiling Panels Removal of the Lateral (Sidewall) Overhead Stowage-Compartment Installation of the Lateral (Sidewall) Overhead Stowage-Compartment Removal of the Center Overhead Stowage-Compartments Installation of the Center Overhead Stowage-Compartments
R 52-10-00-010-801 52-10-00-410-801
Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door
EFF : ALL 05-22-50 SROS
Page 604 Jan 01/04
3. __________ Job Set-up Subtask 05-22-50-010-053 A. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the MID passenger/crew door and a STEPLADDER 1.0 M (3.3 FT) in the position (2) Open the MID passenger/crew door (Ref. TASK 52-10-00-010-801). (3) Remove the galleys, if installed. (4) Remove the lavatories, if installed. (5) Remove the overhead stowage compartments (Ref. TASK 25-24-51-000-801), (Ref. TASK 25-24-61-000-801). (6) Remove the ceiling panels from FR36 to FR53.5 (Ref. TASK 25-23-41000-801). R R
(7) Lift the insulation sufficiently to do the inspection without removal of the wiring and ducting. 4. Procedure _________ Subtask 05-22-50-210-053 A. Do a general visual inspection of the MID cabin overhead-compartment (zones 253 and 254). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, wiring) are attached correctly. 5. Close-up ________ Subtask 05-22-50-410-053 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Put the insulation back in position.
EFF : ALL 05-22-50 SROS
Page 605 Jul 01/06
R
(3) Install the ceiling panels from FR36 to FR53.5 (Ref. TASK 25-23-41400-801).
R
(4) Install the overhead stowage compartment (Ref. TASK 25-24-51-400-801), (Ref. TASK 25-24-61-400-801).
R
(5) Install the lavatories, if removed.
R
(6) Install the galleys, if removed.
R
(7) Close the MID passenger/crew door (Ref. TASK 52-10-00-410-801). Subtask 05-22-50-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-22-50 SROS
Page 606 Jul 01/06
___________________________________________________________________________ ZONAL INSPECTION : AFT CABIN AFT OF MID CABIN TO FRONT OF AFT CABIN UTILITY AREA - INSPECTION/CHECK _______________________ TASK 05-22-60-200-802 Zonal Inspection of Aft Cabin 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-261-02 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 ------------------------------------------------------------------------------25-21-41-000-801 25-21-41-400-801 25-23-43-000-802 25-23-43-400-802 25-23-48-000-801 R R
25-23-48-400-801 52-10-00-010-801 52-10-00-410-801 53-00-00-000-801 53-00-00-400-801
Removal of the Passenger Seats Installation of the Passenger Seats Removal of the Sidewall Panel(s) Installation of the Sidewall Panel(s) Removal of the Door Frame Linings of the Emergency Exit Installation of the Door Frame Linings of the Emergency Exit Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door Removal of the Floor Panels in the Cabin from FR17 to FR80 Installation of the Floor Panels in the Cabin from FR17 to FR80
EFF : ALL 05-22-60 SROS
Page 601 Apr 01/04
3. __________ Job Set-up Subtask 05-22-60-010-051 A. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the aft passenger/crew door. R
(2) Open the aft passenger/crew door 833, 843 (Ref. TASK 52-10-00-010801). (3) Remove the seats (Ref. TASK 25-21-41-000-801). (4) Remove the lavatories, if installed. (5) Remove the door frame linings (Ref. TASK 25-23-48-000-801). (6) Remove the sidewall panels and the floor panels from FR53.5 to FR72 (Ref. TASK 53-00-00-000-801), (Ref. TASK 25-23-43-000-802).
R
NOTE : Lift the insulation to do the inspection. ____ 4. Procedure _________ Subtask 05-22-60-210-051 A. Do a general visual inspection of the aft cabin (zones 261 and 262). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-22-60-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the floor panels and the sidewall panels from FR53.5 to FR72 (Ref. TASK 53-00-00-400-801), (Ref. TASK 25-23-43-400-802). (3) Install the door frame linings (Ref. TASK 25-23-48-400-801).
EFF : ALL 05-22-60 SROS
Page 602 Jul 01/06
R
(4) Install the lavatories, if removed.
R
(5) Install the seats (Ref. TASK 25-21-41-400-801).
R
(6) Close the aft passenger/crew door 833, 843, (Ref. TASK 52-10-00-410801). Subtask 05-22-60-860-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-22-60 SROS
Page 603 Apr 01/04
TASK 05-22-60-200-804 Zonal Inspection of Aft Cabin Overhead Compartment 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-263-01 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 ------------------------------------------------------------------------------25-23-41-000-801 25-23-41-400-801 25-24-51-000-801 25-24-51-400-801 25-24-61-000-801 25-24-61-400-801 52-10-00-010-801 52-10-00-410-801
Removal of the Ceiling Panels Installation of the Ceiling Panels Removal of the Lateral (Sidewall) Overhead Stowage-Compartment Installation of the Lateral (Sidewall) Overhead Stowage-Compartment Removal of the Center Overhead Stowage-Compartments Installation of the Center Overhead Stowage-Compartments Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door
3. __________ Job Set-up Subtask 05-22-60-010-053 A. Get Access R R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the aft passenger/crew door. (2) Open the aft passenger/crew door 833 (843) (Ref. TASK 52-10-00-010801).
EFF : ALL 05-22-60 SROS
Page 604 Jul 01/06
(3) Remove the lavatories, if installed. (4) Remove the overhead stowage compartments (Ref. TASK 25-24-51-000-801), (Ref. TASK 25-24-61-000-801). (5) Remove the ceiling panels from FR53.5 to FR72 (Ref. TASK 25-23-41000-801). R R
(6) Lift the insulation sufficiently to do the inspection without removal of the wiring and ducting. 4. Procedure _________ Subtask 05-22-60-210-053 A. Do a general visual inspection of the aft cabin overhead compartment (zones 263 and 264). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-22-60-410-053 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Put the insulation back in position.
R
(3) Install the ceiling panels from FR53.5 to FR72 (Ref. TASK 25-23-41400-801).
R
(4) Install the lavatories, if removed.
R
(5) Install the overhead stowage compartment (Ref. TASK 25-24-51-400-801), (Ref. TASK 25-24-61-400-801).
R
(6) Close the aft passenger/crew door 833 (843) (Ref. TASK 52-10-00-410801).
EFF : ALL 05-22-60 SROS
Page 605 Jul 01/06
Subtask 05-22-60-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-22-60 SROS
Page 606 Jul 01/06
ZONAL INSPECTION : AFT CABIN UTILITY AREA - INSPECTION/CHECK ____________________________________________________________ TASK 05-22-70-200-802 Zonal Inspection of Aft Cabin Utility Area 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-271-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R R
No specific No specific
R
non-metallic scraper with a width of approximately 9 mm (0.35 in.) 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
B. Consumable Materials
R R R
------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R
Material No. 15-010
R
USA MIL-C-11796-C CLASS 1A CORROSION PREVENTIVE FILLER COMPOUND (Ref. 20-31-00)
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------25-22-41-000-801 25-22-41-400-801 25-22-44-000-801 25-22-44-400-801 25-23-47-000-801 25-23-47-400-801
Removal of the Wall-Mounted Cabin-Attendant Seat Installation of the Wall-Mounted Cabin-Attendant Seat Removal of the Free-Standing Cabin-Attendant Seat, Seat Rail Mounted Installation of the Free-Standing Cabin-Attendant Seat, Seat Rail Mounted Removal of the Door Frame Linings of the AFT Passenger/Crew Door Installation of the Door Frame Linings of the AFT Passenger/Crew Door
EFF : ALL 05-22-70 SROS
Page 601 Jan 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------25-27-15-000-801 25-27-15-400-801 25-27-41-000-801 25-27-41-400-801 25-27-42-000-801 25-27-42-400-801 52-10-00-010-801 52-10-00-410-801 53-00-00-000-801 53-00-00-400-801
Removal of the Emergency Equipment Stowage Installation of the Emergency Equipment Stowage Removal of the Stowages Installation of the Stowages Removal of the Doghouses Installation of the Doghouses Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door Removal of the Floor Panels in the Cabin from FR17 to FR80 Installation of the Floor Panels in the Cabin from FR17 to FR80
3. __________ Job Set-up Subtask 05-22-70-010-051 A. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the aft passenger/crew door (2) Open the aft passenger/crew door 833 (843) (Ref. TASK 52-10-00-010801). (3) Remove the galleys, if installed. (4) Remove the lavatories, if installed. (5) Remove the cabin attendant seats, if installed (Ref. TASK 25-22-41-000-801), (Ref. TASK 25-22-44-000-801). (6) Remove the stowages, if installed (Ref. TASK 25-27-15-000-801), (Ref. TASK 25-27-41-000-801), (Ref. TASK 25-27-42-000-801). (7) Remove the door frame linings (Ref. TASK 25-23-47-000-801). (8) Remove the floor panels from FR72 to FR80 (Ref. TASK 53-00-00-000801). NOTE : Lift the insulation sufficiently to do the inspection. ____
EFF : ALL 05-22-70 R SROS
Page 602 Jan 01/05
R R R
(9) Remove the corrosion preventive filling compound STORAGE PRESERVATION (Material No. 15-010) in the seat track with a non-metallic scraper with a width of approximately 9 mm (0.35 in.) 4. Procedure _________ Subtask 05-22-70-210-051 A. Do a general visual inspection of the aft cabin utility-area (zones 271 and 272). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-22-70-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items.
R R
(2) Install the corrosion preventive filling compound STORAGE PRESERVATION (Material No. 15-010) in the seat track.
R
(3) Install the floor panels from FR72 to FR80 (Ref. TASK 53-00-00-400801).
R
(4) Install the door frame linings (Ref. TASK 25-23-47-400-801).
R
(5) Install the stowages, if removed (Ref. TASK 25-27-15-400-801), (Ref. TASK 25-27-41-400-801), (Ref. TASK 25-27-42-400-801).
R
(6) Install the cabin attendant seats, if removed (Ref. TASK 25-22-41-400-801), (Ref. TASK 25-22-44-400-801).
R
(7) Install the lavatories, if removed.
R
(8) Install the galleys, if removed.
R
(9) Close the aft passenger/crew door 833 (843) (Ref. TASK 52-10-00-410801). Subtask 05-22-70-860-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-22-70 SROS
Page 603 Jan 01/05
INTENTIONALLY BLANK
R 05-22-70 SROS
Page 604 Jan 01/05
TASK 05-22-70-200-804 Zonal Inspection of Aft Cabin Utility Area Overhead Compt 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-273-01 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 R R
25-23-41-000-801 25-23-41-400-801 25-23-47-000-801 25-23-47-400-801 25-80-00-000-801 25-80-00-400-801 52-10-00-010-801 52-10-00-410-801
Removal of the Ceiling Panels Installation of the Ceiling Panels Removal of the Door Frame Linings of the AFT Passenger/Crew Door Installation of the Door Frame Linings of the AFT Passenger/Crew Door Removal of the Insulation Blankets Installation of the Insulation Blankets Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door
3. __________ Job Set-up Subtask 05-22-70-010-053 A. Get Access R R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the aft passenger/crew door. (2) Open the aft passenger/crew door 833 (843) (Ref. TASK 52-10-00-010801).
EFF : ALL 05-22-70 SROS
Page 605 Apr 01/04
(3) Remove the galleys, if installed. (4) Remove the lavatories, if installed. R
(5) Remove the door frame linings (Ref. TASK 25-23-47-000-801).
R
(6) Remove the ceiling panels from FR72 to FR80 271AZ, 271BZ, 271CZ, 272AZ, 272BZ, 272CZ (Ref. TASK 25-23-41-000-801).
R
(7) Remove the insulation (Ref. TASK 25-80-00-000-801). 4. Procedure _________ Subtask 05-22-70-210-053 A. Do a general visual inspection of the aft cabin overhead-compartment (zones 273 and 274). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-22-70-410-053 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the insulation (Ref. TASK 25-80-00-400-801). (3) Install the ceiling panels from FR72 to FR80 271AZ, 271BZ, 271CZ, 272AZ, 272BZ, 272CZ (Ref. TASK 25-23-41-400-801).
R
(4) Install the door frame linings (Ref. TASK 25-23-47-400-801).
R
(5) Install the lavatories, if removed.
R
(6) Install the galleys, if removed.
R
(7) Close the aft passenger/crew door 833 (843) (Ref. TASK 52-10-00-410801).
EFF : ALL 05-22-70 SROS
Page 606 Apr 01/04
R R
Subtask 05-22-70-860-051 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-22-70 SROS
Page 607 Jan 01/04
ZONAL INSPECTION : STABILIZERS AND FUSELAGE REAR SECTION - INSPECTION/CHECK ___________________________________________________________________________ TASK 05-23-00-200-801 Zonal Inspection of the Stabilizers and the Fuselage Tail (zone 300). 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information Not Applicable 3. __________ Job Set-up Subtask 05-23-00-869-050 A. Not applicable. 4. Procedure _________ Subtask 05-23-00-210-050 A. Visual inspection. (1) Do a general visual inspection of the stabilizers and the fuselage tail from the ground.
EFF : ALL 05-23-00 R SROS
Page 601 Jan 01/04
TASK 05-23-00-200-802 R
Zonal Inspection of Empennage and Rear Fuselage 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-300-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 15M (49 FT) - ADJUSTABLE
3. __________ Job Set-up Subtask 05-23-00-010-050 A. Get Access R R
(1) Put an ACCESS PLATFORM 15M (49 FT) - ADJUSTABLE in position at the stabilizers and the rear fuselage section (zone 300). 4. Procedure _________ Subtask 05-23-00-210-051 A. Do a general visual inspection of the stabilizers and the rear fuselage (zone 300). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see.
EFF : ALL 05-23-00 SROS
Page 602 Jan 01/04
5. Close-up ________ Subtask 05-23-00-410-050 R
A. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-23-00 SROS
Page 603 Jan 01/04
_____________________________________________________________________ ZONAL INSPECTION : FUSELAGE REAR SECTION AFT OF AFT PRESSURE BULKHEAD ________________ INSPECTION/CHECK TASK 05-23-10-200-801 Zonal Inspection of Rear Fuselage Section 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: ZL-311-01 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
28-27-48-000-801 28-27-48-400-801 05-23-10-991-001-A 05-23-10-991-002-A
Removal of the Trim Tank Transfer Pump (709QN) Installation of the Trim Tank Transfer Pump (709QN) Fig. 601 Fig. 602
EFF : ALL 05-23-10 SROS
Page 601 Jan 01/07
3. __________ Job Set-up Subtask 05-23-10-010-050 A. Get Access (Ref. Fig. 601/TASK 05-23-10-991-001-A, 602/TASK 05-23-10-991-002-A) (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the rear fuselage section (zone 311 and 312). R
(2) Open the access doors 312AR, 313AL and lock them in position.
R R
(3) Remove the pump sealing case, if installed (Ref. TASK 28-27-48-000801). 4. Procedure _________ Subtask 05-23-10-210-050 A. Do a general visual inspection of the rear fuselage section (Zones 311, 312 and 313). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, wiring) are attached correctly. 5. Close-up ________ Subtask 05-23-10-410-050 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items.
R R
(2) Install the pump sealing case, if removed (Ref. TASK 28-27-48-400801).
R
(3) Close the access doors 312AR, 313AL. Subtask 05-23-10-860-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-10 SROS
Page 602 Jan 01/07
Access Panel on the Fuselage Aft Tail-Section (Zones 311 and 312) Figure 601/TASK 05-23-10-991-001-A EFF : ALL 05-23-10 R SROS
Page 603 Jan 01/07
Access Panels on the Fuselage Tail-Cone APU-Compartment (Zones 313, 314, 315, 316 and 317). Figure 602/TASK 05-23-10-991-002-A EFF : ALL Page 604 Jan 01/07 R SROS
05-23-10
TASK 05-23-10-200-802 Zonal Inspection of Tail Cone APU Air Intake Area 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-313-01 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
05-23-10-991-002-A
Fig. 602
3. __________ Job Set-up Subtask 05-23-10-010-051 R
A. Get Access (Ref. Fig. 602/TASK 05-23-10-991-002-A) (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the tail cone, APU air-intake area (zone 313 and 314). (2) Open and secure the access door 313AL.
EFF : ALL 05-23-10 SROS
Page 605 Oct 01/04
4. Procedure _________ Subtask 05-23-10-210-051 A. Do a general visual inspection of the tail cone, APU air-intake area (zones 313 and 314). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-23-10-410-051 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. Subtask 05-23-10-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-10 R SROS
Page 606 Oct 01/04
TASK 05-23-10-200-803 Zonal Inspection of Tail Cone APU and Accessory Compt 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-315-01 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
05-23-10-991-002-A
Fig. 602
3. __________ Job Set-up Subtask 05-23-10-010-052 R
A. Get Access (Ref. Fig. 602/TASK 05-23-10-991-002-A) (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the tail cone, APU and accessory compartment(zones 315 and 316). (2) Open and secure the APU access doors 315AL, 316AR.
EFF : ALL 05-23-10 SROS
Page 607 Oct 01/04
4. Procedure _________ Subtask 05-23-10-210-052 A. Do a general visual inspection of the tail cone, APU accessory compartment (zones 315 and 316). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, piping) are attached correctly. 5. Close-up ________ Subtask 05-23-10-410-052 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the APU access doors 315AL, 316AR. Subtask 05-23-10-860-052 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-10 R SROS
Page 608 Oct 01/04
TASK 05-23-10-200-804 Zonal Inspection of Tail Cone APU Exhaust Area 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: ZL-317-01 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
05-23-10-991-002-A
Fig. 602
3. __________ Job Set-up Subtask 05-23-10-010-053 R
A. Get Access (Ref. Fig. 602/TASK 05-23-10-991-002-A) (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the tail cone, APU exhaust-area (zone 317). (2) Open and secure the APU-Exhaust access fairing 317AL.
EFF : ALL 05-23-10 SROS
Page 609 Oct 01/04
4. Procedure _________ Subtask 05-23-10-210-053 A. Do a general visual inspection of the tail cone, APU exhaust area (zone 317). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (piping) are attached correctly. 5. Close-up ________ Subtask 05-23-10-410-053 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the APU-Exhaust access fairing 317AL. Subtask 05-23-10-860-053 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. R
EFF : ALL 05-23-10 SROS
Page 610 Jul 01/05
TASK 05-23-10-200-806 Zonal Inspection of Horizontal Stabilizer Center Box (Internal) 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: ZL-319-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R R
No specific No specific
adjustable access platform 8.30 m (27 ft. 3 in.) 1 WARNING NOTICE
B. Referenced Information
R R R
------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R R R R
55-11-14-000-801 55-11-14-400-801 05-23-10-991-001-A 05-23-10-991-002-A
Removal of the THS Front-Spar Center-Box Access-Panels 319AL, 319BL, 319AR, 319BR/319DR, 319ER Installation of the THS Front-Spar Center-Box Access-Panels 319AL, 319BL, 319AR, 319BR/319DR, 319ER Fig. 601 Fig. 602
EFF : ALL 05-23-10 SROS
Page 611 Jul 01/05
3. __________ Job Set-up Subtask 05-23-10-941-051 A. Safety Precautions (1) Put a WARNING NOTICE in position - to tell persons not to operate the flight controls. - to tell persons not to operate the fuel system. R R R
Subtask 05-23-10-010-055-C B. Get Access (Ref. Fig. 601/TASK 05-23-10-991-001-A, 602/TASK 05-23-10-991-002-A)
R R
(1) Put an adjustable access platform in position at the horizontal-stabilizer center box (zone 319).
R
(2) Open and secure the access doors 312AR, 313AL.
R
(3) Remove the access panels 319DR, 319ER (Ref. TASK 55-11-14-000-801).
R
(4) Disconnect the pipe of the scavenge water system. 4. Procedure _________ Subtask 05-23-10-210-055 A. Do a general visual inspection of the horizontal-stabilizer center box (Internal) (zone 319). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (piping) are attached correctly. 5. Close-up ________
R R
Subtask 05-23-10-410-055-C A. Close Access
R
(1) Connect the pipe of the scavenge water system.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
R
(3) Install the access panels 319DR, 319ER (Ref. TASK 55-11-14-400-801).
EFF : ALL 05-23-10 SROS
Page 612 Jul 01/05
R
(4) Close the access doors 312AR, 313AL. Subtask 05-23-10-942-051
R
B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-10 SROS
Page 613 Jul 01/05
ZONAL INSPECTION : VERTICAL STABILIZER AND RUDDER - INSPECTION/CHECK ____________________________________________________________________ TASK 05-23-20-200-801 R
Zonal Inspection of Dorsal Fin 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 Refer to the MPD TASK: ZL-321-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R
No specific No specific
1 ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------53-45-11-000-801 53-45-11-400-801
Removal of the Dorsal Fin (321AL) Installation of the Dorsal Fin (321AL)
EFF : ALL 05-23-20 SROS
Page 601 Jan 01/04
3. __________ Job Set-up Subtask 05-23-20-941-050 A. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-23-20-010-050 B. Get Access (1) Put an ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE in position at the dorsal fin (zone 321). (2) Remove the access panel 321AL (Ref. TASK 53-45-11-000-801). 4. Procedure _________ Subtask 05-23-20-210-050 R
A. Inspection
R
(1) Do a general visual inspection of the dorsal fin (zone 321).
R
(2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and structure you can see. - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-23-20-410-050 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the dorsal fin 321AL (Ref. TASK 53-45-11-400-801).
EFF : ALL 05-23-20 SROS
Page 602 Jul 01/04
Subtask 05-23-20-942-050 B. Put the Aircraft back to its Initial Configuration R R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-20 SROS
Page 603 Jan 01/04
TASK 05-23-20-200-802 R
Zonal Inspection of Vertical Stabilizer Leading Edge 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 Refer to the MPD TASK: ZL-322-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R
No specific No specific
1 ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------55-32-11-000-801 55-32-11-400-801
Removal of the Vertical Stabilizer Leading-Edge Installation of the Vertical Stabilizer Leading-Edge
EFF : ALL 05-23-20 SROS
Page 604 Jan 01/04
3. __________ Job Set-up Subtask 05-23-20-941-051 A. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. R R
Subtask 05-23-20-010-051-A B. Get Access
R R
(1) Put an ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE in position at the vertical-stabilizer leading edge (zone 322).
R R
(2) Remove the access panels 322AL, 322BL, 322CL, 322DL (Ref. TASK 55-3211-000-801). 4. Procedure _________ Subtask 05-23-20-210-051
R
A. Do a general visual inspection of the vertical-stabilizer leading edge (zone 322). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (wiring) are attached correctly. 5. Close-up ________
R R
Subtask 05-23-20-410-051-A 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 access panels 322AL, 322BL, 322CL, 322DL (Ref. TASK 5532-11-400-801). Subtask 05-23-20-942-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-20 SROS
Page 605 Jul 01/06
TASK 05-23-20-200-803 Zonal Inspection of Vertical Stabilizer Spar Box 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 Refer to the MPD TASK: ZL-323-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
1 ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------05-23-20-991-002
Fig. 601
3. __________ Job Set-up Subtask 05-23-20-941-052 A. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls.
EFF : ALL 05-23-20 R SROS
Page 606 Jul 01/06
Subtask 05-23-20-010-052 B. Get Access (Ref. Fig. 601/TASK 05-23-20-991-002) (1) Put an ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE in position at the vertical-stabilizer spar box (zone 323). R
(2) Open and safety the access door 312AR. (3) Remove the access panels 311AZ, 311BZ. 4. Procedure _________ Subtask 05-23-20-210-052 A. Do a general visual inspection of the vertical-stabilizer spar box (zone 323). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (piping) are attached correctly. 5. Close-up ________ Subtask 05-23-20-410-052 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels 311AZ, 311BZ. (3) Close the access door 312AR. Subtask 05-23-20-942-052 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-20 SROS
Page 607 Jul 01/06
Access Panels on the Fuselage Aft Tail-Section Figure 601/TASK 05-23-20-991-002 EFF : ALL 05-23-20 R SROS
Page 608 Jul 01/06
TASK 05-23-20-200-804 Zonal Inspection of Vertical Stabilizer Spar Box 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 Refer to the MPD TASK: ZL-323-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific No specific
adjustable access platform 16.80 m (55 ft. 1 in.) 1 WARNING NOTICE
B. Consumable Materials ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------Material No. 05-052 SELF-ADHES.PVC DISKS FOR HOISTING POINT BLANKING (Ref. 20-31-00)
EFF : ALL 05-23-20 SROS
Page 609 Jul 01/06
C. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------53-55-11-000-801 53-55-11-400-801 55-32-11-000-801 55-32-11-400-801 55-33-13-000-801 55-33-13-400-801
Removal of the Vertical Stabilizer Fairings Installation of the Vertical Stabilizer Fairings Removal of the Vertical Stabilizer Leading-Edge Installation of the Vertical Stabilizer Leading-Edge Removal of the Vertical-Stabilizer Trailing-Edge Access-Panels Installation of the Vertical-Stabilizer Trailing-Edge Access-Panels
R 3. __________ Job Set-up Subtask 05-23-20-941-053 A. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. R R
Subtask 05-23-20-010-053-A B. Get Access
R R
(1) Put an adjustable access platform in position at the vertical-stabilizer spar box (zone 323).
R
(2) Open the access door 312AR
R
(3) Remove the access panels 311AZ, 311BZ.
R R R
(4) Remove the access panels 322AL, 322BL, 322CL, 322DL (Ref. TASK 55-3211-000-801), 323CL, 323DL, 325LL. (Ref. TASK 53-55-11-000-801)
R R
(5) Remove the access panels 325ML, 325NL, 325PL, 325QL, 325RL (Ref. TASK 55-33-13-000-801).
R R
(6) Remove the vertical stabilizer fairings 323CL, 323DL and 325LL (Ref. TASK 53-55-11-000-801).
R
(7) Remove and discard the self-adhesive discs from the hoisting points.
EFF : ALL 05-23-20 SROS
Page 610 Jul 01/06
4. Procedure _________ Subtask 05-23-20-210-053
R
A. Do a general visual inspection of the vertical-stabilizer spar box (zone 323). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (piping) are attached correctly. 5. Close-up ________
R R
Subtask 05-23-20-410-053-A A. Close Access
R R
(1) Put the SPECIAL MATERIALS (Material No. 05-052) on the hoisting points.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
R R
(3) Install the access panels 325ML, 325NL, 325PL, 325QL, 325RL. (Ref. TASK 55-33-13-400-801)
R R
(4) Install the fairings 323CL, 323DL, 325LL. (Ref. TASK 53-55-11-400801)
R R
(5) Install the access panels 322AL, 322BL, 322CL, 322DL. (Ref. TASK 5532-11-400-801)
R
(6) Install the access panels 311AZ, 311BZ.
R
(7) Close the access door 312AR.
R
(8) Remove the access platform(s). Subtask 05-23-20-942-053 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-20 SROS
Page 611 Jul 01/06
TASK 05-23-20-200-805 Zonal Inspection of Vertical Stabilizer Tip 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 Refer to the MPD TASK: ZL-324-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
1 ACCESS PLATFORM 15M (49 FT) - ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------55-34-11-000-801 55-34-11-400-801
Removal of the Vertical Stabilizer Tip Installation of the Vertical Stabilizer Tip
EFF : ALL 05-23-20 R SROS
Page 612 Jul 01/06
3. __________ Job Set-up Subtask 05-23-20-941-054 A. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. R R
Subtask 05-23-20-010-054-A B. Get Access
R R
(1) Put an ACCESS PLATFORM 15M (49 FT) - ADJUSTABLE in position at the vertical stabilizer tip (zone 324).
R
(2) Remove the access panel 324CT (Ref. TASK 55-34-11-000-801). 4. Procedure _________ Subtask 05-23-20-210-054 A. Do a general visual inspection of the vertical stabilizer tip (zone 324). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring) are attached correctly. 5. Close-up ________
R R
Subtask 05-23-20-410-054-A A. Close Access
R R
(1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Install the access panel 324CT (Ref. TASK 55-34-11-400-801). Subtask 05-23-20-942-054 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-20 SROS
Page 613 Jul 01/06
INTENTIONALLY BLANK
R 05-23-20 SROS
Page 614 Jul 01/06
TASK 05-23-20-200-806 R
Zonal Inspection of Vertical Stabilizer Trailing Edge 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 Refer to the MPD TASK: ZL-325-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R
No specific No specific
1 ACCESS PLATFORM 15M (49 FT) - ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------55-33-13-000-801 55-33-13-400-801
Removal of the Vertical-Stabilizer Trailing-Edge Access-Panels Installation of the Vertical-Stabilizer Trailing-Edge Access-Panels
EFF : ALL 05-23-20 SROS
Page 615 Jan 01/04
3. __________ Job Set-up Subtask 05-23-20-941-055 A. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. R R
Subtask 05-23-20-010-055-A B. Get Access
R R
(1) Put an ACCESS PLATFORM 15M (49 FT) - ADJUSTABLE in position at the vertical-stabilizer trailing edge (zone 325).
R
(2) Remove the access panel 325NL (Ref. TASK 55-33-13-000-801). 4. Procedure _________ Subtask 05-23-20-210-055 A. Do a general visual inspection of the vertical-stabilizer trailing edge (zone 325). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring) are attached correctly. 5. Close-up ________
R R
Subtask 05-23-20-410-055-A A. Close Access
R R
(1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Install the access panel 325NL (Ref. TASK 55-33-13-400-801). Subtask 05-23-20-942-055 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-20 SROS
Page 616 Jul 01/04
TASK 05-23-20-200-807 Zonal Inspection of Vertical Stabilizer Trailing Edge 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 Refer to the MPD TASK: ZL-325-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific No specific
adjustable access platform 16.80 m (55 ft. 1 in.) 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------55-33-13-000-801 55-33-13-400-801
Removal of the Vertical-Stabilizer Trailing-Edge Access-Panels Installation of the Vertical-Stabilizer Trailing-Edge Access-Panels
EFF : ALL 05-23-20 SROS
Page 617 Jul 01/04
3. __________ Job Set-up Subtask 05-23-20-941-056 A. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. R R
Subtask 05-23-20-010-056-A B. Get Access
R R
(1) Put an adjustable access platform in position at the vertical-stabilizer trailing edge (zone 325).
R R
(2) Remove the access panels 325LL, 325ML, 325NL, 325PL, 325QL, 325RL (Ref. TASK 55-33-13-000-801). 4. Procedure _________ Subtask 05-23-20-210-056 A. Do a general visual inspection of the vertical-stabilizer trailing edge (zone 325). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring) are attached correctly. 5. Close-up ________
R R
Subtask 05-23-20-410-056-A 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 access panels 325LL, 325ML, 325NL, 325PL, 325QL, 325RL (Ref. TASK 55-33-13-400-801). Subtask 05-23-20-942-056 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-20 SROS
Page 618 Jul 01/04
TASK 05-23-20-200-809 Zonal Inspection of Rudder 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 Refer to the MPD TASK: ZL-326-01 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 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R R R
55-33-13-000-801 55-33-13-400-801 55-42-13-000-801 55-42-13-400-801
Removal of the Vertical-Stabilizer Trailing-Edge Access-Panels Installation of the Vertical-Stabilizer Trailing-Edge Access-Panels Removal of the Leading Edge Access-Panels 326 Installation of the Leading Edge Access-Panels 326
EFF : ALL 05-23-20 SROS
Page 619 Jul 01/04
3. __________ Job Set-up Subtask 05-23-20-941-058 A. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-23-20-010-058-A B. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the rudder (zone 326). (2) Remove the trailing-edge panel 325NL (Ref. TASK 55-33-13-000-801). (3) Remove the vertical stabilizer leading-edge panels 326ML, 326NL, 326PL (Ref. TASK 55-42-13-000-801). 4. Procedure _________ Subtask 05-23-20-210-058 R
A. Do a general visual inspection of the rudder (zone 326) in the area of the bearings 2, 3 and 4. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-23-20-410-058-A A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the leading-edge panels 326ML, 326NL, 326PL (Ref. TASK 55-4213-400-801). (3) Install the vertical stabilizer trailing-edge panels 325NL (Ref. TASK 55-33-13-400-801).
EFF : ALL 05-23-20 SROS
Page 620 Jan 01/07
Subtask 05-23-20-942-058 R
B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-20 SROS
Page 621 Jul 01/04
TASK 05-23-20-200-810 Zonal Inspection of Rudder 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 Refer to the MPD TASK: ZL-326-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific No specific
adjustable access platform 16.80 m (55 ft. 1 in.) 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R R
55-33-13-000-801 55-33-13-400-801 55-42-13-000-801 55-42-13-400-801
Removal of the Vertical-Stabilizer Trailing-Edge Access-Panels Installation of the Vertical-Stabilizer Trailing-Edge Access-Panels Removal of the Leading Edge Access-Panels 326 Installation of the Leading Edge Access-Panels 326
EFF : ALL 05-23-20 SROS
Page 622 Jul 01/04
3. __________ Job Set-up Subtask 05-23-20-941-059 A. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-23-20-010-059-A B. Get Access (1) Put an adjustable access platform in position at the rudder (zone 326). (2) Remove the access panels 325NL, 325SL, 325UL, 325VL (Ref. TASK 55-3313-000-801), 326ML, 326NL, 326PL, 326RL, 326SL (Ref. TASK 55-42-13-000-801). 4. Procedure _________ R R R R R
Subtask 05-23-20-210-059-A A. Do a general visual inspection of the rudder (zone 326) in the area of the bearings 1 to 8. Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-23-20-410-059-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 326ML, 326NL, 326PL, 326RL, 326SL (Ref. TASK 55-42-13-400-801). 325NL, 325SL, 325UL, 325VL (Ref. TASK 55-33-13-400-801). Subtask 05-23-20-942-059 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-20 SROS
Page 623 Apr 01/05
TASK 05-23-20-200-811 Zonal Inspection of Rudder (Front Spar FWD Face and Internal Structure as far as visible) 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 Refer to the MPD TASK: ZL-326-03 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
1 ACCESS PLATFORM 17M (56 FT) - ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------53-55-11-000-801 53-55-11-400-801 55-33-13-000-801 55-33-13-400-801 55-34-11-000-801 55-34-11-400-801 55-42-13-000-801
Removal of the Vertical Stabilizer Fairings Installation of the Vertical Stabilizer Fairings Removal of the Vertical-Stabilizer Trailing-Edge Access-Panels Installation of the Vertical-Stabilizer Trailing-Edge Access-Panels Removal of the Vertical Stabilizer Tip Installation of the Vertical Stabilizer Tip Removal of the Leading Edge Access-Panels 326
R EFF : ALL 05-23-20 SROS
Page 624 Jul 01/06
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------55-42-13-400-801 55-44-11-000-801 55-44-11-400-801
Installation of the Leading Edge Access-Panels 326 Removal of the Rudder Tip Installation of the Rudder Tip
3. __________ Job Set-up Subtask 05-23-20-941-060 A. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-23-20-010-060-A B. Get Access (1) Put an ACCESS PLATFORM 17M (56 FT) - ADJUSTABLE in position at the rudder (zone 326). (2) Remove the access panels 325ML, 325NL, 325PL, 325QL, 325RL, 325MR, 325NR, 325PR, 325QR, 325RR (Ref. TASK 55-33-13-000-801). (3) Remove the access panels 326ML, 326NL, 326PL, 326QL (Ref. TASK 55-4213-000-801). R
(4) Remove the access panels 325LL, 325LR, (Ref. TASK 53-55-11-000-801). (5) Remove the rudder tip 326AT (Ref. TASK 55-44-11-000-801). (6) Remove the tip 324CT (Ref. TASK 55-34-11-000-801). 4. Procedure _________ Subtask 05-23-20-210-060
R R R
A. Do a general visual inspection of the front spar forward face and the internal structure of the rudder (zone 326) as far as you can see. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (wiring) are attached correctly.
EFF : ALL 05-23-20 SROS
Page 625 Jul 01/06
5. Close-up ________ Subtask 05-23-20-410-060-A A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the tip 324CT (Ref. TASK 55-34-11-400-801). (3) Install the rudder tip 326AT (Ref. TASK 55-44-11-400-801). R
(4) Install the access panels 325LL, 325LR (Ref. TASK 53-55-11-400-801). (5) Install the access panels 325ML, 325NL, 325PL, 325QL, 325RL, 325MR, 325NR, 325PR, 325QR, 325RR (Ref. TASK 55-33-13-400-801). (6) Install the access panels 326ML, 326NL, 326PL, 326QL (Ref. TASK 5542-13-400-801). Subtask 05-23-20-942-060 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-20 SROS
Page 626 Jul 01/06
______________________________________________________________________________ ZONAL INSPECTION : TRIMMABLE HORIZONTAL STABILIZER LEFT SIDE AND LEFT ELEVATOR ________________ INSPECTION/CHECK TASK 05-23-30-200-801 R
Zonal Inspection of Horizontal Stabilizer Leading Edge 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 Refer to the MPD TASK: ZL-331-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R
No specific No specific
1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------55-12-11-000-801 55-12-11-400-801 55-15-11-000-801 55-15-11-400-801
Removal of the Horizontal Stabilizer Leading-Edge Installation of the Horizontal Stabilizer Leading-Edge Removal of the THS Apron Fairing Assemblies Installation of the THS Apron Fairing Assemblies
EFF : ALL 05-23-30 SROS
Page 601 Jan 01/04
3. __________ Job Set-up Subtask 05-23-30-941-050 A. Safety Precautions R R
(1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-23-30-010-050 B. Get Access
R R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the horizontal-stabilizer leading edge (zones 331 and 341).
R
(2) Remove the access panels:
R R
(a) For the left side 331AT, 333AB, 333AT (Ref. TASK 55-15-11-000801). 331BT, 331CT, 331DT, 331ET (Ref. TASK 55-12-11-000-801).
R R
(b) For the right side 341AT, 343AT, 343AB (Ref. TASK 55-15-11-000801). 341BT, 341CT, 341DT, 341ET (Ref. TASK 55-12-11-000-801). 4. Procedure _________ Subtask 05-23-30-210-050 A. Do a general visual inspection of the horizontal-stabilizers leading edge (zones 331 and 341). Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-23-30-410-050 A. Close Access
R R
(1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Install the access panels
R R
(a) For the left side 331AT, 333AB, 333AT (Ref. TASK 55-15-11-400801). 331BT, 331CT, 331DT (Ref. TASK 55-12-11-400-801).
EFF : ALL 05-23-30 SROS
Page 602 Jan 01/04
R R R
(b) For the right side: 341AT, 343AT, 343AB (Ref. TASK 55-15-11-400801). 341BT, 341CT, 341DT, 341ET (Ref. TASK 55-12-11-400-801). Subtask 05-23-30-942-050 B. Put the Aircraft back to its Initial Configuration
R R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-30 SROS
Page 603 Jan 01/04
TASK 05-23-30-200-802 R
Zonal Inspection of Horizontal Stabilizer Tip 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 Refer to the MPD TASK: ZL-332-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R
No specific No specific
1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------55-14-11-000-801 55-14-11-400-801
Removal of the Trimmable Horizontal Stabilizer Tips Installation of the Trimmable Horizontal Stabilizer Tips
EFF : ALL 05-23-30 SROS
Page 604 Jan 01/04
3. __________ Job Set-up Subtask 05-23-30-941-051 A. Safety Precautions R R
(1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-23-30-010-051 B. Get Access
R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the horizontal stabilizer tip (zones 332 and 342).
R R
(2) Remove the tip on the left and right sides 332AB, 332AT, 342AB, 342AT (Ref. TASK 55-14-11-000-801). 4. Procedure _________ Subtask 05-23-30-210-051 A. Do a general visual inspection of the horizontal stabilizer tip (zones 332 and 342). Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-23-30-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items.
R R R
(2) Install the tip on the left and right sides 332AB, 332AT, 342AB, 342AT (Ref. TASK 55-14-11-400-801).
EFF : ALL 05-23-30 SROS
Page 605 Jan 01/04
Subtask 05-23-30-942-051 B. Put the Aircraft back to its Initial Configuration R R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-30 SROS
Page 606 Jan 01/04
TASK 05-23-30-200-804 Zonal Inspection of Horizontal Stabilizer Lateral Box 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 Refer to the MPD TASK: ZL-333-01 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 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R R
55-11-14-000-802 55-11-14-400-802 55-12-11-000-801 55-12-11-400-801 55-15-11-000-801 55-15-11-400-801
Removal of the THS Front-Spar Access-Panels 333AL, 343AR Installation of the THS Front-Spar Access-Panels 333AL, 343AR Removal of the Horizontal Stabilizer Leading-Edge Installation of the Horizontal Stabilizer Leading-Edge Removal of the THS Apron Fairing Assemblies Installation of the THS Apron Fairing Assemblies
EFF : ALL 05-23-30 SROS
Page 607 Jul 01/04
3. __________ Job Set-up Subtask 05-23-30-941-053 A. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-23-30-010-053 B. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the horizontal-stabilizer side box (zone 333 and 343). (2) Remove the access panels (a) For the left side 331AT, 333AT, 333AB (Ref. TASK 55-15-11-000801). 331BT (Ref. TASK 55-12-11-000-801). 333AL (Ref. TASK 55-1114-000-802). (b) For the right side 341AT, 343AT, 343AB (Ref. TASK 55-15-11-000801). 341BT (Ref. TASK 55-12-11-000-801). 343AR (Ref. TASK 55-1114-000-802). 4. Procedure _________ Subtask 05-23-30-210-053 A. Do a general visual inspection of the horizontal-stabilizer side box (Rib 3 to Rib 4) (zones 333 and 343). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (piping) are attached correctly.
EFF : ALL 05-23-30 R SROS
Page 608 Jul 01/04
5. Close-up ________ Subtask 05-23-30-410-053 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels (a) For the left side 331AT, 333AT, 333AB (Ref. TASK 55-15-11-400801). 331BT (Ref. TASK 55-12-11-400-801). 333AL (Ref. TASK 55-1114-400-802). (b) For the right side 341AT, 343AT, 343AB (Ref. TASK 55-15-11-400801). 341BT (Ref. TASK 55-12-11-400-801). 343AR (Ref. TASK 55-1114-400-802). Subtask 05-23-30-942-053 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-23-30 R SROS
Page 609 Jan 01/06
TASK 05-23-30-200-805 Zonal Inspection of Horizontal Stabilizer Trailing Edge (From Fuselage Fairing to Rib 10) 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 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-334-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
warning notices 1 ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------55-13-11-000-801 55-13-11-400-801
Removal of the Trailing-Edge Access Panels Installation of the Trailing-Edge Access Panels
3. __________ Job Set-up Subtask 05-23-30-941-054 A. Safety Precautions R R
(1) Put warning notices in the cockpit to tell persons not to operate the flight controls.
EFF : ALL 05-23-30 SROS
Page 610 Jan 01/06
Subtask 05-23-30-010-054 B. Get Access (1) Put an ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE in position at the horizontal-stabilizer trailing edge (zones 334 and 344). (2) Remove the access panels - For the left side: 334AB, 334BB, 334CB (Ref. TASK 55-13-11-000-801). - For the right side: 344AB, 344BB, 344CB (Ref. TASK 55-13-11-000-801). 4. Procedure _________ Subtask 05-23-30-210-054 A. Do a general visual inspection of the horizontal-stabilizer trailing edge from fuselage fairing to rib 10 (zones 334 and 344). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (piping) are attached correctly. 5. Close-up ________ Subtask 05-23-30-410-054 A. Close Access (1) Install the access panels - For the left side: 334AB, 334BB, 334CB (Ref. TASK 55-13-11-400-801). - For the right side: 344AB, 344BB, 344CB (Ref. TASK 55-13-11-400-801).
EFF : ALL 05-23-30 R SROS
Page 611 Jan 01/06
Subtask 05-23-30-942-054 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-23-30 R SROS
Page 612 Jan 01/06
TASK 05-23-30-200-806 Zonal Inspection of Horizontal Stabilizer Trailing Edge (From Fuselage Fairing to Rib 21) 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 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-334-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
warning notices 1 ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------55-13-11-000-801 55-13-11-400-801
Removal of the Trailing-Edge Access Panels Installation of the Trailing-Edge Access Panels
3. __________ Job Set-up Subtask 05-23-30-941-055 A. Safety Precautions R R
(1) Put warning notices in the cockpit to tell persons not to operate the flight controls.
EFF : ALL 05-23-30 SROS
Page 613 Jan 01/06
Subtask 05-23-30-010-055 B. Get Access (1) Put an ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE in position at the horizontal-stabilizer trailing edge (zones 334 and 344). (2) Remove the access panels - For the left side: 334AB, 334BB, 334CB, 334DB, 334EB, 334FB, 334GB (Ref. TASK 55-13-11-000-801). - For the right side: 344AB, 344BB, 344CB, 344DB, 344EB, 344FB, 344GB (Ref. TASK 55-13-11-000-801). 4. Procedure _________ Subtask 05-23-30-210-055 A. Do a general visual inspection of the horizontal-stabilizer trailing edge from fuselage fairing to rib 21 (zones 334 and 344). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (piping) are attached correctly. 5. Close-up ________ Subtask 05-23-30-410-055 A. Close Access (1) Install the access panels - For the left side: 334AB, 334BB, 334CB, 334DB, 334EB, 334FB, 334GB (Ref. TASK 55-13-11-400-801). - For the right side: 344AB, 344BB, 344CB, 344DB, 344EB, 344FB, 344GB (Ref. TASK 55-13-11-400-801).
EFF : ALL 05-23-30 R SROS
Page 614 Jan 01/06
Subtask 05-23-30-942-055 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-23-30 R SROS
Page 615 Jan 01/06
TASK 05-23-30-200-807 Zonal Inspection of Elevator (Area between Ribs 8 and 9) 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 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-335-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
warning notices 1 ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------55-13-11-000-801 55-13-11-400-801 55-22-11-000-801 55-22-11-400-801
Removal of the Trailing-Edge Access Panels Installation of the Trailing-Edge Access Panels Removal of the Elevator Leading Edge Installation of the Elevator Leading Edge
EFF : ALL 05-23-30 SROS
Page 616 Jan 01/06
3. __________ Job Set-up Subtask 05-23-30-941-056 A. Safety Precautions (1) Put warning notices in the cockpit to tell persons not to operate the flight controls. Subtask 05-23-30-010-056 B. Get Access (1) Put an ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE in position at the elevator (zones 335 and 345). (2) Remove the access panels - For the left side: 335BB (Ref. TASK 55-22-11-000-801), 334BB, 334CB, 334DB (Ref. TASK 55-13-11-000-801). - For the right side: 345BB (Ref. TASK 55-22-11-000-801), 344BB, 344CB, 344DB (Ref. TASK 55-13-11-000-801). 4. Procedure _________ Subtask 05-23-30-210-056 R R
A. Do a general visual inspection of the elevator between HTP ribs 8 and 9 (zones 335 and 345). Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see.
EFF : ALL 05-23-30 SROS
Page 617 Jan 01/07
5. Close-up ________ Subtask 05-23-30-410-056 A. Close Access (1) Install the access panels - For the left side: 335BB (Ref. TASK 55-22-11-400-801), 334BB, 334CB, 334DB (Ref. TASK 55-13-11-400-801). - For the right side: 345BB (Ref. TASK 55-22-11-400-801), 344BB, 344CB, 344DB (Ref. TASK 55-13-11-400-801).
R
R
Subtask 05-23-30-942-056 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-23-30 SROS
Page 618 Jan 01/06
TASK 05-23-30-200-808 Zonal Inspection of Elevator (Leading Edge as far as Visible) 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 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-335-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
1 ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------55-13-11-000-801 55-13-11-400-801 55-22-11-000-801 55-22-11-400-801
Removal of the Trailing-Edge Access Panels Installation of the Trailing-Edge Access Panels Removal of the Elevator Leading Edge Installation of the Elevator Leading Edge
EFF : ALL 05-23-30 SROS
Page 619 Jan 01/06
3. __________ Job Set-up Subtask 05-23-30-941-057 A. Safety Precautions R R
(1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-23-30-010-057 B. Get Access (1) Put an ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE in position at the elevator (zones 335 and 345). (2) Remove the access panels: - For the left side: 335AB, 335BB, 335CB, 335DB, 335EB, (Ref. TASK 55-22-11-000-801), 334AB, 334BB, 334CB, 334DB, 334EB, (Ref. TASK 55-13-11-000-801). - For the right side: 345AB, 345BB, 345CB, 345DB, 345EB, (Ref. TASK 55-22-11-000-801), 344AB, 344BB, 344CB, 344DB, 344EB, (Ref. TASK 55-13-11-000-801).
R
R
335FB 334FB, 334GB 345FB 344FB, 344GB
4. Procedure _________ Subtask 05-23-30-210-057 A. Do a general visual inspection of the elevator (zones 335 and 345) leading edge, as far as you can see. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see.
EFF : ALL 05-23-30 SROS
Page 620 Jan 01/06
5. Close-up ________ Subtask 05-23-30-410-057 A. Close Access (1) Install the access panels: - For the left side: 335AB, 335BB, 335CB, 335DB, 335EB, (Ref. TASK 55-22-11-400-801), 334AB, 334BB, 334CB, 334DB, 334EB, (Ref. TASK 55-13-11-400-801). - For the right side: 345AB, 345BB, 345CB, 345DB, 345EB, (Ref. TASK 55-22-11-400-801), 344AB, 344BB, 344CB, 344DB, 344EB, (Ref. TASK 55-13-11-400-801).
R
R
335FB 334FB, 334GB 345FB 344FB, 344GB
Subtask 05-23-30-942-057 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-23-30 SROS
Page 621 Jan 01/06
ZONAL INSPECTION : POWER PLANT, NACELLES AND PYLONS - INSPECTION/CHECK ______________________________________________________________________ TASK 05-24-00-200-801 Zonal Inspection as far as visible from the ground of the Power Plant, the Nacelles and the Pylons (zone 400). 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------54-50-00-200-804
Inspection for Missing Fasteners on the Pylon Fairing Panels
3. __________ Job Set-up Subtask 05-24-00-869-050 A. Not applicable. 4. Procedure _________ Subtask 05-24-00-210-050 A. Inspection (1) Do a general visual inspection of the power plant, the nacelles and the pylons from the ground during the aircraft walkaround. (2) Inspect the pylon fairing panels for missing fasteners (Ref. TASK 5450-00-200-804).
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TASK 05-24-00-200-802 R
Zonal Inspection of Power Plants, Nacelles and Pylons. 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-400-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------54-50-00-200-804
Inspection for Missing Fasteners on the Pylon Fairing Panels
3. __________ Job Set-up Subtask 05-24-00-010-050 A. Get Access R R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at zone 400. 4. Procedure _________ Subtask 05-24-00-210-051 A. Inspection
R R
(1) Do a general visual inspection of the power plants, the nacelles and the pylons (zone 400). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see.
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(2) Inspect the pylon fairing panels for missing fasteners (Ref. TASK 5450-00-200-804). R
5. Close-up ________
R
Subtask 05-24-00-860-050
R
A. Put the Aircraft back to its Initial Configuration
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(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
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(2) Make sure that the work area is clean and clear of tools and other items.
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ZONAL INSPECTION : ENGINE - INSPECTION/CHECK ____________________________________________ TASK 05-24-10-200-808-A General Visual Inspection of the Engine Air Intake and Intake Lip 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-411-03 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) warning notice adjustable access platform 2.30 m (7 ft. 7 in.) access platform 2.5 m (8 ft. 2 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 78-30-00-040-804 78-30-00-440-804 05-24-10-991-045 05-24-10-991-046 05-24-10-991-047 05-24-10-991-048
Energize the Ground Service Network De-energize the Ground Service Network Deactivation of the Thrust Reverser for Maintenance Reactivation of the Thrust Reverser after Maintenance Fig. 601 Fig. 602 Fig. 603 Fig. 604
3. __________ Job Set-up Subtask 05-24-10-861-066 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801).
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Subtask 05-24-10-941-095 B. Safety Precautions (1) Make sure that the engine 1 (2) shutdown occurred not less than 5 minutes before you do the inspection. (2) Put a warning notice in the cockpit to tell persons not to start the engines. Subtask 05-24-10-010-099 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 05-24-10-865-098 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 05-24-10-040-074 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3000-040-804).
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Subtask 05-24-10-010-100 F. Get Access (Ref. Fig. 601/TASK 05-24-10-991-045, 602/TASK 05-24-10-991-046, 603/TASK 05-24-10-991-047, 604/TASK 05-24-10-991-048) (1) Put an adjustable access platform in position at the engine air intake and intake lip (zones 411 and 421). (2) Remove the access panels FOR 4030EM1 411AR, 411AL FOR 4030EM2 421AR, 421AL 4. Procedure _________ Subtask 05-24-10-210-088 A. Inspection. (1) Do a general visual inspection of the engine air intake and intake lip (zones 411 and 421). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting) are attached correctly. 5. Close-up ________ Subtask 05-24-10-440-074 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3000-440-804). Subtask 05-24-10-865-099 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
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Access Doors/ Panels of the Engine 1 Nacelle - Right Side Figure 601/TASK 05-24-10-991-045 R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-10 Page 604 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
Access Doors/ Panels of the Engine 1 Nacelle - Left Side Figure 602/TASK 05-24-10-991-046 R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-10 Page 605 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
Access Doors/ Panels of the Engine 2 Nacelle - Right Side Figure 603/TASK 05-24-10-991-047 R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-10 Page 606 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
Access Doors/ Panels of the Engine 2 Nacelle - Left Side Figure 604/TASK 05-24-10-991-048 R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-10 Page 607 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
Subtask 05-24-10-410-090 C. Installation of the Panels. (Ref. Fig. 601/TASK 05-24-10-991-045, 602/TASK 05-24-10-991-046, 603/TASK 05-24-10-991-047, 604/TASK 05-24-10-991-048) (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels: FOR 4030EM1 411AR, 411AL FOR 4030EM2 421AR, 421AL Subtask 05-24-10-942-094 D. Close Access (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Remove the warning notice in the cockpit. (4) Close the access door 811. (5) Remove the access platform(s). Subtask 05-24-10-862-065 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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TASK 05-24-10-200-809-A General Visual Inspection of the Engine Air Intake and Intake Lip 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-411-04 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 notice adjustable access platform 2.30 m (7 ft. 7 in.) access platform 2.5 m (8 ft. 2 in.)
B. 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 05-24-10-991-045 05-24-10-991-046 05-24-10-991-047 05-24-10-991-048
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. 601 Fig. 602 Fig. 603 Fig. 604
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3. __________ Job Set-up Subtask 05-24-10-861-067 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 05-24-10-941-096 B. Safety Precautions (1) Make sure that the engine 1 (2) shutdown occurred not less than 5 minutes before you do the inspection. (2) Put a warning notice in the cockpit to tell persons not to start the engines. Subtask 05-24-10-010-101 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 05-24-10-865-100 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 05-24-10-040-075 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3000-040-804). Subtask 05-24-10-010-102 F. Get Access (Ref. Fig. 601/TASK 05-24-10-991-045, 602/TASK 05-24-10-991-046, 603/TASK 05-24-10-991-047, 604/TASK 05-24-10-991-048) (1) Put an adjustable access platform in position at the engine air intake and intake lip (zones 411 and 421). (2) Open the fan cowl doors (Ref. TASK 71-13-00-010-802) FOR 4030EM1 415AL, 415BL, 416AR, 416BR FOR 4030EM2 425AL, 425BL, 426AR, 426BR (3) Remove the access panels: FOR 4030EM1 411AL, 411AR FOR 4030EM2 421AL, 421AR 4. Procedure _________ Subtask 05-24-10-210-089 A. Inspection. (1) Do a general visual inspection of the engine air intake and intake lip (zones 411 and 421). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting, wiring) are attached correctly.
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5. Close-up ________ Subtask 05-24-10-440-075 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3000-440-804). Subtask 05-24-10-865-101 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 05-24-10-410-091 C. Installation of the Panels. (Ref. Fig. 601/TASK 05-24-10-991-045, 602/TASK 05-24-10-991-046, 603/TASK 05-24-10-991-047, 604/TASK 05-24-10-991-048) (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels: FOR 4030EM1 411AL, 411AR FOR 4030EM2 421AL, 421AR (3) Close the fan cowl doors (Ref. TASK 71-13-00-410-802) FOR 4030EM1 415AL, 415BL, 416AR, 416BR FOR 4030EM2 425AL, 425BL, 426AR, 426BR Subtask 05-24-10-942-095 D. Close Access (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items. (2) Close the protective door of the AC/DC emergency power center 740VU.
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(3) Remove the warning notice in the cockpit. (4) Close the access door 811. (5) Remove the access platform(s). Subtask 05-24-10-862-066 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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TASK 05-24-10-200-810-A General Visual Inspection of the Fan Frame and Accessory Gear Box 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-412-02 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) 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 WARNING NOTICE
B. 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
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
3. __________ Job Set-up Subtask 05-24-10-861-068 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801).
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Subtask 05-24-10-941-097 B. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to start the engines. Subtask 05-24-10-865-102 C. Get access to the avionics compartment. Then 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 05-24-10-010-103 D. Get Access (1) Open the fan cowl doors (Ref. TASK 71-13-00-010-802). FOR 4030EM1 415AL, 415BL, 416AR, 416BR FOR 4030EM2 425AL, 425BL, 426AR, 426BR. (2) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the fan frame and accessory gear box (zones 412 and 422). Subtask 05-24-10-040-076 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3000-040-804).
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4. Procedure _________ Subtask 05-24-10-210-090 A. Inspection. (1) Do a general visual inspection of the fan frame and accessory gear box (zones 412 and 422). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting) are attached correctly. 5. Close-up ________ Subtask 05-24-10-440-076 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3000-440-804). Subtask 05-24-10-865-103 B. Get access to the avionics compartment. Then 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 05-24-10-410-092 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the fan cowl doors (Ref. TASK 71-13-00-410-802). FOR 4030EM1 415AL, 415BL, 416AR, 416BR FOR 4030EM2 425AL, 425BL, 426AR, 426BR
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Subtask 05-24-10-942-096 D. Close Access (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Close the protective door of the AC/DC emergency power center 740VU. Subtask 05-24-10-862-067 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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TASK 05-24-10-200-811-A General Visual Inspection of the Hot Section 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-413-02 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) warning notice adjustable access platform 2.30 m (7 ft. 7 in.) access platform 2.5 m (8 ft. 2 in.)
B. 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 78-30-00-860-801 78-30-00-860-802 05-24-10-991-045 05-24-10-991-046 05-24-10-991-047 05-24-10-991-048
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 Manually Deploy the Translating Cowl (5047EG1 5047EG2) Manually Stow the Translating Cowl (5047EG1 Or 5047EG2) Fig. 601 Fig. 602 Fig. 603 Fig. 604
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3. __________ Job Set-up Subtask 05-24-10-861-069 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 05-24-10-941-098 B. Safety Precautions (1) Make sure that the engine 1 (2) shutdown occurred not less than 5 minutes before you do the inspection. (2) Put a warning notice in the cockpit to tell persons not to start the engines. Subtask 05-24-10-010-104 C. Get Access to the Avionics Compartment. (1) Put an 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 05-24-10-865-104 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 05-24-10-040-077 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3000-040-804). Subtask 05-24-10-010-105 F. Get Access (Ref. Fig. 601/TASK 05-24-10-991-045, 602/TASK 05-24-10-991-046, 603/TASK 05-24-10-991-047, 604/TASK 05-24-10-991-048) (1) Put an adjustable access platform in position at the engine hot section (zones 413 and 423). (2) Open the fan cowl doors (Ref. TASK 71-13-00-010-802). FOR 4030EM1 415AL, 415BL, 416AR, 416BR FOR 4030EM2 425AL, 425BL, 426AR, 426BR (3) Manually deploy the thrust reverser (Ref. TASK 78-30-00-860-801). (4) Open the thrust reverser doors (Ref. TASK 78-30-00-010-801). FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR 4. Procedure _________ Subtask 05-24-10-210-091 A. Inspection. (1) Do a general visual inspection of the engine hot section (zones 413 and 423). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting) are attached correctly.
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5. Close-up ________ Subtask 05-24-10-440-077 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3000-440-804). Subtask 05-24-10-865-105 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 05-24-10-410-093 C. Close Access (Ref. Fig. 601/TASK 05-24-10-991-045, 602/TASK 05-24-10-991-046, 603/TASK 05-24-10-991-047, 604/TASK 05-24-10-991-048) (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the thrust reverser doors (Ref. TASK 78-30-00-410-801). FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR (3) Manually stow the thrust reverser (Ref. TASK 78-30-00-860-802). (4) Close the fan cowl doors (Ref. TASK 71-13-00-410-802). FOR 4030EM1 415AL, 415BL, 416AR, 416BR FOR 4030EM2 425AL, 425BL, 426AR, 426BR
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Subtask 05-24-10-942-097 D. Close Access (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Remove the warning notice in the cockpit. (4) Close the access door 811. (5) Remove the access platform(s). Subtask 05-24-10-862-068 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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TASK 05-24-10-200-812-A General Visual Inspection of the Exhaust Nozzle 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-414-02 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) warning notice adjustable access platform 2.30 m (7 ft. 7 in.) access platform 2.5 m (8 ft. 2 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 78-30-00-010-801 78-30-00-040-804 78-30-00-410-801 78-30-00-440-804 05-24-10-991-045 05-24-10-991-046 05-24-10-991-047 05-24-10-991-048
Energize the Ground Service Network De-energize the Ground Service Network 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. 601 Fig. 602 Fig. 603 Fig. 604
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3. __________ Job Set-up Subtask 05-24-10-861-070 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 05-24-10-941-099 B. Safety Precautions (1) Make sure that the engine 1 (2) shutdown occurred not less than 5 minutes before you do the inspection. (2) Put a warning notice in the cockpit to tell persons not to start the engines. Subtask 05-24-10-010-106 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 05-24-10-865-106 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 05-24-10-040-078 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3000-040-804). Subtask 05-24-10-010-107 F. Get Access (Ref. Fig. 601/TASK 05-24-10-991-045, 602/TASK 05-24-10-991-046, 603/TASK 05-24-10-991-047, 604/TASK 05-24-10-991-048) (1) Put an adjustable access platform in position at the exhaust nozzle (zones 410 and 420). (2) Open the thrust reverser doors (Ref. TASK 78-30-00-010-801). FOR 4030EM1 415BL, 416BR, 417AL, 418AR FOR 4030EM2 425BL, 426BR, 427AL, 428AR 4. Procedure _________ Subtask 05-24-10-210-092 A. Inspection. (1) Do a general visual inspection of the exhaust nozzle (zones 410 and 420). (2) Make sure that: - there is no damage, corrosion, leaks or cracks on all the parts of the components and the structure you can see, - all the installations are attached correctly. 5. Close-up ________ Subtask 05-24-10-440-078 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3000-440-804).
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Subtask 05-24-10-865-107 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 05-24-10-410-094 C. Closing of the Thrust Reverser Doors. (Ref. Fig. 601/TASK 05-24-10-991-045, 602/TASK 05-24-10-991-046, 603/TASK 05-24-10-991-047, 604/TASK 05-24-10-991-048) (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the thrust reverser doors (Ref. TASK 78-30-00-410-801). FOR 4030EM1 415BL, 416BR, 417AL, 418AR FOR 4030EM2 425BL, 426BR, 427AL, 428AR Subtask 05-24-10-942-098 D. Close Access (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Remove the warning notice in the cockpit. (4) Close the access door 811. (5) Remove the access platform(s). Subtask 05-24-10-862-069 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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TASK 05-24-10-200-813-A General Visual Inspection of the Fan Cowl 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-415-02 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) warning notice adjustable access platform 2.30 m (7 ft. 7 in.) access platform 2.5 m (8 ft. 2 in.)
B. 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 05-24-10-991-045 05-24-10-991-046 05-24-10-991-047 05-24-10-991-048
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. 601 Fig. 602 Fig. 603 Fig. 604
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3. __________ Job Set-up Subtask 05-24-10-861-071 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 05-24-10-941-100 B. Safety Precautions (1) Make sure that the engine 1 (2) shutdown occurred not less than 5 minutes before you do the inspection. (2) Put a warning notice in the cockpit to tell persons not to start the engines Subtask 05-24-10-010-108 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 05-24-10-865-108 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 05-24-10-040-079 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3000-040-804). Subtask 05-24-10-010-109 F. Get Access (Ref. Fig. 601/TASK 05-24-10-991-045, 602/TASK 05-24-10-991-046, 603/TASK 05-24-10-991-047, 604/TASK 05-24-10-991-048) (1) Put an adjustable access platform in position at the fan cowl (zones 410 and 420). (2) Open the fan cowl doors (Ref. TASK 71-13-00-010-802). FOR 4030EM1 415AL, 415BL, 416AR, 416BR FOR 4030EM2 425AL, 425BL, 426AR, 426BR (3) Remove the access panels FOR 4030EM1 415CL FOR 4030EM2 425CL 4. Procedure _________ Subtask 05-24-10-210-093 A. Inspection. (1) Do a general visual inspection of the fan cowls (zones 410 and 420). (2) Make sure that: - there is no damage, corrosion, leaks or cracks on all the parts of the components and the structure you can see, - all the installations (ducting) are attached correctly.
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5. Close-up ________ Subtask 05-24-10-440-079 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3000-440-804). Subtask 05-24-10-865-109 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 05-24-10-410-095 C. Installation of the Panels. (Ref. Fig. 601/TASK 05-24-10-991-045, 602/TASK 05-24-10-991-046, 603/TASK 05-24-10-991-047, 604/TASK 05-24-10-991-048) (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels: FOR 4030EM1 415CL FOR 4030EM2 425CL (3) Close the fan cowl doors (Ref. TASK 71-13-00-410-802). FOR 4030EM1 415AL, 415BL, 416AR, 416BR FOR 4030EM2 425AL, 425BL, 426AR, 426BR Subtask 05-24-10-942-099 D. Close Access (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items. (2) Close the protective door of the AC/DC emergency power center 740VU.
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(3) Remove the warning notice in the cockpit. (4) Close the access door 811. (5) Remove the access platform(s). Subtask 05-24-10-862-070 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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TASK 05-24-10-200-814-A General Visual Inspection of the Thrust Reverser 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-417-02 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) 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 71-13-00-010-803 71-13-00-410-803 78-30-00-040-804 78-30-00-440-804 78-30-00-860-801 78-30-00-860-802 78-36-00-010-802 78-36-00-410-802 05-24-10-991-045 05-24-10-991-046 05-24-10-991-047 05-24-10-991-048
Energize the Ground Service Network De-energize the Ground Service Network Opening of the Fan Cowl Doors Closing of the Fan Cowl Doors Deactivation of the Thrust Reverser for Maintenance Reactivation of the Thrust Reverser after Maintenance Manually Deploy the Translating Cowl (5047EG1 5047EG2) Manually Stow the Translating Cowl (5047EG1 Or 5047EG2) Opening of the Thrust Reverser Cowl Doors Closing of the Thrust Reverser Cowl Doors Fig. 601 Fig. 602 Fig. 603 Fig. 604
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3. __________ Job Set-up Subtask 05-24-10-861-072 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 05-24-10-941-101 B. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to start the engines. Subtask 05-24-10-865-110 C. Get access to the avionics compartment. Then 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 05-24-10-040-080 D. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3000-040-804).
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Subtask 05-24-10-010-110 E. Get Access (Ref. Fig. 601/TASK 05-24-10-991-045, 602/TASK 05-24-10-991-046, 603/TASK 05-24-10-991-047, 604/TASK 05-24-10-991-048) (1) Open the fan cowl doors (Ref. TASK 71-13-00-010-803) FOR 4030EM1 415BL, 416BR FOR 4030EM2 425BL, 426BR (2) Manually deploy the thrust reverser (Ref. TASK 78-30-00-860-801). (3) Open the thrust reverser doors (Ref. TASK 78-36-00-010-802). FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR (4) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the thrust reverser (zones 410 and 420). (5) Open or remove the access panels: FOR 4030EM1 417DL, 417EL, 417FL, 417GL, 417HL, 418BR, 418CR, 418FR, 418GR, 418HR, 418JR FOR 4030EM2 427DL, 427EL, 427FL, 427GL, 427HL, 428BR, 428CR, 428FR, 428GR, 428HR, 428JR 4. Procedure _________ Subtask 05-24-10-210-094 A. Inspection. (1) Do a general visual inspection of the thrust reverser (zones 410 and 420). (2) Make sure that: - there is no damage, corrosion, leaks or cracks on all the parts of the components and the structure you can see, - all the installations (ducting) are attached correctly.
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5. Close-up ________ Subtask 05-24-10-410-096 A. Installation of the Panels (Ref. Fig. 601/TASK 05-24-10-991-045, 602/TASK 05-24-10-991-046, 603/TASK 05-24-10-991-047, 604/TASK 05-24-10-991-048) (1) Close or install the access panels: FOR 4030EM1 417DL, 417EL, 417FL, 417GL, 417HL, 418BR, 418CR, 418FR, 418GR, 418HR, 418JR. FOR 4030EM2 427DL, 427EL, 427FL, 427GL, 427HL, 428BR, 428CR, 428FR, 428GR, 428HR, 428JR. (2) Close the thrust reverser doors (Ref. TASK 78-36-00-410-802). FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR (3) Manually stow the thrust reverser (Ref. TASK 78-30-00-860-802). (4) Close the fan cowl doors (Ref. TASK 71-13-00-410-803) FOR 4030EM1 415BL, 416BR FOR 4030EM2 425BL, 426BR Subtask 05-24-10-440-080 B. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3000-440-804). Subtask 05-24-10-865-111 C. Get access to the avionics compartment. Then 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 05-24-10-862-071 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 all the fixtures, tools, test and support equipment used during this procedure. (3) Make sure that the work area is clean and clear of tools and other items.
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ZONAL INSPECTION : ENGINE - INSPECTION/CHECK ____________________________________________ TASK 05-24-10-200-808-B General Visual Inspection of the Engine Air Intake and Intake Lip 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-411-03 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) warning notice adjustable access platform 2.30 m (7 ft. 7 in.) access platform 2.5 m (8 ft. 2 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 78-31-00-040-805 78-31-00-440-805 05-24-10-991-049 05-24-10-991-050 05-24-10-991-051 05-24-10-991-052
Energize the Ground Service Network De-energize the Ground Service Network Deactivation of the Thrust Reverser for Maintenance Activation of the Thrust Reverser after Maintenance Fig. 601 Fig. 602 Fig. 603 Fig. 604
3. __________ Job Set-up Subtask 05-24-10-861-073 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801).
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Subtask 05-24-10-941-102 B. Safety Precautions (1) Make sure that the engine 1 (2) shutdown occurred not less than 5 minutes before you do the inspection. (2) Put a warning notice in the cockpit to tell persons not to start the engines. Subtask 05-24-10-010-111 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 05-24-10-865-112 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 05-24-10-040-081 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3100-040-805).
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Subtask 05-24-10-010-112 F. Get Access (Ref. Fig. 601/TASK 05-24-10-991-049, 602/TASK 05-24-10-991-050, 603/TASK 05-24-10-991-051, 604/TASK 05-24-10-991-052) (1) Put an adjustable access platform in position at the engine air intake and intake lip (zones 411 and 421). (2) Remove the access panels FOR 4030EM1 411AR, 411AL FOR 4030EM2 421AR, 421AL 4. Procedure _________ Subtask 05-24-10-210-095 A. Inspection. (1) Do a general visual inspection of the engine air intake and intake lip (zones 411 and 421). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting) are attached correctly. 5. Close-up ________ Subtask 05-24-10-440-081 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3100-440-805). Subtask 05-24-10-865-113 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
EFF : 701-749, 05-24-10 Page 603 Config-3 Jul 01/04 SROS
Access Door/ Panels of the Engine 1 Nacelle - Right Side Figure 601/TASK 05-24-10-991-049 EFF : 701-749, 05-24-10 Page 604 Config-3 Jul 01/04 SROS
Access Door/ Panels of the Engine 1 Nacelle - Left Side Figure 602/TASK 05-24-10-991-050 EFF : 701-749, 05-24-10 Page 605 Config-3 Jul 01/04 SROS
Access Door/ Panels of the Engine 2 Nacelle - Right Side Figure 603/TASK 05-24-10-991-051 EFF : 701-749, 05-24-10 Page 606 Config-3 Jul 01/04 SROS
Access Door/ Panels of the Engine 2 Nacelle - Left Side Figure 604/TASK 05-24-10-991-052 EFF : 701-749, 05-24-10 Page 607 Config-3 Jul 01/04 SROS
Subtask 05-24-10-410-097 C. Installation of the Panels. (Ref. Fig. 601/TASK 05-24-10-991-049, 602/TASK 05-24-10-991-050, 603/TASK 05-24-10-991-051, 604/TASK 05-24-10-991-052) (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels FOR 4030EM1 411AR, 411AL FOR 4030EM2 421AR, 421AL Subtask 05-24-10-942-100 D. Close Access (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Remove the warning notice in the cockpit. (4) Close the access door 811. (5) Remove the access platform(s). Subtask 05-24-10-862-072 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
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TASK 05-24-10-200-809-B General Visual Inspection of the Engine Air Intake and Intake Lip 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-411-04 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 notice adjustable access platform 2.30 m (7 ft. 7 in.) access platform 2.5 m (8 ft. 2 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------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 05-24-10-991-049 05-24-10-991-050 05-24-10-991-051 05-24-10-991-052
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. 601 Fig. 602 Fig. 603 Fig. 604
3. __________ Job Set-up Subtask 05-24-10-861-074 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801).
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Subtask 05-24-10-941-103 B. Safety Precautions (1) Make sure that the engine 1 (2) shutdown occurred not less than 5 minutes before you do the inspection. (2) Put a warning notice in the cockpit to tell persons not to start the engines. Subtask 05-24-10-010-113 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 05-24-10-865-114 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 05-24-10-040-082 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3100-040-805).
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Subtask 05-24-10-010-114 F. Get Access (Ref. Fig. 601/TASK 05-24-10-991-049, 602/TASK 05-24-10-991-050, 603/TASK 05-24-10-991-051, 604/TASK 05-24-10-991-052) (1) Put an adjustable access platform in position at the engine air intake and intake lip (zones 411 and 421). (2) Open the fan cowl doors (Ref. TASK 71-13-00-010-805) FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR (3) Remove the access panels: FOR 4030EM1 411AL, 411AR FOR 4030EM2 421AL, 421AR 4. Procedure _________ Subtask 05-24-10-210-096 A. Inspection. (1) Do a general visual inspection of the engine air intake and intake lip (zones 411 and 421). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting, wiring) are attached correctly. 5. Close-up ________ Subtask 05-24-10-440-082 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3100-440-805).
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Subtask 05-24-10-865-115 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 05-24-10-410-098 C. Installation of the Panels. (Ref. Fig. 601/TASK 05-24-10-991-049, 602/TASK 05-24-10-991-050, 603/TASK 05-24-10-991-051, 604/TASK 05-24-10-991-052) (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels: FOR 4030EM1 411AL, 411AR FOR 4030EM2 421AL, 421AR (3) Close the fan cowl doors (Ref. TASK 71-13-00-410-805) FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR Subtask 05-24-10-942-101 D. Close Access (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Remove the warning notice in the cockpit. (4) Close the access door 811. (5) Remove the access platform(s).
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Subtask 05-24-10-862-073 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : 701-749, 05-24-10 Page 613 Config-3 Jul 01/04 SROS
TASK 05-24-10-200-810-B General Visual Inspection of the Fan Frame and Accessory Gear Box 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-412-02 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) 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------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
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
3. __________ Job Set-up Subtask 05-24-10-861-075 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 05-24-10-941-104 B. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to start the engines.
EFF : 701-749, 05-24-10 Page 614 Config-3 Jan 01/05 SROS
Subtask 05-24-10-865-116 C. Get access to the avionics compartment. Then 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 05-24-10-010-115 D. 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 an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the fan frame and accessory gear box (zones 412 and 422). Subtask 05-24-10-040-083 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3100-040-805).
EFF : 701-749, 05-24-10 Page 615 Config-3 Jul 01/04 SROS
4. Procedure _________ Subtask 05-24-10-210-097 A. Inspection. (1) Do a general visual inspection of the fan frame and accessory gear box (zones 412 and 422). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting) are attached correctly. 5. Close-up ________ Subtask 05-24-10-440-083 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3100-440-805). Subtask 05-24-10-865-117 B. Get access to the avionics compartment. Then 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 05-24-10-410-099 C. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the fan cowl doors (Ref. TASK 71-13-00-410-805). FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR
EFF : 701-749, 05-24-10 Page 616 Config-3 Jul 01/04 SROS
Subtask 05-24-10-942-102 D. Close Access (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Close the protective door of the AC/DC emergency power center 740VU. Subtask 05-24-10-862-074 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : 701-749, 05-24-10 Page 617 Config-3 Jul 01/04 SROS
TASK 05-24-10-200-811-B General Visual Inspection of the Hot Section 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-413-02 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) warning notice adjustable access platform 2.30 m (7 ft. 7 in.) access platform 2.5 m (8 ft. 2 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 71-13-00-010-805 71-13-00-410-805 78-30-00-010-803 78-30-00-410-803 78-31-00-040-805 78-31-00-440-805 05-24-10-991-049 05-24-10-991-050 05-24-10-991-051 05-24-10-991-052
Energize the Ground Service Network De-energize the Ground Service Network Open the Fan Cowl Doors Close the Fan Cowl Doors Open the Thrust Reverser Cowl Doors Close the Thrust Reverser Cowl Doors Deactivation of the Thrust Reverser for Maintenance Activation of the Thrust Reverser after Maintenance Fig. 601 Fig. 602 Fig. 603 Fig. 604
EFF : 701-749, 05-24-10 Page 618 Config-3 Jul 01/04 SROS
3. __________ Job Set-up Subtask 05-24-10-861-076 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 05-24-10-941-105 B. Safety Precautions (1) Make sure that the engine 1 (2) shutdown occurred not less than 5 minutes before you do the inspection. (2) Put a warning notice in the cockpit to tell persons not to start the engines. Subtask 05-24-10-010-116 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 05-24-10-865-118 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, 05-24-10 Page 619 Config-3 Jul 01/04 SROS
Subtask 05-24-10-040-084 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3100-040-805). Subtask 05-24-10-010-117 F. Get Access (Ref. Fig. 601/TASK 05-24-10-991-049, 602/TASK 05-24-10-991-050, 603/TASK 05-24-10-991-051, 604/TASK 05-24-10-991-052) (1) Put an adjustable access platform in position at the engine hot section (zones 413 and 423). (2) Open the fan cowl doors (Ref. TASK 71-13-00-010-805). FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR (3) Open the thrust reverser doors (Ref. TASK 78-30-00-010-803). FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR 4. Procedure _________ Subtask 05-24-10-210-098 A. Inspection. (1) Do a general visual inspection of the engine hot section (zones 413 and 423). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting) are attached correctly.
EFF : 701-749, 05-24-10 Page 620 Config-3 Jul 01/04 SROS
5. Close-up ________ Subtask 05-24-10-440-084 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3100-440-805). Subtask 05-24-10-865-119 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 05-24-10-410-100 C. Close Access (Ref. Fig. 601/TASK 05-24-10-991-049, 602/TASK 05-24-10-991-050, 603/TASK 05-24-10-991-051, 604/TASK 05-24-10-991-052) (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the thrust reverser doors (Ref. TASK 78-30-00-410-803). FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR (3) Close the fan cowl doors (Ref. TASK 71-13-00-410-805). FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR Subtask 05-24-10-942-103 D. Close Access (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items. (2) Close the protective door of the AC/DC emergency power center 740VU.
EFF : 701-749, 05-24-10 Page 621 Config-3 Jul 01/04 SROS
(3) Remove the warning notice in the cockpit. (4) Close the access door 811. (5) Remove the access platform(s). Subtask 05-24-10-862-075 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : 701-749, 05-24-10 Page 622 Config-3 Jul 01/04 SROS
TASK 05-24-10-200-812-B General Visual Inspection of the Exhaust Nozzle 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-414-02 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) warning notice adjustable access platform 2.30 m (7 ft. 7 in.) access platform 2.5 m (8 ft. 2 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 78-30-00-010-803 78-30-00-410-803 78-31-00-040-805 78-31-00-440-805 05-24-10-991-049 05-24-10-991-050 05-24-10-991-051 05-24-10-991-052
Energize the Ground Service Network De-energize the Ground Service Network Open the Thrust Reverser Cowl Doors Close the Thrust Reverser Cowl Doors Deactivation of the Thrust Reverser for Maintenance Activation of the Thrust Reverser after Maintenance Fig. 601 Fig. 602 Fig. 603 Fig. 604
3. __________ Job Set-up Subtask 05-24-10-861-077 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801).
EFF : 701-749, 05-24-10 Page 623 Config-3 Jul 01/04 SROS
Subtask 05-24-10-941-106 B. Safety Precautions (1) Make sure that the engine 1 (2) shutdown occurred not less than 5 minutes before you do the inspection. (2) Put a warning notice in the cockpit to tell persons not to start the engines. Subtask 05-24-10-010-118 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 05-24-10-865-120 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 05-24-10-040-085 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3100-040-805).
EFF : 701-749, 05-24-10 Page 624 Config-3 Jul 01/04 SROS
Subtask 05-24-10-010-119 F. Get Access (Ref. Fig. 601/TASK 05-24-10-991-049, 602/TASK 05-24-10-991-050, 603/TASK 05-24-10-991-051, 604/TASK 05-24-10-991-052) (1) Put an adjustable access platform in position at the exhaust nozzle (zones 410 and 420). (2) Open the thrust reverser doors (Ref. TASK 78-30-00-010-803). FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AR, 428AR 4. Procedure _________ Subtask 05-24-10-210-099 A. Inspection. (1) Do a general visual inspection of the exhaust nozzle (zones 410 and 420). (2) Make sure that: - there is no damage, corrosion, leaks or cracks on all the parts of the components and the structure you can see, - all the installations are attached correctly. 5. Close-up ________ Subtask 05-24-10-440-085 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3100-440-805). Subtask 05-24-10-865-121 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
EFF : 701-749, 05-24-10 Page 625 Config-3 Jul 01/04 SROS
Subtask 05-24-10-410-101 C. Closing of the Thrust Reverser Doors. (Ref. Fig. 601/TASK 05-24-10-991-049, 602/TASK 05-24-10-991-050, 603/TASK 05-24-10-991-051, 604/TASK 05-24-10-991-052) (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the thrust reverser doors (Ref. TASK 78-30-00-410-803). FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR Subtask 05-24-10-942-104 D. Close Access (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Remove the warning notice in the cockpit. (4) Close the access door 811. (5) Remove the access platform(s). Subtask 05-24-10-862-076 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : 701-749, 05-24-10 Page 626 Config-3 Jul 01/04 SROS
TASK 05-24-10-200-813-B General Visual Inspection of the Fan Cowl 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-415-02 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) warning notice adjustable access platform 2.30 m (7 ft. 7 in.) access platform 2.5 m (8 ft. 2 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------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 05-24-10-991-049 05-24-10-991-050 05-24-10-991-051 05-24-10-991-052
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. 601 Fig. 602 Fig. 603 Fig. 604
3. __________ Job Set-up Subtask 05-24-10-861-078 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801).
EFF : 701-749, 05-24-10 Page 627 Config-3 Jul 01/04 SROS
Subtask 05-24-10-941-107 B. Safety Precautions (1) Make sure that the engine 1 (2) shutdown occurred not less than 5 minutes before you do the inspection. (2) Put a warning notice in the cockpit to tell persons not to start the engines Subtask 05-24-10-010-120 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 05-24-10-865-122 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 05-24-10-040-086 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3100-040-805).
EFF : 701-749, 05-24-10 Page 628 Config-3 Jul 01/04 SROS
Subtask 05-24-10-010-121 F. Get Access (Ref. Fig. 601/TASK 05-24-10-991-049, 602/TASK 05-24-10-991-050, 603/TASK 05-24-10-991-051, 604/TASK 05-24-10-991-052) (1) Put an adjustable access platform in position at the fan cowl (zones 410 and 420). (2) Open the fan cowl doors (Ref. TASK 71-13-00-010-805). FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR (3) Remove the access panels FOR 4030EM1 415BL, 415CL, 416BR, 416CR FOR 4030EM2 425BL, 425CL, 426BR, 426CR 4. Procedure _________ Subtask 05-24-10-210-100 A. Inspection. (1) Do a general visual inspection of the fan cowls (zones 410 and 420). (2) Make sure that: - there is no damage, corrosion, leaks or cracks on all the parts of the components and the structure you can see, - all the installations (ducting) are attached correctly. 5. Close-up ________ Subtask 05-24-10-440-086 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3100-440-805).
EFF : 701-749, 05-24-10 Page 629 Config-3 Jul 01/04 SROS
Subtask 05-24-10-865-123 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 05-24-10-410-102 C. Installation of the Panels. (Ref. Fig. 601/TASK 05-24-10-991-049, 602/TASK 05-24-10-991-050, 603/TASK 05-24-10-991-051, 604/TASK 05-24-10-991-052) (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels: FOR 4030EM1 415BL, 415CL, 416BR, 416CR FOR 4030EM2 425BL, 425CL, 426BR, 426CR (3) Close the fan cowl doors (Ref. TASK 71-13-00-410-805). FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR Subtask 05-24-10-942-105 D. Close Access (1) Remove the ground support and maintenance equipment, the special and standard tools and all other items. (2) Close the protective door of the AC/DC emergency power center 740VU. (3) Remove the warning notice in the cockpit. (4) Close the access door 811. (5) Remove the access platform(s).
EFF : 701-749, 05-24-10 Page 630 Config-3 Jul 01/04 SROS
Subtask 05-24-10-862-077 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : 701-749, 05-24-10 Page 631 Config-3 Jul 01/04 SROS
TASK 05-24-10-200-814-B General Visual Inspection of the Thrust Reverser 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-417-02 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) 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R
24-42-00-861-801 24-42-00-862-801 71-13-00-010-805 71-13-00-410-805 78-30-00-010-803 78-30-00-410-803
Energize the Ground Service Network De-energize the Ground Service Network Open the Fan Cowl Doors Close the Fan Cowl Doors Open the Thrust Reverser Cowl Doors Close the Thrust Reverser Cowl Doors
78-31-00-040-805 78-31-00-440-805 05-24-10-991-049 05-24-10-991-050 05-24-10-991-051 05-24-10-991-052
Deactivation of the Thrust Reverser for Maintenance Activation of the Thrust Reverser after Maintenance Fig. 601 Fig. 602 Fig. 603 Fig. 604
R
R
EFF : 701-749, 05-24-10 Page 632 Config-3 Apr 01/05 SROS
3. __________ Job Set-up Subtask 05-24-10-865-124 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 05-24-10-941-108 B. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to start the engines. Subtask 05-24-10-865-125 C. Get access to the avionics compartment. Then 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 05-24-10-040-087 D. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3100-040-805).
