Class_seat.pdf

F4643 EADS SOGERMA ZONE INDUSTRIELLE DE L'ARSENAL B.P. 60109 17303 ROCHEFORT CEDEX FRANCE Tel. : 33.5.46.82.84.84 - FAX : 33.5.46.82.88.13

COMPONENT MAINTENANCE MANUAL WITH ILLUSTRATED PARTS LIST

CLASS SEAT

FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01

FFCL4-02WY03-01 FFCL5-02WY01-01 FFCL5-02WY02-01

First Issue: FEB 20/09

25-26-80

TP1 REV 1 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE RECORD OF REVISIONS Rev Issue No Date 1 APR 15/09

Date Inserted APR 15/09

by

Rev No

Issue Date

Date Inserted

by

SOGERMA

RECORD OF REVISIONS PAGE 1 APR 15/09

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EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 RECORD OF TEMPORARY REVISIONS Temporary Rev. No.

Page Number

Inserted Date

Removed By

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RECORD OF TEMPORARY REVISIONS PAGE 1 FEB 20/09

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EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 SERVICE BULLETIN LIST SB number and revision

Included in revision

Date of incorporation

SERVICE BULLETIN LIST PAGE 1 FEB 20/09

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EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 AMENDMENT LIST Evolution Sheet

Applicability

Description

25-26-80

Identification P/N

Amdt

AMENDMENT LIST PAGE 1 FEB 20/09

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EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE LIST OF EFFECTIVE PAGES SUBJECT

PAGE

DATE

TITLE PAGE

1 APR 15/09

RECORD OF REVISIONS

1 APR 15/09 2 BLANK

RECORD OF TEMPORARY REVISIONS

1 FEB 20/09 2 BLANK

SERVICE BULLETIN LIST

1 FEB 20/09 2 BLANK

AMENDMENT LIST

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LIST OF EFFECTIVE PAGES

1 2 3 4

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TABLE OF CONTENTS

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INTRODUCTION

1 2 3 4

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DESCRIPTION AND OPERATION

SUBJECT

PAGE

DATE

DESCRIPTION AND OPERATION (Cond’t)

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TESTING AND FAULT ISOLATION

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SCHEMATIC AND WIRING DIAGRAMS

2001 2002 2003 2004 2005 2006 2007 2008 2009 2010 2011 2012 2013 2014 2015 2016

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DISASSEMBLY

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EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE SUBJECT

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DISASSEMBLY (Cond’t)

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CLEANING

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INSPECTION/ CHECK

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REPAIR

ASSEMBLY

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SUBJECT

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ASSEMBLY (Cond’t)

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FITS AND CLEARANCES

8001 8002 8003 8004

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SPECIAL TOOLS, FIXTURES, EQUIPMENT AND CONSUMABLES

9001 9002 9003 9004

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STORAGE

ILLUSTRATED PARTS LIST

15001 FEB 20/09 15002 BLANK INTRO IPL 1 INTRO IPL 2 INTRO IPL 3 INTRO IPL 4 INTRO IPL 5 INTRO IPL 6 INTRO IPL 7 INTRO IPL 8 INTRO IPL 9 INTRO IPL10

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EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE SUBJECT ALPHANUM. INDEX

DETAILED PARTS LIST

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SUBJECT

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DETAILED PARTS LIST (Cont’d)

DATE

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EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE SUBJECT DETAILED PARTS LIST (Cont’d)

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SUBJECT

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LIST OF EFFECTIVE PAGES PAGE 4 APR 15/09

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EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TABLE OF CONTENTS PAGE 1

RECORD OF REVISIONS RECORD OF TEMPORARY REVISIONS

1

SERVICE BULLETIN LIST

1

AMENDMENT LIST

1

LIST OF EFFECTIVE PAGES

1

TABLE OF CONTENTS

1

INTRODUCTION 1. General 2. Layout of manual 3. Revision of the document 4. Certification of operations 5. WARNINGS-CAUTIONS-NOTES 6. List of Abbreviations