EFF : 701-749, 05-24-10 Page 633 Config-3 Jul 01/04 SROS
Subtask 05-24-10-010-122 E. Get Access (Ref. Fig. 601/TASK 05-24-10-991-049, 602/TASK 05-24-10-991-050, 603/TASK 05-24-10-991-051, 604/TASK 05-24-10-991-052) R
(1) Open the fan cowl doors (Ref. TASK 71-13-00-010-805). FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR
R R R R
(2) Open the thrust reverser doors (Ref. TASK 78-30-00-010-803). FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR
R
(3) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the thrust reverser (zones 410 and 420).
R
(4) Open or remove the access panels: FOR 4030EM1 417BL, 417CL, 417DL, 417EL, 417FL, 417GL, 418BR, 418CR, 418DR, 418ER, 418FR, 418GR, 418HR, 418JR. FOR 4030EM2 427BL, 427CL, 427DL, 427EL, 427FL, 427GL, 428BR, 428CR, 428DR, 428ER, 428FR, 428GR, 428HR, 428JR 4. Procedure _________ Subtask 05-24-10-210-101 A. Inspection. (1) Do a general visual inspection of the thrust reverser (zones 410 and 420). (2) Make sure that: - there is no damage, corrosion, leaks or cracks on all the parts of the components and the structure you can see, - all the installations (ducting) are attached correctly.
EFF : 701-749, 05-24-10 Page 634 Config-3 Apr 01/05 SROS
5. Close-up ________ Subtask 05-24-10-410-103 A. Installation of the Panels (Ref. Fig. 601/TASK 05-24-10-991-049, 602/TASK 05-24-10-991-050, 603/TASK 05-24-10-991-051, 604/TASK 05-24-10-991-052) (1) Close or install the FOR 4030EM1 417BL, 417CL, 417DL, 418FR, 418GR, 418HR, FOR 4030EM2 427BL, 427CL, 427DL, 428FR, 428GR, 428HR,
access panels: 417EL, 417FL, 417GL, 418BR, 418CR, 418DR, 418ER, 418JR. 427EL, 427FL, 427GL, 428BR, 428CR, 428DR, 428ER, 428JR.
(2) Close the thrust reverser doors (Ref. TASK 78-30-00-410-803). FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR R R
(3) Close the fan cowl doors (Ref. TASK 71-13-00-410-805). FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR
R R
Subtask 05-24-10-440-087 B. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3100-440-805). Subtask 05-24-10-865-126 C. Get access to the avionics compartment. Then remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): - FOR 4030EM1 12KS1, 13KS1 - FOR 4030EM2 12KS2, 13KS2
EFF : 701-749, 05-24-10 Page 635 Config-3 Apr 01/05 SROS
Subtask 05-24-10-862-078 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 all the fixtures, tools, test and support equipment used during this procedure. (3) Make sure that the work area is clean and clear of tools and other items.
EFF : 701-749, 05-24-10 Page 636 Config-3 Jul 01/04 SROS
ZONAL INSPECTION : ENGINE PYLON - INSPECTION/CHECK __________________________________________________ TASK 05-24-50-200-806-A Zonal Inspection of the Pylon Leading Edge 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-451-02 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) warning notice access platform 2.5 m (8 ft. 2 in.) adjustable access platform 4.60 m (15 ft. 1 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 78-30-00-040-804 78-30-00-440-804 05-24-50-991-034 05-24-50-991-033
Energize the Ground Service Network De-energize the Ground Service Network Deactivation of the Thrust Reverser for Maintenance Reactivation of the Thrust Reverser after Maintenance Fig. 601 Fig. 602
3. __________ Job Set-up Subtask 05-24-50-861-065 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-50 Page 601 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
Subtask 05-24-50-941-080 B. Safety Precautions (1) Make sure that the engine 1(2) shutdown occurred no less than 5 minutes before you do the inspection. (2) Put a warning notice in the cockpit to tell persons not to start the engines. Subtask 05-24-50-010-086 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 05-24-50-865-090 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 05-24-50-040-070 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3000-040-804).
R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-50 Page 602 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
Subtask 05-24-50-010-087 F. Get Access (Ref. Fig. 601/TASK 05-24-50-991-034, 602/TASK 05-24-50-991-033) (1) Put an adjustable access platform in position at the pylon leading edge (zones 451, 461). (2) Remove the access panels: (a) For the pylon 1 451BL, 451CL, 451DL, 451BR, 451CR, 451DR (b) For the pylon 2 461BL, 461CL, 461DL, 461BR, 461CR, 461DR 4. Procedure _________ Subtask 05-24-50-210-080 A. Inspection. (1) Do a general visual inspection of the pylon leading edge (zones 451, 461). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-24-50-440-070 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3000-440-804). Subtask 05-24-50-865-091 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
R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-50 Page 603 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
Access Door/ Panels, Engine 1 Pylon Figure 601/TASK 05-24-50-991-034 R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-50 Page 604 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
Access Doors/ Panels, Engine 2 Pylon Figure 602/TASK 05-24-50-991-033 R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-50 Page 605 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
Subtask 05-24-50-410-080 C. Installation of the Panels. (Ref. Fig. 601/TASK 05-24-50-991-034, 602/TASK 05-24-50-991-033) (1) Make sure that the work area is clean and clear of tools and other items. (2) Close Access (3) Install the access panels: (a) For the pylon 2 461BL, 461CL, 461DL, 461BR, 461CR, 461DR (b) For the pylon 1 451BL, 451CL, 451DL, 451BR, 451CR, 451DR Subtask 05-24-50-942-085 D. Close Access (1) Close the protective door of the AC/DC emergency power-center 740VU. (2) Remove the warning notice in the cockpit. (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. Subtask 05-24-50-862-061 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-50 Page 606 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
TASK 05-24-50-200-802 Zonal Inspection of the Upper Forward of the Pylon 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-452-01 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) 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 54-52-11-000-809 54-52-11-400-809 78-30-00-040-804 78-30-00-440-804
Energize the Ground Service Network De-energize the Ground Service Network Removal of the Access Panels (RIBJ8 to RIB8A) Installation of the Access Panels (RIBJ8 to RIB8A) Deactivation of the Thrust Reverser for Maintenance Reactivation of the Thrust Reverser after Maintenance
3. __________ Job Set-up Subtask 05-24-50-861-066 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 05-24-50-941-081 B. Safety Precautions (1) Put a WARNING NOTICE to tell persons not to start the engines.
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Subtask 05-24-50-865-092 C. Get access to the avionics compartment. Then 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 05-24-50-040-071 D. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3000-040-804). Subtask 05-24-50-010-088 E. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the pylon leading edge (zones 452, 462). (2) Remove the access panels (Ref. TASK 54-52-11-000-809): (a) For the pylon 1 452AL, 452BL, 452CL 452BR, 452CR. (b) For the pylon 2 462AL, 462BL, 462CL 462BR, 462CR.
R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-50 Page 608 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
4. Procedure _________ Subtask 05-24-50-210-081 A. Inspection. (1) Do a general visual inspection of the upper forward section of the pylon (zones 452, 462). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-24-50-440-071 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3000-440-804). Subtask 05-24-50-865-093 B. Get access to the avionics compartment. Then 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 05-24-50-410-081 C. Installation of the Panels. CAUTION : WHEN YOU INSTALL THE ACCESS PANELS 452AL AND 462AL, MAKE SURE _______ THAT THE OVERPRESSURE DOOR IS CLOSED CORRECTLY. IF THE OVERPRESSURE DOOR IS NOT CLOSED, A FLOW OF HOT AIR CAN CAUSE A BLEED OVERHEAT DETECTION. (1) Make sure that the work area is clean and clear of tools and other items.
R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-50 Page 609 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
(2) Install the access panels (Ref. TASK 54-52-11-400-809): (a) For the pylon 2 462AL, 462BL, 462CL 462BR, 462CR . (b) For the pylon 1 452AL, 452BL, 452CL 452BR, 452CR. Subtask 05-24-50-862-062 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 all the fixtures, tools, test and support equipment used during this procedure.
R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-50 Page 610 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
TASK 05-24-50-200-808-A Zonal Inspection of the Lower of the Pylon 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-453-01 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 notice access platform 2.5 m (8 ft. 2 in.) adjustable access platform 4.60 m (15 ft. 1 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 78-30-00-440-804 78-31-00-040-802 05-24-50-991-034 05-24-50-991-033
Energize the Ground Service Network De-energize the Ground Service Network Reactivation of the Thrust Reverser after Maintenance Deactivation of the Thrust Reverser System for Maintenance Fig. 601 Fig. 602
3. __________ Job Set-up Subtask 05-24-50-861-067 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-50 Page 611 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
Subtask 05-24-50-941-082 B. Safety Precautions (1) Make sure that the engine 1(2) shutdown occurred no less than 5 minutes before you do the inspection. (2) Put a warning notice to tell persons not to start the engines. Subtask 05-24-50-010-089 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 05-24-50-865-094 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 05-24-50-040-072 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3100-040-802). Subtask 05-24-50-010-090 F. Get Access (Ref. Fig. 601/TASK 05-24-50-991-034, 602/TASK 05-24-50-991-033) (1) Put an adjustable access platform in position at the pylon leading edge (zones 453, 463).
R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-50 Page 612 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
(2) Remove the access panels: (a) For the pylon 1 453AL, 453BL, 453CL, 453AR, 453BR, 453CR (b) For the pylon 2 463AL, 463BL, 463CL, 463AR, 463BR, 463CR 4. Procedure _________ Subtask 05-24-50-210-082 A. Inspection. (1) Do a general visual inspection of the lower section of the pylon (zones 453, 463). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-24-50-440-072 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3000-440-804). Subtask 05-24-50-865-095 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
R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-50 Page 613 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
Subtask 05-24-50-410-082 C. Installation of the Panels. (Ref. Fig. 601/TASK 05-24-50-991-034, 602/TASK 05-24-50-991-033) CAUTION : MAKE SURE THAT THE SPRING RETAINER AT THE FWD EDGE OF THE PANEL _______ (453AL, 453AR, 463AL, 463AR) IS IN THE CORRECT POSITION BELOW THE ADJACENT PANEL. IF NOT, THE PANEL IS NOT CORRECTLY ATTACHED. (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels: (a) For the pylon 2 463AL, 463BL, 463CL, 463AR, 463BR, 463CR (b) For the pylon 1 453AL, 453BL, 453CL, 453AR, 453BR, 453CR Subtask 05-24-50-942-086 D. Close Access (1) Close the protective door of the AC/DC emergency power-center 740VU. (2) Remove the warning notice in the cockpit. (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. Subtask 05-24-50-862-063 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-50 Page 614 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
TASK 05-24-50-200-809-A Zonal Inspection of the Lower and Rear Pylon Fairings 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-454-05 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 notice access platform 2.5 m (8 ft. 2 in.) 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 78-30-00-040-804 78-30-00-440-804 05-24-50-991-034 05-24-50-991-033
Energize the Ground Service Network De-energize the Ground Service Network Deactivation of the Thrust Reverser for Maintenance Reactivation of the Thrust Reverser after Maintenance Fig. 601 Fig. 602
3. __________ Job Set-up Subtask 05-24-50-861-068 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801).
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Subtask 05-24-50-941-083 B. Safety Precautions (1) Make sure that the engine 1(2) shutdown occurred no less than 5 minutes before you do the inspection. (2) Put a warning notice to tell persons not to start the engines. Subtask 05-24-50-010-091 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 05-24-50-865-096 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 05-24-50-040-073 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3000-040-804). Subtask 05-24-50-010-092 F. Get Access (Ref. Fig. 601/TASK 05-24-50-991-034, 602/TASK 05-24-50-991-033) (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the pylon leading edge (zones 454, 464).
R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-50 Page 616 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
(2) Remove the access panels: (a) For the pylon 1 454BL, 454CL, 454KL, 454EL, 454ML, 454GL, 454HL, 454JL, 454BR, 454KR, 454NR, 454ER. (b) For the pylon 2 464BL, 464CL, 464KL, 464EL, 464ML, 464GL, 464HL, 464JL, 464BR, 464NR, 464KR 464ER. 4. Procedure _________ Subtask 05-24-50-210-083 A. Inspection. (1) Do a general visual inspection of the lower and rear pylon fairings (zones 454, 464). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-24-50-440-073 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3000-440-804). Subtask 05-24-50-865-097 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
R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-50 Page 617 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
Subtask 05-24-50-410-083 C. Installation of the Panels. (Ref. Fig. 601/TASK 05-24-50-991-034, 602/TASK 05-24-50-991-033) (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels: (a) For the pylon 2 464BL, 464CL, 464KL, 464EL, 464ML, 464GL, 464HL, 464JL, 464BR, 464NR, 464KR, 464ER. (b) For the pylon 1 454BL, 454CL, 454KL, 454EL, 454ML, 454GL, 454HL, 454JL, 454BR, 454NR, 454KR, 454ER. Subtask 05-24-50-942-087 D. Close Access (1) Close the protective door of the AC/DC emergency power-center 740VU. (2) Close the access door 811. Subtask 05-24-50-862-064 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801). (2) Remove all the fixtures, tools, test and support equipment used during this procedure.
R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-50 Page 618 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
TASK 05-24-50-200-810-A Zonal Inspection of the Lower and Rear Pylon Fairings 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-454-06 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 notice access platform 2.5 m (8 ft. 2 in.) 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 78-30-00-040-804 78-30-00-440-804 05-24-50-991-034 05-24-50-991-033
Energize the Ground Service Network De-energize the Ground Service Network Deactivation of the Thrust Reverser for Maintenance Reactivation of the Thrust Reverser after Maintenance Fig. 601 Fig. 602
3. __________ Job Set-up Subtask 05-24-50-861-069 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801).
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Subtask 05-24-50-941-084 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred no less than 5 minutes before you do the inspection. (2) Put a warning notice to tell persons not to start the engines. Subtask 05-24-50-010-093 C. Get Access to the Avionics Compartment (1) Put an 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 05-24-50-865-098 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 05-24-50-040-074 E. Deactivation of the Thrust Reverser (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3000-040-804). Subtask 05-24-50-010-094-A F. Get Access (Ref. Fig. 601/TASK 05-24-50-991-034, 602/TASK 05-24-50-991-033) (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the aft side of the engine pylon (zones 454 and 464).
R EFF : 001-049, 201-249, 251-252, 255-299, 05-24-50 Page 620 301-399, 401-449, 451-499, Config-2 Jul 01/05 SROS
(2) Remove the access panels:
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(a) For pylon 1: 454AL, 454BL, 454CL, 454KL, 454EL, 454ML, 454GL, 454HL, 454JL, 454BR, 454NR, 454KR, 454ER, 454MR, 454GR, 454HR.
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(b) For pylon 2: 464AL, 464BL, 464CL, 464KL, 464EL, 464ML, 464GL, 464HL, 464JL, 464BR, 464NR, 464KR, 464ER, 464MR, 464GR, 464HR. 4. Procedure _________ Subtask 05-24-50-210-084 A. Inspection (1) Do a general visual inspection of the lower and aft pylon fairings (zones 454 and 464). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-24-50-440-074 A. Reactivation of the Thrust Reverser (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3000-440-804). Subtask 05-24-50-865-099 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
EFF : 001-049, 201-249, 251-252, 255-299, 05-24-50 Page 621 301-399, 401-449, 451-499, Config-2 Jul 01/06 SROS
Subtask 05-24-50-410-084-A C. Installation of the Panels (Ref. Fig. 601/TASK 05-24-50-991-034, 602/TASK 05-24-50-991-033) (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels:
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(a) For pylon 2: 464AL, 464BL, 464CL, 464KL, 464EL, 464ML, 464GL, 464HL, 464JL, 464BR, 464NR, 464KR, 464ER, 464MR, 464GR, 464HR.
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(b) For pylon 1: 454AL, 454BL, 454CL, 454KL, 454EL, 454ML, 454GL, 454HL, 454JL, 454BR, 454NR, 454KR, 454ER, 454MR, 454GR, 454HR. Subtask 05-24-50-942-088 D. Close Access (1) Close the protective door of the AC/DC emergency power-center 740VU. (2) Close the access door 811. Subtask 05-24-50-862-065 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801). (2) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : 001-049, 201-249, 251-252, 255-299, 05-24-50 Page 622 301-399, 401-449, 451-499, Config-2 Jul 01/06 SROS
ZONAL INSPECTION : ENGINE PYLON - INSPECTION/CHECK __________________________________________________ TASK 05-24-50-200-806-B Zonal Inspection of the Pylon Leading Edge 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-451-02 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) warning notice access platform 2.5 m (8 ft. 2 in.) adjustable access platform 4.60 m (15 ft. 1 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 78-31-00-040-805 78-31-00-440-805 05-24-50-991-035 05-24-50-991-036
Energize the Ground Service Network De-energize the Ground Service Network Deactivation of the Thrust Reverser for Maintenance Activation of the Thrust Reverser after Maintenance Fig. 601 Fig. 602
3. __________ Job Set-up Subtask 05-24-50-861-071 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801).
EFF : 701-749, 05-24-50 Page 601 Config-3 Jul 01/04 SROS
Subtask 05-24-50-941-086 B. Safety Precautions (1) Make sure that the engine 1(2) shutdown occurred no less than 5 minutes before you do the inspection. (2) Put a warning notice in the cockpit to tell persons not to start the engines. Subtask 05-24-50-010-096 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 05-24-50-865-102 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 05-24-50-040-076 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3100-040-805).
EFF : 701-749, 05-24-50 Page 602 Config-3 Jul 01/04 SROS
Subtask 05-24-50-010-097 F. Get Access (Ref. Fig. 601/TASK 05-24-50-991-035, 602/TASK 05-24-50-991-036) (1) Put an adjustable access platform in position at the pylon leading edge (zones 451, 461). (2) Remove the access panels: (a) For the pylon 1 451AL, 451BL, 451CL, 451DL, 451EL, 451BR, 451CR, 451DR (b) For the pylon 2 461AL, 461BL, 461CL, 461DL, 461EL, 461BR, 461CR, 461DR 4. Procedure _________ Subtask 05-24-50-210-086 A. Inspection. (1) Do a general visual inspection of the pylon leading edge (zones 451, 461). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-24-50-440-076 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser serviceable (Ref. TASK 78-31-00440-805).
EFF : 701-749, 05-24-50 Page 603 Config-3 Jul 01/04 SROS
Access Door/ Panels, Engine 1 Pylon Figure 601/TASK 05-24-50-991-035 EFF : 701-749, 05-24-50 Page 604 Config-3 Jul 01/04 SROS
Access Door/ Panels, Engine 2 Pylon Figure 602/TASK 05-24-50-991-036 EFF : 701-749, 05-24-50 Page 605 Config-3 Jul 01/04 SROS
Subtask 05-24-50-865-103 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 05-24-50-410-086 C. Installation of the Panels. (Ref. Fig. 601/TASK 05-24-50-991-035, 602/TASK 05-24-50-991-036) (1) Make sure that the work area is clean and clear of tools and other items. (2) Close Access (3) Install the access panels: (a) For the pylon 2 461AL, 461BL, 461CL, 461DL, 461EL, 461BR, 461CR, 461DR (b) For the pylon 1 451AL, 451BL, 451CL, 451DL, 451EL, 451BR, 451CR, 451DR Subtask 05-24-50-942-089 D. Close Access (1) Close the protective door of the AC/DC emergency power-center 740VU. (2) Remove the warning notice in the cockpit. (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 : 701-749, 05-24-50 Page 606 Config-3 Jul 01/04 SROS
Subtask 05-24-50-862-067 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : 701-749, 05-24-50 Page 607 Config-3 Jul 01/04 SROS
TASK 05-24-50-200-802-A Zonal Inspection of the Upper Forward of the Pylon 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-452-01 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) 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 54-52-11-000-809 54-52-11-400-809 78-31-00-040-805 78-31-00-440-805
Energize the Ground Service Network De-energize the Ground Service Network Removal of the Access Panels (RIBJ8 to RIB8A) Installation of the Access Panels (RIBJ8 to RIB8A) Deactivation of the Thrust Reverser for Maintenance Activation of the Thrust Reverser after Maintenance
3. __________ Job Set-up Subtask 05-24-50-861-070 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 05-24-50-941-085 B. Safety Precautions (1) Put a WARNING NOTICE to tell persons not to start the engines.
EFF : 701-749, 05-24-50 Page 608 Config-3 Jan 01/05 SROS
Subtask 05-24-50-865-100 C. Get access to the avionics compartment. Then 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 05-24-50-040-075 D. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3100-040-805). Subtask 05-24-50-010-095 E. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the pylon leading edge (zones 452, 462). (2) Remove the access panels (Ref. TASK 54-52-11-000-809): (a) For the pylon 1 452AL, 452BL, 452CL 452BR, 452CR. (b) For the pylon 2 462AL, 462BL, 462CL 462BR, 462CR.
EFF : 701-749, 05-24-50 Page 609 Config-3 Jul 01/04 SROS
4. Procedure _________ Subtask 05-24-50-210-085 A. Inspection. (1) Do a general visual inspection of the upper forward section of the pylon (zones 452, 462). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-24-50-440-075 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3100-440-805). Subtask 05-24-50-865-101 B. Get access to the avionics compartment. Then 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 05-24-50-410-085 C. Installation of the Panels. CAUTION : WHEN YOU INSTALL THE ACCESS PANELS 452AL AND 462AL, MAKE SURE _______ THAT THE OVERPRESSURE DOOR IS CLOSED CORRECTLY. IF THE OVERPRESSURE DOOR IS NOT CLOSED, A FLOW OF HOT AIR CAN CAUSE A BLEED OVERHEAT DETECTION. (1) Make sure that the work area is clean and clear of tools and other items.
EFF : 701-749, 05-24-50 Page 610 Config-3 Jul 01/04 SROS
(2) Install the access panels (Ref. TASK 54-52-11-400-809): (a) For the pylon 2 462AL, 462BL, 462CL 462BR, 462CR . (b) For the pylon 1 452AL, 452BL, 452CL 452BR, 452CR. Subtask 05-24-50-862-066 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 all the fixtures, tools, test and support equipment used during this procedure.
EFF : 701-749, 05-24-50 Page 611 Config-3 Jul 01/04 SROS
TASK 05-24-50-200-808-B Zonal Inspection of the Lower of the Pylon 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-453-01 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 notice access platform 2.5 m (8 ft. 2 in.) adjustable access platform 4.60 m (15 ft. 1 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 78-31-00-040-805 78-31-00-440-805 05-24-50-991-035 05-24-50-991-036
Energize the Ground Service Network De-energize the Ground Service Network Deactivation of the Thrust Reverser for Maintenance Activation of the Thrust Reverser after Maintenance Fig. 601 Fig. 602
3. __________ Job Set-up Subtask 05-24-50-861-072 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801).
EFF : 701-749, 05-24-50 Page 612 Config-3 Jul 01/04 SROS
Subtask 05-24-50-941-087 B. Safety Precautions (1) Make sure that the engine 1(2) shutdown occurred no less than 5 minutes before you do the inspection. (2) Put a warning notice to tell persons not to start the engines. Subtask 05-24-50-010-098 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 05-24-50-865-104 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 05-24-50-040-077 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3100-040-805). Subtask 05-24-50-010-099 F. Get Access (Ref. Fig. 601/TASK 05-24-50-991-035, 602/TASK 05-24-50-991-036) (1) Put an adjustable access platform in position at the pylon leading edge (zones 453, 463).
EFF : 701-749, 05-24-50 Page 613 Config-3 Jul 01/04 SROS
(2) Remove the access panels: (a) For the pylon 1 453BL, 453CL, 453BR, 453CR (b) For the pylon 2 463BL, 463CL, 463BR, 463CR 4. Procedure _________ Subtask 05-24-50-210-087 A. Inspection. (1) Do a general visual inspection of the lower section of the pylon (zones 453, 463). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-24-50-440-077 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3100-440-805). Subtask 05-24-50-865-105 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 05-24-50-410-087 C. Installation of the Panels. (Ref. Fig. 601/TASK 05-24-50-991-035, 602/TASK 05-24-50-991-036) (1) Make sure that the work area is clean and clear of tools and other items.
EFF : 701-749, 05-24-50 Page 614 Config-3 Jul 01/04 SROS
(2) Install the access panels: (a) For the pylon 2 463BL, 463CL, 463BR, 463CR (b) For the pylon 1 453BL, 453CL, 463BR, 453CR Subtask 05-24-50-942-090 D. Close Access (1) Close the protective door of the AC/DC emergency power-center 740VU. (2) Remove the warning notice in the cockpit. (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. Subtask 05-24-50-862-068 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : 701-749, 05-24-50 Page 615 Config-3 Jul 01/04 SROS
TASK 05-24-50-200-809-B Zonal Inspection of the Lower and Rear Pylon Fairings 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-454-05 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 notice access platform 2.5 m (8 ft. 2 in.) 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 78-31-00-040-805 78-31-00-440-805 05-24-50-991-035 05-24-50-991-036
Energize the Ground Service Network De-energize the Ground Service Network Deactivation of the Thrust Reverser for Maintenance Activation of the Thrust Reverser after Maintenance Fig. 601 Fig. 602
3. __________ Job Set-up Subtask 05-24-50-861-073 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801).
EFF : 701-749, 05-24-50 Page 616 Config-3 Jul 01/04 SROS
Subtask 05-24-50-941-088 B. Safety Precautions (1) Make sure that the engine 1(2) shutdown occurred no less than 5 minutes before you do the inspection. (2) Put a warning notice to tell persons not to start the engines. Subtask 05-24-50-010-100 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 05-24-50-865-106 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 05-24-50-040-078 E. Deactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3100-040-805). Subtask 05-24-50-010-101 F. Get Access (Ref. Fig. 601/TASK 05-24-50-991-035, 602/TASK 05-24-50-991-036) (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the pylon leading edge (zones 454, 464).
EFF : 701-749, 05-24-50 Page 617 Config-3 Jul 01/04 SROS
(2) Remove the access panels: (a) For the pylon 1 454BL, 454CL, 454KL, 454EL, 454ML, 454GL, 454HL, 454JL, 454BR, 454NR, 454KR, 454ER. (b) For the pylon 2 464BL, 464CL, 464KL, 464EL, 464ML, 464GL, 464HL, 464JL, 464BR, 464NR, 464KR, 464ER. 4. Procedure _________ Subtask 05-24-50-210-088 A. Inspection. (1) Do a general visual inspection of the lower and rear pylon fairings (zones 454, 464). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-24-50-440-078 A. Reactivation of the Thrust Reverser. (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3100-440-805). Subtask 05-24-50-865-107 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
EFF : 701-749, 05-24-50 Page 618 Config-3 Jul 01/04 SROS
R R R
Subtask 05-24-50-410-088 C. Installation of the Panels. (Ref. Fig. 601/TASK 05-24-50-991-035, 602/TASK 05-24-50-991-036)
R R
(1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Install the access panels:
R R
(a) For the pylon 2 464BL, 464CL, 464KL, 464EL, 464ML, 464GL, 464HL, 464JL, 464BR, 464NR, 464KR, 464ER.
R R
(b) For the pylon 1 454BL, 454CL, 454KL, 454EL, 454ML, 454GL, 454HL, 454JL, 454BR, 454NR, 454KR, 454ER. Subtask 05-24-50-942-091
R
D. Close Access (1) Close the protective door of the AC/DC emergency power-center 740VU. (2) Close the access door 811. Subtask 05-24-50-862-069
R
E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801). (2) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : 701-749, 05-24-50 Page 619 Config-3 Jan 01/05 SROS
TASK 05-24-50-200-810-B Zonal Inspection of the Lower and Rear Pylon Fairings 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-454-06 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 notice access platform 2.5 m (8 ft. 2 in.) 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 78-31-00-040-805 78-31-00-440-805 05-24-50-991-035 05-24-50-991-036
Energize the Ground Service Network De-energize the Ground Service Network Deactivation of the Thrust Reverser for Maintenance Activation of the Thrust Reverser after Maintenance Fig. 601 Fig. 602
3. __________ Job Set-up Subtask 05-24-50-861-074 A. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801).
EFF : 701-749, 05-24-50 Page 620 Config-3 Jul 01/04 SROS
Subtask 05-24-50-941-089 B. Safety Precautions (1) Make sure that the engine 1, (2) shutdown occurred no less than 5 minutes before you do the inspection. (2) Put a warning notice to tell persons not to start the engines. Subtask 05-24-50-010-102 R
C. Get Access to the Avionics Compartment
R
(1) Put an 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 05-24-50-865-108 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 05-24-50-040-079
R
E. Deactivation of the Thrust Reverser (1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-3100-040-805).
R R R
Subtask 05-24-50-010-103-A F. Get Access (Ref. Fig. 601/TASK 05-24-50-991-035, 602/TASK 05-24-50-991-036)
R R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the aft side of the engine pylon (zones 454 and 464).
EFF : 701-749, 05-24-50 Page 621 Config-3 Apr 01/05 SROS
R
(2) Remove the access panels:
R R R
(a) For pylon 1: 454AL, 454BL, 454CL, 454KL, 454EL, 454ML, 454GL, 454HL, 454JL, 454BR, 454NR, 454KR, 454ER, 454MR, 454GR, 454HR.
R R R
(b) For pylon 2: 464AL, 464BL, 464CL, 464KL, 464EL, 464ML, 464GL, 464HL, 464JL, 464BR, 464NR, 464KR, 464ER, 464MR, 464GR, 464HR. 4. Procedure _________ Subtask 05-24-50-210-089
R
A. Inspection (1) Do a general visual inspection of the lower and aft pylon fairings (zones 454 and 464). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see, - all the installations (ducting, piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-24-50-440-079
R
A. Reactivation of the Thrust Reverser (1) Make sure that the thrust reverser is serviceable (Ref. TASK 78-3100-440-805). Subtask 05-24-50-865-109 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
EFF : 701-749, 05-24-50 Page 622 Config-3 Apr 01/05 SROS
R R R
Subtask 05-24-50-410-089-A C. Installation of the Panels (Ref. Fig. 601/TASK 05-24-50-991-035, 602/TASK 05-24-50-991-036)
R R
(1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Install the access panels:
R R R
(a) For pylon 2: 464AL, 464BL, 464CL, 464KL, 464EL, 464ML, 464GL, 464HL, 464JL, 464BR, 464NR, 464KR, 464ER, 464MR, 464GR, 464HR.
R R R
(b) For pylon 1: 454AL, 454BL, 454CL, 454KL, 454EL, 454ML, 454GL, 454HL, 454JL, 454BR, 454NR, 454KR, 454ER, 454MR, 454GR, 454HR. Subtask 05-24-50-942-092 D. Close Access (1) Close the protective door of the AC/DC emergency power-center 740VU. (2) Close the access door 811. Subtask 05-24-50-862-070 E. Put the Aircraft back to its Initial Configuration (1) De-energize the ground service network (Ref. TASK 24-42-00-862-801). (2) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : 701-749, 05-24-50 Page 623 Config-3 Apr 01/05 SROS
ZONAL INSPECTION : WING - INSPECTION/CHECK __________________________________________ TASK 05-25-00-200-801 Zonal Inspection as far as visible from the Ground of the Left and Right Wings (zone 500 and 600). 1. __________________ Reason for the Job R
NOTE : This task can contribute to fuel savings. ____ 2. ______________________ Job Set-up Information Not Applicable 3. __________ Job Set-up Subtask 05-25-00-869-050 A. Not applicable. 4. Procedure _________ Subtask 05-25-00-210-050 A. Do a general visual inspection of the left and right wing (zone 500 and 600) from the ground.
EFF : ALL 05-25-00 SROS
Page 601 Jan 01/07
TASK 05-25-00-200-802 Zonal Inspection of Wing Lower Surface Including Slats and Flaps 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: ZL-500-01 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
1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------27-50-00-866-801 27-50-00-866-801 27-50-00-866-802 27-50-00-866-802
Extension of the Flaps/Slats on the Ground Extension of the Flaps/Slats on the Ground (RR-Engines) Retraction of the Flaps/Slats on the Ground Retraction of the Flaps/Slats on the Ground (RR-Engines)
EFF : ALL 05-25-00 SROS
Page 602 Jan 01/07
3. __________ Job Set-up **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-25-00-866-050 A. Aircraft Maintenance Configuration R
(1) Fully extend the flaps/slats (Ref. TASK 27-50-00-866-801). **ON A/C 701-749, Subtask 05-25-00-866-050-A A. Aircraft Maintenance Configuration (1) Fully extend the flaps/slats (Ref. TASK 27-50-00-866-801). **ON A/C ALL Subtask 05-25-00-941-051 B. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-25-00-010-050 C. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the left and right lower wing surface. 4. Procedure _________ Subtask 05-25-00-210-051 A. Do a general visual inspection of the wing lower surface. This includes the slats and flaps (Zones 500 and 600). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see.
EFF : ALL 05-25-00 SROS
Page 603 Jan 01/07
5. Close-up ________ R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-25-00-942-050 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) Retract the flaps/slats (Ref. TASK 27-50-00-866-802). (3) Remove all the fixtures, tools, test and support equipment used during this procedure. **ON A/C 701-749, Subtask 05-25-00-942-050-A 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) Retract the flaps/slats (Ref. TASK 27-50-00-866-802). (3) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-25-00 SROS
Page 604 Jul 01/05
**ON A/C ALL TASK 05-25-00-200-803 Zonal Inspection of Wing Upper Surface (Including Slats, Flaps and Spoilers) 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: ZL-500-02 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
1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------27-50-00-866-801 27-50-00-866-801 27-50-00-866-802 27-50-00-866-802 27-60-00-866-801 27-60-00-866-802
Extension of the Flaps/Slats on the Ground Extension of the Flaps/Slats on the Ground (RR-Engines) Retraction of the Flaps/Slats on the Ground Retraction of the Flaps/Slats on the Ground (RR-Engines) Extension of the Spoilers for Maintenance Retraction of the Spoilers after Maintenance
EFF : ALL 05-25-00 SROS
Page 605 Jan 01/07
3. __________ Job Set-up **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-25-00-866-052 A. Aircraft Maintenance Configuration (1) Extend the spoilers (Ref. TASK 27-60-00-866-801). (2) Fully extend the flaps/slats (Ref. TASK 27-50-00-866-801). **ON A/C 701-749, Subtask 05-25-00-866-052-A A. Aircraft Maintenance Configuration R
(1) Extend the spoilers (Ref. TASK 27-60-00-866-801). (2) Fully extend the flaps/slats (Ref. TASK 27-50-00-866-801). **ON A/C ALL Subtask 05-25-00-941-052 B. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-25-00-010-051 C. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the left and right upper wing surface.
EFF : ALL 05-25-00 SROS
Page 606 Jan 01/07
4. Procedure _________ Subtask 05-25-00-210-052 A. Do a general visual inspection of the wing upper surface. This includes the slats, flaps and spoilers (zones 500 and 600). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-25-00-942-051 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) Retract the flaps/slats (Ref. TASK 27-50-00-866-802). (3) Retract the spoilers (Ref. TASK 27-60-00-866-802). (4) Remove all the fixtures, tools, test and support equipment used during this procedure. **ON A/C 701-749, Subtask 05-25-00-942-051-A 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) Retract the flaps/slats (Ref. TASK 27-50-00-866-802). (3) Retract the spoilers (Ref. TASK 27-60-00-866-802). (4) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-25-00 SROS
Page 607 Jul 01/05
ZONAL INSPECTION : WING FIXED LEADING EDGE - INSPECTION/CHECK _____________________________________________________________ TASK 05-25-20-200-801 R R
Zonal Inspection of Inboard Fixed Leading Edge Structure 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: ZL-521-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------27-80-00-866-801 27-80-00-866-802
Extension of the Slats on the Ground Retraction of the Slats on the Ground
R 3. __________ Job Set-up Subtask 05-25-20-866-050 A. Aircraft Maintenance Configuration R R
(1) Fully extend the slats (Ref. TASK 27-80-00-866-801).
EFF : ALL 05-25-20 SROS
Page 601 Jan 01/04
Subtask 05-25-20-941-050 B. Safety Precautions R R R
(1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. 4. Procedure _________ Subtask 05-25-20-210-050
R
A. Do a general visual inspection of the inboard fixed leading-edge structure (Zones 521 and 621). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, wiring) are attached correctly. 5. Close-up ________
R Subtask 05-25-20-866-051 R R
A. Put the Aircraft back to its Initial Configuration
R
(1) Retract the slats (Ref. TASK 27-80-00-866-802). Subtask 05-25-20-942-050
R R R
B. Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-25-20 SROS
Page 602 Jan 01/04
TASK 05-25-20-200-802 R
Zonal Inspection of Center Fixed Leading Edge Structure 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: ZL-522-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R
No specific No specific
1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R
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
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
3. __________ Job Set-up Subtask 05-25-20-866-052 A. Aircraft Maintenance Configuration (1) Fully extend the slats (Ref. TASK 27-80-00-866-801).
EFF : ALL 05-25-20 SROS
Page 603 Jan 01/04
Subtask 05-25-20-941-051 B. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-25-20-010-051-B C. Get Access (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the slats (Zones 522 and 622). (2) Remove the access panels: R
(a) For the left side: 522BB, 522CB, 522EB, 522HB, 522JB, 522LB, 522NB, 522TB, 522UB, 522AT (Ref. TASK 57-42-37-000-801), 522AB (Ref. TASK 57-41-37-000-801).
R
(b) For the right side: 622BB, 622CB, 622EB, 622HB, 622JB, 622LB, 622NB, 622TB, 622UB, 622AT, (Ref. TASK 57-42-37-000-801), 622AB (Ref. TASK 57-41-37-000-801). 4. Procedure _________ Subtask 05-25-20-210-051 A. Do a general visual inspection of the center fixed leading-edge structure (Zones 522 and 622). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, wiring) are attached correctly.
EFF : ALL 05-25-20 SROS
Page 604 Jan 01/07
5. Close-up ________ Subtask 05-25-20-410-051-B A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the access panels: R
(a) For the left side: 522BB, 522CB, 522EB, 522HB, 522JB, 522LB, 522NB, 522TB, 522UB, 522AT (Ref. TASK 57-42-37-400-801), 522AB (Ref. TASK 57-41-37-400-801).
R
(b) For the right side: 622BB, 622CB, 622EB, 622HB, 622JB, 622LB, 622NB, 622TB, 622UB, 622AT, (Ref. TASK 57-42-37-400-801), 622AB (Ref. TASK 57-41-37-400-801). Subtask 05-25-20-866-053 B. 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) Retract the slats (Ref. TASK 27-80-00-866-802). Subtask 05-25-20-942-051 C. Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-25-20 SROS
Page 605 Jan 01/07
TASK 05-25-20-200-803 Zonal Inspection of Outer Fixed Leading Edge Structure 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: ZL-523-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------R
No specific No specific
1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R
27-80-00-866-801 27-80-00-866-802 57-42-37-000-801 57-42-37-400-801
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
3. __________ Job Set-up Subtask 05-25-20-866-054 A. Aircraft Maintenance Configuration R
(1) Fully extend the slats (Ref. TASK 27-80-00-866-801).
EFF : ALL 05-25-20 SROS
Page 606 Apr 01/04
Subtask 05-25-20-941-052 B. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-25-20-010-052-A C. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the slats (Zones 523 and 623). (2) Remove the access panels: R R
(a) For the left side: 523CB, 523EB, 523GB, 523JB, 523LB, 523NB (Ref. TASK 57-42-37-000-801).
R R
(b) For the right side: 623CB, 623EB, 623GB, 623JB, 623LB, 623NB (Ref. TASK 57-42-37-000-801). 4. Procedure _________ Subtask 05-25-20-210-052 A. Do a general visual inspection of the outer fixed leading edge structure (Zones 523 and 623). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (ducting, wiring) are attached correctly. 5. Close-up ________ Subtask 05-25-20-410-052-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:
R R
(a) For the left side: 523CB, 523EB, 523GB, 523JB, 523LB, 523NB (Ref. TASK 57-42-37-400-801).
EFF : ALL 05-25-20 SROS
Page 607 Apr 01/05
R R
(b) For the right side: 623CB, 623EB, 623GB, 623JB, 623LB, 623NB (Ref. TASK 57-42-37-400-801). Subtask 05-25-20-942-052 B. Put the Aircraft back to its Initial Configuration (1) Retract the slats (Ref. TASK 27-80-00-866-802). (2) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-25-20 SROS
Page 608 Apr 01/05
ZONAL INSPECTION : WING FLAP TRACK FAIRINGS AND WING TIP - INSPECTION/CHECK ___________________________________________________________________________ TASK 05-25-30-200-801 Zonal Inspection of Flap Tracks and Flap Track Fairings (Including RAT Attachment Points, as far as visible) 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: ZL-531-01 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
1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------27-50-00-866-801 27-50-00-866-802 57-56-11-000-801 57-56-11-000-802 57-56-11-000-803 57-56-11-000-804 57-56-11-400-801 57-56-11-400-802 57-56-11-400-803
Extension of the Flaps on the Ground Retraction of the Flaps on the Ground Removal of the Movable Flap Track Fairing No. 2 Removal of the Movable Flap Track Fairing No. 3 Removal of the Movable Flap Track Fairing No. 4 Removal of the Movable Flap Track Fairing No. 5 Installation of Movable Flap Track Fairing No. 2 Installation of Movable Flap Track Fairing No. 3 Installation of the Movable Flap Track Fairing No. 4
EFF : ALL 05-25-30 SROS
Page 601 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------57-56-11-400-804
Installation of the Movable Flap Track Fairing No. 5
3. __________ Job Set-up Subtask 05-25-30-866-050 A. Aircraft Maintenance Configuration R
(1) Fully extend the flaps (Ref. TASK 27-50-00-866-801). Subtask 05-25-30-941-050 B. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-25-30-010-050 C. Get Access
R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at zone 530(630). (2) Remove the flap track fairings 531CB, 532CB, 533CB, 534CB, 631CB, 632CB, 633CB, 634CB (Ref. TASK 57-56-11-000-801), (Ref. TASK 57-5611-000-802), (Ref. TASK 57-56-11-000-803), (Ref. TASK 57-56-11-000804). 4. Procedure _________ Subtask 05-25-30-210-050
R
A. Do a general visual inspection of all the flap tracks and flap track fairings. This includes the RAT attachment points, as far as you can see. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations are attached correctly.
EFF : ALL 05-25-30 SROS
Page 602 Jan 01/07
5. Close-up ________ Subtask 05-25-30-410-050 A. Close Access (1) Install the flap track fairings 531CB, 532CB, 533CB, 534CB, 631CB, 632CB, 633CB, 634CB (Ref. TASK 57-56-11-400-801), (Ref. TASK 57-5611-400-802), (Ref. TASK 57-56-11-400-803), (Ref. TASK 57-56-11-400804). Subtask 05-25-30-866-051 B. Put the Aircraft back to its Initial Configuration (1) Fully retract the flaps (Ref. TASK 27-50-00-866-802). Subtask 05-25-30-942-051 C. Remove all the fixtures, tools, test and support equipment used during this procedure. (1) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-25-30 R SROS
Page 603 Jan 01/07
TASK 05-25-30-200-802 Zonal inspection of Flap Tracks and Flap Track Fairings 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: ZL-531-02 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
1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------27-50-00-866-801 27-50-00-866-802 57-56-11-000-801 57-56-11-000-802 57-56-11-000-803 57-56-11-000-804 57-56-11-000-805 57-56-11-000-806 57-56-11-400-801
Extension of the Flaps on the Ground Retraction of the Flaps on the Ground Removal of the Movable Flap Track Fairing No. 2 Removal of the Movable Flap Track Fairing No. 3 Removal of the Movable Flap Track Fairing No. 4 Removal of the Movable Flap Track Fairing No. 5 Removal of the Fixed Flap Track Fairings Nos. 2 thru 5 (without Fixed Flap Track Fairing No 4 on the Right Side) Removal of the Fixed Flap Track Fairing No. 4 on the Right Side Installation of Movable Flap Track Fairing No. 2
EFF : ALL 05-25-30 SROS
Page 604 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------57-56-11-400-802 57-56-11-400-803 57-56-11-400-804 57-56-11-400-805 57-56-11-400-806
Installation of Installation of Installation of Installation of thru 5 (without Right Side) Installation of the Right Side
Movable Flap Track Fairing No. 3 the Movable Flap Track Fairing No. 4 the Movable Flap Track Fairing No. 5 the Fixed Flap Track Fairings Nos 2 Fixed Flap Track Fairing No. 4 on the the Fixed Flap Track Fairing No. 4 on
3. __________ Job Set-up Subtask 05-25-30-866-052 A. Aircraft Maintenance Configuration R
(1) Fully extend the flaps (Ref. TASK 27-50-00-866-801). Subtask 05-25-30-941-051 B. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-25-30-010-051 C. Get Access (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the flap track fairings. (2) Remove the movable flap track fairings 531CB, 532CB, 533CB, 534CB, 631CB, 632CB, 633CB, 634CB (Ref. TASK 57-56-11-000-801), (Ref. TASK 57-56-11-000-802), (Ref. TASK 57-56-11-000-803), (Ref. TASK 57-56-11000-804). (3) Remove the fixed flap track fairings 531AB, 532AB, 533AB, 534AB, 631AB, 632AB, 633AB, 634AB (Ref. TASK 57-56-11-000-805), (Ref. TASK 57-56-11-000-806).
EFF : ALL 05-25-30 SROS
Page 605 Jan 01/07
4. Procedure _________ Subtask 05-25-30-210-051 A. Do a general visual inspection of the flap tracks and the flap track fairings. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations are attached correctly. 5. Close-up ________ Subtask 05-25-30-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the fixed flap track fairings 531AB, 532AB, 533AB, 534AB, 631AB, 632AB, 633AB, 634AB, (Ref. TASK 57-56-11-400-805), (Ref. TASK 57-56-11-400-806). (3) Install the movable flap track fairings 531CB, 532CB, 533CB, 534CB, 631CB, 632CB, 633CB, 634CB (Ref. TASK 57-56-11-400-801), (Ref. TASK 57-56-11-400-802), (Ref. TASK 57-56-11-400-803), (Ref. TASK 57-56-11400-804). Subtask 05-25-30-866-053 B. Put the Aircraft back to its Initial Configuration (1) Fully retract the flaps (Ref. TASK 27-50-00-866-802). Subtask 05-25-30-942-052 C. Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-25-30 R SROS
Page 606 Jan 01/07
TASK 05-25-30-200-809 Zonal Inspection of Wing Tip. 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: ZL-535-01 R
NOTE : This task can contribute to fuel saving. ____ 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------57-37-11-000-801 57-37-11-400-801
Removal of the Winglet Access Panels Installation of the Winglet Access Panels
EFF : ALL 05-25-30 SROS
Page 607 Jan 01/07
3. __________ Job Set-up Subtask 05-25-30-010-058 A. Get Access (1) Put an ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE in position at the wing tip (zones 535 and 635). (2) For the left side: Remove the access panels 535AB, 535BB (Ref. TASK 57-37-11-000-801).
R
(3) For the right side: Remove the access panels 635AB, 635BB (Ref. TASK 57-37-11-000-801). 4. Procedure _________ Subtask 05-25-30-210-058 A. Do a general visual inspection of the wing tip (zones 535 and 635). Make sure that: - there is no damage (corrosion or cracks) on all the parts of the components and the structure you can see - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-25-30-410-058 A. Close Access (1) For the left side Install the access panels 535AB, 535BB (Ref. TASK 57-37-11-400-801). (2) For the right side Install the access panels 635AB, 635BB (Ref. TASK 57-37-11-400-801). Subtask 05-25-30-942-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-25-30 SROS
Page 608 Jan 01/07
ZONAL INSPECTION : WING FUEL TANK - INSPECTION/CHECK ____________________________________________________ TASK 05-25-40-200-801 R
Zonal Inspection of Inner Fuel Tank. 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 : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND DAMAGE. _______ 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 Refer to the MPD TASK: ZL-541-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
safety barriers warning notices 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
EFF : ALL 05-25-40 SROS
Page 601 Jul 01/04
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-11-28-650-803 28-00-00-610-801 28-10-00-910-802 28-25-00-650-801 57-27-11-000-801 57-27-11-400-801
Pressure Refuel with Automatic Control from the Panel 990VU Fuel Safety Procedures Access to Fuel Tanks and Work Areas Pressure Defuel Procedure Removal of the Underwing Tank Access-Panels Installation of the Underwing Tank Access-Panels
3. __________ Job Set-up Subtask 05-25-40-650-050 R
A. Defuel the tanks (Ref. TASK 28-25-00-650-801). Subtask 05-25-40-941-053 B. Safety Precautions (1) Put the safety barriers in position. (2) Put the warning notices in position: - to tell persons not to operate the fuel system - to tell persons not to refuel the aircraft - to tell persons not to operate the flight controls. Subtask 05-25-40-010-050 C. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the inner fuel tank (zones 541 and 641). (2) Remove the access panels: (a) For the left side: 541AB, 541BB, 541BZ, 541CB, 541CZ (Ref. TASK 57-27-11-000-801). (b) For the right side: 641AB, 641BB, 641BZ, 641CB, 641CZ (Ref. TASK 57-27-11-000-801).
EFF : ALL 05-25-40 SROS
Page 602 Jul 01/04
Subtask 05-25-40-941-050 D. Safety Precautions (1) Obey the fuel safety procedures (Ref. TASK 28-00-00-610-801). (2) Get access to the fuel tank (Ref. TASK 28-10-00-910-802). 4. Procedure _________ Subtask 05-25-40-210-050 R R
A. Do a general visual inspection of the inner fuel tank between rib 1 and rib 7 (zones 541 and 641). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - All the installations (ducting, wiring) are attached correctly. 5. Close-up ________ Subtask 05-25-40-410-050 A. Close Access
R R
(1) Install the access panels:
R R
(a) For the left side: 541AB, 541BB, 541BZ, 541CB, 541CZ (Ref. TASK 57-27-11-400-801).
R R
(b) For the right side: 641AB, 641BB, 641BZ, 641CB, 641CZ (Ref. TASK 57-27-11-400-801). Subtask 05-25-40-650-051 B. Refuel the tanks (Ref. TASK 12-11-28-650-803) Subtask 05-25-40-942-051
R R
C. Put the Aircraft back to its Initial Configuration
R R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-25-40 SROS
Page 603 Jan 01/04
R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-25-40 SROS
Page 604 Jan 01/04
TASK 05-25-40-200-802 R R
Zonal Inspection of Inner Fuel Tank (Rib 1 to Rib 23). 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 : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND DAMAGE. _______ 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 Refer to the MPD TASK: ZL-541-02 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific No specific No specific
safety barriers warning notices 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
EFF : ALL 05-25-40 SROS
Page 605 Jan 01/04
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-11-28-650-803 28-00-00-610-801 28-10-00-910-802 28-25-00-650-801 57-27-11-000-801 57-27-11-400-801
Pressure Refuel with Automatic Control from the Panel 990VU Fuel Safety Procedures Access to Fuel Tanks and Work Areas Pressure Defuel Procedure Removal of the Underwing Tank Access-Panels Installation of the Underwing Tank Access-Panels
3. __________ Job Set-up Subtask 05-25-40-650-052 R
A. Defuel the tanks (Ref. TASK 28-25-00-650-801) Subtask 05-25-40-941-054 B. Safety Precautions (1) Put the safety barriers in position. (2) Put the warning notices in position: - to tell persons not to operate the fuel system - to tell persons not to refuel the aircraft - to tell persons not to operate the flight controls.
R R
Subtask 05-25-40-010-051 C. Get Access R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the inner fuel tank (zones 541 and 641). (2) Remove the access panels:
R R
(a) For the left side: 541AB, 541BB, 541CB, 541DB, 541EB, 541FB, 541GB, 541HB, 541JB, 541KB, 541LB, 541MB, 541NB, 541PB, 541QB, 541RB, 541SB, 541AZ, 541BZ, 541CZ, 541DZ, 541EZ, 541FZ, 541GZ (Ref. TASK 57-27-11-000-801).
R
EFF : ALL 05-25-40 SROS
Page 606 Jan 01/04
R R
(b) For the right side: 641AB, 641BB, 641CB, 641DB, 641EB, 641FB, 641GB, 641HB, 641JB, 641KB, 641LB, 641MB, 641NB, 641PB, 641QB, 641RB, 641SB, 641AZ, 641BZ, 641CZ, 641DZ, 641EZ, 641FZ, 641GZ (Ref. TASK 57-27-11-000-801).
R
Subtask 05-25-40-941-051 D. Safety Precautions (1) Obey the fuel safety procedures (Ref. TASK 28-00-00-610-801). (2) Get access to the fuel tank (Ref. TASK 28-10-00-910-802). 4. Procedure _________ Subtask 05-25-40-210-051 R R
A. Do a general visual inspection of the inner fuel tank between rib 1 and rib 23 (zones 541 and 641). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (ducting, wiring) are attached correctly. 5. Close-up ________ Subtask 05-25-40-410-051 A. Close Access
R R
(1) Install the access panels:
R R
(a) For the left side: 541AB, 541BB, 541CB, 541DB, 541EB, 541FB, 541GB, 541HB, 541JB, 541KB, 541LB, 541MB, 541NB, 541PB, 541QB, 541RB, 541SB, 541AZ, 541BZ, 541CZ, 541DZ, 541EZ, 541FZ, 541GZ (Ref. TASK 57-27-11-400-801).
R R R
(b) For the right side: 641AB, 641BB, 641CB, 641DB, 641EB, 641FB, 641GB, 641HB, 641JB, 641KB, 641LB, 641MB, 641NB, 641PB, 641QB, 641RB, 641SB, 641AZ, 641BZ, 641CZ, 641DZ, 641EZ, 641FZ, 641GZ (Ref. TASK 57-27-11-400-801).
R
Subtask 05-25-40-650-053 B. Refuel the tanks. (Ref. TASK 12-11-28-650-803)
EFF : ALL 05-25-40 SROS
Page 607 Jan 01/04
Subtask 05-25-40-942-050 R R
C. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-25-40 SROS
Page 608 Jan 01/04
TASK 05-25-40-200-803 Zonal Inspection of Outer Fuel Tank (Rib 23 to Rib 33). 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 : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND DAMAGE. _______ 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 Refer to the MPD TASK: ZL-542-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific
safety barriers warning notices 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
EFF : ALL 05-25-40 R SROS
Page 609 Apr 01/05
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-11-28-650-803 28-00-00-610-801 28-10-00-910-802 28-25-00-650-801 57-27-11-000-801 57-27-11-400-801
Pressure Refuel with Automatic Control from the Panel 990VU Fuel Safety Procedures Access to Fuel Tanks and Work Areas Pressure Defuel Procedure Removal of the Underwing Tank Access-Panels Installation of the Underwing Tank Access-Panels
R 3. __________ Job Set-up Subtask 05-25-40-650-054 A. Defuel the tanks (Ref. TASK 28-25-00-650-801) Subtask 05-25-40-941-055 B. Safety Precautions (1) Put the safety barriers in position. (2) Put the warning notices in position: - to tell persons not to operate the fuel system - to tell persons not to refuel the aircraft - to tell persons not to operate the flight controls. Subtask 05-25-40-010-052 C. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the outer fuel tank (zones 542 and 642). (2) Remove the access panels: (a) For the left side: 542AB, 542BB, 542CB, 542DB, 542EB, 542FB, 542GB, 542HB, 542JB, 542KB (Ref. TASK 57-27-11-000-801). R
EFF : ALL 05-25-40 SROS
Page 610 Apr 01/05
(b) For the right side: 642AB, 642BB, 642CB, 642DB, 642EB, 642FB, 642GB, 642HB, 642JB, 642KB (Ref. TASK 57-27-11-000-801). R Subtask 05-25-40-941-052 D. Safety Precautions (1) Obey the fuel safety procedures (Ref. TASK 28-00-00-610-801). (2) Get access to the fuel tank (Ref. TASK 28-10-00-910-802). 4. Procedure _________ Subtask 05-25-40-210-052 A. Do a general inspection of the outer fuel tank from rib 23 to rib 33 (zones 542 and 642). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-25-40-410-052 A. Close Access (1) Install the access panels: (a) For the left side: 542AB, 542BB, 542CB, 542DB, 542EB, 542FB, 542GB, 542HB, 542JB, 542KB (Ref. TASK 57-27-11-400-801). R (b) For the right side: 642AB, 642BB, 642CB, 642DB, 642EB, 642FB, 642GB, 642HB, 642JB, 642KB (Ref. TASK 57-27-11-400-801). R
EFF : ALL 05-25-40 SROS
Page 611 Apr 01/05
Subtask 05-25-40-650-055 B. Refuel the tanks. (Ref. TASK 12-11-28-650-803) Subtask 05-25-40-942-052 C. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-25-40 R SROS
Page 612 Apr 01/05
ZONAL INSPECTION : WING VENT SURGE TANK - INSPECTION/CHECK __________________________________________________________ TASK 05-25-50-200-802 R
Zonal Inspection of Vent Surge Tank WARNING : OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND DAMAGE. _______ 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 Refer to the MPD TASK: ZL-550-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific No specific No specific
safety barriers warning notices 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-11-28-650-803 28-00-00-610-801 28-10-00-910-802 28-25-00-650-804 57-27-11-000-801 57-27-11-400-801
Pressure Refuel with Automatic Control from the Panel 990VU Fuel Safety Procedures Access to Fuel Tanks and Work Areas To Defuel One Wing (Inner and Outer Tanks) Only (For Access) Removal of the Underwing Tank Access-Panels Installation of the Underwing Tank Access-Panels
EFF : ALL 05-25-50 SROS
Page 601 Jan 01/04
3. __________ Job Set-up Subtask 05-25-50-650-050 R
A. Defuel the wings (Ref. TASK 28-25-00-650-804). Subtask 05-25-50-941-052 B. Safety Precautions (1) Put the safety barriers in position. (2) Put the warning notices in position: - to tell persons not to operate the fuel system - to tell persons not to refuel the aircraft - to tell persons not to operate the flight controls.
R R
Subtask 05-25-50-010-051 C. Get Access R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the vent surge tank (zones 550 and 650). (2) Remove the access panels:
R R
(a) For the left side: 550AB, 550BB, 550CB, 550DB, 550EB, 550FB (Ref. TASK 57-27-11-000-801).
R R
(b) For the right side: 650AB, 650BB, 650CB, 650DB, 650EB, 650FB (Ref. TASK 57-27-11-000-801). Subtask 05-25-50-941-053 D. Safety Precautions (1) Obey the fuel safety procedures (Ref. TASK 28-00-00-610-801). (2) Get access to the vent surge tank (Ref. TASK 28-10-00-910-802)
EFF : ALL 05-25-50 SROS
Page 602 Jan 01/04
4. Procedure _________ Subtask 05-25-50-210-051 A. Do a general visual inspection of the vent surge tank (zones 550 and 650). Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-25-50-410-051 A. Close Access R R
(1) Install the access panels:
R
(a) For the left side: 550AB, 550BB, 550CB, 550DB, 550EB, 550FB (Ref. TASK 57-27-11-400-801).
R
(b) For the right side: 650AB, 650BB, 650CB, 650DB, 650EB, 650FB (Ref. TASK 57-27-11-400-801).
R Subtask 05-25-50-650-051 B. Refuel the tanks. (Ref. TASK 12-11-28-650-803) Subtask 05-25-50-942-050 R R
C. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-25-50 SROS
Page 603 Jan 01/04
________________________________________________________________________ ZONAL INSPECTION : AFT SECTION OF WING AND TRAILING EDGE FIXED STRUCTURE ________________ INSPECTION/CHECK TASK 05-25-70-200-803 Zonal Inspection of Main Landing Gear Well. 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 Refer to the MPD TASK: ZL-571-01 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 ------------------------------------------------------------------------------32-12-00-010-801 32-12-00-410-801
Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-25-70-010-051 A. Get Access R
(1) Open the main landing-gear doors 734, 744 (Ref. TASK 32-12-00-010801).
R R R
(2) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the main landing-gear well (zones 571 and 671).
EFF : ALL 05-25-70 SROS
Page 601 Jan 01/06
4. Procedure _________ Subtask 05-25-70-210-051 R R
A. Do a general visual inspection of the main landing-gear well (zones 571 and 671). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-25-70-410-051 A. Close Access
R R
(1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Close the main landing-gear doors 734 and 744 (Ref. TASK 32-12-00410-801). Subtask 05-25-70-860-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R
EFF : ALL 05-25-70 SROS
Page 602 Jan 01/06
TASK 05-25-70-200-804 R
Zonal Inspection of Shroud Box. 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 Refer to the MPD TASK: ZL-572-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific No specific
warning notices 1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
3. __________ Job Set-up R
Subtask 05-25-70-941-050
R
A. Safety Precautions
R R
(1) Put warning notices in the cockpit to tell persons not to operate the flight controls.
EFF : ALL 05-25-70 SROS
Page 603 Jan 01/04
R
**ON A/C 001-001, 201-202, 251-252, 401-449, Subtask 05-25-70-010-052-A B. Get Access (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the shroud box (zones 572 and 672). (2) Remove the access panels:
R
(a) For the left side: 572AB.
R
(b) For the right side: 672AB.
R
**ON A/C 002-049, 203-249, 255-299, 301-399, 451-499, 701-749,
R
Subtask 05-25-70-010-052
R
B. Get Access
R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the shroud box (zones 572 and 672).
R
(2) Remove the access panels:
R
(a) For the left side: 572BB, 572CB and 572EB.
R
(b) For the right side: 672BB, 672CB and 672EB.
R
**ON A/C ALL 4. Procedure _________ Subtask 05-25-70-210-052 A. Do a general visual inspection of the shroud box (zones 572 and 672). Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see.
EFF : ALL 05-25-70 SROS
Page 604 Jul 01/06
5. Close-up ________ R
**ON A/C 001-001, 201-202, 251-252, 401-449, Subtask 05-25-70-410-052-A A. Close Access (1) Install the access panels:
R
(a) For the left side: 572AB.
R
(b) For the right side: 672AB.
R
**ON A/C 002-049, 203-249, 255-299, 301-399, 451-499, 701-749,
R
Subtask 05-25-70-410-052
R
A. Close Access
R
(1) Install the access panels:
R
(a) For the left side: 572BB, 572CB and 572EB.
R
(b) For the right side: 672BB, 672CB and 672EB.
R
**ON A/C ALL Subtask 05-25-70-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-25-70 SROS
Page 605 Jul 01/06
TASK 05-25-70-200-805 Zonal Inspection of Inner Trailing Edge Fixed Structure (RIB 6 to RIB 12) 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 Refer to the MPD TASK: ZL-573-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
27-50-00-866-801 27-50-00-866-802
Extension of the Flaps on the Ground Retraction of the Flaps on the Ground
R
EFF : ALL 05-25-70 SROS
Page 606 Jul 01/06
3. __________ Job Set-up Subtask 05-25-70-866-050 A. Aircraft Maintenance Configuration R
(1) Fully extend the flaps (Ref. TASK 27-50-00-866-801). Subtask 05-25-70-941-051 B. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-25-70-010-053 C. Get Access (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the zone 573(673). (2) Remove the access panels: (a) For the left side: 573CB, 573DB, 573FB, 573GB. (b) For the right side: 673CB, 673DB, 673FB, 673GB. 4. Procedure _________ Subtask 05-25-70-210-053
R
A. Do a general visual inspection of the inner trailing-edge fixed structure (RIB6 to RIB12). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (wiring) are attached correctly.
EFF : ALL 05-25-70 SROS
Page 607 Jul 01/06
5. Close-up ________ Subtask 05-25-70-410-053 A. Close Access (1) Install the access panels: (a) For the left side: 573CB, 573DB, 573FB, 573GB. (b) For the right side: 673CB, 673DB, 673FB, 673GB. Subtask 05-25-70-860-052 B. Put the Aircraft back to its Initial Configuration (1) Retract the flaps (Ref. TASK 27-50-00-866-802). (2) Remove all the fixtures, tools, test and support equipment used during this procedure. (3) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-25-70 R SROS
Page 608 Jul 01/06
TASK 05-25-70-200-806 Zonal Inspection of Center Trailing Edge Fixed Structure (RIB 12 to RIB 27) 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 Refer to the MPD TASK: ZL-574-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE 1 WARNING NOTICE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------27-50-00-866-801 27-50-00-866-802
Extension of the Flaps on the Ground Retraction of the Flaps on the Ground
3. __________ Job Set-up Subtask 05-25-70-866-052 A. Aircraft Maintenance Configuration (1) Fully extend the flaps (Ref. TASK 27-50-00-866-801).
EFF : ALL 05-25-70 R SROS
Page 609 Jul 01/06
Subtask 05-25-70-941-052 B. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls. Subtask 05-25-70-010-054 C. Get Access (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the zone 574(674). (2) Remove the access panels: (a) For the left side: 574AT. (b) For the right side: 674AT. 4. Procedure _________ Subtask 05-25-70-210-054 A. Do a general visual inspection of the center trailing-edge fixed structure (RIB12 to RIB27). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-25-70-410-054 A. Close Access (1) Install the access panels: (a) For the left side: 574AT. (b) For the right side: 674AT.
EFF : ALL 05-25-70 R SROS
Page 610 Jul 01/06
Subtask 05-25-70-860-053 B. Put the Aircraft back to its Initial Configuration (1) Retract the flaps (Ref. TASK 27-50-00-866-802). (2) Remove all the fixtures, tools, test and support equipment used during this procedure. (3) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-25-70 R SROS
Page 611 Jul 01/06
TASK 05-25-70-200-807 Zonal Inspection of Outer Trailing Edge Fixed Structure (RIB 27 to RIB 39) 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 Refer to the MPD TASK: ZL-575-01 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 WARNING NOTICE
3. __________ Job Set-up Subtask 05-25-70-941-053 A. Safety Precautions (1) Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls.
EFF : ALL 05-25-70 R SROS
Page 612 Jul 01/06
Subtask 05-25-70-010-055 B. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at zone 575(675). (2) Remove the access panels: (a) For the left side: 575AB, 575BB, 575CB, 575DB, 575AT, 575BT. (b) For the right side: 675AB, 675BB, 675CB, 675DB, 675AT, 675BT. 4. Procedure _________ Subtask 05-25-70-210-055 A. Do a general visual inspection of the outer trailing-edge fixed structure (RIB27 to RIB39). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-25-70-410-055 A. Close Access (1) Install the access panels: (a) For the left side: 575AB, 575BB, 575CB, 575DB, 575AT, 575BT. (b) For the right side: 675AB, 675BB, 675CB, 675DB, 675AT, 675BT. Subtask 05-25-70-860-054 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-25-70 SROS
Page 613 Jul 01/06
ZONAL INSPECTION : WING AILERON - INSPECTION/CHECK __________________________________________________ TASK 05-25-90-200-801 R
Zonal Inspection of Inboard Aileron. 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 Refer to the MPD TASK: ZL-591-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific No specific
warning notices 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
3. __________ Job Set-up R
Subtask 05-25-90-941-050
R
A. Safety Precautions
R R
(1) Put warning notices in the cockpit to tell persons not to operate the flight controls.
EFF : ALL 05-25-90 SROS
Page 601 Jan 01/04
Subtask 05-25-90-010-050 R
B. Get Access
R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the inboard aileron (zones 591 and 691). (2) Remove the access panels:
R
(a) For the left side: 591AB, 591BB, 591CB, 591DB, 575AB, 575BB.
R
(b) for the right side: 691AB, 691BB, 691CB, 691DB, 675AB, 675BB. 4. Procedure _________ Subtask 05-25-90-210-050 A. Do a general visual inspection of the inboard aileron (zones 591 and 691). Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-25-90-410-050 A. Close Access
R R
(1) Install the access panels:
R
(a) For the left side: 591AB, 591BB, 591CB, 591DB, 575AB, 575BB.
R R
(b) For the right side: 691AB, 691BB, 691CB, 691DB, 675AB, 675BB.
R R
Subtask 05-25-90-860-050 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-25-90 SROS
Page 602 Jan 01/04
TASK 05-25-90-200-802 R
Zonal Inspection of Outboard Aileron. 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 Refer to the MPD TASK: ZL-592-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific No specific
warning notices 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
3. __________ Job Set-up Subtask 05-25-90-010-051 A. Get Access R R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the outboard aileron (zones 592 and 692). (2) Put warning notices in the cockpit to tell persons not to operate the flight controls.
EFF : ALL 05-25-90 SROS
Page 603 Jan 01/04
(3) Remove the access panels: R
(a) For the left side: 592AB, 592BB, 592CB, 592DB, 575CB, 575DB.
R
(b) For the right side: 692AB, 692BB, 692CB, 692DB, 675CB, 675DB. 4. Procedure _________ Subtask 05-25-90-210-051 A. Do a general visual inspection of the outboard aileron (zones 592 and 692). Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-25-90-410-051 A. Close Access
R R
(1) Install the access panels:
R
(a) For the left side: 592AB, 592BB, 592CB, 592DB, 575CB, 575DB.
R R
(b) For the right side: 692AB, 692BB, 692CB, 692DB, 675CB, 675DB.
R R
Subtask 05-25-90-860-051 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-25-90 SROS
Page 604 Jan 01/04
ZONAL INSPECTION : LANDING GEAR AND LANDING GEAR DOORS - INSPECTION/CHECK _________________________________________________________________________ TASK 05-27-00-200-803 R
Zonal inspection of Landing Gear and Landing Gear Doors. 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-700-01 2. ______________________ Job Set-up Information Not Applicable 3. __________ Job Set-up Subtask 05-27-00-869-051
R R
A. Not applicable. 4. Procedure _________ Subtask 05-27-00-210-051 A. Inspection (1) Do a general visual inspection of the landing gears and the landing gear doors (zone 700). (2) Make sure that: - There is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - All the installations (wiring) are attached correctly.
EFF : ALL 05-27-00 SROS
Page 601 Jan 01/04
ZONAL INSPECTION : NOSE GEAR AND DOORS - INSPECTION/CHECK _________________________________________________________ TASK 05-27-10-200-804 R
Zonal Inspection of Nose Landing Gear. 1. __________________ Reason for the Job
R
Refer to the MPD TASK: ZL-711-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-22-00-010-801 32-22-00-410-801
Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-27-10-010-052 A. Get Access R R
(1) Put an ACCESS PLATFORM 2M (6 FT) in position at the NLG main doors 713 and 714.
R
(2) Open the nose landing-gear main-doors 713, 714 (Ref. TASK 32-22-00010-801).
EFF : ALL 05-27-10 SROS
Page 601 Jan 01/04
4. Procedure _________ Subtask 05-27-10-210-053 A. Inspection R
(1) Do a general visual inspection of the nose landing-gear (zone 711). (2) Make sure that: - There is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - All the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-27-10-410-052 A. Close Access (1) Close the nose landing-gear main-doors. (Ref. TASK 32-22-00-410-801).
R R R
Subtask 05-27-10-860-050 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-27-10 SROS
Page 602 Jan 01/04
TASK 05-27-10-200-806 Zonal Inspection of the Nose Landing Gear (Zones 710) 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-22-00-010-801 32-22-00-410-801
Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-27-10-010-053 A. Get Access (1) Open the nose landing-gear main-doors 713, 714, (Ref. TASK 32-22-00010-801). 4. Procedure _________ Subtask 05-27-10-210-055 A. Do a general visual inspection of the nose landing gear, from the ground ,as far as visible (including zones 713 and 714). Make sure that: - There is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - All the installations (wiring) are attached correctly.
EFF : ALL 05-27-10 R SROS
Page 603 Jan 01/04
5. Close-up ________ Subtask 05-27-10-410-053 A. Close Access (1) Close the nose landing gear doors (Ref. TASK 32-22-00-410-801). (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-27-10 R SROS
Page 604 Jan 01/04
TASK 05-27-10-200-807 Zonal Inspection of Nose Landing Gear Main Doors. 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 Refer to the MPD TASK: ZL-713-01 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
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-22-00-010-801 32-22-00-410-801
Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-27-10-010-054 A. Get Access R
(1) Open the nose landing-gear doors 713, 714 (Ref. TASK 32-22-00-010801). (2) Put an ACCESS PLATFORM 2M (6 FT) in position at the nose landing-gear doors 713 and 714.
EFF : ALL 05-27-10 SROS
Page 605 Jan 01/07
4. Procedure _________ Subtask 05-27-10-210-056 A. Inspection (1) Do a general visual inspection of the nose landing-gear main-doors (zones 713 and 714). (2) Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-27-10-410-054 A. Close Access R R
(1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Close the nose landing-gear doors. (Ref. TASK 32-22-00-410-801). Subtask 05-27-10-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R
EFF : ALL 05-27-10 SROS
Page 606 Jan 01/06
TASK 05-27-10-200-808 Zonal Inspection of Nose Landing Gear Aft Doors. 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-715-01 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
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-22-00-010-801 32-22-00-410-801
Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-27-10-010-055 A. Get Access (1) Put an ACCESS PLATFORM 2M (6 FT) in position at the nose landing-gear (NLG) doors 715 and 716. R
(2) Open the nose landing-gear doors (Ref. TASK 32-22-00-010-801).
EFF : ALL 05-27-10 SROS
Page 607 Jan 01/07
4. Procedure _________ Subtask 05-27-10-210-057 A. Inspection (1) Do a general visual inspection of the NLG aft doors (zones 715 and 716). (2) Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-27-10-410-055 A. Close Access (1) Close the nose landing-gear doors (Ref. TASK 32-22-00-410-801). Subtask 05-27-10-860-052 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-27-10 R SROS
Page 608 Jan 01/07
ZONAL INSPECTION : MAIN LANDING GEAR AND DOORS - INSPECTION/CHECK _________________________________________________________________ TASK 05-27-30-200-804 R
Zonal Inspection of LH and RH Main Landing Gear. 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-731-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-12-00-010-801 32-12-00-410-801
Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-27-30-010-051 A. Get Access R
(1) Open the main landing-gear (MLG) doors (Ref. TASK 32-12-00-010-801). (2) Put an ACCESS PLATFORM 2M (6 FT) in position at the main landing gear (zones 730 and 740).
EFF : ALL 05-27-30 SROS
Page 601 Jan 01/04
4. Procedure _________ Subtask 05-27-30-210-052 A. Inspection R R
(1) Do a general visual inspection of the main landing gears (zones 731 and 741). (2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-27-30-410-051 A. Close Access (1) Close the main landing-gear doors (Ref. TASK 32-12-00-410-801). Subtask 05-27-30-860-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-27-30 SROS
Page 602 Oct 01/04
TASK 05-27-30-200-809 Zonal Inspection of the Main Landing Gear (Zones 730 and 740). 1. __________________ Reason for the Job R R
Self Explanatory 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-12-00-010-801 32-12-00-410-801
Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-27-30-010-052 A. Get Access R
(1) Open is main landing gear main doors 734, 744 (Ref. TASK 32-12-00010-801). 4. Procedure _________ Subtask 05-27-30-210-057 A. Make a general visual inspection of the main landing gear, from the ground, as far as visible (zones 731 and 741). Make sure that: - there is no damage, corrosion, leaks or cracks on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-27-30-410-052 A. Close Access (1) Close the main landing-gear main doors 734, 744 (Ref. TASK 32-12-00410-801). (2) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-27-30 SROS
Page 603 Jul 01/03
TASK 05-27-30-200-810 R
Zonal Inspection of Main Landing Gear Leg Doors. 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-732-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-12-00-010-801 32-12-00-410-801
Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-27-30-010-053 A. Get Access R
(1) Open the main landing-gear (MLG) doors (Ref. TASK 32-12-00-010-801). (2) Put an ACCESS PLATFORM 2M (6 FT) in position at the main landing gear (zones 730 and 740).
R EFF : ALL 05-27-30 SROS
Page 604 Jan 01/04
4. Procedure _________ Subtask 05-27-30-210-058 A. Inspection R R
(1) Do a general visual inspection of the MLG leg doors (zone 732 and 742). (2) Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see 5. Close-up ________ Subtask 05-27-30-410-053 A. Close Access
R R R R
(1) Close the main landing-gear doors (Ref. TASK 32-12-00-410-801). Subtask 05-27-30-860-051 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-27-30 SROS
Page 605 Jan 01/04
TASK 05-27-30-200-811 R
Zonal Inspection of Main Landing Gear Hinge Door. 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-733-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-12-00-010-801 32-12-00-410-801
Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-27-30-010-054 A. Get Access R
(1) Open the main landing-gear (MLG) doors (Ref. TASK 32-12-00-010-801). (2) Put an ACCESS PLATFORM 2M (6 FT) in position at the main landing gear (zones 730 and 740). 4. Procedure _________ Subtask 05-27-30-210-059 A. Inspection
R R R
(1) Do a general visual inspection of the MLG hinge doors (zones 733 and 743).
EFF : ALL 05-27-30 SROS
Page 606 Jan 01/04
(2) Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see 5. Close-up ________ Subtask 05-27-30-410-054 A. Close Access R R R R
(1) Close the main landing-gear doors (Ref. TASK 32-12-00-410-801). Subtask 05-27-30-860-052 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-27-30 SROS
Page 607 Jan 01/04
TASK 05-27-30-200-812 R
Zonal Inspection of Main Landing Gear Main Doors. 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-734-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-12-00-010-801 32-12-00-410-801
Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance
3. __________ Job Set-up Subtask 05-27-30-010-055 A. Get Access R
(1) Open the main landing-gear (MLG) doors (Ref. TASK 32-12-00-010-801). (2) Put an ACCESS PLATFORM 2M (6 FT) in position at the main landing gear (zones 730 and 740).
EFF : ALL 05-27-30 SROS
Page 608 Jan 01/04
4. Procedure _________ Subtask 05-27-30-210-060 A. Inspection R R
(1) Do a general visual inspection of the main landing-gear main-doors (zone 734 and 744). (2) Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see 5. Close-up ________ Subtask 05-27-30-410-055 A. Close Access
R R R R R
(1) Close the MLG doors (Ref. TASK 32-12-00-410-801). Subtask 05-27-30-860-053 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-27-30 SROS
Page 609 Jan 01/04
______________________________________________________________________________ ZONAL INSPECTION : PASSENGER/CREW DOORS, CARGO COMPARTMENT DOORS AND EMERGENCY EXITS - INSPECTION/CHECK ________________________ TASK 05-28-00-200-801 Zonal Inspection as far as visible from the ground of the Doors (zone 800) 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information Not Applicable 3. __________ Job Set-up Subtask 05-28-00-869-050 A. Not applicable. 4. Procedure _________ Subtask 05-28-00-210-050 A. Do a general visual inspection of the passenger/crew doors, the emergency exits and the cargo doors as far as visible from the ground during the aircraft walkaround.
EFF : ALL 05-28-00 R SROS
Page 601 Jan 01/04
TASK 05-28-00-200-802 Zonal Inspection of Doors 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-800-01 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
1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
3. __________ Job Set-up Subtask 05-28-00-010-050 A. Get Access R R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position next to the doors. 4. Procedure _________ Subtask 05-28-00-210-051 A. Do a general visual inspection of the Passenger/Crew doors, the emergency exits, the cargo compartment doors and the forward avionics compartment doors (zones 811, 821, 822, 831, 832, 833, 834, 841, 842, 843 and 844). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see.
EFF : ALL 05-28-00 SROS
Page 602 Jan 01/07
5. Close-up ________ Subtask 05-28-00-410-050 A. Close Access (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-28-00 SROS
Page 603 Jan 01/07
ZONAL INSPECTION : FORWARD AVIONICS COMPARTMENT - INSPECTION/CHECK __________________________________________________________________ TASK 05-28-10-200-801 Zonal Inspection of Forward Avionics Compartment Door 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-811-01 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
1 ACCESS PLATFORM 2M (6 FT)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 53-12-13-000-801 53-12-13-400-801 05-28-10-991-001
Energize the Ground Service Network De-energize the Ground Service Network Removal of the Avionics-Compartment Floor Panels Installation of the Avionics-Compartment Floor Panels Fig. 601
3. __________ Job Set-up Subtask 05-28-10-861-050 R
A. Energize the ground service network (Ref. TASK 24-42-00-861-801). Subtask 05-28-10-010-050 B. Get Access (Ref. Fig. 601/TASK 05-28-10-991-001) (1) Put an ACCESS PLATFORM 2M (6 FT) in position at the access door 811. (2) Open the forward avionics compartment door 811.
EFF : ALL 05-28-10 SROS
Page 601 Jan 01/07
R R
FWD Avionics Compartment Door (Zone 811) Figure 601/TASK 05-28-10-991-001
EFF : ALL 05-28-10 SROS
Page 602 Jan 01/04
R
(3) Open the access floor panel 121EF (Ref. TASK 53-12-13-000-801). 4. Procedure _________ Subtask 05-28-10-210-050
R R
A. Do a general visual inspection of the forward avionics compartment door (zone 811). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-28-10-410-050 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Close the forward avionics compartment door 811.
R R
(3) Close the access floor panel 121EF (Ref. TASK 53-12-13-400-801). Subtask 05-28-10-862-050
R
B. Put the Aircraft back to its Initial Configuration
R R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R
(2) De-energize the ground service network (Ref. TASK 24-42-00-862-801).
EFF : ALL 05-28-10 SROS
Page 603 Jan 01/04
__________________________________________________________________________ ZONAL INSPECTION : LOWER DECK FORWARD AFT AND BULK CARGO COMPARTMENT DOORS ________________ INSPECTION/CHECK TASK 05-28-20-200-802 R
Zonal Inspection of Forward Cargo Compartment Door 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-821-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------52-30-00-010-801 52-30-00-410-801 R
05-28-20-991-001
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 Fig. 601
3. __________ Job Set-up Subtask 05-28-20-010-051 R
A. Get Access (Ref. Fig. 601/TASK 05-28-20-991-001)
R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the access door 821.
R
(2) Open the forward cargo-compartment door 821 (Ref. TASK 52-30-00-010801).
EFF : ALL 05-28-20 SROS
Page 601 Jan 01/04
Access Panels on the Cargo-Compartment Door Zone 821-822 Figure 601/TASK 05-28-20-991-001 EFF : ALL 05-28-20 R SROS
Page 602 Jan 01/04
4. Procedure _________ Subtask 05-28-20-210-051 A. Do a general visual inspection of the forward cargo compartment door (zone 821). This includes: - The lock fittings at the door sill. - The door frames at the fuselage door seals. - The visible part of the door sill. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-28-20-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the forward cargo-compartment door 821 (Ref. TASK 52-30-00-410801). Subtask 05-28-20-860-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-28-20 R SROS
Page 603 Apr 01/04
TASK 05-28-20-200-803 R R
Zonal Inspection of Forward Cargo Compartment Door (Including Door Hinge Arms Attachment Area) 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-821-02 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 ------------------------------------------------------------------------------52-30-00-010-801 52-30-00-410-801 05-28-20-991-001 05-28-20-991-002
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 Fig. 601 Fig. 602
3. __________ Job Set-up Subtask 05-28-20-010-052 A. Get Access (Ref. Fig. 601/TASK 05-28-20-991-001, 602/TASK 05-28-20-991-002) R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at zone 821.
R
(2) Open the forward cargo-compartment door 821, (Ref. TASK 52-30-00-010801). (3) Remove the access panels 821AR, 821BR, 821CR, 821DR, 132AR, 132BR, 132CR, 132DR, 132ER, 132FR, 132GR, 132HR, 132JR, 132KR, 132LR.
EFF : ALL 05-28-20 SROS
Page 604 Apr 01/04
R R
Forward-Fuselage Lower Section Figure 602/TASK 05-28-20-991-002
EFF : ALL 05-28-20 SROS
Page 605 Jan 01/04
4. Procedure _________ Subtask 05-28-20-210-052 R
A. Do a general visual inspection of the forward cargo-compartment door (zone 821). This includes the door-hinge arms attachment-area. Make sure that : - there is no damage(corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (piping) are attached correctly. 5. Close-up ________ Subtask 05-28-20-410-052 A. Close Access (1) Install the access panels 821AR, 821BR, 821CR, 821DR, 132AR, 132BR, 132CR, 132DR, 132ER, 132FR, 132GR, 132HR, 132JR, 132KR, 132LR. (2) Close the forward cargo-compartment door 821, (Ref. TASK 52-30-00410-801). Subtask 05-28-20-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-28-20 SROS
Page 606 Jul 01/04
TASK 05-28-20-200-804 R
Zonal Inspection of Aft Cargo Compartment Door 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-822-01 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------52-30-00-010-801 52-30-00-410-801
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 05-28-20-010-053 A. Get Access R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the access door 822.
R
(2) Open the aft cargo-compartment door 822 (Ref. TASK 52-30-00-010-801).
EFF : ALL 05-28-20 SROS
Page 607 Jan 01/04
4. Procedure _________ Subtask 05-28-20-210-053 R R R R R R R
A. Do a general visual inspection of the aft cargo-compartment door (zone 822). This includes: - The lock fittings at the door sill. - The door frames at the fuselage door seals. - The visible part of the door sill. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (piping, wiring) are attached correctly.
R
5. Close-up ________ Subtask 05-28-20-410-053 A. Close Access R R
(1) Make sure that the work area is clean and clear of tools and other items.
R
(2) Close the aft cargo-compartment door 822 (Ref. TASK 52-30-00-410801).
R R R
Subtask 05-28-20-860-053 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-28-20 SROS
Page 608 Jan 01/04
TASK 05-28-20-200-805 Zonal Inspection of Aft Cargo Compartment Door (Including Door Hinge Arms Attachment Area) 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-822-02 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 ------------------------------------------------------------------------------52-30-00-010-801 52-30-00-410-801 05-28-20-991-001 05-28-20-991-003
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 Fig. 601 Fig. 603
3. __________ Job Set-up Subtask 05-28-20-010-054 A. Get Access (Ref. Fig. 601/TASK 05-28-20-991-001, 603/TASK 05-28-20-991-003) (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at zone 822. R
(2) Open the aft cargo-compartment door 822, (Ref. TASK 52-30-00-010801). (3) Remove the access panels 822AR, 822BR, 822CR, 822DR, 152AR, 152BR, 152CR, 152DR, 152ER, 152FR, 152GR, 152HR, 152JR, 152KR, 152LR.
EFF : ALL 05-28-20 SROS
Page 609 Jul 01/04
R R
Aft-Fuselage Lower-Section Access-Panels - Zone 822 Figure 603/TASK 05-28-20-991-003
EFF : ALL 05-28-20 SROS
Page 610 Apr 01/04
4. Procedure _________ Subtask 05-28-20-210-054 R
A. Do a general visual inspection of the aft cargo-compartment door (zone 822). This includes the door-hinge arms attachment-area. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-28-20-410-054 A. Close Access (1) Install the access panels 822AR, 822BR, 822CR, 822DR, 152AR, 152BR, 152CR, 152DR, 152ER, 152FR, 152GR, 152HR, 152JR, 152KR, 152LR. (2) Close the aft cargo-compartment door 822, (Ref. TASK 52-30-00-410801). Subtask 05-28-20-860-054 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-28-20 SROS
Page 611 Jul 01/04
TASK 05-28-20-200-806 R
Zonal Inspection of Bulk Cargo Compartment Door (Including Fuselage Frames, Stop Fittings at Fuselage Frames, Door Seals, and Visible Part of Door Sill). 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-823-01 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 ------------------------------------------------------------------------------52-30-00-010-803 52-30-00-410-803
Opening of the BULK Cargo-Compartment Door Closing of the BULK Cargo-Compartment Door
3. __________ Job Set-up Subtask 05-28-20-010-055 A. Get Access R R
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the bulk cargo-compartment door 823. (2) Open the bulk cargo-compartment door 823 (Ref. TASK 52-30-00-010803).