1 1 2 3 3 4 4

DESCRIPTION AND OPERATION 1. Description 2. Operation 3. Technical data

1 1 10 14

TESTING AND FAULT ISOLATION 1. Testing 2. Fault Isolation

1001 1001 1007

SCHEMATIC AND WIRING DIAGRAMS

2001

DISASSEMBLY 1. General 2. Preliminary Steps 3. Removal of the headrest 4. Disassembly of the headrest 5. Removal of the cushions 6. Removal of the seat from the pallet 7. Disassembly of the pallet 8. Removal of the armrest 9. Disassembly of the armrest 10. Removal of the legrest 11. Disassembly of the legrest 12. Removal of the seat back and the seat bottom 13. Disassembly of the seat back 14. Disassembly of the seat bottom 15. Disassembly of the base

3001 3001 3001 3002 3003 3005 3007 3012 3014 3015 3017 3018 3019 3020 3022 3023

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TABLE OF CONTENTS PAGE 1 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE PAGE CLEANING 1. General 2. Polycarbonate shroud 3. General cleaning 4. Electrical parts 5. Seat cover 6. Metal parts 7. Seat belt 8. Leather

4001 4001 4001 4002 4003 4004 4006 4007 4008

INSPECTION/CHECK 1. General 2. Check Procedure 3. Replacement of Parts

5001 5001 5002 5004

REPAIR 1. General 2. Metal Parts 3. Decor location 4. Electrical parts 5. Repair procedure for leather 6. Velcro tape

6001 6001 6001 6002 6004 6006 6009

ASSEMBLY 1. General 2. Assembly of the pallet 3. Assembly of the base 4. Assembly of the seat bottom 5. Assembly of the seat back 6. Installation of the seat back and the seat bottom on the base 7. Assembly of the legrest 8. Installation of the legrest on the base 9. Assembly of the armrest 10. Installation of the armrest on the base 11. Installation of the seat on the pallet 12. Actuator calibration 13. Installation of the cushions 14. Assembly of the headrest 15. Installation of the headrest

7001 7001 7002 7004 7008 7009 7011 7013 7014 7015 7017 7018 7023 7025 7026 7028

FITS AND CLEARANCES 1. General 2. Specific tightening torque value 3. Mechanical controls adjustment

8001 8001 8001 8002

SPECIAL TOOLS, FIXTURES, EQUIPMENT AND CONSUMABLES 1. Special tools, fixtures and equipments 2. Consumables 3. Suppliers list

9001 9001 9002 9003

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TABLE OF CONTENTS PAGE 2 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 PAGE STORAGE 1. Storage

15001 15001

ILLUSTRATED PARTS LIST 1. Introduction 2. Equipment designator index

1 1 8

DETAILED PART LIST

10001

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TABLE OF CONTENTS PAGE 3 FEB 20/09

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TABLE OF CONTENTS PAGE 4 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE INTRODUCTION TASK 25-26-80-990-801-A01 1.

General A. This document writing follows the directives of the "A.T.A. Specification No.2200" updating 2000.1. The instructions in this manual give the information necessary to do maintenance functions ranging from simple checks and replacement to complete shop type repair for the equipment, manufactured and supported by : EADS SOGERMA ZONE INDUSTRIELLE DE L'ARSENAL B.P. 60109 17303 ROCHEFORT CEDEX FRANCE Tel. : 33.5.46.82.84.84 - FAX : 33.5.46.82.88.13 - TELEX : 790 413F - SITA : RCOSSCR B. This document is applicable to the equipment that follows: Business class

CTR CLASS SEATS LH CLASS SEATS RH CLASS SEATS

: FFCL4-01WY03-01 : FFCL5-01WY01-01 : FFCL5-01WY02-01

First class

CTR CLASS SEATS LH CLASS SEATS RH CLASS SEATS

: FFCL4-02WY03-01 : FFCL5-02WY01-01 : FFCL5-02WY02-01

25-26-80

INTRO PAGE 1 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-990-802-A01 2.

Layout of manual A. This manual contains a general description and operation followed by data for maintenance, repair, disassembly and assembly of the equipment. It is followed by an illustrated parts list (IPL) which gives detailed information. B. The manual is divided into separate sections: (1) Title Page (2) Record of Revisions (3) List of Effective Pages (4) Table of Contents (5) Introduction (6) Procedures and IPL Sections C. This manual will be updated as required by revisions: Service Bulletins can be issued separately. Their effect on this manual will be made evident by reissue of the appropriate list of Service Bulletins.

25-26-80

INTRO PAGE 2 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-990-803-A01 3.