EFF : ALL 05-28-20 SROS
Page 612 Jul 01/04
4. Procedure _________ Subtask 05-28-20-210-055 R R
A. Do a general visual inspection of the bulk cargo-compartment door (zone 823). This inspection includes the fuselage frames, the stop fittings, the door seals and the visible part of the door sill. Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (piping, wiring) are attached correctly. 5. Close-up ________ Subtask 05-28-20-410-055 A. Close Access (1) Close the bulk cargo-compartment door 823 (Ref. TASK 52-30-00-410803). Subtask 05-28-20-860-056 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-28-20 SROS
Page 613 Jul 01/04
TASK 05-28-20-200-807 Zonal Inspection of Bulk Cargo Compartment Door. 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-823-02 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 ------------------------------------------------------------------------------25-80-00-000-801 25-80-00-400-801 52-30-00-010-803 52-30-00-410-803
Removal of the Insulation Blankets Installation of the Insulation Blankets Opening of the BULK Cargo-Compartment Door Closing of the BULK Cargo-Compartment Door
3. __________ Job Set-up Subtask 05-28-20-010-056 A. Get Access (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the bulk cargo-compartment door 823. (2) Open the bulk cargo-compartment door 823 (Ref. TASK 52-30-00-010803). (3) Lift or remove the insulation blankets (Ref. TASK 25-80-00-000-801).
EFF : ALL 05-28-20 R SROS
Page 614 Apr 01/04
4. Procedure _________ Subtask 05-28-20-210-056 A. Do a general visual inspection of the bulk cargo-compartment door (zone 823). Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-28-20-410-056 A. Close Access (1) Install the insulation blankets, if removed (Ref. TASK 25-80-00-400801). (2) Close the bulk cargo-compartment door 823 (Ref. TASK 52-30-00-410803). Subtask 05-28-20-860-057 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-28-20 R SROS
Page 615 Apr 01/04
TASK 05-28-20-200-808 Zonal Inspection of Forward Cargo Compartment Door 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-821-03 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 ------------------------------------------------------------------------------25-80-00-000-801 25-80-00-400-801 52-30-00-010-801 52-30-00-410-801 05-28-20-991-001
Removal of the Insulation Blankets Installation of the Insulation Blankets 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 Fig. 601
3. __________ Job Set-up Subtask 05-28-20-010-057 A. Get Access (Ref. Fig. 601/TASK 05-28-20-991-001) (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the access door 821. (2) Open the forward cargo-compartment door 821 (Ref. TASK 52-30-00-010801). (3) Remove the access panels 821AR, 821BR, 821CR, 821DR.
EFF : ALL 05-28-20 R SROS
Page 616 Apr 01/04
(4) Remove the insulation blankets (Ref. TASK 25-80-00-000-801). 4. Procedure _________ Subtask 05-28-20-210-057 A. Do a general visual inspection of the forward cargo-compartment door (zone 821). Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-28-20-410-057 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Install the insulation blankets (Ref. TASK 25-80-00-400-801). (3) Install the access panels 821AR, 821BR, 821CR, 821DR. (4) Close the forward cargo-compartment door 821 (Ref. TASK 52-30-00-410801). Subtask 05-28-20-860-052 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure.
EFF : ALL 05-28-20 R SROS
Page 617 Apr 01/04
TASK 05-28-20-200-809 Zonal Inspection of AFT Cargo Compartment Door. 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-822-03 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 ------------------------------------------------------------------------------25-80-00-000-801 25-80-00-400-801 52-30-00-010-801 52-30-00-410-801
Removal of the Insulation Blankets Installation of the Insulation Blankets 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 05-28-20-010-058 A. Get Access (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the aft cargo-compartment door 822. (2) Open the aft cargo-compartment door 822 (Ref. TASK 52-30-00-010-801). (3) Remove the access panels 822AR, 822BR, 822CR, 822DR. (4) Remove or lift the insulation blankets (Ref. TASK 25-80-00-000-801).
EFF : ALL 05-28-20 R SROS
Page 618 Apr 01/04
4. Procedure _________ Subtask 05-28-20-210-058 A. Do a general visual inspection of the aft cargo-compartment door (zone 822). Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-28-20-410-058 A. Close Access (1) Install the insulation blankets (Ref. TASK 25-80-00-400-801). (2) Install the access panels 822AR, 822BR, 822CR, 822DR. (3) Close the aft cargo-compartment door 822 (Ref. TASK 52-30-00-410801). Subtask 05-28-20-860-055 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-28-20 SROS
Page 619 Apr 01/04
_________________________________________________________________ ZONAL INSPECTION : LEFT PASSENGER/ CREW DOORS AND EMERGENCY EXITS ________________ INSPECTION/CHECK TASK 05-28-30-200-801 R
Zonal Inspection of FWD Passenger/Crew Door (Including Door Stops on Fuselage Side, Door Seals and Scuff Plates) 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-831-01 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 ------------------------------------------------------------------------------52-10-00-010-801 52-10-00-410-801
Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door
3. __________ Job Set-up Subtask 05-28-30-010-050 A. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the passenger/crew doors 831 and 841 . (2) Open the passenger/crew doors 831 and 841 (Ref. TASK 52-10-00-010801).
EFF : ALL 05-28-30 SROS
Page 601 Apr 01/04
4. Procedure _________ Subtask 05-28-30-210-050 A. Do a general visual inspection of the passenger/crew doors (zones 831 and 841). This inspection includes the door stops on the fuselage side, the door seals and the scuff plates. Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-28-30-410-050 A. Close Access (1) Close the passenger/crew doors 831 and 841 (Ref. TASK 52-10-00-410801). Subtask 05-28-30-860-056 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-28-30 R SROS
Page 602 Apr 01/04
TASK 05-28-30-200-802 Zonal Inspection of FWD Passenger/Crew Door 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-831-02 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
25-23-49-000-801
R R
25-23-49-400-801 25-80-00-000-801 25-80-00-400-801 52-10-00-010-801 52-10-00-410-801
Removal of the Lining of the Forward Passenger/Crew Door(s) Installation of the Lining of the Forward Passenger/Crew Door(s) Removal of the Insulation Blankets Installation of the Insulation Blankets Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door
3. __________ Job Set-up Subtask 05-28-30-010-051 A. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the passenger/crew doors 831 and 841. (2) Open the passenger/crew doors 831 and 841 (Ref. TASK 52-10-00-010801).
EFF : ALL 05-28-30 SROS
Page 603 Jan 01/06
(3) Remove the access panels: (a) For the FWD passenger/crew door 831 (left side): 831AZ, 831BZ, 831CZ, 831DZ, 831EZ, 831FZ, 831GZ, 831HZ, 831JZ (Ref. TASK 25-23-49-000-801). (b) For the FWD passenger/crew door 841 (right side): 841AZ, 841BZ, 841CZ, 841DZ, 841EZ, 841FZ, 841GZ, 841HZ, 841JZ (Ref. TASK 25-23-49-000-801). (4) Lift or remove the insulation blankets (Ref. TASK 25-80-00-000-801). 4. Procedure _________ Subtask 05-28-30-210-051 A. Do a general visual inspection of the forward passenger/crew doors (zones 831 and 841) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-28-30-410-051 A. Close Access (1) Install the insulation blankets (Ref. TASK 25-80-00-400-801). (2) Install the access panels: (a) For the FWD passenger/crew door 831 (left side): 831AZ, 831BZ, 831CZ, 831DZ, 831EZ, 831FZ, 831GZ, 831HZ, 831JZ (Ref. TASK 25-23-49-400-801). (b) For the FWD passenger/crew door 841 (right side): 841AZ, 841BZ, 841CZ, 841DZ, 841EZ, 841FZ, 841GZ, 841HZ, 841JZ (Ref. TASK 25-23-49-400-801). (3) Close the passenger/crew doors 831 and 841 (Ref. TASK 52-10-00-410801).
EFF : ALL 05-28-30 R SROS
Page 604 Apr 01/04
R R
Subtask 05-28-30-860-057 B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-28-30 SROS
Page 605 Jan 01/04
TASK 05-28-30-200-809 R
Zonal Inspection of Emergency Exit (Including Door Stops on Fuselage Side, Door Seals and Scuff Plates) 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-834-01 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
52-20-00-010-801 52-20-00-410-801
Opening of the Emergency Exit Door Closing of the Emergency Exit Door
3. __________ Job Set-up Subtask 05-28-30-010-058 A. Get Access R R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at zone 834(844).
R
(2) Open the emergency exit doors 834, 844, (Ref. TASK 52-20-00-010-801).
EFF : ALL 05-28-30 SROS
Page 606 Apr 01/04
4. Procedure _________ Subtask 05-28-30-210-058 R R
A. Do a general visual inspection of the emergency exit doors (zones 834 and 844). This inspection includes the door stops on the fuselage side, the door seals and the scuff plates. - Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-28-30-410-058 A. Close Access (1) Close the emergency exit doors 834, 844, (Ref. TASK 52-20-00-410801). Subtask 05-28-30-860-052 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-28-30 SROS
Page 607 Jul 01/05
TASK 05-28-30-200-810 Zonal Inspection of Emergency Exit 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-834-02 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 ------------------------------------------------------------------------------25-23-53-000-801 25-23-53-400-801
Removal of the Lining of the Emergency Exit Door Installation of the Lining of the Emergency Exit Door
3. __________ Job Set-up R
**ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499,
R
Subtask 05-28-30-010-059-A
R
A. Get Access
R R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at zone 834(844).
R
(2) Remove the access panels.
R R
(a) For the emergency exit 834: 834KZ, 834LZ, 834MZ, 834NZ, 834PZ, 834QZ, (Ref. TASK 25-23-53-000-801).
R R
(b) For the emergency exit 844: 844KZ, 844LZ, 844MZ, 844NZ, 844PZ, 844QZ, (Ref. TASK 25-23-53-000-801).
EFF : ALL 05-28-30 SROS
Page 608 Jul 01/06
R
(3) Lift the insulation blankets. **ON A/C 301-399, 701-749, Subtask 05-28-30-010-059 A. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at zone 834(844). (2) Remove the access panels. (a) For the emergency exit 834: 834AZ, 834BZ, 834CZ, 834DZ, 834EZ, 834FZ, 834GZ, 834HZ, 834JZ, (Ref. TASK 25-23-53-000-801). (b) For the emergency exit 844: 844AZ, 844BZ, 844CZ, 844DZ, 844EZ, 844FZ, 844GZ, 844HZ, 844JZ, (Ref. TASK 25-23-53-000-801). (3) Lift the insulation blankets. **ON A/C ALL 4. Procedure _________ Subtask 05-28-30-210-059 A. Do a general visual inspection of the emergency exits (zones 834 and 844). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring) are attached correctly. 5. Close-up ________
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 401-449, 451-499,
R
Subtask 05-28-30-410-059-A
R
A. Close Access
R
(1) Put in position back the insulation.
R
(2) Install the access panels.
R R
(a) For the emergency exit 834: 834KZ, 834LZ, 834MZ, 834NZ, 834PZ, 834QZ, (Ref. TASK 25-23-53-400-801).
EFF : ALL 05-28-30 SROS
Page 609 Jul 01/06
R R
(b) For the emergency exit 844: 844KZ, 844LZ, 844MZ, 844NZ, 844PZ, 844QZ, (Ref. TASK 25-23-53-400-801). **ON A/C 301-399, 701-749, Subtask 05-28-30-410-059 A. Close Access (1) Put in position back the insulation. (2) Install the access panels. (a) For the emergency exit 834: 834AZ, 834BZ, 834CZ, 834DZ, 834EZ, 834FZ, 834GZ, 834HZ, 834JZ, (Ref. TASK 25-23-53-400-801). (b) For the emergency exit 844: 844AZ, 844BZ, 844CZ, 844DZ, 844EZ, 844FZ, 844GZ, 844HZ, 844JZ, (Ref. TASK 25-23-53-400-801). **ON A/C ALL Subtask 05-28-30-860-053 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-28-30 SROS
Page 610 Jul 01/06
TASK 05-28-30-200-811 R
Zonal Inspection of Emergency Exit (Doors 3) 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-834-03 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R
No specific
1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------25-23-48-000-801 25-23-48-400-801
Removal of the Door Frame Linings of the Emergency Exit Installation of the Door Frame Linings of the Emergency Exit Removal of the Lining of the Emergency Exit Door Installation of the Lining of the Emergency Exit Door
25-23-53-000-801 25-23-53-400-801 R 3. __________ Job Set-up R R
Subtask 05-28-30-010-060-B A. Get Access
R R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the zone 834(844).
R
(2) Remove the access panels.
R R
(a) For the emergency exit 834: 834KZ, 834LZ, 834MZ, 834NZ, 834PZ, 834QZ, (Ref. TASK 25-23-53-000-801).
EFF : ALL 05-28-30 SROS
Page 611 Apr 01/04
R R
(b) For the emergency exit 844: 844KZ, 844LZ, 844MZ, 844NZ, 834PZ, 834QZ, (Ref. TASK 25-23-53-000-801).
R
(3) Remove the frame lining panels.
R R
(a) For the emergency exit 834: 261TX, 261UX, 261XX, 261YX, (Ref. TASK 25-23-48-000-801).
R R
(b) For the emergency exit 844: 262TX, 262UX, 262XX, 262YX, (Ref. TASK 25-23-48-000-801).
R
(4) Lift the insulation. 4. Procedure _________
R R R R R R R
Subtask 05-28-30-210-060-B A. Do a general visual inspection of the emergency exits 834 and 844 (Type 1). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring) are attached correctly. 5. Close-up ________
R R
Subtask 05-28-30-410-060-B A. Close Access
R
(1) Put in position back the insulation.
R
(2) Install the frame lining panels.
R R
(a) For the emergency exit 834: 261TX, 261UX, 261XX, 261YX, (Ref. TASK 25-23-48-400-801).
R R
(b) For the emergency exit 844: 262TX, 262UX, 262XX, 262YX, (Ref. TASK 25-23-48-400-801).
R
(3) Install the access panels
R R
(a) For the emergency exit 834: 834KZ, 834LZ, 834MZ, 834NZ, 834PZ, 834QZ, (Ref. TASK 25-23-53-400-801).
R R
(b) For the emergency exit 844: 844KZ, 844LZ, 844MZ, 844NZ, 844PZ, 844QZ, (Ref. TASK 25-23-53-400-801).
EFF : ALL 05-28-30 SROS
Page 612 Apr 01/04
R R
Subtask 05-28-30-860-060-A B. Put the Aircraft back to its Initial Configuration
R R
(1) Remove all the fixtures, tools, test and support equipment used during this procedure.
R R
(2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-28-30 SROS
Page 613 Jan 01/05
TASK 05-28-30-200-812 Zonal Inspection of MID Passenger/Crew Doors 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-832-01 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 ------------------------------------------------------------------------------52-10-00-010-801 52-10-00-410-801
Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door
3. __________ Job Set-up Subtask 05-28-30-010-061 A. Get Access R R
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at zone 832(842). (2) Open the MID passenger/crew doors 832, 842, (Ref. TASK 52-10-00-010801).
EFF : ALL 05-28-30 SROS
Page 614 Jan 01/06
4. Procedure _________ Subtask 05-28-30-210-061 R R R
A. Do a general visual inspection of the MID passenger/crew doors (this includes door stops on fuselage side, door seals and scuff plates) (zones 832 and 842). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-28-30-410-061 A. Close Access (1) Close the MID passenger/crew doors 832, 842, (Ref. TASK 52-10-00-410801). Subtask 05-28-30-860-058 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-28-30 SROS
Page 615 Jan 01/06
TASK 05-28-30-200-813 Zonal Inspection of MID Passenger/Crew Door 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-832-02 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
25-23-51-000-801
R R
25-23-51-400-801 25-80-00-000-801 25-80-00-400-801 52-10-00-010-801 52-10-00-410-801
Removal of the Lining of the Middle Passenger/Crew Door(s) Installation of the Lining of the Middle Passenger/Crew Door(s) Removal of the Insulation Blankets Installation of the Insulation Blankets Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door
3. __________ Job Set-up Subtask 05-28-30-010-062 A. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the MID passenger/crew doors 832 and 842. (2) Open the MID passenger/crew doors 832 and 842 (Ref. TASK 52-10-00010-801).
EFF : ALL 05-28-30 SROS
Page 616 Jan 01/06
(3) Remove the access panels:
R
(a) For the MID passenger/crew door 832 (left side): 832AZ, 832BZ, 832CZ, 832DZ, 832EZ, 832FZ, 832GZ, 832HZ, 832JZ (Ref. TASK 25-23-51-000-801).
R
(b) For the MID passenger/crew door 842 (right side): 842AZ, 842BZ, 842CZ, 842DZ, 842EZ, 842FZ, 842GZ, 842HZ, 842JZ (Ref. TASK 25-23-51-000-801). (4) Lift or remove the insulation blankets (Ref. TASK 25-80-00-000-801). 4. Procedure _________ Subtask 05-28-30-210-062
R
A. Inspection
R R R
(1) Do a general visual inspection of the MID passenger/crew doors (zones 832 and 842).
R
(2) Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. - all the installations (wiring) are attached correctly.
R
5. Close-up ________ Subtask 05-28-30-410-062 A. Close Access R
(1) Install the insulation blankets (Ref. TASK 25-80-00-400-801). (2) Install the access panels:
R
(a) For the MID passenger/crew door 832 (left side): 832AZ, 832BZ, 832CZ, 832DZ, 832EZ, 832FZ, 832GZ, 832HZ, 832JZ (Ref. TASK 25-23-51-400-801).
R R
(b) For the MID passenger/crew door 842 (right side): 842AZ, 842BZ, 842CZ, 842DZ, 842EZ, 842FZ, 842GZ, 842HZ, 842JZ (Ref. TASK 25-23-51-400-801).
R
(3) Close the passenger/crew doors 832 and 842 (Ref. TASK 52-10-00-410801).
EFF : ALL 05-28-30 SROS
Page 617 Jul 01/04
Subtask 05-28-30-860-059 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-28-30 R SROS
Page 618 Apr 01/04
TASK 05-28-30-200-814 Zonal Inspection of AFT Passenger/Crew Doors 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-833-01 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 ------------------------------------------------------------------------------52-10-00-010-801 52-10-00-410-801
Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door
3. __________ Job Set-up Subtask 05-28-30-010-063 A. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the aft passenger/crew doors 833 and 843. (2) Open the passenger/crew doors 833 and 843 (Ref. TASK 52-10-00-010801).
EFF : ALL 05-28-30 R SROS
Page 619 Jan 01/06
4. Procedure _________ Subtask 05-28-30-210-063 R R R
A. Do a general visual inspection of the AFT passenger/crew doors (this includes door stops on fuselage side, door seals and scuff plates) (zones 833 and 843). Make sure that there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see. 5. Close-up ________ Subtask 05-28-30-410-063 A. Close Access (1) Close the passenger/crew doors 833 and 843 (Ref. TASK 52-10-00-410801). Subtask 05-28-30-860-050 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-28-30 SROS
Page 620 Jan 01/06
TASK 05-28-30-200-815 Zonal Inspection of AFT Passenger/Crew Door 1. __________________ Reason for the Job Refer to the MPD TASK: ZL-833-02 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
25-23-52-000-802 25-23-52-400-802 25-80-00-000-801 25-80-00-400-801 52-10-00-010-801 52-10-00-410-801
Removal of the Lining of the Aft Passenger/Crew Door Installation of the Lining of the Aft Passenger/Crew Door Removal of the Insulation Blankets Installation of the Insulation Blankets Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door
3. __________ Job Set-up Subtask 05-28-30-010-064 A. Get Access (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the passenger/crew doors 833 and 843. (2) Open the passenger/crew doors 833 and 843 (Ref. TASK 52-10-00-010801).
EFF : ALL 05-28-30 SROS
Page 621 Jan 01/06
(3) Remove the access panels: (a) For the AFT passenger/crew door 833 (left side): 833AZ, 833BZ, 833CZ, 833DZ, 833EZ, 833FZ, 833GZ, 833HZ, 833JZ (Ref. TASK 25-23-52-000-802). (b) For the AFT passenger/crew door 843 (right side): 843AZ, 843BZ, 843CZ, 843DZ, 843EZ, 843FZ, 843GZ, 843HZ, 843JZ (Ref. TASK 25-23-52-000-802). (4) Lift or remove the insulation blankets (Ref. TASK 25-80-00-000-801). 4. Procedure _________ Subtask 05-28-30-210-064 A. Do a general visual inspection of the passenger/crew doors (zones 833 and 843). Make sure that: - there is no damage (corrosion, leaks or cracks) on all the parts of the components and the structure you can see - all the installations (wiring) are attached correctly. 5. Close-up ________ Subtask 05-28-30-410-064 A. Close Access (1) Install the insulation blankets (Ref. TASK 25-80-00-400-801) (2) Install the access panels: R
(a) For the AFT passenger/crew door 833 (left side): 833AZ, 833BZ, 833CZ, 833DZ, 833EZ, 833FZ, 833GZ, 833HZ, 833JZ (Ref. TASK 25-23-52-400-802). (b) For the AFT passenger/crew door 843 (right side): 843AZ, 843BZ, 843CZ, 843DZ, 843EZ, 843FZ, 843GZ, 843HZ, 843JZ (Ref. TASK 25-23-52-400-802). (3) Close the passenger/crew doors 833 and 843 (Ref. TASK 52-10-00-410801).
R EFF : ALL 05-28-30 SROS
Page 622 Jul 01/04
Subtask 05-28-30-860-051 B. Put the Aircraft back to its Initial Configuration (1) Remove all the fixtures, tools, test and support equipment used during this procedure. (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-28-30 R SROS
Page 623 Jul 01/04
UNSCHEDULED MAINTENANCE CHECKS - DESCRIPTION AND OPERATION __________________________________________________________ R R R R R R R R R R R R R R R R R R R R R R R
1. _______ General Section 05-51 gives the checks and inspections that you must do after the aircraft has gone through special or abnormal conditions, such as: - hard/overweight landing - landing-gear-down limit speed exceeded - flap/slat limit speed exceeded - bird or hail strike - tire burst or tread throw - brake emergency application or overheat - flight in excessive turbulence or in excess of VMO - lightning strike or static discharge - engine bird strike or slush ingestion - tail runway impact - NLG towing overload or overrun - NLG steering angle exceeded - leaving runway or taxiway - flight through dust storm or dust contamination on ground - flight through volcanic ash or volcanic ash contamination on ground - engine failure - engine side loads - mercury spillage - abnormal pax/crew door movement. It also contains the manufacturers recommendations for non revenue flight requirements following maintenance actions (REF. ATA 05-59).
EFF : ALL 05-50-00 SROS
Page 1 Jan 01/07
UNSCHEDULED MAINTENANCE CHECKS - MAINTENANCE PRACTICES ______________________________________________________ TASK 05-50-00-790-801 Leaks - Permitted Values 1. __________________ Reason for the Job This task gives you all the fluid leak measurement procedures for flight control, fuel, hydraulic, landing gear, cargo door and power plant systems. 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------28-11-00-280-802 29-00-00-790-801 71-00-00-860-817 71-71-00-200-801
Fuel Tank Leaks - General Information Check of the External Leakage of Hydraulic Components Engine Operation Limits and Guidelines Leakage Rates at Drains Mast
3. __________ Job Set-up Subtask 05-50-00-869-050 A. Not applicable. 4. Procedure _________ R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-50-00-360-050 A. Measurement of Leaks (1) Measurement of hydraulic system leaks (Ref. TASK 29-00-00-790-801). (2) Measurement of flight-control system leaks (Ref. TASK 29-00-00-790801). (3) Measurement of fuel system leaks (Ref. TASK 28-11-00-280-802).
EFF : ALL 05-50-00 SROS
Page 201 Jul 01/05
(4) Measurement of landing-gear system leaks (Ref. TASK 29-00-00-790801). (5) Measurement of cargo door leaks (Ref. TASK 29-00-00-790-801). (6) Measurement of power-plant system leaks (Ref. TASK 71-00-00-860-817). **ON A/C 701-749, Subtask 05-50-00-360-050-A A. Measurement of Leaks (1) Measurement of hydraulic system leaks (Ref. TASK 29-00-00-790-801). (2) Measurement of flight-control system leaks (Ref. TASK 29-00-00-790801). (3) Measurement of fuel system leaks (Ref. TASK 28-11-00-280-802). (4) Measurement of landing-gear system leaks (Ref. TASK 29-00-00-790801). (5) Measurement of cargo door leaks (Ref. TASK 29-00-00-790-801). (6) Measurement of power-plant system leaks (Ref. TASK 71-71-00-200-801).
R EFF : 001-049, 201-249, 251-252, 255-299, 05-50-00 301-399, 401-449, 451-499, 701-749, SROS
Page 202 Jul 01/05
INSPECTIONS - DESCRIPTION AND OPERATION _______________________________________ R R R R R R
1. _______ General This section contains the inspections that are necessary after an incident or flight in abnormal conditions; and will in most cases, be called for as a result of flight crew report. If there is no inspection in this section applicable to incident or abnormal flight conditions that occurred, operators must tell Airbus and make a request for more instructions.
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A. Inspection Coverage It is not possible to give precise details of the inspection procedure to be adopted after every incident because of the wide variations of weight, speed, nature and direction of loads, weather conditions and component failure patterns. Therefore these inspections have been written for the worst possible case. In order to gain an indication of the severity of the incident and to facilitate rapid location of primary damage it is essential that full information be obtained from the flight crew. Therefore before you start an inspection, consult the crew and get data on the following: - Weather conditions - Aircraft speed and flight attitude - Aircraft weight and fuel distribution - Landing : was touchdown straight, drifting, wing low, nose up or down? - Was any noise of impact or indicative of structure or component failure heard? - Applicable instrument indications Printout of the maintenance data recorder-tape will give valuable additional data and indication of system malfunction.
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B. Inspection Sequence To permit simultaneous inspection of several areas of the aircraft the inspection has been divided into a number of Packages. For example: Inspection after Hail Impact requires on Phase 1 a complete airframe external check. Therefore this is divided into four major zones: fuselage, wings, nacelles/pylons and stabilizers. These major zones are further divided into smaller zones or major components. The small zones are then broken down into items, which can be individually signed off when inspection is completed. The inspections are divided into three phases: - Phase 1: is a general inspection for primary damage and indication of remote damage and is mainly external. - Phase 2: is a more detailed inspection and is mainly internal. It can be necessary to remove some components. - Phase 3: is a very detailed inspection with component removal and strip down.
EFF : ALL 05-51-00 SROS
Page 1 Jan 01/07
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If the Phase 1 inspection shows no damage, no further examination is necessary. If Phase 1 shows damage then Phase 2 must be done. If Phase 2 shows damage then Phase 3 must be done. C. Inspection Presentation (Ref. Fig. 001) The layout of the inspection form is as follows: - columns 1, 3, 4, 5, 6 and 8 are explained on the figure - columns 2 and 7 are provided for use by the operators inspectors, if they wish to use them, for inspection intensity code and accomplishment signature. The forms may thus be photo-copied, used as job cards and then filed with the aircraft technical record on completion.
EFF : ALL 05-51-00 SROS
Page 2 Jan 01/07
Inspection Layout Table Figure 001 EFF : ALL 05-51-00 SROS
Page 3 Apr 01/98
INSPECTION AFTER HARD/OVERWEIGHT LANDING - INSPECTION/CHECK ___________________________________________________________ R
TASK 05-51-11-200-802
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Inspection after Hard/Overweight Landing
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1. __________________ Reason for the Job
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After a flight crew report of a hard/overweight landing, you must do the following inspection before the subsequent flight. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment
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------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R R R R
No specific No specific No specific FOR FIN 4030EM2 No specific
R
safety barriers warning notices wheel chocks 1 ACCESS PLATFORM 17M (56 FT) - ADJUSTABLE
B. Referenced Information
R R R
------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R R R R R R R R R R R R R R
07-11-00-581-801 23-71-00-710-801 24-38-00-740-801 24-41-00-861-801 24-41-00-862-801 27-50-00-866-801 27-50-00-866-802 27-54-00-200-801 27-54-00-710-801 27-60-00-866-801 27-60-00-866-802 27-80-00-866-801
Lifting of the Aircraft for Maintenance Operations Operational Test of the CVR and of the Recording on all Four Channels BITE Test of the BCL (1PB1, 1PB2, 1PB3) Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Extension of the Flaps on the Ground Retraction of the Flaps on the Ground Detailed Visual Inspection of the Flap Transmission Assy Operational Test of the Flap System Extension of the Spoilers for Maintenance Retraction of the Spoilers after Maintenance Extension of the Slats on the Ground
EFF : ALL 05-51-11 SROS
Page 601 Jan 01/07
------------------------------------------------------------------------------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 R R R R R R R R R R R R R R R R
27-80-00-866-802 28-25-00-650-803 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 31-33-00-710-803 31-36-00-200-803 32-00-00-481-801 32-11-00-220-801
32-11-00-220-802 32-12-00-010-801 32-12-00-410-801 32-22-00-010-801 32-22-00-410-801 32-31-00-710-801 49-12-00-200-801 57-56-11-000-801 57-56-11-000-802 57-56-11-000-803 71-00-00-000-803 71-00-00-000-805 71-00-00-700-834 71-00-00-720-821 71-13-00-010-802 71-13-00-010-805
Retraction of the Slats on the Ground To Drain the Remaining Fuel (Wing Tanks) 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) Operational Check for Digital Flight Data Recorder System by using MCDU Check of the Load-Report Parameter after Hard/Overweight Landing or Excessive Turbulence Installation of the Safety Devices on the Landing Gears Detailed Inspection of Main Gear Structure comprising: Main Fittings, Sliding Piston, Bogie Beam, Pitch Trimmer, Sidestay Assy, Lock Pins Assembly ... Check of Shock Absorber Nitrogen Charge Pressure Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance Functional Test of the Normal Extension and Retraction System Visual Check of APU Suspension System Including Shockmount Structure And Brackets Removal of the Movable Flap Track Fairing No. 2 Removal of the Movable Flap Track Fairing No. 3 Removal of the Movable Flap Track Fairing No. 4 Removal of the Engine Removal of the Demountable Power Plant Test No.7 The Engine Performance Test Test No. 9 - Power Assurance Test Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Open the Fan Cowl Doors
EFF : ALL 05-51-11 SROS
Page 602 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R R R R R R R R
78-30-00-410-801
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**ON A/C 002-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 701-749, Post SB 31-3091 For A/C 401-449,451-499,
R R R
05-51-11-991-054 05-51-11-991-057 05-51-11-991-058
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**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499,
R
05-51-11-991-005
R
**ON A/C 701-749,
R
05-51-11-991-005-A
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499,
R
05-51-11-991-009
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**ON A/C 701-749,
R
05-51-11-991-009-A
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499,
R
05-51-11-991-018
78-30-00-410-803 78-31-00-710-804 78-31-00-740-802 79-00-00-200-805 79-22-11-200-801 05-51-11-991-001
Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Close the Thrust Reverser Cowl Doors Thrust Reverser Cycling Test (MCDU) Test of the Thrust Reverser Deployment and Stowage (Engine not Running) Inspect Master Magnetic Chip Detector for Evidence of Abnormal Deposits Inspection of the Magnetic Chip Detector (5006EN) Fig. 601
Fig. 602 Fig. 603 Fig. 604
Fig. 605
Fig. 605A
Fig. 606
Fig. 606A
Fig. 607
EFF : ALL 05-51-11 SROS
Page 603 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
**ON A/C 701-749,
R
05-51-11-991-018-A
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499,
R
05-51-11-991-021
R
**ON A/C 701-749,
R
05-51-11-991-021-A
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499,
R
05-51-11-991-022
R
**ON A/C 701-749,
R
05-51-11-991-022-A
R
**ON A/C ALL
R R R R R R R R R R R R R R
05-51-11-991-023 05-51-11-991-025 05-51-11-991-026 05-51-11-991-027 05-51-11-991-028 05-51-11-991-029 05-51-11-991-030 05-51-11-991-031 05-51-11-991-032 05-51-11-991-033 FOR FIN 4030EM2 71-13-00-410-802 71-13-00-410-805
Fig. 607A
Fig. 608
Fig. 608A
Fig. 609
Fig. 609A
Fig. Fig. Fig. Fig. Fig. Fig. Fig. Fig. Fig. Fig.
610 611 612 613 614 615 616 617 618 619
Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Close the Fan Cowl Doors
EFF : ALL 05-51-11 SROS
Page 604 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R R
78-30-00-010-801
R
3. __________ Job Set-up
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Subtask 05-51-11-210-103
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78-30-00-010-803
Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Open the Thrust Reverser Cowl Doors
A. General
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(1) Definitions
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(a) A hard landing is: - a landing with a vertical the center of gravity or - a vertical speed (V/S) of weight less than 155 tons - a vertical speed (V/S) of weight more than or equal
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(b) An overweight landing is: - a landing at more than the maximum landing weight with a vertical acceleration of more than 1.4g at the center of gravity or - a landing at more than the maximum landing weight with a vertical speed (V/S) of more than 360 ft/min.
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acceleration of more than 1.75g at more than 600 ft/min for an A/C or more than 540 ft/min for an A/C to 155 tons.
(2) Inspection requirements
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(a) After a hard/overweight landing, it is necessary to do the hard/overweight landing inspection before the subsequent flight. To prevent inspection that is not necessary, when there is a suspected hard/overweight landing (flight crew report, damage found on the aircraft, etc.), it is possible to refer to the DFDRS landing impact parameters to know if the landing was a hard/overweight landing.
EFF : ALL 05-51-11 SROS
Page 605 Jan 01/07
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Subtask 05-51-11-941-056 B. Procedure to Confirm a Suspected Hard/Overweight Landing
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(1) Definition of a suspected Hard/Overweight Landing A suspected hard/overweight landing is a landing after which the flight crew makes a report of a hard/overweight landing.
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NOTE : It is the responsibility of the flight crew to make a report ____ if they think there was a hard/overweight landing.
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(2) Confirmation of a hard/overweight landing
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(a) After a suspected hard/overweight landing, and to prevent inspection that is not necessary, it is possible to refer to the DFDRS landing impact parameters to confirm that a hard/overweight landing occurred and that the inspection is necessary.
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NOTE : If you do not (or if you cannot) read the landing impact ____ parameters, you must do the inspection after hard/overweight landing before the subsequent flight. - To know the impact parameters, refer to the DFDRS readout. - If the landing impact parameters confirm hard/overweight landing, you must do the inspection after hard/overweight landing.
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Subtask 05-51-11-941-057 C. Inspection Preparation
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(1) We cannot give you accurate instruction for the inspection procedure to be done after each incident. This is because there can be important differences in the weight, the speed and the direction of the loads. Thus, before you start, we recommend that you get data:
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(a) From the crew about the landing conditions. For example, find out: - If the touchdown was on main gears or on main and nose gears or high pitch rate on nose gear - If the landing was straight, drifting, wing-low, tail or nose heavy - If the crew heard a noise possibly related to a structural failure.
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NOTE : After a hard/overweight landing, there are two possible ____ cases with their applicable requirements:
EFF : ALL 05-51-11 SROS
Page 606 Jan 01/07
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- Hard touchdown on In this case, the not necessary. - Hard touchdown on In this case, the
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main gears only: inspection of the nose gear area is nose and main gears: full inspection is necessary.
NOTE : Inspections are visual unless specified differently in the ____ text. Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures.
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(b) From the flight recorder (DFDR): - vertical acceleration, vertical speed (V/S), weight of the aircraft.
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(2) With these items of data, refer to the inspection definition diagram. (Ref. Fig. 601/TASK 05-51-11-991-001)
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**ON A/C 002-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 701-749, Post SB 31-3091 For A/C 401-449,451-499,
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Subtask 05-51-11-210-103-A
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A. General
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(1) Definitions
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(a) Delta VRTA Vertical acceleration Increment (DELTA VRTA): It is the difference between the Vertical Acceleration (VRTA) before the aircraft touch down (representing the aircraft actual lift) and the peak of VRTA after touch down.
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(b) RALR Radio Altitude Rate (RALR): It represents the aircraft vertical rate of descent.
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(c) A Hard Landing (GW <= MLW) is defined as: RALR < -10 ft/s and DELTA VRTA > 0.75 g or DELTA VRTA > 1.0 g or RALR < -13 ft/s
R EFF : ALL 05-51-11 SROS
Page 607 Jan 01/07
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Inspection - Definition Diagram Figure 601/TASK 05-51-11-991-001
EFF : ALL 05-51-11 SROS
Page 608 Jul 01/04
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(d) An Overweight Landing (GW > MLW) is defined as: RALR < -6 ft/s and DELTA VRTA > 0.5 g or DELTA VRTA > 0.7 g or VALR < -9 ft/s
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(e) Load report 15: - The ACMS load report 15 is not a hard landing detector. As stated in 3.B.(1), the primary source of identifying a suspected hard landing is the flight crew. Load report 15 data provides a snapshot of aircraft parameters before, at, and after an abnormal load condition either in the air or at touchdown. The report is generated for all landing, and is automatically printed or transmitted via ACARS, when one of its triggering conditions is met. These parameters give additional information which can be used by maintenance crew further to a flight crew report, in order to confirm if a hard landing occured and determine the need for, and level of, any subsequent inspection. Therefore, triggering of a load report 15 does not necessarily mean that a hard landing has occured. Nevertheless there have been cases on which load report 15 has triggered without pilot report and subsequent investigation has confirmed the hard landing. Hence Airbus recommend that whenever load report 15 is generated with trigger code 4XXX other than 4000, it should be systematically investigated and handled as a suspected hard landing and classified as detailed in subtask 05-51-11-941-052 B.(3) Action following a confirmed hard/overweight landing.
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NOTE : RALR, VRTA and GW are landing impact parameters indicated ____ on the FDIMU load report 15 (Ref. TASK 31-36-00-200-803).
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(2) Inspection requirements
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(a) After a hard / overweight landing, it is necessary to perform the hard / overweight landing inspection prior to the subsequent flight. To avoid unnecessary inspection, when there is a suspected hard / overweight landing (flight crew report, damage found on the aircraft, etc), it is possible to refer to the DFDRS / DMU / Load report 15 landing impact parameters to know if the landing was a hard / overweight landing.
R EFF : 002-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, 701-749, SROS
Page 609 Jan 01/07
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Subtask 05-51-11-941-056-A B. Procedure to confirm a Suspected Hard / Overweight Landing
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(1) Suspected Hard / Overweight Landing Definition. A suspected hard / overweight landing is a landing after which the flight crew make a reports of a hard / overweight landing.
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NOTE : It is the responsibility of the flight crew to make a report ____ if they think there was a hard / overweight landing.
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(2) Hard / Overweight landing confirmation After a suspected Hard / Overweight landing, and to avoid doing an unnecessary inspection, it is possible to consult the DFDRS or DMU / FDIMU load report 15 action chart to confirm that a hard / overweight landing occured and that the inspection is necessary.
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NOTE : If you do not (or if you cannot) read the landing impact ____ parameters from the load report 15, you must do the inspection after hard / overweight landing before the subsequent flight as in the instruction in paragraph 2.B.(3)(a)3 or paragraph 2.B.(3)(b)3. You can refer to the DMU / FDIMU load report 15 read out. You must do the inspection after hard / overweight landing.
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(3) Actions following a confirmed Hard / Overweight landing. (Ref. Fig. 602/TASK 05-51-11-991-054, 603/TASK 05-51-11-991-057, 604/TASK 05-51-11-991-058)
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(a) With GW <= MLW, the hard landing is split according to severity in 3 areas:
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1 _
ZONE 1: DELTA VRTA <= 1.0 g and RALR >= -10 ft/s or DELTA VRTA <= 0.75 g and |RALR| >= -13 ft/s No maintenance required
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2 _
ZONE 2: 1.0 g < DELTA VRTA <= 1.2 g and RALR >= -13 ft/s or 0.75 g < DELTA VRTA <= 1.2 g and -10 ft/s > RALR >= -13 ft/s Do this procedure: - perform the inspection as per paragraph 4 - download DFDR data (or QAR if available) - provide Airbus with DFDR raw data of the event, load report 15, pilot report, load trim sheet.
R EFF : 002-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, 701-749, SROS
Page 610 Jan 01/07
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Definition of Hard Landing (GW <= MLW) Figure 602/TASK 05-51-11-991-054
R EFF : 002-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, 701-749, SROS
Page 611 Jan 01/07
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Definition of Overweight Landing (GW > MLW) Figure 603/TASK 05-51-11-991-057
R EFF : 002-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, 701-749, SROS
Page 612 Jan 01/07
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Load Report 15 - Overweight / Hard Landing routes Figure 604/TASK 05-51-11-991-058
R EFF : 002-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, 701-749, SROS
Page 613 Jan 01/07
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- if no findings / damages as per paragraph 4., A/C can be returned temporarily to service for 30 days 100 Flight Cycles max (which ever occurs first) pending Airbus analysis of the event. - Airbus will assess the event for final clearance or further in structions.
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3 _
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ZONE 3: RALR < -13 ft/s or DELTA VRTA > 1.2 g Do this procedure: - Aircraft cannot return to service at this step without Airbus advice. - download DFDR data (or QAR if available) - immediately contact Airbus and provide DFDR raw data of the event, load report 15, pilot report, load trim sheet. - perform inspection as per paragraph 4 and report any findings / damages. - Airbus will analyse the event to assess if the aircraft can return to service.
(b) With GW > MLW, the overweight landing is described as follows:
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1 _
ZONE 1: DELTA VRTA <= 0.7 g and RALR >= -6 ft/s or DELTA VRTA <= 0.5 g and RALR >= -9 ft/s No maintenance required
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2 _
ZONE 2: 0.7 g < DELTA VRTA <= 0.8 g and RALR > -9 ft/s or 0.5 g < DELTA VRTA <= 0.8 g and -6 ft/s > RALR >= -9 ft/s Do this procedure: - perform the inspection as per paragraph 4 - download DFDR data (or QAR if available) - provide Airbus with DFDR raw data of the event, load report 15, pilot report, load trim sheet. - if no findings / damages as per paragraph 4., A/C can be returned temporarily to service for 30 days 100 Flight Cycles max (which ever occurs first) pending Airbus analysis of the event. - Airbus will assess the event for final clearance or further instructions.
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3 _
ZONE 3: RALR < -9 ft/s or DELTA VRTA > 0.8 g Aircraft cannot return to service at this step without Airbus advice Do this procedure: - download DFDR data (or QAR if available)
R EFF : 002-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, 701-749, SROS
Page 614 Jan 01/07
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- immediately contact Airbus and provide DFDR raw data of the event, load report 15, pilot report, load trim sheet. - perform inspection as per paragraph 4 and report any findings / damages. - Airbus will analyse the event to assess if the A/C can return to service. Subtask 05-51-11-941-057-A C. Inspection Preparation
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(1) We cannot give you accurate details of the inspection procedure to be applied after each incident. This is because there can be important variations in the weight, the speed and the direction of the loads. Thus, before you start, we recommand that you get information:
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(a) From the crew about the landing conditions. For exemple, find out: - if the touch down was on main gears or on main and nose gears or high pitch rate on nose gear. - if the landing was straight, drifting, wing-low, tail or nose heavy. - if the crew heard a noise possibly related to a structural failure.
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NOTE : After a hard / overweight landing, two cases have to be ____ considered with their applicable requirements: - hard touchdown on main gears only: In this case, the inspection of nose gear area is not required. - hard touchdown on nose and main gears: In this case the complete inspection is required.
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NOTE : Inspection are visual unless specified differently in the ____ text. Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures.
R EFF : 002-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, 701-749, SROS
Page 615 Jan 01/07
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**ON A/C ALL
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Subtask 05-51-11-941-058
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D. Safety Precautions
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(1) Put warning notices in the cockpit to tell persons not to operate the aircraft systems.
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(2) Install the safety devices on the landing gears (Ref. TASK 32-00-00481-801).
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(3) Put wheel chocks in position on the landing gears.
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(4) Lift the aircraft (Ref. TASK 07-11-00-581-801).
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NOTE : Lifting the aircraft is only necessary for the PHASE 2 ____ inspections.
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(5) Put the safety barriers in position.
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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 05-51-11-010-052
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E. Get Access
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(1) Open the main landing gear doors (Ref. TASK 32-12-00-010-801).
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(2) Open the nose landing gear doors (Ref. TASK 32-22-00-010-801).
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(3) Open the fan cowl doors (Ref. TASK 71-13-00-010-802). FOR 4030EM1 415BL, 416BR FOR 4030EM2 425BL, 426BR
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(4) Open the thrust reverser doors (Ref. TASK 78-30-00-010-801). FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR
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(5) Put an ACCESS PLATFORM 17M (56 FT) - ADJUSTABLE in position near the aircraft to do the inspection procedure.
R EFF : ALL 05-51-11 SROS
Page 616 Jan 01/07
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**ON A/C 701-749,
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Subtask 05-51-11-010-052-A
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E. Get Access
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(1) Open the main landing gear doors (Ref. TASK 32-12-00-010-801).
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(2) Open the nose landing gear doors (Ref. TASK 32-22-00-010-801).
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(3) Open the fan cowl doors (Ref. TASK 71-13-00-010-805). FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR
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(4) Open the thrust reverser doors (Ref. TASK 78-30-00-010-803). FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR
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(5) Put an ACCESS PLATFORM 17M (56 FT) - ADJUSTABLE in position near the aircraft to do the inspection procedure.
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**ON A/C ALL
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Subtask 05-51-11-860-052
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F. Aircraft Maintenance Configuration
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(1) Pressurize the Green hydraulic system (Ref. TASK 29-00-00-863-801).
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(2) Pressurize the Yellow hydraulic system (Ref. TASK 29-00-00-863-803).
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(3) Pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-802).
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(4) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801).
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(5) Fully extend the flaps (Ref. TASK 27-50-00-866-801)
R EFF : ALL 05-51-11 SROS
Page 617 Jan 01/07
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(6) Fully extend the slats (Ref. TASK 27-80-00-866-801).
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(7) Fully extend the spoilers (Ref. TASK 27-60-00-866-801).
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(8) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801).
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(9) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803).
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(10) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802).
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(11) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
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4. Procedure _________
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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 05-51-11-210-087
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A. Inspection of the Pylon (Ref. Fig. 605/TASK 05-51-11-991-005, 606/TASK 05-51-11-991-009, 607/TASK 05-51-11-991-018, 608/TASK 05-51-11-991-021, 609/TASK 05-51-11-991-022) (Ref. TASK 71-00-00-000-803), (Ref. TASK 28-25-00-650-803).
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NOTE : Inspections are visual unless specified differently in the text. ____ Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures.
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If there is damage on the aircraft structure, refer to the Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures. If it is necessary to open (remove) access panels and doors, examine them. Make sure that : - They are aligned correctly, - They have no distortion or cracks, - The paint is not damaged, - All the fasteners and safety devices are in the correct position
R EFF : ALL 05-51-11 SROS
Page 618 Jan 01/07
Inboard Engine-Pylon Station Figure 605/TASK 05-51-11-991-005
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EFF : 001-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, SROS
Page 619 Jan 01/07
Engine-Pylon Station Figure 605A/TASK 05-51-11-991-005-A
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EFF : 701-749, 05-51-11 SROS
Page 620 Jan 01/07
Pylon Box Figure 606/TASK 05-51-11-991-009
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EFF : 001-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, SROS
Page 621 Jan 01/07
Pylon Box Figure 606A/TASK 05-51-11-991-009-A
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EFF : 701-749, 05-51-11 SROS
Page 622 Jan 01/07
Engine-to-pylon Attach Fittings Figure 607/TASK 05-51-11-991-018
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R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, SROS
Page 623 Jan 01/07
Engine-to-pylon Attach Fittings Figure 607A/TASK 05-51-11-991-018-A
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R EFF : 701-749, 05-51-11 SROS
Page 624 Jan 01/07
Pylon-to-Wing Forward Attach-Fittings Figure 608/TASK 05-51-11-991-021
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R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, SROS
Page 625 Jan 01/07
Pylon-to-Wing Forward Attach Fittings Figure 608A/TASK 05-51-11-991-021-A
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R EFF : 701-749, 05-51-11 SROS
Page 626 Jan 01/07
Pylon-to-Wing Aft Attach-Fittings Figure 609/TASK 05-51-11-991-022
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R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, SROS
Page 627 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Engine Pylons | | | | | | | | | | | | | | | | A.| | Examine externally: | X | | | | | | | | the doors, all the pylon panels, the | | | | | | | | | secondary structure (forward and aft) | | | | | | | | | and the bottom fairing (forward, | | | | | | | | | center and aft) for: | | | | | | | | | - buckling, cracks and pulled or | | | | | | | | | missing fasteners. | | | | | | | | | | | | | | | | B.| | Examine the primary structure and | X | | | | | | | | pylon lower area for distortion | | | | | | | | | and cracks, the condition of the | | | | | | | | | paint, loose rivets, signs of | | | | | | | | | shearing. | | | | | | | | | | | | | | | | C.| | If you find damage during the | | | | | | | | | inspection of the Pylon: | | | | | | | | | | | | | | | | | | (1) Remove or open the access doors | | X | | | | | | | and panels. | | | | | | | | | (2) Examine the panels and the | | X | | | | | | | adjacent structure for | | | | | | | | | distortion, buckles, wrinkles or | | | | | | | | | tears. | | | | | | | | | - the plates have no buckles, | | | | | | | | | wrinkles or tears where they | | | | | | | | | are riveted to the panels. | | | | | | | | | (3) Do an internal inspection of the | | X | | | | | | | pylon box (primary structure) for | | | | | | | | | distortion. | | | | | | | | | (4) Examine the spars connected to | | X | | | | | | | the side panels for: | | | | | | | | | - correct condition and damage. | | | | | | | | | (5) Examine the attachment between | | X | | | | | | | the main ribs (1, 10, 12 and 18A),| | | | | | | | | the side panels, the upper and | | | | | | | | | lower spars for damage. | | | | | | | | | (6) Examine the fire protection | | X | | | | | | | system for damage, specially the | | | | | | | | | the attachments of the fire | | | | | | | | | extinguisher bottles and | | | | | | | | | extinguishing distribution pipes. | | | | | |
R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, SROS
Page 628 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (7) Examine the electrical cables, | | X | | | | | | | the hydraulic pipes, the fuel | | | | | | | | | pipes, the components of the | | | | | | | | | engine air-bleed system and | | | | | | | | | draining pipes for damage. | | | | | | | | | (8) Examine the different components | | | | | | | | | installed on the primary | | | | | | | | | structure. | | | | | | | | | | | | | | | | | | If you find damage: | | | | | | | | | (a) Remove the engine | | | X | | | | | | (Ref. TASK 71-00-00-000-803). | | | | | | | | | (b) Examine the engine-to-pylon | | | X | | | | | | attach fitting at the head of | | | | | | | | | Rib 1 (pyramid) and under Rib 10 | | | | | | | | | for: | | | | | | | | | - cracks, distortion, rupture and | | | | | | | | | signs of oxydation or burning. | | | | | | | | | (c) Remove the pylon-to-wing center | | | | | | | | | fillets. | | | | | | | | | (d) Do a detailed visual inspection | | | | | | | | | of the forward attach fitting | | | | | | | | | at Rib 12. | | | | | | | | | (e) Do a detailed visual inspection | | | X | | | | | | of the spigot between Rib 12 | | | | | | | | | and 13 for: | | | | | | | | | - damage buckling, cracks and | | | | | | | | | pulled or missing fasteners. | | | | | | | | | (f) Do a detailed visual inspection | | | X | | | | | | of the rear attach fitting at | | | | | | | | | Rib 18. | | | | | | | | | (g) Do a detailed visual inspection | | | X | | | | | | of the ball-bearings installed at | | | | | | | | | Rib 18A and examine the inner and | | | | | | | | | outer ball surfaces for cracks. | | | | | | | | | | | | | | | | | | If you find damage: | | | | | | | | | (h) Defuel the wing | | | X | | | | | | (Ref. TASK 28-25-00-650-803). | | | | | | | | | (i) Get access to the internal | | | X | | | | | | structure adjacent to Ribs 14, | | | | | | | | | 14A, 25 and 26. | | | | | | | | | Examine these items: | | | | | |
R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, SROS
Page 629 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - the rear face of the front spar | | | | | | | | | - the front face of the rear spar | | | | | | | | | - the pylon forward attachment | | | | | | | | | - the pylon aft attachment | | | | | | | | | - the stringers and brackets for: | | | | | | | | | - no damage, cracks, correct | | | | | | | | | condition of the paint and | | | | | | | | | sealant. | | | | | | | | | (j) Examine all the pipes and holes | | | X | | | | | | for: | | | | | | | | | - correct attachment and leakage. | | | | | | -------------------------------------------------------------------------------
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Subtask 05-51-11-210-088
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B. Inspection of the nacelles (Ref. TASK 78-31-00-710-804)
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NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Nacelles | | | | | | | | | | | | | | | | A.| | Do an external inspection of: | X | | | | | | | | the air intake cowls, the fan cowls | | | | | | | | | and the thrust reverser cowls for | | | | | | | | | distortion, cracks and delamination. | | | | | | | | | Make sure that: | | | | | | | | | - the paint is not cracked or flaked | | | | | | | | | - the rivets are not loose | | | | | | | | | - there are no signs of shearing. | | | | | | | | | | | | | | | | | | If you find damage during the | | | | | | | | | inspection : | | | | | | | | | | | | | | | | B.| | Do an internal inspection of the | | X | | | | | | | same items for damage. | | | | | |
R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, SROS
Page 630 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | | | | | | | | C.| | Examine all the cowl latches for | | X | | | | | | | damage. | | | | | | | | | Make sure that they operate | | | | | | | | | correctly. | | | | | | | | | If you find damage on the thrust | | | | | | | | | reverser cowls: | | | | | | | | | - do an operational test of the | | | X | | | | | | thrust reverser system. Make sure | | | | | | | | | that the thrust reversers can move | | | | | | | | | fully and freely | | | | | | | | | (Ref. TASK 78-31-00-710-804). | | | | | | -------------------------------------------------------------------------------
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Subtask 05-51-11-210-089
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C. Inspection of the Engines (Ref. TASK 71-00-00-720-821), (Ref. TASK 79-2211-200-801), (Ref. TASK 71-00-00-000-803)
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Engines | | | | | | | | | | | | | | | | A.| | Turn the fan rotor by hand | X | | | | | | | | Make sure that: | | | | | | | | | there is no bearing roughness, | | | | | | | | | unusual noises and bindings (high | | | | | | | | | rubbing of the seals and the | | | | | | | | | shrouds is normal). | | | | | | | | | | | | | | | | B.| | Examine the primary nozzle for damage | X | | | | | | | | (distortion, cracks, loose and | | | | | | | | | missing rivets, signs of shearing | | | | | | | | | or delamination). | | | | | | | | | Make sure that it is correctly | | | | | | | | | attached to the engine. | | | | | | | | | | | | | | | | C.| | Examine the nose cowl attachments | X | | | | | | | | to the fan case for distortion, | | | | | | | | | delamination, cracks. | | | | | | | | | Make sure that the fasteners are not | | | | | |
R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, SROS
Page 631 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | pulled or torn. | | | | | | | | | | | | | | | | D.| | If you find damage during the | | | | | | | | | inspection on the Engines: | | | | | | | | | | | | | | | | | | (1) Do a full inspection of the | | X | | | | | | | engine. | | | | | | | | | (2) If you find a minor seal or | | X | | | | | | | shroud interference the engine | | | | | | | | | is serviceable after you do a | | | | | | | | | satisfactory power assurance | | | | | | | | | check. | | | | | | | | | (3) After the test, examine the | | X | | | | | | | magnetic chip detectors and | | | | | | | | | the elements of the scavenge | | | | | | | | | oil filter. | | | | | | | | | Make sure that there are no | | | | | | | | | signs of bearing distress. | | | | | | | | | (Ref. TASK 79-22-11-200-801). | | | | | | | | | If you find damage: | | | | | | | | | - remove the engine | | | X | | | -------------------------------------------------------------------------------
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**ON A/C 701-749,
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Subtask 05-51-11-210-087-A
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A. Inspection of the Pylon (Ref. Fig. 605A/TASK 05-51-11-991-005-A, 606A/TASK 05-51-11-991-009-A, 607A/TASK 05-51-11-991-018-A, 608A/TASK 05-51-11-991-021-A, 609A/TASK 0551-11-991-022-A) (Ref. TASK 71-00-00-000-805), (Ref. TASK 28-25-00-650-803).
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NOTE : Inspections are visual unless specified differently in the text. ____ Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures.
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If there is damage on the aircraft structure, refer to the Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures. If it is necessary to open (remove) access panels and doors, examine them. Make sure that :
R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-11 301-399, 401-449, 451-499, 701-749, SROS
Page 632 Jan 01/07
Pylon-to-Wing Aft Attach-fittings Figure 609A/TASK 05-51-11-991-022-A
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R EFF : 701-749, 05-51-11 SROS
Page 633 Jan 01/07
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-
They are aligned correctly, They have no distortion or cracks, The paint is not damaged, All the fasteners and safety devices are in the correct position
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Engine Pylons | | | | | | | | | | | | | | | | A.| | Examine externally: | X | | | | | | | | the doors, all the pylon panels, the | | | | | | | | | secondary structure (forward and aft) | | | | | | | | | and the bottom fairing (forward, | | | | | | | | | center and aft) for: | | | | | | | | | - buckling, cracks and pulled or | | | | | | | | | missing fasteners. | | | | | | | | | | | | | | | | B.| | Examine the primary structure and | X | | | | | | | | pylon lower area for distortion | | | | | | | | | and cracks, the condition of the | | | | | | | | | paint, loose rivets, signs of | | | | | | | | | shearing. | | | | | | | | | | | | | | | | C.| | If you find damage during the | | | | | | | | | inspection of the pylon: | | | | | | | | | | | | | | | | | | (1) Remove or open the access doors | | X | | | | | | | and panels. | | | | | | | | | (2) Examine the panels and the | | X | | | | | | | adjacent structure for | | | | | | | | | distortion buckles, wrinkles or | | | | | | | | | tears: | | | | | | | | | - the plates have no buckles, | | | | | | | | | wrinkles or tears where they | | | | | | | | | are riveted to the panels. | | | | | | | | | (3) Do an internal inspection of the | | X | | | | | | | pylon box (primary structure) for | | | | | | | | | distortion. | | | | | | | | | (4) Examine the spars connected to | | X | | | | | | | the side panels for: | | | | | | | | | - correct condition and damage. | | | | | | | | | (5) Examine the attachment between | | X | | | | | | | the main ribs (1, 10, 12 and 18A),| | | | | | | | | the side panels, the upper and | | | | | | | | | lower spars for damage. | | | | | |
R EFF : 701-749, 05-51-11 SROS
Page 634 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (6) Examine the fire protection | | X | | | | | | | system for damage, specially the | | | | | | | | | the attachments of the fire | | | | | | | | | extinguisher bottles and | | | | | | | | | extinguishing distribution pipes. | | | | | | | | | (7) Examine the electrical cables, | | X | | | | | | | the hydraulic pipes, the fuel | | | | | | | | | pipes, the components of the | | | | | | | | | engine air-bleed system and | | | | | | | | | draining pipes for damage. | | | | | | | | | (8) Examine the different components | | | | | | | | | installed on the primary | | | | | | | | | structure. | | | | | | | | | | | | | | | | | | If you find damage: | | | | | | | | | (a) Remove the engine | | | X | | | | | | (Ref. TASK 71-00-00-000-805). | | | | | | | | | (b) Examine the engine-to-pylon | | | X | | | | | | attach fitting at the head of | | | | | | | | | Rib 1 (pyramid) and under Rib 10 | | | | | | | | | for: | | | | | | | | | - cracks distorsion rupture and | | | | | | | | | signs of oxydation or burning. | | | | | | | | | (c) Remove the pylon-to-wing center | | | | | | | | | fillets. | | | | | | | | | (d) Do a detailed visual inspection | | | | | | | | | of the forward attach fitting | | | | | | | | | at Rib 12. | | | | | | | | | (e) Do a detailed visual inspection | | | X | | | | | | of the spigot between Rib 12 | | | | | | | | | and 13 for: | | | | | | | | | - damage bulking, cracks and | | | | | | | | | pulled or missing fasteners. | | | | | | | | | (f) Do a detailed visual inspection | | | X | | | | | | of the rear attach fitting at | | | | | | | | | Rib 18. | | | | | | | | | (g) Do a detailed visual inspection | | | X | | | | | | of the ball-bearings installed at | | | | | | | | | Rib 18A and examine the inner and | | | | | | | | | outer ball surfaces for cracks. | | | | | | | | | | | | | | | | | | If you find damage: | | | | | | | | | (h) Defuel the wing | | | X | | |
R EFF : 701-749, 05-51-11 SROS
Page 635 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (Ref. TASK 28-25-00-650-803). | | | | | | | | | (i) Get access to the internal | | | X | | | | | | structure adjacent to Ribs 14, | | | | | | | | | 14A, 25 and 26. | | | | | | | | | Examine of these items: | | | | | | | | | - the rear face of the front spar | | | | | | | | | - the front face of the rear spar | | | | | | | | | - the pylon forward attachment | | | | | | | | | - the pylon aft attachment | | | | | | | | | - the stringers and brackets for: | | | | | | | | | - no damage, cracks, correct | | | | | | | | | condition of the paint and | | | | | | | | | sealant. | | | | | | | | | (j) Examine all the pipes and holes | | | X | | | | | | for: | | | | | | | | | - correct attachment and leakege | | | | | | -------------------------------------------------------------------------------
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Subtask 05-51-11-210-088-A
R R
B. Inspection of the nacelles (Ref. TASK 78-31-00-740-802)
R R R R
NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures.
R R R R R R R R R R R R R R R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Nacelles | | | | | | | | | | | | | | | | A.| | Do an external inspection of: | X | | | | | | | | the air intake cowls, the fan cowls | | | | | | | | | and the thrust reverser cowls for | | | | | | | | | distortion, cracks and delamination. | | | | | | | | | Make sure that: | | | | | | | | | - the paint is not cracked or flaked | | | | | | | | | - the rivets are not loose | | | | | | | | | - there are no signs of shearing. | | | | | | | | | | | | | | |
R EFF : 701-749, 05-51-11 SROS
Page 636 Jan 01/07
R R R R R R R R R R R R R R R R R R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | If you find damage during the | | | | | | | | | inspection : | | | | | | | | | | | | | | | | B.| | Do an internal inspection of the | | X | | | | | | | same items for damage. | | | | | | | | | | | | | | | | C.| | Examine all the cowl latches for | | X | | | | | | | damage. | | | | | | | | | Make sure that they operate | | | | | | | | | correctly. | | | | | | | | | If you find damage on the thrust | | | | | | | | | reverser cowls: | | | | | | | | | - do an operational test of the | | | X | | | | | | thrust reverser system. Make sure | | | | | | | | | that the thrust reversers can move | | | | | | | | | fully and freely | | | | | | | | | ( ref. TASK 78-31-00-740-802). | | | | | | -------------------------------------------------------------------------------
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Subtask 05-51-11-210-089-A
R R
C. Inspection of the Engines (Ref. TASK 71-00-00-700-834), (Ref. TASK 79-0000-200-805), (Ref. TASK 71-00-00-000-805)
R R R R R R R R R R R R R R R R R R R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Engines | | | | | | | | | | | | | | | | A.| | Turn the fan rotor by hand | X | | | | | | | | Make sure that: | | | | | | | | | there is no bearing roughness, | | | | | | | | | unusual noises and bindings (high | | | | | | | | | rubbing of the seals and the | | | | | | | | | shrouds is normal). | | | | | | | | | | | | | | | | B.| | Examine the primary nozzle for damage | X | | | | | | | | (distortion, cracks, loose and | | | | | | | | | missing rivets, signs of shearing | | | | | | | | | or delamination). | | | | | | | | | Make sure that it is correctly | | | | | | | | | attached to the engine. | | | | | |
R EFF : 701-749, 05-51-11 SROS
Page 637 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | | | | | | | | C.| | Examine the nose cowl attachments | X | | | | | | | | to the fan case for distortion, | | | | | | | | | delamination, cracks. | | | | | | | | | Make sure that the fasteners are not | | | | | | | | | pulled or torn. | | | | | | | | | | | | | | | | D.| | If you find damage during the | | | | | | | | | inspection on the Engines: | | | | | | | | | | | | | | | | | | (1) Do a full inspection of the | | X | | | | | | | engine. | | | | | | | | | (2) If you find a minor seal or | | X | | | | | | | shroud interference the engine | | | | | | | | | is serviceable after you do a | | | | | | | | | satisfactory power assurance | | | | | | | | | check. | | | | | | | | | (3) After the test, examine the | | X | | | | | | | magnetic chip detectors and | | | | | | | | | the elements of the scavenge | | | | | | | | | oil filter. | | | | | | | | | Make sure that there are no | | | | | | | | | signs of bearing distress. | | | | | | | | | (Ref. TASK 79-00-00-200-805). | | | | | | | | | If you find damage: | | | | | | | | | - remove the engine | | | X | | | -------------------------------------------------------------------------------
R
**ON A/C ALL
R
Subtask 05-51-11-210-090
R R R
D. Inspection of the Landing Gears (Ref. Fig. 610/TASK 05-51-11-991-023) (Ref. TASK 32-11-00-220-801), (Ref. TASK 32-11-00-220-802).
R R R R
NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures.
R EFF : ALL 05-51-11 SROS
Page 638 Jan 01/07
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 R R R R R R R R R R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Main Landing Gear | | | | | | | | | | | | | | | | | | Do a detailed inspection of these | X | | | | | | | | parts: | | | | | | | | | - the MLG leg assembly | | | | | | | | | - the MLG side stay assembly | | | | | | | | | - the articulating link | | | | | | | | | - the bogie beam assembly | | | | | | | | | - the bogie alignement pitch trimmer | | | | | | | | | - the torque links | | | | | | | | | - the brake rod | | | | | | | | | Make sure that there is no: | | | | | | | | | - distortion | | | | | | | | | - neckings | | | | | | | | | - damage to protective finish | | | | | | | | | - cracking | | | | | | | | | - excessive wear | | | | | | | | | - fretting | | | | | | | | | - scores, dents and burrs | | | | | | | | | | | | | | | | B.| | Make sure that the MLG sefety lock | X | | | | | | | | can be installed easily. | | | | | | | | | | | | | | | | C.| | Examine the wheels and the tires for | X | | | | | | | | unusual damage or distortion. | | | | | | | | | | | | | | | | D.| | Do a detailed visual inspection of | X | | | | | | | | the main gear for damage or distortion| | | | | | | | | at static and dynamic joints | | | | | | | | | (Ref. TASK 32-11-00-220-801). | | | | | | | | | | | | | | | | E.| | Remove and do a detailed inspection | | X | | | | | | | of the MLG lower articulating link. | | | | | | | | | Measure the dimention z between the | | | | | | | | | hole centers. | | | | | | | | | NOTE: If the distance is more than | | | | | | | | | 599.05 mm (23.5846 in.), you | | | | | | | | | must tell Airbus and wait for | | | | | | | | | instructions. | | | | | | | | | | | | | | | | | | If you find damage or distortion, or | | | | | | | | | if you think that a distortion | | | | | | | | | occured. | | | | | |
R EFF : ALL 05-51-11 SROS
Page 639 Jan 01/07
Main Landing Gear Figure 610/TASK 05-51-11-991-023- 14 (SHEET 1)
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R EFF : ALL 05-51-11 SROS
Page 640 Jan 01/07
Main Landing Gear Figure 610/TASK 05-51-11-991-023- 24 (SHEET 2)
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R EFF : ALL 05-51-11 SROS
Page 641 Jan 01/07
Main Landing Gear Figure 610/TASK 05-51-11-991-023- 34 (SHEET 3)
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R EFF : ALL 05-51-11 SROS
Page 642 Jan 01/07
Main Landing Gear Figure 610/TASK 05-51-11-991-023- 44 (SHEET 4)
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R EFF : ALL 05-51-11 SROS
Page 643 Jan 01/07
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 R R R R R R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | | | | | | | | | | (1) Do a check of these parts: | | X | | | | | | | - main gear complete | | | | | | | | | - main fitting | | | | | | | | | - side stay assembly | | | | | | | | | - shock absorber | | | | | | | | | - pitch trimmer and articulating | | | | | | | | | link | | | | | | | | | - bogie beam | | | | | | | | | - axles. | | | | | | | | | If you can isolate the source of | | | | | | | | | the damage or distortion. | | | | | | | | | | | | | | | | | | (2) Remove the applicable primary | | | X | | | | | | component for maintenance. | | | | | | | | | | | | | | | | | | (3) Do a pressure/extension check of | | X | | | | | | | the shock absorber. | | | | | | | | | (Ref. TASK 32-11-00-220-802) | | | | | | | | | | | | | | | | | | | | | | | | |2. | | Inspection of the Main Gear Fittings | | | | | | | | | | | | | | | | A.| | Do a detailed visual inspection of | X | | | | | | | | these parts (and their attachment | | | | | | | | | points): | | | | | | | | | - the forward pintle-pin fitting | | | | | | | | | - the rear pintle-pin fitting | | | | | | | | | - the gear rib 6 | | | | | | | | | - the bellcrank of the main gear | | | | | | | | | actuator | | | | | | | | | - the side stay attachment fitting | | | | | | | | | - the main gear actuator fittings. | | | | | | | | | Make sure that: | | | | | | | | | - there are no cracks, damage or | | | | | | | | | distortion | | | | | | | | | - the paint is not damaged | | | | | | | | | - the sealant is in correct condition | | | | | | | | | - there are no fluid leaks (fuel | | | | | | | | | where applicable). | | | | | | | | | | | | | | | | B.| | If there is damage or distortion at | | | | | | | | | the rear spar, get access to the fuel | | | | | |
R EFF : ALL 05-51-11 SROS
Page 644 Jan 01/07
R R R R R R R R R R R R R R R R R R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | tank (adjacent to the applicable area)| | | | | | | | | | | | | | | | | | (1) Do a detailed visual inspection | | X | | | | | | | of the internal structure adjacent| | | | | | | | | to the external damage. | | | | | | | | | Make sure that: | | | | | | | | | - there is no damaged paint | | | | | | | | | - there are no cracks in the | | | | | | | | | structure | | | | | | | | | - the sealant and the sealant bead| | | | | | | | | are in the correct condition | | | | | | | | | - the fasteners are correct | | | | | | | | | - the secondary structure, ribs, | | | | | | | | | riblets, stringers, brackets | | | | | | | | | and plates are not damaged | | | | | | | | | - the pipes, electrical cables | | | | | | | | | and raceways are not damaged. | | | | | | -------------------------------------------------------------------------------
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Subtask 05-51-11-210-091
R R
E. Inspection of the Nose Landing Gear (Ref. Fig. 611/TASK 05-51-11-991-025, 612/TASK 05-51-11-991-026)
R R R R
NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures.
R R R R R R R R R R R R R R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Nose Landing Gear | | | | | | | | | | | | | | | | A.| | Examine the wheels and tires for | X | | | | | | | | unusual damage or distortion. | | | | | | | | | (Ref. TASK 32-41-00-210-802) | | | | | | | | | | | | | | | | B.| | Do a detailed visual inspection of | X | | | | | | | | these parts: | | | | | | | | | - the NLG leg assembly | | | | | | | | | - the NLG drag stay assembly | | | | | |
R EFF : ALL 05-51-11 SROS
Page 645 Jan 01/07
Nose Landing Gear Figure 611/TASK 05-51-11-991-025
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R EFF : ALL 05-51-11 SROS
Page 646 Jan 01/07
Nose Landing-Gear Section between FR11 and FR17 Figure 612/TASK 05-51-11-991-026
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R EFF : ALL 05-51-11 SROS
Page 647 Jan 01/07
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 R R R R R R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - the torque links | | | | | | | | | Make sure that there is no: | | | | | | | | | - distortion | | | | | | | | | - necking | | | | | | | | | - damage to protective finish | | | | | | | | | - cracking | | | | | | | | | - excessive wear | | | | | | | | | - fretting | | | | | | | | | - scores, dents and burrs. | | | | | | | | | | | | | | | | | | If you find damage or distortion, or | | | | | | | | | if you think that a distortion | | | | | | | | | occurred. | | | | | | | | | | | | | | | | | | (1) Do a check of these parts: | | X | | | | | | | - nose gear complete | | | | | | | | | - nose fitting | | | | | | | | | - drag stay assembly | | | | | | | | | - shock absorber | | | | | | | | | - axles. | | | | | | | | | If you can isolate the source of | | | | | | | | | damage or distortion: | | | | | | | | | (2) Remove the applicable primary | | | X | | | | | | component for maintenance. | | | | | | | | | (3) Do a pressure/extension check of | | X | | | | | | | the shock absorber. | | | | | | | | | (Ref. TASk 32-21-00-220-803) | | | | | | | | | | | | | | | | C.| | Make sure that the NLG safety lock | X | | | | | | | | can be installed easily. | | | | | | | | | | | | | | | | D.| | Examine the nose gear upper strut | X | | | | | | | | attachments between FR11 and FR11A. | | | | | | | | | Examine the area around the bearing, | | | | | | | | | the attachment of the fitting on the | | | | | | | | | forward frame and roof of the nose | | | | | | | | | wheel well and the link rods. | | | | | | | | | | | | | | | | E.| | Examin the nose gear actuating | X | | | | | | | | cylinder attachment fitting (FR13). | | | | | | | | | Examin the attachment of the actuating| | | | | | | | | cylinder fitting to the apper link | | | | | | | | | at FR13 and FR14. | | | | | |
R EFF : ALL 05-51-11 SROS
Page 648 Jan 01/07
R R R R R R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | | | | | | | | F. | Examin the nose gear leg attachments | X | | | | | | | | between FR16A and FR17. | | | | | | | | | Examine the attachments and the | | | | | | | | | longitudinal beams. | | | | | | -------------------------------------------------------------------------------
R
Subtask 05-51-11-210-101
R
F. Inspection of the Landing Gear Doors (Ref. TASK 32-31-00-710-801).
R R R R
NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures.
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
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Main Landing Gear | | | | | | | | | Doors | | | | | | | | | | | | | | | | A.| | Do an inspection of the doors, the | X | | | | | | | | hinges and the adjacent structure. | | | | | | | | | | | | | | | | | | If you find damage on the doors, the | | | | | | | | | attached parts or adjacent structure: | | | | | | | | | (1) Do a check of the into-wind and | | X | | | | | | | out-of-wind tolerances of the | | | | | | | | | doors with the landing gear | | | | | | | | | retracted | | | | | | | | | | | | | | | |2. | | Inspection of the Nose-Landing-Gear | | | | | | | | | Doors | | | | | | | | | | | | | | | | A.| | Do an inspection of the doors, the | X | | | | | | | | hinges and the adjacent structure. | | | | | | | | | | | | | | | | | | If you find damage on the doors, the | | | | | | | | | attached parts or adjacent structure: | | | | | | | | | (1) Do a check of the into-wind and | | X | | | | | | | out-of-wind tolerances of the | | | | | |
R EFF : ALL 05-51-11 SROS
Page 649 Jan 01/07
R R R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | doors with the landing gear | | | | | | | | | retracted | | | | | | -------------------------------------------------------------------------------
R
Subtask 05-51-11-210-093
R
G. Inspection of the Flap Operating Mechanism (Ref. TASK 27-54-00-200-801).
R R R R
NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures.
R R R R R R R R R R R R R R R R R R R R R R R R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Flap Operating | | | | | | | | | Mechanism | | | | | | | | | | | | | | | | A.| | Do an inspection of the flap | X | | | | | | | | operating mechanism | | | | | | | | | (Ref. TASK 27-54-00-200-80100). | | | | | | | | | | | | | | | | B.| | If you find damage on the Flap | | | | | | | | | operating mechanism: | | | | | | | | | (1) Remove the applicable components | | X | | | | | | | for maintenance. | | | | | | | | | | | | | | | | C.| | Do an inspection of the component | | X | | | | | | | attachments. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the component attachments | | | X | | | | | | and do an inspection of the | | | | | | | | | component attachment/structure | | | | | | | | | interface. | | | | | | -------------------------------------------------------------------------------
R EFF : ALL 05-51-11 SROS
Page 650 Jan 01/07
R R R
Subtask 05-51-11-210-094 H. Check after damage on the Flap-Track Attachment Fittings (Ref. TASK 2825-00-650-803).
R R R R
NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures.
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
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Flap-Track Forward | | | | | | | | | Attachment-Fittings, Tracks 2 thru | | | | | | | | | 5 | | | | | | | | | | | | | | | | A.| | Do a detailed visual inspection of | X | | | | | | | | the forward attachment brackets of | | | | | | | | | the flap track beam. | | | | | | | | | Make sure that: | | | | | | | | | - all fasteners are in the correct | | | | | | | | | condition | | | | | | | | | - there are no cracks | | | | | | | | | - the spherical bearings did not | | | | | | | | | move | | | | | | | | | - there are no leaks in the area of | | | | | | | | | the brackets | | | | | | | | | - the structure in the area of the | | | | | | | | | brackets is not distorted | | | | | | | | | - the beam-to-wing clearance is | | | | | | | | | correct. | | | | | | | | | | | | | | | | | | If you find damage: | | | | | | | | | (1) Defuel the wing | | X | | | | | | | (2) Open the tank to the air. | | X | | | | | | | (3) Remove the flap track beam. | | X | | | | | | | (4) Do a general internal inspection | | X | | | | | | | at the area of damage and the | | | | | | | | | adjacent area. | | | | | | | | | | | | | | | |2. | | Inspection of the Attachment Fittings | | | | | | | | | of the Aft Flap Tracks No. 2 thru | | | | | | | | | No. 5 | | | | | | | | | | | | | | | | A.| | Do a detailed visual inspection of the| X | | | | |
R EFF : ALL 05-51-11 SROS
Page 651 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | attachment fittings of flap track | | | | | | | | | No. 2 for cracks, damage or | | | | | | | | | distortion. | | | | | | | | | Make sure that the spherical bearing | | | | | | | | | did not move on: | | | | | | | | | - the spigot fitting | | | | | | | | | - the spherical bearing | | | | | | | | | - the cantilever structure of the | | | | | | | | | bearing support ribs. | | | | | | | | | | | | | | | | B.| | Attachment fittings of the Aft-Flap | | | | | | | | | tracks 2 thru 5 | | | | | | | | | | | | | | | | | | If you find damage: | | | | | | | | | (1) Defuel the wing | | X | | | | | | | (2) Open the wing tank to the air. | | X | | | | | | | (3) Do a general internal inspection | | X | | | | | | | at the damaged area and the | | | | | | | | | adjacent area. | | | | | | | | | | | | | | | | B.| | Do a detailed visual inspection of | X | | | | | | | | the flap-tracks No. 3 thru 5 aft | | | | | | | | | attachment-fittings attached to the | | | | | | | | | rear spar for cracks, fuel leaks or | | | | | | | | | damage. | | | | | | | | | Make sure that the fasteners are in | | | | | | | | | the correct condition. | | | | | | -------------------------------------------------------------------------------
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Subtask 05-51-11-210-102
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J. Inspection of the Wing (Ref. Fig. 613/TASK 05-51-11-991-027) (Ref. TASK 57-56-11-000-801), (Ref. TASK 57-56-11-000-802), (Ref. TASK 28-25-00-650-803), (Ref. TASK 27-54-00-710-801), (Ref. TASK 57-56-11-000803).
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NOTE : Refer to the AD F-2006-008 for other possible inspection ____ requirements for the wing bottom skin (at Rib 6 - STGR20) before the subsequent flight.
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NOTE : All the inspections are visual unless specified differently in the ____ text.
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Page 652 Jan 01/07
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Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Upper Wing Skin from| | | | | | | | | Rib 1 to Wing Tip | | | | | | | | | | | | | | | | A.| | Examine this part for cracks, | X | | | | | | | | distortion, paint and sealant | | | | | | | | | damage. | | | | | | | | | Make sure that the fasteners are | | | | | | | | | in the correct condition. | | | | | | | | | Carefully examine the | | | | | | | | | fasteners at the rear spar between | | | | | | | | | rib 10 and rib 10A and between | | | | | | | | | rib 25 and rib 26. | | | | | | | | | | | | | | | | B.| | If you find damage adjacent to the | | | | | | | | | flap beams No. 2, 3, or 4. | | | | | | | | | (1) Remove the applicable flap beam | | X | | | | | | | fairing: | | | | | | | | | - for fairing No. 2 | | | | | | | | | (Ref. TASK 57-56-11-000-801) | | | | | | | | | - for fairing No. 3 | | | | | | | | | (Ref. TASK 57-56-11-000-802). | | | | | | | | | - for fairing No. 4 | | | | | | | | | (Ref. TASK 57-56-11-000-803). | | | | | | | | | | | | | | | |2. | | Inspection of the Lower Wing Skin | | | | | | | | | from Rib 1 to Wing Tip | | | | | | | | | | | | | | | | A.| | Carefully examine the areas adjacent | X | | | | | | | | to the flap beams, the engine pylons | | | | | | | | | and the MLG attachments for cracks, | | | | | | | | | distortion, fluid leaks, paint and | | | | | | | | | sealant damage. Make sure that the | | | | | | | | | fasteners are in the correct | | | | | | | | | condition. | | | | | | | | | | | | | | | |3. | | Inspection of the Flap Beam Assembly | | | | | | | | | and the Flap Track | | | | | | | | | | | | | | | | A.| | Examine these parts for damage or | X | | | | | | | | cracks. | | | | | |
R EFF : ALL 05-51-11 SROS
Page 653 Jan 01/07
Structure of the Wing Figure 613/TASK 05-51-11-991-027- 13 (SHEET 1)
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R EFF : ALL 05-51-11 SROS
Page 654 Jan 01/07
Structure of the Wing Figure 613/TASK 05-51-11-991-027- 23 (SHEET 2)
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R EFF : ALL 05-51-11 SROS
Page 655 Jan 01/07
Structure of the Wing Figure 613/TASK 05-51-11-991-027- 33 (SHEET 3)
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R EFF : ALL 05-51-11 SROS
Page 656 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | Make sure that: | | | | | | | | | - the paint and sealant are not | | | | | | | | | damaged | | | | | | | | | - the fasteners and safety devices | | | | | | | | | are in the correct condition | | | | | | | | | - the clearance to the wing is | | | | | | | | | correct. | | | | | | | | | | | | | | | | B.| | If you find damage to the flap beam | | | | | | | | | or flap track: | | | | | | | | | (1) Remove the applicable flap beam | | | X | | | | | | assembly for component | | | | | | | | | maintenance. | | | | | | | | | (2) Get access to the area adjacent | | | X | | | | | | to the applicable flap beam. | | | | | | | | | Do a general internal inspection | | | | | | | | | of the ribs, the internal side of | | | | | | | | | the lower skin, the internal face | | | | | | | | | of the rear spar for beams 3 and | | | | | | | | | 4, the internal face of the false | | | | | | | | | rear spar for the No. 2 beam and | | | | | | | | | the applicable flap beam | | | | | | | | | attachments. | | | | | | | | | | | | | | | | C.| | Do an inspection of the ram air | X | | | | | | | | turbine for correct stowage. | | | | | | | | | | | | | | | | | | If it is not latched: | | | | | | | | | (1) Examine all the installation. | | X | | | | | | | If you find damage: | | | | | | | | | (2) Do a functional test of the ram | | X | | | | | | | air turbine and system. | | | | | | | | | | | | | | | |4. | | Inspection of the Trailing Edge | | | | | | | | | | | | | | | | A.| | Do a detailed visual inspection of | X | | | | | | | | the inner, mid and outer rear spar and| | | | | | | | | all supporting structure parts for | | | | | | | | | cracks, damage, distortion or fluid | | | | | | | | | leaks. | | | | | | | | | Make sure that: | | | | | | | | | - the paint and sealant are not | | | | | | | | | damaged | | | | | |
R EFF : ALL 05-51-11 SROS
Page 657 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - the fasteners and safety devices | | | | | | | | | are in the correct condition. | | | | | | | | | | | | | | | | | | If there are signs of damage on the | | | | | | | | | rear spar: | | | | | | | | | (1) Defuel the wing | | X | | | | | | | (Ref. TASK 28-25-00-650-80300). | | | | | | | | | (2) Get access to the internal wing | | X | | | | | | | at the area of damage. | | | | | | | | | (3) Do a general internal inspection | | X | | | | | | | of all the ribs, riblets, | | | | | | | | | stringers, brackets and plates | | | | | | | | | in the damaged area for damage | | | | | | | | | (cracks). | | | | | | | | | Make sure that: | | | | | | | | | - the paint and sealant are not | | | | | | | | | damaged | | | | | | | | | - the fasteners are in the correct| | | | | | | | | condition. | | | | | | | | | | | | | | | | B.| | If you find damage on the wing, do an | | X | | | | | | | operational test of the flaps | | | | | | | | | (Ref. TASK 27-54-00-710-80100). | | | | | | | | | Make sure the flaps and the spoilers | | | | | | | | | move smoothly and freely. | | | | | | | | | | | | | | | | C.| | Do a detailed visual inspection of all| X | | | | | | | | the supporting structure parts for | | | | | | | | | cracks, damage, distortion or fluid | | | | | | | | | leaks. | | | | | | | | | Make sure that: | | | | | | | | | - the fasteners and safety devices | | | | | | | | | are in the correct condition | | | | | | | | | - the paint and sealant are not | | | | | | | | | damaged. | | | | | | | | | | | | | | | | | | If there are signs of damage to the | | | | | | | | | trailing edge false-work. | | | | | | | | | (1) Do a general inspection of these | | X | | | | | | | items: | | | | | | | | | - fixed shroud | | | | | | | | | - fixed shroud attachments | | | | | | | | | - shroud box | | | | | |
EFF : ALL 05-51-11 SROS
Page 658 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - shroud box attachments | | | | | | | | | - support ribs | | | | | | | | | - support rib attachments | | | | | | | | | - lower panel-support struts | | | | | | | | | - riblets stringers and | | | | | | | | | brackets. | | | | | | | | | Make sure that: | | | | | | | | | - there is no damage | | | | | | | | | - the paint and sealant are not | | | | | | | | | damaged | | | | | | | | | - the fasteners are in the | | | | | | | | | correct condition. | | | | | | | | | | | | | | | | C.| | Do an inspection of all the pipes, | X | | | | | | | | the hoses, the electrical looms and | | | | | | | | | the raceways. | | | | | | -------------------------------------------------------------------------------
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Subtask 05-51-11-210-096
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K. Inspection of the Center Fuselage between FR38 and FR54 (Ref. Fig. 614/TASK 05-51-11-991-028, 615/TASK 05-51-11-991-029, 616/TASK 05-51-11-991-030, 617/TASK 05-51-11-991-031)
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NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Center Fuselage | | | | | | | | | | | | | | | | A.| | Examine the belly fairing panels for | X | | | | | | | | loose fasteners, cracked or flaking | | | | | | | | | paint and delamination. | | | | | | | | | Make sure that: | | | | | | | | | -the attachments are correct. | | | | | | | | | | | | | | | | | | If you find damage during the | | | | | | | | | inspection: | | | | | |
EFF : ALL 05-51-11 SROS
Page 659 Jan 01/07
Main Structure Figure 614/TASK 05-51-11-991-028
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EFF : ALL 05-51-11 SROS
Page 660 Jan 01/07
Center Wing Box (Section 21) Figure 615/TASK 05-51-11-991-029
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EFF : ALL 05-51-11 SROS
Page 661 Jan 01/07
Aft Pressure Bulkhead Figure 616/TASK 05-51-11-991-030
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EFF : ALL 05-51-11 SROS
Page 662 Jan 01/07
Belly Fairing Figure 617/TASK 05-51-11-991-031
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EFF : ALL 05-51-11 SROS
Page 663 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | | | | | | | | | | (1) Remove the panels and examine | | X | | | | | | | internally the belly fairing. | | | | | | | | | Make sure that the attachments | | | | | | | | | of all the components are correct | | | | | | | | | and that the rivets are not loose.| | | | | | | | | (2) Examine the fuselage skin | | X | | | | | | | externally, below the belly | | | | | | | | | fairing zone for buckling, loose | | | | | | | | | rivets, cracked or flaking paint. | | | | | | | | | | | | | | | | B.| | Examine the canted frames at the | X | | | | | | | | boundaries of the wheel wells, their | | | | | | | | | junctions, the fittings at FR47 and | | | | | | | | | the adjacent areas. | | | | | | | | | | | | | | | | C.| | Examine the main gear and the center- | X | | | | | | | | gear locking-system attachment. | | | | | | | | | Examine the center gear mounting | | | | | | | | | at FR53.2. | | | | | | | | | | | | | | | | D.| | Examine the longitudinal edging | X | | | | | | | | spars of the keel beam section. | | | | | | | | | | | | | | | | | | If you find damage: | | | | | | | | | (1) Examine the structure of the | | X | | | | | | | keel beam. | | | | | | | | | (2) Examine the structure of the | | X | | | | | | | passenger compartment floor in | | | | | | | | | the main and center gear well. | | | | | | | | | If you find damage: | | | | | | | | | (3) From FR38 to FR54 examine | | | X | | | | | | internally the junction of the | | | | | | | | | panels of the upper fuselage at | | | | | | | | | stingers 5L and 5R. | | | | | | -------------------------------------------------------------------------------
EFF : ALL 05-51-11 SROS
Page 664 Jan 01/07
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Subtask 05-51-11-210-097 L. Inspection of the Tail Section (Zone 310) (Ref. Fig. 618/TASK 05-51-11-991-032, 619/TASK 05-51-11-991-033) (Ref. TASK 31-33-00-710-803), (Ref. TASK 23-71-00-710-801), (Ref. TASK 49-12-00-200-801)
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NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Tail Section | | | | | | | | | | | | | | | | A.| | Examine externally the skin panels | X | | | | | | | | for cracked or flaking paint, loose | | | | | | | | | rivets, wrinkles or buckling. | | | | | | | | | | | | | | | | | | If you find damage on the skin panels:| | | | | | | | | | | | | | | | | | (1) Examine the skin panels and | | X | | | | | | | stringers for cracked or flaking | | | | | | | | | paint, loose rivets, wrinkles or | | | | | | | | | buckles, signs of shearing, | | | | | | | | | distorted and twisted stringers. | | | | | | | | | | | | | | | | B.| | Do a general visual inspection of: | X | | | | | | | | - the attachment areas of the | | | | | | | | | horizontal stabilizer | | | | | | | | | - the attachment area of the vertical | | | | | | | | | stabilizer. | | | | | | | | | | | | | | | | | | If you find damage on the attachment | | | | | | | | | area: | | | | | | | | | | | | | | | | | | (1) Examine the horizontal stabilizer | | X | | | | | | | attachments for damage and signs | | | | | | | | | of movement. | | | | | | | | | (2) Examine the hinges of the elevator| | X | | | | | | | and the rudder for cracks | | | | | | | | | (3) Make sure the DFDR operates | | X | | | | | | | correctly. | | | | | | | | | | | | | | |
EFF : ALL 05-51-11 SROS
Page 665 Jan 01/07
Cone/Rear Fuselage Figure 618/TASK 05-51-11-991-032
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EFF : ALL 05-51-11 SROS
Page 666 Jan 01/07
Structure Components Figure 619/TASK 05-51-11-991-033
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EFF : ALL 05-51-11 SROS
Page 667 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | C.| | Open the access door 312AR for DFDR: | X | | | | | | | | - make sure that the recording unit | | | | | | | | | is not damaged and is attached | | | | | | | | | correctly. | | | | | | | | | | | | | | | | D.| | Do a general inspection of the APU | X | | | | | | | | compartment for leakage and damage. | | | | | | | | | | | | | | | | | | If you find damage: | | | | | | | | | | | | | | | | | | (1) Make sure that the APU is | | X | | | | | | | correctly installed. | | | | | | | | | (2) Examine the mountings for damage, | | X | | | | | | | distortion and signs of movement: | | | | | | | | | (3) Examine the container brackets | | X | | | | | | | and the container of the APU fire | | | | | | | | | extinguisher for damage. | | | | | | | | | Make sure that the installation | | | | | | | | | and attachment are correct. | | | | | | | | | | | | | | | | | | If you find damage in the | | | | | | | | | unpressurized area: | | | | | | | | | - make sure that the CVR operates | | | | | | | | | correctly: | | | | | | ------------------------------------------------------------------------------|
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Subtask 05-51-11-210-098
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M. Inspection of Avionics Compartment (Ref. TASK 24-38-00-740-801).