Revision of the document Two types of revisions of the manual are used to follow the evolution of this equipment. A. Normal revision (1) Normal revisions are periodically issued. (2) They are printed on white paper. (3) A List of Revisions lets a better follow-up of these revisions. (4) A vertical line drawn in the left margin indicates the changes in the text. B. Temporary revision (1) Temporary revisions can be issued forward the next normal revision. (2) They are printed on yellow paper. (3) A List of Temporary Revisions lets their follow-up. (4) A letter comes with these temporary revisions to give all the necessary information about the insertion of these revisions. C. General rules for the insertion of temporary revisions (1) A yellow page (with a higher sequential number) can replace a yellow page. (2) A yellow page cannot replace a white page.

TASK 25-26-80-990-804-A01 4.

Certification of operations A. The maintenance operations described in the present COMPONENT MAINTENANCE MANUAL were examined in the manufacturer's workshop by closely observing the disassembly, assembly, testing and trouble shooting instructions detailed in this document.

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INTRO PAGE 3 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-990-805-A01 5.

WARNINGS-CAUTIONS-NOTES A. Special adjuncts to the text are expressed by the following headings: WARNING : CALL ATTENTION FOR USE OF MATERIALS, PROCESSES, METHODS, PROCEDURES OR TOLERANCES WHICH MUST BE ADHERED CAREFULLY TO AVOID ANY INJURY. CAUTION : CALL ATTENTION TO METHODS AND PROCEDURES WHICH MUST BE ADHERED TO AVOID DAMAGE TO EQUIPMENT. NOTE : Call attention to methods which make the procedures easier.

TASK 25-26-80-990-806-A01 6.

List of Abbreviations ACMM

: ABBREVIATED COMPONENT MAINTENANCE MANUEL

AR

: AS REQUIRED. INDICATES THAT AN INDEFINITE QUANTITY IS REQUIRED

AS

: AEROSPACE STANDARD

ASSY

: ASSEMBLY

ATA

: AIR TRANSPORT ASSOCIATION OF AMERICA

CMM

: COMPONENT MAINTENANCE MANUAL

CTR

: CENTRAL

FIG

: FIGURE

IPL

: ILLUSTRATED PARTS LIST

LB.

: POUND

LEP

: LIST OF EFFECTIVE PAGES

LH

: LEFT HAND

N/A

: NOT APPLICABLE

NUM

: NUMBER

Qty

: QUANTITY

REV

: REVISION

RH

: RIGHT HAND

SB

: SERVICE BULLETIN

TR

: TEMPORARY REVISION

25-26-80

INTRO PAGE 4 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE DESCRIPTION AND OPERATION TASK 25-26-80-870-801-A01 1.

Description A. Typical installation (1) Valid for FFCLx-01WY SERIES, Business class.

FFCL5-01WY02-01

FWD

FFCL4-01WY03-01

FFCL5-01WY01-01

TYPICAL INSTALLATION DESCRIPTION FIGURE 1 / GRAPHIC 25-26-80-991-024-A01

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PAGE 1 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE (2) Valid for FFCLx-02WY SERIES, First class.

FFCL5-02WY02-01

FWD

FFCL4-02WY03-01

FFCL5-02WY01-01

TYPICAL INSTALLATION DESCRIPTION FIGURE 2 / GRAPHIC 25-26-80-991-065-A01

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PAGE 2 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE B. Single seat Business class (1) The seat equipped is made of two parts. (a) The seat (b) The lower part LH RH

Seats assy FFCL5-01WY01-01 FFCL5-01WY02-01

Seats FFCL1-2A1007-01 FFCL1-2A1007-02

Lower Parts FFCL1-2B0801-01 FFCL1-2B0801-02

NOTE : The two equipped seats are constituted with symmetrical assemblies. The seat shown on Figure 3 is the left hand equipped seat PN: FFCL5-01WY0101

HEADREST

SEAT BACK BELT SEAT BOTTOM

LOWER PART

LEGREST ARMREST

ARMREST COMMAND BUTTON MECHANICAL OVERRIDE CONTROL

SINGLE SEAT DESCRIPTION VALID FOR FFCL5-01WY SERIES FIGURE 3 / GRAPHIC 25-26-80-991-025-A01

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PAGE 3 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE C. Single seat First class (1) The seat equipped is made of two parts. (a) The seat (b) The lower part LH RH

Seats assy FFCL5-02WY01-01 FFCL5-02WY02-01

Seats FFCL1-5A1007-01 FFCL1-5A1007-02

Lower Parts FFCL1-5B0800-01 FFCL1-5B0800-02

NOTE : The two equipped seats are constituted with symmetrical assemblies. The seat shown on Figure 4 is the left hand equipped seat PN: FFCL5-02WY0101

HEADREST

SEAT BACK BELT

SEAT BOTTOM

LEGREST LOWER PART

MECHANICAL OVERRIDE CONTROL

SINGLE SEAT DESCRIPTION VALID FOR FFCL5-02WY SERIES FIGURE 4 / GRAPHIC 25-26-80-991-066-A01

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PAGE 4 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE D. Double seat Business class (1) The seat equipped is made of two parts (a) The seat (b) The lower part Seat equipped FFCL4-01WY03-01

Seat FFCL1-2A1007-01, LH PLACE FFCL1-2A1007-02, RH PLACE

Lower Part FFCL1-2B0844-01

SEAT BACK

BELT

SEAT BOTTOM

HEADREST

LEGREST LOWER PART

ARMREST

MECHANICAL OVERRIDE CONTROL

ARMREST COMMAND BUTTON

DOUBLE SEAT DESCRIPTION VALID FOR FFCL4-01WY SERIES FIGURE 5 / GRAPHIC 25-26-80-991-026-A01

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PAGE 5 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE E. Double seat First class (1) The seat equipped is made of two parts (a) The seat (b) The lower part Seat equipped FFCL4-02WY03-01

Seat FFCL1-5A1007-01, LH PLACE FFCL1-5A1007-02, RH PLACE

Lower Part FFCL1-5B0840-01

SEAT BACK

BELT

SEAT BOTTOM

HEADREST

LEGREST LOWER PART

MECHANICAL OVERRIDE CONTROL

DOUBLE SEAT DESCRIPTION VALID FOR FFCL4-02WY SERIES FIGURE 6 / GRAPHIC 25-26-80-991-067-A01

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PAGE 6 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE F.

Minimum maintenance (1) The seat structure has a limited number of components. (2) All covering components are easily removable without any specific tools. (3) No special inspection and very little servicing are necessary for this equipment. A minimum maintenance is sufficient. (4) One special tool is necessary for the assembly/disassembly of the seats from the lower parts (reference : 64300FFCL1-01CX01-01).

G. Comfort (1) The seat is designed to give a maximum efficiency and comfort with a minimum weight. (2) The design of the seat bottom, seat back and legrest, as well as the foam shapes, are the result of technical and human engineering studies. H. Conception (1) The coverings are made of thermoformed or injected plastics according to the company requirements. (2) All structure components are protected against corrosion. - Chemical protection: - Alodine 1200 (A1200) - Electrolytic protection: - Sulfuric Acid Anodizing (SAA) (according to the company requirements) - Chromic Acid Anodizing (CAA) - White cadmium plating (according to the company requirements) - Paint: - Primer and final coat I.

Legs and structure (1) Legs are made of machined aluminum alloy and give an excellent mechanical strength and wear resistance. (2) The structure is attached to the floor tracks with two shear pins, two locking blocks on the rear and two locking blocks on the front.

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EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE J.

Seat bottom/seat back (1) A reduction gear actuator system gives the possibility to easily get the desired position. (2) The seat back is hinged on the seat bottom. (3) A mechanical system gives the displacement of the entirety. The mechanical override control, installed under the legrest on the base operates this system.

K. Legrest (1) The legrest is hinged on the seat bottom. (2) A reduction gear actuator system gives the possibility to easily get the desired position. (3) A mechanical system gives the displacement of the legrest. The mechanical override control, installed under the legrest on the base operates this system. L.

Armrest The armrest is adjustable according to the occupant's needs, in low or high position. The command button installed on the armrest operates this system.

M. Seat Function Control Unit (1) The SFCU is installed on the armrest of the seat furniture console (refer to CMM 25-23-30 and 25-23-31). (2) The SFCU buttons operate the seat actuator electrically (see Figure 7). (a) The left side controls give to the seat occupant the possibility to adjust the seat in the desired position. (b) The right side controls give to the seat occupant the possibility to adjust the seat in the programmed positions.