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NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures.
EFF : ALL 05-51-11 SROS
Page 668 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Avionics | | | | | | | | | Compartment | | | | | | | | | | | | | | | | A.| | Open the access doors to the avionics | X | | | | | | | | compartment. Examine the electrical | | | | | | | | | and electronic components, the | | | | | | | | | batteries and the racks. | | | | | | | | | Make sure that they are not damaged | | | | | | | | | and are installed correctly. | | | | | | | | | | | | | | | | | | If you find damage on the avionics | | | | | | | | | compartment: | | | | | | | | | (1) If there is structural damage | | X | | | | | | | that makes repairs necessary: | | | | | | | | | refer to the NTM. | | | | | | | | | | | | | | | | B.| | Make sure that the quick access | | X | | | | | | | recorder (QAR) operates correctly | | | | | | | | | | | | | | | | C.| | Make sure that the batteries are | X | | | | | | | | attached correctly. Make sure that | | | | | | | | | there are no leaks. | | | | | | | | | | | | | | | | D.| | Make sure that the batteries operate | | X | | | | | | | correctly | | | | | | -------------------------------------------------------------------------------
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Subtask 05-51-11-210-099
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N. Inspection of the Cargo Compartments (Ref. TASK 24-38-00-740-801)
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NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive test procedures.
EFF : ALL 05-51-11 SROS
Page 669 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Cargo Compartment | | | | | | | | | | | | | | | | A.| | Do a visual inspection of the cargo | X | | | | | | | | compartments for general condition | | | | | | | | | and damage. | | | | | | | | | | | | | | | | B.| | Open the bulk cargo-compartment | X | | | | | | | | door: | | | | | | | | | - make sure that the APU battery is | | | | | | | | | attached correctly. Make sure that | | | | | | | | | there are no leaks. | | | | | | | | | | | | | | | | C.| | Examine the unpressurized area behind | X | | | | | | | | the pressure bulkhead. | | | | | | | | | Open the access door 162TW for CVR | | | | | | | | | and water system inspection. | | | | | | | | | - Make sure that the CVR is not | | | | | | | | | damaged and is attached correctly. | | | | | | | | | - Do an inspection of the water | | | | | | | | | system. | | | | | | | | | Make sure that the water tanks are | | | | | | | | | correctly attached and that there | | | | | | | | | are no leaks. | | | | | | | | | | | | | | | | | | If you find damage on the Cargo | | | | | | | | | compartment: | | | | | | | | | (1) Examine the loading and | | X | | | | | | | unloading systems of the | | | | | | | | | containers/pallets and examine | | | | | | | | | the cargo restraint system. In | | | | | | | | | the forward and aft cargo | | | | | | | | | compartments, examine the side | | | | | | | | | guides, pallet locks and rollers | | | | | | | | | (ball units, roller assemblies, | | | | | | | | | drive units, guide latches and | | | | | | | | | tracks). | | | | | | | | | Make sure that they can move | | | | | | | | | freely. | | | | | | | | | (2) Make sure that the APU battery | | X | | | | | | | operates correctly | | | | | | -------------------------------------------------------------------------------
EFF : ALL 05-51-11 SROS
Page 670 Jan 01/07
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Subtask 05-51-11-210-100 P. Inspection of the Equipment/Furnishings
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Equipment/ | | | | | | | | | Furnishings | | | | | | | | | | | | | | | | A.| | Do a check of the equipment/ | X | | | | | | | | furnishings below: | | | | | | | | | - the passenger and crew seats | | | | | | | | | - the coat stowages | | | | | | | | | - the partitions | | | | | | | | | - the side and ceiling panels in the | | | | | | | | | passenger compartment | | | | | | | | | - the flight and passenger compartment| | | | | | | | | stowages | | | | | | | | | - the buffet/galley | | | | | | | | | - the lavatories | | | | | | | | | - the emergency evacuation equipment. | | | | | | -------------------------------------------------------------------------------
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5. Close-up ________
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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 05-51-11-410-052
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A. Close Access
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(1) Remove the safety devices installed on the landing gears.
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(2) Close all the access doors opened during the inspection procedure.
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(3) Close the main landing gear doors (Ref. TASK 32-12-00-410-801).
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(4) Close the nose landing gear doors (Ref. TASK 32-22-00-410-801).
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(5) Close the thrust reverser doors (Ref. TASK 78-30-00-410-801). FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR
EFF : ALL 05-51-11 SROS
Page 671 Jan 01/07
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(6) Close the fan cowl doors (Ref. TASK 71-13-00-410-802). FOR 4030EM1 415BL, 416BR FOR 4030EM2 425BL, 426BR
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**ON A/C 701-749,
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Subtask 05-51-11-410-052-A
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A. Close Access
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(1) Remove the safety devices installed on the landing gears.
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(2) Close all the access doors opened during the inspection procedure.
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(3) Close the main landing gear doors (Ref. TASK 32-12-00-410-801).
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(4) Close the nose landing gear doors (Ref. TASK 32-22-00-410-801).
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(5) Close the thrust reverser doors (Ref. TASK 78-30-00-410-803). FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR
R R R R R
(6) Close the fan cowl doors (Ref. TASK 71-13-00-410-805). FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR
R
**ON A/C ALL
R
Subtask 05-51-11-866-052
R
B. Aircraft Maintenance Configuration
R
(1) Retract the spoilers (Ref. TASK 27-60-00-866-802).
R
(2) Retract the slats (Ref. TASK 27-80-00-866-802).
R
(3) Retract the flaps (Ref. TASK 27-50-00-866-802)
EFF : ALL 05-51-11 SROS
Page 672 Jan 01/07
R R
(4) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801).
R R
(5) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803).
R R
(6) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802).
R R
(7) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
R R
Subtask 05-51-11-942-052 C. Close Access
R
(1) Remove the warning notice(s).
R R
(2) Make sure that the work area is clean and clear of tools and other items.
R
(3) Remove the access platform(s).
EFF : ALL 05-51-11 SROS
Page 673 Jan 01/07
INSPECTION AFTER LANDING GEAR DOWN LIMITING SPEED EXCEEDED - INSPECTION/CHECK _____________________________________________________________________________ TASK 05-51-12-200-801 Inspection After Landing Gear Extension at More than the Gear Down Limiting Speed. 1. __________________ Reason for the Job This inspection is applicable if: - the landing gear extends/retracts, while the aircraft speed is more than the limit speed (VLO). - the aircraft speed increases to more than the limit speed (VLE), while the landing gear is downlocked. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
safety barriers warning notice
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------07-11-00-581-801 07-11-00-586-801 24-41-00-862-801 27-50-00-866-801 27-50-00-866-802 28-10-00-910-802 29-00-00-864-801 29-00-00-864-802 29-00-00-864-803 32-00-00-481-801
Lifting of the Aircraft for Maintenance Operations Lowering of the Aircraft for Maintenance Operations De-energize the Aircraft Electrical Circuits from the External Power A Extension of the Flaps on the Ground Retraction of the Flaps on the Ground Access to Fuel Tanks and Work Areas 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) Installation of the Safety Devices on the Landing Gears
EFF : ALL 05-51-12 SROS
Page 601 Apr 01/98
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
R R
32-11-00-220-802 32-11-13-000-801 32-11-13-860-801 32-12-00-010-801 32-12-00-410-801 32-12-14-000-801 32-12-14-200-801 32-21-00-220-803 32-21-13-000-801 32-22-00-010-801 32-22-00-410-801 32-22-11-000-801 32-31-16-000-801 53-35-11-000-801 05-51-12-991-001 05-51-12-991-002 05-51-12-991-003 05-51-12-991-004 05-51-12-991-005 05-51-12-991-007 05-51-12-991-008
Check of Shock Absorber Nitrogen Charge Pressure Removal of the MLG Shock Absorber To Close the Seal Changeover Valve Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Removal of the MLG Fixed Fairing Assembly Inspection of the MLG Fixed Fairing Assembly Check Nose Gear Shock Absorber Nitrogen Charge Pressure Removal of the NLG Shock Absorber Assembly Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance Removal of the NLG Main Door Assy Removal of the NLG Door Actuator (5203GA,5204GA) Removal of the Wing-to-Fuselage Fairings Fig. 601 Fig. 602 Fig. 603 Fig. 604 Fig. 605 Fig. 606 Fig. 607
3. __________ Job Set-up Subtask 05-51-12-941-050 A. Safety Precautions (1) Put a warning notice in the cockpit to tell persons not to operate the aircraft system. (2) Put the safety barriers in position. Subtask 05-51-12-010-050 B. Get Access (1) Open the main landing gear doors (Ref. TASK 32-12-00-010-801). (2) Open the nose landing gear doors (Ref. TASK 32-22-00-010-801).
EFF : ALL 05-51-12 SROS
Page 602 Jul 01/05
Subtask 05-51-12-091-050 C. Safety Precautions (1) Install the safety devices on the landing gears (Ref. TASK 32-00-00481-801). (2) Lift the aircraft (Ref. TASK 07-11-00-581-801). R R
NOTE : Lifting of the aircraft is only necessary for the PHASE 2 ____ inspection. Subtask 05-51-12-866-050 D. Aircraft Maintenance Configuration (1) Fully extend the flap (Ref. TASK 27-50-00-866-801). Subtask 05-51-12-864-050 E. Aircraft Maintenance Configuration (1) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (2) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803). (3) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-802). (4) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). Subtask 05-51-12-010-051 F. Get Access (1) Open all the access panels in the main landing gear compartment.
EFF : ALL 05-51-12 SROS
Page 603 Jan 01/06
4. Procedure _________ Subtask 05-51-12-210-050 A. Inspection of the Fuselage NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non-Destructive Testing Manual (NTM) and use non destructive test procedures. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Fuselage | | | | | | | | | | | | | | | | A.| | Examine the external fuselage | X | | | | | | | | and the skin panels for: | | | | | | | | | - distortion, cracks, pulled or torn | | | | | | | | | fasteners and damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Internally examine the frames, | | X | | | | | | | the stringers and the cleats for: | | | | | | | | | buckling, cracks and damaged | | | | | | | | | paintwork. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-12-210-051 B. Inspection of Nose Landing Gear Well and Doors (Ref. Fig. 601/TASK 05-51-12-991-001) (Ref. TASK 32-22-11-000-801), (Ref. TASK 32-31-16-000-801). ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Nose Landing Gear | | | | | | | | | Bay | | | | | | | | | (Ref. Fig. 601/TASK 05-51-12-991-001) | | | | | | | | | | | | | | | | A.| | Examine the hinge fittings of the nose| X | | | | | | | | landing gear, the attach fitting of | | | | | | | | | the actuating cylinder, the drag | | | | | | | | | strut, the attach fittings for: | | | | | | | | | - distortion, cracks, pulled or torn | | | | | |
EFF : ALL 05-51-12 R SROS
Page 604 Jan 01/02
Nose Landing Gear Figure 601/TASK 05-51-12-991-001 EFF : ALL 05-51-12 R SROS
Page 605 Jan 01/02
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | fasteners and damaged paintwork. | | | | | | | | | | | | | | | | B.| | Examine the NLG well roof, the | X | | | | | | | | forward and aft side wall | | | | | | | | | structure for: | | | | | | | | | - distortion, cracks, pulled or torn | | | | | | | | | fasteners and damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Get access to the avionics | | X | | | | | | | compartment and internally | | | | | | | | | examine the NLG well roof, and | | | | | | | | | the forward and aft side | | | | | | | | | wall, the struts for: | | | | | | | | | - distortion, cracks, pulled or | | | | | | | | | torn fasteners and damage | | | | | | | | | paintwork. | | | | | | | | | | | | | | | | C.| | Examine the components installed in | X | | | | | | | | the nose landing gear well, the | | | | | | | | | manifold, the electrical looms, the | | | | | | | | | rods, the pipes, the bellcranks for: | | | | | | | | | - distortion, cracks, rupture and | | | | | | | | | fluid leakage. | | | | | | | | | | | | | | | |2. | | Examine the nose landing gear doors. | | | | | | | | | | | | | | | | A.| | Examine the doors, the door hinge | X | | | | | | | | fittings and the adjacent structure | | | | | | | | | for: | | | | | | | | | - distortion, cracks, pulled or torn | | | | | | | | | fasteners, delamination and damaged | | | | | | | | | paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the doors | X | | | | | | | | (Ref. TASK 32-22-11-000-801). | | | | | | | | | | | | | | | | B.| | Examine the door actuating cylinder, | X | | | | | | | | the rods, the related linkages, the | | | | | | | | | valve for fluid leakage, cracks, | | | | | | | | | pulled or torn fasteners. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the nose landing gear door | | X | | | | | | | actuating cylinder | | | | | |
EFF : ALL 05-51-12 R SROS
Page 606 Jan 01/02
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (Ref. TASK 32-31-16-000-801). | | | | | | ------------------------------------------------------------------------------Subtask 05-51-12-210-052 C. Inspection of the Belly Fairing (Ref. Fig. 602/TASK 05-51-12-991-002, 603/TASK 05-51-12-991-003, 604/TASK 05-51-12-991-004) (Ref. TASK 53-35-11-000-801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the belly fairing | | | | | | | | | (Ref. Fig. 602/TASK 05-51-12-991-002) | | | | | | | | | (Ref. Fig. 603/TASK 05-51-12-991-003) | | | | | | | | | (Ref. Fig. 604/TASK 05-51-12-991-004) | | | | | | | | | | | | | | | | A.| | Examine the panels, the rods, the | X | | | | | | | | external surface, for: | | | | | | | | | - distortion, cracks, pulled or torn | | | | | | | | | fasteners, delamination, and | | | | | | | | | damaged paintwork. | | | | | | | | | Make sure that the panels and the rods| | | | | | | | | are correctly installed. | | | | | | | | | | | | | | | | B.| | Externally examine the cover of the | X | | | | | | | | keel beam for: | | | | | | | | | - distortion, cracks, delamination, | | | | | | | | | damaged paintwork, pulled or torn | | | | | | | | | fasteners. | | | | | | | | | Make sure that the attachment is | | | | | | | | | correct. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the panels and internally | | X | | | | | | | examine the structure of the belly| | | | | | | | | fairing, the skin for: | | | | | | | | | - distortion, cracks, buckling | | | | | | | | | and damaged paintwork, box | | | | | | | | | rivets | | | | | | | | | (Ref. TASK 53-35-11-000-801). | | | | | | | | | (2) Examine all the components | | X | | | |
EFF : ALL 05-51-12 R SROS
Page 607 Jan 01/02
Wing Center Box Figure 602/TASK 05-51-12-991-002 EFF : ALL 05-51-12 SROS
Page 608 Apr 01/98
Wing Center Box - Main Structure Figure 603/TASK 05-51-12-991-003 EFF : ALL 05-51-12 SROS
Page 609 Apr 01/98
Belly Fairing Structure Figure 604/TASK 05-51-12-991-004 EFF : ALL 05-51-12 SROS
Page 610 Apr 01/98
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | installed in the belly fairing, | | | | | | | | | the ducts, the pipes, the | | | | | | | | | electrical loom and their mount, | | | | | | | | | the safety devices, for: | | | | | | | | | - distortion, cracks, fluid | | | | | | | | | leakage, breaks, rupture, | | | | | | | | | pulled or torn fasteners, | | | | | | | | | damaged paintwork, loose rivets.| | | | | | | | | Make sure that the attachment is | | | | | | | | | correct and that the components | | | | | | | | | are in the correct condition. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-12-210-053 D. Inspection of Main Landing Gear Bay FR47 to FR53 and Doors (Ref. Fig. 605/TASK 05-51-12-991-005) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Main Landing Gear | | | | | | | | | Well FR47 to FR53 | | | | | | | | | (Ref. Fig. 605/TASK 05-51-12-991-005) | | | | | | | | | | | | | | | | A.| | Examine the diagonal frames at the | X | | | | | | | | edges of the wheel wells, their | | | | | | | | | junctions at FR47 and the adjacent | | | | | | | | | structure for: | | | | | | | | | - distortion, cracks, pulled or torn | | | | | | | | | fasteners and damaged paintwork. | | | | | | | | | | | | | | | | B.| | Examine the attachment of the main | X | | | | | | | | landing gear for: | | | | | | | | | - distortion, cracks. | | | | | | | | | If you find damage: | | | | | | | | | (1) Examine the components, the pipes,| | X | | | | | | | the ducts, the electrical looms | | | | | | | | | and their mounts, the control | | | | | | | | | cables, the pulleys, the | | | | | | | | | transmission systems, the | | | | | | | | | manifold, the safety devices for: | | | | | |
EFF : ALL 05-51-12 R SROS
Page 611 Jan 01/02
Main Landing Gear and Doors Figure 605/TASK 05-51-12-991-005 EFF : ALL 05-51-12 R SROS
Page 612 Jan 01/02
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - distortion, cracks, pulled or | | | | | | | | | torn fasteners, fluid leakage | | | | | | | | | and damaged paintwork. | | | | | | | | | Make sure that the attachment is | | | | | | | | | correct and that the components | | | | | | | | | are in the correct condition. | | | | | | | | | | | | | | | |2. | | Inspection of the Landing Gear Doors | | | | | | | | | | | | | | | | A.| | Examine the landing gear doors, their | X | | | | | | | | hinges and the adjacent structure for:| | | | | | | | | - cracks, delamination, pulled or torn| | | | | | | | | fasteners and damaged paintwork. | | | | | | | | | | | | | | | | B.| | Examine the door actuating cylinders, | X | | | | | | | | the selector valves and their hoses | | | | | | | | | and pipes for: | | | | | | | | | - damage. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-12-210-054 E. Inspection of Nose Landing Gear (Ref. Fig. 601/TASK 05-51-12-991-001) (Ref. TASK 32-21-00-220-803) (Ref. TASK 32-21-13-000-801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Nose Landing Gear | | | | | | | | | (Ref. Fig. 601/TASK 05-51-12-991-001) | | | | | | | | | | | | | | | | A.| | Examine the nose landing gear | X | | | | | | | | components, the pipes, the electrical | | | | | | | | | looms, the hoses for: | | | | | | | | | - damage, fluid leakage and damaged | | | | | | | | | paintwork. | | | | | | | | | | | | | | | | B.| | Examine the shock absorber for: | X | | | | | | | | - correct pressure charge, fluid | | | | | | | | | leakage, and damage | | | | | | | | | (Ref. TASK 32-21-00-220-803). | | | | | |
EFF : ALL 05-51-12 R SROS
Page 613 Jan 01/02
R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | If you find leaks: | | | | | | | | | (1) Remove the shock absorber for | | X | | | | | | | maintenance. | | | | | | | | | (Ref. TASK 32-21-13-000-801) | | | | | | |2. | | Inspection of the Fixed Fairing | | | | | | | | | | | | | | | | A.| | Examine the door, the linkage rollers,| X | | | | | | | | the uplock hooks for: | | | | | | | | | - damage. | | | | | | | | | Make sure that the attachment is | | | | | | | | | correct. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-12-210-055 F. Inspection of the Main Landing Gear (Ref. Fig. 605/TASK 05-51-12-991-005) (Ref. TASK 32-11-13-000-801) (Ref. TASK 32-11-00-220-802) (Ref. TASK 3211-13-860-801) (Ref. TASK 32-12-14-000-801) (Ref. TASK 32-12-14-200-801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Main Landing Gear | | | | | | | | | (Ref. Fig. 605/TASK 05-51-12-991-005) | | | | | | | | | | | | | | | | A.| | Examine the main landing gear and its | X | | | | | | | | components, hoses, pipes and | | | | | | | | | electrical harnesses for damage and | | | | | | | | | distortion. | | | | | | | | | Examine dynamic and static joints for:| | | | | | | | | - distortion. | | | | | | | | | | | | | | | | B.| | Examine the shock absorber for: | X | | | | | | | | - hydraulic fluid leaks. | | | | | | | | | If you find leaks: | | | | | | | | | - remove the shock absorber for | | X | | | | | | | maintenance. | | | | | | | | | (Ref. TASK 32-11-13-000-801) | | | | | | | | | | | | | | | | C.| | Examine the gland seals for: | X | | | | | | | | - hydraulic fluid leakage. | | | | | |
EFF : ALL 05-51-12 SROS
Page 614 Jan 01/06
R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | If you find leaks: | | | | | | | | | (1) Close the seal change-over valve | | X | | | | | | | (Ref. TASK 32-11-13-860-801). | | | | | | | | | If the seal change-over valve is | | | | | | | | | already closed: | | | | | | | | | (2) Remove the shock absorber for | | | X | | | | | | maintenance | | | | | | | | | (Ref. TASK 32-11-13-000-801). | | | | | | | | | | | | | | | | D.| | Do a pressure/extension check of the | X | | | | | | | | shock absorber | | | | | | | | | (Ref. TASK 32-11-00-220-802). | | | | | | | | | | | | | | | |2. | | Inspection of the fixed fairing doors | | | | | | | | | and hinged fairing | | | | | | | | | (Ref. Fig. 605/TASK 05-51-12-991-005).| | | | | | | | | | | | | | | | A.| | Examine the fixed fairing for: | X | | | | | | | | - damage | | | | | | | | | (Ref. TASK 32-12-14-200-801). | | | | | | | | | Make sure that the attachment is | | | | | | | | | correct. | | | | | | | | | If found: | | | | | | | | | (1) Remove the fixed fairing | | X | | | | | | | (Ref. TASK 32-12-14-000-801). | | | | | | -------------------------------------------------------------------------------
EFF : ALL 05-51-12 SROS
Page 615 Jul 01/05
Subtask 05-51-12-210-057 G. Inspection of the Wing (RIB1 to RIB39) (Ref. Fig. 606/TASK 05-51-12-991-007, 607/TASK 05-51-12-991-008) (Ref. TASK 28-10-00-910-802)
R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Wing (MLG | | | | | | | | | Attachment Points) | | | | | | | | | (Ref. Fig. 608/TASK 05-51-12-991-008) | | | | | | | A.| | Examine these parts (and their points | X | | | | | | | | of attachment): | | | | | | | | | - the forward pintle-pin fitting | | | | | | | | | - the rear pintle-pin fitting | | | | | | | | | - the gear rib 6 | | | | | | | | | - the bellcrank of the MLG actuator | | | | | | | | | - the side stay attachment fitting | | | | | | | | | - the retraction actuator attachment | | | | | | | | | fittings for: | | | | | | | | | - cracks, damage and distortion, | | | | | | | | | flaked point, cracked sealant, | | | | | | | | | fluid leaks (fuel, where | | | | | | | | | applicable). | | | | | | | | | If you find damage on the rear spar: | | | | | | | | | (1) Get access to the fuel tank | | X | | | | | | | adjacent to the applicable area. | | | | | | | | | (2) Examine the internal structure | | | | | | | | | adjacent to the external damage or| | X | | | | | | | distortion for: | | | | | | | | | - damaged paint, cracks in | | | | | | | | | structure or sealant | | | | | | | | | (especially cracks in the | | | | | | | | | sealant bead), damaged | | | | | | | | | fasteners, damaged secondary | | | | | | | | | structure (ribs, riblets, | | | | | | | | | stringers, brackets and plates),| | | | | | | | | damaged pipes, electrical cables| | | | | | | | | and raceways. | | | | | | | | | | | | | | | |2. | | Inspection of the Wing | | | | | | | | | (Ref. Fig. 607/TASK 05-51-12-991-007) | | | | | | | A.| | Examine the wing lower skin for: | X | | | | | | | | - fuel leaks, pulled or missing | | | | | | | | | fasteners, cracks and distortion. | | | | | |
EFF : ALL 05-51-12 SROS
Page 616 Jul 01/05
Wing Box - Structure Figure 606/TASK 05-51-12-991-007 EFF : ALL 05-51-12 SROS
Page 617 Apr 01/98
Main Landing Gear Attachments - Structure Figure 607/TASK 05-51-12-991-008 EFF : ALL 05-51-12 SROS
Page 618 Apr 01/98
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | If you find damage: | | | | | | | | | (1) Defuel the wing and get access | | X | | | | | | | into it | | | | | | | | | (Ref. TASK 28-10-00-910-902). | | | | | | | | | (2) Examine the internal structure | | | | | | | | | adjacent to the damage for: | | | | | | | | | - missing or pulled fasteners, | | X | | | | | | | damaged ribs, damaged riblets, | | | | | | | | | damaged stringers, cracks. | | | | | | | | | Make sure that the sealant bead is| | | | | | | | | in the correct condition. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-12-210-058 H. Inspection of the Pylon
R R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Pylon | | | | | | | | | | | | | | | | A.| | Examine the external panels, the skin,| X | | | | | | | | the external structure for: | | | | | | | | | - distortion, cracks, pulled or torn | | | | | | | | | fasteners and damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Open the access doors and panels | | X | | | | | | | in the aircraft structure. | | | | | | | | | (2) Examine the adjacent structure | | | | | | | | | for: | | | | | | | | | - cracks, damaged paintwork, | | | | | | | | | distortion, pulled or torn | | | | | | | | | fasteners. | | | | | | | | | (3) Do a visual check of the fire | | X | | | | | | | protection system, extinguisher | | | | | | | | | bottle attachment, electrical | | | | | | | | | wires, fuel lines, air | | | | | | | | | conditioning ducts, and other | | | | | | | | | components for: | | | | | | | | | - distortion, cracks, correct | | | | | | | | | attachment, fluid leakage, | | | | | |
EFF : ALL 05-51-12 SROS
Page 619 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | and damaged paintwork. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-12-410-050 J. Close Access (1) Close all the access doors opened during the inspection. (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). Subtask 05-51-12-866-051 K. Aircraft Maintenance Configuration (1) Retract the flaps (Ref. TASK 27-50-00-866-802). 5. Close-up ________ Subtask 05-51-12-586-050 A. Lower the Aircraft (1) Lower the aircraft (Ref. TASK 07-11-00-586-801). Subtask 05-51-12-942-050 B. 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) Remove the warning notice(s). (3) Remove the access platform(s).
EFF : ALL 05-51-12 R SROS
Page 620 Jan 01/02
INSPECTION AFTER FLAP/SLAT LIMITING SPEED EXCEEDED - INSPECTION/CHECK _____________________________________________________________________ TASK 05-51-13-200-801 Inspection after Flap/Slat Extension at more than the Flap/Slat Limiting Speed 1. __________________ Reason for the Job This inspection is necessary after an activation of the overspeed audio warning: - If the overspeed was not more than 10 Kts higher than the value shown on the VFE placard, only an extension and retraction test of the flaps and slats is necessary (refer to the operational test of the flight control surfaces paragraph given in this procedure). NOTE : If you find unsatisfactory condition(s) during the operational test, ____ you must do the full inspection given in this procedure. - If the overspeed was more than 10 Kts higher than the value shown on the VFE placard, you must do the full inspection given in this procedure. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
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No No No No
specific specific specific specific
adjustable access platform safety barriers warning notice wheel chocks
EFF : ALL 05-51-13 SROS
Page 601 Jul 01/05
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 24-41-00-862-801 27-50-00-866-801 27-50-00-866-802 27-54-00-200-801 27-54-00-200-802 27-54-00-710-801 27-60-00-866-801 27-60-00-866-802 27-64-00-710-801 27-80-00-866-801 27-80-00-866-802 27-84-00-210-801 27-84-00-710-801 28-10-00-910-802 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 32-00-00-481-801 32-12-00-010-801 52-30-00-010-801 52-30-00-410-801
Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Extension of the Flaps on the Ground Retraction of the Flaps on the Ground Detailed Visual Inspection of the Flap Transmission Assy Detailed Visual Inspection of the Cruise Rollers, Flap Tracks and Carriages, Rotary Actuators and Attachments Operational Test of the Flap System Extension of the Spoilers for Maintenance Retraction of the Spoilers after Maintenance Operational Test of the Spoilers Extension of the Slats on the Ground Retraction of the Slats on the Ground Detailed Visual Inspection of the Slat Transmission Assy, Slat Tracks and Rollers, Pinions and Curved Rack Gears Operational Test of the Slat System Access to Fuel Tanks and Work Areas 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) Installation of the Safety Devices on the Landing Gears Open the MLG Doors for 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
EFF : ALL 05-51-13 R SROS
Page 602 Oct 01/03
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------57-56-11-000-801 57-56-11-000-802 57-56-11-000-803 57-56-11-000-804 57-56-11-000-805
Removal of Removal of Removal of Removal of Removal of 5 (without Side)
the Movable Flap Track Fairing No. 2 the Movable Flap Track Fairing No. 3 the Movable Flap Track Fairing No. 4 the Movable Flap Track Fairing No. 5 the Fixed Flap Track Fairings Nos. 2 thru Fixed Flap Track Fairing No 4 on the Right
3. __________ Job Set-up Subtask 05-51-13-941-050 A. Safety Precautions (1) Put the safety barriers in position. R
(2) Put the wheel chocks in position at the main landing gear. (3) Put a warning notice in position in the cockpit to tell persons not to operate the systems. Subtask 05-51-13-010-050 B. Get Access (1) Open the main landing gear doors (Ref. TASK 32-12-00-010-801). (2) Open the aft cargo compartment door (Ref. TASK 52-30-00-010-801). (3) Put an adjustable access platform in position near the area you want to inspect. (4) Install the safety devices on the landing gear (Ref. TASK 32-00-00481-801). Subtask 05-51-13-860-050 C. 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).
EFF : ALL 05-51-13 SROS
Page 603 Jul 01/05
(3) Fully extend the spoilers (Ref. TASK 27-60-00-866-801). (4) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (5) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803). (6) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802). (7) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). 4. Procedure _________ Subtask 05-51-13-210-050 A. Inspection of the Wing NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non-destructive Testing Manual (NTM) and use the non-destructive test procedures.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the wing leading edge | | | | | | | | | | | | | | | | A. | |Examine the upper and lower skin panels| x | | | | | | | |of the leading edge for: | | | | | | | | |- distorted, cracked, pulled or damaged| | | | | | | | | fasteners, damaged paintwork and | | | | | | | | | distortion. | | | | | | | | |If you find damage: | | | | | | | | |(1)Get access to the area near the | | x | | | | | | | leading edge (the other side of the | | | | | | | | | damage). | | | | | | | | |(2)Examine the area for distortion and | | x | | | | | | | damage on ribs, riblets, stringers | | | | | | | | | and plates. | | | | | | | | | | | | | | | |2. | |Inspection of the wing trailing edge | | | | | | | | | | | | | | | | A. | |Examine the upper and lower skin panels| x | | | | | | | |of the trailing edge for: | | | | | |
EFF : ALL 05-51-13 SROS
Page 604 Jul 01/05
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | |- distortion, cracks, pulled and | | | | | | | | | damaged fasteners, damaged paintwork,| | | | | | | | | damaged electrical harnesses. | | | | | | | | |If you find damage: | | | | | | | | |(1)Get access to the external structure| | x | | | | | | | of the trailing edge (the other | | | | | | | | | side of the damage) | | | | | | | | |(2)Examine the area for distortion, | | x | | | | | | | damage on ribs, riblets, brackets, | | | | | | | | | stringers and plates for damage. | | | | | | | | | | | | | | | |3. | |Inspection of the wing tip | | | | | | | | | | | | | | | | A. | |Examine the upper and lower skin panels| x | | | | | | | |of the wing tip, the attachment fitting| | | | | | | | |of the winglet for: | | | | | | | | |- distortion and damage, pulled and | | | | | | | | | damaged fasteners, damaged paintwork,| | | | | | | | | defective attachment. | | | | | | | | |If you find damage: | | | | | | | | |(1)Get access to the internal structure| | x | | | | | | | of the wing tip (the opposite side | | | | | | | | | to the damage). | | | | | | | | |(2)Examine the area for distortion, | | | | | | | | | damage on ribs, riblets, brackets, | | x | | | | | | | stringers and plates for damage. | | | | | | | | | | | | | | | |4. | |Inspection of the winglet assembly | | | | | | | | | | | | | | | | A. | |Examine the upper and lower skin panels| x | | | | | | | |of the winglet assembly and the winglet| | | | | | | | |attachment fittings for: | | | | | | | | |- distortion, cracked skin, pulled and | | | | | | | | | damaged fasteners, damaged paintwork,| | | | | | | | | delamination. | | | | | | | | |Also examine, the winglet attachment | | | | | | | | |fittings for: | | | | | | | | |- distortion and damage to the fittings| | | | | | | | | and the adjacent structure. | | | | | | | | |If you find damage: | | | | | | | | |(1)Get access to the internal structure| | x | | | | | | | of the winglet assembly. | | | | | | | | |(2)Examine the area for distortion, | | x | | | |
EFF : ALL 05-51-13 SROS
Page 605 Jul 01/05
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NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non-destructive Testing Manual and use non-destructive test procedures. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the flap assemblies and | | | | | | | | |flap transmission system | | | | | | | | | | | | | | | | A. | |Examine the inboard and outboard flaps,| x | | | | | | | |the attachment fittings, the torque | | | | | | | | |limiters of the flap transmission | | | | | | | | |system for: | | | | | | | | |- cracks, distortion, pulled or torn | | | | | | | | | fasteners, honeycomb and core | | | | | | | | | delamination, damaged paintwork. | | | | | | | | |Make sure that the torque limiter | | | | | | | | |operates correctly. | | | | | | | | |If you find damage: | | | | | | | | |(1)Examine the flap transmission | | x | | | | | | | assemblies for damage | | | | | | | | | (Ref. TASK 27-54-00-200-801). | | | | | | | | | If you find damage: | | | | | |
EFF : ALL 05-51-13 SROS
Page 606 Jul 01/05
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (a)Remove the system actuator, the | | | x | | | | | | shafts, the bearings, the | | | | | | | | | gearboxes for inspection and | | | | | | | | | servicing. | | | | | | | | |(2)Examine the flap tracks and the | | | x | | | | | | rollers for damage | | | | | | | | | (Ref. TASK 27-54-00-200-802). | | | | | | | | | | | | | | | |2. | |Inspection of the flap track | | | | | | | | |attachments | | | | | | | | | | | | | | | | A. | |Examine the attachment of the flap | | | | | | | | |tracks 1 at the wing root and their | x | | | | | | | |attachment fittings for: | | | | | | | | |- distortion, cracks, pulled or torn | | | | | | | | | fasteners and damaged paintwork. | | | | | | | | |If you find damage: | | | | | | | | |(1)Get access to the main landing gear | | x | | | | | | | well and to the aft cargo | | | | | | | | | compartment. | | | | | | | | |(2)Examine the frames, the structure, | | | | | | | | | the cleats, the stringers for | | | | | | | | | distortion, cracks, pulled or torn | | x | | | | | | | fasteners and damaged paintwork. | | | | | | | | | | | | | | | | B. | |Examine the attachments, the beam | | | | | | | | |assemblies of the flap tracks No. 2 to | x | | | | | | | |No. 5 for: | | | | | | | | |- distortion, cracks, pulled or torn | | | | | | | | | fasteners and damaged paintwork. | | | | | | | | | Do a check of the clearance. | | | | | | | | |If you find damage: | | | | | | | | |(1)Remove the flap track fairings | | x | | | | | | | No. 2 to No. 5. | | | | | | | | | (Ref. TASK 57-56-11-000-801) | | | | | | | | | (Ref. TASK 57-56-11-000-802) | | | | | | | | | (Ref. TASK 57-56-11-000-803) | | | | | | | | | (Ref. TASK 57-56-11-000-804) | | | | | | | | | (Ref. TASK 57-56-11-000-805) | | | | | | | | |(2)Examine the beam assemblies of the | | | | | | | | | flap tracks No. 2 to No. 5, their | | x | | | | | | | forward pins and their aft spigots | | | | | | | | | for: | | | | | |
EFF : ALL 05-51-13 SROS
Page 607 Jul 01/05
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - distortion, cracks, pulled or torn| | | | | | | | | fasteners and damaged paintwork. | | | | | | | | | Do a check of the clearance. | | | | | | | | |(3)Defuel the tanks | | | | | | | | | (Ref. TASK 28-10-00-910-802) and | | | | | | | | | examine the rib near the flap track | | x | | | | | | | attachment fittings for: | | | | | | | | | - cracks, distortion, damaged, | | | | | | | | | pulled or torn fasteners and | | | | | | | | | damaged paintwork. | | | | | | | | |Also examine the sealant beads. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-13-210-052
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C. Inspection of the Slat System (Ref. TASK 27-84-00-210-801) NOTE : All the inspection are visual unless specified differently in the ____ text. Operators can refer to the Non-destructive Testing Manual (NTM) and use non-destructive test procedures.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the slat assemblies | | | | | | | | |and slat transmission | | | | | | | | | | | | | | | | A. | |Examine the slats, the hold down stop | | | | | | | | |brackets, the attachments, the anti-ice| x | | | | | | | |telescopic duct attachment, the torque | | | | | | | | |limiters of the slat system for: | | | | | | | | |- cracks, distortion, honeycomb and | | | | | | | | | core delamination, pulled or torn | | | | | | | | | fasteners, damaged paintwork. | | | | | | | | |Make sure that the torque limiters | | | | | | | | |operate correctly. | | | | | | | | |If you find damage: | | | | | | | | |(1)Examine the slat transmission | | x | | | | | | | system for damage | | | | | | | | | (Ref. TASK 27-84-00-210-801). | | | | | |
EFF : ALL 05-51-13 SROS
Page 608 Jul 01/05
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | If you find damage: | | | | | | | | | (a)Remove the system actuator, the | | | | | | | | | shafts, the bearings, the gear | | | x | | | | | | boxes for inspection and | | | | | | | | | servicing. | | | | | | | | |(2)Examine the slat track rollers for | | x | | | | | | | damage | | | | | | | | | (Ref. TASK 27-84-00-210-801). | | | | | | | | |(3)Examine the pipes, the hoses, | | x | | | | | | | the components, the electrical | | | | | | | | | harnesses and their brackets for: | | | | | | | | | - cracks, distortion, pulled or torn| | | | | | | | | fasteners, fluid leakage and | | | | | | | | | damaged paintwork. | | | | | | | | | | | | | | | |2. | |Inspection of the slat track | | | | | | | | |attachments | | | | | | | | | | | | | | | | A. | |Examine the tracks No. 1 to No.7 and | | | | | | | | |their mountings, the rack teeth of the | | | | | | | | |tracks No. 1 to No. 7 and their | x | | | | | | | |attachments for: | | | | | | | | | - distortion, cracks, pulled or torn | | | | | | | | | fasteners and damaged paintwork. | | | | | | | | |If you find damage: | | | | | | | | |(1)Open all the access panels of the | | x | | | | | | | wing. | | | | | | | | |(2)Examine the remaining tracks and | | x | | | | | | | their mountings, the rack teeth of | | | | | | | | | the remaining tracks and their | | | | | | | | | attachments for: | | | | | | | | | - cracks, distortion, pulled or torn| | | | | | | | | fasteners and damaged paintwork. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-13-410-050 D. Close Access (1) Close the aft cargo compartment door (Ref. TASK 52-30-00-410-801). (2) Close all the access panels opened during the procedure.
EFF : ALL 05-51-13 SROS
Page 609 Jul 01/05
Subtask 05-51-13-860-051 E. Put the system back to its operational 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) Pressurize the Yellow hydraulic system (Ref. TASK 29-00-00-863-803). (4) Pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-802). (5) Retract the flaps (Ref. TASK 27-50-00-866-802). (6) Retract the slats (Ref. TASK 27-80-00-866-802). (7) Retract the spoilers (Ref. TASK 27-60-00-866-802). Subtask 05-51-13-710-050 R
F. Do this test. (1) Operate the flap system. Make sure that the travel is full and that the flaps move freely (Ref. TASK 27-54-00-710-801). (2) Operate the slat system. Make sure that the travel is full and that the slats move freely (Ref. TASK 27-84-00-710-801). (3) Operate the spoiler system. Make sure that the travel is full and that the spoilers move freely (Ref. TASK 27-64-00-710-801). Subtask 05-51-13-860-052 G. Put the Aircraft back to its Initial Configuration (1) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (2) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803).
EFF : ALL 05-51-13 SROS
Page 610 Jul 01/05
(3) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802). (4) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). 5. Close-up ________ Subtask 05-51-13-942-050 A. Put the Aircraft back to its Initial Configuration (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. (4) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-51-13 R SROS
Page 611 Oct 01/03
INSPECTION OF AIRFRAME AFTER BIRD OR HAIL STRIKE - INSPECTION/CHECK ___________________________________________________________________ TASK 05-51-14-200-801 Inspection of the Aircraft after a Bird or a Hail Strike 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 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. 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
safety barriers warning notice wheel chocks adjustable access platform 16.8 m (55 ft. 1 in.)
EFF : ALL 05-51-14 SROS
Page 601 Jan 01/07
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 24-41-00-862-801 27-14-00-710-801 27-24-00-710-801 27-34-00-710-801 27-44-00-710-801 27-50-00-866-801 27-50-00-866-802 27-54-00-710-801 27-60-00-866-801 27-60-00-866-802 27-64-00-710-801 27-80-00-866-802 27-84-00-710-801 28-10-00-910-801 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 32-00-00-081-801 32-00-00-481-801 32-11-00-220-801
32-12-00-010-801
Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Operational Test of the Aileron and Hydraulic Actuation Operational Test of the Rudder Servo Control with each Hydraulic System Operational Test of the Elevator and Hydraulic Actuation Operational Test of the Trimmable Horizontal Stabilizer (THS) Actuator Jamming Protection Device Extension of the Flaps on the Ground Retraction of the Flaps on the Ground Operational Test of the Flap System Extension of the Spoilers for Maintenance Retraction of the Spoilers after Maintenance Operational Test of the Spoilers Retraction of the Slats on the Ground Operational Test of the Slat System Safety Procedures When You Do Work in a Fuel Tank 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) Removal of the Safety Devices from the Landing Gears Installation of the Safety Devices on the Landing Gears Detailed Inspection of Main Gear Structure comprising: Main Fittings, Sliding Piston, Bogie Beam, Pitch Trimmer, Sidestay Assy, Lock Pins Assembly ... Open the MLG Doors for Maintenance
EFF : ALL 05-51-14 R SROS
Page 602 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-12-00-410-801 32-21-00-220-801 32-22-00-010-801 32-22-00-410-801 32-31-00-710-801 34-11-15-200-801
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53-15-11-200-801 56-11-11-200-801 56-11-12-200-801 56-12-11-200-801 56-21-15-200-801 71-00-00-200-803 72-00-00-200-811 05-51-14-991-001
Close the MLG Doors after Maintenance Detailed Inspection of the Nose Gear Structure comprising : Main Fitting (Barrel), Sliding Member, Torque Links, Drag Stay Upper and Lower Arm .... Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance Functional Test of the Normal Extension and Retraction System Inspection/Check of the Pitot Probe (9DA1, 9DA2, 9DA3) Detailed Inspection of the Radome (110AL) Inspection of the Windshields (3DG1,3DG2). Inspection of the Fixed Windows (7DG1,7DG2) Inspection of the Sliding Windows (8DG1,8DG2). Detailed Visual Inspection of Passenger Cabin Window Panes including Passenger/ Crew Door and Emergency Exit Window Panes Inspection after a Birdstrike and Foreign Object Damage Inspection Procedure After Birdstrike (Foreign Object Damage) Fig. 601
3. __________ Job Set-up Subtask 05-51-14-941-050 A. Safety Precautions (1) Put the safety barriers in position. (2) Put wheel chocks in position at the main landing gears. (3) Put a warning notice in position in the cockpit to tell persons not to operate the systems. Subtask 05-51-14-860-052 B. 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) Pressurize the Yellow hydraulic system (Ref. TASK 29-00-00-863-803). EFF : ALL 05-51-14 SROS
Page 603 Jan 01/07
(4) Pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-802). Subtask 05-51-14-010-050 C. Get Access (1) Open the NLG doors (Ref. TASK 32-22-00-010-801). (2) Open the MLG doors (Ref. TASK 32-12-00-010-801). (3) Put an adjustable access platform in position near the area you must inspect. (4) Install the safety devices on the landing gear (Ref. TASK 32-00-00481-801). Subtask 05-51-14-860-050 D. Aircraft Maintenance Configuration (1) Extend the flaps to the FULL position (Ref. TASK 27-50-00-866-801). (2) Extend the spoilers (Ref. TASK 27-60-00-866-801). (3) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (4) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802). (5) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803). (6) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). 4. Procedure _________ Subtask 05-51-14-869-050 A. General NOTE : All the necessary inspections are visual unless the text gives ____ other instructions. Operators can refer to the Non-destructive Testing Manual (NTM) and use non-destructive procedures.
EFF : ALL 05-51-14 R SROS
Page 604 Jan 01/07
(1) Inspection recommendations on composite parts (a) if you find damage (signs of impact, damaged paintwork, abrasions, scratches or dents) on a composite part, you must do an inspection of the related damaged area for delamination and internal damage. (2) If there is damage to the aircraft structure, refer to the Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures. Subtask 05-51-14-210-050 B. Inspection of the Radome the Windows and the external structure of the fuselage (Ref. TASK 53-15-11-200-801) (Ref. TASK 56-11-11-200-801) (Ref. TASK 5611-12-200-801) (Ref. TASK 56-12-11-200-801) (Ref. TASK 56-21-15-200-801) (Ref. TASK 34-11-15-200-801) (Ref. Fig. 601/TASK 05-51-14-991-001) NOTE : All the necessary inspections are visual unless specified ____ differently in the text procedure. Operators can refer to the Non Destructive Testing Manual (NTM) and use non destructive procedure.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the Radome | | | | | | | | | | | | | | | | A.| |Examine the radome for erosion, | X | | | | | | | |delamination and core damage. | | | | | | | | |Make sure that the lightning arrestors | | | | | | | | |are in the correct condition | | | | | | | | |(Ref. TASK 53-15-11-200-801) | | | | | | | | | | | | | | | |2. | |Inspection of the Windshields, the | | | | | | | | |Fixed Windows and the Sliding Windows | | | | | | | | | | | | | | | | A.| |Examine the windshields, the fixed | X | | | | | | | |windows and the sliding windows for: | | | | | | | | |-delamination, cracking, change in | | | | | | | | | color | | | | | | | | | (Ref. TASK 56-11-11-200-801) | | | | | | | | | (Ref. TASK 56-11-12-200-801) | | | | | | | | | (Ref. TASK 56-12-11-200-801) | | | | | |
EFF : ALL 05-51-14 SROS
Page 605 Jul 01/02
Belly Fairing Structure Figure 601/TASK 05-51-14-991-001 EFF : ALL 05-51-14 R SROS
Page 606 Apr 01/02
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | |If you find damage (heavy bird strike) | | X | | | | | | |(1) Examine the windshield and sliding | | | | | | | | | window pillars and frames | | | | | | | | | internally for : | | | | | | | | | .distortion,cracks and pulled or | | | | | | | | | torn fasteners. | | | | | | | | | | | | | | | |3. | |Inspection of the Cabin Windows | | | | | | | | | | | | | | | | A.| |Examine the cabin windows for: | X | | | | | | | |-cracks, delamination and crazing. | | | | | | | | | (Ref. TASK 56-21-15-200-801). | | | | | | | | | | | | | | | |4. | |Inspection of the External Structure of| | | | | | | | |the Fuselage | | | | | | | | | | | | | | | | A.| |Examine the skin, the doors, the | X | | | | | | | |fairings, the fillets for: | | | | | | | | |-distortion, cracks, pulled or torn | | | | | | | | | fasteners and erosion and damaged | | | | | | | | | paintwork. | | | | | | | | |(1) If you find erosion | | | | | | | | | - check for delamination. | | X | | | | | | |(2) If you find other damage, get | | X | | | | | | | access to and internally examine: | | | | | | | | | - all the frames, the stringers, | | | | | | | | | the clips, the fittings and the | | | | | | | | | component mounts at and near the | | | | | | | | | location of the damage for: | | | | | | | | | . damaged paintwork, distortion | | | | | | | | | and pulled or torn fasteners | | | | | | | | | - all the components, the pipes, | | | | | | | | | the ducts, the electrical | | | | | | | | | harnesses, the cables, the | | | | | | | | | pulleys and the mechanical | | | | | | | | | linkages for: | | | | | | | | | - distortion, cracks, rupture, | | | | | | | | | breaks and fluid leakage. | | | | | | | B.| |Examine all the antennas, the | | | | | | | | |TAT sensor, the pitot probe | X | | | | | | | |the angle-of-attack sensor the | | | | | | | | |drain masts for: | | | | | | | | |- cracks and damage. | | | | | |
EFF : ALL 05-51-14 SROS
Page 607 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | C.| |Examine all the exterior lights (anti- | X | | | | | | | |collision lights, landing lights, | | | | | | | | |navigation lights, wing and engine scan| | | | | | | | |lights, logo lights) for: | | | | | | | | |-damage. | | | | | | | D.| |Examine all the exterior video systems | X | | | | | | | |(if installed) for: | | | | | | | | |- damage. | | | | | | | | | | | | | | | |5. | |Inspection of the Belly Fairing | | | | | | | | | | | | | | | | A.| |Examine externally all the belly | X | | | | | | | |fairing panels, specially the leading- | | | | | | | | |edge root fairing and the upper and | | | | | | | | |lower wing fairings, for: | | | | | | | | |- erosion, distortion, cracks, pulled | | | | | | | | | or torn fasteners and damaged | | | | | | | | | paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the damaged panels and | | X | | | | | | | internally examine the belly | | | | | | | | | fairing structure for: | | | | | | | | | .cracks, buckling and damaged | | | | | | | | | paintwork. | | | | | | | | | (2) Examine all the components, | | | | | | | | | pipes, ducts, electrical | | | | | | | | | harnesses and their mounts, for: | | | | | | | | | -distortion, cracks, breaks and | | X | | | | | | | fluid leakage. | | | | | | | | | Make sure that the components | | | | | | | | | are correctly installed and | | | | | | | | | attached | | | | | | ------------------------------------------------------------------------------Subtask 05-51-14-210-053 C. Inspection of the Landing Gear and the Landing Gear Doors (Ref. TASK 32-11-00-220-801) (Ref. TASK 32-21-00-220-801) NOTE : All the necessary inspections are visual unless specified ____ differently in the test procedure. Operators can refer to the Non Destructive Testing Manual (NTM) and use non destructive procedure.
EFF : ALL 05-51-14 SROS
Page 608 Jan 01/07
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the Nose Landing Gear and| | | | | | | | |NLG Doors | | | | | | | | | | | | | | | | A.| |If the NLG was extended when the bird | X | | | | | | | |or hail strike occurred, examine: | | | | | | | | |- the rods, the components, the lights,| | | | | | | | | the electrical harnesses that are on | | | | | | | | | the NLG, for: | | | | | | | | | . damage | | | | | | | | | (Ref. TASK 32-21-00-220-801) | | | | | | | | |- the forward and aft doors and the | | | | | | | | | fixed fairing, for: | | | | | | | | | . erosion, cracks, damaged paintwork | | | | | | | | | and pulled or torn fasteners | | | | | | | | | | | | | | | | B.| |If the NLG was retracted when the bird | X | | | | | | | |or hail strike occurred, examine the | | | | | | | | |forward and aft doors and the fixed | | | | | | | | |fairing, for: | | | | | | | | |- erosion, cracks, dents, scratches, | | | | | | | | | damaged paintwork and pulled or torn | | | | | | | | | fasteners | | | | | | | | | | | | | | | | | | | | | | | | |2. | |Inspection of the Main Landing Gear and| | | | | | | | |MLG Doors | | | | | | | | | | | | | | | | A.| |If the MLG was extended when the bird | X | | | | | | | |or hail strike occurred, examine: | | | | | | | | |- the rods, the components, the pipes, | | | | | | | | | the electrical harnesses that are on | | | | | | | | | the MLG, for: | | | | | | | | | . damage | | | | | | | | | (Ref. TASK 32-11-00-220-801) | | | | | | | | |- the hinged doors and the fixed and | | | | | | | | | hinged fairings, for: | | | | | | | | | . erosion, cracks, damaged paintwork | | | | | | | | | and pulled or torn fasteners. | | | | | | | | | | | | | | | | B.| |If the MLG was retracted when the bird | X | | | | | | | |or hail strike occurred, examine the | | | | | | | | |hinged doors and the fixed and hinged | | | | | | | | |fairings, for: | | | | | |
EFF : ALL 05-51-14 R SROS
Page 609 Apr 01/02
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | |- erosion, cracks, dents, scratches, | | | | | | | | | damaged paintwork and pulled or torn | | | | | | | | | fasteners. | | | | | | ------------------------------------------------------------------------------R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-14-210-058 D. Inspection of the Nacelles and the Engines (Ref. TASK 72-00-00-200-811) NOTE : All the necessary inspections are visual unless specified ____ differently in the test procedure. Operators can refer to the Non Destructive Testing Manual (NTM) and use the non destructive procedure. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the Engines and the | | | | | | | | |Nacelles | | | | | | | | | | | | | | | | A.| |Examine the engine and the nacelle | X | | | | | | | |(Ref. TASK 72-00-00-200-811) | | | | | | ------------------------------------------------------------------------------**ON A/C 701-749, Subtask 05-51-14-210-058-A D. Inspection of the Nacelles and the Engines (Ref. TASK 71-00-00-200-803) NOTE : All the necessary inspections are visual unless specified ____ differently in the test procedure. Operators can refer to the Non Destructive Testing Manual (NTM) and use the non destructive procedure.
EFF : ALL 05-51-14 SROS
Page 610 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the Engines and the | | | | | | | | |Nacelles | | | | | | | | | | | | | | | | A.| |Examine the engine and the nacelle | X | | | | | | | |(Ref. TASK 71-00-00-200-803) | | | | | | ------------------------------------------------------------------------------**ON A/C ALL Subtask 05-51-14-210-055 E. Inspection of the Pylons NOTE : All the necessary inspections are visual unless specified ____ differently in the text procedure. Operators can refer to the Non Destructive Testing Manual (NTM) and use non destructive procedure.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the Pylons | | | | | | | | | | | | | | | | A.| |Examine the pylons externally for | X | | | | | | | |erosion, distortion, cracks, pulled | | | | | | | | |or torn fasteners and damaged | | | | | | | | |paintwork. | | | | | | | | |If you find damage: | | | | | | | | |(1) If you find only erosion: | | | | | | | | | - no other inspection operations | | | | | | | | | are necessary. | | | | | | | | |(2) If you find other damage: | | X | | | | | | | - examine the pylon internally for:| | | | | | | | | .distortion, cracks, pulled or | | | | | | | | | torn fasteners and damaged | | | | | | | | | paintwork | | | | | | | | | - examine the components, the | | | | | | | | | pipes, the ducts, the electrical | | | | | | | | | harnesses and their mounts for: | | | | | | | | | distortion, cracks, rupture, | | | | | | | | | breaks and fluid leakage. | | | | | |
EFF : ALL 05-51-14 SROS
Page 611 Jan 01/07
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| ------------------------------------------------------------------------------Subtask 05-51-14-210-056 F. Inspection of the Stabilizer NOTE : All the necessary inspections are visual unless specified ____ differently on the text procedure. Operators can refer to the Non Destructive Testing Manual (NTM) and use non destructive procedure.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the Vertical Stabilizer | | | | | | | | | | | | | | | | A.| |Examine the dorsal fin, the leading | | | | | | | | |edge and the tip fairing | X | | | | | | | |externally for: | | | | | | | | |- erosion, delamination, cracks, pulled| | | | | | | | | or torn fasteners, honeycomb | | | | | | | | | delamination, core damage and damaged| | | | | | | | | paintwork. | | | | | | | | | If you find damaged: | | | | | | | | | (1) If you find erosion | | | | | | | | | - check for delamination | | X | | | | | | | (2) If you find other damage: | | | | | | | | | - examine internally the area at | | X | | | | | | | and near the damage for: | | | | | | | | | . distortion, cracks, pulled or| | | | | | | | | torn fasteners, honeycomb | | | | | | | | | delamination, core damage | | | | | | | | | and damaged paintwork. | | | | | | | | | | | | | | | | B.| |Examine the spar box of the vertical | X | | | | | | | |stabilizer for erosion, scores and | | | | | | | | |damaged paintwork. | | | | | | | | | | | | | | | | C.| |Examine the rudder and the trailing| | | | | | | | |edge access doors externally for: | | | | | | | | |- erosion, distortion, cracks, pulled | X | | | | | | | | or torn fasteners, honeycomb | | | | | |
EFF : ALL 05-51-14 SROS
Page 612 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | delamination, core damage and damaged| | | | | | | | | paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) If you find only erosion | | | | | | | | | - no other inspection operations | | | | | | | | | are necessary. | | | | | | | | | (2) If you find other damage | | | | | | | | | - examine the rudder hinge and | | X | | | | | | | the actuator attach fittings | | | | | | | | | for: | | | | | | | | | .damaged paintwork,cracks and | | | | | | | | | distortion. | | | | | | | | | | | | | | | |2. | |Inspection of the Horizontal Stabilizer| | | | | | | | | | | | | | | | A.| |Examine the leading edge and the tip | X | | | | | | | |fairing externally for: | | | | | | | | |- erosion, distortion, cracks, pulled | | | | | | | | | or torn fasteners, core damage and | | | | | | | | | damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) If you find only erosion | | | | | | | | | - no other inspection operations | | | | | | | | | are necessary. | | | | | | | | | (2) If you find other damage | | | | | | | | | - examine the leading edge and | | | | | | | | | tip fairing internally for: | | | | | | | | | .cracks, distortion, pulled or | | X | | | | | | | torn fasteners and damage | | | | | | | | | paintwork. | | | | | | | | | | | | | | | | B.| |Examine the spar box of the horizontal | | | | | | | | |stabilizer for erosion, scores and | X | | | | | | | |damaged paintwork. | | | | | | | | | | | | | | | | C.| |Examine the elevators and the trailing | | | | | | | | |access doors externally for erosion, | X | | | | | | | |cracks, pulled or torn fasteners, | | | | | | | | |honeycomb delamination, core damage and| | | | | | | | |damaged paintwork. | | | | | | | | |If you find damage | | | | | | | | |(1) If you find only erosion | | | | | | | | | - no other inspection operations | | | | | |
EFF : ALL 05-51-14 SROS
Page 613 Jan 01/07
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | are necessary. | | | | | | | | |(2) If you find other damage | | | | | | | | | - examine the elevator hinge and | | X | | | | | | | the actuator attach fittings for:| | | | | | | | | .distortion, cracks and damaged | | | | | | | | | paintwork. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-14-210-057 G. Inspection of the Wing (Ref. TASK 28-10-00-910-801). NOTE : All the necessary inspections are visual unless specified in the ____ text procedure. Operators can refer to the Non destructive Testing Manual (NTM) and use non destructive testing procedure.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the Wing | | | | | | | | | | | | | | | | A.| |Examine the upper and lower surface of | | | | | | | | |wing for: | X | | | | | | | |-erosion distortion and damage | | | | | | | | | If you find damage | | | | | | | | | (1) Get access to the internal | | X | | | | | | | structure (the other side of the | | | | | | | | | damage) | | | | | | | | | (Ref. TASK 28-10-00-910-801) | | | | | | | | | (2) Examine the fuel tank sealant | | | | | | | | | the ribs, the riblets, the | | | | | | | | | stringers, the brackets, the | | | | | | | | | plates, the components, the | | | | | | | | | harnesses for: | | | | | | | | | - damage | | | | | | | | | | | | | | | | B.| |Examine externally the leading edge, | | | | | | | | |the fillets and the slats for erosion, | X | | | | | | | |distortion, cracks, pulled or torn | | | | | | | | |fasteners and damaged paintwork. | | | | | |
EFF : ALL 05-51-14 SROS
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | |If you find damage: | | | | | | | | |(1) If you find only erosion | | | | | | | | | - no other inspection operations | | | | | | | | | are necessary. | | | | | | | | |(2) If you find other damage | | | | | | | | | - examine internally the leading | | | | | | | | | edge section at and near the | | X | | | | | | | damage for distortion, cracks, | | | | | | | | | pulled or torn fasteners and | | | | | | | | | damaged paintwork. | | | | | | | | |(3) Examine the ducts and the related | | | | | | | | | attach points for damage. | | | | | | | | | - examine the slat section for | | | | | | | | | distortion, cracks, pulled or | | | | | | | | | torn fasteners and damaged | | | | | | | | | paintwork | | | | | | | | | - examine the actuators, the slat | | X | | | | | | | tracks and the slat-track attach | | | | | | | | | points for damage | | | | | | | | | - examine the rollers of the slat | | X | | | | | | | tracks for brinelling. | | | | | | | | | | | | | | | | C.| |Examine externally the trailing edge | | | | | | | | |falsework, the flaps, the ailerons | | | | | | | | |and spoilers for erosion, distortion, | X | | | | | | | |cracks, pulled or torn fasteners and | | | | | | | | |damaged paintwork. | | | | | | | | |If you find damage: | | | | | | | | |(1) If you find only erosion: | | | | | | | | | - no other inspection operations | | | | | | | | | are necessary. | | | | | | | | |(2) If you find other damage: | | | | | | | | | - get access to the internal | | X | | | | | | | structure (the other side of the | | | | | | | | | damage). | | | | | | | | | - examine the falsework internally | | X | | | | | | | at and near the damage for | | | | | | | | | damaged paintwork, distortion, | | | | | | | | | cracks, pulled or torn fasteners | | | | | | | | | - examine the flap carriages and | | X | | | | | | | the fairings for distortion, | | | | | | | | | cracks and damaged paintwork | | | | | | | | | - examine the flap tracks for | | X | | | | | | | brinelling | | | | | | | | | - examine the aileron servo| | | | | | | | | controls and the hinge fittings | | | | | | | | | for damage | | | | | | | | | - examine the spoiler servo| | X | | | |
EFF : ALL 05-51-14 SROS
Page 615 Jan 01/07
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | controls and the hinge fittings | | | | | | | | | for damage. | | | | | | | | | | | | | | | | D.| |Examine the wing tips for erosion, | X | | | | | | | |distortion, cracks, pulled or torn | | | | | | | | |fasteners and damaged paintwork. | | | | | | | | | | | | | | | | E.| |Examine the exterior lights (strobe | X | | | | | | | |lights at the wing tips, navigation | | | | | | | | |lights). | | | | | | | | | | | | | | | | F.| |Examine the main structure of the wing | X | | | | | | | |for erosion and scores. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-14-410-050 H. Close Access (1) Remove the safety devices from on the landing gears (Ref. TASK 32-0000-081-801) . (2) Close all the access panels that you opened during the procedure. (3) Close the NLG doors (Ref. TASK 32-22-00-410-801). (4) Close the MLG doors (Ref. TASK 32-12-00-410-801). (5) Remove the access platform(s). Subtask 05-51-14-860-051 J. Put the system back to its operational configuration. (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Retract the flaps (Ref. TASK 27-50-00-866-802). (3) Retract the slats (Ref. TASK 27-80-00-866-802). (4) Retract the spoilers (Ref. TASK 27-60-00-866-802).
EFF : ALL 05-51-14 R SROS
Page 616 Jan 01/07
Subtask 05-51-14-710-050 K. Do the tests below NOTE : The tests below are necessary only if: ____ - you did work on the system subsequent to the inspection for damage - you found damage on the structure adjacent to the landing gear doors or a flight control surface. (1) Operate the ailerons 3 times. Make sure that the travel is full and that the ailerons move freely (Ref. TASK 27-14-00-710-801). (2) |Operate the rudder 3 times. Make sure that the travel is full and that the rudder moves freely (Ref. TASK 27-24-00-710-801). (3) Operate the elevator 3 times. Make sure that the travel is full and that the elevator moves freely (Ref. TASK 27-34-00-710-801). (4) Operate the THS 3 times. Make sure that the travel is full that the THS moves freely (Ref. TASK 27-44-00-710-801). (5) Operate the flaps 3 times. Make sure that the travel is full and that the flaps move freely (Ref. TASK 27-54-00-710-801). (6) Operate the spoilers 3 times. Make sure that the travel is full and that the spoilers move freely (Ref. TASK 27-64-00-710-801). (7) Operate the slats 3 times. Make sure that the travel is full and that the slats move freely (Ref. TASK 27-84-00-710-801). (8) Retract and extend the landing gear 3 times. Make sure that the landing gear and the doors move freely (Ref. TASK 32-31-00-710-801). (9) If you find damage only on the landing gear doors or on the structure adjacent to the landing gear doors: (a) Open the NLG doors (Ref. TASK 32-22-00-010-801). (b) Make sure that the NLG doors move freely. (c) Close the NLG doors (Ref. TASK 32-22-00-410-801). (d) Open the MLG doors (Ref. TASK 32-12-00-010-801). (e) Make sure that the MLG doors move freely.
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Page 617 Apr 01/98
(f) Close the MLG doors (Ref. TASK 32-12-00-410-801). 5. Close-up ________ R R
Subtask 05-51-14-860-054 A. Put the Aircraft back to its Initial Configuration
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(1) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801).
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(2) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802).
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(3) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803).
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(4) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). Subtask 05-51-14-942-050
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B. Put the Aircraft back to its Initial Configuration (1) Remove the warning notice(s). (2) Remove the ground support and maintenance equipment, the special and standard tools and all other items. (3) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-51-14 SROS
Page 618 Apr 01/02
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_____________________________________________________________ INSPECTION AFTER A TIRE BURST OR TREAD THROW OR WHEEL FAILURE ________________ INSPECTION/CHECK TASK 05-51-15-200-801
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Inspection of the Aircraft after a Tire Burst or Tread Throw or Wheel Failure 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
safety barriers warning notice wheel chocks adjustable access platform 16.8 m (55 ft. 1 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------05-51-16-200-801 24-41-00-861-801 24-41-00-862-801 27-14-00-710-801 27-50-00-866-801 27-50-00-866-802 27-54-00-710-801 27-60-00-866-801 27-60-00-866-802 27-80-00-866-801 27-80-00-866-802 27-84-00-710-801 29-00-00-863-801
Inspection After Brake Overheat Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Operational Test of the Aileron and Hydraulic Actuation Extension of the Flaps on the Ground Retraction of the Flaps on the Ground Operational Test of the Flap System Extension of the Spoilers for Maintenance Retraction of the Spoilers after Maintenance Extension of the Slats on the Ground Retraction of the Slats on the Ground Operational Test of the Slat System Pressurize the Green Hydraulic System with the Ground Hydraulic Supply
EFF : ALL 05-51-15 SROS
Page 601 Jul 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------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 32-00-00-081-801 32-00-00-481-801
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32-12-00-010-801 32-12-00-410-801 32-22-00-010-801 32-22-00-410-801 32-31-00-710-801 34-51-00-740-801 34-52-00-710-801 53-12-13-000-801 72-00-00-200-811 78-31-00-710-804 78-31-00-740-802 05-51-15-991-001
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) Removal of the Safety Devices from the Landing Gears Installation of the Safety Devices on the Landing Gears Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance Functional Test of the Normal Extension and Retraction System BITE Test of the DME Operational test of the lights of the ATC control unit Removal of the Avionics-Compartment Floor Panels Inspection Procedure After Birdstrike (Foreign Object Damage) Thrust Reverser Cycling Test (MCDU) Test of the Thrust Reverser Deployment and Stowage (Engine not Running) Fig. 601
3. __________ Job Set-up Subtask 05-51-15-941-050 A. Safety Precautions (1) Put the safety barriers in position. R
(2) Put wheel chocks in position at the main landing gear. (3) Put a warning notice in position in the cockpit to tell persons not to operate the systems.
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Page 602 Jul 01/05
Subtask 05-51-15-860-052 B. Aircraft Maintenance Configuration (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801). (2) Pressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (3) Pressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803). (4) Pressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802). Subtask 05-51-15-010-050 C. Get Access (1) Open the NLG doors (Ref. TASK 32-22-00-010-801). (2) Open the MLG doors (Ref. TASK 32-12-00-010-801). (3) Put an adjustable access platform in position near the area that you must inspect. (4) Install the safety devices on the landing gear (Ref. TASK 32-00-00481-801). Subtask 05-51-15-860-050 D. Aircraft Maintenance Configuration (1) Extend the flaps to full position (Ref. TASK 27-50-00-866-801). (2) Extend the slats to full position (Ref. TASK 27-80-00-866-801). (3) Extend the spoilers to full position (Ref. TASK 27-60-00-866-801). (4) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (5) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803).
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Page 603 Apr 01/98
(6) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802). (7) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). 4. Procedure _________ (Ref. Fig. 601/TASK 05-51-15-991-001) Subtask 05-51-15-869-050 A. General NOTE : All the necessary inspections are visual unless the text gives ____ other instructions. Operators can refer to the Non-destructive Testing Manual (NTM) and use non-destructive procedures. (1) Inspection recommendations on composite parts R R
(a) If you find damage (signs of impact, damaged paintwork, abrasions, scratches or dents) on a composite part, you must do an inspection of the related damaged area for delamination and internal damage. (2) If there is damage to the aircraft structure, refer to the Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures. (3) If a tire burst occurs when the landing gear is fully retracted, then only examine the items of equipment below: - the landing gear well, - the landing gear doors, - the landing gear assemblies, - the hydraulic bay compartment. (4) If you replace a component because of an inspection, you must do an operational test of the related system.
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Page 604 Jul 01/05
Structure of the Belly Fairing Figure 601/TASK 05-51-15-991-001 EFF : ALL 05-51-15 R SROS
Page 605 Apr 01/02
Subtask 05-51-15-210-051 B. Inspection of the Brakes (1) If a tire burst occurs because of an emergency operation or locking of the brackes, examine the brakes (Ref. TASK 05-51-16-200-801). (2) During the inspection, if you find tire debris, remove them. Subtask 05-51-15-210-050 C. Inspection of the Fuselage Lower Section (Ref. Fig. 601/TASK 05-51-15-991-001) (Ref. TASK 34-51-00-740-801) (Ref. TASK 34-52-00-710-801) (Ref. TASK 5312-13-000-801) NOTE : All the necessary inspections are visual unless specified ____ differently in the procedure text. Operators can refer to the Non-Destructive Testing Manual (NTM) and use non destructive procedures. If a tire burst occurs when the landing gear is fully retracted, examine only: - the landing gear well - the landing gear doors - the landing gear - the hydraulics compartment. If you replace a component after an inspection, you must do an operational test of the related system.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Fuselage Lower | | | | | | | | | Section. This includes the | | | | | | | | | cargo doors | | | | | | | | | | | | | | | | A.| | Examine the skin panels for | X | | | | | | | | distortion, pulled or torn fasteners, | | | | | | | | | scratches, dents, damaged paintwork. | | | | | | | | | If you find damage : | | | | | | | | | (1) Remove the floor panels of the | | X | | | | | | | FWD cargo compartment | | | | | | | | | Remove the floor panels of the | | | | | | | | | avionics compartment. | | | | | | | | | (Ref. TASK 53-12-13-000-801) | | | | | | | | | - examine the frames, the | | | | | |
EFF : ALL 05-51-15 SROS
Page 606 Jan 01/06
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | stringers, the clips, the | | | | | | | | | fittings for: | | | | | | | | | . distortion, cracks, pulled or | | | | | | | | | torn fasteners and damaged | | | | | | | | | paintwork adjacent to the | | | | | | | | | damaged area. | | | | | | | | | | | | | | | | | | (2) Examine the components, the | | X | | | | | | | pipes, the ducts, the electrical | | | | | | | | | harnesses, the control cables, the| | | | | | | | | pulleys, the mounts, the safety | | | | | | | | | devices, for : | | | | | | | | | - rupture, cracks, impacts, and | | | | | | | | | fluid leakage. | | | | | | | | | | | | | | | | B.| | Examine externally : | | | | | | | | | - the ATC, DME and TCAS antennas which| | | | | | | | | are on the lower fuselage | | | | | | | | | - the drain mast | X | | | | | | | | - the TAT sensor | | | | | | | | | - the pitot probes | | | | | | | | | - the angle-of-attack sensor | | | | | | | | | for cracks, dents, scratches. | | | | | | | | | If you find damage : | | | | | | | | | (1) Do an operational test of the DME | | X | | | | | | | (Ref. TASK 34-51-00-740-801). | | | | | | | | | | | | | | | | | | (2) Do an operational test of the | | X | | | | | | | ATC/MODE | | | | | | | | | (Ref. TASK 34-52-00-710-801). | | | | | | | | | | | | | | | |2. | | Inspection of the NLG well. | | | | | | | | | | | | | | | | A.| | Examine the structure, the components,| | | | | | | | | the pipes, the ducts, the electrical | X | | | | | | | | harnesses, the manifolds, the mounts | | | | | | | | | for: | | | | | | | | | - cracks, rupture, pulled or torn | | | | | | | | | fasteners, impacts, fluid leakage, | | | | | | | | | condition of the safety devices, and| | | | | | | | | damaged paintwork. | | | | | | | | | | | | | | | |3. | | Inspection of the Belly Fairing | | | | | | | | | (Ref. Fig 601/TASK 05-51-15-991-001) | | | | | | | | | | | | | | | | A.| | Examine externally all the access | | | | | | | | | panels and doors of the belly fairing | X | | | | | | | | and the lower wing fairing for : | | | | | | EFF : ALL 05-51-15 R SROS
Page 607 Jan 01/06
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - cracks, impacts, loose, pulled or | | | | | | | | | torn fasteners and damaged | | | | | | | | | paintwork. | | | | | | | | | Make sure that the panels are | | | | | | | | | correctly attached. | | | | | | | | | If you find damage : | | | | | | | | | (1) Remove the access panels or open | | | | | | | | | the access doors and internally | | | | | | | | | examine the belly fairing | | X | | | | | | | structure, the hydraulics | | | | | | | | | compartment, all the components | | | | | | | | | for : | | | | | | | | | - cracks, buckling, damaged | | | | | | | | | paintwork. | | | | | | | | | | | | | | | | | | (2) Examine all the components, the | | | | | | | | | pipes, the ducts, the electrical | | X | | | | | | | harnesses and the mounts for : | | | | | | | | | - distortion, cracks, breaks, | | | | | | | | | fluid leakage. | | | | | | | | | Also examine the safety devices | | | | | | | | | and make sure that the components | | | | | | | | | are correctly installed. | | | | | | | | | | | | | | | |4. | | Inspection of the MLG Well | | | | | | | | | | | | | | | | A.| | Examine the protective panels, the | X | | | | | | | | structure of the main landing gear | | | | | | | | | well for : | | | | | | | | | - distortion, damage, pulled or torn | | | | | | | | | fasteners, delamination, honeycomb | | | | | | | | | damage and damaged components. | | | | | | | | | | | | | | | | B.| | Examine the fuel and hydraulic | | | | | | | | | components, the mounts for : | X | | | | | | | | - distortion, leakage, burns marks or | | | | | | | | | damage. | | | | | | | | | Make sure that they are correctly | | | | | | | | | attached. | | | | | |
EFF : ALL 05-51-15 SROS
Page 608 Jan 01/06
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| ------------------------------------------------------------------------------Subtask 05-51-15-210-053 D. Inspection of the Landing Gear and the Landing Gear Doors NOTE : All the necessary inspections are visual unless specified ____ differently in the text procedure. Operators can refer to the Non-Destructive Testing Manual (NTM) and use non destructive procedures. If a tire burst occurs when the landing gear is fully retracted, examine only: - the landing gear well - the landing gear doors - the landing gear - the hydraulics compartment. If you replace a component after an inspection, you must do an operational test of the related system. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Main Landing Gear | | | | | | | | | | | | | | | | A.| | Examine the applicable main landing | | | | | | | | | gear in the area of the incident for: | X | | | | | | | | - fluid and hydraulic leakage damage | | | | | | | | | to hydraulic hoses | | | | | | | | | - damage to hydraulic pipes and | | | | | | | | | harnesses. | | | | | | | | | | | | | | | | B.| | Examine the bogie beam assembly and | | | | | | | | | its components for: | | | | | | | | | - damaged paintwork, distorsion, | | | | | | | | | damage. | | | | | | | | | Make sure that the components are in | | | | | | | | | good condition and correctly attached.| | | | | | | | | | | | | | | | C.| | Examine the sliding tube, the main | | | | | | | | | fitting the components for: | | | | | | | | | - damaged chromium plating, damaged | | | | | | | | | paintwork, hydraulic and fluid | | | | | |
EFF : ALL 05-51-15 R SROS
Page 609 Jan 01/02
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | leakage, distorsion, damage of the | | | | | | | | | hose and hydraulic pipes. | | | | | | | | | Make sure that the MLG leg components | | | | | | | | | are correctly attached. | | | | | | | | | | | | | | | |2. | | Inspection of the Main Landing Gear | | | | | | | | | Door | | | | | | | | | | | | | | | | A.| | Examine the honeycomb structure of the| | | | | | | | | MLG door for: | | | | | | | | | - delamination, core damage and | X | | | | | | | | cracks. | | | | | | | | | | | | | | | | B.| | Examine the door hinge actuator | | | | | | | | | attachment, the proximity sensor | | | | | | | | | attachment and the uplock roller | | | | | | | | | attachment for: | X | | | | | | | | - separation distorsion and damage. | | | | | | | | | | | | | | | | C.| | Examine the door actuator and its | | | | | | | | | hydraulic hoses and pipes for: | X | | | | | | | | - fluid leakage, distorsion and | | | | | | | | | damage. | | | | | | | | | | | | | | | |3. | | Inspection of the Nose Landing Gear | | | | | | | | | | | | | | | | A.| | Examine the nose landing gear in the | | | | | | | | | area of the incident. | X | | | | | | | | Examine the harnesses for: | | | | | | | | | - distorsion and damage. | | | | | | | | | | | | | | | | B.| | Examine the hydraulic hoses, the | | | | | | | | | hydraulic pipes, the components of the| X | | | | | | | | nose wheel steering system for: | | | | | | | | | - hydraulic leakage, distorsion and | | | | | | | | | damage. | | | | | | | | | | | | | | | | C.| | Examine the nose landing gear shock | | | | | | | | | absorber, the strut for: | X | | | | | | | | - chromium plating damage, loose | | | | | | | | | fittings and fluid leakage. | | | | | | | | | | | | | | | |4. | | Inspection of the NLG Doors | | | | | |
EFF : ALL 05-51-15 R SROS
Page 610 Jan 01/02
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | | | | | | | | A.| | Examine the honeycomb structure of the| | | | | | | | | aft and forward doors | | | | | | | | | - for delamination, pulled or torn | X | | | | | | | | fasteners, dents, scratches and | | | | | | | | | damaged paintwork. | | | | | | | | | | | | | | | | B.| | Examine the door actuator, the hinges,| | | | | | | | | the attachments and the actuating | | | | | | | | | cylinder for: | X | | | | | | | | - fluid leakage, distorsion, damage | | | | | | | | | and damaged paintwork. | | | | | | ------------------------------------------------------------------------------R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-15-210-057 E. Inspection of the Nacelles and the Engines (Ref. TASK 72-00-00-200-811) NOTE : All the necessary inspections are visual unless specified ____ differently in the text procedure. Operators can refer to the Non-Destructive Testing Manual (NTM) and use non destructive procedures. If a tire burst occurs when the landing gear is fully retracted, examine only: - the landing gear well - the landing gear doors - the landing gear - the hydraulics compartment. If you replace a component after an inspection, you must do an operational test of the related system.
EFF : ALL 05-51-15 SROS
Page 611 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Engines and the | | | | | | | | | Nacelles | | | | | | | | | | | | | | | | A.| | Examine the engines and the nacelles | X | | | | | | | |(Ref. TASK 72-00-00-200-811) | | | | | | ------------------------------------------------------------------------------**ON A/C 701-749, Subtask 05-51-15-210-057-A E. Inspection of the Nacelles and the Engines NOTE : All the necessary inspections are visual unless specified ____ differently in the text procedure. Operators can refer to the Non-Destructive Testing Manual (NTM) and use non destructive procedures. If a tire burst occurs when the landing gear is fully retracted, examine only: - the landing gear well - the landing gear doors - the landing gear - the hydraulics compartment. If you replace a component after an inspection, you must do an operational test of the related system. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Engines and the | | | | | | | | | Nacelles | | | | | | | | | | | | | | | | A.| | Examine the engines and the nacelles | X | | | | | -------------------------------------------------------------------------------
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Page 612 Jul 01/05
**ON A/C ALL Subtask 05-51-15-210-055 F. Inspection of the Pylons NOTE : All the necessary inspections are visual unless specified ____ differently in the procedure text. Operators can refer to the Non-Destructive Testing Manual (NTM) and use non destructive procedures. If a tire burst occurs when the landing gear is fully retracted, examine only: - the landing gear well - the landing gear doors - the landing gear - the hydraulics compartment. If you replace a component after an inspection, you must do an operational test of the related system.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Pylons | | | | | | | | | | | | | | | | A.| | Examine the pylons externally for | | | | | | | | | distortions, cracks, scratches, dents | | | | | | | | | pulled or torn fasteners and damaged | X | | | | | | | | paintwork. | | | | | | | | | If you find damage : | | | | | | | | | (1) Examine the internal structure of | | | | | | | | | the pylon for distortion, cracks, | | X | | | | | | | pulled or torn fasteners, damaged | | | | | | | | | structure and damaged paintwork. | | | | | | | | | (2) Examine the components, the pipes,| | X | | | | | | | the ducts, the electrical | | | | | | | | | harnesses, the mounts for | | | | | | | | | distortion, rupture, breaks, and | | | | | | | | | fluid leakage. | | | | | | -------------------------------------------------------------------------------
EFF : ALL 05-51-15 SROS
Page 613 Jul 01/05
Subtask 05-51-15-210-056 G. Inspection of the Wings NOTE : All the necessary inspections are visual unless specified ____ differently in the procedure text. Operators can refer to the Non-Destructive Testing Manual (NTM) and use non destructive procedures. If a tire burst occurs when the landing gear is fully retracted, examine only: - the landing gear well - the landing gear doors - the landing gear - the hydraulics compartment. If you replace a component after an inspection, you must do an operational test of the related system.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Trailing Edge | | | | | | | | | Falsework | | | | | | | | | | | | | | | | A.| | Examine the shroud box, the composite | | | | | | | | | closure panel for: | X | | | | | | | | - skin damage, and distortion. | | | | | | | | | | | | | | | | B.| | Examine the flap seal, the trailing | | | | | | | | | edge composite structure for: | X | | | | | | | | - damage and distortion. | | | | | | | | | | | | | | | | C.| | Examine the trailing edge falsework, | | | | | | | | | the structure of the rear spar for: | X | | | | | | | | - damaged paintwork, dents, tears, | | | | | | | | | damage and distortion. | | | | | | | | | If you find damage: | | | | | | | | | (1) Get access to the internal | | | | | | | | | structure | | X | | | | | | | (2) Examine the internal structure | | | | | | | | | the pipes, the electrical wiring | | | | | | | | | and the conduits for | | X | | | | | | | . cracks pulled or torn fasteners | | | | | | | | | and distortion. | | | | | | | | | | | | | | | |2. | | Inspection of the Leading Edge | | | | | | | | | | | | | | |
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Page 614 Jul 01/05
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | Examine the leading edge from the | | | | | | | | | RIB 1 to the RIB 10A for: | X | | | | | | | | - damage, distortion, dents, skin | | | | | | | | | tears and damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Get access to the inside area. | | X | | | | | | | (2) Examine the area of the damage, | | | | | | | | | the riblets for: | | X | | | | | | | . distortion, pulled or torn | | | | | | | | | fasteners damage, electrical | | | | | | | | | conduits. | | | | | | | | | | | | | | | |3. | | Inspection of the Slat | | | | | | | | | | | | | | | | A.| | Examine the internal structure of the | | | | | | | | | slats for: | | | | | | | | | - distortion, cracks, pulled or torn | | | | | | | | | fasteners, scratches, dents and | | | | | | | | | damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Examine the slat section at and | | | | | | | | | near the damage for: | | | | | | | | | - distortion, cracks, pulled or | | X | | | | | | | torn fasteners and damaged | | | | | | | | | paintwork. | | | | | | | | | (2) Examine the slat tracks and the | | X | | | | | | | slat track attachments for damage.| | | | | | | | | (3) Examine the rollers of the slat | | X | | | | | | | tracks for damage. | | | | | | | | | | | | | | | |4. | | Inspection of the Flaps and the | | | | | | | | | Ailerons | | | | | | | | | | | | | | | | A.| | Examine externally the flaps, and the | | | | | | | | | ailerons for : | | | | | | | | | - distortion, cracks, pulled or torn | X | | | | | | | | fasteners, scratches, dents and | | | | | | | | | damaged paintwork. | | | | | | | | | If you find damage : | | | | | | | | | (1) Examine the flap carriages and the| | X | | | | | | | fairings for : | | | | | | | | | - distortion, cracks and damaged | | | | | | | | | paintwork. | | | | | |
EFF : ALL 05-51-15 SROS
Page 615 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (2) Examine the flap tracks for | | X | | | | | | | damage. | | | | | | | | | (3) Examine the aileron servo controls| | X | | | | | | | and the hinge fittings for damage.| | | | | | ------------------------------------------------------------------------------Subtask 05-51-15-410-050 H. Close Access (1) Remove the safety devices installed on the landing gears (Ref. TASK 32-00-00-081-801). (2) Close all the access panels that you opened during the procedure. (3) Close the NLG doors (Ref. TASK 32-22-00-410-801). (4) Close the MLG doors (Ref. TASK 32-12-00-410-801). Subtask 05-51-15-860-051 J. 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) Pressurize the Yellow hydraulic system (Ref. TASK 29-00-00-863-803). (4) Pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-802). (5) Retract the flaps (Ref. TASK 27-50-00-866-802). (6) Retract the slats (Ref. TASK 27-80-00-866-802). (7) Retract the spoilers (Ref. TASK 27-60-00-866-802).
EFF : ALL 05-51-15 R SROS
Page 616 Jan 01/02
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**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-15-710-050 K. Do the tests below. NOTE : The tests below are necessary only if: ____ - you did work on the system after you have done the inspection for damage - you found damage on the structure adjacent to the landing gear doors or a flight control surfaces. (1) Operate the flap system. Make sure that the travel is full and that the flap moves freely (Ref. TASK 27-54-00-710-801). (2) Operate the slat system. Make sure that the travel is full and that the slat moves freely (Ref. TASK 27-84-00-710-801). (3) Operate the aileron system. Make sure that the travel is full and that the aileron moves freely (Ref. TASK 27-14-00-710-801). (4) Extend and retract the landing gear. Make sure that landing gear and the landing gear doors move freely (Ref. TASK 32-31-00-710-801). (5) If you find damage only on the landing gear doors or on the structure adjacent to the landing gear doors: (a) Open the NLG doors (Ref. TASK 32-22-00-010-801). (b) Make sure that the NLG doors move freely. (c) Close the NLG doors (Ref. TASK 32-22-00-410-801). (d) Open the MLG doors (Ref. TASK 32-12-00-010-801). Make sure that the MLG doors move freely. (e) Close the MLG doors (Ref. TASK 32-12-00-410-801). (6) Operate the thrust reverser system for correct operation. (Ref. TASK 78-31-00-710-804)
R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-15 301-399, 401-449, 451-499, SROS
Page 617 Jul 01/05
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**ON A/C 701-749,
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Subtask 05-51-15-710-050-A
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K. Do the tests below.
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NOTE : The tests below are necessary only if: ____ - you did work on the system after you have done the inspection for damage - you found damage on the structure adjacent to the landing gear doors or a flight control surfaces.
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(1) Operate the flap system. Make sure that the travel is full and that the flap moves freely (Ref. TASK 27-54-00-710-801).
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(2) Operate the slat system. Make sure that the travel is full and that the slat moves freely (Ref. TASK 27-84-00-710-801).
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(3) Operate the aileron system. Make sure that the travel is full and that the aileron moves freely (Ref. TASK 27-14-00-710-801).
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(4) Extend and retract the landing gear. Make sure that landing gear and the landing gear doors move freely (Ref. TASK 32-31-00-710-801).
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(5) If you find damage only on the landing gear doors or on the structure adjacent to the landing gear doors:
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(a) Open the NLG doors (Ref. TASK 32-22-00-010-801).
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(b) Make sure that the NLG doors move freely.
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(c) Close the NLG doors (Ref. TASK 32-22-00-410-801).
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(d) Open the MLG doors (Ref. TASK 32-12-00-010-801). Make sure that the MLG doors move freely.
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(e) Close the MLG doors (Ref. TASK 32-12-00-410-801).
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(6) Operate the thrust reverser system for correct operation. (Ref. TASK 78-31-00-740-802)
R EFF : 701-749, 05-51-15 SROS
Page 618 Oct 01/00
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**ON A/C ALL Subtask 05-51-15-860-053 L. Put the Aircraft back to its Initial Configuration (1) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (2) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803). (3) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802). (4) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). 5. Close-up ________ Subtask 05-51-15-942-050 A. Put the Aircraft back to its Initial Configuration (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. (4) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-51-15 SROS
Page 619 Oct 01/00
INSPECTION AFTER BRAKE EMERGENCY APPLICATION OR OVERHEAT - INSPECTION/CHECK ___________________________________________________________________________ TASK 05-51-16-200-801 Inspection After Brake Overheat 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 : 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. R R R R R R R R
CAUTION : DO NOT USE POWDER EXTINGUISHANTS. THE DEPOSITS EXTINGUISH THE FIRE, _______ BUT THEY ALSO PREVENT SATISFACTORY DISSIPATION OF THE HEAT. THIS CAN CAUSE PERMANENT STRUCTURAL DAMAGE TO: - THE BRAKE - THE WHEEL - THE WHEEL AXLE. YOU MUST NOT APPLY THE EXTINGUISHANT (WATER MIST INCLUDED) WITH A SPRAY GUN DIRECTLY ON THE CARBON HEAT PACK OF THE BRAKE. THIS CAN CAUSE THERMAL SHOCK. 1. __________________ Reason for the Job This inspection is necessary after a crew report of: - a brake temperature of more than 800 deg. C, - wheel fuse plug(s) melt. The temperature of the brakes can be too high after: - an acceleration stop, - the emergency application of the brakes, - frequent use of the brakes, - a failure of the braking control. If the temperature of the brakes is too high, one or more of the fuse plugs can melt. This causes: - damage to the tire, - possible damage to the wheel, - too much load on the opposite tire which can cause damage.
EFF : ALL 05-51-16 SROS
Page 601 Jan 01/07
2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
warning notice wheel chocks
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------05-51-15-200-801 R 32-11-00-210-801 32-40-00-200-801 32-41-11-000-801 32-41-11-400-801 32-41-14-000-801 32-41-14-400-801 32-42-00-710-801 32-42-27-000-801 32-42-27-400-801 32-43-00-710-801
Inspection of the Aircraft after a Tire Burst or Tread Throw or Wheel Failure Inspection for Discoloration of the Overheat Indication Paint Inspection/Check of the Brakes Removal of the MLG Wheel Installation of the MLG Wheel 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) Operational Test of the Normal Braking System Removal of the Wheel Brake Installation of the Wheel Brake Operational Test of the Alternate Braking System
3. __________ Job Set-up Subtask 05-51-16-941-050 A. Safety Precautions R
(1) Instructions after brake overheat:
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(a) If a tire is inflated, do not go near the area around the wheel for approximately one hour. When you go near, go from the front or rear and not from the side of the wheel.
EFF : ALL 05-51-16 SROS
Page 602 Jul 01/05
(b) Unless there is a fire, do not apply the extinguishing agent (liquid, water, mist, foam, etc.) with a spray gun into a hot tire if it is inflated. Do not apply the extinguishing agent directly into the heat pack of the brake or into the wheel. This can cause thermal shock to the stressed parts. Specially, do not use CO2 as this has a strong cooling effect which is not the same in all areas. It can cause an explosion in the stressed parts. Extinguishant on hot wheels can: - increase the time necessary for the fuse(s) to melt, or - prevent operation of the fuse(s). You must let the brake get cool by itself for at least one hour or use the cooling fans (if installed).
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NOTE : You can use blowers or air conditioning equipment only ____ after: - the temperature of the fuses decreases (more than one hour after the aircraft stops) or - the fuses are melted. You must not use these if you can see flames or burning embers.
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(c) If there is a fire, immediately extinguish the fire. Do not wait until the tires are deflated. Come near the wheel only from the front or from the rear.
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NOTE : We do not recommend that you use multi-purpose powders as ____ they can change into solid or enameled deposit. These agents extinguish the fire but they decrease the heat dissipation speed. This can cause permanent structural damage to the brake, the wheel or wheel axle. (d) Do not apply the parking brake. (e) Put a warning notice in the cockpit to tell persons not to operate the landing gear control lever.
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(f) Put the wheel chocks in position. (g) Clean all the parts if extinguishing agents were used.
EFF : ALL 05-51-16 SROS
Page 603 Jul 01/05
4. Procedure _________ Subtask 05-51-16-210-052 A. Inspection of the Aircraft (1) If there is a tire burst: - do the Inspection of the Aircraft after a Tire Burst or Tread Throw (Ref. TASK 05-51-15-200-801). Subtask 05-51-16-210-050 B. Inspection of the Wheels and Brakes (Ref. TASK 32-42-27-000-801) (Ref. TASK 32-42-27-400-801) (Ref. TASK 3240-00-200-801) (Ref. TASK 32-11-00-210-801) (Ref. TASK 32-41-11-000-801) (Ref. TASK 32-41-11-400-801) (Ref. TASK 32-41-14-000-801) (Ref. TASK 3241-14-400-801)
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| |Inspection after wheel fuse plug(s) | | | | | | | | |melt and the reported cockpit | | | | | | | | |indication of the brake temperature is | | | | | | | | |not more than 800 deg.C. | | | | | | | | | | | | | | | | | |(1) Remove the related wheel and the | X | | | | | | | | adjacent wheel for overhaul | | | | | | | | | (Ref. TASK 32-41-11-000-801). | | | | | | | | | (Refer to the manufacturers | | | | | | | | | instructions for the overhaul | | | | | | | | | procedure). | | | | | | | | |(2) Examine the brake unit for damage | X | | | | | | | | or distortion. | | | | | | | | | (Ref. TASK 32-40-00-200-801) | | | | | | | | | (a) Make sure that there is no | | | | | | | | | hydraulic fluid leakage at | | | | | | | | | the piston, liners, supply | | | | | | | | | lines, self blanking unions and| | | | | | | | | bleed screws. | | | | | | | | | (b) Clean the piston housing with | | | | | | | | | a cloth and make sure it is in | | | | | | | | | the correct condition (no | | | | | | | | | separation, no blisters). | | | | | | | | | (c) Make sure that the heat pack is| | | | | | | | | serviceable: | | | | | |
EFF : ALL 05-51-16 SROS
Page 604 Jul 01/06
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - carbon integrity | | | | | | | | | - free movement of the rotor | | | | | | | | | discs | | | | | | | | | - cracks or signs of oxidation | | | | | | | | | on the part of the rotor | | | | | | | | | discs you can see. | | | | | | | | | NOTE: Be careful with the | | | | | | | | | discs to prevent damage| | | | | | | | | to the protective | | | | | | | | | finish (anti-oxidation | | | | | | | | | paint). | | | | | | | | |If you find damage: | | | | | | | | |- Remove the damaged brake unit for | | X | | | | | | | overhaul | | | | | | | | | (Ref. TASK 32-42-27-000-801). | | | | | | | | | (Refer to the manufacturers | | | | | | | | | instructions for the overhaul | | | | | | | | | procedure). | | | | | | | | |(3) Installation of the removed | | | | | | | | | components | | | | | | | | | (a) Install serviceable components:| | | | | | | | | - for the wheels | | | | | | | | | (Ref. TASK 32-41-11-400-801) | | | | | | | | | - for the brakes | | | | | | | | | (Ref. TASK 32-42-27-400-801). | | | | | | | | | | | | | | | | B.| |Inspection after wheel fuse plug(s) | | | | | | | | |melt and/or the reported cockpit | | | | | | | | |indication of the brake temperature is | | | | | | | | |equal to or more than 800 deg.C. | | | | | | | | | | | | | | | | | |(1) Remove the related wheel for | X | | | | | | | | overhaul | | | | | | | | | (Ref. TASK 32-41-11-000-801). | | | | | | | | | (Refer to the manufacturers | | | | | | | | | instructions for the overhaul | | | | | | | | | procedure). | | | | | | | | | NOTE: If fuse plug is melted, also | | | | | | | | | remove the adjacent wheel for| | | | | | | | | overhaul. | | | | | | | | |(2) Remove the brake for overhaul | X | | | | | | | | (Ref. TASK 32-42-27-000-801). | | | | | | | | | (Refer to the manufacturers | | | | | |
EFF : ALL 05-51-16 SROS
Page 605 Jul 01/06
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | instructions for the overhaul | | | | | | | | | procedure). | | | | | | | | |(3) Remove the axle sleeve | X | | | | | | | | (Ref. TASK 32-41-14-000-801). | | | | | | | | |(4) Do the inspection of the Axle for | X | | | | | | | | Discoloration of the overheat | | | | | | | | | indication paint | | | | | | | | | (Ref. TASK 32-11-00-200-801). | | | | | | | | |(5) Examine the axle sleeve for | X | | | | | | | | distortion and damaged surface. | | | | | | | | |(6) Installation of the removed | | | | | | | | | components | | | | | | | | | (a) Install serviceable components:| | | | | | | | | - for the axle sleeve | | | | | | | | | (Ref. TASK 32-41-14-400-801) | | | | | | | | | - for the brakes | | | | | | | | | (Ref. TASK 32-42-27-400-801) | | | | | | | | | - for the wheels | | | | | | | | | (Ref. TASK 32-41-11-400-801). | | | | | | ------------------------------------------------------------------------------Subtask 05-51-16-710-050 C. Operational Test
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(1) Do an operational test of the normal braking system (Ref. TASK 32-4200-710-801). (2) Do an operational test of the alternate braking system (Ref. TASK 3243-00-710-801). 5. Close-up ________ Subtask 05-51-16-942-050 A. Put the Aircraft back to its Initial Configuration (1) Remove the warning notice(s). (2) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
R EFF : ALL 05-51-16 SROS
Page 606 Jul 01/05
___________________________________________________________________ INSPECTION AFTER FLIGHT IN EXCESSIVE TURBULENCE OR IN EXCESS OF VMO ________________ INSPECTION/CHECK TASK 05-51-17-200-801 Inspection after Flight in Excessive Turbulence or in Excess of VMO/MMO 1. __________________ Reason for the Job To do an inspection of the aircraft for structural damage after a flight where excessive load factors occurred. Such load factors can be caused by high turbulence, maneuvers not in the usual limits or in excess of VMO/MMO. To know if the inspection is necessary, refer to Para.3.A.
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2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No
specific specific specific specific
safety barriers warning notice wheel chocks adjustable access platform 16.8 m (55 ft. 1 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-861-801 24-41-00-862-801 27-14-00-710-801 27-24-00-710-801 27-34-00-710-801 27-50-00-866-801 27-54-00-710-801 27-64-00-710-801 27-84-00-710-801
Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Operational Test of the Aileron and Hydraulic Actuation Operational Test of the Rudder Servo Control with each Hydraulic System Operational Test of the Elevator and Hydraulic Actuation Extension of the Flaps on the Ground Operational Test of the Flap System Operational Test of the Spoilers Operational Test of the Slat System
EFF : ALL 05-51-17 SROS
Page 601 Jul 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------28-10-00-910-802 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
31-36-00-200-803 32-00-00-481-801 32-12-00-010-801 32-12-00-410-801 53-35-11-000-802 71-13-00-010-802 71-13-00-010-805 71-13-00-410-802 71-13-00-410-805 78-30-00-010-801 78-30-00-010-803 78-30-00-410-801 78-30-00-410-803 78-31-00-710-804 78-31-00-740-802
Access to Fuel Tanks and Work Areas 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) Check of the Load-Report Parameter after Hard/Overweight Landing or Excessive Turbulence Installation of the Safety Devices on the Landing Gears Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Removal of the Fillet Fairings Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Open the Fan Cowl Doors Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Close the Fan Cowl Doors Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Open the Thrust Reverser Cowl Doors Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Close the Thrust Reverser Cowl Doors Thrust Reverser Cycling Test (MCDU) Test of the Thrust Reverser Deployment and Stowage (Engine not Running)
EFF : ALL 05-51-17 SROS
Page 602 Jul 01/06
3. __________ Job Set-up Subtask 05-51-17-200-050 A. Inspection Requirements (1) Definitions R R
NOTE : Excessive turbulence is identified as turbulence that causes ____ large, sudden changes in altitude and/or attitude. It usually causes large variations in airspeed. Passengers and crew are moved violently against their seat belts and loose objects are moved around the aircraft. A flight in excessive turbulence or maneuvering is specified as a flight in which the vertical load factor is out of the range -1g to +2.5g (inclusive) in clean configuration or is out of the range 0g to +2g (inclusive) with the flaps extended. A flight in excess of VM0/MMO is specified as a flight in which:
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(a) the speed is equal to or more than VM0 + 20kts, or
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(b) the mach number is equal to or more than MM0 + 0.02M, or
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(c) the speed or mach number is equal to or more than VMO or MMO, and at which there is a vertical load factor out of the range 0g to +2g (inclusive).
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(2) Confirmation that inspection is necessary (a) After a flight crew report of flight in excessive turbulence, you must do the inspection unless: - The parameters recorded by the DFDR or the DMU load report 15 are less than the values specified above. To know the impact parameters, refer to the DFDR readout or to the DMU load report 15 (Ref. TASK 31-36-00-200-803).
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(b) After a flight crew report of flight in excess of VMO/MMO, you must do the inspection unless: - the values in the flight crew report are less than the values specified above,
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or - the parameters recorded by the DFDR are less than the values specified above.
EFF : ALL 05-51-17 SROS
Page 603 Jul 01/06
Subtask 05-51-17-941-050 B. Safety Precautions (1) Put the safety barriers in position. (2) Put the wheel chocks in position at the main landing gear. (3) Put a warning notice in position in the cockpit to tell persons not to operate the systems. R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-17-010-050 C. Get Access (1) Open the main landing gear doors (Ref. TASK 32-12-00-010-801).
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(2) Put an adjustable access platform in position near the area you want to examine. (3) Install the safety devices on the landing gears (Ref. TASK 32-00-00481-801).
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(4) Open the fan cowls doors (Ref. TASK 71-13-00-010-802) FOR 4030EM1 415BL, 416BR FOR 4030EM2 425BL, 426BR.
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(5) Open the thrust reverser doors (Ref. TASK 78-30-00-010-801) FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR.
EFF : ALL 05-51-17 SROS
Page 604 Jul 01/05
**ON A/C 701-749, Subtask 05-51-17-010-050-A C. Get Access (1) Open the main landing gear doors (Ref. TASK 32-12-00-010-801). R R
(2) Put an adjustable access platform in position near the area you want to examine. (3) Install the safety devices on the landing gears (Ref. TASK 32-00-00481-801).
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(4) Open the fan cowls doors (Ref. TASK 71-13-00-010-805) FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR.
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(5) Open the thrust reverser doors (Ref. TASK 78-30-00-010-803) FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR. **ON A/C ALL Subtask 05-51-17-860-050 D. Aircraft Maintenance Configuration (1) Extend the flaps (Ref. TASK 27-50-00-866-801). (2) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (3) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803). (4) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802). (5) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
EFF : ALL 05-51-17 SROS
Page 605 Jul 01/05
4. Procedure _________ Subtask 05-51-17-210-050 A. Inspection of the Fuselage (Ref. TASK 53-35-11-000-802) NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the non-destructive testing manual (NTM) and use non-destructive test procedures.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Fuselage | | | | | | | | | | | | | | | | A.| | Remove the wing-to-fuselage fillets | | | | | | | | | (Ref. Task 53-35-11-000-802). | | | | | | | | | Examine the junction between the wing | X | | | | | | | | spar box, the rear spar splice, the | | | | | | | | | fuselage skin panels, the panel | | | | | | | | | splices for: | | | | | | | | | - distortion, cracks, pulled or torn | | | | | | | | | fasteners, damaged paintwork. | | | | | | | | | | | | | | | | B.| | Examine the fuselage between FR26 and | | | | | | | | | FR38, the skin panels, the splicing, | X | | | | | | | | the rivets for: | | | | | | | | | - distortion, cracks, pulled or torn | | | | | | | | | fasteners, damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the FWD cargo-compartment | | | | | | | | | panel and examine internally the | | | | | | | | | structure, the frames, the | | X | | | | | | | splices, the rivets, the | | | | | | | | | stringers for: | | | | | | | | | - distortion, cracks, pulled or | | | | | | | | | torn fasteners and damaged | | | | | | | | | paintwork. | | | | | | | | | | | | | | | | C.| | At FR38, examine the top of the joint | | | | | | | | | between STGR10L and 10R for: | | | | | | | | | - cracks, distortion, pulled or torn | | | | | | | | | fasteners, damaged paintwork. | X | | | | | | | | If you find damage: | | | | | | | | | (1) Examine internally the structure, | | | | | |
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Page 606 Jul 01/06
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | the stringers, the frames for: | | | | | | | | | - cracks, distortion, pulled or | | X | | | | | | | torn fasteners. | | | | | | | | | | | | | | | | D.| | Examine the fuselage between FR38 and | | | | | | | | | FR91, the skin panels, the splicing, | | | | | | | | | the rivets for: | | | | | | | | | - distortion, cracks, pulled or torn | X | | | | | | | | fasteners, damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Examine internally the structure, | | | | | | | | | the stringers, the frames for: | | | | | | | | | - damage, distortion, pulled or | | X | | | | | | | torn fasteners. | | | | | | | | | | | | | | | | E.| | At FR54, examine the top of the joint | | | | | | | | | between STGR10 and 10R for: | | | | | | | | | - cracks, distortion, pulled or torn | X | | | | | | | | fasteners, damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Examine internally the structure, | | | | | | | | | the stringers, the frames for: | | | | | | | | | - damage, distortion, pulled or | | X | | | | | | | torn fasteners. | | | | | | | | | | | | | | | | F.| | Examine the cut-out corners and rivets| X | | | | | | | | of the door surround panels for: | | | | | | | | | - cracks, distortion, pulling and | | | | | | | | | tears and damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Examine internally the cut-out | | | | | | | | | corners of the door surround | | X | | | | | | | panels for: | | | | | | | | | - cracks, distortion, pulling, | | | | | | | | | tears and other damage. | | | | | | | | | | | | | | | | G.| | Examine the horizontal stabilizer | | | | | | | | | cut-out corners (FR87 to FR91) for: | X | | | | | | | | - cracks, distortion and other damage.| | | | | | | | | If you find damage: | | | | | | | | | (1) Internally examine the cut-out | | | | | | | | | edges of the top and bottom | | | | | | | | | stringers for: | | | | | |
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Page 607 Jul 01/06
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - cracks, damaged paintwork, | | X | | | | | | | pulled or torn fasteners. | | | | | | | | | | | | | | | |2. | | Inspection of the Belly Fairing | | | | | | | | | | | | | | | | A.| | Examine externally the belly fairing | | | | | | | | | panels for: | X | | | | | | | | - cracks, delamination, pulled or torn| | | | | | | | | fasteners and damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the damaged panel. | | X | | | | | | | (2) Examine internally the belly | | | | | | | | | fairing structure, all the | | | | | | | | | components, the pipes, the ducts, | | X | | | | | | | the electrical harnesses for: | | | | | | | | | - distortion, cracks, pulled or | | | | | | | | | torn fasteners and fluid | | | | | | | | | leakage. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-17-210-051 B. Inspection of the Vertical Stabilizer
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NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non-destructive Testing Manual (NTM) and use non-destructive procedures. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Vertical Stabilizer | | | | | | | | | | | | | | | | A.| | Examine the spar box for: | | | | | | | | | - cracks, pulled or torn fasteners, | X | | | | | | | | delamination, damaged paint | | | | | | | | | - wash. | | | | | | | | | If you find damage: | | | | | | | | | (1) Examine the attachment fittings | | | | | | | | | and their adjacent structure, the | | X | | | | | | | front and rear spar webs for: | | | | | |
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Page 608 Jul 01/05
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - damaged paintwork, cracks, | | | | | | | | | delamination, pulled or torn | | | | | | | | | fasteners. | | | | | | | | | (2) On the rear spar, examine the | | | | | | | | | hydraulic lines, the mechanical | | X | | | | | | | linkage, the electrical harnesses,| | | | | | | | | their brackets for: | | | | | | | | | - distortion, cracks, fluid | | | | | | | | | leakage. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-17-210-052 C. Inspection of the Horizontal Stabilizer NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non-destructive Testing Manual (NTM) and use non-destructive test procedures.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Horizontal | | | | | | | | | Stabilizer | | | | | | | | | | | | | | | | A.| | Examine the top and bottom skin | | | | | | | | | panels, the actuator fitting, the ribs| X | | | | | | | | for: | | | | | | | | | - cracks, distortion, pulled or torn | | | | | | | | | fasteners, damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Examine the rear spar web on each | | | | | | | | | side of the pivot bearing fitting | | X | | | | | | | for: | | | | | | | | | - cracks, distortion, pulled or | | | | | | | | | torn fasteners and damaged | | | | | | | | | paintwork. | | | | | | | | | (2) Examine the hydraulic pipes, the | | X | | | | | | | electrical harnesses, the | | | | | | | | | components for: | | | | | | | | | - rupture, cracks, distortion and | | | | | |
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Page 609 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | fluid leakage. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-17-210-053 D. Inspection of the Wing (Ref. TASK 28-10-00-910-802) NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non-destructive Testing Manual (NTM) and use non-destructive procedures.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Wing | | | | | | | | | | | | | | | | A.| | Examine the skin panels for: | | | | | | | | | - distortion, cracks, tears, fluid | X | | | | | | | | leakage or other damage. | | | | | | | | | If you find damage: | | | | | | | | | (1) Get access to the fuel tanks. | | X | | | | | | | (Ref. TASK 28-10-00-910-802) | | | | | | | | | (2) Examine the front spar and the | | X | | | | | | | rear spar, the stringers, the | | | | | | | | | internal structure of the wing, | | | | | | | | | the skin panels, the fasteners | | | | | | | | | for: | | | | | | | | | - cracks, distortion, pulled or | | | | | | | | | torn fasteners. | | | | | | | | | (3) Make sure that the sealant | | X | | | | | | | beads are in the correct | | | | | | | | | condition. | | | | | | | | | (4) Examine the ducts, lines, pipes, | | | | | | | | | the mechanical linkages and | | X | | | | | | | their support for: | | | | | | | | | - distortion, cracks, fluid | | | | | | | | | leakage, damage. | | | | | | | | | Make sure that the attachments | | | | | | | | | are correct. | | | | | | | | | (5) Examine the attachment fitting | | | | | |
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Page 610 Jul 01/05
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | of the engine pylon. | | X | | | | | | | | | | | | | |2. | | Inspection of the Aileron | | | | | | | | | | | | | | | | A.| | Examine the aileron for: | X | | | | | | | | - cracks, distortion, torn or pulled | | | | | | | | | fasteners. | | | | | | | | | If you find damage: | | | | | | | | | (1) Examine the aileron hinge and the | | | | | | | | | actuator for: | | X | | | | | | | - cracks, distortion, torn or | | | | | | | | | pulled fasteners. | | | | | | | | | | | | | | | |3. | | Inspection of the Flaps and Slats | | | | | | | | | | | | | | | | A.| | Examine the slats and flaps and their | X | | | | | | | | fairings for: | | | | | | | | | - cracks, distortion, torn or pulled | | | | | | | | | fasteners. | | | | | | | | | | | | | | | |4. | | Inspection of the Spoilers | | | | | | | | | | | | | | | | A.| | Examine the spoilers for: | | | | | | | | | - distortion, cracks, pulled or torn | X | | | | | | | | fasteners. | | | | | | | | | If you find damage: | | | | | | | | | (1) Examine the spoiler hinges and | | X | | | | | | | actuator for: | | | | | | | | | - cracks, distortion and other | | | | | | | | | damage. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-17-210-054 E. Inspection of the Pylons NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the non-destructive testing manual (NTM) and use non-destructive procedures.
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Page 611 Jul 01/05
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Pylon | | | | | | | | | | | | | | | | A.| | Examine the lateral panels around the | X | | | | | | | | access door cut-out for: | | | | | | | | | - cracks, distortion, damaged | | | | | | | | | paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Open the access door and remove | | X | | | | | | | the access panels. | | | | | | | | | (2) Examine the lower spar, the rib- | | X | | | | | | | to-panel attachments, the | | | | | | | | | structure for: | | | | | | | | | - distortion, cracks, rupture and | | | | | | | | | fluid leakage. | | | | | | | | | (3) Examine the components, the pipes,| | | | | | | | | the ducts, the electrical | | X | | | | | | | harnesses and their brackets for: | | | | | | | | | - distortion, cracks, rupture and | | | | | | | | | fluid leakage. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-17-210-055 F. Inspection of the Nacelle
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NOTE : All the inspections are visual unless specified differently in the ____ text. Operators can refer to the Non-destructive Testing Manual (NTM) and use non-destructive test procedures. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Nacelle | | | | | | | | | | | | | | | | A.| | Examine the nacelle for: | | | | | | | | | - cracks, distortion, delamination, | X | | | | | | | | damaged paintwork, loose rivets and | | | | | | | | | signs of shearing. | | | | | | | | | If you find damage: | | | | | | | | | (1) Open the fan cowl doors. | | X | | | | | | | (2) Open the thrust reverser doors. | | X | | | |
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Page 612 Jul 01/05
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (3) Examine the doors internally for: | | X | | | | | | | - damage. | | | | | | | | | (4) Examine the attachments of the | | | | | | | | | air intake cowl to the fan case | | X | | | | | | | for: | | | | | | | | | - cracks, distortion, pulled or | | | | | | | | | torn fasteners. | | | | | | | | | Make sure that the attachments are| | | | | | | | | correct. | | | | | | | | | (5) Examine all the cowl hinges, | | | | | | | | | fittings and the cowl attachment | | X | | | | | | | points on the pylon for: | | | | | | | | | - damage. | | | | | | | | | (6) Examine the components, the pipes,| | | | | | | | | the ducts, the electrical | | | | | | | | | harnesses for: | | X | | | | | | | - damage | | | | | | | | | - fluid leakage. | | | | | | ------------------------------------------------------------------------------**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-17-410-050 G. Close Access (1) Close the main landing gear doors (Ref. TASK 32-12-00-410-801).
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(2) Close the fan cowl doors (Ref. TASK 71-13-00-410-802) FOR 4030EM1 415BL, 416BR FOR 4030EM2 425BL, 426BR.
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(3) Close the thrust reverser doors (Ref. TASK 78-30-00-410-801) FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR. (4) Close the main landing gear door (Ref. TASK 32-12-00-410-801).
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Page 613 Jul 01/05
**ON A/C 701-749, Subtask 05-51-17-410-050-A G. Close Access (1) Close the main landing gear doors (Ref. TASK 32-12-00-410-801).
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(2) Close the fan cowl doors (Ref. TASK 71-13-00-410-805) FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR.
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(3) Close the thrust reverser doors (Ref. TASK 78-30-00-410-803) FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR. (4) Close the main landing gear door (Ref. TASK 32-12-00-410-801). **ON A/C ALL Subtask 05-51-17-860-051 H. 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).
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(3) Pressurize the Yellow hydraulic system (Ref. TASK 29-00-00-863-803).
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(4) Pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-802).
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Page 614 Jul 01/05
Subtask 05-51-17-710-050 J. Do the flight system test NOTE : The tests below are necessary only if you find damage to the ____ structure adjacent to a flight control surface. (1) Operate the aileron system. Make sure that the travel is full and that the ailerons move freely (Ref. TASK 27-14-00-710-801). (2) Operate the flap system. Make sure that the travel is full and that the flaps move freely (Ref. TASK 27-54-00-710-801). (3) Operate the slat system. Make sure that the travel is full and that the slats move freely (Ref. TASK 27-84-00-710-801).
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(4) Operate the spoiler system. Make sure that the travel is full and that the spoilers move freely (Ref. TASK 27-64-00-710-801).
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(5) Operate the THS system. Make sure that the travel is full and that the THS moves freely.
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(6) Operate the elevator system. Make sure that the travel is full and that the elevators move freely (Ref. TASK 27-34-00-710-801).
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(7) Operate the rudder system. Make sure that the travel is full and that the rudder moves freely (Ref. TASK 27-24-00-710-801).
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**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-17-710-051 K. Do a test of the thrust reverser system. NOTE : The test below is necessary only if you find damage to the ____ structure adjacent to a cowl surface. (1) Operate the thrust reverser system (Ref. TASK 78-31-00-710-804). Make sure that the travel is full and that the thrust reverser moves freely.
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Page 615 Jul 01/05
**ON A/C 701-749, Subtask 05-51-17-710-051-A K. Do a test of the thrust reverser system. NOTE : The test below is necessary only if you find damage to the ____ structure adjacent to a cowl surface. (1) Operate the thrust reverser system (Ref. TASK 78-31-00-740-802). Make sure that the travel is full and that the thrust reverser moves freely. **ON A/C ALL 5. Close-up ________ Subtask 05-51-17-860-052 A. Put the Aircraft back to its Initial Configuration R
(1) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801).
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(2) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803).
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(3) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802).
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(4) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). Subtask 05-51-17-942-050 B. Put the Aircraft back to its Initial Configuration (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.
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INSPECTION AFTER LIGHTNING STRIKE - INSPECTION/CHECK ____________________________________________________ TASK 05-51-18-200-801 Inspection after Lightning Strike WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A _______ FALL CAN KILL OR INJURE YOU. 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 After a lightning strike, before the aircraft continues in service, you must: - do a general inspection of the total surface of the aircraft to find the strike areas, - do a careful inspection of the strike areas to find the type and quantity of possible damage. - if you find damage, make a decision about the necessary repair/action. NOTE : To do this inspection, you must have: ____ - a set of access platforms, 2 m (6.56 ft.) to 17 m (55.9 ft.) - or an adjustable access platform, 2 m (6.56 ft.) to 17 m (55.9 ft.) - or a manlift aerial boom, 2 m (6.56 ft.) to 17 m (55.9 ft.) 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific
warning notices adjustable access platform 17 m (55 ft. 9 in.)
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Page 601 Apr 01/99
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------23-11-00-710-801 23-12-00-710-801 23-36-00-710-808 23-61-00-200-801 24-22-51-210-802 24-41-00-862-801 27-14-00-710-801 27-14-51-000-801 27-14-51-000-802 27-14-51-400-801 27-14-51-400-802 27-24-00-710-801 27-24-51-000-801 27-24-51-400-801 27-34-00-710-801 R R
27-34-51-000-801 27-34-51-400-801 27-44-00-710-801 27-50-00-866-801 27-50-00-866-802 27-54-00-710-801 27-60-00-866-801 27-60-00-866-802 27-64-00-710-801 27-84-00-710-801 29-00-00-864-804
Operational Test of the HF System Operational Test of the VHF System Operational Test of the Landscape-Camera System Check the Resistance from the Static Discharger to the Base (Retainer) and from the Base (Retainer) to the Aircraft Structure Visual Inspection of the Lightning Protection Module (19XU1,19XU2) De-energize the Aircraft Electrical Circuits from the External Power A Operational Test of the Aileron and Hydraulic Actuation Removal of the Inboard Aileron Servo-Control (7CS1,7CS2,8CS1,8CS2) Removal of the Outboard Aileron Servo-Control (9CS1,9CS2,10CS1,10CS2) Installation of the Inboard Aileron Servo-Control (7CS1,7CS2,8CS1,8CS2) Installation of the Outboard Aileron Servo-Control (9CS1,9CS2,10CS1,10CS2) Operational Test of the Rudder Servo Control with each Hydraulic System Removal of the Rudder Servo Control (5002CY1, 5002CY2, 5002CY3) Installation of the Rudder Servo Control (5002CY1, 5002CY2, 5002CY3) Operational Test of the Elevator and Hydraulic Actuation Removal of the Elevator Servo-Control Units Installation of the Elevator Servo-Control Units Operational Test of the Trimmable Horizontal Stabilizer (THS) Actuator Jamming Protection Device Extension of the Flaps/Slats on the Ground Retraction of the Flaps/Slats on the Ground Operational Test of the Flap System Extension of the Spoilers for Maintenance Retraction of the Spoilers after Maintenance Operational Test of the Spoilers Operational Test of the Slat System Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action
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------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------30-31-00-710-801 30-42-00-710-801 R
30-71-00-740-801 30-81-00-710-801 32-00-00-481-801 32-11-00-220-801
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32-12-00-010-801 32-12-00-410-801 32-21-00-220-801 32-22-00-010-801 32-22-00-410-801 32-31-00-740-801 32-46-00-740-801 33-41-00-710-802 33-42-11-400-801 33-47-00-710-801 33-48-00-710-801 33-49-00-710-801 34-11-00-710-801 34-11-15-200-801 34-11-19-000-801 34-11-19-400-801 34-13-00-710-803 34-13-00-740-803 34-22-00-710-801 34-36-00-710-801 34-36-00-710-802 34-36-00-710-803 34-36-00-720-801 34-36-00-720-802
Operational Test of the Probe Ice Protection Operational Test of the Windshield Anti Icing and Defogging BITE Test of the Waste Water Ice Protection (via CIDS POWER-UP) Operational Test of the Ice Detection System Installation of the Safety Devices on the Landing Gears Detailed Inspection of Main Gear Structure comprising: Main Fittings, Sliding Piston, Bogie Beam, Pitch Trimmer, Sidestay Assy, Lock Pins Assembly ... Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Detailed Inspection of the Nose Gear Structure comprising : Main Fitting (Barrel), Sliding Member, Torque Links, Drag Stay Upper and Lower Arm .... Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance BITE Test of the Normal Extension and Retraction System BITE Test of the BSCU and its Related Systems Operational Test of the Navigation Lights Installation of the Landing Light (6LB1, 6LB2) Operational Test of the Logo Lights Operational Test of the Anti-Collision/Strobe Lighting Operational Test of the Wing and Engine Scan Lighting Operational Test of the AIR DATA Switching Inspection/Check of the Pitot Probe (9DA1, 9DA2, 9DA3) Removal of the Angle of Attack Sensor (3FP1, 3FP2, 3FP3) Installation of the Angle of Attack Sensor (3FP1, 3FP2, 3FP3) AOA SENSOR TEST SYSTEM TEST of the ADR Operational test of the Standby Compass Operational Test of the ILS Operational Test of the ILS Function Operational Test of the GPS Function Functional Test of the ILS Functional Test of the ILS Function
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Page 603 Jul 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------34-41-00-710-802 34-41-00-740-801 34-41-11-000-801 34-41-11-400-801
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34-42-00-740-801 34-43-00-740-801 34-48-00-740-801 34-51-00-740-801 34-52-00-740-801 34-53-00-710-801 34-55-00-710-801 49-00-00-710-801 53-15-11-200-801 55-32-11-000-801 55-34-11-000-801 56-11-11-200-801 56-11-12-200-801 56-12-11-200-801 73-21-00-710-803 73-21-00-710-812 78-31-00-710-804 78-31-00-740-802 05-51-18-991-004 05-51-18-991-005
Operational test of the Weather-Radar Antenna Scanning BITE test of the Weather Radar Removal of the Weather Radar Antenna Assembly (7SQ, 11SQ) Installation of the Weather Radar Antenna Assembly (7SQ, 11SQ) BITE Test of the Radio Altimeter BITE test of the TCAS Operational test of GPW Computer by BITE BITE Test of the DME BITE test of the ATC Operational Test of the ADF Operational Test of the VOR Operational Test of the APU Detailed Inspection of the Radome (110AL) Removal of the Vertical Stabilizer Leading-Edge Removal of the Vertical Stabilizer Tip Inspection of the Windshields (3DG1,3DG2). Inspection of the Fixed Windows (7DG1,7DG2) Inspection of the Sliding Windows (8DG1,8DG2). Full Authority Digital Engine Control (FADEC) System Static Test Test of the FADEC System Thrust Reverser Cycling Test (MCDU) Test of the Thrust Reverser Deployment and Stowage (Engine not Running) Fig. 601 Fig. 602
3. __________ Job Set-up Subtask 05-51-18-210-076 A. General (1) Lightning (a) Lightning always has two or more attachment points (one entry and one exit) on the aircraft skin. (b) Lightning moves back along the surface of the aircraft (swept stroke zone). This can cause a chain of scattered attachment points along a line in the direction of travel of the aircraft. (c) Lightning hits some areas more frequently than others.
EFF : ALL 05-51-18 SROS
Page 604 Jan 01/06
(2) Aircraft zoning (Ref. Fig. 601/TASK 05-51-18-991-004) (a) The aircraft is divided into three zones related to the probability of lightning strike: 1 _
Zone 1: - surfaces where there is a high probability of initial lightning attachment (entry or exit).
2 _
Zone 2: - surfaces where there is a high probability of a swept stroke zone. The lightning strike has its initial point of attachment in Zone 1 and moves into Zone 2.
3 _
Zone 3: - this zone includes all of the aircraft surfaces that are not in Zone 1 and 2. In Zone 3 there is a low probability of attachment of a lightning strike. However, high lightning currents can go through Zone 3 by direct conduction between 2 attachment points. Zone 3 currents will also go into Zones 1 and 2.
(b) Zones 1 and 2 are divided into A and B areas related to the probability of continued attachment of the arc (hang on). The probability of arc hang on is low in A areas and high in B areas. 1 _
Zone 1A: - area where there is a high probability of initial attachment and low probability of arc hang on, such as the forward-mounted pitot probes, the radome diverter strips and the nacelle leading edges.
2 _
Zone 1B: - area where there is a high probability of initial attachment and high probability of arc hang on, such as the wing, stabilizers and fin tips and some trailing edge areas.
3 _
Zone 2A: - a swept stroke zone with low probability of arc hang on, such as mid-chord regions of the wing surface, aft of an engine and the total fuselage surface.
4 _
Zone 2B: - a swept stroke zone with high probability of arc hang on, such as the wing trailing edge aft of Zone 2A.
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Page 605 Apr 01/98
Lightning Strike Inspection Areas Figure 601/TASK 05-51-18-991-004 EFF : ALL 05-51-18 SROS
Page 606 Apr 01/98
(3) Effects on the aircraft structure and systems. There are two types of possible risks to the aircraft: - indirect effects - direct effects. (a) Indirect effects. 1 _
Electromagnetic fields: - the electromagnetic fields related to the lightning attachment can cause unwanted transient voltages and currents in the aircraft wiring and systems. In some conditions (low intensity strike, high protection), the effect on the systems can be temporary and the systems can operate correctly again after the strike. In other conditions (low protection, no circuit protection devices), the damage can be permanent and it will be necessary to replace parts.
(b) Direct effects The direct effects are the physical damage related to signs such as: 1 _
Pitting/meltthrough: - this is the action of the electrical arc formed when a lightning stroke attaches to the aircraft (arc root damage at the attachment points or damage caused by current flow which can appear also far from the attachment points). - signs of a lightning attachment are pitting and scorch marks and paint discoloration. On composite components, in addition to paint discoloration and skin puncturing, some delamination of the fibers can occur. If there is skin puncturing, there can be damage to the grounded equipment below composite material fairings. - you must always compare the damage you find with the limits given in the Structural Repair Manual (SRM).
2 _
Magnetic force: - the damage usually occurs where a small area causes the density of the current to be high (e.g. a bonding lead installed at a control surface hinge).
3 _
Resistive heating: - when lightning currents flow through an aircraft structure, energy is changed to heat along its path. - resistive heating usually causes marks of the weld type, specially where the lightning current flows for some time.
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Page 607 Apr 01/98
4 _
Acoustic shock wave: - When a lightning strike occurs, there is an acoustic shock wave. If the intensity of this shock wave is high, it can cause deformation of thin metal skins or rupture of thin composite skins.
(4) Inspection requirements: (a) Aircraft are designed to keep the effects of lightning to a minimum and make sure it can continue its flight and land safely after a lightning attachment. (b) It is not possible to accurately know where the attachment will occur but Zone 1 and Zone 2 show the most probable areas of lightning attachment. (c) Lightning strikes do not always give the same quantity of damage. The quantity of damage comes from the intensity of the lightning strike. (d) Therefore, it is necessary to do a full inspection after a lightning strike to make an estimate of the damage and make sure that the aircraft can, as a minimum, continue service in a Master Minimum Equipment List (MMEL) condition. The inspection after a lightning strike refers to: - the type of the system (critical/essential) to specify the tests that are necessary - the requirements of the MMEL NOTE : Critical function: ____ If a critical function fails, it can result in a failure condition that can prevent continued safe flight and landing of the aircraft. Essential function: If an essential function fails, it can result in a failure condition which can have an effect on : - the performance of the aircraft - or the ability of the flight crew to fly the aircraft in the adverse conditions.
EFF : ALL 05-51-18 SROS
Page 608 Apr 01/98
Subtask 05-51-18-210-077 B. Inspection Preparation (1) Before you start, we recommend that you get information from the crew about the flight condition. (2) Make sure that you have the related aircraft Post Flight Report (PFR). (3) All events reported by the crew or by the PFR must be checked in addition/ conjunction with this inspection. Subtask 05-51-18-481-051 C. Safety Precautions Make sure that the safety devices are installed on the landing gears (Ref. TASK 32-00-00-481-801). Subtask 05-51-18-866-051 D. Extension of the Flight Control Surfaces (1) Extend the flaps and the slats (Ref. TASK 27-50-00-866-801). (2) Extend the spoilers (Ref. TASK 27-60-00-866-801). Subtask 05-51-18-010-050 E. Get Access (1) Open the nose gear doors and install the safety devices (Ref. TASK 32-22-00-010-801). (2) Open the main gear doors and install the safety devices (Ref. TASK 32-12-00-010-801). Subtask 05-51-18-860-051 F. Aircraft Maintenance Configuration (1) Make sure that the electrical circuits are de-energized (Ref. TASK 24-41-00-862-801). (2) Make sure that the hydraulic systems are depressurized (Ref. TASK 2900-00-864-804).
EFF : ALL 05-51-18 SROS
Page 609 Apr 01/98
(3) Put warning notices in the cockpit to tell persons not to operate the systems. (4) Put the adjustable access platform in position. 4. Procedure _________ Subtask 05-51-18-210-050 A. Inspection of the total Surface of the Aircraft (Ref. Fig. 602/TASK 05-51-18-991-005) NOTE : All the necessary inspections are visual unless the text gives ____ other instructions. Operators can refer to the Non-destructive Testing Manual (NTM) and use non-destructive procedures. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Radome and the | | | | | | | | | Access Door 121AL (Glide/Slope | | | | | | | | | Antenna access. | | | | | | | | | | | | | | | | A.| | Examine visually the radome external | X | | | | | | | | skin and the lightning diverters for | | | | | | | | | burn marks, change of color, | | | | | | | | | puncturing and other damage. | | | | | | | | | | | | | | | | B.| | Examine the access door 121AL (glide/ | X | | | | | | | | slope antenna access) for burn marks, | | | | | | | | | puncturing and other damage. | | | | | | | | | | | | | | | |2. | | Inspection of the Windshield, Fixed | | | | | | | | | Windows, Sliding Windows and Window | | | | | | | | | Frames. | | | | | | | | | | | | | | | | A.| | Examine visually the windshield, | X | | | | | | | | fixed windows, sliding windows and the| | | | | | | | | window frames for burn marks, change | | | | | | | | | of color and other damage. | | | | | | | | | | | | | | | |3. | | inspection of the Landing Gear Doors | | | | | | | | | | | | | | | | A.| | Examine the skin of all landing gear | X | | | | | | | | doors for burn marks, change of color,| | | | | |
EFF : ALL 05-51-18 R SROS
Page 610 Apr 01/02
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | puncturing and delamination. | | | | | | | | | | | | | | | | B.| | Examine the electrical bonding leads | X | | | | | | | | for breakage and defective attachment.| | | | | | | | | | | | | | | |4. | | Inspection of the Landing Gears. | | | | | | | | | | | | | | | | | | NOTE: Do these checks if the lightning| | | | | | | | | strike occurred: | | | | | | | | | - when the LG was extended and locked | | | | | | | | | down, | | | | | | | | | - during the extension of the LG. | | | | | | | | | and when you find a through hole | | | | | | | | | during the inspection of the landing | | | | | | | | | gears doors. | | | | | | | | | | | | | | | | A.| | Examine all the landing gears. | X | | | | | | | | (1) Examine the LG structure and the | | | | | | | | | points where it is attached for | | | | | | | | | change of color, burn marks and | | | | | | | | | other damage. | | | | | | | | | (2) Examine the shock absorber for | | | | | | | | | change of color and burn marks. | | | | | | | | | (3) Examine all the components | | | | | | | | | attached to the landing gear and | | | | | | | | | fully examine the electrical looms| | | | | | | | | and components for a change of | | | | | | | | | color and burn marks. | | | | | | | | | | | | | | | |5. | | Inspection of the Belly Fairing | | | | | | | | | | | | | | | | A.| | Examine the belly fairing panels | X | | | | | | | | (including the wing-to-fuselage | | | | | | | | | fairings) for change of color, burn | | | | | | | | | marks, puncturing and delamination. | | | | | | | | | Examine fairing screws and fasteners | X | | | | | | | | for burn marks. | | | | | | | | | | | | | | | |6. | | Inspection of the Fuselage | | | | | | | | | | | | | | | | A.| | Externally examine all of the fuselage| X | | | | | | | | skin including rivets and screws for | | | | | | | | | change of color, burns marks and | | | | | |
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Page 611 Apr 01/02
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Location of the Antennas, Probes and Sensors and Exterior Lights Figure 602/TASK 05-51-18-991-005- 12 (SHEET 1)
EFF : ALL 05-51-18 SROS
Page 612 Jan 01/00
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Location of the Antennas, Probes and Sensors and Exterior Lights Figure 602/TASK 05-51-18-991-005- 22 (SHEET 2)
EFF : ALL 05-51-18 SROS
Page 613 Jan 01/00
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | small holes. | | | | | | | | | | | | | | | | B.| | Examine all the probes, sensors and | X | | | | | | | | drain masts and the adjacent area for | | | | | | | | | burn marks and change of color. | | | | | | | | | | | | | | | | C.| | Examine carefully all the | X | | | | | | | | communication and navigation antennas | | | | | | | | | and the adjacent area for burn marks, | | | | | | | | | change of color, puncturing and | | | | | | | | | delamination. | | | | | | | | | | | | | | | | D.| | Examine all exterior lights and | X | | | | | | | | adjacent area for burn marks and other| | | | | | | | | damage. | | | | | | | | | | | | | | | | E.| | Examine the APU exhaust for burn marks| X | | | | | | | | and change of color. | | | | | | | | | | | | | | | |7. | | Inspection of the Wings | | | | | | | | | | | | | | | | A.| | Examine the top and bottom skin of the| X | | | | | | | | wings and the leading and trailing | | | | | | | | | edges for burn marks, change of color | | | | | | | | | | | | | | | | B.| | Examine the slats for burn marks and | X | | | | | | | | damage. | | | | | | | | | | | | | | | | C.| | Examine the flap track fairings for | X | | | | | | | | burn marks, change of color, | | | | | | | | | puncturing and other damage. | | | | | | | | | | | | | | | | D.| | Examine the flaps for burn marks, | X | | | | | | | | change of color, puncturing and | | | | | | | | | delamination. | | | | | | | | | | | | | | | | E.| | Examine the spoilers for burn marks, | X | | | | | | | | change of color, puncturing and | | | | | | | | | delamination. | | | | | | | | | | | | | | | | F.| | Examine the ailerons for burn marks, | X | | | | | | | | change of color, puncturing and | | | | | | | | | delamination. | | | | | |
EFF : ALL 05-51-18 R SROS
Page 614 Apr 01/02
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | | | | | | | | G.| | Examine all the static dischargers for| X | | | | | | | | burn marks, damaged tip and breakage. | | | | | | | | | | | | | | | | H.| | Examine the wing tip for burn marks | X | | | | | | | | and burn holes. | | | | | | | | | | | | | | | | I.| | Examine the lights on the wing tip for| X | | | | | | | | burn marks and other damage. | | | | | | | | | | | | | | | |8. | | Inspection of the Engine Nacelles and | | | | | | | | | the Pylons. | | | | | | | | | | | | | | | | A.| | Examine each air intake, inlet cowl, | X | | | | | | | | fan cowl, thrust reverser, exhaust | | | | | | | | | nozzle and the pylon for burn marks, | | | | | | | | | change of color, puncturing and | | | | | | | | | delamination. | | | | | | | | | | | | | | | |9. | | Inspection of the Vertical Stabilizer | | | | | | | | | | | | | | | | A.| | Examine all the static dischargers for| X | | | | | | | | burn marks, damaged tip and breakage. | | | | | | | | | | | | | | | | B.| | Examine the skin of the vertical | X | | | | | | | | stabilizer and the rudder (specially | | | | | | | | | the leading and the trailing edges, | | | | | | | | | the rudder surface in the hinge area | | | | | | | | | and the antenna fairings), the fin | | | | | | | | | tip cap, the fin and rudder tip cap | | | | | | | | | lightning diverters for burn marks, | | | | | | | | | change of color, puncturing, | | | | | | | | | delamination and other damage. | | | | | | | | | | | | | | | |10. | | Inspection of the Horizontal | | | | | | | | | Stabilizer | | | | | | | | | | | | | | | | A.| | Examine all the static dischargers for| X | | | | | | | | burn marks, damaged tip and breakage. | | | | | | | | | | | | | | | | B.| | Examine the skin of the horizontal | X | | | | | | | | stabilizer and elevators (specially | | | | | | | | | the leading and the trailing edges, | | | | | |
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Page 615 Apr 01/02
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | the elevator surface in the hinge | | | | | | | | | area and the tip) for burn marks, | | | | | | | | | change of color, puncturing, | | | | | | | | | delamination and other damage. | | | | | | ------------------------------------------------------------------------------R R R
Subtask 05-51-18-710-056 B. Operational test of the HF system (Ref. TASK 23-11-00-710-801)
R R R R R R R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | Do the operational test of the HF | X | | | | | | | | system (Ref. TASK 23-11-00-710-801). | | | | | | -------------------------------------------------------------------------------
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**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 402-449, 451-499, 701-749, Subtask 05-51-18-210-051
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C. Check after Damage on the Radome and/or the Access Door 121AL (Ref. TASK 53-15-11-200-801) (Ref. TASK 34-41-00-740-801) (Ref. TASK 3441-00-710-802) (Ref. TASK 34-36-00-710-802) (Ref. TASK 34-36-00-720-802) (Ref. TASK 34-41-11-000-801) (Ref. TASK 34-41-11-400-801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage on the radome | | | | | | | | | during the inspection: | | | | | | | | | (1) Do the detailed inspection of the | | X | | | | | | | radome | | | | | | | | | (Ref. TASK 53-15-11-200-801). | | | | | | | | | If you find a through hole: | | | | | | | | | (a) Examine the weather radar and | | | X | | | | | | the WR antenna drive for burn | | | | | | | | | marks, pitting and other | | | | | | | | | damage. | | | | | |
EFF : ALL 05-51-18 SROS
Page 616 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | If you find damage: | | | | | | | | | - if you find damage on the | | | X | | | | | | flat plate antenna, replace | | | | | | | | | it: | | | | | | | | | (Ref. TASK 34-41-11-000-801)| | | | | | | | | (Ref. TASK 34-41-11-400-801)| | | | | | | | | - do the BITE test of the | | | X | | | | | | weather radar: | | | | | | | | | (Ref. TASK 34-41-00-740-801)| | | | | | | | | - do the operational test of | | | X | | | | | | the weather-radar antenna | | | | | | | | | scanning. | | | | | | | | | (Ref. TASK 34-41-00-710-802)| | | | | | | | | (b) Examine the localizer antenna | | | X | | | | | | for burn marks, pitting and | | | | | | | | | other damage. | | | | | | | | | | | | | | | | B.| | If you find a through hole on the | | X | | | | | | | access door 121AL (glide/slope antenna| | | | | | | | | access): | | | | | | | | | (1) Examine the glide/slope antenna | | | X | | | | | | for sign of arc attachment. | | | | | | | | | | | | | | | | C.| | If you find damage on the localizer | | | | | | | | | antenna and/or the glide/slope | | | | | | | | | antenna: | | | | | | | | | (1) Do the functional test of the ILS | | | X | | | | | | function of the MMR: | | | | | | | | | (Ref. TASK 34-36-00-720-802) | | | | | | | | | NOTE: If an ILS ground test unit is | | | | | | | | | not available, do an operational| | | | | | | | | test of the ILS function of the | | | | | | | | | MMR: | | | | | | | | | (Ref. TASK 34-36-00-710-802) | | | | | | -------------------------------------------------------------------------------
R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-18 301-399, 402-449, 451-499, 701-749, SROS
Page 617 Jul 01/05
**ON A/C 401-401, Subtask 05-51-18-210-051-A R
C. Check after Damage on the Radome and/or the Access Door 121AL (Ref. TASK 53-15-11-200-801) (Ref. TASK 34-41-00-740-801) (Ref. TASK 3441-00-710-802) (Ref. TASK 34-36-00-710-801) (Ref. TASK 34-36-00-720-801) (Ref. TASK 34-41-11-000-801) (Ref. TASK 34-41-11-400-801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage on the radome | | | | | | | | | during the inspection: | | | | | | | | | (1) Do the detailed inspection of the | | X | | | | | | | radome | | | | | | | | | (Ref. TASK 53-15-11-200-801). | | | | | | | | | If you find a through hole: | | | | | | | | | (a) Examine the weather radar and | | | X | | | | | | the WR antenna drive for burn | | | | | | | | | marks, pitting and other | | | | | | | | | damage. | | | | | | | | | If you find damage: | | | | | | | | | - if you find damage on the | | | X | | | | | | flat plate antenna, replace | | | | | | | | | it: | | | | | | | | | (Ref. TASK 34-41-11-000-801)| | | | | | | | | (Ref. TASK 34-41-11-400-801)| | | | | | | | | - do the BITE test of the | | | X | | | | | | weather radar: | | | | | | | | | (Ref. TASK 34-41-00-740-801)| | | | | | | | | - do the operational test of | | | X | | | | | | the weather-radar antenna | | | | | | | | | scanning. | | | | | | | | | (Ref. TASK 34-41-00-710-802)| | | | | | | | | (b) Examine the localizer antenna | | | X | | | | | | for burn marks, pitting and | | | | | | | | | other damage. | | | | | | | | | | | | | | | | B.| | If you find a through hole on the | | X | | | | | | | access door 121AL (glide/slope antenna| | | | | | | | | access): | | | | | | | | | (1) Examine the glide/slope antenna | | | X | | | | | | for sign of arc attachment. | | | | | | | | | | | | | | |
EFF : 401-401, 05-51-18 SROS
Page 618 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | C.| | If you find damage on the localizer | | | | | | | | | antenna and/or the glide/slope | | | | | | | | | antenna: | | | | | | | | | (1) Do the functional test of the ILS:| | | X | | | | | | (Ref. TASK 34-36-00-720-801) | | | | | | | | | NOTE: If an ILS ground test unit is | | | | | | | | | not available, do an operational| | | | | | | | | test of the ILS | | | | | | | | | (Ref. TASK 34-36-00-710-801) | | | | | | ------------------------------------------------------------------------------**ON A/C ALL Subtask 05-51-18-210-053 R
D. Check after Damage on the Windshield, Fixed Windows, Sliding Windows and the Window Frames (Ref. TASK 56-11-11-200-801) (Ref. TASK 56-11-12-200-801) (Ref. TASK 5612-11-200-801) (Ref. TASK 30-42-00-710-801) (Ref. TASK 34-22-00-710-801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage during the | | | | | | | | | inspection: | | | | | | | | | (1) Do the inspection of the related | | X | | | | | | | component: | | | | | | | | | - for the windshield | | | | | | | | | (Ref. TASK 56-11-11-200-801) | | | | | | | | | - for the fixed windows | | | | | | | | | (Ref. TASK 56-11-12-200-801) | | | | | | | | | - for the sliding windows | | | | | | | | | (Ref. TASK 56-12-11-200-801) | | | | | | | | | (2) Do the operational test of the | | X | | | | | | | windshield anti icing and | | | | | | | | | defogging | | | | | | | | | (Ref. TASK 30-42-00-710-801) | | | | | | | | | (3) Do the operational test of the | | X | | | | | | | standby compass | | | | | | | | | (Ref. TASK 34-22-00-710-801) | | | | | | -------------------------------------------------------------------------------
EFF : ALL 05-51-18 SROS
Page 619 Jul 01/05
Subtask 05-51-18-210-078 R
E. Check after Damage on the Landing Gear Doors NOTE : If there is damage to the aircraft structure, refer to the ____ Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage during the | | | | | | | | | inspection: | | | | | | | | | (1) Refer to allowable damage and | | X | | | | | | | repair (Ref. SRM). | | | | | | | | | (2) If you find a through hole: | | X | | | | | | | - examine internally the adjacent | | | | | | | | | and underneath area including | | | | | | | | | all the components (pipes, items| | | | | | | | | of equipment, electrical | | | | | | | | | harnesses...) for damage. | | | | | | | | | if you find damage: | | | | | | | | | - replace or repair the | | | X | | | | | | the related component | | | | | | | | | | | | | | | | B.| | If you find damage on the electrical | | | | | | | | | bonding leads during the inspection: | | | | | | | | | (1) Replace the electrical bonding | | X | | | | | | | lead and/or the defective | | | | | | | | | attachment. | | | | | | -------------------------------------------------------------------------------
EFF : ALL 05-51-18 SROS
Page 620 Jul 01/05
Subtask 05-51-18-210-052 R
F. Check after Damage on the Nose and/or the Main Landing Gear (Ref. TASK 32-21-00-220-801) (Ref. TASK 32-11-00-220-801) (Ref. TASK 3231-00-740-801) (Ref. TASK 32-46-00-740-801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage on the nose and/or | | | | | | | | | the main landing gear during the | | | | | | | | | inspection: | | | | | | | | | (1) do the inspection of the LG: | | | | | | | | | (a) For the NLG: | | X | | | | | | | - (Ref. TASK 32-21-00-220-801)| | | | | | | | | (b) For the MLG: | | X | | | | | | | - (Ref. TASK 32-11-00-220-801)| | | | | | | | | (2) Do a BITE test of the landing gear| | X | | | | | | | (Ref. TASK 32-31-00-740-801) | | | | | | | | | (3) Do a BITE test of the BSCU | | X | | | | | | | (Ref. TASK 32-46-00-740-801) | | | | | | | | | | | | | | | | B.| | If you find damage on the components | | | | | | | | | attached to the landing gear: | | | | | | | | | (1) Examine the electrical components | | X | | | | | | | internally. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-18-210-079
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G. Check after Damage on the Belly Fairing NOTE : If there is damage to the aircraft structure, refer to the ____ Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures.
EFF : ALL 05-51-18 SROS
Page 621 Jul 01/05
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage during the | | | | | | | | | inspection: | | | | | | | | | (1) Refer to the allowable damage and | | X | | | | | | | repair (Ref. SRM). | | | | | | | | | (2) If you find a through hole: | | | | | | | | | (a) Get access internally and | | X | | | | | | | examine the adjacent and | | | | | | | | | underneath area to do a check | | | | | | | | | of all the components (pipes, | | | | | | | | | items of equipment, electrical| | | | | | | | | harnesses...) for damage. | | | | | | | | | If you find damage: | | | | | | | | | - replace or repair the | | | X | | | | | | related component. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-18-210-080 H. Check after damage on the ADIRS Probes and Sensors NOTE : If there is damage to the aircraft structure, refer to the ____ Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures. (Ref. TASK 34-11-15-200-801) (Ref. TASK 34-13-00-740-803) (Ref. TASK 3413-00-710-803) (Ref. TASK 34-11-19-000-801) (Ref. TASK 34-11-19-400-801) (Ref. TASK 30-31-00-710-801) (Ref. TASK 3411-00-710-801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | Pitot probes | | | | | | | | | (1) If you find damage during the | | | | | | | | | inspection: | | | | | | | | | (a) do the inspection/check of the| | X | | | | | | | pitot probes | | | | | | | | | (Ref. TASK 34-11-15-200-801). | | | | | | | | | (b) If you find damage on the | | | | | | | | | adjacent area: | | | | | | | | | - refer to the allowable | | X | | | | | | | damage and repair (Ref. SRM)| | | | | |
EFF : ALL 05-51-18 SROS
Page 622 Jan 01/07
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | | | | | | | | B.| | Static probes | | | | | | | | | (1) If you find damage during the | | | | | | | | | inspection: | | | | | | | | | (a) refer to allowable damage and | | X | | | | | | | repair (Ref. SRM) | | | | | | | | | | | | | | | | C.| | TAT sensors | | | | | | | | | (1) If you find damage during the | | | | | | | | | inspection: | | | | | | | | | (a) do the SYSTEM TEST of the ADR | | X | | | | | | | (Ref. TASK 34-13-00-740-803). | | | | | | | | | (b) If you find damage on the | | | | | | | | | adjacent area: | | | | | | | | | - refer to the allowable | | X | | | | | | | damage and repair (Ref. SRM)| | | | | | | | | | | | | | | | D.| | AOA sensors | | | | | | | | | (1) If you find damage during the | | | | | | | | | inspection: | | | | | | | | | (a) Do the AOA SENSOR TEST | | X | | | | | | | (Ref. TASK 34-13-00-710-803) | | | | | | | | | (b) Manually rotate the AOA | | X | | | | | | | sensors to the full up | | | | | | | | | position then to the full down| | | | | | | | | position and make sure that | | | | | | | | | there is no hard point. | | | | | | | | | If you find a hard point: | | | | | | | | | - replace the related AOA | | | X | | | | | | sensor | | | | | | | | | (Ref. TASK 34-11-19-000-801)| | | | | | | | | (Ref. TASK 34-11-19-400-801)| | | | | | | | | (c) If you find damage on the | | | | | | | | | adjacent area: | | | | | | | | | - refer to the allowable | | X | | | | | | | damage and repair (Ref. SRM)| | | | | | | | | | | | | | | | E.| | If you find damage on AOA, TAT, static| | | | | | | | | or pitot probes: | | | | | | | | | (1) Do the operational test of the | | X | | | | | | | probe ice protection system | | | | | | | | | (Ref. TASK 30-31-00-710-801). | | | | | | | | | (2) Do an operational test of the AIR | | X | | | |
EFF : ALL 05-51-18 R SROS
Page 623 Apr 01/02
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | DATA switching | | | | | | | | | (Ref. TASK 34-11-00-710-801) | | | | | | ------------------------------------------------------------------------------Subtask 05-51-18-210-081 R
J. Check after damage on the Ice Detection Probes (Ref. TASK 30-81-00-710-801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | Ice detection probes | | | | | | | | | (1) If you find damage during the | | | | | | | | | inspection: | | | | | | | | | (a) Do the operational test of the| | X | | | | | | | ice detection system | | | | | | | | | (Ref. TASK 30-81-00-710-801). | | | | | | ------------------------------------------------------------------------------Subtask 05-51-18-210-082
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K. Check after damage on the Drain Masts (Ref. TASK 30-71-00-740-801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | Drain masts | | | | | | | | | (1) If you find damage during the | | | | | | | | | inspection: | | | | | | | | | (a) Do the BITE test of the waste | | X | | | | | | | water ice-protection system | | | | | | | | | (Ref. TASK 30-71-00-740-801). | | | | | | -------------------------------------------------------------------------------
EFF : ALL 05-51-18 SROS
Page 624 Jul 01/05
Subtask 05-51-18-210-083 R
L. Check after Damage on the Exterior Lights (Ref. TASK 33-41-00-710-802) (Ref. TASK 33-42-11-400-801) (Ref. TASK 3347-00-710-801) (Ref. TASK 33-48-00-710-801) (Ref. TASK 33-49-00-710-801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage on exterior lights:| | | | | | | | | (1) Do the operational test of the | | X | | | | | | | related system: | | | | | | | | | (a) For the navigation lights: | | | | | | | | | - (Ref. TASK 33-41-00-710-802)| | | | | | | | | (b) For the landing lights: | | | | | | | | | - do the test given in the | | | | | | | | | installation of the landing | | | | | | | | | lights | | | | | | | | | (Ref. TASK 33-42-11-400-801)| | | | | | | | | (c) For the logo lights: | | | | | | | | | - (Ref. TASK 33-47-00-710-801)| | | | | | | | | (d) For the anti-collision/strobe | | | | | | | | | lightning: | | | | | | | | | - (Ref. TASK 33-48-00-710-801)| | | | | | | | | (e) For the wing and engine scan | | | | | | | | | lightning: | | | | | | | | | - (Ref. TASK 33-49-00-710-801)| | | | | | ------------------------------------------------------------------------------Subtask 05-51-18-210-084
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M. Not applicable. Subtask 05-51-18-210-085
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N. Check after Damage on the Communication Antennas NOTE : If there is damage to the aircraft structure, refer to the ____ Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures. (Ref. TASK 23-12-00-710-801) (Ref. TASK 23-11-00-710-801) (Ref. TASK 5532-11-000-801)
EFF : ALL 05-51-18 SROS
Page 625 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | VHF antennas | | | | | | | | | (1) If you find damage during the | | | | | | | | | inspection: | | | | | | | | | (a) Do the operational test of the| | X | | | | | | | VHF system | | | | | | | | | (Ref. TASK 23-12-00-710-801). | | | | | | | B.| | HF fairing | | | | | | | | | (1) If you find damage on the HF | | | | | | | | | fairing: | | | | | | | | | - refer to allowable damage and | | X | | | | | | | repair (Ref. SRM) | | | | | | | | | (2) If you find a through hole on the | | | | | | | | | HF fairing during the inspection: | | | | | | | | | (a) Remove the HF fairing | | X | | | | | | | (Ref. TASK 55-32-11-000-801) | | | | | | | | | (b) Examine the HF antenna for | | X | | | | | | | signs of arc attachment | | | | | | | | | (c) Do the operational test of the| | X | | | | | | | HF system | | | | | | | | | (Ref. TASK 23-11-00-710-801). | | | | | | ------------------------------------------------------------------------------R R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 402-449, 451-499, 701-749, Subtask 05-51-18-210-086
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P. Check after Damage on the Navigation Antennas NOTE : If there is damage to the aircraft structure, refer to the ____ Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures. (Ref. TASK 34-51-00-740-801) (Ref. TASK 34-42-00-740-801) (Ref. TASK 3443-00-740-801) (Ref. TASK 34-53-00-710-801) (Ref. TASK 34-52-00-740-801) (Ref. TASK 34-55-00-710-801) (Ref. TASK 3448-00-740-801) (Ref. TASK 55-34-11-000-801) (Ref. TASK 34-36-00-710-803)
EFF : ALL 05-51-18 SROS
Page 626 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | DME antennas | | | | | | | | | (1) If you find damage during the | | | | | | | | | inspection: | | | | | | | | | - do the BITE test of the DME | | X | | | | | | | (Ref. TASK 34-51-00-740-801). | | | | | | | | | | | | | | | | B.| | Radio altimeter antennas | | | | | | | | | (1) If you find damage during the | | | | | | | | | inspection: | | | | | | | | | - do the BITE test of the radio | | X | | | | | | | altimeter | | | | | | | | | (Ref. TASK 34-42-00-740-801). | | | | | | | | | | | | | | | | C.| | ADF antenna(s) | | | | | | | | | (1) If you find a through hole during | | | | | | | | | the inspection: | | | | | | | | | - do the operational test of the | | X | | | | | | | ADF | | | | | | | | | (Ref. TASK 34-53-00-710-801). | | | | | | | | | | | | | | | | D.| | ATC antenna(s) | | | | | | | | | (1) If you find damage during the | | | | | | | | | inspection: | | | | | | | | | - do the BITE test of the ATC | | X | | | | | | | (Ref. TASK 34-52-00-740-801). | | | | | | | | | | | | | | | | E.| | TCAS antennas | | | | | | | | | (1) If you find damage during the | | | | | | | | | inspection: | | | | | | | | | - do the BITE test of the TCAS | | X | | | | | | | (Ref. TASK 34-43-00-740-801). | | | | | | | | | | | | | | | | F.| | GPS antennas | | | | | | | | | (1) If you find a through hole during | | | | | | | | | the inspection: | | | | | | | | | - do the operational test of the | | X | | | | | | | GPS | | | | | | | | | (Ref. TASK 34-36-00-710-803) | | | | | | | | | | | | | | | | G.| | VOR/MKR antennas | | | | | | | | | (1) If you find damage on the fin tip | | | | | | | | | cap (VOR fairing): | | | | | | | | | - refer to allowable damage and | | X | | | |
R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-18 301-399, 402-449, 451-499, 701-749, SROS
Page 627 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | repair (Ref. SRM) | | | | | | | | | If you find a through hole on the | | | | | | | | | fin tip cap: | | | | | | | | | - remove the fin tip cap | | X | | | | | | | (Ref. TASK 55-34-11-000-801) | | | | | | | | | - examine the VOR antenna for | | X | | | | | | | signs of arc attachment | | | | | | | | | (2) If you find damage on the MKR | | | | | | | | | antenna and/or a through hole on | | | | | | | | | the fin tip cap: | | | | | | | | | - do the operational test of the | | X | | | | | | | VOR/MKR system | | | | | | | | | (Ref. TASK 34-55-00-710-801). | | | | | | | | | | | | | | | | H.| | GPWS system | | | | | | | | | (1) If you find damage on the radio | | | | | | | | | altimeter antennas and/or ILS | | | | | | | | | antennas (glide and/or localizer):| | | | | | | | | - do the BITE test of the GPWS | | X | | | | | | | (Ref. TASK 34-48-00-740-801). | | | | | | ------------------------------------------------------------------------------**ON A/C 401-401, Subtask 05-51-18-210-086-A R
P. Check after Damage on the Navigation Antennas NOTE : If there is damage to the aircraft structure, refer to the ____ Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures. (Ref. TASK 34-51-00-740-801) (Ref. TASK 34-42-00-740-801) (Ref. TASK 3443-00-740-801) (Ref. TASK 34-53-00-710-801) (Ref. TASK 34-52-00-740-801) (Ref. TASK 34-55-00-710-801) (Ref. TASK 3448-00-740-801) (Ref. TASK 55-34-11-000-801)
R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-18 301-399, 401-449, 451-499, 701-749, SROS
Page 628 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | DME antennas | | | | | | | | | (1) If you find damage during the | | | | | | | | | inspection: | | | | | | | | | - do the BITE test of the DME | | X | | | | | | | (Ref. TASK 34-51-00-740-801). | | | | | | | | | | | | | | | | B.| | Radio altimeter antennas | | | | | | | | | (1) If you find damage during the | | | | | | | | | inspection: | | | | | | | | | - do the BITE test of the radio | | X | | | | | | | altimeter | | | | | | | | | (Ref. TASK 34-42-00-740-801). | | | | | | | | | | | | | | | | C.| | ADF antenna(s) | | | | | | | | | (1) If you find a through hole during | | | | | | | | | the inspection: | | | | | | | | | - do the operational test of the | | X | | | | | | | ADF | | | | | | | | | (Ref. TASK 34-53-00-710-801). | | | | | | | | | | | | | | | | D.| | ATC antenna(s) | | | | | | | | | (1) If you find damage during the | | | | | | | | | inspection: | | | | | | | | | - do the BITE test of the ATC | | X | | | | | | | (Ref. TASK 34-52-00-740-801). | | | | | | | | | | | | | | | | E.| | TCAS antennas | | | | | | | | | (1) If you find damage during the | | | | | | | | | inspection: | | | | | | | | | - do the BITE test of the TCAS | | X | | | | | | | (Ref. TASK 34-43-00-740-801). | | | | | | | | | | | | | | | | F.| | VOR/MKR antennas | | | | | | | | | (1) If you find damage on the fin tip | | | | | | | | | cap (VOR fairing): | | | | | | | | | - refer to allowable damage and | | X | | | | | | | repair (Ref. SRM) | | | | | | | | | If you find a through hole on the | | | | | | | | | fin tip cap: | | | | | | | | | - remove the fin tip cap | | X | | | | | | | (Ref. TASK 55-34-11-000-801) | | | | | | | | | - examine the VOR antenna for | | X | | | | | | | signs of arc attachment | | | | | |
EFF : 401-401, 05-51-18 R SROS
Page 629 Apr 01/02
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (2) If you find damage on the MKR | | | | | | | | | antenna and/or a through hole on | | | | | | | | | the fin tip cap: | | | | | | | | | - do the operational test of the | | X | | | | | | | VOR/MKR system | | | | | | | | | (Ref. TASK 34-55-00-710-801). | | | | | | | | | | | | | | | | G.| | GPWS system | | | | | | | | | (1) If you find damage on the radio | | | | | | | | | altimeter antennas and/or ILS | | | | | | | | | antennas (glide and/or localizer):| | | | | | | | | - do the BITE test of the GPWS | | X | | | | | | | (Ref. TASK 34-48-00-740-801). | | | | | | ------------------------------------------------------------------------------**ON A/C ALL Subtask 05-51-18-210-087 R
Q. Check after Damage on the Fuselage Skin NOTE : If there is damage to the aircraft structure, refer to the ____ Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage during the | | | | | | | | | inspection: | | | | | | | | | (1) Refer to the flow chart for the | | X | | | | | | | allowable damage and repair | | | | | | | | | (Ref. SRM). | | | | | | | | | (2) If you find a through hole: | | X | | | | | | | (a) Examine internally the | | | | | | | | | adjacent area of the damage | | | | | | | | | specially the components, the | | | | | | | | | pipes and the electrical looms| | | | | | | | | for damage. | | | | | | | | | If you find damage: | | | | | | | | | - repair or replace the | | | X | | |
EFF : ALL 05-51-18 SROS
Page 630 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | related component. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-18-210-088 R
R. Check of the APU after Damage on the APU Exhaust (Ref. TASK 49-00-00-710801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage on the APU exhaust | | | | | | | | | during the inspection: | | | | | | | | | (1) Do the operational test of the | | X | | | | | | | APU | | | | | | | | | (Ref. TASK 49-00-00-710-801). | | | | | | ------------------------------------------------------------------------------Subtask 05-51-18-210-089
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S. Check after Damage on the Wings NOTE : If there is damage to the aircraft structure, refer to the ____ Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures. (Ref. TASK 27-84-00-710-801) (Ref. TASK 27-54-00-710-801) (Ref. TASK 2764-00-710-801) (Ref. TASK 27-14-51-000-801) (Ref. TASK 27-14-51-000-802) (Ref. TASK 27-14-51-400-801) (Ref. TASK 2714-51-400-802) (Ref. TASK 27-14-00-710-801)
EFF : ALL 05-51-18 SROS
Page 631 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage on the top or | | | | | | | | | bottom of the wings: | | | | | | | | | (1) Refer to allowable damage and | | X | | | | | | | repair (Ref. SRM) | | | | | | | | | | | | | | | | B.| | If you find damage on the slats: | | | | | | | | | (1) Refer to allowable damage and | | X | | | | | | | repair (Ref. SRM) | | | | | | | | | (2) Do the operational test of the | | X | | | | | | | slats | | | | | | | | | (Ref. TASK 27-84-00-710-801). | | | | | | | | | | | | | | | | C.| | If you find damage on the flap track | | | | | | | | | fairings: | | | | | | | | | (1) Refer to allowable damage and | | X | | | | | | | repair (Ref. SRM) | | | | | | | | | | | | | | | | D.| | If you find damage on the flaps: | | | | | | | | | (1) Refer to allowable damage and | | X | | | | | | | repair (Ref. SRM) | | | | | | | | | (2) Examine the bonding leads (on the | | X | | | | | | | hinges) of the related damaged | | | | | | | | | flap for breakage and defective | | | | | | | | | attachment. | | | | | | | | | If you find damage: | | | | | | | | | - replace the bonding lead and/or | | | X | | | | | | the defective attachment | | | | | | | | | (3) Do the operational test of the | | X | | | | | | | flaps | | | | | | | | | (Ref. TASK 27-54-00-710-801). | | | | | | | | | | | | | | | | E.| | If you find damage on the spoilers: | | | | | | | | | (1) Refer to allowable damage and | | X | | | | | | | repair (Ref. SRM) | | | | | | | | | (2) Examine the bonding leads (on the | | X | | | | | | | hinges) of the related damaged | | | | | | | | | spoiler for breakage and | | | | | | | | | defective attachment. | | | | | | | | | If you find damage: | | | | | | | | | - replace the bonding lead and/or | | | X | | | | | | the defective attachment | | | | | | | | | (3) Do the operational test of the | | X | | | | | | | spoilers | | | | | |
EFF : ALL 05-51-18 R SROS
Page 632 Apr 01/02
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (Ref. TASK 27-64-00-710-801). | | | | | | | | | | | | | | | | F.| | If you find damage on the ailerons: | | | | | | | | | (1) Refer to allowable damage and | | X | | | | | | | repair (Ref. SRM) | | | | | | | | | (2) Examine all the bonding leads of | | X | | | | | | | the aileron hinges and | | | | | | | | | servocontrols of the related | | | | | | | | | damaged aileron for breakage and | | | | | | | | | defective attachment. | | | | | | | | | If you find damage: | | | | | | | | | - replace the bonding lead and/or | | | X | | | | | | the defective attachment | | | | | | | | | (3) Examine the piston rod of each | | X | | | | | | | servocontrol (it must be fully | | | | | | | | | extended) of the related damaged | | | | | | | | | aileron for burn marks, damage and| | | | | | | | | leaks. | | | | | | | | | If you find a leak or damage: | | | | | | | | | (a) Replace the related aileron | | | X | | | | | | servocontrol | | | | | | | | | (Ref. TASK 27-14-51-000-801) | | | | | | | | | (Ref. TASK 27-14-51-400-801) | | | | | | | | | (Ref. TASK 27-14-51-000-802) | | | | | | | | | (Ref. TASK 27-14-51-400-802) | | | | | | | | |NOTE: If you are at a line station and | | | | | | | | | you cannot do the inspection of | | | | | | | | | the piston rod, do this check: | | | | | | | | | - operate the ailerons 10 times | | | | | | | | | fully in each direction then | | | | | | | | | make sure from the ground that | | | | | | | | | there are no leaks below the | | | | | | | | | aileron servocontrols. | | | | | | | | | You must do this check before | | | | | | | | | each flight until the return to| | | | | | | | | the main base. You can do the | | | | | | | | | check before each flight for a | | | | | | | | | maximum of 3 days or 10 flights| | | | | | | | | - At the first return to the main| | | | | | | | | base, you must do the | | | | | | | | | inspection of the piston rods. | | | | | | | | | (4) Do the operational test of the | | X | | | | | | | ailerons | | | | | |
EFF : ALL 05-51-18 R SROS
Page 633 Apr 01/02
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (Ref. TASK 27-14-00-710-801). | | | | | | ------------------------------------------------------------------------------**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-18-210-054 T. Check after Damage on the Engine Nacelles and Pylons NOTE : If there is damage to the aircraft structure, refer to the ____ Structural Repair Manual (SRM) and/or to the applicable Nacelle Structural Repair Manual. The SRM has the approved damage limits and repair procedures.
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(Ref. TASK 78-31-00-710-804) (Ref. TASK 73-21-00-710-803) (Ref. TASK 2422-51-210-802)
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage on the air intake, | | | | | | | | | inlet cowl, fan cowl, thrust reverser,| | | | | | | | | exhaust nozzle or the pylon: | | | | | | | | | (1) Refer to the allowable damage and | | X | | | | | | | repair (Ref. SRM and/or applicable| | | | | | | | | Nacelle SRM). | | | | | | | | | (2) At the first return to the main | | X | | | | | | | base, do the inspection of the | | | | | | | | | lightning protection module | | | | | | | | | (Ref. TASK 24-22-51-210-802) | | | | | | | | | (3) If you find damage on the thrust | | | | | | | | | reverser: | | | | | | | | | (a) Do an operational test of the | | X | | | | | | | thrust reverser system | | | | | | | | | (Ref. TASK 78-31-00-710-804). | | | | | | | | | (4) If you find a through hole | | | | | | | | | on the fan cowl: | | | | | | | | | (a) Do a ground test of the FADEC | | X | | | | | | | (Ref. TASK 73-21-00-710-803) | | | | | | -------------------------------------------------------------------------------
EFF : ALL 05-51-18 SROS
Page 634 Jan 01/06
**ON A/C 701-749, Subtask 05-51-18-210-054-A T. Check after Damage on the Engine Nacelles and Pylons NOTE : If there is damage to the aircraft structure, refer to the ____ Structural Repair Manual (SRM) and/or to the applicable Nacelle Structural Repair Manual. The SRM has the approved damage limits and repair procedures.
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(Ref. TASK 78-31-00-740-802) (Ref. TASK 73-21-00-710-812) (Ref. TASK 2422-51-210-802)
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage on the air intake, | | | | | | | | | inlet cowl, fan cowl, thrust reverser,| | | | | | | | | exhaust nozzle or the pylon: | | | | | | | | | (1) Refer to the allowable damage and | | X | | | | | | | repair (Ref. SRM and/or applicable| | | | | | | | | Nacelle SRM). | | | | | | | | | (2) At the first return to the main | | X | | | | | | | base, do the inspection of the | | | | | | | | | lightning protection module | | | | | | | | | (Ref. TASK 24-22-51-210-802) | | | | | | | | | (3) If you find damage on the thrust | | | | | | | | | reverser: | | | | | | | | | (a) Do an operational test of the | | X | | | | | | | thrust reverser system | | | | | | | | | (Ref. TASK 78-31-00-740-802). | | | | | | | | | (4) If you find a through hole | | | | | | | | | on the fan cowl: | | | | | | | | | (a) Do a ground test of the FADEC | | X | | | | | | | (Ref. TASK 73-21-00-710-812) | | | | | | -------------------------------------------------------------------------------
EFF : 701-749, 05-51-18 SROS
Page 635 Jan 01/06
**ON A/C ALL Subtask 05-51-18-210-090 R
U. Check after Damage on the Stabilizers NOTE : If there is damage to the aircraft structure, refer to the ____ Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures. (Ref. TASK 27-24-51-000-801) (Ref. TASK 27-24-51-400-801) (Ref. TASK 2724-00-710-801) (Ref. TASK 27-34-51-000-801) (Ref. TASK 27-34-51-400-801) (Ref. TASK 27-34-00-710-801) (Ref. TASK 2744-00-710-801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage during the | | | | | | | | | inspection on the skin of the vertical| X | | | | | | | | stabilizer and the rudder, the fin | | | | | | | | | tip cap, the fin and rudder tip cap | | | | | | | | | lightning diverters: | | | | | | | | | (1) Refer to allowable damage and | | X | | | | | | | repair (Ref. SRM) | | | | | | | | | (2) Examine all the electrical bonding| | X | | | | | | | leads of the rudder hinges and | | | | | | | | | servocontrols for breakage and | | | | | | | | | defective attachment. | | | | | | | | | If you find damage: | | | | | | | | | (a) replace the electrical bonding| | | X | | | | | | lead and/or the defective | | | | | | | | | attachment | | | | | | | | | (3) At the first return to the main | | X | | | | | | | base, examine the piston rod of | | | | | | | | | each rudder servocontrol (it must | | | | | | | | | be fully extended) for damage and | | | | | | | | | burn marks and make sure that | | | | | | | | | there are no leaks. | | | | | | | | | If you find a leak or damage: | | | | | | | | | - replace the related rudder | | | X | | | | | | servocontrol | | | | | | | | | (Ref. TASK 27-24-51-000-801) | | | | | | | | | (Ref. TASK 27-24-51-400-801). | | | | | | | | | (4) Do an operational test of the | | X | | | |
EFF : ALL 05-51-18 SROS
Page 636 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | rudder | | | | | | | | | (Ref. TASK 27-24-00-710-801). | | | | | | | | | | | | | | | | B.| | If you find damage during the | | | | | | | | | inspection of the horizontal | | | | | | | | | stabilizer and elevators: | | | | | | | | | (1) Refer to allowable damage and | | X | | | | | | | repair (Ref. SRM) | | | | | | | | | (2) Examine all the electrical bonding| | X | | | | | | | leads of the elevator hinges and | | | | | | | | | servocontrols of the related | | | | | | | | | damaged elevator for breakage and | | | | | | | | | defective attachment. | | | | | | | | | If you find damage: | | | | | | | | | (a) replace the electrical bonding| | | X | | | | | | lead and/or the defective | | | | | | | | | attachment. | | | | | | | | | (3) Examine the piston rod of each | | X | | | | | | | elevator servocontrol (it must be | | | | | | | | | fully extended) of the related | | | | | | | | | damaged elevator for burn marks, | | | | | | | | | damage and leaks. | | | | | | | | | If you find a leak or damage: | | | | | | | | | (a) Replace the related elevator | | | X | | | | | | servocontrol | | | | | | | | | (Ref. TASK 27-34-51-000-801) | | | | | | | | | (Ref. TASK 27-34-51-400-801) | | | | | | | | |NOTE: If you are at a line station and | | | | | | | | | you cannot do the inspection of | | | | | | | | | the piston rod, do this check: | | | | | | | | | - operate the elevators 10 times | | | | | | | | | fully in each direction then | | | | | | | | | make sure from the ground that | | | | | | | | | there are no leaks below the | | | | | | | | | elevator servocontrols. | | | | | | | | | You must do this check before | | | | | | | | | each flight until the return to| | | | | | | | | the main base. You can do the | | | | | | | | | check before each flight for a | | | | | | | | | maximum of 3 days or 10 flights| | | | | | | | | - At the first return to the main| | | | | | | | | base, you must do the | | | | | | | | | inspection of the piston rods. | | | | | |
EFF : ALL 05-51-18 R SROS
Page 637 Apr 01/02
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (4) Do an operational test of the | | X | | | | | | | elevators | | | | | | | | | (Ref. TASK 27-34-00-710-801). | | | | | | | | | (5) Do an operational test of the THS | | X | | | | | | | (Ref. TASK 27-44-00-710-801). | | | | | | ------------------------------------------------------------------------------Subtask 05-51-18-210-091 R
V. Check after Damage on the Static Dischargers (Ref. TASK 23-61-00-200-801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage on the static | | | | | | | | | dischargers of the wing or vertical | | | | | | | | | and horizontal stabilizer. | | | | | | | | | (1) Do a check of the related static | | X | | | | | | | discharger | | | | | | | | | (Ref. TASK 23-61-00-200-801). | | | | | | | | | NOTE: (Ref. CDL 6.01.23 P01): | | | | | | | | | - 2 static dischargers can be | | | | | | | | | missing on each wing. | | | | | | | | | - 2 static discharger can be | | | | | | | | | missing on each horizontal | | | | | | | | | stabilizer tip zone (including| | | | | | | | | the elevator). | | | | | | | | | - 2 static discharger can be | | | | | | | | | missing on the vertical | | | | | | | | | stabilizer tip zone (including| | | | | | | | | the rudder). | | | | | | -------------------------------------------------------------------------------
EFF : ALL 05-51-18 SROS
Page 638 Jul 01/05
**ON A/C 401-449, 451-499, Subtask 05-51-18-210-093 R
W. Check after Damage on the Exterior Video Systems (Ref. TASK 23-36-00-710-808) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| |If you find damage on the Landscape| | | | | | | | |Camera: | | | | | | | | |(1) Do the operational test of the | | X | | | | | | | Landscape- Camera System: | | | | | | | | | (Ref. TASK 23-36-00-710-808). | | | | | | -----------------------------------------------------------------------------**ON A/C ALL 5. Close-up ________ Subtask 05-51-18-866-052 A. Retraction of the Flight control surfaces (1) Retract the flaps and the slats (Ref. TASK 27-50-00-866-802). (2) Retract the spoilers (Ref. TASK 27-60-00-866-802). Subtask 05-51-18-410-050 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the NLG doors (Ref. TASK 32-22-00-410-801). (3) Close the MLG doors (Ref. TASK 32-12-00-410-801). (4) Close all the access doors, and the access panels opened during the inspection procedure. (5) Remove the access platform(s).
EFF : ALL 05-51-18 SROS
Page 639 Jul 01/05
(6) Remove the warning notice(s).
EFF : ALL 05-51-18 SROS
Page 640 Jul 01/02
INSPECTION AFTER ENGINE BIRD STRIKE OR SLUSH INGESTION - INSPECTION/CHECK _________________________________________________________________________ TASK 05-51-19-200-801 Inspection after Engine Bird Strike or Slush Ingestion 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. 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------71-00-00-200-803 72-00-00-200-811
Inspection after a Birdstrike and Foreign Object Damage Inspection Procedure After Birdstrike (Foreign Object Damage)
3. __________ Job Set-up Subtask 05-51-19-941-050 A. Not Applicable.
EFF : ALL 05-51-19 SROS
Page 601 Jan 01/07
4. Procedure _________ **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-19-210-050 A. Inspection of the engine (Ref. TASK 72-00-00-200-811) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Do the inspection after Birdstrike: | X | | | | | | | | (Ref. TASK 72-00-00-200-81100) | | | | | | ------------------------------------------------------------------------------**ON A/C 701-749, Subtask 05-51-19-210-050-A A. Inspection of the engine (Ref. TASK 71-00-00-200-803) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Do the inspection after a Birdstrike: | X | | | | | | | | (Ref. TASK 71-00-00-200-80300) | | | | | | -------------------------------------------------------------------------------
R EFF : ALL 05-51-19 SROS
Page 602 Jan 01/07
INSPECTION AFTER TAIL RUNWAY IMPACT - INSPECTION/CHECK ______________________________________________________ TASK 05-51-21-200-801 Inspection after a Tail Runway Impact 1. __________________ Reason for the Job This inspection is applicable when the tail hits the runway during the take-off or the landing. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
adjustable access platform 7 m (22 ft. 12 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R
32-11-00-220-802 49-12-00-200-801 49-16-00-200-801 05-51-21-991-001
Check of Shock Absorber Nitrogen Charge Pressure Visual Check of APU Suspension System Including Shockmount Structure And Brackets Inspection of the Air Intake System Fig. 601
3. __________ Job Set-up Subtask 05-51-21-010-050 A. Get Access (1) Put an adjustable access platform in position at the tail cone. (2) Open the access panels 312AR, 313AL, 316AR and 315AL.
EFF : ALL 05-51-21 SROS
Page 601 Jan 01/07
4. Procedure _________ (Ref. Fig. 601/TASK 05-51-21-991-001) Subtask 05-51-21-210-050 A. Inspection of the Tail Cone (Ref. TASK 49-16-00-200-801), (Ref. TASK 4912-00-200-801)
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the Fuselage | | | | | | | | | | | | | | | | A.| |Externally examine the skin panels | X | | | | | | | |(FR75 thru FR78) for damaged paintwork | | | | | | | | |and any other type of damage. | | | | | | | | |If you find damage: | | | | | | | | |- internally examine the frames, the | | X | | | | | | | skin panels, the clips and the | | | | | | | | | stringers for damaged paintwork, | | | | | | | | | distortion, cracks, scratches, dents,| | | | | | | | | pulled or torn fasteners (Extend | | | | | | | | | inspection area as necessary). | | | | | | | | | | | | | | | |2. | |Inspection of the APU Air Intake and | | | | | | | | |the APU compartment | | | | | | | | | | | | | | | | A.| |Examine the APU diverter, intake flap, | X | | | | | | | |intake nose and drain mast for: | | | | | | | | |- damaged paintwork, distortion, | | | | | | | | | cracks, scratches, dents, pulled or | | | | | | | | | torn fasteners. | | | | | | | | |If you find damage: | | | | | | | | |- do the inspection of the Air Intake | | X | | | | | | | system: | | | | | | | | | (Ref. TASK 49-16-00-200-801) | | | | | | | | | | | | | | | | B.| |Examine the APU compartment for leakage| | | | | | | | |and damage: | | | | | | | | |if you find damage: | | | | | | | | |(1) make sure that the APU is correctly| | | | | | | | |installed. | | | | | | | | |(2) examine the mountings for damage, | | | | | | | | |distortion and signs of movement | | | | | | | | |(Ref. TASK 49-12-00-200-804). | | | | | |
EFF : ALL 05-51-21 SROS
Page 602 Oct 01/04
Location of APU Components to be Inspected Figure 601/TASK 05-51-21-991-001 EFF : ALL 05-51-21 SROS
Page 603 Apr 01/98
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| ------------------------------------------------------------------------------Subtask 05-51-21-210-051 B. Inspection of the Main Landing Gear (MLG) (Ref. TASK 32-11-00-220-802)
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the Shock Absorber | | | | | | | | |Pressure | | | | | | | | | | | | | | | | A.| |Do a check of the MLG shock-absorber | X | | | | | | | |pressure | | | | | | | | |(Ref. TASK 32-11-00-220-80200). | | | | | | | | | | | | | | | ------------------------------------------------------------------------------5. Close-up ________ Subtask 05-51-21-410-050 A. Close Access (1) Close the access panels 312AR, 313AL, 316AR and 315AL. Subtask 05-51-21-942-050 B. Put the Aircraft back to its Initial Configuration (1) Remove the access platform(s). (2) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-51-21 SROS
Page 604 Jan 01/07
INSPECTION AFTER NLG TOWING OVERLOAD OR OVERRUN - INSPECTION/CHECK __________________________________________________________________ TASK 05-51-22-200-801 Inspection after NLG Towing Overload or Overrun 1. __________________ Reason for the Job This procedure is necessary when unwanted movements have occurred after the shear pin of the tow bar has broken during towing. Do an inspection of the nose gear only: - if, after the shear pin has broken . the aircraft moves farther than the tow bar - or if, after a turn (aircraft pushed), the bar touches the tow vehicle. Do not do this inspection if you stopped towing when the shear pin broke. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No
specific specific specific specific
safety barriers warning notice wheel chocks adjustable access platform 2.5 m (8 ft. 2 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------05-56-00-200-801 24-41-00-861-801 24-41-00-862-801 24-42-00-861-801 24-42-00-862-801 29-00-00-863-801 29-00-00-864-801
Measurement of the Aircraft by Photogrammetry after Abnormal Operation of the Aircraft Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Energize the Ground Service Network De-energize the Ground Service Network Pressurize the Green Hydraulic System with the Ground Hydraulic Supply Depressurize the Green Hydraulic System (Pressurized with the Hydraulic Ground Supply)
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Page 601 Apr 01/98
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-00-00-081-801 32-00-00-481-801
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32-22-00-010-801 32-22-00-410-801 32-30-00-867-801 32-30-00-867-802 32-31-00-720-802 32-31-22-000-801 05-51-22-991-001
Removal of the Safety Devices from the Landing Gears Installation of the Safety Devices on the Landing Gears Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance Retraction of the Landing Gear for Maintenance Extension of the Landing Gear After Maintenance Functional Check to Ensure that the Safety Valve Closes at 280 KTS Removal of the NLG Actuator (5201GA) Fig. 601
3. __________ Job Set-up Subtask 05-51-22-941-050 A. Safety Precautions (1) Put the safety barriers in position. (2) Put a warning notice in position in the cockpit, on the panel 312VU, to tell persons not to operate the nose landing gear and the NLG doors. (3) Put wheel chocks in position at the main landing gear. (4) Install the safety devices on the landing gear (Ref. TASK 32-00-00481-801). Subtask 05-51-22-860-052 B. Aircraft Maintenance Configuration (1) Energize the ground service network (Ref. TASK 24-42-00-861-801) (2) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-801) (3) Pressurize the Green hydraulic system (Ref. TASK 29-00-00-863-801)
EFF : ALL 05-51-22 SROS
Page 602 Jan 01/07
Subtask 05-51-22-010-050 C. Get Access (1) Open the NLG door (Ref. TASK 32-22-00-010-801). (2) Open the access door 811. (3) Put an adjustable access platform in position near the aircraft. Subtask 05-51-22-860-050 D. Aircraft Maintenance Configuration (1) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (2) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). 4. Procedure _________ (Ref. Fig. 601/TASK 05-51-22-991-001) Subtask 05-51-22-210-050 A. Inspection of the NLG well (Ref. TASK 05-56-00-200-801) (Ref. TASK 32-31-22-000-801) (Ref. Fig. 601/TASK 05-51-22-991-001) NOTE : All the necessary inspections are visual unless specified ____ differently on the test procedure. Operators can refer to the Non Destructive Testing Manual (NTM) and use non destructive procedure. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the NLG Well | | | | | | | | | (Ref. Fig. 601/TASK 05-51-22-991-001) | | | | | | | A.| | Examine the attachment fittings of the| | | | | | | | | drag stay assembly and the bearings | X | | | | | | | | for: | | | | | | | | | - distortion, cracks and damaged | | | | | | | | | paintwork | | | | | | | | | | | | | | |
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Page 603 Jan 01/02
Structure of the NLG Well Figure 601/TASK 05-51-22-991-001 EFF : ALL 05-51-22 SROS
Page 604 Apr 01/98
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | B.| | Examine the attachment fitting of the | | | | | | | | | lockstay assembly for: | X | | | | | | | | - distortion, damaged paintwork and | | | | | | | | | cracks. | | | | | | | | | | | | | | | | C.| | Examine the attach fitting of the NLG | X | | | | | | | | actuator for: | | | | | | | | | - cracks, distortion and damaged | | | | | | | | | paintwork. | | | | | | | | | | | | | | | | D.| | Examine the attach fittings of the | X | | | | | | | | NLG leg for crack, distortion and | | | | | | | | | - cracks, distortion and damaged | | | | | | | | | paintwork. | | | | | | | | | | | | | | | | E.| | Get access to the avionic compartment.| | | | | | | | | Examine the structure, the machined | X | | | | | | | | panels, the attach fittings, the | | | | | | | | | support strut for: | | | | | | | | | - cracks, distortion, damaged | | | | | | | | | paintwork, pulled or torn fasteners.| | | | | | | | | If you find damage: | | | | | | | | | (1) Do a check of the angles between | | X | | | | | | | the NLG and the aircraft | | | | | | | | | (Ref. TASK 05-56-00-200-801) | | | | | | | | | (2) Remove the NLG actuator for | | | | | | | | | inspection | | X | | | | | | | (Ref. TASK 32-31-22-000-801) | | | | | | ------------------------------------------------------------------------------Subtask 05-51-22-210-051 B. Inspection of the Nose Landing Gear NOTE : All the necessary inspections are visual unless specified ____ differently in the test procedure. Operators can refer to the Non Destructive Testing Manual (NTM) and use non destructive testing procedure.
EFF : ALL 05-51-22 SROS
Page 605 Jan 01/07
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection the nose landing gear. | | | | | | | | | | | | | | | | A.| | Examine the shock absorber, the | | | | | | | | | wheels, the tires, the towing lug for:| X | | | | | | | | - distortion, cracks, damage, torn or | | | | | | | | | pulled fasteners, and damaged | | | | | | | | | paintwork. | | | | | | ------------------------------------------------------------------------------| Subtask 05-51-22-860-053 C. 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) Subtask 05-51-22-410-050 D. Close Access (1) Close the NLG doors (Ref. TASK 32-22-00-410-801). (2) Close the access door 811. (3) Close all the access doors that you opened during the inspection. (4) Remove the access platform(s). (5) Remove the safety devices installed on the landing gear (Ref. TASK 32-00-00-081-801).
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Page 606 Jan 01/02
Subtask 05-51-22-710-050 E. Do the subsequent test. R R
NOTE : The test below is necessary only if you find damage on the ____ structure adjacent to the landing gear or on the attachments. (1) Extend and retract the landing gear 5 times. Make sure the nose landing gear moves freely. (Ref. TASK 32-30-00-867-801) (Ref. TASK 32-31-00-720-802) (Ref. TASK 32-30-00-867-802)
R Subtask 05-51-22-860-051 F. Put the system back to its operational configuration. (1) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). (2) De-energize the ground service network (Ref. TASK 24-42-00-862-801)> (3) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). 5. Close-up ________ Subtask 05-51-22-942-050 A. Put the Aircraft back to its Initial Configuration (1) Remove the warning notice(s). (2) Remove the ground support and maintenance equipment, the special and standard tools and all other items. (3) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-51-22 SROS
Page 607 Oct 01/00
INSPECTION AFTER NLG STEERING ANGLE EXCEEDED - INSPECTION/CHECK _______________________________________________________________ TASK 05-51-23-200-801 Inspection of the Nose Landing Gear after a NLG Steering Angle of more than 95⁰ 1. __________________ Reason for the Job
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NOTE : If the 95⁰ NLG steering angle was exceeded by a large value (a ____ maximum of 180⁰ for example when tow vehicle control is not kept in icy conditions), it is possible that damage occurred not only to the NLG but also to its attachment structure. If this occurs, do the NLG well inspection after NLG Towing Overload or Overrun (Ref. TASK 05-51-22-200-801). 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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32-21-00-220-805
Inspection of the NLG After the NLG Steering Angle is Exceeded
3. __________ Job Set-up Subtask 05-51-23-941-050 A. Not applicable. 4. Procedure _________ Subtask 05-51-23-210-050-A A. Inspection (1) Do the Inspection of the NLG after a NLG steering angle is exceeded (Ref. TASK 32-21-00-220-805).
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Page 601 Jan 01/07
INSPECTION AFTER LEAVING RUNWAY OR TAXIWAY - INSPECTION/CHECK _____________________________________________________________ TASK 05-51-24-200-801 Inspection after Leaving a Runway or a Taxiway 1. __________________ Reason for the Job A number of factors can possibly change the loads on the landing gear and the structure. They are, for example: - the speed and the weight of the aircraft - the condition of the ground (soft or hard) - the depth the landing gear goes into the ground. R R R
NOTE : Recovery must obey the ARM requirement. If recovery is different to ____ the ARM requirement or if no recovery report is available, refer to Airbus for special instructions. You must think of all these factors when you do this inspection. You must always do this inspection fully before the next flight of the aircraft. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific No specific No specific FOR FIN 4030EM2 No specific
safety barriers warning notice wheel chocks adjustable access platform 8.3 m (27 ft. 3 in.)
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Page 601 Jul 01/05
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------05-56-00-200-801 24-41-00-861-801 24-41-00-862-801 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 27-80-00-866-801 27-80-00-866-802 28-10-00-910-802 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 32-00-00-081-801 32-00-00-481-801 32-11-11-000-801 32-11-13-000-801 32-11-15-000-801 32-12-00-010-801 32-12-00-410-801 32-21-11-000-801 32-21-13-000-801 32-21-16-000-801 32-21-17-000-801 32-22-00-010-801
Measurement of the Aircraft by Photogrammetry after Abnormal Operation of the Aircraft Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power 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 Spoilers for Maintenance Retraction of the Spoilers after Maintenance Extension of the Slats on the Ground Retraction of the Slats on the Ground Access to Fuel Tanks and Work Areas 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) Removal of the Safety Devices from the Landing Gears Installation of the Safety Devices on the Landing Gears Removal of the MLG Leg Assembly Removal of the MLG Shock Absorber Removal of the MLG Bogie-Alignment Pitch Trimmer (Weight on Wheels) Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Removal of the NLG Leg Assy (5002GN) Removal of the NLG Shock Absorber Assembly Removal of the Upper Drag Stay Assembly Removal of the Lock Stay Assembly Open the NLG Doors for Maintenance
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Page 602 Jul 01/05
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-22-00-410-801 32-31-22-000-801 32-31-46-000-801 32-41-11-000-801 32-41-12-000-801 71-00-00-000-803 71-00-00-000-805 71-00-00-400-803 71-00-00-400-805 71-13-00-010-802 71-13-00-010-805 71-13-00-410-802 71-13-00-410-805 78-31-00-710-804 78-31-00-740-802 05-51-24-991-001 05-51-24-991-002 FOR FIN 4030EM2 53-35-13-000-801 53-35-13-000-802 78-30-00-010-801 78-30-00-010-803 78-30-00-410-801 78-30-00-410-803
Close the NLG Doors after Maintenance Removal of the NLG Actuator (5201GA) Removal of the MLG Actuator 5222GA(5223GA) Removal of the MLG Wheel Removal of the NLG Wheel Removal of the Engine Removal of the Demountable Power Plant Installation of the Engine Installation of the Demountable Power Plant Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Open the Fan Cowl Doors Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Close the Fan Cowl Doors Thrust Reverser Cycling Test (MCDU) Test of the Thrust Reverser Deployment and Stowage (Engine not Running) Fig. 601 Fig. 602 Removal of the Access Panels 191AB, 191BB, 192BB, 191DB, 197AB, 197AT, 198AT, 197BB, 198BB, 197EB, 198EB, 197FB, 197GB, 198GB, 198HB and 197HB. Removal of the Belly Fairing Access Panels Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Open the Thrust Reverser Cowl Doors Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Close the Thrust Reverser Cowl Doors
3. __________ Job Set-up Subtask 05-51-24-941-050 A. Safety Precautions (1) Put a warning notice in position in the cockpit to tell persons not to operate the systems. (2) Put wheel chocks in position at the main landing gear.
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Page 603 Jan 01/06
(3) Install the safety devices on the landing gear (Ref. TASK 32-00-00481-801). (4) Put the safety barriers in position. Subtask 05-51-24-860-052 B. Aircraft Maintenance Configuration R
(1) Energize the ground service network (Ref. TASK 24-42-00-861-801).
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(2) Pressurize the Green hydraulic system (Ref. TASK 29-00-00-863-801).
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(3) Pressurize the Yellow hydraulic system (Ref. TASK 29-00-00-863-803).
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(4) Pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-802). **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-24-010-050 C. Get Access (1) Open the NLG doors (Ref. TASK 32-22-00-010-801). (2) Open the MLG doors (Ref. TASK 32-12-00-010-801). (3) Open the access door 811. (4) Open the fan cowl doors (Ref. TASK 71-13-00-010-802) FOR 4030EM1 415BL, 416BR FOR 4030EM2 425BL, 426BR (5) Open the thrust reverser door (Ref. TASK 78-30-00-010-801) FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR
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Page 604 Jan 01/06
(6) Open all the access doors and the access panels of the belly fairing (Ref. TASK 53-35-13-000-801) (Ref. TASK 53-35-13-000-802). (7) Put an adjustable access platform in position near the area where you must do the inspection. **ON A/C 701-749, Subtask 05-51-24-010-050-A C. Get Access (1) Open the NLG doors (Ref. TASK 32-22-00-010-801). (2) Open the MLG doors (Ref. TASK 32-12-00-010-801). (3) Open the access door 811. (4) Open the fan cowl doors (Ref. TASK 71-13-00-010-805) FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR (5) Open the thrust reverser door (Ref. TASK 78-30-00-010-803) FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR (6) Open all the access doors and the access panels of the belly fairing (Ref. TASK 53-35-13-000-801) (Ref. TASK 53-35-13-000-802). (7) Put an adjustable access platform in position near the area where you must do the inspection. **ON A/C ALL Subtask 05-51-24-860-050 D. Aircraft Maintenance Configuration (1) Extend the flaps to full position (Ref. TASK 27-50-00-866-801). (2) Extend the slats to full position (Ref. TASK 27-80-00-866-801).
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Page 605 Jan 01/06
(3) Extend the spoilers (Ref. TASK 27-60-00-866-801). (4) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (5) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803). (6) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802). (7) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). 4. Procedure _________ Subtask 05-51-24-210-050 A. Inspection of the Fuselage NOTE : All the inspections are visual unless specified differently in the ____ procedure. The inspection areas must be clean. Operators can refer to the Non-Destructive Testing Manual (NTM) and use non destructive procedures.
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the bottom surface of | | | | | | | | | the fuselage. This includes the | | | | | | | | | cargo doors. | | | | | | | | | | | | | | | | A.| | Externally examine all the bottom | | | | | | | | | surface of the fuselage, the area | X | | | | | | | | around the door at FR17 below the | | | | | | | | | cabin floor, the skin panels | | | | | | | | | between FR17 and FR19 (bottom part | | | | | | | | | of the fuselage) | | | | | | | | | and between FR10 and FR13 and | | | | | | | | | stringers 37LH and 37RH and the NLG | | | | | | | | | doors and fairings for: | | | | | | | | | - dents, distortion, cracks, pulled or| | | | | | | | | torn fasteners and damaged | | | | | | | | | paintwork. | | | | | | | | | Internally examine all the parts that | | | | | |
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Page 606 Jan 01/06
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | you can see of the area at FR17, | | | | | | | | | without removal of parts for | | | | | | | | | - dents, distortion, cracks, pulled or| | | | | | | | | torn fasteners and damaged | | | | | | | | | paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Get access and internally | | | | | | | | | examine: | | | | | | | | | - all the frames, stringers, | | | | | | | | | clips, fittings and component | | | | | | | | | mounts at and near the location | | X | | | | | | | of the damage for: | | | | | | | | | . distortion, cracks, dents, | | | | | | | | | pulled or torn fasteners and | | | | | | | | | damaged paintwork. | | | | | | | | | - all the components, pipes, | | | | | | | | | ducts, electrical harnesses, | | | | | | | | | cables, pulleys and mechanical | | X | | | | | | | linkages for: | | | | | | | | | . distortion, cracks, dents, | | | | | | | | | rupture, breaks and fluid | | | | | | | | | leakage. | | | | | | | | | | | | | | | | B.| | Examine the APU air intake for: | X | | | | | | | | - blockage and damage. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-24-210-051 B. Inspection of the Belly Fairing and the MLG Doors (Ref. Fig. 601/TASK 05-51-24-991-001) NOTE : All the inspections are visual unless specified differently in the ____ procedure. The inspection areas must be clean. Operators can refer to the Non-Destructive Testing manual (NTM) and use non destructive procedures.
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Page 607 Jan 01/06
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Structure of the Belly Fairing Figure 601/TASK 05-51-24-991-001
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Page 608 Jul 01/04
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Belly Fairing | | | | | | | | | | | | | | | | A.| | Examine externally and internally all | | | | | | | | | the panels, the leading edge fairing, | X | | | | | | | | the upper and lower fairings for: | | | | | | | | | - distortion, cracks, dents, pulled or| | | | | | | | | torn fasteners, damaged paintwork, | | | | | | | | | honeycomb and core damage and | | | | | | | | | delamination. | | | | | | | | | | | | | | | | B.| | Examine all the components, pipes, | | | | | | | | | ducts, electrical harnesses, mounts | X | | | | | | | | and supports for: | | | | | | | | | - distortion, cracks, breaks, and | | | | | | | | | fluid leakage. | | | | | | | | | | | | | | | | C.| | Make sure that the components are | X | | | | | | | | correctly installed. | | | | | | | | | | | | | | | | D.| | Examine externally the air| | | | | | | | | conditioning pack inlets for: | X | | | | | | | | - damage and blockage. | | | | | | | | | | | | | | | |2. | | Inspection of the Main Landing Gear | | | | | | | | | Doors | | | | | | | | | | | | | | | | A.| | Examine the honeycomb structure for: | X | | | | | | | | - delamination, core damage and | | | | | | | | | cracks. | | | | | | | | | | | | | | | | B.| | Examine the door hinge actuator | | | | | | | | | attachments, the proximity sensor | X | | | | | | | | attachments, the uplock roller | | | | | | | | | attachment for: | | | | | | | | | - distortion damage and separation. | | | | | | | | | | | | | | | | C.| | Examine the door actuator and its | | | | | | | | | hydraulic hoses, pipes for: | X | | | | | | | | - fluid leakage, distortion and | | | | | | | | | damage. | | | | | | -------------------------------------------------------------------------------
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Subtask 05-51-24-210-052 C. Inspection of the Nose Landing Gear and the NLG Well (Ref. TASK 32-21-16-000-801) (Ref. TASK 05-56-00-200-801) (Ref. TASK 3221-17-000-801) (Ref. TASK 32-21-11-000-801) (Ref. TASK 32-31-22-000-801) (Ref. TASK 32-41-12-000-801) (Ref. TASK 32-21-13-000-801) (Ref. Fig. 602/TASK 05-51-24-991-002) NOTE : If the landing gear goes into soft ground, there is a risk of ____ damage to the primary structure of the landing gear. Airbus recommends that you replace the landing gear. NOTE : All the inspections are visual unless specified differently in the ____ procedure. The inspection areas must be clean. Operators can refer to the Non-Destructive Testing Manual (NTM) and use non destructive procedures. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Nose Landing Gear | | | | | | | | | | | | | | | | A.| | Examine externally the nose landing | | | | | | | | | gear and the components which are on | | | | | | | | | it, the attachment fittings and the | X | | | | | | | | bearing of the drag strut assembly | | | | | | | | | for: | | | | | | | | | - cracks, dents, scores, tears, | | | | | | | | | rupture, distortion, fluid leakage | | | | | | | | | and damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Do a measurement of the nose | | X | | | | | | | landing gear. | | | | | | | | | (Ref. TASK 05-56-00-200-801) | | | | | | | | | (2) Remove the drag strut assembly | | X | | | | | | | for inspection. | | | | | | | | | (Ref. TASK 32-21-16-000-801) | | | | | | | | | | | | | | | | B.| | Examine externally the NLG shock | | | | | | | | | absorber, the chrome-plated area for: | X | | | | | | | | - blue stains or bronze marks and | | | | | | | | | damage. | | | | | | | | | If you find damage: | | | | | |
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Location of the NLG Well Figure 602/TASK 05-51-24-991-002
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Page 611 Jul 01/04
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (1) Remove the shock absorber for | | X | | | | | | | overhaul. | | | | | | | | | (Ref. TASK 32-21-13-000-801) | | | | | | | | | | | | | | | | C.| | Examine the NLG wheels for: | | | | | | | | | - distortion, damage, valve damage, | | | | | | | | | cracks, impacts, rim damage, and | | | | | | | | | examine the tires for: | X | | | | | | | | . tread separation, cuts, ply | | | | | | | | | delamination and bulges. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the NLG wheel for overhaul | | X | | | | | | | | | | | | | |2. | | Inspection of the NLG Well | | | | | | | | | (Ref. Fig. 602/TASK 05-51-24-991-002) | | | | | | | | | | | | | | | | A.| | Examine externally the attachment | | | | | | | | | fittings of the lockstay assembly | X | | | | | | | | for: | | | | | | | | | - distortion, cracks and damaged | | | | | | | | | paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the lockstay assembly | | X | | | | | | | for inspection. | | | | | | | | | (Ref. TASK 32-21-17-000-801). | | | | | | | | | | | | | | | | B.| | Examine the attachment fittings, the | | | | | | | | | components, the internal structure, | X | | | | | | | | the manifolds, the pipes, the | | | | | | | | | electrical harnesses, the mounts for: | | | | | | | | | - distortion, rupture, impacts, fluid | | | | | | | | | leakage and pulled or torn | | | | | | | | | fasteners. | | | | | | | | | | | | | | | | C.| | Examine the attachment of the NLG | | | | | | | | | actuating cylinder for: | | | | | | | | | - distortion, cracks, dents, pulled or| X | | | | | | | | torn fasteners and damaged | | | | | | | | | paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the actuating cylinder for | | X | | | | | | | inspection. | | | | | | | | | (Ref. TASK 32-31-22-000-801) | | | | | |
EFF : ALL 05-51-24 SROS
Page 612 Jul 01/04
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | | | | | | | | D.| | Get access to the avionics compartment| | | | | | | | | and examine the NLG well roof and the | X | | | | | | | | lateral struts for: | | | | | | | | | - distortion, cracks, pulled or torn | | | | | | | | | fasteners and damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the nose landing gear for | | | | | | | | | strip-down inspection. | | X | | | | | | | (Ref. TASK 32-21-11-000-801) | | | | | | | | | (2) Examine the NLG attach fittings | | X | | | | | | | for: | | | | | | | | | - distortion , cracks pulled or | | | | | | | | | torn fasteners and damaged | | | | | | | | | paintwork. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-24-210-053 D. Inspection of the main landing gear and the MLG well (Ref. TASK 32-11-11-000-801) (Ref. TASK 32-31-46-000-801) (Ref. TASK 3241-11-000-801) (Ref. TASK 32-11-15-000-801) (Ref. TASK 32-11-13-000-801)
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NOTE : If the landing gear goes into soft ground, there is a risk of ____ damage to the primary structure of the landing gear. Airbus recommends that you replace the landing gear.
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NOTE : All the inspections are visual unless specified differently in the ____ procedure. The inspection areas must be clean. Operators can refer to the Non-Destructive Testing Manual (NTM) and use non destructive procedures.
EFF : ALL 05-51-24 SROS
Page 613 Jul 01/04
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Main Landing Gear | | | | | | | | | | | | | | | | A.| | Examine the MLG leg in the rear | | | | | | | | | pintle area for: | X | | | | | | | | - shock damage. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the MLG for inspection | | X | | | | | | | (Ref. TASK 32-11-11-000-801) | | | | | | | | | - Contact Airbus for aircraft | | | | | | | | | structural inspection requirements. | | | | | | | | | | | | | | | | B.| | Examine the MLG shock absorber for: | | | | | | | | | - cracks, scores, rupture and leaks | | | | | | | | | distortion damage. | X | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the shock absorber and | | | | | | | | | examine the components | | X | | | | | | | (Ref. TASK 32-11-13-000-801) | | | | | | | C.| | Examine the MLG retraction actuator | X | | | | | | | | and the components attached to it for:| | | | | | | | | - distortion, cracks, damage. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove and examine the actuator | | X | | | | | | | (Ref. TASK 32-31-46-000-801). | | | | | | | | | | | | | | | | D.| | Examine the bogie alignment pitch| | | | | | | | | trimmer for: | | | | | | | | | - damage, leaks, rupture, cracks, | X | | | | | | | | distortion. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the bogie alignment | | X | | | | | | | pitch-trimmer for overhaul | | | | | | | | | (Ref. TASK 32-11-15-000-801). | | | | | | | | | | | | | | | | E.| | Examine the side stay and attachment | | | | | | | | | for: | X | | | | | | | | - cracks, damage and distortion. | | | | | | | | | | | | | | | | F.| | Examine the brake rods for: | X | | | | | | | | - damage, leaks, rupture, cracks, | | | | | | | | | distortion. | | | | | | | | | | | | | | | | G.| | Examine the MLG wheels for: | | | | | |
EFF : ALL 05-51-24 SROS
Page 614 Jul 01/04
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - distortion, damage, impacts, cracks,| X | | | | | | | | valve damage, rim damage and examine| | | | | | | | | the tires for bulges, tread | | | | | | | | | separation, cuts, ply delamination. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the wheels for overhaul | | | | | | | | | (Ref. TASK 32-41-11-000-801). | | | | | | | | | | | | | | | |2. | | Inspection of the MLG well | | | | | | | | | | | | | | | | A.| | Examine the protective panels, the | X | | | | | | | | internal structure for: | | | | | | | | | - distortion, cracks, dents, rupture, | | | | | | | | | breaks, honeycomb delamination and | | | | | | | | | core damage. | | | | | | | | | Make sure that the fasteners are not| | | | | | | | | pulled or torn and that the | | | | | | | | | paintwork is not damaged. | | | | | | | | | | | | | | | | B.| | Examine the pipes, ducts, electrical | | | | | | | | | looms and their supports for: | X | | | | | | | | - fluid leakage, distortion, rupture, | | | | | | | | | cracks, correct attachment and the | | | | | | | | | condition of the safety devices. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-24-210-055 E. Inspection of the Wing (Ref. TASK 28-10-00-910-802)
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NOTE : All the inspections are visual unless specified differently in the ____ procedure. The inspection areas must be clean. Operators can refer to the Non-Destructive Testing Manual (NTM) and use non destructive procedures.
EFF : ALL 05-51-24 SROS
Page 615 Jul 01/04
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Wing | | | | | | | | | | | | | | | | A.| | Examine externally the skin panels, | X | | | | | | | | the external structure of the wing | | | | | | | | | for: | | | | | | | | | - cracks, dents, distortion, impacts, | | | | | | | | | damaged paintwork, fluid leakage. | | | | | | | | | If you find damage: | | | | | | | | | (1) Get access to the fuel tanks. | | X | | | | | | | (Ref. TASK 28-10-00-910-802) | | | | | | | | | (2) Examine the front spar and the | | | | | | | | | rear spar, the stringers, the | | X | | | | | | | ribs, the internal structure of | | | | | | | | | the wing and the fasteners for: | | | | | | | | | - cracks, dents, distortion, | | | | | | | | | damaged, torn or pulled | | | | | | | | | fasteners. | | | | | | | | | (3) Make sure that the sealant beads | | | | | | | | | are in the correct condition. | | | | | | | | | (4) Examine the ducts, lines, pipes | | X | | | | | | | mechanical linkages and their | | | | | | | | | supports for: | | | | | | | | | - distortion, cracks, fluid, | | | | | | | | | leakage. | | | | | | | | | Make sure that the components are | | | | | | | | | not damaged and are correctly | | | | | | | | | attached. | | | | | | | | | | | | | | | | B.| | Examine the flap track attachments | | | | | | | | | and the adjacent structure for: | X | | | | | | | | - distortion, cracks, pulled fasteners| | | | | | | | | fluid leakage. | | | | | | | | | | | | | | | | C.| | Examine the wing internal structure | | | | | | | | | adjacent to the front and aft | X | | | | | | | | mountings of the flap beams for: | | | | | | | | | - distortion, cracks and damage to the| | | | | | | | | sealants. | | | | | | | | | | | | | | | | D.| | Examine the area where the MLG is | | | | | | | | | attached and the adjacent structure | X | | | | | | | | for: | | | | | | | | | - cracks or fuel leakage and | | | | | |
EFF : ALL 05-51-24 SROS
Page 616 Jul 01/04
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | distortion. | | | | | | | | | | | | | | | | E.| | Examine the internal structure of the | | | | | | | | | aft spar where the MLG and MLG | X | | | | | | | | sidestay are attached for: | | | | | | | | | - distortion, damage, pulled fasteners| | | | | | | | | and damage to the sealant bead. | | | | | | ------------------------------------------------------------------------------**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-24-210-056 F. Inspection of the Nacelles and the Engines (Ref. TASK 71-00-00-000-803) (Ref. TASK 71-00-00-400-803) (Ref. TASK 7831-00-710-804) NOTE : All the inspections are visual unless specified differently in the ____ procedure. The inspections areas must be clean. Operators can refer to the Non-Destructive Testing Manual (NTM) and use non destructive procedures. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Nacelles and the | | | | | | | | | Engines | | | | | | | | | | | | | | | | A.| | Examine the nacelles: | X | | | | | | | | - the fan cowl doors | | | | | | | | | - the thrust reverser doors | | | | | | | | | - the primary nozzle | | | | | | | | | - the attachments of the nose cowl to | | | | | | | | | the fan case | | | | | | | | | - all the cowl attachment points on | | | | | | | | | the pylon | | | | | | | | | - all the cowl hinge fittings | | | | | | | | | - the components | | | | | | | | | - the supports and brackets | | | | | | | | | - the ducts and pipes | | | | | |
EFF : ALL 05-51-24 SROS
Page 617 Jan 01/07
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - the cowl latches for: | | | | | | | | | . distortion, cracks, dents, pulled | | | | | | | | | or torn fasteners, correct | | | | | | | | | attachment, fluid leakage, damage,| | | | | | | | | loose rivets, signs of shearing | | | | | | | | | and damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Do an operational test of the | | X | | | | | | | thrust reverser system to make | | | | | | | | | sure that it operates freely | | | | | | | | | (Ref. TASK 73-31-00-710-804). | | X | | | | | | | | | | | | | | B.| | Examine the engines for foreign object| X | | | | | | | | damage: | | | | | | | | | (Ref. TASK 72-00-00-200-811) | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the engine | | | X | | | | | | (Ref. TASK 71-00-00-000-803). | | | | | | | | | (2) Examine the engine-to-pylon attach| | | X | | | | | | fittings for damage. | | | | | | ------------------------------------------------------------------------------**ON A/C 701-749, Subtask 05-51-24-210-056-A F. Inspection of the Nacelles and the Engines (Ref. TASK 71-00-00-000-805) (Ref. TASK 71-00-00-400-805) (Ref. TASK 7831-00-740-802) NOTE : All the inspections are visual unless specified differently in the ____ procedure. The inspection areas must be clean. Operators can refer to the Non-Destructive Testing Manual (NTM) and use non destructive procedures.
R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-24 301-399, 401-449, 451-499, 701-749, SROS
Page 618 Jul 01/05
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Nacelles and the | | | | | | | | | Engines | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | |
A.| | | | | | | | | | | | | | | | | | | | | | |
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Examine the nacelles: | - the fan cowl doors | - the thrust reverser doors | - the primary nozzle | - the attachments of the nose cowl to | the fan case | - all the cowl attachment points on | the pylon | - all the cowl hinge fittings | - the components | - the supports and brackets | - the ducts and pipes | - the cowl latches for: | . distortion, cracks, dents, pulled | or torn fasteners, correct | attachment, fluid leakage, damage,| loose rivets, signs of shearing | and damaged paintwork. | If you find damage: | (1) Do an operational test of the | thrust reverser system to make | sure that it operates freely | (Ref. TASK 78-31-00-740-802). |
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| Examine the engines for foreign object| damage: | (Ref. TASK 72-00-00-200-803) | If you find damage: | (1) Remove the engine | (REF. TASK 71-00-00-000-805). | (2) Examine the engine-to-pylon attach| fittings for damage. |
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EFF : 701-749, 05-51-24 SROS
Page 619 Jul 01/04
**ON A/C ALL Subtask 05-51-24-210-057 G. Inspection of the Pylon R R R R R
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NOTE : All the inspections are visual unless specified differently in the ____ procedure. The inspection areas must be clean. Operators can refer to the Non-Destructive Testing Manual (NTM) and use non destructive procedures. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Pylons | | | | | | | | | | | | | | | | A.| | Examine the pylons externally for: | | | | | | | | | - distortion, cracks, pulled or torn | X | | | | | | | | fasteners, and damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Examine the pylon internally for | | | | | | | | | distortion, cracks, pulled or torn| | X | | | | | | | fasteners, damaged paintwork. | | | | | | | | | (2) Examine the components, the pipes,| | | | | | | | | the ducts, the electrical | | | | | | | | | harnesses, the mounts for: | | X | | | | | | | - distortion, cracks, rupture and | | | | | | | | | fluid leakage. | | | | | | | | | (3) Examine the pylon-to-wing | | | | | | | | | attachment for distortion and | | X | | | | | | | cracks. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-24-860-051 H. 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).
EFF : ALL 05-51-24 SROS
Page 620 Jul 01/04
(3) Pressurize the Yellow hydraulic system (Ref. TASK 29-00-00-863-803). (4) Pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-802). (5) Retract the flaps (Ref. TASK 27-50-00-866-802). (6) Retract the slats (Ref. TASK 27-80-00-866-802). (7) Retract the spoilers (Ref. TASK 27-60-00-866-802). 5. Close-up ________ R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-24-410-050 A. Close Access (1) Close the NLG doors (Ref. TASK 32-22-00-410-801). (2) Close the MLG doors (Ref. TASK 32-12-00-410-801). (3) Close the access door 811. (4) Close the fan cowl doors (Ref. TASK 71-13-00-410-802).
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(a) FOR 4030EM1 415BL, 416BR
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(b) FOR 4030EM2 425BL, 426BR (5) Close the thrust reverser doors (Ref. TASK 78-30-00-410-801).
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(b) FOR 4030EM2 427AL, 428AR (6) Close all the access doors and panels that you opened during the inspection.
EFF : ALL 05-51-24 SROS
Page 621 Jul 01/05
**ON A/C 701-749, Subtask 05-51-24-410-050-A A. Close Access (1) Close the NLG doors (Ref. TASK 32-22-00-410-801). (2) Close the MLG doors (Ref. TASK 32-12-00-410-801). (3) Close the access door 811. R
(4) Close the fan cowl doors (Ref. TASK 71-13-00-410-805). (a) FOR 4030EM1 415AL, 416AR (b) FOR 4030EM2 425AL, 426AR (5) Close the thrust reverser doors (Ref. TASK 78-30-00-410-803). (a) FOR 4030EM1 417AL, 418AR (b) FOR 4030EM2 427AL, 428AR (6) Close all the access doors and panels that you opened during the inspection. **ON A/C ALL Subtask 05-51-24-860-053 B. Put the system back to its operational configuration. (1) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801) (2) De-energize the ground service network (Ref. TASK 24-42-00-862-801) (3) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801)
EFF : ALL 05-51-24 SROS
Page 622 Jul 01/04
(4) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803) (5) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802) Subtask 05-51-24-942-050 C. Put the Aircraft back to its Initial Configuration (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. (4) Remove the safety devices that you installed on the landing gear (Ref. TASK 32-00-00-081-801). (5) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-51-24 SROS
Page 623 Oct 01/00
______________________________________________________________________________ INSPECTION AFTER FLIGHT THROUGH DUST STORM/VOLCANIC ASH OR SEVERE CONDITION ON GROUND - INSPECTION/CHECK _________________________ TASK 05-51-25-200-802 Inspection after Flight through Dust Storm or Dust contamination on Ground 1. __________________ Reason for the Job Do this inspection after flight in a severe dust storm or after dust contamination on ground. R R
NOTE : If the dust contamination occurred when the aircraft was on ground ____ with applicable protection by covers and blankets (ref. AMM 10-11-00), and if there is no dust behind the covers, the inspections specified in para. 4D.(Inspection of the probes and sensors) and in para.4F.(Inspection of the nacelles and engines) are not necessary. NOTE : This inspection specifies an adjustable access platform (2.5m to ____ 17m/8.2ft to 55.9ft) to get access to the different parts of the aircraft during the inspection. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 17M (56 FT) - ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-21-11-615-801 12-24-34-600-801 12-32-28-281-812 12-32-29-281-801 24-41-00-862-801 26-21-00-720-819
External Cleaning Draining of the Standby Static Pressure-Lines Sample Fuel for Microbiological Contamination Analysis Sampling for Analysis De-energize the Aircraft Electrical Circuits from the External Power A Functional Check of the Distribution Piping for Leakage and Obstruction
EFF : ALL 05-51-25 SROS
Page 601 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------26-22-00-200-801 27-50-00-866-801 27-50-00-866-802 27-60-00-866-801 27-60-00-866-802 27-80-00-866-801 28-12-00-210-802 29-00-00-864-801 29-00-00-864-802 29-00-00-864-803 R
29-10-00-200-803 30-11-00-710-801 30-11-51-000-802 30-11-51-400-802 32-00-00-481-801 32-12-00-010-801 32-12-00-410-801 32-16-00-010-801 32-22-00-010-801 32-22-00-410-801 34-11-00-170-801 34-11-00-170-802 34-11-00-170-803 35-12-41-100-802 49-16-00-100-801 49-16-00-200-801 49-20-00-290-809 49-20-00-290-810 49-91-44-000-801 49-91-44-400-801 53-15-11-200-801
Detailed Visual Inspection of the APU Fire-Extinguishing Distribution-Piping Extension of the Flaps on the Ground Retraction of the Flaps/Slats on the Ground Extension of the Spoilers for Maintenance Retraction of the Spoilers after Maintenance Extension of the Slats on the Ground Visual Check Of The Wing And Trim Vent Surge Tank Overpressure Protectors (5201QS1, 5201QS2, 5204QS) (Burst Discs) For Integrity 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) Check of the Clogging Indicators of High Pressure (HP), Return, Engine Driven Pump (EDP) Case drain, Reservoir Fill and Air Pressurization Unit Filters. Operational Test of the Wing Ice-Protection System Removal of the Wing Anti-ice Control Valve Filter Installation of the Wing Anti-ice Control Valve Filter Installation of the Safety Devices on the Landing Gears Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Open the CLG Doors for Maintenance Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance Flushing of the Principal Total Pressure Lines Flushing of the Principal Static Pressure Lines Draining and Flushing of the Standby Static and Standby Total Pressure Lines Cleaning of the mask full-face / Quick donning Cleaning of the Air Intake System Inspection of the Air Intake System Borescope Inspection of the Load Compressor - Access Through the LCIT-Sensor Bore Borescope Inspection of the APU Power Section Removal of the Oil Cooler (5100KT8) Installation of the Oil Cooler (5100KT8) Detailed Inspection of the Radome (110AL)
EFF : ALL 05-51-25 SROS
Page 602 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------56-11-11-200-801 56-11-12-200-801 56-12-11-200-801 56-21-15-200-801 71-00-00-200-802 71-00-00-200-813 71-13-00-200-803 71-13-00-220-801 R
71-61-00-220-801 71-61-41-200-802 78-30-00-210-802 78-32-00-200-802 AMM 122227 PB 301 AMM 122232 PB 301
Inspection of the Windshields (3DG1,3DG2). Inspection of the Fixed Windows (7DG1,7DG2) Inspection of the Sliding Windows (8DG1,8DG2). Detailed Visual Inspection of Passenger Cabin Window Panes including Passenger/ Crew Door and Emergency Exit Window Panes Inspection Procedures After the Ingestion of Volcanic Ash or Sand Examine the Power Plant after Contamination with Volcanic Ash Inspection of the Fan Cowl Doors Visual Inspection of Forward and Aft fan Cowls (5130EA) ,(5140EA), (5150EA), (5110EA) and (5120EA). Detailed Inspection of Intake Cowl Lip and Inner Skin Visual Check of the Airwashed Surfaces for Distortion and Security of Installation Visual Inspection of the Thrust Reverser (4120KS to 4130KS) (Thrust Reverser Closed) Inspection of the Thrust Reverser Structure (for corrective action) (for corrective action)
3. __________ Job Set-up Subtask 05-51-25-210-076 A. General (1) Inspection requirements (a) The dust particles can be of different sizes, they can enter all orifices and cause erosion, etching or shot peening on the surface. The dust can stay: - on all exposed lubricated surfaces - in all corners - in bottom places The dust can cause contamination on all filter elements. (b) All the necessary inspections are visual unless the text gives other instructions. Operators can refer to the Non-destructive Testing Manual (NTM) and use non-destructive procedures.
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(c) If you find damage to the aircraft structure, refer to the Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures. (d) If you find damage to paint/protection, refer to the Structural Repair Manual (SRM). The SRM has the approved paint/protection repair procedures. (e) Examine the aircraft surfaces, structures, systems for contamination, erosion/abrasion, dents, etching, delamination or other damage. Subtask 05-51-25-210-078 B. Inspection Preparation
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(1) If contamination occurred in flight or during landing or take off: (a) Before you start, we recommend that you get information from the crew about the flight conditions. (b) Make sure that you have the related aircraft Post Flight Report (PFR). (c) Do a check of all the events reported by the crew or by the PFR in addition/conjunction with this inspection. (2) If contamination occurred with the aircraft in parking configuration, it is not necessary to do a check of the systems which are protected by the applicable protective covers/devices if you do not find dust behind them. Subtask 05-51-25-481-052 C. Safety Precautions (1) Make sure that the safety devices are installed on the landing gears (Ref. TASK 32-00-00-481-801). Subtask 05-51-25-866-056 D. Extension of the Flight Control Surfaces (1) Extend the flaps (Ref. TASK 27-50-00-866-801). (2) Extend the slats (Ref. TASK 27-80-00-866-801).
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(3) Extend the spoilers (Ref. TASK 27-60-00-866-801). Subtask 05-51-25-010-052 E. Get Access (1) Open the main gear doors and install the safety devices (Ref. TASK 32-12-00-010-801). (2) Open the nose gear doors and install the safety devices (Ref. TASK 32-22-00-010-801). (3) Open the center gear doors and install the safety devices (Ref. TASK 32-16-00-010-801). Subtask 05-51-25-860-052 F. Aircraft Maintenance Configuration (1) Make sure that the hydraulic systems are depressurized (2) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (3) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803). (4) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802). (5) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). (6) Put warning notices in the cockpit to tell persons not to operate the systems. (7) Put an ACCESS PLATFORM 17M (56 FT) - ADJUSTABLEin position near the area you must inspect.
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4. Procedure _________ Subtask 05-51-25-160-052 A. Cleaning of the Aircraft CAUTION : DO NOT RUB THE SURFACE WHEN YOU REMOVE THE DUST FROM THE _______ AIRCRAFT. IF YOU RUB THE SURFACE, YOU CAN CAUSE EROSION/ ABRASION. CAUTION : DO NOT USE FLUIDS TO REMOVE THE DUST. IF THERE IS A LAYER OF _______ DUST ON THE AIRCRAFT SURFACES, REMOVE THE DUST WITH A VACUUM CLEANER (OR, IF YOU CANNOT USE A VACUUM CLEANER, USE AN AIR BLOWER, A SOFT CLOTH OR A HAND BRUSH). FLUIDS CAN MIX WITH THE DUST AND MAKE A PASTE THAT CAN CAUSE EROSION/ABRASION. THIS PASTE CAN GO INTO AREAS THAT ARE NOT EASY TO CLEAN. (1) If there is a layer of dust on the aircraft surfaces, remove the dust with a vacuum cleaner, an air blower, a soft cloth or a soft brush. (2) Clean the aircraft internally. (3) Clean the aircraft externally (Ref. TASK 12-21-11-615-801). Subtask 05-51-25-210-079 R
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B. Internal Inspection (Ref. TASK 35-12-41-100-802) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the cabin area | | | | | | | | | | | | | | | | A.| |Examine the cabin area for dust | X | | | | | | | |contamination. | | | | | | | | |If you find contamination: | | | | | | | | |(1) Clean all the contaminated surfaces| | X | | | | | | | | | | | | | | B.| |Examine the cockpit for dust | X | | | | | | | |contamination. | | | | | | | | |If you find contamination: | | | | | | | | |(1) Clean all the contaminated surfaces| | X | | | | | | |(2) Examine the oxygen full face masks | | X | | | | | | | for contamination. | | | | | | | | | If you find contamination: | | | | | | | | | (a) Clean the oxygen full face | | | X | | |
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | masks | | | | | | | | | (Ref. TASK 35-12-41-100-802). | | | | | | | C.| |Examine the avionics compartment (all | X | | | | | | | |the items you can see), specially: | | | | | | | | |- around the ventilated components | | | | | | | | |- the plugs | | | | | | | | |- the equipments | | | | | | | | |for dust contamination. | | | | | | | | |If you find contamination: | | | | | | | | |(1) Clean all the contaminated surfaces| | X | | | | | | | | | | | | | | D.| |Examine the cargo compartments for dust| X | | | | | | | |contamination. | | | | | | | | |If you find contamination: | | | | | | | | |(1) Clean all the contaminated surfaces| | X | | | | | | | (specially the PDU sensors). | | | | | | | | |(2) Examine the cargo drainage system | | X | | | | | | | (if installed) for dust | | | | | | | | | contamination. | | | | | | | | | If you find contamination: | | | | | | | | | (a) Replace the filters of the | | | X | | | | | | drain funnels. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-25-210-080 C. Inspection (Ref. TASK (Ref. TASK (Ref. TASK
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of the Fuselage, the Wings and the Stabilizers 53-15-11-200-801) (Ref. TASK 56-11-11-200-801) 56-11-12-200-801) (Ref. TASK 56-12-11-200-801) 56-21-15-200-801) (Ref. AMM 122227 PB 301)
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the fuselage | | | | | | | | | | | | | | | | A.| | Examine the radome skin for damage | X | | | | | | | | (Ref. TASK 53-15-11-200-801). | | | | | | | | | | | | | | | | B.| | Examine the windshield, the fixed | X | | | | | | | | windows and the sliding windows for | | | | | | | | | damage: | | | | | |
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - for the windshield | | | | | | | | | (Ref. TASK 56-11-11-200-801) | | | | | | | | | - for the fixed windows | | | | | | | | | (Ref. TASK 56-11-12-200-801) | | | | | | | | | - for the sliding windows | | | | | | | | | (Ref. TASK 56-12-11-200-801). | | | | | | | | | | | | | | | | C.| | Examine the passenger cabin windows, | X | | | | | | | | the passenger/crew doors and the | | | | | | | | | emergency exit windows for damage | | | | | | | | | (Ref. TASK 56-21-15-200-801). | | | | | | | | | | | | | | | | D.| | Examine all of the fuselage skin, the | X | | | | | | | | belly fairing and the wing-to-fuselage| | | | | | | | | fairings for damage. | | | | | | | | | | | | | | | | E.| | Examine the ram air inlet and outlet, | X | | | | | | | | the air inlet and outlet flaps for | | | | | | | | | damage. | | | | | | | | | | | | | | | |2. | | Inspection of the Wings | | | | | | | | | | | | | | | | A.| | Examine all the static dischargers for| X | | | | | | | | damage. | | | | | | | | | | | | | | | | B.| | Examine the top and bottom skin of the| X | | | | | | | | wings for damage. | | | | | | | | | | | | | | | | C.| | Examine the flap track fairings for | X | | | | | | | | damage. | | | | | | | | | | | | | | | | D.| | Examine the skin of all the control | X | | | | | | | | surfaces ( slats, flaps, ailerons and | | | | | | | | | spoilers), specially the leading and | | | | | | | | | the trailing edges, for damage. | | | | | | | | | | | | |
| E.| | | | F.| |
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Examine the hinge areas of the spoilers and the ailerons for contamination. Examine the flap tracks, flap inter connecting strut, track 4 sensor,
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | roller mechanisms, steady bearings and| | | | | | | | | universal joints for contamination. | | | | | | | | | Make sure that there is no dust | | | | | | | | | deposit on the roller stops. | | | | | | | | | If you find contamination: | | | | | | | | | (1) Clean and lubricate the related | | X | | | | | | | components | | | | | | | | | (Ref. AMM 12-22-27 PB 301). | | | | | | | | | | | | | | | | G.| | Examine the piston rod of each | X | | | | | | | | servocontrol of the ailerons and the | | | | | | | | | spoilers for contamination. | | | | | | | | | If you find contamination: | | | | | | | | | (1) Clean the piston rod of the | | X | | | | | | | servocontrols. | | | | | | | | | | | | | | | |3. | | Inspection of the Vertical Stabilizer | | | | | | | | | | | | | | | | A.| | Examine all the static dischargers for| X | | | | | | | | damage. | | | | | | | | | | | | | | | | B.| | Examine the skin of the vertical | X | | | | | | | | stabilizer and the rudder, specially | | | | | | | | | the leading and the trailing edges, | | | | | | | | | for damage. | | | | | | | | | | | | | | | | C.| | Examine the hinge areas of the rudder | X | | | | | | | | for contamination. | | | | | | | | | | | | | | | | D.| | Examine the piston rod of each | X | | | | | | | | servocontrol of the rudder for | | | | | | | | | contamination. | | | | | | | | | If you find contamination: | | | | | | | | | (1) Clean the piston rod of the | | X | | | | | | | servocontrols. | | | | | | | | | | | | | | | |4. | | Inspection of the Horizontal | | | | | | | | | Stabilizers | | | | | | | | | | | | | | | | A.| | Examine all the static dischargers for| X | | | | | | | | damage. | | | | | | | | | | | | | | | | B.| | Examine the skin of the horizontal | X | | | | |
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | stabilizers and the elevators, | | | | | | | | | specially the leading and the trailing| | | | | | | | | edges, for damage. | | | | | | | | | | | | | | | | C.| | Examine the hinge areas of the | X | | | | | | | | elevators for contamination. | | | | | | | | | | | | | | | | D.| | Examine the piston rod of each | X | | | | | | | | servocontrol of the elevators for | | | | | | | | | contamination. | | | | | | | | | If you find contamination: | | | | | | | | | (1) Clean the piston rod of the | | X | | | | | | | servocontrols. | | | | | | | | | | | | | | | |5. | | Inspection of the external lights | | | | | | | | | | | | | | | | A.| | Examine all the external lights for | X | | | | | | | | damage. | | | | | | | | | If you find damage: | | | | | | | | | (1) Replace the related component(s). | | X | | | | | | | | | | | | | |6. | | Inspection of the antennas and the | | | | | | | | | drain masts | | | | | | | | | | | | | | | | A.| | Examine all the antennas and the drain| X | | | | | | | | masts for damage. | | | | | | | | | If you find damage: | | | | | | | | | (1) Replace the related component(s). | | X | | | | ------------------------------------------------------------------------------Subtask 05-51-25-210-081 D. Inspection of the Probes and Sensors NOTE : If the aircraft was on the ground with the applicable protective ____ covers/devices installed (ref. AMM 10-11-00) when the dust contamination occurred, this inspection is not necessary if there is no dust behind the covers.
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NOTE : If the crew report shows an important dust storm. ____ If the maintenance crew reports an important dust storm with probe covers in position. If a general inspection shows evidence of an heavy contamination:
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- you must flush of all the pressure lines. (Ref. TASK 12-24-34-600-801) (Ref. TASK 34-11-00-170-801) (Ref. TASK 34-11-00-170-802) (Ref. TASK 34-11-00-170-803)
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the sensors and probes | | | | | | | | | | | | | | | | A.| | Inspect all the probes and sensors. | X | | | | | | | | | | | | | | | | |(1) Examine all the probes and sensors | | | | | | | | | for damage and contamination (not | | | | | | | | | clogged): | | | | | | | | | - the pitot probes | | | | | | | | | - the static probes | | | | | | | | | - the TAT sensors | | | | | | | | | - the AOA sensors | | | | | | | | | - the ice detector probes | | | | | | | | | (if installed). | | | | | | | | |NOTE: Make sure that the AOA sensors | | | | | | | | | move freely and that the drain | | | | | | | | | holes of the pitot probes are not| | | | | | | | | clogged. | | | | | | | | | | | | | | | | | |(2) Drain the standby static pressure | X | | | | | | | | lines and make sure that there | | | | | | | | | are no signs of dust | | | | | | | | | (Ref. TASK 12-24-34-600-801). | | | | | | | | | If you find contamination: | | | | | | | | | (a) Flush all the pressure lines | | | X | | | | | | (Ref. TASK 34-11-00-170-801) | | | | | | | | | (Ref. TASK 34-11-00-170-802) | | | | | | | | | (Ref. TASK 34-11-00-170-803). | | | | | | -------------------------------------------------------------------------------
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Subtask 05-51-25-210-082 E. Inspection of the Landing Gear Doors, the Landing Gears and the Landing Gear Wells (Ref. AMM 122232 PB 301)
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the landing gear doors, | | | | | | | | |the landing gears and the landing gear | | | | | | | | |wells. | | | | | | | | |NOTE: If you find contamination, you | X | | | | | | | | must: | | | | | | | | | (a) Remove the contamination from | | X | | | | | | | surface, the moving joints | | | | | | | | | and the chromed areas of | | | | | | | | | shock absorbers and actuators | | | | | | | | | before the next flight. | | | | | | | | | (b) Do a full lubrication of | | | X | | | | | | the landing gears before a | | | | | | | | | maximum of 10 flight cycles | | | | | | | | | (Ref. AMM 12-22-32, PB 301). | | | | | | | | | | | | | | | | A.| |Inspection of the doors | | | | | | | | |(1) Examine all the doors for damage | X | | | | | | | | and/or contamination, specially on:| | | | | | | | | - the door skin | | | | | | | | | - the door hinges | | | | | | | | | - the proximity sensors | | | | | | | | | - the actuators bare rods. | | | | | | | | | | | | | | | | B.| |Inspection of the landing gears | | | | | | | | |(1) Examine all the landing gear | X | | | | | | | | structures and the components | | | | | | | | | installed on them for damage and/or| | | | | | | | | contamination, specially on: | | | | | | | | | - the attachment points of the | | | | | | | | | landing gears | | | | | | | | | - the proximity sensors | | | | | | | | | - the actuator rods | | | | | | | | | - the chromed area of the shock | | | | | | | | | absorbers | | | | | | | | | - the mechanical linkages and the | | | | | | | | | moving joints. | | | | | | | | | | | | | | | | C.| |Inspection of the landing gear wells. | | | | | |
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | |(1) Examine all the landing gear wells | X | | | | | | | | and the components installed in | | | | | | | | | them for damage and/or | | | | | | | | | contamination. | | | | | | ------------------------------------------------------------------------------R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-25-210-083 F. Inspection of the Nacelles and the Engines NOTE : If the aircraft was on the ground with the applicable protective ____ covers/devices installed (Ref. AMM 10-11-00) when the dust contamination occurred, this inspection is not necessary if there is no dust behind the covers. NOTE : If the aircraft was on the ground without the applicable ____ protective covers/devices installed, we recommend that after you start the engines, you let the engines run a few minutes before you use the bleed air systems. This is to make sure that the engines blow out remaining particles. (Ref. TASK 71-61-00-220-801) (Ref. TASK 71-13-00-220-801) (Ref. TASK 78-30-00-210-802) (Ref. TASK 26-21-00-720-819) (Ref. TASK 71-00-00-200-802) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the nacelles and engines | | | | | | | | | | | | | | | | A.| |Inspection of the nacelles | | | | | | | | |(1) Examine the air intake cowl for | X | | | | | | | | damage | | | | | | | | | (Ref. TASK 71-61-00-220-801). | | | | | | | | |(2) Examine the fan cowl doors for | X | | | | | | | | damage | | | | | | | | | (Ref. TASK 71-13-00-220-801). | | | | | | | | |(3) Examine the thrust reversers for | X | | | | | | | | damage | | | | | |
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (Ref. TASK 78-30-00-210-802). | | | | | | | | | | | | | | | | B.| |Inspection of the engines | | | | | | | | |(1) Examine the fire extinguisher | X | | | | | | | | outlets for contamination. | | | | | | | | | If you find contamination: | | | | | | | | | (a) Do a check of the | | X | | | | | | | distribution piping for | | | | | | | | | obstruction | | | | | | | | | (Ref. TASK 26-21-00-720-819). | | | | | | | | |(2) Do the inspection of the engines | X | | | | | | | | after dust ingestion | | | | | | | | | (Ref. TASK 71-00-00-200-802). | | | | | | ------------------------------------------------------------------------------**ON A/C 701-749, Subtask 05-51-25-210-083-A F. Inspection of the Nacelles and the Engines NOTE : If the aircraft was on the ground with the applicable protective ____ covers/devices installed (Ref. AMM 10-11-00) when the dust contamination occurred, this inspection is not necessary if there is no dust behind the covers. NOTE : If the aircraft was on the ground without the applicable ____ protective covers/devices installed, we recommend that after you start the engines, you let the engines run a few minutes before you start the bleed air systems. This is to make sure that the engines blow out remaining particles. (Ref. TASK 71-61-41-200-802) (Ref. TASK 71-13-00-200-803) (Ref. TASK 78-32-00-200-802) (Ref. TASK 26-21-00-720-819) (Ref. TASK 71-00-00-200-813)
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the nacelles and engines | | | | | | | | | | | | | | | | A.| |Inspection of the nacelles | | | | | | | | |(1) Examine the air intake cowl for | X | | | | | | | | damage | | | | | | | | | (Ref. TASK 71-61-41-200-802). | | | | | | | | |(2) Examine the fan cowl doors for | X | | | | | | | | damage | | | | | | | | | (Ref. TASK 71-13-00-200-803). | | | | | | | | |(3) Examine the thrust reversers for | X | | | | | | | | damage | | | | | | | | | (Ref. TASK 78-32-00-200-802). | | | | | | | | | | | | | | | | B.| |Inspection of the engines | | | | | | | | |(1) Examine the fire extinguisher | X | | | | | | | | outlets for contamination. | | | | | | | | | If you find contamination: | | | | | | | | | (a) Do a check of the | | X | | | | | | | distribution piping for | | | | | | | | | obstruction | | | | | | | | | (Ref. TASK 26-21-00-720-819). | | | | | | | | |(2) Do inspection/check of the engine | X | | | | | | | | after dust ingestion | | | | | | | | | (Ref. TASK 71-00-00-200-813). | | | | | | ------------------------------------------------------------------------------**ON A/C ALL Subtask 05-51-25-210-084
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G. Inspection (Ref. TASK (Ref. TASK (Ref. TASK (Ref. TASK
of the APU 49-16-00-200-801) (Ref. TASK 49-16-00-100-801). 49-91-44-000-801) (Ref. TASK 49-91-44-400-801) 49-20-00-290-809) (Ref. TASK 49-20-00-290-810) 26-22-00-200-801)
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Page 615 Jul 01/06
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the APU | | | | | | | | | | | | | | | | A.| |Examine the APU intake and exhaust for | X | | | | | | | |contamination and/or damage | | | | | | | | |(Ref. TASK 49-16-00-200-801). | | | | | | | | |If you find contamination: | | | | | | | | |(1) If the APU was not in operation | | | | | | | | | during the dust contamination: | | | | | | | | | (a) Clean the APU air intake and | | X | | | | | | | exhaust | | | | | | | | | (Ref. TASK 49-16-00-100-801). | | | | | | | | |(2) If the APU was in operation during | | | | | | | | | the dust contamination: | | | | | | | | | (a) Clean the APU air intake and | | X | | | | | | | exhaust | | | | | | | | | (Ref. TASK 49-16-00-100-801). | | | | | | | | | (b) Examine the oil cooler for | | X | | | | | | | contamination | | | | | | | | | (Ref. TASK 49-91-44-000-801) | | | | | | | | | (Ref. TASK 49-91-44-400-801). | | | | | | | | | If you find contamination: | | | | | | | | | - do an APU inspection/check | | | X | | | | | | (Ref. TASK 49-20-00-290-809) | | | | | | | | | (Ref. TASK 49-20-00-290-810).| | | | | | | | | NOTE: We recommend that you | | | | | | | | | replace the APU if you | | | | | | | | | find large contamination | | | | | | | | | in the oil cooler. | | | | | | | | | (c) Examine the fire extinguisher | | X | | | | | | | outlets for contamination | | | | | | | | | (Ref. TASK 26-22-00-200-801). | | | | | | -------------------------------------------------------------------------------
EFF : ALL 05-51-25 SROS
Page 616 Jul 01/06
Subtask 05-51-25-210-085 H. Inspection of the Hydraulic System (Ref. TASK 29-10-00-200-803) (Ref. TASK 12-32-29-281-801)
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the hydraulic system | | | | | | | | | | | | | | | | A.| |Examine the filters for contamination | X | | | | | | | |(clogging indicators and filter | | | | | | | | |elements) | | | | | | | | |(Ref. TASK 29-10-00-200-803). | | | | | | | | |If you find contamination: | | | | | | | | |(1) replace the filter elements. | | X | | | | | | |(2) get a sample of fluid and make | | X | | | | | | | sure that the contamination is in | | | | | | | | | the permitted limits | | | | | | | | | (Ref. TASK 12-32-29-281-801). | | | | | | | | | | | | | | | | B.| |Examine the RAT for contamination | X | | | | | | | |and/or damage. | | | | | | | | | | | | | | | | C.| |Examine the sliding unions for | X | | | | | | | |contamination. | | | | | | | | |If you find contamination: | | | | | | | | |(1) Clean the sliding unions. | | X | | | | -------------------------------------------------------------------------------
EFF : ALL 05-51-25 SROS
Page 617 Jan 01/03
Subtask 05-51-25-210-086 R
J. Inspection of the Fuel System (Ref. TASK 28-12-00-210-802) (Ref. TASK 12-32-28-281-812) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the fuel system | | | | | | | | | | | | | | | | A.| | Examine the NACA vent intakes for | X | | | | | | | | contamination | | | | | |
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| | | (Ref. TASK 28-12-00-210-802). | | | | | | | | | If you find contamination: | | | | | | | | | (1) Get a sample of fuel from the | | X | | | | | | | water drain valves and do a check | | | | | | | | | for particle contamination | | | | | | | | | (Ref. TASK 12-32-28-281-812). | | | | | | | | | If you find contamination: | | | | | | | | | (a) Clean the fuel tanks. | | X | | | | | | | | | | | | | ------------------------------------------------------------------------------Subtask 05-51-25-210-087 K. Inspection of the Anti-Ice System (Ref. TASK 30-11-00-710-801) (Ref. TASK 30-11-51-000-802) (Ref. TASK 3011-51-400-802) NOTE : If the anti-ice system was selected OFF in flight, this inspection ____ is not necessary. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the anti-ice system | | | | | | | | | | | | | | | | A.| | Do an operational test of the wing | X | | | | | | | | anti-ice system: | | | | | | | | | (ref. TASK 30-11-00-710-801). | | | | | | | | | If the valve response time is | | | | | | | | | incorrect: | | | | | | | | | (1) Clean the valve and replace the | | X | | | | | | | valve filter | | | | | |
EFF : ALL 05-51-25 SROS
Page 618 Jan 01/06
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (Ref. TASK 30-11-51-000-802) | | | | | | | | | (Ref. TASK 30-11-51-400-802). | | | | | | ------------------------------------------------------------------------------5. Close-up ________ Subtask 05-51-25-866-054 A. Retraction of the Flight Control Surfaces (1) Retract the flaps and the slats (Ref. TASK 27-50-00-866-802). (2) Retract the spoilers (Ref. TASK 27-60-00-866-802). Subtask 05-51-25-410-052 B. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the NLG doors (Ref. TASK 32-22-00-410-801). (3) Close the MLG doors (Ref. TASK 32-12-00-410-801). (4) Close all the access doors, and the access panels opened during the inspection procedure. Subtask 05-51-25-860-053 C. Put the Aircraft back to its Initial Configuration (1) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862801). (2) Remove the access platform(s). (3) Remove the warning notice(s).
EFF : ALL 05-51-25 R SROS
Page 619 Jan 01/06
TASK 05-51-25-200-803 Inspection after Flight through Volcanic Ash or Volcanic Ash contamination on Ground 1. __________________ Reason for the Job Do this inspection after flight in volcanic ash or after volcanic ash contamination on ground. R R R R
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NOTE : If the volcanic ash contamination occurred when the aircraft was on ____ ground with applicable protection by covers and blankets (Ref. AMM 10-11-00), and if there is no ash behind the covers, this inspections specified in para. 4.D. (Inspection of the probes and sensors) and in para. 4.F. (Inspection of the nacelles and engines ) are not necessary. NOTE : This inspection specifies an adjustable access platform (2,5m to ____ 17m/8ft.2in/to55ft.9in) to get access to the different parts of the aircraft during this inspection. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
1 ACCESS PLATFORM 17M (56 FT) - ADJUSTABLE
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-15-38-613-801 12-21-11-615-801 12-24-34-600-801 12-24-38-680-801 12-32-28-281-812 12-32-29-281-801 21-51-51-000-801
Fill the Potable Water System (Aircraft Electrical Power Available) External Cleaning Draining of the Standby Static Pressure-Lines Draining of the Potable Water System (with Electrical Power) Sample Fuel for Microbiological Contamination Analysis Sampling for Analysis Removal of the Pack Flow Control-Valve (511HB,512HB)
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Page 620 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------21-51-51-400-801 21-63-52-000-801 21-63-52-400-801 24-41-00-862-801 26-21-00-720-819 26-22-00-200-801 27-50-00-866-801 27-50-00-866-802 27-60-00-866-801 27-60-00-866-802 27-80-00-866-801 27-84-61-000-801 27-84-61-400-801 27-84-62-000-801 27-84-62-400-801 28-12-00-210-802 28-14-00-210-801 29-00-00-864-801 29-00-00-864-802 29-00-00-864-803 R
29-10-00-200-803 30-11-51-000-802 30-11-51-400-802 30-21-51-000-801 30-21-51-400-801 32-00-00-481-801
Installation of the Pack Flow Control-Valve (511HB,512HB) Removal of the Trim-Air Pressure-Regulating Valve (638HK, 639HK) Installation of the Trim-Air Pressure-Regulating Valve (638HK, 639HK) De-energize the Aircraft Electrical Circuits from the External Power A Functional Check of the Distribution Piping for Leakage and Obstruction Detailed Visual Inspection of the APU Fire-Extinguishing Distribution-Piping Extension of the Flaps on the Ground Retraction of the Flaps/Slats on the Ground Extension of the Spoilers for Maintenance Retraction of the Spoilers after Maintenance Extension of the Slats on the Ground Removal of the Slat 1 Installation of the Slat 1 Removal of the Slat 2, 3, 4, 5, 6, 7 Installation of the Slat 2, 3, 4, 5, 6, 7 Visual Check Of The Wing And Trim Vent Surge Tank Overpressure Protectors (5201QS1, 5201QS2, 5204QS) (Burst Discs) For Integrity Visual Check of Drain Mast Outlet for Blockage 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) Check of the Clogging Indicators of High Pressure (HP), Return, Engine Driven Pump (EDP) Case drain, Reservoir Fill and Air Pressurization Unit Filters. Removal of the Wing Anti-ice Control Valve Filter Installation of the Wing Anti-ice Control Valve Filter Removal of the Engine-Air-Intake Anti Ice Valve (4000DN) Installation of the Engine-Air-Intake Anti Ice Valve (4000DN) Installation of the Safety Devices on the Landing Gears
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Page 621 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------32-12-00-010-801 32-12-00-410-801 32-16-00-010-801 32-22-00-010-801 32-22-00-410-801 34-11-00-170-801 34-11-00-170-802 34-11-00-170-803 35-12-41-100-802 36-11-51-000-801 36-11-51-400-801 36-11-52-000-801 36-11-52-400-801 36-12-52-000-801 36-12-52-400-801 49-16-00-100-801 49-16-00-200-801 49-20-00-290-809 49-20-00-290-810 49-91-44-000-801 49-91-44-400-801 53-15-11-200-801 56-11-11-200-801 56-11-12-200-801 56-12-11-200-801 56-21-15-200-801 71-00-00-200-802 71-00-00-200-813 71-13-00-200-803 71-13-00-220-801 R
71-61-00-220-801 71-61-41-200-802 78-30-00-210-802 78-32-00-200-802
Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Open the CLG Doors for Maintenance Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance Flushing of the Principal Total Pressure Lines Flushing of the Principal Static Pressure Lines Draining and Flushing of the Standby Static and Standby Total Pressure Lines Cleaning of the mask full-face / Quick donning Removal of the HP Bleed Valve (4000HA) Installation of the HP Bleed Valve (4000HA) Removal of the Bleed Valve (4001HA) Installation of the Bleed Valve (4001HA) Removal of the Crossbleed Valve (6HV) Installation of the Crossbleed Valve (6HV) Cleaning of the Air Intake System Inspection of the Air Intake System Borescope Inspection of the Load Compressor - Access Through the LCIT-Sensor Bore Borescope Inspection of the APU Power Section Removal of the Oil Cooler (5100KT8) Installation of the Oil Cooler (5100KT8) Detailed Inspection of the Radome (110AL) Inspection of the Windshields (3DG1,3DG2). Inspection of the Fixed Windows (7DG1,7DG2) Inspection of the Sliding Windows (8DG1,8DG2). Detailed Visual Inspection of Passenger Cabin Window Panes including Passenger/ Crew Door and Emergency Exit Window Panes Inspection Procedures After the Ingestion of Volcanic Ash or Sand Examine the Power Plant after Contamination with Volcanic Ash Inspection of the Fan Cowl Doors Visual Inspection of Forward and Aft fan Cowls (5130EA) ,(5140EA), (5150EA), (5110EA) and (5120EA). Detailed Inspection of Intake Cowl Lip and Inner Skin Visual Check of the Airwashed Surfaces for Distortion and Security of Installation Visual Inspection of the Thrust Reverser (4120KS to 4130KS) (Thrust Reverser Closed) Inspection of the Thrust Reverser Structure
EFF : ALL 05-51-25 SROS
Page 622 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------AMM AMM
122227 PB 301 122232 PB 301
(for corrective action) (for corrective action)
3. __________ Job Set-up Subtask 05-51-25-210-077 A. General WARNING : DO NOT BREATHE VOLCANIC ASH. DO NOT GET VOLCANIC ASH IN YOUR _______ EYES. PUT ON PROTECTIVE CLOTHES, EYE GOGGLES AND A RESPIRATOR MASK. MAKE SURE THAT THE RESPIRATOR MASK CAN REMOVE VOLCANIC ASH FROM THE AIR. VOLCANIC ASH CAN CAUSE EYE IRRITATION AND INJURY TO THE RESPIRATORY SYSTEM. (1) Volcanic ash (a) Volcanic ash is hard, very abrasive and acid (pH between 2 and neutral). It can cause erosion/abrasion, etching or shot-peening on the surfaces and can remove the finishes/protection and thus cause damage/corrosion. (b) The ash particles can be of different sizes but the texture of volcanic ash is almost the same as talcum powder and can enter all orifices and go through many seals. Volcanic ash will stay: - on bare and lubricated surfaces. - in all corners. - in bottom places. It can cause unusual wear and contamination of many aircraft systems and filter elements. (c) The volcanic ash will melt when it goes through the chamber of the engines. The melted ash has very high adhesive qualities and engine parts and thus decreases engine performance. obstruct the fuel injectors and can cause an engine
combustion bonds to It may shutdown.
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Page 623 Jan 01/07
(2) Inspection requirements (a) Volcanic ash can cause severe damage/contamination on the structure/systems of the aircraft. It is not possible to estimate the quantity and the type of damage after volcanic ash contamination. Therefore, it is necessary to do a full inspection of the aircraft to know the damage and make a decision about the necessary repair/action. (b) All the necessary inspections are visual unless the text gives other instructions. Operators can refer to the Non-destructive Testing Manual (NTM) and use non-destructive procedures. (c) If you find damage to the aircraft structure, refer to the Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures. (d) If you find damage to paint/protection, refer to the Structural Repair Manual (SRM). The SRM has the approved paint/protection repair procedures. (e) Examine the aircraft surfaces, structures, systems for contamination, erosion/abrasion, dents, etching, delamination or other damage. Subtask 05-51-25-210-088 B. Inspection Preparation R
(1) If contamination occurred in flight or during landing or take off: (a) Before you start, we recommend that you get information from the crew about the flight conditions. (b) Make sure that you have the related aircraft Post Flight Report (PFR). (c) Do a check of all the events reported by the crew or by the PFR in addition/conjunction with this inspection. (2) If contamination occurred with the aircraft in the parking configuration, it is not necessary to do a check of the systems which are protected by the applicable protective covers/devices if you do not find ash behind them.
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Page 624 Jan 01/07
Subtask 05-51-25-481-053 C. Safety Precautions (1) Install the safety devices on the landing gears (Ref. TASK 32-00-00481-801). Subtask 05-51-25-866-057 D. Extension of the Flight Control Surfaces (1) Extend the flaps (Ref. TASK 27-50-00-866-801). (2) Extend the slats (Ref. TASK 27-80-00-866-801). (3) Extend the spoilers (Ref. TASK 27-60-00-866-801). Subtask 05-51-25-010-053 E. Get Access R
(1) Open the main gear doors and install the safety devices (Ref. TASK 32-12-00-010-801). (2) Open the nose gear doors and install the devices (Ref. TASK 32-22-00010-801). (3) Open the center gear doors and install the safety devices (Ref. TASK 32-16-00-010-801). Subtask 05-51-25-860-054 F. Aircraft Maintenance Configuration (1) Make sure that the hydraulic systems are depressurized (2) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (3) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803). (4) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802). (5) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
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Page 625 Jan 01/07
(6) Put warning notices in the cockpit to tell persons not to operate the systems. R R
(7) Put an ACCESS PLATFORM 17M (56 FT) - ADJUSTABLE in position near the area you must inspect. 4. Procedure _________ Subtask 05-51-25-160-053 A. Cleaning of the Aircraft CAUTION : DO NOT RUB THE SURFACE WHEN YOU REMOVE THE ASH FROM THE _______ AIRCRAFT. IF YOU RUB THE SURFACE, YOU CAN CAUSE EROSION/ ABRASION. CAUTION : DO NOT USE FLUIDS TO REMOVE THE ASH. IF THERE IS A LAYER OF ASH _______ ON THE AIRCRAFT SURFACES, REMOVE THE ASH WITH A VACUUM CLEANER (OR, IF YOU CANNOT USE A VACUUM CLEANER, USE AN AIR BLOWER, A SOFT CLOTH OR A HAND BRUSH). FLUIDS CAN MIX WITH THE ASH AND MAKE A PASTE THAT CAN CAUSE EROSION/ABRASION. THIS PASTE CAN GO INTO AREAS THAT ARE NOT EASY TO CLEAN. (1) If there is a layer of volcanic ash on the aircraft surfaces, remove the volcanic ash with a vacuum cleaner, an air blower, a soft cloth or a soft brush. (2) Clean the aircraft internally. (3) Clean the aircraft externally (Ref. TASK 12-21-11-615-801). Subtask 05-51-25-210-089
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B. Internal Inspection (Ref. TASK 35-12-41-100-802) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the cabin area | | | | | | | | | | | | | | | | A.| |Examine the cabin area for ash | X | | | | | | | |contamination. | | | | | | | | |If you find contamination: | | | | | | | | |(1) Clean all the contaminated surfaces| | X | | | | | | | | | | | | | | B.| |Examine the cockpit for ash | X | | | | |
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Page 626 Jan 01/03
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | |contamination. | | | | | | | | |If you find contamination: | | | | | | | | |(1) Clean all the contaminated surfaces| | X | | | | | | |(2) Examine the oxygen full face masks | | X | | | | | | | for contamination. | | | | | | | | | If you find contamination: | | | | | | | | | (a) Clean the oxygen full face | | | X | | | | | | masks | | | | | | | | | (Ref. TASK 35-12-41-100-802). | | | | | | | C.| |Examine the avionics compartment (all | X | | | | | | | |the items you can see), specially: | | | | | | | | |- around the ventilated components | | | | | | | | |- the plugs | | | | | | | | |- the equipments | | | | | | | | |for ash contamination. | | | | | | | | |If you find contamination: | | | | | | | | |(1) Clean all the contaminated surfaces| | X | | | | | | |NOTE: If the crew report shows a very | | | | | | | | | dense cloud of volcanic ashes, | | | | | | | | | clean the computers in the | | | | | | | | workshop. | | | | | | | | | | | | | | | | D.| |Examine the cargo compartments for ash | X | | | | | | | |contamination. | | | | | | | | |If you find contamination: | | | | | | | | |(1) Clean all the contaminated surfaces| | X | | | | | | | (specially the PDU sensors). | | | | | | | | |(2) Examine the cargo drainage system | | X | | | | | | | (if installed) for ash | | | | | | | | | contamination. | | | | | | | | | If you find contamination: | | | | | | | | | (a) Replace the filters of the | | | X | | | | | | drain funnels. | | | | | | -------------------------------------------------------------------------------
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Page 627 Jan 01/03
Subtask 05-51-25-210-090 C. Inspection (Ref. TASK (Ref. TASK (Ref. TASK
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of the Fuselage, the Wings and the Stabilizers 53-15-11-200-801) (Ref. TASK 56-11-11-200-801) 56-11-12-200-801) (Ref. TASK 56-12-11-200-801) 56-21-15-200-801) (Ref. AMM 122227 PB 301)
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the fuselage | | | | | | | | | | | | | | | | A.| | Examine the radome skin for damage | X | | | | | | | | (Ref. TASK 53-15-11-200-801). | | | | | | | | | | | | | | | | B.| | Examine the windshield, the fixed | X | | | | | | | | windows and the sliding windows for | | | | | | | | | damage: | | | | | | | | | - for the windshield | | | | | | | | | (Ref. TASK 56-11-11-200-801) | | | | | | | | | - for the fixed windows | | | | | | | | | (Ref. TASK 56-11-12-200-801) | | | | | | | | | - for the sliding windows | | | | | | | | | (Ref. TASK 56-12-11-200-801). | | | | | | | | | | | | | | | | C.| | Examine the passenger cabin windows, | X | | | | | | | | the passenger/crew doors and the | | | | | | | | | emergency exit windows for damage | | | | | | | | | (Ref. TASK 56-21-15-200-801). | | | | | | | | | | | | | | | | D.| | Examine all of the fuselage skin, the | X | | | | | | | | belly fairing and the wing-to-fuselage| | | | | | | | | fairings for damage. | | | | | | | | | | | | | | | | E.| | Examine the ram air inlet and outlet, | X | | | | | | | | the air inlet and outlet flaps for | | | | | | | | | damage. | | | | | | | | | | | | | | | |2. | | Inspection of the Wings | | | | | | | | | | | | | | | | A.| | Examine all the static dischargers for| X | | | | | | | | damage. | | | | | | | | | | | | | | | | B.| | Examine the top and bottom skin of the| X | | | | | | | | wings for damage. | | | | | | | | | | | | | | |
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Page 628 Jan 01/03
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | C.| | Examine the flap track fairings for | X | | | | | | | | damage. | | | | | | | | | | | | | | | | D.| | Examine the skin of all the control | X | | | | | | | | surfaces ( slats, flaps, ailerons | | | ||| | | | and the spoilers), specially the | | | | | | | | | leading and the trailing edges, | | | | | | | | | for damage. | | | | | | | | | | | | | | | | E.| | Examine the hinge areas of the | X | | | | | | | | spoilers and the ailerons for | | | | | | | | | contamination. | | | | | | | | | | | | | | | | F.| | Examine the flap tracks, flap inter | X | | | | | | | | connecting strut, track 4 sensor, | | | | | | | | | roller mechanisms, steady bearings and| | | | | | | | | universal joints for contamination. | | | | | | | | | Make sure that there is no ash deposit| | | | | | | | | on the roller stops. | | | | | | | | | If you find contamination: | | | | | | | | | (1) Clean and lubricate the related | | X | | | | | | | components | | | | | | | | | (Ref. AMM 12-22-27 PB 301). | | | | | | | | | | | | | | | | G.| | Examine the piston rod of each | X | | | | | | | | servocontrol of the ailerons and the | | | | | | | | | spoilers for contamination. | | | | | | | | | If you find contamination: | | | | | | | | | (1) Clean the piston rod of the | | X | | | | | | | servocontrols. | | | | | | | | | | | | | | | |3. | | Inspection of the Vertical Stabilizer | | | | | | | | | | | | | | | | A.| | Examine all the static dischargers for| X | | | | | | | | damage. | | | | | | | | | | | | | | | | B.| | Examine the skin of the vertical | X | | | | | | | | stabilizer and the rudder, specially | | | | | | | | | the leading and the trailing edges, | | | | | | | | | for damage. | | | | | | | | | | | | | | | | C.| | Examine the hinge areas of the rudder | X | | | | | | | | for contamination. | | | | | |
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Page 629 Jan 01/03
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | | | | | | | | D.| | Examine the piston rod of each | X | | | | | | | | servocontrol of the rudder for | | | | | | | | | contamination. | | | | | | | | | If you find contamination: | | | | | | | | | (1) Clean the piston rod of the | | X | | | | | | | servocontrols. | | | | | | | | | | | | | | | |4. | | Inspection of the Horizontal | | | | | | | | | Stabilizers | | | | | | | | | | | | | | | | A.| | Examine all the static dischargers for| X | | | | | | | | damage. | | | | | | | | | | | | | | | | B.| | Examine the skin of the horizontal | X | | | | | | | | stabilizers and the elevators, | | | | | | | | | specially the leading and the trailing| | | | | | | | | edges, for damage. | | | | | | | | | | | | | | | | C.| | Examine the hinge areas of the | X | | | | | | | | elevators for contamination. | | | | | | | | | | | | | | | | D.| | Examine the piston rod of each | X | | | | | | | | servocontrol of the elevators for | | | | | | | | | contamination. | | | | | | | | | If you find contamination: | | | | | | | | | (1) Clean the piston rod of the | | X | | | | | | | servocontrols. | | | | | | | | | | | | | | | |5. | | Inspection of the external lights | | | | | | | | | | | | | | | | A.| | Examine all the external lights for | X | | | | | | | | damage. | | | | | | | | | If you find damage: | | | | | | | | | (1) Replace the related component(s). | | X | | | | | | | | | | | | | |6. | | Inspection of the antennas and the | | | | | | | | | drain masts | | | | | | | | | | | | | | | | A.| | Examine all the antennas and the drain| X | | | | | | | | masts for damage. | | | | | | | | | If you find damage: | | | | | | | | | (1) Replace the related component(s). | | X | | | |
EFF : ALL 05-51-25 SROS
Page 630 Jan 01/03
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| ------------------------------------------------------------------------------Subtask 05-51-25-210-091 D. Inspection of the Probes and Sensors NOTE : If the aircraft was on ground with the applicable protective ____ covers/devices installed (Ref.AMM 10-11-00) when the volcanic ash contamination occurred, this inspection is not necessary if there is no ash behind the covers.
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NOTE : If the crew report shows a very dense cloud of volcanic ashes, ____ If the maintenance reports a very dense cloud of volcanic ashes with probe covers not in position,. If a general inspection shows evidence of heavy contamination: - you must flush all the pressure lines: (Ref. TASK 12-24-34-600-801) (Ref. TASK 34-11-00-170-801) (Ref. TASK 34-11-00-170-802) (Ref. TASK 34-11-00-170-803) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the sensors and probes | | | | | | | | | | | | | | | | A.| | Inspect all the probes and sensors | X | | | | | | | | | | | | | | | | |(1) Examine all the probes and sensors | | | | | | | | | for damage and contamination (not | | | | | | | | | clogged): | | | | | | | | | - the pitot probes | | | | | | | | | - the static probes | | | | | | | | | - the TAT sensors | | | | | | | | | - the AOA sensors | | | | | | | | | - the ice detector probes | | | | | | | | | (if installed) | | | | | | | | |NOTE: Make sure that the AOA sensors | | | | | | | | | move freely and that the drain | | | | | | | | | holes of the pitot probes are not| | | | | | | | | clogged. | | | | | | | | | | | | | | | | | |(2) Drain the standby static pressure | X | | | | | | | | lines and make sure that there are | | | | | |
EFF : ALL 05-51-25 SROS
Page 631 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | no signs of ash | | | | | | | | | (Ref. TASK 12-24-34-600-801). | | | | | | | | | If you find contamination: | | | | | | | B.| | Flush all the pressure lines | | X | | | | | | | (Ref. TASK 34-11-00-170-801) | | | | | | | | | (Ref. TASK 34-11-00-170-802) | | | | | | | | | (Ref. TASK 34-11-00-170-803). | | | | | | ------------------------------------------------------------------------------Subtask 05-51-25-210-092 E. Inspection of the Landing Gear Doors, the Landing Gears and the Landing Gear Wells (Ref. AMM 122232 PB 301)
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the landing gear doors, | | | | | | | | |the landing gears and the landing gear | | | | | | | | |wells. | | | | | | | | |NOTE: If you find contamination, you | | | | | | | | | must: | | | | | | | | | (a) Remove the contamination from| | | | | | | | | surface, the moving joints | | | | | | | | | and the chromed areas of | | | | | | | | | shock absorbers and actuators| | | | | | | | | before the next flight. | | | | | | | | | (b) Do a full lubrication of the | | | | | | | | | landing gears before a | | | | | | | | | maximum of 10 flight cycles | | | | | | | | | (Ref. AMM 12-22-32, PB 301). | | | | | | | | | | | | | | | | A.| |Inspection of the doors | | | | | | | | |(1) Examine all the doors for damage | X | | | | | | | | and/or contamination, specially on:| | | | | | | | | - the door skin | | | | | | | | | - the door hinges | | | | | | | | | - the proximity sensors | | | | | | | | | - the actuator bare rods. | | | | | | | | | | | | | | | | B.| |Inspection of the landing gears | | | | | | | | |(1) Examine all the landing gear | X | | | | |
EFF : ALL 05-51-25 SROS
Page 632 Jan 01/03
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | structures and the components | | | | | | | | | installed on them for damage and/or| | | | | | | | | contamination, specially on: | | | | | | | | | - the attachment points of the | | | | | | | | | landing gears | | | | | | | | | - the proximity sensors | | | | | | | | | - the actuator rods | | | | | | | | | - the chromed area of the shock | | | | | | | | | absorbers | | | | | | | | | - the mechanical linkages and the | | | | | | | | | moving joints. | | | | | | | | | | | | | | | | C.| |Inspection of the landing gear wells | | | | | | | | |(1) Examine all the landing gear wells | X | | | | | | | | and the components installed in | | | | | | | | | them for damage and/or | | | | | | | | | contamination. | | | | | | ------------------------------------------------------------------------------R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-25-210-100 F. Inspection of the Nacelles and the Engines NOTE : If the aircraft was on the ground with the applicable protective ____ covers/devices installed (Ref. AMM 10-11-00) when the volcanic ash contamination occurred, thisinspection is not necessary if there is no ash behind the covers. NOTE : If the aircraft was on the ground without the applicable ____ protective covers/devices installed, we recommend that after you start the engines, you let the engines run a few minutes before you use the bleed air systems. This is to make sure that the engines blow out remaining particles. (Ref. TASK 71-61-00-220-801) (Ref. TASK 71-13-00-220-801) (Ref. TASK 78-30-00-210-802) (Ref. TASK 26-21-00-720-819) (Ref. TASK 71-00-00-200-802)
EFF : ALL 05-51-25 SROS
Page 633 Jul 01/05
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the nacelles and engines | | | | | | | | | | | | | | | | A.| |Inspection of the nacelles | | | | | | | | |(1) Examine the air intake cowl for | X | | | | | | | | damage | | | | | | | | | (Ref. TASK 71-61-00-220-801). | | | | | | | | |(2) Examine the fan cowl doors for | X | | | | | | | | damage | | | | | | | | | (Ref. TASK 71-13-00-220-801). | | | | | | | | |(3) Examine the thrust reversers for | X | | | | | | | | damage | | | | | | | | | (Ref. TASK 78-30-00-210-802). | | | | | | | | | | | | | | | | B.| |Inspection of the engines | | | | | | | | |(1) Examine the fire extinguisher | X | | | | | | | | outlets for contamination. | | | | | | | | | If you find contamination: | | | | | | | | | (a) Do a check of the | | X | | | | | | | distribution piping for | | | | | | | | | obstruction | | | | | | | | | (Ref. TASK 26-21-00-720-819). | | | | | | | | |(2) Do the inspection of the engines | X | | | | | | | | after flight through volcanic ash | | | | | | | | | (Ref. TASK 71-00-00-200-802). | | | | | | ------------------------------------------------------------------------------**ON A/C 701-749, Subtask 05-51-25-210-100-A F. Inspection of the Nacelles and the Engines NOTE : If the aircraft was on the ground with the applicable protective ____ covers/devices installed (Ref. AMM 10-11-00) when the volcanic ash contamination occurred, thisinspection is not necessary if there is no ash behind the covers. NOTE : If the aircraft was on the ground without the applicable ____ protective covers/devices installed, we recommend that after you start the engines, you let the engines run a few minutes before you use the bleed air systems. This is to make sure that the engines blow out remaining particles.
R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-25 301-399, 401-449, 451-499, 701-749, SROS
Page 634 Jul 01/05
(Ref. TASK 71-61-41-200-802) (Ref. TASK 71-13-00-200-803) (Ref. TASK 78-32-00-200-802) (Ref. TASK 26-21-00-720-819) (Ref. TASK 71-00-00-200-813) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the nacelles and engines | | | | | | | | | | | | | | | | A.| |Inspection of the nacelles | | | | | | | | |(1) Examine the air intake cowl for | X | | | | | | | | damage | | | | | | | | | (Ref. TASK 71-61-41-200-802). | | | | | | | | |(2) Examine the fan cowl doors for | X | | | | | | | | damage | | | | | | | | | (Ref. TASK 71-13-00-200-803). | | | | | | | | |(3) Examine the thrust reversers for | X | | | | | | | | damage | | | | | | | | | (Ref. TASK 78-32-00-200-802). | | | | | | | | | | | | | | | | B.| |Inspection of the engines | | | | | | | | |(1) Examine the fire extinguisher | X | | | | | | | | outlets for contamination. | | | | | | | | | If you find contamination: | | | | | | | | | (a) Do a check of the | | X | | | | | | | distribution piping for | | | | | | | | | obstruction | | | | | | | | | (Ref. TASK 26-21-00-720-819). | | | | | | | | |(2) Do inspection/check of the engine | X | | | | | | | | after flight through volcanic ash | | | | | | | | | (Ref. TASK 71-00-00-200-813). | | | | | | ------------------------------------------------------------------------------**ON A/C ALL Subtask 05-51-25-210-094
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G. Inspection (Ref. TASK (Ref. TASK (Ref. TASK (Ref. TASK
of the APU 49-16-00-200-801) (Ref. TASK 49-16-00-100-801) 49-91-44-000-801) (Ref. TASK 49-91-44-400-801) 49-20-00-290-809) (Ref. TASK 49-20-00-290-810) 26-22-00-200-801)
EFF : ALL 05-51-25 SROS
Page 635 Jul 01/06
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the APU | | | | | | | | | | | | | | | | A.| |Examine the APU intake and exhaust for | X | | | | | | | |contamination and/or damage | | | | | | | | |(Ref. TASK 49-16-00-200-801). | | | | | | | | |If you find contamination: | | | | | | | | |(1) If the APU was not in operation | | | | | | | | | during volcanic ash contamination: | | | | | | | | | (a) Clean the APU air intake and | | X | | | | | | | exhaust | | | | | | | | | (Ref. TASK 49-16-00-100-801). | | | | | | | | |(2) If the APU was in operation during | | | | | | | | | volcanic ash contamination: | | | | | | | | | (a) Clean the APU air intake and | | X | | | | | | | exhaust | | | | | | | | | (Ref. TASK 49-16-00-100-801). | | | | | | | | | (b) Examine the oil cooler for | | X | | | | | | | contamination | | | | | | | | | (Ref. TASK 49-91-44-000-801) | | | | | | | | | (Ref. TASK 49-91-44-400-801). | | | | | | | | | If you find contamination: | | | | | | | | | - do an APU inspection/check | | | X | | | | | | (Ref. TASK 49-20-00-290-809) | | | | | | | | | (Ref. TASK 49-20-00-290-810).| | | | | | | | | NOTE: We recommend that you | | | | | | | | | replace the APU if you | | | | | | | | | find large contamination | | | | | | | | | in the oil cooler. | | | | | | | | | (c) Examine the fire extinguisher | | X | | | | | | | outlets for contamination | | | | | | | | | (Ref. TASK 26-22-00-200-801). | | | | | | -------------------------------------------------------------------------------
EFF : ALL 05-51-25 SROS
Page 636 Jul 01/06
Subtask 05-51-25-210-095 R
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H. Inspection of the Fuel System (Ref. TASK 28-12-00-210-802) (Ref. TASK 12-32-28-281-812) (Ref. TASK 2814-00-210-801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the fuel system | | | | | | | | | | | | | | | | A.| | Examine the NACA vent intakes for | X | | | | | | | | contamination | | | | | | | | | (Ref. TASK 28-12-00-210-802). | | | | | | | | | If you find contamination: | | | | | | | | | (1) Get a sample of fuel from the | | X | | | | | | | water drain valves and do a check | | | | | | | | | for particle contamination | | | | | | | | | (Ref. TASK 12-32-28-281-812). | | | | | | | | | If you find contamination: | | | | | | | | | (a) Clean the fuel tanks. | | X | | | | | | | | | | | | | | B.| |Examine the Refuel/Defuel control | X | | | | | | | |panel for contamination. | | | | | | | | |If you find contamination: | | | | | | | | |(1) Clean the panel. | | X | | | | | | | | | | | | | | C.| |Examine the refuel/defuel coupling and | X | | | | | | | |the refuel/defuel coupling cap for | | | | | | | | |contamination. | | | | | | | | |If you find contamination. | | | | | | | | |(1) Clean the refuel/defuel coupling | | X | | | | | | | and the refuel/defuel coupling cap.| | | | | | | | | | | | | | | | D.| |Examine the overwing refuel adaptor/ | X | | | | | | | |cap for contamination. | | | | | | | | |If you find contamination: | | | | | | | | |(1) Clean the adaptor/cap. | | X | | | | | | | | | | | | | | E.| |Examine the fuel drain mast for | X | | | | | | | |contamination | | | | | | | | |(Ref. TASK 28-14-00-210-801). | | | | | | | | |If you find contamination: | | | | | | | | |(1) Clean the fuel drain mast. | | X | | | | -------------------------------------------------------------------------------
EFF : ALL 05-51-25 SROS
Page 637 Jan 01/06
Subtask 05-51-25-210-096 J. Inspection of the Anti-Ice System NOTE : If the anti-ice system was selected OFF ____ is not necessary. (Ref. TASK 27-84-61-000-801) (Ref. TASK (Ref. TASK 27-84-62-000-801) (Ref. TASK (Ref. TASK 30-11-51-000-802) (Ref. TASK (Ref. TASK 30-21-51-000-801) (Ref. TASK
in flight, this inspection 27-84-61-400-801) 27-84-62-400-801) 30-11-51-400-802) 30-21-51-400-801)
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the anti-ice system | | | | | | | | | | | | | | | | A.| |Examine the air inlet and the outlet | X | | | | | | | |of the pre-cooler for contamination. | | | | | | | | | | | | | | | | | |If you find contamination: | | | | | | | | |(1) If the anti-ice system was not in | | | | | | | | | operation during or after volcanic | | | | | | | | | ash contamination: | | | | | | | | | (a) Disconnect and remove the duct | | X | | | | | | | immediately upstream of the | | | | | | | | | wing anti-ice valve. | | | | | | | | | (b) Examine the valve for | | X | | | | | | | contamination. | | | | | | | | | If you find contamination: | | | | | | | | | - Clean the ducts upstream of | | | X | | | | | | the wing anti-ice valve. | | | | | | | | | - Clean the valve and replace | | | X | | | | | | the valve filter | | | | | | | | | (Ref. TASK 30-11-51-000-802) | | | | | | | | | (Ref. TASK 30-11-51-400-802).| | | | | | | | |(2) If the anti-ice system was in | | | | | | | | | operation during or immediately | | | | | | | | | after volcanic ash contamination: | | | | | | | | | (a) Remove the valve filter and | X | | | | | | | | install a clean filter | | | | | | | | | (Ref. TASK 30-11-51-000-802) | | | | | | | | | (Ref. TASK 30-11-51-400-802). | | | | | | | | | (b) Disconnect the anti-ice duct | X | | | | | | | | from the telescopic duct and do| | | | | | | | | a check for contamination. | | | | | |
EFF : ALL 05-51-25 R SROS
Page 638 Jul 01/03
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | If you find contamination: | | | | | | | | | - Clean all the anti-ice ducts | | X | | | | | | | from the pylon interface to | | | | | | | | | the telescopic duct outlet. | | | | | | | | | - Clean the wing anti-ice valve| | X | | | | | | | - Do a check for contamination | | X | | | | | | | at the slat anti-ice duct | | | | | | | | | outlets. Clean them if | | | | | | | | | necessary. | | | | | | | | | (c) Disconnect the slat inter| X | | | | | | | | connecting ducts and do a check| | | | | | | | | for contamination. | | | | | | | | | If you find contamination: | | | | | | | | | - Remove the slats for | | X | | | | | | | component maintenance | | | | | | | | | (Ref. TASK 27-84-61-000-801) | | | | | | | | | (Ref. TASK 27-84-61-400-801) | | | | | | | | | (Ref. TASK 27-84-62-000-801) | | | | | | | | | (Ref. TASK 27-84-62-400-801).| | | | | | | | | (d) Make sure that the telescopic | X | | | | | | | | duct operates correctly and | | | | | | | | | do a check for contamination. | | | | | | | | | If you find contamination: | | | | | | | | | - Remove the telescopic duct | | X | | | | | | | for component maintenance | | | | | | | | | (Ref. TASK 30-11-41-000-801) | | | | | | | | | (Ref. TASK 30-11-41-400-801).| | | | | | | | | | | | | | | | B.| |Examine the nacelle anti-ice valves for| X | | | | | | | |contamination | | | | | | | | |(Ref. TASK 30-21-51-000-801) | | | | | | | | |(Ref. TASK 30-21-51-400-801). | | | | | | | | |If you find contamination: | | | | | | | | |(1) Clean the ducts. | | X | | | | -------------------------------------------------------------------------------
EFF : ALL 05-51-25 SROS
Page 639 Jan 01/03
Subtask 05-51-25-210-097 K. Inspection (Ref. TASK (Ref. TASK (Ref. TASK (Ref. TASK (Ref. TASK
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of the Air Conditioning 36-11-52-000-801) (Ref. 36-12-52-000-801) (Ref. 21-51-51-000-801) (Ref. 21-63-52-000-801) (Ref. 36-11-51-000-801) (Ref.
System TASK 36-11-52-400-801) TASK 36-12-52-400-801) TASK 21-51-51-400-801) TASK 21-63-52-400-801) TASK 36-11-51-400-801)
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the air conditioning | | | | | | | | |system | | | | | | | | | | | | | | | | A.| |Examine the high pressure bleed valves | X | | | | | | | |for contamination | | | | | | | | |(Ref. TASK 36-11-51-000-801) | | | | | | | | |(Ref. TASK 36-11-51-400-801). | | | | | | | | |If you find contamination : | | | | | | | | |(1) Clean the ducts. | | X | | | | | | | | | | | | | | B.| |Examine the bleed valves for | X | | | | | | | |contamination | | | | | | | | |(Ref. TASK 36-11-52-000-801) | | | | | | | | |(Ref. TASK 36-11-52-400-801). | | | | | | | | |If you find contamination : | | | | | | | | |(1) Clean the ducts. | | X | | | | | | | | | | | | | | C.| |Examine the cross-bleed valves for | X | | | | | | | |contamination | | | | | | | | |(Ref. TASK 36-12-52-000-801) | | | | | | | | |(Ref. TASK 36-12-52-400-801). | | | | | | | | |If you find contamination : | | | | | | | | |(1) Clean the ducts. | | X | | | | | | |(2) Replace the cross-bleed valve. | | X | | | | | | | | | | | | | | D.| |Examine the flow control valves for | X | | | | | | | |contamination. | | | | | | | | |(Ref. TASK 21-51-51-000-801) | | | | | | | | |(Ref. TASK 21-51-51-400-801). | | | | | | | | |If you find contamination : | | | | | | | | |(1) Clean the ducts. | | X | | | | | | |(2) Replace the filter. | | X | | | | | | | | | | | | | | E.| |Examine the primary heat exchangers, | X | | | | |
EFF : ALL 05-51-25 SROS
Page 640 Jan 01/03
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | |main heat exchangers, condensers, | | | | | | | | |reheaters and water extractors for | | | | | | | | |contamination. | | | | | | | | |If you find contamination : | | | | | | | | |(1) Clean the related component (refer | | X | | | | | | | to the manufacturers instructions | | | | | | | | | for the cleaning procedure). | | | | | | | | | | | | | | | | F.| |Examine the trim air pressure | X | | | | | | | |regulating valves for contamination | | | | | | | | |(Ref. TASK 21-63-52-000-801) | | | | | | | | |(Ref. TASK 21-63-52-400-801). | | | | | | | | |If you find contamination : | | | | | | | | |(1) Clean the ducts. | | X | | | | | | |(2) Replace the filter. | | X | | | | | | | | | | | | | | G.| |Examine the water extractor drain lines| X | | | | | | | |for contamination and blockage. | | | | | | | | | | | | | | | | H.| |Examine the air cycle machine for | X | | | | | | | |contamination. | | | | | | | | |If you find contamination: | | | | | | | | |(1) Replace the filter. | | X | | | | ------------------------------------------------------------------------------Subtask 05-51-25-210-098 L. Inspection of the Hydraulic System (Ref. TASK 29-10-00-200-803) (Ref. TASK 12-32-29-281-801)
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the hydraulic system | | | | | | | | | | | | | | | | A.| |Examine the filters for contamination | X | | | | | | | |(clogging indicators and filter | | | | | | | | |elements) | | | | | | | | |(Ref. TASK 29-10-00-200-803). | | | | | | | | |If you find contamination: | | | | | | | | |(1) replace the filter elements. | | X | | | | | | |(2) get a sample of fluid and make | | X | | | |
EFF : ALL 05-51-25 SROS
Page 641 Jan 01/03
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | sure that contamination is in | | | | | | | | | the permitted limits | | | | | | | | | (Ref. TASK 12-32-29-281-801). | | | | | | | | | | | | | | | | B.| |Examine the RAT for contamination | X | | | | | | | |and/or damage. | | | | | | | | | | | | | | | | C.| |Examine the sliding unions for | X | | | | | | | |contamination. | | | | | | | | |If you find contamination: | | | | | | | | |(1) Clean the sliding unions. | | X | | | | ------------------------------------------------------------------------------Subtask 05-51-25-210-099 M. Inspection of the Potable Water System (Ref. TASK 12-24-38-680-801) (Ref. TASK 12-15-38-613-801).
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the potable water system | | | | | | | | | | | | | | | | A.| |Drain the potable water system, flush | X | | | | | | | |and refill with potable water | | | | | | | | |(Ref. TASK 12-24-38-680-801) | | | | | | | | |(Ref. TASK 12-15-38-613-801). | | | | | | ------------------------------------------------------------------------------5. Close-up ________ Subtask 05-51-25-866-055 A. Retraction of the Flight control surfaces (1) Retract the flaps and the slats (Ref. TASK 27-50-00-866-802). (2) Retract the spoilers (Ref. TASK 27-60-00-866-802).
EFF : ALL 05-51-25 SROS
Page 642 Jan 01/03
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Subtask 05-51-25-410-053 B. Close Access
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(1) Make sure that the work area is clean and clear of tools and other items.
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(2) Close the NLG doors (Ref. TASK 32-22-00-410-801).
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(3) Close the MLG doors (Ref. TASK 32-12-00-410-801).
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(4) Close all the access doors, and the access panels opened during the inspection procedure.
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Subtask 05-51-25-860-055
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C. Put the Aircraft back to its Initial Configuration
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(1) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801)
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(2) Remove the access platform(s).
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(3) Remove the warning notice(s).
EFF : ALL 05-51-25 SROS
Page 643 Jul 01/02
INSPECTION AFTER ENGINE FAILURE - INSPECTION/CHECK __________________________________________________ TASK 05-51-26-200-801 Inspection of the Aircraft after Engine Failure 1. __________________ Reason for the Job You must do this inspection after an engine failure if: - the engine is not balanced after one or several blades (fan or other blades) is /are damaged/missing. - the engine is seized. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
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No No No No
specific specific specific specific
safety barriers warning notices wheel chocks adjustable access platform 5.0 m (16 ft. 5 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------05-56-00-200-801 32-00-00-481-801 71-00-00-000-803 71-00-00-000-805 71-00-00-400-803 71-13-00-010-802 71-13-00-010-805 71-13-00-410-802 71-13-00-410-805 78-30-00-010-801
Measurement of the Aircraft by Photogrammetry after Abnormal Operation of the Aircraft Installation of the Safety Devices on the Landing Gears Removal of the Engine Removal of the Demountable Power Plant Installation of the Engine Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Open the Fan Cowl Doors Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Close the Fan Cowl Doors Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS)
EFF : ALL 05-51-26 SROS
Page 601 Jan 01/07
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------78-30-00-010-803 78-30-00-410-801 78-30-00-410-803
Open the Thrust Reverser Cowl Doors Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Close the Thrust Reverser Cowl Doors
3. __________ Job Set-up Subtask 05-51-26-941-050 A. Safety Precautions (1) Put the safety barriers in position. (2) Put warning notices in position in the cockpit to tell persons not to operate the systems. (3) Put wheel chocks in position at the main gears. (4) Install the safety devices on the landing gear (Ref. TASK 32-00-00481-801). R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-26-010-050 B. Get Access (1) Open the fan cowls doors (Ref. TASK 71-13-00-010-802).
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(a) FOR 4030EM1 415BL, 416BR
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(b) FOR 4030EM2 425BL, 426BR (2) Open the thrust reverser doors (Ref. TASK 78-30-00-010-801).
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(a) FOR 4030EM1 417AL, 418AR
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(b) FOR 4030EM2 427AL, 428AR
EFF : ALL 05-51-26 SROS
Page 602 Jul 01/05
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(3) Put an adjustable access platform in position near the damaged engine. **ON A/C 701-749, Subtask 05-51-26-010-050-A B. Get Access (1) Open the fan cowls doors (Ref. TASK 71-13-00-010-805). (a) FOR 4030EM1 415AL, 416AR (b) FOR 4030EM2 425AL, 426AR (2) Open the thrust reverser doors (Ref. TASK 78-30-00-010-803). (a) FOR 4030EM1 417AL, 418AR (b) FOR 4030EM2 427AL, 428AR
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(3) Put an adjustable access platform in position near the damaged engine. **ON A/C ALL Subtask 05-51-26-860-050 C. Aircraft Maintenance Configuration (1) Make sure that the hydraulic systems are depressurized **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-26-010-051 D. Engine Removal (1) Remove the engine (Ref. TASK 71-00-00-000-803).
EFF : ALL 05-51-26 SROS
Page 603 Jan 01/07
**ON A/C 701-749, Subtask 05-51-26-010-051-A D. Engine Removal (1) Remove the engine (Ref. TASK 71-00-00-000-805). **ON A/C ALL 4. Procedure _________ R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-26-210-050 A. Inspection of the Pylon and the Nacelle (Ref. TASK 05-56-00-200-801) NOTE : All the necessary inspections are visual unless specified ____ differently in the text procedure. Operators can refer to the Non Destructive Testing Manual (NTM) and use non destructive procedure. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of Outboard and Inboard | | | | | | | | | Pylons | | | | | | | | | | | | | | | | A.| | Examine the items below for cracks, | | | | | | | | | signs of shear, damaged or missing | X | | | | | | | | fasteners, cracked paint: | | | | | | | | | - external panels | | | | | | | | | - the plates you find in: | | | | | | | | | . the visor | | | | | | | | | . the forward secondary structure | | | | | | | | | . the primary structure | | | | | | | | | . the pylon-to-wing fillet | | | | | | | | | . the aft secondary structure | | | | | | | | | . the aft bottom fairing | | | | | | | | | . the center bottom fairing | | | | | | | | | . all access doors and panels. | | | | | |
EFF : ALL 05-51-26 SROS
Page 604 Jul 01/05
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | If you find damage: | | | | | | | | | (1) Open the doors and panels to get | | X | | | | | | | access to the structure. | | | | | | | | | (2) Examine the adjacent structure for| | X | | | | | | | distortion and the plates for | | | | | | | | | - buckles or warps, wrinkles or | | | | | | | | | tears. | | | | | | | | | (3) Examine the items below for | | X | | | | | | | - distortion, pulled or missing | | | | | | | | | fasteners, tears or cracked | | | | | | | | | paint: | | | | | | | | | . the primary structure | | | | | | | | | . the fasteners | | | | | | | | | . the longerons | | | | | | | | | . the lateral plates | | | | | | | | | . the main ribs | | | | | | | | | . the lateral panels. | | | | | | | | | (4) Examine the fire protection system| | | | | | | | | and specially the items below for | | | | | | | | | - distortion, fluid leaks and | | | | | | | | | other damage: | | X | | | | | | | . the attachments of the fire | | | | | | | | | extinguishing bottles | | | | | | | | | . the attachment of the pipes | | | | | | | | | . the electrical wiring | | | | | | | | | . the hydraulic pipes | | | | | | | | | . the fuel pipes | | | | | | | | | . the air conditioning pipes and| | | | | | | | | components | | | | | | | | | . the components that are in the| | | | | | | | | engine pylon. | | | | | | | | | | | | | | | | B.| | Examine externally the hinge fittings | | | | | | | | | of: | X | | | | | | | | - the fan cowls | | | | | | | | | - the thrust reverser cowls. | | | | | | | | | | | | | | | |2. | | Inspection of the Nacelles | | | | | | | | | | | | | | | | A.| | Examine the fan cowls. | X | | | | | | | | | | | | | | | B.| | Examine the thrust reverser cowls | X | | | | | | | | | | | | | |
EFF : 001-049, 201-249, 251-252, 255-299, 05-51-26 301-399, 401-449, 451-499, SROS
Page 605 Jan 01/07
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------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | If you find damage: | | | | | | | | | (1) Examine externally the engine-to- | | X | | | | | | | pylon attach fittings below the | | | | | | | | | main ribs for: | | | | | | | | | - damage, rupture, signs of burns | | | | | | | | | oxidation, cracks, distortion. | | | | | | | | | (2) Remove the fillets from the | | X | | | | | | | outboard and inboard pylons. | | | | | | | | | (3) Examine | | | | | | | | | - the forward pylon-to-wing attach| | | | | | | | | fitting | | | | | | | | | - the aft pylon-to-wing attach | | | | | | | | | fitting. | | | | | | | | | If you find damage: | | | | | | | | | (a) Examine the area adjacent to | | | | | | | | | the forward and aft | | | | | | | | | attachments of the pylon for: | | | X | | | | | | - the correct condition of all| | | | | | | | | fasteners and safety | | | | | | | | | devices, cracks and damage. | | | | | | | | | (b) Examine the wing bottom skin | | | | | | | | | adjacent to the forward and | | | | | | | | | aft attachments of the pylon | | | X | | | | | | for : | | | | | | | | | - cracks, fluid leaks, damage,| | | | | | | | | the correct condition of all| | | | | | | | | fasteners and safety | | | | | | | | | devices. | | | | | | | | | If you find damage: | | | | | | | | | (1) Defuel the wing and get access | | | X | | | | | | into it. | | | | | | | | | (2) Examine: | | | | | | | | | - the internal structure | | | | | | | | | - the rear and front spars | | | X | | | | | | - the ribs | | | | | | | | | - the stringers | | | | | | | | | - the pylon attachments | | | | | | | | | - the brackets | | | | | | | | | - the structure adjacent to the | | | | | | | | | outboard and inboard pylons. | | | | | | | | | If you find damage: | | | | | | | | | (1) Do a measurement of the aircraft. | | | X | | | | | | (Ref. TASK 05-56-00-200-801) | | | | | |
EFF : 001-049, 201-249, 251-252, 255-299, 05-51-26 301-399, 401-449, 451-499, SROS
Page 606 Jan 01/07
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| ------------------------------------------------------------------------------**ON A/C 701-749, Subtask 05-51-26-210-050-A A. Inspection of the Pylon and the Nacelle (Ref. TASK 05-56-00-200-801) NOTE : All the necessary inspections are visual unless specified ____ differently in the text procedure. Operators can refer to the Non Destructive Testing Manual (NTM) and use non destructive procedure. ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of Outboard and Inboard | | | | | | | | | Pylons | | | | | | | | | | | | | | | | A.| | Examine the items below for cracks, | | | | | | | | | signs of shear, damaged or missing | X | | | | | | | | fasteners, cracked paint: | | | | | | | | | - external panels | | | | | | | | | - the plates you find in: | | | | | | | | | . the visor | | | | | | | | | . the forward secondary structure | | | | | | | | | . the primary structure | | | | | | | | | . the pylon-to-wing fillet | | | | | | | | | . the aft secondary structure | | | | | | | | | . the aft bottom fairing | | | | | | | | | . the center bottom fairing | | | | | | | | | . all access doors and panels. | | | | | | | | | If you find damage: | | | | | | | | | (1) Open the doors and panels to get | | X | | | | | | | access to the structure. | | | | | | | | | (2) Examine the adjacent structure for| | X | | | | | | | distortion and the plates for | | | | | | | | | - buckles or warps, wrinkles or | | | | | | | | | tears. | | | | | | | | | (3) Examine the items below for | | X | | | |
R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-26 301-399, 401-449, 451-499, 701-749, SROS
Page 607 Jul 01/05
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R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - distortion, pulled or missing | | | | | | | | | fasteners, tears or cracked | | | | | | | | | paint: | | | | | | | | | . the primary structure | | | | | | | | | . the fasteners | | | | | | | | | . the longerons | | | | | | | | | . the lateral plates | | | | | | | | | . the main ribs | | | | | | | | | . the lateral panels. | | | | | | | | | (4) Examine the fire protection system| | | | | | | | | and specially the items below for | | | | | | | | | - distortion, fluid leaks and | | | | | | | | | other damage: | | X | | | | | | | . the attachments of the fire | | | | | | | | | extinguishing bottles | | | | | | | | | . the attachment of the pipes | | | | | | | | | . the electrical wiring | | | | | | | | | . the hydraulic pipes | | | | | | | | | . the fuel pipes | | | | | | | | | . the air conditioning pipes and| | | | | | | | | components | | | | | | | | | . the components that are in the| | | | | | | | | engine pylon. | | | | | | | | | | | | | | | | B.| | Examine externally the hinge fittings | | | | | | | | | of: | X | | | | | | | | - the fan cowls | | | | | | | | | - the thrust reverser cowls. | | | | | | | | | | | | | | | |2. | | Inspection of the Nacelles | | | | | | | | | | | | | | | | A.| | Examine the fan cowls. | X | | | | | | | | | | | | | | | B.| | Examine the thrust reverser cowls | X | | | | | | | | If you find damage: | | | | | | | | | (1) Examine externally the engine-to- | | X | | | | | | | pylon attach fittings below the | | | | | | | | | main ribs for: | | | | | | | | | - damage, rupture, signs of burns | | | | | | | | | oxidation, cracks, distortion. | | | | | | | | | (2) Remove the fillets from the | | X | | | | | | | outboard and inboard pylons. | | | | | | | | | (3) Examine | | | | | |
EFF : 701-749, 05-51-26 SROS
Page 608 Jan 01/07
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - the forward pylon-to-wing attach| | | | | | | | | fitting | | | | | | | | | - the aft pylon-to-wing attach | | | | | | | | | fitting. | | | | | | | | | If you find damage: | | | | | | | | | (a) Examine the area adjacent to | | | | | | | | | the forward and aft | | | | | | | | | attachments of the pylon for: | | | X | | | | | | - the correct condition of all| | | | | | | | | fasteners and safety | | | | | | | | | devices, cracks and damage. | | | | | | | | | (b) Examine the wing bottom skin | | | | | | | | | adjacent to the forward and | | | | | | | | | aft attachments of the pylon | | | X | | | | | | for : | | | | | | | | | - cracks, fluid leaks, damage,| | | | | | | | | the correct condition of all| | | | | | | | | fasteners and safety | | | | | | | | | devices. | | | | | | | | | If you find damage: | | | | | | | | | (1) Defuel the wing and get access | | | X | | | | | | into it. | | | | | | | | | (2) Examine: | | | | | | | | | - the internal structure | | | | | | | | | - the rear and front spars | | | X | | | | | | - the ribs | | | | | | | | | - the stringers | | | | | | | | | - the pylon attachments | | | | | | | | | - the brackets | | | | | | | | | - the structure adjacent to the | | | | | | | | | outboard and inboard pylons. | | | | | | | | | If you find damage: | | | | | | | | | (1) Do a measurement of the aircraft. | | | X | | | | | | (Ref. TASK 05-56-00-200-801) | | | | | | -------------------------------------------------------------------------------
EFF : 701-749, 05-51-26 R SROS
Page 609 Apr 01/02
**ON A/C ALL 5. Close-up ________ R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-26-410-051 A. Engine Installation (1) Install the engine (Ref. TASK 71-00-00-400-803). Subtask 05-51-26-410-050 B. Close Access (1) Close the fan cowls doors (Ref. TASK 71-13-00-410-802).
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(a) FOR 4030EM1 415BL, 416BR
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(b) FOR 4030EM2 425BL, 426BR (2) Close the thrust reverser doors (Ref. TASK 78-30-00-410-801).
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(a) FOR 4030EM1 417AL, 418AR
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(b) FOR 4030EM2 427AL, 428AR (3) Close all the access panels that you opened during the inspection. **ON A/C 701-749, Subtask 05-51-26-410-051-A A. Engine Installation (1) Install the engine
EFF : ALL 05-51-26 SROS
Page 610 Jul 01/05
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Subtask 05-51-26-410-050-A B. Close Access
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(1) Close the fan cowls doors (Ref. TASK 71-13-00-410-805).
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(a) FOR 4030EM1 415AL, 416AR
R R
(b) FOR 4030EM2 425AL, 426AR
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(2) Close the thrust reverser doors (Ref. TASK 78-30-00-410-803).
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(a) FOR 4030EM1 417AL, 418AR
R R
(b) FOR 4030EM2 427AL, 428AR
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**ON A/C ALL Subtask 05-51-26-942-050 C. Put the Aircraft back to its Initial Configuration (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. (4) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-51-26 SROS
Page 611 Oct 01/00
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INSPECTION AFTER IMPACT ON ENGINE COWLS - INSPECTION/CHECK __________________________________________________________ TASK 05-51-27-200-801
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Inspection after Impact on Engine Cowls 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 FOR FIN 4000EM2 No specific
safety barriers warning notice adjustable access platform 5.0 m (16 ft. 5 in.) adjustable access platform 5.0 m (16 ft. 5 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------71-00-00-000-803 71-00-00-000-805 71-00-00-400-803 71-00-00-400-805 71-13-00-010-802 71-13-00-010-805 71-13-00-410-802 71-13-00-410-805 78-30-00-010-801 78-30-00-410-801 78-30-00-410-803 FOR FIN 4030EM2 78-30-00-010-803
Removal of the Engine Removal of the Demountable Power Plant Installation of the Engine Installation of the Demountable Power Plant Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Open the Fan Cowl Doors Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Close the Fan Cowl Doors Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Close the Thrust Reverser Cowl Doors Open the Thrust Reverser Cowl Doors
EFF : ALL 05-51-27 SROS
Page 601 Jul 01/05
3. __________ Job Set-up Subtask 05-51-27-941-050 A. Safety Precautions (1) Put the safety barriers in position. (2) On the panel 145VU: - put a warning notice to tell persons not to start the engine. R R
(3) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure. (4) On the panel 285VU: - make sure that the ON legend of the ENG/FADEC GND PWR/1, (2), pushbutton switch is off - put a warning notice to tell persons not to energize the FADEC system. (5) On the panel 125VU: - make sure that the ENG MASTER switch 1, (2), is in the OFF position - put a warning notice to tell persons not to energize the ECU.
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**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-27-010-050 B. Get Access
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(1) Open the fan cowl doors (Ref. TASK 71-13-00-010-802).
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(a) FOR 4030EM1 415BL, 416BR
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(b) FOR 4030EM2 425BL, 426BR (2) Open the thrust reverser doors (Ref. TASK 78-30-00-010-801).
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(a) FOR 4030EM1 417AL, 418AR
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(b) FOR 4030EM2 427AL, 428AR
EFF : ALL 05-51-27 SROS
Page 602 Jul 01/05
(3) Put an adjustable access platform in position near the damaged engine. **ON A/C 701-749, Subtask 05-51-27-010-050-A B. Get Access R
(1) Open the fan cowl doors (Ref. TASK 71-13-00-010-805). (a) FOR 4030EM1 415AL, 416AR (b) FOR 4030EM2 425AL, 426AR (2) Open the thrust reverser doors (Ref. TASK 78-30-00-010-803). (a) FOR 4000EM1 417AL, 418AR (b) FOR 4000EM2 427AL, 428AR (3) Put an adjustable access platform in position near the damaged engine.
R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-27 301-399, 401-449, 451-499, 701-749, SROS
Page 603 Jul 01/05
**ON A/C ALL 4. Procedure _________ R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-27-210-050 A. Inspection of the Engine (Ref. TASK 71-00-00-000-803) (Ref. TASK 71-00-00-400-803)
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R R R R R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Examine the cowl after a side impact | | | | | | | | |and damage only to the cowl. | | | | | | | | | | | | | | | | A.| |Externally examine the cowl fittings | X | | | | | | | |and the adjacent area of the pylon: | | | | | | | | |(1) Pylon side panels when damage on | | | | | | | | | thrust reverser or core cowl. | | | | | | | | |(2) Cantilever structure when damage on| | | | | | | | | inlet cowl, fan cowl or thrust | | | | | | | | | reverser for: | | | | | | | | | - damage. | | | | | | | | | | | | | | | |2. | |Examine the cowl after a side impact | | | | | | | | |and subsequent damage to the engine or | | | | | | | | |the equipment/accessories attached to | | | | | | | | |it for: | | | | | | | | |- damage. | | | | | | | | | | | | | | | | A.| |Examine pylon panels, doors and auxi- | X | | | | | | | |liary structure for distortion, | | | | | | | | |wrinkles, buckles, tearing of plates at| | | | | | | | |the rivets and stringers attached to | | | | | | | | |panels. | | | | | | | | | | | | | | | | B.| |Examine pylon main frame for: | X | | | | | | | |- cracks, cracked or flaking paint, | | | | | | | | | loose rivets and signs of shearing | | | | | | | | | and distorsion. | | | | | | | | |If you find damage: | | | | | | | | |(1) Examine panels and adjacent | | X | | | |
EFF : ALL 05-51-27 SROS
Page 604 Jul 01/05
R R
R R R
R R R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | structure for: | | | | | | | | | - buckles, tearing of plates at the| | | | | | | | | rivets, stringers attached to | | | | | | | | | panels, distorsion and wrinkles. | | | | | | | | |(2) Examine pylon main frame for: | | X | | | | | | | - distortion and condition of spars| | | | | | | | | and ribs attached to the side | | | | | | | | | panels. | | | | | | | | | If you find damage: | | | | | | | | | (a) Remove the engine | | | X | | | | | | (Ref. TASK 71-00-00-000-803). | | | | | | | | | (b) Examine the FWD and AFT | | | X | | | | | | attachments of the engine pylon| | | | | | | | | for: | | | | | | | | | - distortion and cracks. | | | | | | | | | (c) Remove the center panels of the| | | x | | | | | | pylon-to-wing fillet. | | | | | | | | | (d) Examine the pylon-to-wing | | | X | | | | | | attach fittings for: | | | | | | | | | - distortion and cracks. | | | | | | | | | (e) Install the engine | | | x | | | | | | (Ref. TASK 71-00-00-400-803). | | | | | | -------------------------------------------------------------------------------
R EFF : 001-049, 201-249, 251-252, 255-299, 05-51-27 301-399, 401-449, 451-499, SROS
Page 605 Jul 01/05
**ON A/C 701-749, Subtask 05-51-27-210-050-A A. Inspection of the Engine (Ref. TASK 71-00-00-000-805) (Ref. TASK 71-00-00-400-805)
R
R R R R R R R R R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Examine the cowl after a side impact | | | | | | | | |and damage only to the cowl. | | | | | | | | | | | | | | | | A.| |Externally examine the cowl fittings | X | | | | | | | |and the adjacent area of the pylon: | | | | | | | | |(1) Pylon side panels when damage on | | | | | | | | | thrust reverser or core cowl. | | | | | | | | |(2) Cantilever structure when damage on| | | | | | | | | inlet cowl, fan cowl or thrust | | | | | | | | | reverser for: | | | | | | | | | - damage. | | | | | | | | | | | | | | | |2. | |Examine the cowl after a side impact | | | | | | | | |and subsequent damage to the engine or | | | | | | | | |the equipment/accessories attached to | | | | | | | | |it for: | | | | | | | | |- damage. | | | | | | | | | | | | | | | | A.| |Examine pylon panels, doors and auxi- | X | | | | | | | |liary structure for distortion, | | | | | | | | |wrinkles, buckles, tearing of plates at| | | | | | | | |the rivets and stringers attached to | | | | | | | | |panels. | | | | | | | | | | | | | | | | B.| |Examine pylon main frame for: | X | | | | | | | |- cracks, cracked or flaking paint, | | | | | | | | | loose rivets and signs of shearing | | | | | | | | | and distortion. | | | | | | | | |If you find damage: | | | | | | | | |(1) Examine panels and adjacent | | X | | | | | | | structure for: | | | | | | | | | - buckles, tearing of plates at the| | | | | | | | | rivets, stringers attached to | | | | | | | | | panels, distortion and wrinkles. | | | | | | | | |(2) Examine pylon main frame for: | | X | | | |
EFF : 701-749, 05-51-27 SROS
Page 606 Jul 01/05
R R R
R R R
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - distortion and condition of spars| | | | | | | | | and ribs attached to the side | | | | | | | | | panels. | | | | | | | | | If you find damage: | | | | | | | | | (a) Remove the engine | | | X | | | | | | (Ref. TASK 71-00-00-000-805). | | | | | | | | | (b) Examine the FWD and AFT | | | X | | | | | | attachments of the engine pylon| | | | | | | | | for: | | | | | | | | | - distortion and cracks. | | | | | | | | | (c) Remove the center panels of the| | | x | | | | | | pylon-to-wing fillet. | | | | | | | | | (d) Examine the pylon-to-wing | | | X | | | | | | attach fittings for: | | | | | | | | | - distortion and cracks. | | | | | | | | | (e) Install the engine | | | x | | | | | | (Ref. TASK 71-00-00-400-805). | | | | | | ------------------------------------------------------------------------------**ON A/C ALL 5. Close-up ________
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**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-27-410-050 A. Close Access (1) Close the thrust reverser door (Ref. TASK 78-30-00-410-801).
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(a) FOR 4030EM1 417AL, 418AR
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(b) FOR 4030EM2 427AL, 428AR
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(2) Close the fan cowl doors (Ref. TASK 71-13-00-410-802).
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(a) FOR 4030EM1 415BL, 416BR
EFF : ALL 05-51-27 SROS
Page 607 Jul 01/05
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(b) FOR 4030EM2 425BL, 426BR (3) Close all the access panels opened during the inspection. **ON A/C 701-749, Subtask 05-51-27-410-050-A A. Close Access (1) Close the thrust reverser door (Ref. TASK 78-30-00-410-803). (a) FOR 4030EM1 417AL, 418AR (b) FOR 4030EM2 427AL, 428AR
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(2) Close the fan cowl doors (Ref. TASK 71-13-00-410-805). (a) FOR 4030EM1 415AL, 416AR (b) FOR 4030EM2 425AL, 426AR (3) Close all the access panels opened during the inspection. **ON A/C ALL Subtask 05-51-27-942-050 B. Put the Aircraft back to its Initial Configuration (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. (4) Make sure that the work area is clean and clear of tools and other items.
EFF : ALL 05-51-27 SROS
Page 608 Jul 01/05
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INSPECTION AFTER SPILLAGE - INSPECTION/CHECK ____________________________________________ TASK 05-51-28-200-801
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Inspection after Spillage 1. __________________ Reason for the Job
R Self Explanatory 2. ______________________ Job Set-up Information R R
A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R R R R
51-78-00-200-801 51-78-00-615-801 51-78-00-615-802 51-78-00-615-803 51-78-00-615-804
Inspection after Mercury Contamination Aircraft Cleaning after a Sewage Leakage Aircraft Cleaning after a Hydraulic Fluid Leakage Aircraft Cleaning after a Fish Shipment Aircraft Cleaning after an Acid or Alkali Leakage
3. __________ Job Set-up R Subtask 05-51-28-869-050 R R
A. Not applicable.
EFF : ALL 05-51-28 SROS
Page 601 Jul 01/05
4. Procedure _________ Subtask 05-51-28-210-050 R R R R R R R R R R R
A. Refer to the applicable procedure(s): - For aircraft cleaning after a sewage leakage (Ref. TASK 51-78-00-615801). - For aircraft cleaning after a hydraulic fluid leakage (Ref. TASK 51-7800-615-802). - For aircraft cleaning after leakage from a fish shipment (Ref. TASK 5178-00-615-803). - For aircraft cleaning after an acid or alkali leakage (Ref. TASK 51-7800-615-804). - For inspection after mercury spillage (Ref. TASK 51-78-00-200-801).
EFF : ALL 05-51-28 SROS
Page 602 Jul 01/05
INSPECTION AFTER ABNORMAL PAX/CREW DOOR MOVEMENT - INSPECTION/CHECK ___________________________________________________________________ TASK 05-51-29-200-801 Inspection after Abnormal Pax/Crew Door Movement. WARNING : BEFORE YOU START WORK ON THE DOOR MAKE SURE THAT: _______ - THE EMERGENCY CONTROL HANDLE IS IN THE DISARMED POSITION WITH THE SAFETY PIN INSTALLED. - THE PERCUSSION LEVER OF THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER IS IN THE DISARMED POSITION WITH THE SAFETY PIN INSTALLED. THIS MAKES SURE THAT THE DOOR DOES NOT OPEN SUDDENLY. IF THE DOOR OPENS SUDDENLY IT CAN CAUSE INJURY AND/OR DAMAGE. 1. __________________ Reason for the Job You must do this inspection in case of abnormal pax/crew door movement like lifting or pushing down by a loader or a jetway. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
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No specific No specific 98A52108008001 98F52108431000
circuit breaker(s) safety clip(s) adjustable access platform 5.50 m (18 ft. 1 in.) 1 SUPPORT FRAME - BALLAST WEIGHT, DOORS 1 BALLAST WEIGHT - SLIDE RAFT
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-42-00-861-801 24-42-00-862-801 25-23-45-000-801 25-23-45-400-801 25-23-46-000-801
Energize the Ground Service Network De-energize the Ground Service Network Removal of the Door Frame Linings of the FWD Passenger/Crew Door Installation of the Door Frame Linings of the FWD Passenger/Crew Door Removal of the Door Frame Linings of the MID Passenger/Crew Door
EFF : ALL 05-51-29 SROS
Page 601 Oct 01/03
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------25-23-46-400-801 25-23-47-000-801 25-23-47-400-801 R R
25-23-49-000-801 25-23-49-400-801
R R R
25-23-51-000-801 25-23-51-400-801
R 25-23-52-000-802 25-23-52-400-802 R R
25-62-41-000-801 25-62-41-400-801 52-10-00-010-801 52-10-00-410-801 52-10-00-860-801 52-10-00-860-802 52-11-12-000-801 52-11-12-000-802 52-11-12-400-801 52-11-12-400-802 52-11-22-000-801 52-11-22-400-801 52-11-31-000-801 52-11-31-400-801
R R
52-12-00-720-801
Installation of the Door Frame Linings of the MID Passenger/Crew Door Removal of the Door Frame Linings of the AFT Passenger/Crew Door Installation of the Door Frame Linings of the AFT Passenger/Crew Door Removal of the Lining of the FWD Passenger/Crew Door(s) Installation of the Lining of the FWD Passenger/Crew Door(s) Removal of the Lining of the MID Passenger/Crew Door(s) Installation of the Lining of the MID Passenger/Crew Door(s) Removal of the Lining of the AFT Passenger/Crew Door Installation of the Lining of the AFT Passenger/Crew Door Escape Facilities - Removal Escape Facilities - Installation Opening of the Passenger/Crew Door Closing of the Passenger/Crew Door Special Precautions before Work on the Passenger/Crew Door Special Precautions after Work on the Passenger/Crew Door Removal of the Door Support Arm, Door Buffer and Door Stay Mechanism. Removal of the Upper and Lower Guide Arms and the Guide Arm Hinge-Fittings. Installation of the Door Support Arm, Door buffer and Door Stay Mechanism. Installation of the Upper and Lower Guide Arms and the Guide Arm Hinge-Fittings. Removal of the Emergency Escape Slide Release Mechanism- FWD Passenger/Crew Door (831) (841) Installation of the Emergency Escape Slide MechanismFWD Passenger/Crew Door (831) (841) Removal of the Forward Passenger/Crew Door Latch and Stop Fittings Installation of the Forward Passenger/Crew Door Latch and Stop Fittings Functional Test of the MID Passenger/Crew Door (Door 2L/2R)
EFF : ALL 05-51-29 SROS
Page 602 Oct 01/03
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R R
52-12-00-820-801 52-12-12-000-801
R 52-12-12-400-801 R 52-12-21-000-801 R 52-12-21-400-801 R 52-12-22-000-801 R 52-12-22-400-801 R R R
52-12-31-000-801 52-12-31-400-801
R R R R R
52-13-00-720-801 52-13-00-820-801 52-13-12-000-801
R 52-13-12-400-801 R 52-13-21-000-801 R 52-13-21-400-801 R 52-13-22-000-801 R 52-13-22-400-801 R R R
52-13-31-000-801 52-13-31-400-801
R SRM
Adjustment of the MID Passenger/Crew Door (Door 2L/2R) Removal of the Suspension of the MID Passenger/Crew Door (Door 2L/2R) Installation of the Suspension of the MID Passenger/Crew Door (Door 2L/2R) Removal of the Door Locking Mechanism from the MID Passenger/Crew Door (Door 2L/2R) Installation of the Door Locking Mechanism in the MID Passenger/Crew Door (Door 2L/2R) Removal of the Emergency Escape-Slide Release-Mechanism from the MID Passenger/Crew Door (Door 2L/2R) Installation of the Emergency Escape-Slide Release-Mechanism in the MID Passenger/Crew Door (Door 2L/2R) Removal of the Door, Latch and Stop Fittings (Door 2L/2R) Installation of the Door, Latch and Stop Fittings (Door 2L/2R) Functional Test of the AFT Passenger/Crew Door (Door 4L/4R) Adjustment of the AFT Passenger/Crew Door (Door 4L/4R) Removal of the Suspension of the AFT Passenger/Crew Door (Door 4L/4R) Installation of the Suspension of the AFT Passenger/Crew Door (Door 4L/4R) Removal of the Door Locking Mechanism from the AFT Passenger/Crew Door (Door 4L/4R) Installation of the Door Locking Mechanism in the AFT Passenger/Crew Door (Door 4L/4R) Removal of the Emergency Escape-Slide Release-Mechanism from the AFT Passenger/Crew Door (Door 4L/4R) Installation of the Emergency Escape-Slide Release-Mechanism in the AFT Passenger/Crew Door (Door 4L/4R) Removal of the Door Latch and Stop Fittings (Door 4L/4R) Installation of the Door Latch and Stop Fittings (Door 4L/4R)
521000
EFF : ALL 05-51-29 SROS
Page 603 Oct 01/03
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------SRM 530000 05-51-29-991-001 05-51-29-991-002 05-51-29-991-003
Fig. 601 Fig. 602 Fig. 603
3. __________ Job Set-up Subtask 05-51-29-010-050 A. Get Access (1) Energize the aircraft electrical circuits (Ref. TASK 24-42-00-861-801). (2) Put an adjustable access platform in position at the doors 831, 841, 832, 842, 833, 843. (3) Open the passenger/crew doors 831, 841, 832, 842, 833, 843, (Ref. TASK 52-10-00-010-801). Subtask 05-51-29-010-051 B. Get Access to the Avionics Compartment (1) Open the access door 211FF. (2) Set the AVNCS LT switch 1LS to ON. Subtask 05-51-29-865-050 C. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------721VU DOORS & SLIDES CTL 3MJ N09 722VU DOORS & SLIDES CTL 2MJ P41
EFF : ALL 05-51-29 R SROS
Page 604 Oct 01/03
Subtask 05-51-29-860-050 D. Aircraft Maintenance Configuration (1) Observe the special precautions before you start work on the door (Ref. TASK 52-10-00-860-801). (2) Remove the escape slide/raft container (Ref. TASK 25-62-41-000-801). (3) Remove the door frame linings (Ref. TASK 25-23-45-000-801), (Ref. TASK 25-23-46-000-801), (Ref. TASK 25-23-47-000-801). (4) Remove the door lining and insulation (Ref. TASK 25-23-49-000-801), (Ref. TASK 25-23-51-000-801), (Ref. TASK 25-23-52-000-802). (5) Install the SUPPORT FRAME - BALLAST WEIGHT, DOORS (98A52108008001) together with the BALLAST WEIGHT - SLIDE RAFT (98F52108431000) to replace the escape slide and the lining.
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4. Procedure _________ Subtask 05-51-29-210-050 A. Inspection of the Doors (Ref. TASK 52-11-12-000-801), (Ref. TASK 52-1112-400-801) (Ref. TASK 52-11-12-000-802), (Ref. TASK 52-11-12-400-802), (Ref. TASK 52-12-12-000-801), (Ref. TASK 52-12-12-400-801), (Ref. TASK 52-13-12-000801), (Ref. TASK 52-13-12-400-801). (Ref. TASK 52-11-22-000-801) (Ref. TASK 52-11-22-400-801) (Ref. TASK 5212-22-000-801), (Ref. TASK 52-12-22-400-801), (Ref. TASK 52-13-22-000801), (Ref. TASK 52-13-22-400-801). (Ref. TASK 52-12-21-000-801), (Ref. TASK 52-12-21-400-801), (Ref. TASK 52-13-21-000-801), (Ref. TASK 52-13-21-400-801), (Ref. TASK 52-11-31-000801), (Ref. TASK 52-11-31-400-801). (Ref. TASK 52-12-31-000-801), (Ref. TASK 52-12-31-400-801), (Ref. TASK 52-13-31-000-801), (Ref. TASK 52-13-31-400-801), (Ref. SRM 521000), (Ref. SRM 530000). (Ref. Fig. 601/TASK 05-51-29-991-001, 602/TASK 05-51-29-991-002, 603/TASK 05-51-29-991-003) NOTE : All the necessary inspections are visual unless specified ____ differently in the text. Operators can refer to the Non-destructive Testing Manual (NTM) and use non-destructive test procedures.
EFF : ALL 05-51-29 SROS
Page 605 Oct 01/03
Fwd Passenger/Crew Doors Figure 601/TASK 05-51-29-991-001 EFF : ALL 05-51-29 SROS
Page 606 Apr 01/98
Mid Passenger/Crew Doors Figure 602/TASK 05-51-29-991-002 EFF : ALL 05-51-29 SROS
Page 607 Apr 01/98
Aft Passenger/Crew Doors Figure 603/TASK 05-51-29-991-003 EFF : ALL 05-51-29 SROS
Page 608 Apr 01/98
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Pax/Crew Door Open | | | | | | | | | (Ref. Fig. 601/TASK 05-51-29-991-001) | | | | | | | | | (Ref. Fig. 602/TASK 05-51-29-991-002) | | | | | | | | | (Ref. Fig. 603/TASK 05-51-29-991-003) | | | | | | | A.| | Examine the door skin, door structure | X | | | | | | | | and the fuselage structure for | | | | | | | | | distortion, cracks, tears and loose or| | | | | | | | | missing rivets. | | | | | | | | | If you find damage: | | X | | | | | | | (1) Do a structural repair at the | | | | | | | | | door and (or) the fuselage | | | | | | | | | structure | | | | | | | | | (Ref. SRM 52-10-00). | | | | | | | | | | | | | | | | B.| | Examine the door suspension for | X | | | | | | | | damage. | | | | | | | | | If you find damage: | | X | | | | | | | (1) Remove the damaged components | | | | | | | | | (Ref. TASK 52-11-12-000-801) | | | | | | | | | (Ref. TASK 52-11-12-000-802) | | | | | | | | | (Ref. TASK 52-12-12-000-801) | | | | | | | | | (Ref. TASK 52-13-12-000-801) | | | | | | | | | and install a new component | | | | | | | | | (Ref. TASK 52-11-12-400-801) | | | | | | | | | (Ref. TASK 52-11-12-400-802) | | | | | | | | | (Ref. TASK 52-12-12-400-801) | | | | | | | | | (Ref. TASK 52-13-12-400-801). | | | | | | | | | | | | | | | |2. | | Inspection of the Pax/Crew Door in | | | | | | | | | the Up and Closed Position | | | | | | | | | | | | | | | | A.| | Examine the door skin, door structure | X | | | | | | | | and the fuselage structure for | | | | | | | | | distortion, cracks, tears and loose or| | | | | | | | | missing rivets. | | | | | | | | | If you find damage: | | X | | | | | | | (1) Do a structural repair of the | | | | | | | | | door and (or) the fuselage | | | | | | | | | structure | | | | | | | | | (Ref. SRM 52-10-00) | | | | | | | | | (Ref. SRM 53-00-00). | | | | | | | | | | | | | | | | B.| | Examine the locking mechanism for | X | | | | |
EFF : ALL 05-51-29 R SROS
Page 609 Oct 01/03
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | damage. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the damaged component | | X | | | | | | | (Ref. TASK 52-12-21-000-801) | | | | | | | | | (Ref. TASK 52-13-21-000-801) | | | | | | | | | and install a new component | | | | | | | | | (Ref. TASK 52-12-21-400-801) | | | | | | | | | (Ref. TASK 52-13-21-400-801). | | | | | | | | | | | | | | | | C.| | Examine the emergency escape slide | X | | | | | | | | release mechanism for damage. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the damaged component | | X | | | | | | | (Ref. TASK 52-11-22-000-801) | | | | | | | | | (Ref. TASK 52-12-22-000-801) | | | | | | | | | (Ref. TASK 52-13-22-000-801) | | | | | | | | | and install a new component | | | | | | | | | (Ref. TASK 52-11-22-400-801) | | | | | | | | | (Ref. TASK 52-12-22-400-801) | | | | | | | | | (Ref. TASK 52-13-22-400-801). | | | | | | | | | | | | | | | | D.| | Examine the door support mechanism | X | | | | | | | | for damage. | | | | | | | | | If you find damage: | X | | | | | | | | (1) Remove the damaged component | | | | | | | | | (Ref. TASK 52-11-12-000-801) | | | | | | | | | (Ref. TASK 52-12-12-000-801) | | | | | | | | | (Ref. TASK 52-13-12-000-801) | | | | | | | | | and install a new component | | | | | | | | | (Ref. TASK 52-11-12-400-801) | | | | | | | | | (Ref. TASK 52-12-12-400-801) | | | | | | | | | (Ref. TASK 52-13-12-400-801). | | | | | | | | | | | | | | | | E.| | Examine the fittings for damage. | X | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the damaged component | | | | | | | | | (Ref. TASK 52-11-31-000-801) | | | | | | | | | (Ref. TASK 52-12-31-000-801) | | | | | | | | | (Ref. TASK 52-13-31-000-801) | | | | | | | | | and install a new component | | | | | | | | | (Ref. TASK 52-11-31-400-801) | | | | | | | | | (Ref. TASK 52-12-31-400-801) | | | | | | | | | (Ref. TASK 52-13-31-400-801). | | | | | |
EFF : ALL 05-51-29 R SROS
Page 610 Oct 01/03
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| ------------------------------------------------------------------------------Subtask 05-51-29-710-050 B. Adjustment/Test of the Doors (Ref. TASK 52-12-00-720-801) (Ref. TASK 5212-00-820-801) (Ref. TASK 52-13-00-720-801) (Ref. TASK 52-13-00-820-801) (1) Make sure that the work area is clean and clear of tools and other items. (2) Do the test below: ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Do the adjustment/test of the pax/crew| | X | | | | | | | door | | | | | | | | | (Ref. TASK 52-12-00-720-801) | | | | | | | | | (Ref. TASK 52-12-00-820-801) | | | | | | | | | (Ref. TASK 52-13-00-720-801) | | | | | | | | | (Ref. TASK 52-13-00-820-801). | | | | | | ------------------------------------------------------------------------------5. Close-up ________ Subtask 05-51-29-860-051 A. Put the Aircraft back to its Initial Configuration R
(1) Remove the BALLAST WEIGHT - SLIDE RAFT (98F52108431000) and the SUPPORT FRAME - BALLAST WEIGHT, DOORS (98A52108008001). (2) Install the door lining and insulation (Ref. TASK 25-23-49-400-801), (Ref. TASK 25-23-51-400-801), (Ref. TASK 25-23-52-400-802). (3) Install the door frame linings (Ref. TASK 25-23-45-400-801), (Ref. TASK 25-23-46-400-801), (Ref. TASK 25-23-47-400-801). (4) Install the escape slide (escape slide raft) container (Ref. TASK 2562-41-400-801).
EFF : ALL 05-51-29 SROS
Page 611 Oct 01/03
(5) Observe the special precautions after work on the door (Ref. TASK 5210-00-860-802). Subtask 05-51-29-865-051 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 2MJ, 3MJ Subtask 05-51-29-862-050 C. De-energize the ground service network (Ref. TASK 24-42-00-862-801). Subtask 05-51-29-942-050 D. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Set the AVNCS LT switch 1LS to off. (3) Close the access door 211FF. (4) Close the passenger/crew doors. (Ref. TASK 52-10-00-410-801) (5) Remove the access platform(s).
EFF : ALL 05-51-29 R SROS
Page 612 Oct 01/03
______________________________________________________________________ INSPECTION AFTER ENGINE WINDMILLING (AFTER ENGINE IN-FLIGHT SHUT-DOWN) ________________ INSPECTION/CHECK TASK 05-51-34-200-802 Inspection after Engine Windmilling (after Engine In-Flight Shut-Down) 1. __________________ Reason for the Job Self Explanatory 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------71-00-00-200-812 72-00-00-200-810
Examine the Power Plant after it has been stopped in Flight Inspection After Windmilling
3. __________ Job Set-up Subtask 05-51-34-860-051 A. Not applicable. 4. Procedure _________ R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-34-210-051 A. Do the inspection after windmilling (Ref. TASK 72-00-00-200-810) **ON A/C 701-749, Subtask 05-51-34-210-051-A A. Do the procedure to examine the power plant after it has been stopped in flight (Ref. TASK 71-00-00-200-812)
EFF : ALL 05-51-34 SROS
Page 601 Jul 01/05
INSPECTION AFTER VERY HIGH WINDS ON GROUND - INSPECTION/CHECK _____________________________________________________________ TASK 05-51-42-200-801 Inspection after Very High Winds on Ground WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A _______ FALL CAN KILL OR INJURE YOU. 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
warning notices adjustable access platform 11 m (36 ft. 1 in.)
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------24-41-00-862-801 27-24-00-710-802 27-34-00-710-801 27-50-00-866-801 27-54-00-710-801 27-60-00-866-801 27-64-00-710-801
De-energize the Aircraft Electrical Circuits from the External Power A Operational Test of the Rudder Hydraulic Actuation Operational Test of the Elevator and Hydraulic Actuation Extension of the Flaps on the Ground Operational Test of the Flap System Extension of the Spoilers for Maintenance Operational Test of the Spoilers
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Page 601 Apr 01/01
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------R
27-80-00-866-801 27-80-00-866-801 27-84-00-710-801 29-00-00-864-804 32-00-00-481-801 32-12-00-010-801 32-12-00-410-801 32-22-00-010-801 32-22-00-410-801 55-16-00-200-803 55-26-00-200-801 55-26-00-200-802 55-30-00-210-806
Extension of the Slats on the Ground Extension of the Slats on the Ground Operational Test of the Slat System 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 Open the NLG Doors for Maintenance Close the NLG Doors after Maintenance Detailed Inspection of Horizontal Stabilizer Hinge Fittings No 1, 4, 5, 6 and 7 and Support Ribs Detailed Inspection of Elevator Hinge Fittings No 2 and 3 and Actuator Fittings, LH and RH Detailed Inspection of Elevator Hinge Fittings No 1, 4, 5, 6 and 7 Detailed Visual Inspection of the Rudder Hinge Arms and Actuator Support Fittings
3. __________ Job Set-up Subtask 05-51-42-941-050 A. General (1) You must do this inspection if the aircraft was in very high winds on the ground (wind speed of more than 80 knots (150 KM/H)). NOTE : This procedure is for an aircraft that was in the moored ____ configuration before it was in very high winds. Subtask 05-51-42-481-050 B. Safety Precautions Make sure that the safety devices are installed on the landing gears (Ref. TASK 32-00-00-481-801).
EFF : ALL 05-51-42 SROS
Page 602 Jan 01/07
R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-42-866-050 C. Extension of the Flight Control Surfaces (1) Extend the flaps (Ref. TASK 27-50-00-866-801). (2) Extend the slats (Ref. TASK 27-80-00-866-801). (3) Extend the spoilers (Ref. TASK 27-60-00-866-801).
R
**ON A/C 701-749,
R
Subtask 05-51-42-866-050-A
R
C. Extension of the Flight Control Surfaces
R
(1) Extend the flaps (Ref. TASK 27-50-00-866-801).
R
(2) Extend the slats (Ref. TASK 27-80-00-866-801).
R
(3) Extend the spoilers (Ref. TASK 27-60-00-866-801).
R
**ON A/C ALL Subtask 05-51-42-010-050 D. Get Access (1) Open the main gear doors and install the safety devices (Ref. TASK 32-12-00-010-801). (2) Open the nose gear doors and install the safety devices (Ref. TASK 32-22-00-010-801). Subtask 05-51-42-860-050 E. Aircraft Maintenance Configuration (1) Make sure that the electrical circuits are de-energized (Ref. TASK 24-41-00-862-801). (2) Make sure that the hydraulic systems are depressurized (Ref. TASK 2900-00-864-804). (3) Put warning notices in the cockpit to tell persons not to operate the flight control surfaces.
EFF : ALL 05-51-42 SROS
Page 603 Jan 01/07
(4) Put the adjustable access platform in position near the area you must examine. 4. Procedure _________ Subtask 05-51-42-210-050 A. General External Inspection ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | General External Inspection | | | | | | | | | | | | | | | | A.| | Do a general visual inspection of the | X | | | | | | | | aircraft from the ground for | | | | | | | | | distortion, damage and fluid leakage | | | | | | ------------------------------------------------------------------------------Subtask 05-51-42-210-051 B. Inspection of the Landing Gear ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Landing Gear | | | | | | | | | | | | | | | | A.| | Nose Landing Gear | | | | | | | | | | | | | | | | | | (1) Examine the NLG, its attachment | X | | | | | | | | fittings on the structure and all | | | | | | | | | the components installed on the | | | | | | | | | NLG for: | | | | | | | | | - distortion, | | | | | | | | | - leakage, | | | | | | | | | - defective attachment, | | | | | | | | | - other damage. | | | | | | | | | NOTE: Carefully examine the | | | | | | | | | hydraulic and electrical | | | | | | | | | connections and the mooring | | | | | | | | | fitting. | | | | | | | | | | | | | | | | B.| | Main Landing Gear | | | | | | | | | | | | | | | | | | (1) Examine the MLG, its attachment | X | | | | | | | | fittings on structure, the side | | | | | | | | | stay, the forward and aft pintle | | | | | |
EFF : ALL 05-51-42 R SROS
Page 604 Jan 01/07
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | fittings and all the components | | | | | | | | | installed on the MLG for: | | | | | | | | | - distortion, | | | | | | | | | - leakage, | | | | | | | | | - defective attachment, | | | | | | | | | - other damage. | | | | | | | | | NOTE: Carefully examine the | | | | | | | | | hydraulic and electrical | | | | | | | | | connections. | | | | | | ------------------------------------------------------------------------------Subtask 05-51-42-210-052
R
C. Inspection (Ref. TASK (Ref. TASK (Ref. TASK (Ref. TASK
of the Flight Control Surfaces (Ref. TASK 55-16-00-200-803) 55-26-00-200-801) (Ref. TASK 55-26-00-200-802) 55-30-00-210-806) (Ref. TASK 27-24-00-710-802) 27-34-00-710-801) (Ref. TASK 27-54-00-710-801) 27-64-00-710-801) (Ref. TASK 27-84-00-710-801)
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Flight Control | | | | | | | | | Surfaces | | | | | | | | | | | | | | | | A.| | Rudder | | | | | | | | | | | | | | | | | | (1) Examine the rudder external | X | | | | | | | | surface for distortion and damage | | | | | | | | | | | | | | | | | | (2) Do a detailed visual inspection | X | | | | | | | | (Ref. TASK 55-30-00-210-806) | | | | | | | | | of the actuator fittings 1, 2 and | | | | | | | | | 3 at: | | | | | | | | | - the vertical stabilizer | | | | | | | | | center-box, | | | | | | | | | - the rudder front spar. | | | | | | | | | NOTE: Carefully examine the | | | | | | | | | actuator fitting lugs and | | | | | | | | | the areas of the fitting | | | | | | | | | around the fasteners. | | | | | | | | | | | | | | |
EFF : ALL 05-51-42 SROS
Page 605 Jul 01/06
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | B.| | Elevators | | | | | | | | | | | | | | | | | | (1) Examine the elevator external | X | | | | | | | | surface for distortion and damage | | | | | | | | | | | | | | | | | | (2) Do a detailed visual inspection | X | | | | | | | | (Ref. TASK 55-16-00-200-803) | | | | | | | | | (Ref. TASK 55-26-00-200-801) | | | | | | | | | (Ref. TASK 55-26-00-200-802) of | | | | | | | | | these parts in the actuator areas:| | | | | | | | | - the actuator fittings 1 and 2 | | | | | | | | | and their attachments, | | | | | | | | | - the hinge fittings 2, 3 and 4 | | | | | | | | | and their attachments, | | | | | | | | | - the hinge arms 2, 3 and 4 and | | | | | | | | | their attachments | | | | | | | | | at the horizontal stabilizer | | | | | | | | | rear-spar and at the elevator | | | | | | | | | front spar. | | | | | | | | | | | | | | | | C.| | Flaps | | | | | | | | | | | | | | | | | | (1) Do a general visual inspection of | X | | | | | | | | each control surface and its | | | | | | | | | attachments for distortion and | | | | | | | | | damage. | | | | | | | | | | | | | | | | | | (2) Do a visual inspection of: | X | | | | | | | | - the flap track fairings, | | | | | | | | | for distortion and damage. | | | | | | | | | | | | | | | | | | (1) Examine the external surface and | X | | | | | | | | the attachments of each control | | | | | | | | | surface for distortion and damage.| | | | | | | | | | | | | | | |2. | | Operational Test of the Flight Control| | | | | | | | | Surfaces | | | | | | | | | | | | | | | | A.| | Make sure that the work area is clean | X | | | | | | | | and clear of tool(s) and other items. | | | | | | | | | | | | | | | | B.| | Do an operational test of each control| X | | | | | | | | surface and make sure that the related| | | | | |
EFF : ALL 05-51-42 SROS
Page 606 Apr 01/01
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | surface(s) move(s) smoothly and freely| | | | | | | | | | | | | | | | | | (1) For the rudder: | | | | | | | | | (Ref. TASK 27-24-00-710-802) | | | | | | | | | | | | | | | | | | (2) For the elevators: | | | | | | | | | (Ref. TASK 27-34-00-710-801) | | | | | | | | | | | | | | | | | | (3) For the flaps: | | | | | | | | | (Ref. TASK 27-54-00-710-801) | | | | | | | | | | | | | | | | | | (4) For the slats: | | | | | | | | | (Ref. TASK 27-84-00-710-801) | | | | | | | | | | | | | | | | | | (5) For the spoilers: | | | | | | | | | (Ref. TASK 27-64-00-710-801) | | | | | | ------------------------------------------------------------------------------5. Close-up ________ Subtask 05-51-42-410-050 A. Close Access (1) Make sure that the work area is clean and clear of tools and other items. (2) Close the nose gear doors (Ref. TASK 32-22-00-410-801). (3) Close the main gear doors (Ref. TASK 32-12-00-410-801). (4) Remove the access platform(s). (5) Remove the warning notice(s).
EFF : ALL 05-51-42 SROS
Page 607 Apr 01/01
INSPECTIONS AFTER WORK ON SYSTEM ELECTRICAL INSTALLATION - ADJUSTMENT/TEST __________________________________________________________________________ TASK 05-51-43-700-801 Inspection after Work on System Electrical Installation 1. __________________ Reason for the Job R
To give the list of all the inspections to do after work on the aircraft electrical installation (wiring, connectors, etc.). The purpose of this integrity inspection is not to do a check of all the aircraft functions but to make sure that: - basic functions of the aircraft systems operate correctly - there are no unwanted effects on the main functions of systems not directly related to the work done. 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------22-10-00-710-803 22-30-00-710-801 22-96-00-740-801 22-97-00-740-801 24-00-00-710-801 24-24-00-710-801 24-29-00-740-801 24-38-00-740-801 24-41-00-740-803 24-41-00-861-801 26-12-00-710-812 27-54-00-710-802 27-96-00-710-818 29-00-00-710-802 34-13-00-710-803 34-13-00-740-801 34-13-00-740-802 34-13-00-740-803
Operational Test of Autopilot Engagement and Locking Devices of The Side Stick Controller and Rudder Pedals Operational Test of the Autothrust Isolation from Engine Control BITE Test of the Auto Flight System (SYSTEM TEST) Test of the LAND CAT III Capability Integrity Test of the Electrical Power Operational Test of the Emergency Generation System BITE Test of the ECMU (1XM1, 1XM2) BITE Test of the BCL (1PB1, 1PB2, 1PB3) Ground Report of the EPGS Energize the Aircraft Electrical Circuits from the External Power A Operational Test of the Engine Fire and Overheat Detection (Loop/Squib) Operational Test of the Flap and Slat System Integrity Test of the Flight Control System Integrity Test of the Hydraulic Power AOA SENSOR TEST INTERFACE TEST of the ADR Read the CMC for the ADR CURRENT STATUS SYSTEM TEST of the ADR
EFF : ALL 05-51-43 SROS
Page 501 Jan 01/06
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------34-13-00-740-804 34-14-00-740-801 34-14-00-740-802 34-14-00-740-803 34-14-00-740-804 71-00-00-720-817 71-00-00-720-827 73-21-00-710-803 73-21-00-710-812 73-25-34-740-820 73-25-34-740-823 74-00-00-710-803 74-00-00-710-804 78-31-00-710-804 78-31-00-740-802
Read the CMC for the ADR INPUT STATUS INTERFACE TEST of the IR Read the CMC for the IR CURRENT STATUS SYSTEM TEST of the IR Read the CMC for the IR INPUT STATUS Test No. 2A - Engine Motor Leak Test (Wet Method) Thrust Reverser Cowl Doors Open Wet Motoring Engine Full Authority Digital Engine Control (FADEC) System Static Test Test of the FADEC System Bite Test of the EIVMU BITE Test of the EIVMU Operational Test of the Ignition System (Audible Check) Audible Test of the Igniters Thrust Reverser Cycling Test (MCDU) Test of the Thrust Reverser Deployment and Stowage (Engine not Running)
3. __________ Job Set-up Subtask 05-51-43-200-050 A. Not applicable. 4. Procedure _________ Subtask 05-51-43-710-050 R
A. Inspections of the basic Functions of the Aircraft Systems
R R
(1) Do these inspections to make sure that the basic functions of the auto flight system operate correctly: (a) Operational test of autopilot engagement and locking devices of the side stick controller and rudder (Ref. TASK 22-10-00-710803). (b) Operational test of the autothrust isolation from engine control (Ref. TASK 22-30-00-710-801).
EFF : ALL 05-51-43 SROS
Page 502 Oct 01/04
(c) BITE test of the auto flight system (SYSTEM TEST) (Ref. TASK 2296-00-740-801). (d) Test of the LAND CAT III capability (Ref. TASK 22-97-00-740-801). R R
(2) Do these inspections to make sure that the basic functions of the electrical power system operate correctly: (a) Integrity test of the electrical power (Ref. TASK 24-00-00-710801). (b) Operational test of the emergency generation system (Ref. TASK 24-24-00-710-801). (c) BITE test of the ECMU (1XM1, 1XM2) (Ref. TASK 24-29-00-740-801). (d) BITE test of the BCL (1PB1, 1PB2, 1PB3) (Ref. TASK 24-38-00-740801). (e) Ground report of the EPGS (Ref. TASK 24-41-00-740-803). (f) Energize the aircraft electrical circuits from the external power A (Ref. TASK 24-41-00-861-801).
R R
(3) Do this inspection to make sure that the basic functions of the fire protection system operate correctly: (a) Operational test of the engine fire and overheat detection (Loop/Squib) (Ref. TASK 26-12-00-710-812).
R R
(4) Do these inspections to make sure that the basic functions of the flight controls system operate correctly: (a) Integrity test of the flight control system (Ref. TASK 27-96-00710-818). (b) Operational test of the flap and slat system (Ref. TASK 27-54-00710-802).
R R
(5) Do this inspection to make sure that the basic functions of the hydraulic power operate correctly: (a) Integrity test of the hydraulic power (Ref. TASK 29-00-00-710802).
EFF : ALL 05-51-43 SROS
Page 503 Oct 01/04
(6) Do these inspections to make sure that the basic functions of the navigation system operate correctly: (a) AOA sensor test (Ref. TASK 34-13-00-710-803). (b) Interface test of the ADR (Ref. TASK 34-13-00-740-801). (c) Read the CMC for the ADR CURRENT STATUS (for Litton ADIRU) (Ref. TASK 34-13-00-740-802). (d) System test of the ADR (Ref. TASK 34-13-00-740-803). (e) Read the CMC for the ADR INPUT STATUS (for Honeywell ADIRU) (Ref. TASK 34-13-00-740-804). (f) Interface test of the IR (Ref. TASK 34-14-00-740-801). (g) Read the CMC for the IR CURRENT STATUS (for Litton ADIRU) (Ref. TASK 34-14-00-740-802). (h) System test of the IR (Ref. TASK 34-14-00-740-803). (i) Read the CMC for the IR INPUT STATUS (for Honeywell ADIRU) (Ref. TASK 34-14-00-740-804). R
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-43-710-051 B. Inspections of the basic Engine Functions (1) Thrust reverser cycling test (MCDU) (Ref. TASK 78-31-00-710-804). (2) Operational test of the ignition system (Audible Check) (Ref. TASK 74-00-00-710-803). (3) Engine motor leak test (Wet Method) - Thrust reverser cowl doors open (Ref. TASK 71-00-00-720-817). (4) BITE test of the EIVMU (Ref. TASK 73-25-34-740-823). (5) Full Authority Digital Engine Control (FADEC) system static test (Ref. TASK 73-21-00-710-803).
EFF : ALL 05-51-43 SROS
Page 504 Jul 01/05
**ON A/C 701-749, Subtask 05-51-43-710-051-A R
B. Inspections of the basic Engine Functions (1) Test of the thrust reverser deployment and stowage (engine not running) (Ref. TASK 78-31-00-740-802). (2) Audible test of the igniters (Ref. TASK 74-00-00-710-804). (3) Wet motoring engine (Ref. TASK 71-00-00-720-827). (4) BITE test of the EIVMU (Ref. TASK 73-25-34-740-820). (5) Test of the FADEC system (Ref. TASK 73-21-00-710-812).
EFF : 701-749, 05-51-43 SROS
Page 505 Oct 01/04
INSPECTION AFTER FLIGHT WITH HIGH LATERAL LOADS - INSPECTION/CHECK __________________________________________________________________ TASK 05-51-44-200-801 INSPECTION AFTER FLIGHT WITH HIGH LATERAL LOADS 1. __________________ Reason for the Job To do an inspection of the aircraft for structural damage after a flight during which high lateral loads occurred. NOTE : Typical examples of conditions that can cause high lateral load ____ factors are: - loss of control involving yaw and/or roll maneuvers, - severe turbulence with A.P. disconnection or in manual mode, - system failures such as rudder trim runaway with crew take over, - etc. NOTE : If the lateral acceleration occurred when the aircraft was on the ____ ground (landing, taxiing, etc.), it is not necessary to do this procedure. To know if the inspection is necessary, refer to Para. 3.A. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No No No No
specific specific specific specific
safety barriers warning notices wheel chocks 1 ACCESS PLATFORM 17M (56 FT) - ADJUSTABLE
EFF : ALL 05-51-44 SROS
Page 601 Jul 01/06
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------05-23-20-200-804 05-51-17-200-801 24-41-00-861-801 24-41-00-862-801 27-14-00-710-801 27-14-00-820-801 27-24-00-710-801 27-34-00-710-801 27-50-00-866-801 27-54-00-710-801 27-64-00-710-801 27-84-00-710-801 28-25-00-650-803 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 32-00-00-481-801 32-12-00-010-801 32-12-00-410-801 53-15-11-010-801 53-15-11-400-801 53-15-11-700-801 55-34-11-000-801 55-34-11-400-801 71-00-51-000-801
Zonal Inspection of Vertical Stabilizer Spar Box Inspection after Flight in Excessive Turbulence or in Excess of VMO/MMO Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Operational Test of the Aileron and Hydraulic Actuation Adjustment of the Aileron Operational Test of the Rudder Servo Control with each Hydraulic System Operational Test of the Elevator and Hydraulic Actuation Extension of the Flaps on the Ground Operational Test of the Flap System Operational Test of the Spoilers Operational Test of the Slat System To Drain the Remaining Fuel (Wing Tanks) 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) Installation of the Safety Devices on the Landing Gears Open the MLG Doors for Maintenance Close the MLG Doors after Maintenance Opening of the Radome Installation of the Radome Tap Test of the Radome Removal of the Vertical Stabilizer Tip Installation of the Vertical Stabilizer Tip Removal of the Demountable Power Plant
EFF : ALL 05-51-44 SROS
Page 602 Jul 01/06
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------71-13-00-010-802 71-13-00-010-805 71-13-00-410-802 71-13-00-410-805 78-30-00-010-801 78-30-00-010-803 78-30-00-410-801 78-30-00-410-803 78-31-00-710-804 78-31-00-740-802 05-51-44-991-001 05-51-44-991-002 05-51-44-991-003
Opening of the Aft Fan Cowl Doors (5110EA) and (5120EA) Open the Fan Cowl Doors Closing of the Aft Fan Cowl Doors (5110EA) and (5120EA) Close the Fan Cowl Doors Opening of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Open the Thrust Reverser Cowl Doors Closing of the Thrust Reverser Cowl Doors (4120KS to 4130KS) Close the Thrust Reverser Cowl Doors Thrust Reverser Cycling Test (MCDU) Test of the Thrust Reverser Deployment and Stowage (Engine not Running) Fig. 601 Fig. 602 Fig. 603
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 05-51-44-991-004
Fig. 604
**ON A/C 701-749, 05-51-44-991-004-A
Fig. 604A
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 05-51-44-991-006
Fig. 605
**ON A/C 701-749, 05-51-44-991-006-A
Fig. 605A
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 05-51-44-991-008
Fig. 606
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Page 603 Jul 01/06
------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------**ON A/C 701-749, 05-51-44-991-008-A
Fig. 606A
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 05-51-44-991-009
Fig. 607
**ON A/C 701-749, 05-51-44-991-009-A
Fig. 607A
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, 05-51-44-991-010
Fig. 608
**ON A/C 701-749, 05-51-44-991-010-A
Fig. 608A
**ON A/C ALL 3. __________ Job Set-up Subtask 05-51-44-210-052 A. Inspection Requirements (1) Definitions If there is a flight crew report of high lateral acceleration, you must get the data from the DFDR or any other device available to know the lateral load factor before the aircraft is released for flight. NOTE : If excessive turbulence caused the high vertical lateral ____ loads, it is possible that there were also high vertical loads. For high vertical loads, do the inspection after Flight
EFF : ALL 05-51-44 SROS
Page 604 Jul 01/06
in Excessive Turbulence or in Excess of VMO/MMO (Ref. TASK 0551-17-200-801). NOTE : If there is a flight crew report of high lateral acceleration ____ and if the data from the DFDR or any other device available cannot be used to know the lateral load factor, contact AIRBUS before the subsequent flight for more information. (2) Confirmation that inspection is necessary: (a) If the value of the lateral load factor is less than 0.28 g on the two sides of the aircraft: - this inspection is not necessary and the aircraft can return to service. (b) If the value of the lateral load factor is equal to or more than 0.28 g but less than 0.33 g: - do the inspection given in Para. 4. of this procedure, - send the DFDR recording (or equivalent) for the section of the flight during which the event occurred to AIRBUS for analysis. NOTE : Until the results of the AIRBUS analysis are available and ____ on the condition that no damage is found during the visual inspection given in Para. 4., the aircraft can return to service for a period of 30 days/100 Flight Cycles maximum (the one that occurs first). AIRBUS will make an analysis of the event for final clearance or more instructions. (c) If the value of the lateral load factor is equal to or more than 0.33 g: - the aircraft is not permitted to return to flight, - do the inspection given in Para. 4. of this procedure, - send the DFDR recording (or equivalent) for the section of the flight during which the event occurred to AIRBUS for analysis, - get instructions from AIRBUS for preparation of the aircraft for detailed information, - AIRBUS will make an analysis of the event to find if the aircraft can return to service. (3) Inspection Preparation NOTE : All inspections are visual unless specified differently in the ____ text. Operators can refer to the non-destructive testing manual (NTM) and use non-destructive test procedures.
EFF : ALL 05-51-44 SROS
Page 605 Jul 01/06
Subtask 05-51-44-941-050 B. Safety Precautions (1) Put the safety barriers in position. (2) Put the wheel chocks in position at the main landing gear. (3) Put warning notices in position in the cockpit to tell persons not to operate the systems. **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-44-010-050 C. Get Access (1) Open the main-landing-gear doors (Ref. TASK 32-12-00-010-801). (2) Put an ACCESS PLATFORM 17M (56 FT) - ADJUSTABLE in position near the area you must examine. (3) Install the safety devices on the landing gears (Ref. TASK 32-00-00481-801). (4) Open the fan cowl doors (Ref. TASK 71-13-00-010-802): FOR 4030EM1 415BL, 416BR FOR 4030EM2 425BL, 426BR (5) Open the thrust reverser doors (Ref. TASK 78-30-00-010-801): FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR
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Page 606 Jul 01/06
**ON A/C 701-749, Subtask 05-51-44-010-050-A C. Get Access (1) Open the main-landing-gear doors (Ref. TASK 32-12-00-010-801). (2) Put an ACCESS PLATFORM 17M (56 FT) - ADJUSTABLE in position near the area you must examine. (3) Install the safety devices on the landing gears (Ref. TASK 32-00-00481-801). (4) Open the fan cowl doors (Ref. TASK 71-13-00-010-805): FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR (5) Open the thrust reverser doors (Ref. TASK 78-30-00-010-803): FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR **ON A/C ALL Subtask 05-51-44-860-050 D. Aircraft Maintenance Configuration (1) Extend the flaps (Ref. TASK 27-50-00-866-801). (2) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (3) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803). (4) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802). (5) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801).
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Page 607 Jul 01/06
4. Procedure _________ Subtask 05-51-44-210-051 A. Inspection of the Fuselage (Ref. Fig. 601/TASK 05-51-44-991-001, 602/TASK 05-51-44-991-002) (Ref. TASK 53-15-11-400-801), (Ref. TASK 53-15-11-010-801), (Ref. TASK 53-15-11-700-801), (Ref. TASK 05-51-17-200-801), (Ref. TASK 05-23-20-200804). ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Radome | | | | | | | | | | | | | | | | A.| | Examine the radome shell (Ref.TASK | | | | | | | | | 53-15-11-400-801) for: | | | | | | | | | - gap and mismatch. | X | | | | | | | | If out of tolerances: | | | | | | | | | Open the radome (Ref. TASK 53-15-11- | | | | | | | | | 010-801) and do a check of | | | | | | | | | the metallic parts and arrestor | | | | | | | | | pick-up fitting for: | | | | | | | | | - deformation, bending and twist. | | X | | | | | | | If you find a defect, replace the | | | | | | | | | defective part and do a check of the | | | | | | | | | metallic frame. | | | | | | | | | Do a tap test around fitting areas | | | | | | | | | (hinges and latches) | | | | | | | | | (Ref. TASK 53-15-11-700-801). | | | | | | | | | | | | | | | |2. | | Inspection of the FWD/AFT Fuselage | | | | | | | | | | | | | | | | A.| | Do the inspection after Flight in | X | | | | | | | | Excessive Turbulence or in Excess of | | | | | | | | | VMO/MMO (Ref. TASK 05-51-17-200-801) | | | | | | | | | and add these inspections: | | | | | | | | | | | | | | | | B.| | Examine the fuselage externally | | | | | | | | | between FR78 and FR80 above STGR25, | | | | | | | | | the skin panels, the splicing and the | | | | | | | | | rivets for: | | | | | | | | | - distortion, cracks, pulled or torn | X | | | | | | | | fasteners and damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | Examine the internal structure, the | | | | | |
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Page 608 Jul 01/06
Center Fuselage Figure 601/TASK 05-51-44-991-001 EFF : ALL 05-51-44 SROS
Page 609 Jul 01/06
Rear Fuselage and Tail Section Figure 602/TASK 05-51-44-991-002 EFF : ALL 05-51-44 SROS
Page 610 Jul 01/06
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | stringers and the frames for: | | | | | | | | | - distortion, cracks, pulled or torn | | X | | | | | | | fasteners and damaged paintwork. | | | | | | | | | | | | | | | | C.| | Examine the fuselage internally | | | | | | | | | between FR83 to FR88 above STGR27 and | | | | | | | | | FR87 and FR91 at all areas for: | | | | | | | | | - distortion, cracks, pulled or torn | X | | | | | | | | fasteners and damaged paintwork. | | | | | | | | | | | | | | | | D.| | Do a detailed visual inspection of the| X | | | | | | | | fuselage external surface below the | | | | | | | | | fin-to-fuselage fairing, | | | | | | | | | fin-to-fuselage attach fittings | | | | | | | | | with side load fittings and lower | | | | | | | | | surface of the vertical RIB1 | | | | | | | | | (Ref. TASK 05-23-20-200-804). | | | | | | | | | | | | | | | |3. | | Inspection of the center fuselage | | | | | | | | | | | | | | | | A.| | Examine attachment of FR40 to skin | | | | | | | | | fuselage between STGR18 and STGR30 | | | | | | | | | for: | | | | | | | | | - damaged paintwork and damaged | X | | | | | | | | fasteners. | | | | | | | | | | | | | | | | B.| | At FR40, examine upper skin of wing | | | | | | | | | box attachment to STGR27 for: | | | | | | | | | - damaged fasteners. | X | | | | | | | | | | | | | | | C.| | Examine FR40 between upper skin of | | | | | | | | | wing box and STGR18 for: | | | | | | | | | - buckling, distortion and damaged | X | | | | | | | | fasteners. | | | | | | | | | | | | | | | | D.| | At aft FR40 area, examine joint | | | | | | | | | fitting of STGR41 to STGR44 for: | | | | | | | | | - damaged paintwork, damaged fasteners| X | | | | | | | | and cracks in flanges. | | | | | | | | | | | | | | | | E.| | Examine attachment of FR46 to FR53.2 | | | | | | | | | between STGR17 and STGR20 for: | | | | | | | | | - damaged fasteners. | X | | | | |
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Page 611 Jul 01/06
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | | | | | | | | F.| | Examine lower fitting of forward | | | | | | | | | canted longeron attachment to FR47 | | | | | | | | | for: | | | | | | | | | - damaged fasteners. | X | | | | | | | | | | | | | | | G.| | Examine FR39.2 between STGR24 and | | | | | | | | | STGR26 above the floor, FR39.2 between| | | | | | | | | STGR26 and STGR28 below the floor, | | | | | | | | | FR47 between STGR20 and STGR24, FR48 | | | | | | | | | and FR49 between STGR18 and STGR21 | | | | | | | | | for: | | | | | | | | | - buckling, distortion and damaged | X | | | | | | | | fasteners. | | | | | | | | | | | | | | | | H.| | Examine stiffener at Y2565 below | | | | | | | | | lateral pressurized floor between FR48| | | | | | | | | and FR53.2 for: | | | | | | | | | - buckling, distortion and damaged | X | | | | | | | | fasteners. | | | | | | | | | | | | | | | | J.| | Examine attachment of FR49 and FR48 | | | | | | | | | mid frame to lateral pressurized floor| | | | | | | | | at Z-700 for: | | | | | | | | | - damaged fasteners and cracks in | X | | | | | | | | angles. | | | | | | | | | | | | | | | | K.| | Examine lateral FR52 in door stop | | | | | | | | | and fairing area for: | | | | | | | | | - damaged paintwork, damaged | X | | | | | | | | fasteners and cracks in flanges. | | | | | | | | | | | | | | | | L.| | Examine main longeron between FR52 | | | | | | | | | and FR53 for: | | | | | | | | | - buckling and distortion of web and | X | | | | | | | | flanges. | | | | | | | | | | | | | | | | M.| | Examine main longeron attachment to | | | | | | | | | aft extension longeron at Z-1080.2 | | | | | | | | | across FR53.2 for: | | | | | | | | | - damaged fasteners. | X | | | | | | | | | | | | | | | N.| | Examine Z-700 Horizontal Tee | | | | | |
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Page 612 Jul 01/06
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | attachment to lateral pressurized | | | | | | | | | floor between FR53 and FR53.2 and | | | | | | | | | between FR48 and FR50 for: | | | | | | | | | - damaged fasteners. | X | | | | | | | | | | | | | | | P.| | Examine joint fitting of STGR28 | | | | | | | | | attachment to FR53.2 for: | | | | | | | | | - damaged fasteners. | X | | | | | | | | | | | | | | | Q.| | Examine lower skin of wing box | | | | | | | | | attachment to the keel beam fitting: | | | | | | | | | - damaged fasteners. | X | | | | | | | | | | | | | | | R.| | Examine lateral FR53.1 for: | | | | | | | | | - bolting paintwork, damaged | X | | | | | | | | fasteners and cracks. | | | | | | | | | | | | | | | | S.| | Examine external STGR31 attachment | | | | | | | | | to skin panel between FR53.2 and | | | | | | | | | FR53.4 for: | | | | | | | | | - damaged fasteners. | X | | | | | | | | | | | | | | | T.| | Examine attachment of FR53.3 to skin | | | | | | | | | fuselage between STGR30 and STGR35 | | | | | | | | | for: | | | | | | | | | - damaged fasteners. | X | | | | | | | | | | | | | | | U.| | Examine STGR26 between FR53.1 and | | | | | | | | | FR53.3, STGR28 between FR53.2 and | | | | | | | | | FR53.3, STGR30 between FR52 and FR53, | | | | | | | | | the panels, the web and the flange of | | | | | | | | | of the stringer and the stiffener for:| | | | | | | | | - buckling, distortion and damaged | X | | | | | | | | fasteners. | | | | | | -------------------------------------------------------------------------------
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Page 613 Jul 01/06
Subtask 05-51-44-210-053 B. Inspection of the Vertical Stabilizer (Ref. TASK 05-51-17-200-801), (Ref. TASK 55-34-11-000-801), (Ref. TASK 55-34-11-400-801). ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Vertical Stabilizer | | | | | | | | | and Rudder | | | | | | | | | | | | | | | | A.| | Do the inspection after Flight in | X | | | | | | | | Excessive Turbulence or in Excess of | | | | | | | | | VMO/MMO (Ref. TASK 05-51-17-200-801) | | | | | | | | | and add these inspections: | | | | | | | | | | | | | | | | B.| | Do a detailed visual inspection of | | X | | | | | | | the Fin box RIB13. To do this, remove | | | | | | | | | the fin tip (access as per Ref TASk | | | | | | | | | 55-34-11-000-801), (installation | | | | | | | | | as per Ref. TASK 55-34-11-400-801). | | | | | | ------------------------------------------------------------------------------Subtask 05-51-44-210-054 C. Inspection of the Horizontal Stabilizer ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Trimmable Horizontal| | | | | | | | | Stabilizer (THS) and Elevator | | | | | | | | | | | | | | | | A.| | Do a general visual inspection of: | X | | | | | | | | - the upper and lower skins of the | | | | | | | | | THS center and lateral spar boxes, | | | | | | | | | - the front and rear spars of the THS | | | | | | | | | center and lateral spar boxes, | | | | | | | | | - the top and the bottom trailing | | | | | | | | | edges of the THS access panels, | | | | | | | | | - the THS leading-edge skin on the two| | | | | | | | | sides, | | | | | | | | | - the THS tip skin on the two sides, | | | | | | | | | - the lower and upper elevator skins | | | | | | | | | on the two sides, | | | | | |
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Page 614 Jul 01/06
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - the elevator front spar on the two | | | | | | | | | sides. | | | | | | | | | | | | | | | | B.| | If you find damage on the skins of | | | | | | | | | the lateral boxes: | | | | | | | | | (1) Examine the inner side at the | | X | | | | | | | damage location to do a check of | | | | | | | | | STGR and rib conditions. | | | | | | | | | | | | | | | | C.| | Do a detailed visual inspection of: | X | | | | | | | | - the attachment areas, the screw | | | | | | | | | jacks, the two rear supports (and | | | | | | | | | the fittings) and the two side load | | | | | | | | | fittings (Rib 4 at rear spar) of the| | | | | | | | | THS, | | | | | | | | | - all hinge arms, actuator fittings, | | | | | | | | | elevator side-load fittings and | | | | | | | | | their attachments on the two sides, | | | | | | | | | - the skin joints between the THS | | | | | | | | | lateral and central spar boxes, | | | | | | | | | - the spar joints between the THS | | | | | | | | | lateral and central spar boxes, | | | | | | | | | - the THS trailing-edge ribs and | | | | | | | | | their attachments, | | | | | | | | | - the elevator fittings and their | | | | | | | | | attachments to the THS for leakage. | | | | | | | | | | | | | | | | D.| | If you find damage: | | | | | | | | | (1) Do a special detailed inspection | | | | | | | | | of the carbon component for: | | | | | | | | | - exact location of damage and | | X | | | | | | | damage length width and depth. | | | | | | | | | (2) Do a special detailed inspection | | | | | | | | | of the metallic component for: | | | | | | | | | - cracks. | | X | | | | | | | | | | | | | | E.| | Do a functional test of the elevator | X | | | | | | | | movement. | | | | | | -------------------------------------------------------------------------------
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Page 615 Jul 01/06
Subtask 05-51-44-210-055 D. Inspection of the Wing (Ref. Fig. 603/TASK 05-51-44-991-003) (Ref. TASK 05-51-17-200-801), (Ref. TASK 27-14-00-820-801). ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Wing | | | | | | | | | | | | | | | | A.| | Do the inspection after Flight in | X | | | | | | | | Excessive Turbulence or in Excess of | | | | | | | | | VMO/MMO (Ref.TASK 05-51-17-200-801). | | | | | | | | | | | | | | | |2. | | Inspection of the Outer-Wing Wingtip | | | | | | | | | to Main Wingbox joint | | | | | | | | | | | | | | | | A.| | At RIB39, examine the upper and lower | | | | | | | | | skin panel joints for: | | | | | | | | | - cracks, distortion and pulled or | X | | | | | | | | torn fasteners. | | | | | | | | | Make sure that the sealant beads are | X | | | | | | | | in the correct condition. | | | | | | | | | | | | | | | |3. | | Inspection of Fixed Leading-Edge | | | | | | | | | D-Nose Skins | | | | | | | | | | | | | | | | A.| | Examine the D-nose skin-panel joint | | | | | | | | | at slat track center-lines, from slat | | | | | | | | | track 9 and outboard for: | | | | | | | | | - cracks, distortion and pulled or | X | | | | | | | | torn fasteners. | | | | | | | | | Make sure that the sealant beads are | X | | | | | | | | in the correct condition. | | | | | | | | | | | | | | | |4. | | Inspection of the Aileron | | | | | | | | | | | | | | | | A.| | Examine the upper and lower skin | | | | | | | | | panels, the hinges and the spar | | | | | | | | | fasteners for: | | | | | | | | | - damaged paintwork and damaged | X | | | | | | | | filler. | | | | | | | | | | | | | | | | B.| | Examine the fittings for: | | | | | | | | | - damage. | X | | | | |
EFF : ALL 05-51-44 SROS
Page 616 Jul 01/06
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | | | | | | | | C.| | Do the inspection of the aileron | X | | | | | | | | adjustment | | | | | | | | | (Ref. TASK 27-14-00-820-801). | | | | | | | | | | | | | | | |5. | | Inspection of the Flaps and Slats | | | | | | | | | | | | | | | | A.| | At flap track 2, examine aft | X | | | | | | | | attachment (spigot) and flap-to| | | | | | | | | carriage attachment of inboard flap. | | | | | | | | | | | | | | | | B.| | At flap track 4, examine aft | X | | | | | | | | attachment (spigot), flap-to| | | | | | | | | carriage and flap-to-I/M beam | | | | | | | | | attachment of outboard flap. | | | | | | | | | | | | | | | | C.| | Examine attachment-points of movable | X | | | | | | | | flap track fairings 2 to 5. | | | | | | | | | | | | | | | | D.| | Examine the slats and their fairings | | | | | | | | | for: | | | | | | | | | - cracks, distortion and pulled or | X | | | | | | | | torn fasteners. | | | | | | | | | | | | | | | |6. | | Inspection of spoiler | | | | | | | | | | | | | | | | A.| | Examine the center hinge lugs of | | | | | | | | | spoilers 1 to 6 for: | | | | | | | | |- cracks, distortion and other damage. | X | | | | | ------------------------------------------------------------------------------Subtask 05-51-44-210-056 E. Inspection of the Pylons **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, (Ref. Fig. 604/TASK 05-51-44-991-004)
EFF : ALL 05-51-44 SROS
Page 617 Jul 01/06
Structure of the Wing Figure 603/TASK 05-51-44-991-003- 12 (SHEET 1) EFF : ALL 05-51-44 SROS
Page 618 Jul 01/06
Structure of the Wing Figure 603/TASK 05-51-44-991-003- 22 (SHEET 2) EFF : ALL 05-51-44 SROS
Page 619 Jul 01/06
Engine-Pylon Station Figure 604/TASK 05-51-44-991-004 EFF : 001-049, 201-249, 251-252, 255-299, 05-51-44 301-399, 401-449, 451-499, SROS
Page 620 Jul 01/06
**ON A/C 701-749, (Ref. Fig. 604A/TASK 05-51-44-991-004-A) **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, (Ref. Fig. 605/TASK 05-51-44-991-006) **ON A/C 701-749, (Ref. Fig. 605A/TASK 05-51-44-991-006-A) **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, (Ref. Fig. 606/TASK 05-51-44-991-008) **ON A/C 701-749, (Ref. Fig. 606A/TASK 05-51-44-991-008-A) **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, (Ref. Fig. 607/TASK 05-51-44-991-009) **ON A/C 701-749, (Ref. Fig. 607A/TASK 05-51-44-991-009-A) **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, (Ref. Fig. 608/TASK 05-51-44-991-010) **ON A/C 701-749, (Ref. Fig. 608A/TASK 05-51-44-991-010-A)
EFF : 001-049, 201-249, 251-252, 255-299, 05-51-44 301-399, 401-449, 451-499, 701-749, SROS
Page 621 Jul 01/06
Engine-Pylon Station Figure 604A/TASK 05-51-44-991-004-A EFF : 701-749, 05-51-44 SROS
Page 622 Jul 01/06
Engine-Pylon Box Figure 605/TASK 05-51-44-991-006 EFF : 001-049, 201-249, 251-252, 255-299, 05-51-44 301-399, 401-449, 451-499, SROS
Page 623 Jul 01/06
Engine-Pylon Box Figure 605A/TASK 05-51-44-991-006-A EFF : 701-749, 05-51-44 SROS
Page 624 Jul 01/06
Engine-to-Pylon Attach Fittings Figure 606/TASK 05-51-44-991-008 EFF : 001-049, 201-249, 251-252, 255-299, 05-51-44 301-399, 401-449, 451-499, SROS
Page 625 Jul 01/06
Engine-to-Pylon Attach Fittings Figure 606A/TASK 05-51-44-991-008-A EFF : 701-749, 05-51-44 SROS
Page 626 Jul 01/06
Pylon-to-Wing Forward Attach-Fittings Figure 607/TASK 05-51-44-991-009 EFF : 001-049, 201-249, 251-252, 255-299, 05-51-44 301-399, 401-449, 451-499, SROS
Page 627 Jul 01/06
Pylon-to-Wing Forward Attach-Fittings Figure 607A/TASK 05-51-44-991-009-A EFF : 701-749, 05-51-44 SROS
Page 628 Jul 01/06
Pylon-to-Wing Aft Attach-Fittings Figure 608/TASK 05-51-44-991-010 EFF : 001-049, 201-249, 251-252, 255-299, 05-51-44 301-399, 401-449, 451-499, SROS
Page 629 Jul 01/06
Pylon-to-Wing Aft Attach-Fittings Figure 608A/TASK 05-51-44-991-010-A EFF : 701-749, 05-51-44 SROS
Page 630 Jul 01/06
**ON A/C ALL (Ref. TASK 28-25-00-650-803), (Ref. TASK 71-00-51-000-801) ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Pylons | | | | | | | | | | | | | | | | A.| | Examine pylon panels, doors, auxiliary| | | | | | | | | structure, the rivets and the | | | | | | | | | stiffeners for: | | | | | | | | | - distortion, buckling and tearing of | X | | | | | | | | plates at rivet locations. | | | | | | | | | | | | | | | | B.| | Examine the pylon forward secondary | | | | | | | | | structure for: | | | | | | | | | - buckling and missing rivets. | X | | | | | | | | If you find damage: | | | | | | | | | Examine adjacent external and internal| | | | | | | | | area of pylon forward secondary | | | | | | | | | structure for: | | | | | | | | | - distortion, cracks, rupture and | | X | | | | | | | fluid leakage and sheared or slack | | | | | | | | | or missing fasteners. | | | | | | | | | | | | | | | | C.| | Examine the pylon panels between | | | | | | | | | forward and aft pylon-to-wing | | | | | | | | | attachment for: | | | | | | | | | - distortion, wrinkles, buckles, | X | | | | | | | | sheared or slack or missing | | | | | | | | | fasteners and tearing of plates | | | | | | | | | at rivet locations. | | | | | | | | | | | | | | | | D.| | Examine upper spar between spigot | | | | | | | | | hole and aft attachment and around | | | | | | | | | access door for: | | | | | | | | | - distortion, wrinkles, buckles, | X | | | | | | | | sheared or slack or missing | | | | | | | | | fasteners and tearing of plates | | | | | | | | | at rivet locations. | | | | | | | | | If you find damage: | | | | | | | | | Examine pylon main frame (lower spar, | | | | | | | | | upper spar, panels, ribs, rib-to-panel| | | | | | | | | attachments, spar-to-panel | | | | | |
EFF : ALL 05-51-44 SROS
Page 631 Jul 01/06
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | attachments, structure) for: | | | | | | | | | - distortion, cracks, rupture and | | X | | | | | | | fluid leakage. | | | | | | | | | | | | | | | | E.| | Examine the Fan Cowl and Thrust | | | | | | | | | Reverser attachments for: | | | | | | | | | - cracks, distortion and pulled or | X | | | | | | | | torn fasteners. | | | | | | | | | Make sure the Cowl closes correctly. | | | | | | | | | | | | | | | | F.| | Examine the engine-to-pylon | | | | | | | | | attachments for: | | | | | | | | | - distortion and cracks. | X | | | | | | | | If you find damage: | | | | | | | | | (1) Examine the Thrust-Reverser spigot| | | | | | | | | Fitting for: | | | | | | | | | - cracks in the protective | | X | | | | | | | sealant at the most inboard and | | | | | | | | | outboard edges of the spigot | | | | | | | | | attachment flange with the wing | | | | | | | | | surface, | | | | | | | | | - distortion, gapping between | | X | | | | | | | attachment flange and wing | | | | | | | | | surface, | | | | | | | | | - distortion of fasteners, | | X | | | | | | | - cracks. | | X | | | | | | | (2) Examine the Rear Pick-up for: | | | | | | | | | - cracks in the protective | | X | | | | | | | treatment/sealant around the | | | | | | | | | attachment to the wing surface, | | | | | | | | | - distortion, gapping between | | X | | | | | | | attachment flange and wing | | | | | | | | | surface, | | | | | | | | | - distortion of fasteners, | | X | | | | | | | - cracks. | | X | | | | | | | | | | | | | | G.| | Examine the pylon-to-wing fittings | | | | | | | | | for: | | | | | | | | | - distortion and cracks. | X | | | | | | | | If you find damage: | | | | | | | | | Examine the pylon-to-wing attach | | | | | | | | | fitting for: | | | | | | | | | - distortion and cracks. | | X | | | |
EFF : ALL 05-51-44 SROS
Page 632 Jul 01/06
------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| ------------------------------------------------------------------------------Subtask 05-51-44-210-057 F. Inspection of the Nacelles ------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the Nacelles | | | | | | | | | | | | | | | | A.| | Examine the Fan Cowl and Thrust| | | | | | | | | Reverser hinge fitting and latches | | | | | | | | | for: | | | | | | | | | - cracks, distortion and pulled or | X | | | | | | | | torn fasteners. | | | | | | | | | Make sure the Fan Cowl and the Thrust | | | | | | | | | Reverser close correctly. | | | | | | | | | If you find damage: | | | | | | | | | (1) Examine the thrust-reverser | | | | | | | | | fitting adjacent area of the | | | | | | | | | pylon (lateral panel, rib) for: | | | | | | | | | - distortion, cracks and sheared | | X | | | | | | | or slack or missing fasteners. | | | | | | | | | (2) Examine the fan-cowl fitting | | | | | | | | | adjacent internal and external | | | | | | | | | areas of the secondary structure | | | | | | | | | for: | | | | | | | | | - cracks, distortion, dents and | | X | | | | | | | sheared or slack or missing | | | | | | | | | rivets and fasteners. | | | | | | -------------------------------------------------------------------------------
EFF : ALL 05-51-44 SROS
Page 633 Jul 01/06
**ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-44-410-050 G. Close Access (1) Close the main-landing-gear doors (Ref. TASK 32-12-00-410-801). (2) Close the fan cowl doors (Ref. TASK 71-13-00-410-802): FOR 4030EM1 415BL, 416BR FOR 4030EM2 425BL, 426BR (3) Close the thrust reverser doors (Ref. TASK 78-30-00-410-801): FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR **ON A/C 701-749, Subtask 05-51-44-410-050-A G. Close Access (1) Close the main-landing-gear doors (Ref. TASK 32-12-00-410-801). (2) Close the fan cowl doors (Ref. TASK 71-13-00-410-805): FOR 4030EM1 415AL, 416AR FOR 4030EM2 425AL, 426AR (3) Close the thrust reverser doors (Ref. TASK 78-30-00-410-803): FOR 4030EM1 417AL, 418AR FOR 4030EM2 427AL, 428AR
EFF : 001-049, 201-249, 251-252, 255-299, 05-51-44 301-399, 401-449, 451-499, 701-749, SROS
Page 634 Jul 01/06
**ON A/C ALL Subtask 05-51-44-866-050 H. 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) Pressurize the Yellow hydraulic system (Ref. TASK 29-00-00-863-803). (4) Pressurize the Blue hydraulic system (Ref. TASK 29-00-00-863-802). Subtask 05-51-44-200-050 J. Do The Flight System Test NOTE : The tests below are necessary only if you find damage to the ____ structure adjacent to a flight control surface. (1) Operate the aileron system. Make sure that the travel is full and that the aileron moves freely (Ref. TASK 27-14-00-710-801). (2) Operate the flap system. Make sure that the travel is full and that the flap moves freely (Ref. TASK 27-54-00-710-801). (3) Operate the slat system. Make sure that the travel is full and that the slat moves freely (Ref. TASK 27-84-00-710-801). (4) Operate the spoiler system. Make sure that the travel is full and that the spoiler moves freely (Ref. TASK 27-64-00-710-801). (5) Operate the THS system. Make sure that the travel is full and that the THS moves freely.
EFF : ALL 05-51-44 SROS
Page 635 Jul 01/06
(6) Operate the elevator system. Make sure that the travel is full and that the elevator moves freely (Ref. TASK 27-34-00-710-801). (7) Operate the rudder system. Make sure that the travel is full and that the rudder moves freely (Ref. TASK 27-24-00-710-801). **ON A/C 001-049, 201-249, 251-252, 255-299, 301-399, 401-449, 451-499, Subtask 05-51-44-200-051 K. Do a test of the Thrust Reverser System NOTE : The test below is necessary only if you find damage to the ____ structure adjacent to a cowl surface. (1) Operate the thrust reverser system. Make sure that the travel is full and that the thrust reverser moves freely (Ref. TASK 78-31-00-710-804). **ON A/C 701-749, Subtask 05-51-44-200-051-A K. Do a test of the Thrust Reverser System NOTE : The test below is necessary only if you find damage to the ____ structure adjacent to a cowl surface. (1) Operate the thrust reverser system. Make sure that the travel is full and that the thrust reverser moves freely (Ref. TASK 78-31-00-740-802).
EFF : ALL 05-51-44 SROS
Page 636 Jul 01/06
**ON A/C ALL 5. Close-up ________ Subtask 05-51-44-866-051 A. Aircraft Maintenance Configuration (1) Depressurize the Green hydraulic system (Ref. TASK 29-00-00-864-801). (2) Depressurize the Yellow hydraulic system (Ref. TASK 29-00-00-864-803). (3) Depressurize the Blue hydraulic system (Ref. TASK 29-00-00-864-802). (4) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-801). Subtask 05-51-44-860-051 B. Put the Aircraft back to its Initial Configuration (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.
EFF : ALL 05-51-44 SROS
Page 637 Jul 01/06
_____________________________________________________________________________ PRESSURIZATION TEST OF FUSELAGE (LEAKAGE CHECKS) AFTER A/C ABNORMAL OPERATION OR REPAIR - ADJUSTMENT/TEST ___________________________ TASK 05-53-00-780-803 Pressurization Retest and Leakage Rate Measurement WARNING : MAKE SURE THAT: _______ - ONLY THE PERSONS NECESSARY FOR THE PRESSURIZATION TEST ARE IN THE AIRCRAFT DURING THE TEST. - THE PERSONS IN THE AIRCRAFT HAVE MEDICAL CLEARANCE TO DO THIS TYPE OF TEST. BE CAREFUL WHEN YOU CONTROL THE PRESSURE. SUDDEN CHANGES IN PRESSURE CAN CAUSE PAIN AND INJURY. WARNING : THERE MUST BE TWO PERSONS IN THE COCKPIT DURING THE PRESSURIZATION _______ TEST. IF A CHANGE IN PRESSURE HAS AN UNWANTED EFFECT (PAIN, NOISE IN THE EARS, HEADACHE OR OTHER) ON ONE PERSON, THE OTHER PERSON CAN ADJUST THE PRESSURE TO AVOID INJURY. 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. 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. 1. __________________ Reason for the Job To measure the structural leakage.
EFF : ALL 05-53-00 R SROS
Page 501 Jan 01/07
2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific R
No No No No No No No No
specific specific specific specific specific specific specific specific
absolute pressure indicator/digital indication/sensitivity 1mbar(0.01psi) circuit breaker(s) safety clip(s) safety barriers safety plug - ref MS21913-4 safety streamer stop-watch vertical speed indicator warning notices O-ring - ref NAS1612-4
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-33-21-618-801 12-33-21-618-801 23-44-00-860-801 24-41-00-861-801 24-41-00-862-801 31-60-00-860-801 31-60-00-860-802 35-12-41-000-802 35-12-41-400-802 52-51-00-710-801
Pre-conditioning through the High-Pressure Ground Connection Pre-conditioning with the APU Operation of the Service Interphone System 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 Removal of the Full-Face/Quick-Donning Oxygen Mask (8RN1,2,3,4) Installation of the Full-Face/Quick-Donning Oxygen Mask (8RN1,2,3,4) Operational Test of the Cockpit-Door Lock System (CDLS)
EFF : ALL 05-53-00 SROS
Page 502 Jan 01/07
3. __________ Job Set-up R R R R R
Subtask 05-53-00-865-050 A. Open, safety and tag this(these) circuit breaker(s): ------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------C/B NOT APPLICABLE Subtask 05-53-00-860-064-A
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B. Aircraft Maintenance Configuration (1) Put the safety barriers and the warning notices in position to keep persons out of the work area. (2) Put the vertical speed indicator, absolute pressure indicator/digital indication/sensitivity 1mbar(0.01psi) and the stop-watch in position in the cockpit. (3) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861801). (4) Make sure that the avionics equipment ventilation operates correctly. NOTE : If during this test, the avionics equipment ventilation stops, ____ you must stop the test. (5) In the left side of the avionics compartment at frame 14: - put the safety plug - ref MS21913-4 with its O-ring - ref NAS1612-4 on the air inlet of the pressure switch 16WR. - put a safety streamer on the safety plug. (6) On the panel 722VU, open the circuit breaker 1MQ Cockpit Door Lock System (CDLS). (7) We recommend that you remove the crew oxygen masks (Ref. TASK 35-1241-000-802) NOTE : This test requires an absolute pressure higher than the cabin ____ pressures you get during usual aircraft operations. The crew masks have an aneroid capsule that is usually resistant to the absolute pressures you can get during this test.
EFF : ALL 05-53-00 SROS
Page 503 Jan 01/07
But, to prevent high stress on the aneroid capsule, we recommend the removal of the crew oxygen masks. (8) On the AIR section of the panel 225VU: - make sure that the PACK 1 and PACK 2 pushbutton switches are pushed (the FAULT legends are on). (9) On the CABIN PRESS section of the panel 225VU: - release the MOD SEL pushbutton switch (the MAN legend is on) - make sure that the MAN/VALVE SEL switch is in the BOTH position. (10) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00860-801). (11) On the SD on the CAB PRESS page: - make sure that the outflow valves 313HL and 315HL are in the fully open position. (12) On the CARGO AIR COND section of the panel 212VU: - make sure that the BULK (FWD, AFT) ISOL VALVES pushbutton switch is released (the OFF legend is on). (13) On the VENTILATION section of the panel 212VU: - push the EXTRACT pushbutton switch (the OVRD legend is on). (14) On the overboard extract valve (13HQ): (a) Push the latch to release the handle. (b) Pull out the handle to engage the mechanism. (c) Fold out the handle. (d) Set the deactivation switch to the OFF position. (e) Turn the handle counterclockwise until the main and auxiliary flaps of the valve are fully closed. (f) Fold and latch the handle. (15) On the SD, on the CAB PRESS page: - make sure that the VENT EXTRACT ventilation valve is closed. After 30 seconds approximately, the horn in the nose gear well sounds. On the panel 925VU: - push the HORN RESET pushbutton switch.
EFF : ALL 05-53-00 R SROS
Page 504 Jan 01/07
(16) Close and lock the sliding windows and all access doors to the pressurized area. (17) For aircraft on which the optional LDMCR is installed, make sure that the access panel to the staircase is open. (18) on the EXT LT section of the panel 215VU: - set the BEACON switch to ON. (19) Do an interphone communication test between the cockpit and the ground service personnel out of the closed area .(Ref. TASK 23-44-00860-801) (20) Pressurize the pneumatic system: - with the APU (Ref. TASK 12-33-21-618-801) or with the HP ground-supply unit (Ref. TASK 12-33-21-618-801) NOTE : You must shut the access door 811 for this procedure. ____ Subtask 05-53-00-860-071 R
C. Not applicable. Subtask 05-53-00-970-052
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D. Calculation of the Pressure. (1) Use the pressure indicator to measure the ambient pressure (Pamb). (2) Calculate and write these values: - Value A = Pamb + 400 mbar (5.80 psi) - Value B = Pamb + 610 +7 -7 mbar (8.84 +0.10 -0.10 psi) - Value C = Pamb + 578 mbar (8.38 psi) - Value D = Pamb + 570 mbar (8.26 psi) The values A and B are necessary to monitor the system. The values C and D are necessary to mesure the leakage rate.
EFF : ALL 05-53-00 SROS
Page 505 Jan 01/07
4. Procedure _________ Subtask 05-53-00-780-054 A. Procedure to measure the leakage rate. WARNING : DO NOT LET THE CABIN ALTITUDE CHANGE TOO FAST. SUDDEN CHANGES _______ IN PRESSURE CAN CAUSE INJURY TO PERSONS. WARNING : MAKE SURE THAT THE DIFFERENTIAL PRESSURE IS NOT MORE THAN THE _______ VALUE SPECIFIED FOR THIS TEST. WARNING : DO NOT USE THE ECAM DISPLAYS TO READ THE CABIN PRESSURE _______ PARAMETERS (CABIN DIFFERENTIAL PRESSURE, CABIN ALTITUDE, CABIN VERTICAL- SPEED) DURING THIS TEST. THE PRESSURES USED IN THIS TEST ARE MORE THAN THE MAXIMUM LIMIT OF THE RELATED PRESSURE SENSOR. WHEN THESE PRESSURES BECOME MORE THAN THE PRESSURE SENSOR LIMIT, ON THE ECAM DISPLAY: - THE CABIN DIFFERENTIAL PRESSURE INDICATION AND THE CABIN ALTITUDE INDICATION WILL CONTINUE TO SHOW THESE LIMIT VALUES. - THE CABIN VERTICAL-SPEED INDICATION IS NO LONGER CORRECT. IF YOU DO NOT KNOW THE CORRECT CABIN PRESSURE VALUES, YOU CAN MAKE UNWANTED CHANGES IN PRESSURE THAT CAN CAUSE INJURY.
R R R
NOTE : This procedure uses the MAN V/S CTL switch on the CABIN PRESS ____ section of the panel 225VU to control the cabin pressure. This switch, spring loaded to neutral, controls the outflow valves position: - UP: the outflow valves move to the open position (the cabin pressure decreases) - DN: the outflow valves move to the closed position (the cabin pressure increases) We recommend: - short action on this switch (do not hold the switch in the UP or DN position) - that you monitor the cabin vertical speed indication to prevent sudden changes in cabin pressure.
EFF : ALL 05-53-00 SROS
Page 506 Jan 01/07
------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------1. On the AIR section of the panel 225VU: - adjust the cabin temperature control as necessary.
On the AIR section of the panel 225VU: - make sure that the FAULT legend of the PACK 1 and PACK 2 pushbutton switches is off. Air blows into the fuselage.
2. On the CABIN PRESS section of the panel 225VU: - set the MAN V/S CTL switch to DN and release, the switch moves to the neutral position. Do this operation several times. This closes the outflow valves.
On the vertical speed indicator: - the cabin vertical speed must not be more than 500 ft.min (152.39 m.min). On the pressure indicator: - the cabin pressure increases up to value A (Pamb + 400 mbar (5.80 psi)).
NOTE : The cabin vertical speed ____ must not be more than 500 ft.min (152.39 m.min). - stop when you get a cabin pressure of value A (Pamb + 400 mbar (5.80 psi)). 3. With the MAN/V/S CTL switch in the UP or DN position, keep the pressure stable at value A (Pamb + 400 mbar (5.80 psi)) for 5 minutes.
Tell ground personnel to walk around the aircraft and to do a check for leakage. On the vertical speed indicator: - the cabin vertical speed is 0. On the pressure indicator: - the cabin pressure is value A (Pamb + 400 mbar (5.80 psi)).
4. Use the same method as in step 2 to increase cabin pressure up to value B (Pamb + 610 +7 -7 mbar (8.84 +0.10 -0.10 psi)).
On the pressure indicator: - the cabin pressure increases up to value B (Pamb + 610 +7 -7 mbar (8.84 +0.10 -0.10 psi)). On the vertical speed indicator: - the cabin vertical speed must not be more than 500 ft.min (152.39 m.min).
NOTE : the cabin vertical speed ____ must not be more than 500 ft.min (152.39 m.min). 5. With the MAN/V/S CTL switch in the UP or DN position, keep the
On the vertical speed indicator: - the cabin vertical speed is 0.
EFF : ALL 05-53-00 R SROS
Page 507 Jan 01/07
------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------pressure stable at value B (Pamb On the pressure indicator: + 610 +7 -7 mbar (8.84 +0.10 - the cabin pressure is value B (Pamb + 0.10 psi)). 610 +7 -7 mbar (8.84 +0.10 -0.10 psi)). 6. On the AIR section of the panel 225VU: - release the PACK 1 pushbutton switch. On the CABIN PRESS section of the panel 225VU: - with the MAN/V/S CTL switch, stabilize the pressure at value B (Pamb + 610 +7 -7 mbar (8.84 +0.10 -0.10 psi)).
On the AIR section of the panel 225VU: - the OFF legend of the PACK 1 pushbutton switch comes on. On the vertical speed indicator: - the cabin vertical speed is 0. On the pressure indicator: - the cabin pressure is value B (Pamb + 610 +7 -7 mbar (8.84 +0.10 -0.10 psi)).
7. On the CABIN PRESS section of the panel 225VU: - with the MAN/V/S CTL switch in DN position, fully close the outflow valves. On the AIR section of the panel 225VU: - release the PACK 2 pushbutton switch when the outflow valves are closed.
On the SD, on the CAB PRESS page: - the outflow valves are in the fully closed position. On the AIR section of the panel 225VU: - the OFF legend of the PACK 2 pushbutton switch comes on. On the pressure indicator: - the cabin pressure indication decreases.
8. Monitor the decrease of the pressure: - at value C (Pamb + 578 mbar (8.38 psi)), start the stop-watch. - at value D (Pamb + 570 mbar (8.26 psi)), stop the stop-watch and write the time. 9. Calculate the leakage rate: - leakage rate = (value C) (value D) / time The leakage rate is permitted if below 0.64 mbar/s (0.56 psi/min) On the AIR section of the panel
On the vertical speed indicator:
EFF : ALL 05-53-00 R SROS
Page 508 Jan 01/07
R R R
------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------225VU: - the cabin vertical speed must not be - push the PACK 1 and PACK 2 more than 500 ft.min (152.39 m.min). pushbutton switches (the OFF On the pressure indicator: legend is off). - the cabin pressure indication On the CABIN PRESS section of the decreases down to the external panel 225VU: ambient pressure. - with the MAN V/S CTL switch, decrease the cabin pressure until you get a differential pressure of 0 psi. NOTE : The cabin vertical speed ____ must not be more than 500 ft.min (152.39 m.min). 10. Wait until the cabin has completely depressurized and then fully open the outflow valves. 5. Close-up ________
R
Subtask 05-53-00-865-051
R R
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
R R R
------------------------------------------------------------------------------PANEL DESIGNATION FIN LOCATION ------------------------------------------------------------------------------C/B NOT APPLICABLE Subtask 05-53-00-860-065-A
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B. Put the Aircraft back to its Initial Configuration (1) Shut down the APU (Ref. TASK 12-33-21-618-801) or stop the HP ground-air supply unit (Ref. TASK 12-33-21-618-801). (2) On the EXT LT section of the panel 215VU: - set the BEACON switch to OFF.
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Page 509 Jan 01/07
(3) In the left side of the avionics compartment at frame 14: - remove the safety streamer from the safety plug. - remove the safety plug with its O-ring from the air inlet of the pressure switch 16WR. (4) If you removed the crew oxygen masks, install them (Ref. TASK 35-1241-400-802) (5) Remove the pressure indicator, the vertical speed indicator and the stop-watch from the cockpit. (6) On the VENTILATION section of the panel 212VU: - release the EXTRACT pushbutton switch (the FAULT legend comes on) (7) On the panel 722VU, close the circuit breaker 1MQ and do a CDLS test (Ref. TASK 52-51-00-710-801). (8) On the overboard extract valve (13HQ): (a) Push the latch to release the handle. (b) Pull the handle. (c) Set the deactivation switch to ON, and make sure that the two flaps open. (d) Fold and latch the handle. (9) On the VENTILATION section of the panel 212VU: - the FAULT legend of the EXTRACT pushbutton switch goes off (10) Put the system and the aircraft back to the serviceable configuration. (11) Do the EIS stop procedure: (Ref. TASK 31-60-00-860-802) (12) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862801). (13) Remove the warning notices and the safety barriers.
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Page 510 Jan 01/07
TASK 05-53-00-780-803- 01 Pressurization Retest and Leakage Rate Measurement (with ACMS) WARNING : MAKE SURE THAT: _______ - ONLY THE PERSONS NECESSARY FOR THE PRESSURIZATION TEST ARE IN THE AIRCRAFT DURING THE TEST. - THE PERSONS IN THE AIRCRAFT HAVE MEDICAL CLEARANCE TO DO THIS TYPE OF TEST. BE CAREFUL WHEN YOU CONTROL THE PRESSURE. SUDDEN CHANGES IN PRESSURE CAN CAUSE PAIN AND INJURY. WARNING : THERE MUST BE TWO PERSONS IN THE COCKPIT DURING THE PRESSURIZATION _______ TEST. IF A CHANGE IN PRESSURE HAS AN UNWANTED EFFECT (PAIN, NOISE IN THE EARS, HEADACHE OR OTHER) ON ONE PERSON, THE OTHER PERSON CAN ADJUST THE PRESSURE TO AVOID INJURY. 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. 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. 1. __________________ Reason for the Job To measure the structural leakage.
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Page 511 Jul 01/05
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
safety barriers safety plug - ref MS21913-4 safety streamer stop-watch warning notices O-ring - ref NAS1612-4
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------12-33-21-618-801 12-33-21-618-801 23-44-00-860-801 24-41-00-861-801 24-41-00-862-801 31-36-00-740-805 31-60-00-860-801 31-60-00-860-802 34-10-00-860-801 34-10-00-860-803 35-12-41-000-802 35-12-41-400-802 52-51-00-710-801
Pre-conditioning through the High-Pressure Ground Connection Pre-conditioning with the APU Operation of the Service Interphone System Energize the Aircraft Electrical Circuits from the External Power A De-energize the Aircraft Electrical Circuits from the External Power A Access to the Parameter call-up menus. EIS Start Procedure EIS Stop Procedure ADIRS Start Procedure ADIRS Stop Procedure Removal of the Full-Face/Quick-Donning Oxygen Mask (8RN1,2,3,4) Installation of the Full-Face/Quick-Donning Oxygen Mask (8RN1,2,3,4) Operational Test of the Cockpit-Door Lock System (CDLS)
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3. __________ Job Set-up R Subtask 05-53-00-860-066-A A. Aircraft Maintenance Configuration (1) Put the safety barriers and the warning notices in position to keep persons out of the work area. (2) Make sure that the static probe covers are not installed. (3) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861801). (4) Make sure that the avionics equipment ventilation operates correctly. NOTE : If during this test, the avionics equipment ventilation stops, ____ you must stop the test. (5) In the left side of the avionics compartment at frame 14: - put the safety plug - ref MS21913-4 with its O-ring - ref NAS1612-4 on the air inlet of the pressure switch 16WR. - put a safety streamer on the safety plug. (6) We recommend that you remove the crew oxygen masks (Ref. TASK 35-1241-000-802) NOTE : This test requires an absolute pressure higher than the cabin ____ pressures you get during usual aircraft operations. The crew masks have an aneroid capsule that is usually resistant to the absolute pressures you can get during this test. But, to prevent high stress on the aneroid capsule, we recommend the removal of the crew oxygen masks. (7) On the AIR section of the panel 225VU: - make sure that the PACK 1 and PACK 2 pushbutton switches are pushed (the FAULT legends is on). (8) On the CABIN PRESS section of the panel 225VU: - release the MOD SEL pushbutton switch (the MAN legend is on) - make sure that the MAN/VALVE SEL switch is in the BOTH position. (9) On the panel 722VU, open the circuit breaker 1MQ Cockpit Door Lock System (CDLS).
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(10) Do the EIS start procedure (EWD DU, SD DU only) (Ref. TASK 31-60-00860-801). (11) On the SD on the CAB PRESS page: - make sure that the outflow valves 313HL and 315HL are in the fully open position. (12) On the CARGO AIR COND section of the panel 212VU: - make sure that the BULK (FWD, AFT) ISOL VALVES pushbutton switch is released (the OFF legend is on). (13) On the VENTILATION section of the panel 212VU: - push the EXTRACT pushbutton switch (the OVRD legend is on). (14) On the overboard extract valve (13HQ): (a) Push the latch to release the handle. (b) Pull out the handle to engage the mechanism. (c) Fold out the handle. (d) Set the deactivation switch to the OFF position. (e) Turn the handle counterclockwise until the main and auxiliary flaps of the valve are fully closed. (f) Fold and latch the handle. (15) On the SD, on the CAB PRESS page: - make sure that the VENT EXTRACT ventilation valve is closed. After 30 seconds approximately, the horn in the nose gear well sounds. On the panel 925VU: - push the HORN RESET pushbutton switch. (16) Do the ADIRS start procedure (Ref. TASK 34-10-00-860-801). (17) On the MCDU, get access to the ACMS : PARAM ALPHA CALL-UP page. Enter the alpha codes: (Ref. TASK 31-36-00-740-805) - PDC to show the cabin differential pressure - VSCB to show the cabin vertical speed - AOV to show the aft outflow valve position - FOV to show the forward outflow valve position (18) Close and lock the sliding windows and all access doors to the pressurized area.
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(19) on the EXT LT section of the panel 215VU: - set the BEACON switch to ON. (20) Do an interphone communication test between the cockpit and the ground service personnel out of the closed area.(Ref. TASK 23-44-00860-801) (21) Pressurize the pneumatic system: - with the APU (Ref. TASK 12-33-21-618-801) or with the HP ground-supply unit (Ref. TASK 12-33-21-618-801) NOTE : You must shut the access door 811 for this procedure. ____ Subtask 05-53-00-860-072 B. Not applicable. 4. Procedure _________ Subtask 05-53-00-780-055 A. Procedure to measure the leakage rate. WARNING : DO NOT LET THE CABIN ALTITUDE CHANGE TOO FAST. SUDDEN CHANGES _______ IN PRESSURE CAN CAUSE INJURY TO PERSONS. WARNING : MAKE SURE THAT THE DIFFERENTIAL PRESSURE IS NOT MORE THAN THE _______ VALUE SPECIFIED FOR THIS TEST. WARNING : DO NOT USE THE ECAM DISPLAYS TO READ THE CABIN PRESSURE _______ PARAMETERS (CABIN DIFFERENTIAL PRESSURE, CABIN ALTITUDE, CABIN VERTICAL- SPEED) DURING THIS TEST. THE PRESSURES USED IN THIS TEST ARE MORE THAN THE MAXIMUM LIMIT OF THE RELATED PRESSURE SENSOR. WHEN THESE PRESSURES BECOME MORE THAN THE PRESSURE SENSOR LIMIT, ON THE ECAM DISPLAY: - THE CABIN DIFFERENTIAL PRESSURE INDICATION AND THE CABIN ALTITUDE INDICATION WILL CONTINUE TO SHOW THESE LIMIT VALUES. - THE CABIN VERTICAL-SPEED INDICATION IS NO LONGER CORRECT. IF YOU DO NOT KNOW THE CORRECT CABIN PRESSURE VALUES, YOU CAN MAKE UNWANTED CHANGES IN PRESSURE THAT CAN CAUSE INJURY.
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NOTE : This procedure uses the MAN V/S CTL switch on the CABIN PRESS ____ section of the panel 225VU to control the cabin pressure. This switch, spring loaded to neutral, controls the outflow valves position:
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Page 515 Jan 01/07
- UP: the outflow valves move to the open position (the cabin pressure decreases) - DN: the outflow valves move to the closed position (the cabin pressure increases) We recommend: - short action on this switch (do not hold the switch in the UP or DN position) - that you monitor the cabin vertical speed indication to prevent sudden changes in cabin pressure. ------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------1. On the AIR section of the panel 225VU: - adjust the cabin temperature control as necessary.
On the AIR section of the panel 225VU: - make sure that the FAULT legend of the PACK 1 and PACK 2 pushbutton switches is off. Air blows into the fuselage.
2. On the CABIN PRESS section of the panel 225VU: - set the MAN V/S CTL switch to DN and release, the switch moves to the neutral position. Do this operation several times. This closes the outflow valves (AOV and FOV indication on MCDU).
On the MCDU - the cabin more than On the MCDU - the cabin increases
(VSCB indication): vertical speed must not be 500 ft.min (152.39 m.min). (PDC indication): differential pressure up to 400 mbar (5.80 psi).
NOTE : The cabin vertical speed ____ must not be more than 500 ft.min (152.39 m.min) (VSCB indication on MCDU). - stop when you get a cabin differential pressure of 400 mbar (5.80 psi) (PDC indication on MCDU). 3. With the MAN/V/S CTL switch in the UP or DN position, keep the differential pressure stable at 400 mbar (5.80 psi) for 5 minutes.
tell ground personnel to walk around the aircraft and do a check for leakage. On the MCDU (VSCB indication): - the cabin vertical speed is 0.
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------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------On the MCDU (PDC indication): - the cabin differential pressure is 400 mbar (5.80 psi). 4. Use the same method as in step 2 to increase cabin differential pressure up to 610 +7 -7 mbar (8.84 +0.10 -0.10 psi). NOTE : the cabin vertical speed ____ must not be more than 500 ft.min (152.39 m.min) (VSCB indication on MCDU).
On the MCDU (PDC indication): - the cabin differential pressure increases up to 610 +7 -7 mbar (8.84 +0.10 -0.10 psi). On the MCDU (VSCB indication): - the cabin vertical speed must not be more than 500 ft.min (152.39 m.min).
5. With the MAN/V/S CTL switch in the UP or DN position, keep the differential pressure stable at 610 +7 -7 mbar (8.84 +0.10 -0.10 psi).
On the MCDU - the cabin On the MCDU - the cabin 610 +7 -7 psi).
(VSCB indication): vertical speed is 0. (PDC indication): differential pressure is mbar (8.84 +0.10 -0.10
6. On the AIR section of the panel 225VU: - Release the PACK 1 pushbutton switch. On the CABIN PRESS panel 25VU: - with the MAN/V/S CTL switch, stabilize the differential pressure at 610 +7 -7 mbar (8.84 +0.10 -0.10 psi).
On the AIR section of the panel 225VU: - the OFF legend of the PACK 1 pushbutton switch comes on. On the MCDU (VSCB indication): - the cabin vertical speed is 0. On the MCDU (PDC indication): - the cabin differential pressure is 610 +7 -7 mbar (8.84 +0.10 -0.10 psi).
7. On the CABIN PRESS section of the panel 225VU: - with the MAN/V/S CTL switch in DN position, fully close the outflow valves (AOV and FOV indication on MCDU). On the AIR section of the panel 225VU: - release the PACK 2 pushbutton switch when the outflow valves are closed.
On the SD, on the CAB PRESS page: - the outflow valves are in the fully closed position. On the AIR section of the panel 225VU: - the OFF legend of the PACK 2 pushbutton switch comes on. On the MCDU (PDC indication): - the cabin differential pressure indication decreases.
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------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------8. Monitor the differential pressure decrease on the MCDU (PDC indication): - at 578 mbar (8.38 psi), start the stop-watch. - at 570 mbar (8.26 psi), stop the stop-watch and write the time. 9. Calculate the leakage rate: - leakage rate = 578 mbar (8.38 psi) - 570 mbar (8.26 psi) / time. The leakage rate is permitted if below 0.64 mbar/s (0.56 psi/min). On the AIR section of the panel 225VU: - push the PACK 1 and PACK 2 pushbutton switches (the OFF legend is off). On the CABIN PRESS section of the panel 225VU: - with the MAN V/S CTL switch, decrease the cabin differential pressure until you get a differential pressure of 0 psi.
On the MCDU - the cabin more than On the MCDU - the cabin decreases
(VSCB indication): vertical speed must not be 500 ft.min (152.39 m.min). (PDC indication): differential pressure down to 0.
NOTE : The cabin vertical speed ____ must not be more than 500 ft.min (152.39 m.min) (VSCB indication on MCDU). 10. Wait until the cabin has completely depressurized and then fully open the outflow valves (AOV and FOV indication on MCDU).
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Page 518 Jul 01/05
5. Close-up ________ R Subtask 05-53-00-860-067-A A. Put the Aircraft back to its Initial Configuration (1) Shut down the APU (Ref. TASK 12-33-21-618-801) or stop the HP ground-air supply unit (Ref. TASK 12-33-21-618-801). (2) On the EXT LT section of the panel 215VU: - set the BEACON switch to OFF. (3) In the left side of the avionics compartment at frame 14: - remove the safety streamer from the safety plug. - remove the safety plug with its O-ring from the air inlet of the pressure switch 16WR. (4) If you removed the crew oxygen masks, install them (Ref. TASK 35-1241-400-802) (5) On the VENTILATION section of the panel 212VU: - release the EXTRACT pushbutton switch (the FAULT legend comes on) (6) On the panel 722VU, close the circuit breaker 1MQ and do a CDLS test (Ref. TASK 52-51-00-710-801). (7) On the overboard extract valve (13HQ): (a) Push the latch to release the handle. (b) Pull the handle. (c) Set the deactivation switch to ON, and make sure that the two flaps open. (d) Fold and latch the handle. (8) On the VENTILATION section of the panel 212VU: - the FAULT legend of the EXTRACT pushbutton switch goes off (9) Put the system and the aircraft back to the serviceable configuration. (10) Do the ADIRS stop procedure: (Ref. TASK 34-10-00-860-803)
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(11) Do the EIS stop procedure: (Ref. TASK 31-60-00-860-802) (12) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862801). (13) Remove the warning notices and the safety barriers. R
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Page 520 Jul 01/05
DEMAGNETIZATION - MAINTENANCE PRACTICES _______________________________________ TASK 05-54-00-860-801 Demagnetization of the External Parts of the Frames of the Windshield and Sliding Windows 1. __________________ Reason for the Job The demagnetization procedure is applicable to the external parts of the frames of the windshield and sliding windows. R
Use this procedure if you are sure that incorrect deviation of the standby compass occurs after adjustment on the compensation base. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------DM05275A DM05275B MGM50 SAV890-71
1 1 1 1
DEMAGNETIZER - 110V/60HZ DEMAGNETIZER - 220V/50HZ GAUSSMETER DEMAGNETIZER - 230V/50HZ
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------34-22-00-730-801 34-22-23-000-801 34-22-23-400-801
Adjustment test of the standby compass Removal of the Standby Compass (3FC) Installation of the Standby Compass (3FC)
3. __________ Job Set-up Subtask 05-54-00-860-050 A. Aircraft Configuration (1) Make sure that the A/C is not energized (batteries, engines or external power supply).
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Page 201 Jan 01/07
Subtask 05-54-00-020-050 B. Removal of the Standby Compass (1) Remove the standby compass (Ref. TASK 34-22-23-000-801) from the cockpit and keep it away from magnetic sources. 4. Procedure _________ Subtask 05-54-00-280-050 A. Find the Magnetic Zones: (1) Obey the instructions from the manufacturer for the GAUSSMETER (MGM50). (2) Make sure that the Gaussmeter operates correctly: - the pointer must move when you put the instrument near the shaft of the windshield wiper motors. (3) With the Gaussmeter, find the magnetic zones of the external parts of the frames of the windshield and sliding windows. Record the value for each zone. NOTE : Ignore the magnetization on the shaft of the windshield wiper ____ motors. Subtask 05-54-00-869-050 B. Demagnetize: R R R
(1) Obey the instructions from the manufacturer for the DEMAGNETIZER 110V/60HZ (DM05275A), DEMAGNETIZER - 220V/50HZ (DM05275B) or the DEMAGNETIZER - 230V/50HZ (SAV890-71) (2) Energize the demagnetizer. (3) Put the demagnetizer at a very small distance (1 cm approx.) from the part it is necessary to demagnetize. This position gives the reference plane. (4) Push the power supply button (indicator light on) and keep the demagnetizer above the magnetic zone during 2 to 3 seconds. Then move the demagnetizer away slowly at a constant speed and at right angles to the reference plane. You must move the demagnetizer to a minimum distance of 50 cm approx. before you release the button. (5) Do the step (4) again for each zone that you must demagnetize.
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Page 202 Jul 01/02
(6) De-energize the demagnetizer. (7) For each demagnetized zone, read the value shown on the Gaussmeter. Make sure that this value is near zero. (8) If you find zones that are not fully demagnetized, do again the step (4) until the value read on the Gaussmeter is near zero. 5. Close-up ________ Subtask 05-54-00-420-050 A. Installation of the Standby Compass (1) Install the standby compass (Ref. TASK 34-22-23-400-801). Subtask 05-54-00-730-050 B. Compensation of the Standby Compass (1) Do the compensation of the standby compass (Ref. TASK 34-22-00-730801).
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Page 203 Apr 01/98
MEASUREMENT AFTER ABNORMAL OPERATION OF THE AIRCRAFT - INSPECTION/CHECK _______________________________________________________________________ TASK 05-56-00-200-801 Measurement of the Aircraft by Photogrammetry after Abnormal Operation of the Aircraft 1. __________________ Reason for the Job This procedure gives instructions to put the aircraft in the configuration necessary to measure it by photogrammetry. 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 97F08001000000 98F05003000002
safety barriers warning notices wheel chocks adjustable access platform 16.8 m (55 ft. 1 in.) 1 MEASUREMENT TARGET 1 TARGET - MEASUREMENT
B. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------08-10-00-200-801 28-25-00-650-803 32-00-00-481-801 32-12-00-410-801 32-22-00-410-801 05-56-00-991-001 05-56-00-991-002 05-56-00-991-003 05-56-00-991-004 05-56-00-991-005 05-56-00-991-006 05-56-00-991-007
Weighing and Balancing To Drain the Remaining Fuel (Wing Tanks) Installation of the Safety Devices on the Landing Gears Close the MLG Doors after Maintenance Close the NLG Doors after Maintenance Fig. 601 Fig. 602 Fig. 603 Fig. 604 Fig. 605 Fig. 606 Fig. 607
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Page 601 Jul 01/03
3. __________ Job Set-up Subtask 05-56-00-941-050 A. Towing of the Aircraft to the Work Area (1) Tow the aircraft to a place where there is no air movement and a constant temperature or into a hangar. NOTE : Tow the aircraft in a straight line over 10 meters to prevent ____ any lateral stress on the landing gears. Subtask 05-56-00-941-051 B. Safety Precautions (1) Put safety barriers in position around the aircraft. (2) Install the safety devices on the landing gears (Ref. TASK 32-00-00481-801). (3) Put an adjustable access platform in position near the aircraft. (4) Put wheel chocks in position at the main landing gear. Subtask 05-56-00-860-050 C. Aircraft Maintenance Configuration (1) Close the MLG doors (Ref. TASK 32-12-00-410-801). (2) Close the NLG doors (Ref. TASK 32-22-00-410-801). (3) Fully defuel the aircraft (Ref. TASK 28-25-00-650-803). (4) Make sure that: - flight control surfaces are in the neutral position - all doors and panels are closed. (5) Weigh the aircraft, if necessary (Ref. TASK 08-10-00-200-801).
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Page 602 Apr 01/98
Subtask 05-56-00-210-050 D. Safety Precautions (1) Make sure that the area around the aircraft is clear. (2) Put warning notices on the passenger/crew doors to prevent access into the aircraft while you measure the aircraft. Subtask 05-56-00-010-050 E. Installation of the Targets on the Aircraft R R
(1) Use MEASUREMENT TARGET (97F08001000000) or TARGET - MEASUREMENT (98F05003000002) to install the targets. (2) Installation of the targets on the wing (Ref. Fig. 601/TASK 05-56-00-991-001) (a) Install 10 targets on the upper surface of each wing, on the sighting reference rivets that you use to adjust flap tracks (points 1R to 10R and 1L to 10L). (b) Install 2 targets at the end of each wing, at the farthest screws of the wing box (points 11R, 12R, 11L and 12L). (c) Install 3 targets on each wing tip (points 13L to 15L and 13R to 15R). (3) Installation of the targets on the fuselage (Ref. Fig. 602/TASK 05-56-00-991-002) (a) Install 10 targets on each side of the fuselage at the leveling points (red triangles) (points 20R to 24R and 20L to 24L). (b) Install 1 target on each side of the fuselage on the aft lower hole used to attach the hoist fitting at FR39-1 (points 25L and 25R). (c) Install 4 targets below the fuselage on the centerline. Put them on indexed tools installed in the measurement receptacles (points 16 to 19). (d) Install 2 targets on the centerline of the center post of the windshield (points 26 and 27). (e) Install 1 target on the centerline of the blanking plug of the shoring hole, at FR85 (point 28).
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Page 603 Jul 01/03
Location of the Measurement Points on the Wing Figure 601/TASK 05-56-00-991-001 EFF : ALL 05-56-00 SROS
Page 604 Apr 01/98
Location of the Measurement Points on the Fuselage Figure 602/TASK 05-56-00-991-002 EFF : ALL 05-56-00 SROS
Page 605 Apr 01/98
(4) Installation of the targets on the THS (Ref. Fig. 603/TASK 05-56-00-991-003) (a) Install 4 targets on the THS at the hoisting points (points 30L to 33L and 30R to 33R). (5) Installation of the targets on the vertical stabilizer (Ref. Fig. 603/TASK 05-56-00-991-003) (a) Install 4 targets on the left side at the measurement receptacles (points 34 to 37). (6) Installation of the targets on the engine pylons (Ref. Fig. 604/TASK 05-56-00-991-004) (a) Install 2 targets on the outboard side of the pylons at the measurement receptacles (points 41L, 42L, 41R, and 42R). (b) Install 2 targets on the outboard side of the nacelle air intakes, at the measurement receptacles (points 40L (A,B), 40R (A,B)). NOTE : Install all the targets directly on the external surface ____ of the aircraft except at points 16 to 19 where you must use indexed tools. (7) Installation of the targets on the main landing gear (Ref. Fig. 605/TASK 05-56-00-991-005) (a) Install 1 target on the center of the hub of each outboard wheel (L and R) (points 50L, 50R, 53L and 53R). (b) Install 2 targets in an opposite position on the rim of these outboard wheels (L and R) (points 51L, 52L, 54L, 55L, 51R, 52R, 54R, 55R). (8) Installation of the targets on the nose landing gear. (a) Install 1 target on the center of the hub of the left wheel (point 59). (b) Install 2 targets in an opposite position on the rim of this left wheel (points 60 and 61).
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Page 606 Apr 01/98
Location of the Measurement Points on the Vertical Stabilizer and THS Figure 603/TASK 05-56-00-991-003 EFF : ALL 05-56-00 SROS
Page 607 Apr 01/98
Location of the Measurement Points on the Engine Pylons Figure 604/TASK 05-56-00-991-004 EFF : ALL 05-56-00 SROS
Page 608 Apr 01/98
Location of the Measurement Points on the Landing Gear Figure 605/TASK 05-56-00-991-005 EFF : ALL 05-56-00 SROS
Page 609 Apr 01/98
(9) Installation of ground targets (Ref. Fig. 606/TASK 05-56-00-991-006) (a) Install at least 8 ground targets that you will use to give the scale and for calibration. Make a record of the distance between the targets. 4. Procedure _________ Subtask 05-56-00-220-050 A. Aircraft measurement (1) Take the pictures (Ref. Fig. 607/TASK 05-56-00-991-007) (a) Take at least 9 shots from above the aircraft to have pictures which show all the targets that you can see on the wing. Each shot must include at least 2 ground points. (b) Take at least 7 shots from the ground to have pictures which show all the points that you can see from the ground. Each shot must include at least 2 ground points. (2) Use the photogrammetry principle when you: - take photographs - make a note of measures - make the restitution - make the analysis of the results. 5. Close-up ________ Subtask 05-56-00-410-050 A. Removal of the Targets (1) Remove all the targets and indexed tools that you have installed. Subtask 05-56-00-942-050 B. Put the Aircraft back to its Initial Configuration (1) Remove the safety devices installed on the landing gears. (2) Remove the access platform(s).
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Page 610 Apr 01/98
Location of the Measurement Points on the Ground Figure 606/TASK 05-56-00-991-006 EFF : ALL 05-56-00 SROS
Page 611 Apr 01/98
Location of Shooting Positions Figure 607/TASK 05-56-00-991-007 EFF : ALL 05-56-00 SROS
Page 612 Apr 01/98
(3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
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Page 613 Apr 01/98
AIRCRAFT STABILITY - MAINTENANCE PRACTICES __________________________________________ TASK 05-57-00-200-801 Aircraft Stability 1. __________________ Reason for the Job The method given below is used to do graphical checks of the aircraft stability. NOTE : The stability graphs for aircraft on wheels (on dry or wet ground) ____ given in this procedure are applicable to a parked or towed aircraft.
R
NOTE : With the stability graphs (A/C on wheels) given in this procedure, ____ you can do a check of shifting or tipping stability limits, if you need to know only one such limit (when towing for example). It is also used to calculate the ballast necessary for aircraft stability under unfavorable conditions in the following configurations: - aircraft with engines - engines removed - engine re-installation 2. ______________________ Job Set-up Information A. Referenced Information ------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------WBM 1-10-00 05-57-00-991-004 05-57-00-991-005 05-57-00-991-006 05-57-00-991-007 05-57-00-991-008 05-57-00-991-009
Fig. Fig. Fig. Fig. Fig. Fig.
201 202 203 204 205 206
EFF : ALL 05-57-00 SROS
Page 201 Jan 01/07
3. __________ Job Set-up Subtask 05-57-00-869-050 A. Aircraft Maintenance Configuration (1) Make sure that the flaps, the slats, the spoilers, the speed brakes and the thrust reverser are retracted. (2) Make sure that the THS is set to neutral. 4. Procedure _________ Subtask 05-57-00-210-050 A. Stability of the aircraft (1) If necessary, the ballast will be installed: - in the forward cargo compartment (at position 11P and 12P), - in the cabin at level of the FR18. NOTE : Before ballasts are put on the aircraft, make sure that the ____ limits below are not exceeded (Ref. WBM 1-10-00) - maximum weight of section 11P and 12P, - maximum loads on cabin floor, - maximum load on jacking points. (2) Refuelling wing tanks can also be a method to put the aircraft back into balance. In this case, the weight of the fuel must be added to the aircraft weight. (3) This method is applicable to these aircraft configurations for each of which a diagram is given: - diagram for aircraft on wheels, on dry ground, (Ref. Fig. 201/TASK 05-57-00-991-004) - diagram for aircraft on wheels, on wet ground, (Ref. Fig. 202/TASK 05-57-00-991-005) - diagram for aircraft on jacks, (Ref. Fig. 203/TASK 05-57-00-991-006) - diagram for aircraft on nose jack or on NLG wheel jack, (Ref. Fig. 204/TASK 05-57-00-991-007) - diagram for aircraft on one MLG wheel jack, (Ref. Fig. 205/TASK 05-57-00-991-008) - diagram for aircraft on MLG and NLG wheel jacks (Ref. Fig. 206/TASK 05-57-00-991-009)
EFF : ALL 05-57-00 SROS
Page 202 Apr 01/98
Stability, Aircraft on wheels on dry ground (applicable to a parked or towed aircraft) Figure 201/TASK 05-57-00-991-004 EFF : ALL SROS
05-57-00
Page 203 Apr 01/98
Stability, Aircraft on wheels on wet ground (applicable to a parked or towed aircraft) Figure 202/TASK 05-57-00-991-005 EFF : ALL SROS
05-57-00
Page 204 Apr 01/98
Stability, Aircraft on jacks Figure 203/TASK 05-57-00-991-006 EFF : ALL 05-57-00 SROS
Page 205 Apr 01/98
Stability, Aircraft on forward jack or on nose wheel jack Figure 204/TASK 05-57-00-991-007 EFF : ALL 05-57-00 SROS
Page 206 Apr 01/98
Stability, aircraft on one main gear wheel jack Figure 205/TASK 05-57-00-991-008 EFF : ALL 05-57-00 SROS
Page 207 Apr 01/98
Stability, aircraft jacked at main and nose gears for wheel change Figure 206/TASK 05-57-00-991-009 EFF : ALL 05-57-00 SROS
Page 208 Apr 01/98
Subtask 05-57-00-210-052 B. Check of the aircraft stability NOTE : As the same procedure is applicable in any of the above ____ configurations, the diagram related to aircraft on wheels on dry ground is taken as an example. (Ref. Fig. 201/TASK 05-57-00-991-004) (1) Check of aircraft stability: - without crew, - without galleys, - without pallets and containers. For instance, plot point A on the chart from these coordonates: - weight: 160000 kg (352739.5200 lb) - CG: 23% NOTE : Under these conditions, the aircraft will be safe in winds up ____ to 54 kts (100 km/h) (2) Stability of the aircraft when both engines are removed. (a) From point A, make a horizontal line: it cuts across the weight axis at point B (b) From point B, substract the weight of two removed engines 14000 kg (30864.7080 lb) approx., to get point B. (c) From point A, make a vertical line: it cuts across one division of the removed engine scale at point C. (d) Make a line across two divisions on this scale (1 division per engine) to get point C. (e) From this point C, make a vertical line and from point B, make a horizontal line: These two lines cut at point D. For this point, the diagram gives these values: - aircraft weight: 146000 kg (321874.8120 lb) - CG: 29.5% - permissible wind: 38 kts (70 km/h) (3) Calculation of the amount of ballast necessary for engine installation It is considered that engines are installed in the open air, with peak windspeed of 49 kts (90 km/h). The ballast, if necessary shall be installed in the forward cargo-compartment at position 11P.
EFF : ALL 05-57-00 SROS
Page 209 Apr 01/98
(a) continue line BD until it cuts across the 49 kts (90 km/h) average windspeed line at point G. (b) continue line DC until it cuts across the ballast on pallet 11P scale at point E. (c) from point G, make a vertical line until it cross the ballast on pallet 11P scale at point E. (d) Count the number of divisions on the scale between point E and E(in the example 2.3 division). Thus, weight of ballast necessary: 2.3 x 1000 kg (2204.6220 lb) = 2300 kg (5070.6306 lb) NOTE : As the ballast causes only a small increase in the ____ aircraft weight, this weight has been ignored.
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Page 210 Apr 01/98
_______________________________________________________________ NON-REVENUE FLIGHT - REQUIREMENTS FOLLOWING MAINTENANCE ACTIONS DESCRIPTION AND OPERATION _________________________ 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
1. _______ General Non-revenue flight following maintenance actions are not required by AIRBUS except for actions involving items that cannot be properly ground tested to verify that the aircrafts operational characteristics have not been adversly affected. Service experience has shown that a non-revenue flight is good practice following actions or repairs which could affect the aircrafts inherent aerodynamic characteristics. NOTE : Operators Regulatory Authority may require non-revenue flights ____ following certain maintenance actions. 2. Engine _________________________________________________________________________ Replacement Replacement or reinstallation of both engines does not require a non-revenue flight providing the engines have been successfully shop tested prior to installation, properly installed and successfully ground tested in accordance with all applicable maintenance instructions. However, owing to the number of different interfaces concerned, AIRBUS recommends that a non-revenue flight be carried out after changing or installing both engines to check that no double maintenance induced faults have been introduced. NOTE : It is recommended that operators avoid performing maintenance on ____ multiple engines installed on the same aircraft at the same time if at all possible. If it is not possible to avoid maintenance on more than one engine at the same time, it is recommended that different maintenance teams service each engine.
EFF : ALL 05-59-00 SROS
Page 1 Jul 01/06
FERRY FLIGHT WITH GEAR DOWN - MAINTENANCE PRACTICES ___________________________________________________ TASK 05-59-32-869-801 Preparation For Ferry Flight with Gear Down 1. __________________ Reason for the Job To prepare the aircraft for a ferry flight with gear down. R 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
access platform 2.5 m (8 ft. 2 in.)
3. __________ Job Set-up Subtask 05-59-32-941-050 A. General (1) You must put the aircraft systems in the ferry flight with gear down configuration before you can do such a flight. 4. Procedure _________ Subtask 05-59-32-020-050 A. Not applicable. Subtask 05-59-32-860-050 B. Put the Aircraft Systems in the Ferry Flight with Gear Down Configuration (1) Get Access to the Avionics Compartment (a) Put an access platform in position at the access door 811. (b) Open the access door 811.
EFF : ALL 05-59-32 SROS
Page 201 Jul 01/06
(2) In the avionics compartment, on the panel 808VU: (a) Lift the safety cover of the L/G DOWN VMO/MMO SELECTION switch. (b) Set the L/G DOWN VMO/MMO SELECTION switch to L/G ON. 5. Close-up ________ Subtask 05-59-32-942-050 A. Close-up (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. (4) Make an entry in the log book to tell the crew that: - the L/G DOWN VMO/MMO SELECTION switch is at L/G ON.
EFF : ALL 05-59-32 R SROS
Page 202 Jul 01/06
TASK 05-59-32-869-802 Return in Normal Operation after a Ferry flight with Gear Down 1. __________________ Reason for the Job You must put the aircraft in the normal configuration after a ferry flight. 2. ______________________ Job Set-up Information A. Fixtures, Tools, Test and Support Equipment ------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------No specific
access platform 2.5 m (8 ft. 2 in.)
3. __________ Job Set-up Subtask 05-59-32-941-051 A. Not applicable. 4. Procedure _________ Subtask 05-59-32-860-051 A. Put the Aircraft Systems in the Normal Configuration after a Ferry Flight with Gear Down (1) Get Access to the Avionics Compartment (a) Put an access platform in position at the access door 811. (b) Open the access door 811. (2) In the avionics compartment, on the panel 808VU: (a) Set the L/G DOWN VMO/MMO SELECTION switch to NORM. (b) Lock the safety cover of the L/G DOWN VMO/MMO SELECTION switch. Subtask 05-59-32-420-050 B. Not applicable.
EFF : ALL 05-59-32 SROS
Page 203 Jan 01/05
5. Close-up ________ Subtask 05-59-32-942-051 A. Close-up (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. (4) Write in the log book that: - the L/G DOWN VMO/MMO SELECTION switch is set at NORM.
EFF : ALL 05-59-32 SROS
Page 204 Jan 01/05
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