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PAGE 8 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

BACKREST FORWARD DISPLACEMENT

BACKREST REARWARD DISPLACEMENT

SEAT BOTTOM REARWARD DISPLACEMENT TAKE OFF POSITION SEAT BOTTOM FORWARD DISPLACEMENT

LEGREST UPWARD DISPLACEMENT

LEGREST DOWNWARD DISPLACEMENT

SLEEPING POSITION

READING POSITION

SFCU FIGURE 7/ GRAPHIC 25-26-80-991-027-A01

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PAGE 9 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE 25-26-80-870-802-A01 2.

Operation A. SFCU (see Figure 8) 1

2

3

4

6

5

9

8

7

SFCU FIGURE 8/ GRAPHIC 25-26-80-991-028-A01 (1) Seat Back (a) The button (1) makes it possible to move the seat back to the rear position. Press on the button (1) until the desired position. (b) The button (2) makes it possible to raise the seat back. Press on the button (2) until the desired position. (2) Lumbar rest (a) To inflate the lumbar rest, push on the button (4) and release the button when you have the desired position. (b) To deflate the lumbar rest, push on the button (3) and release the button when you have the desired position. (3) Legrest (a) The button (6) makes it possible to move the legrest to the upper position. Press on the button (6) until the desired position. (b) The button (5) makes it possible to move the legrest to the lower position. Press on the button (5) until the desired position.

25-26-80

PAGE 10 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE (4) Seat positions (a) TTL position To put the seat in take off position, push on the button (7) and keep action on button (7) until seat moves toTTL position. (b) Bed position To put the seat in BED position, push on the button (9) and keep action on button (9) until seat moves to BED position. (c) Reading position The reading position is memorized by the IFE system, the occupant can get this position by pressing on the “reading position” button (8). and keeping action on button (8) until seat moves to reading position 1

Press the “reading position” button (8), to put the seat in this position.

2

Adjust the position with the differents adjustment buttons (see adjustment of the seat back, legrest and seat bottom).

B. Mechanical Override Control (see Figure 9) CAUTION : THE MECHANICAL OVERRIDE CONTROL MUST BE USED WITH THE SEAT FREE OF ANY LOAD. DO NOT USE THE ELECTRICAL AND MECHANICAL CONTROLS IN THE SAME TIME. (1) Seat back (a) Pull the lever (2), adjust manually the position of the seat back. (b) Release the lever for locked the position. (2) Lumbar rest (a) Pull the lever (1), adjust manually the position of the seat bottom. (b) Release the lever for locked the position. (3) Legrest (a) Pull the lever (3), adjust manually the position of the legrest. (b) Release the lever for locked the position.

25-26-80

PAGE 11 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

1 2 3

MECHANICAL OVERRIDE CONTROL VALID FOR FFCL5-01WY SERIES FIGURE 9/ GRAPHIC 25-26-80-991-029-A01

25-26-80

PAGE 12 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

1 2 3

MECHANICAL OVERRIDE CONTROL VALID FOR FFCL5-02WY SERIES FIGURE 10/ GRAPHIC 25-26-80-991-068-A01

25-26-80

PAGE 13 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-870-803-A01 Technical data A. Single seat Business class NOTE : The technical data are symetrical for two seats. (1) Seat in take of position :

1217,1 (47.92")

625 (24.6")

660,1 (26")

922,4 (36.32") 1125,6 (48.25")

TECHNICAL DATA VALID FOR FFCL5-01WY SERIES FIGURE 11 GRAPHIC 25-26-80-991-030-A01 (2) Seat in bed position:

544,4 (19.43")

1682,1 (66.22")

476,3 (16.75")

3.

TECHNICAL DATA VALID FOR FFCL5-01WY SERIES FIGURE 12 GRAPHIC 25-26-80-991-031-A01

25-26-80

PAGE 14 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE B. Single seat First class NOTE : The technical data are symetrical for two seats. (1) Seat in take of position :

479.9 (19")

1200 (47.24")

647.7 (25.5")

922,4 (36.32") 1125,6 (48.25")

TECHNICAL DATA VALID FOR FFCL5-02WY SERIES FIGURE 13 GRAPHIC 25-26-80-991-069-A01 (2) Seat in bed position:

433.4 (17.06")

476,3 (16.75")

1666 (65.6")

TECHNICAL DATA VALID FOR FFCL5-02WY SERIES FIGURE 14 GRAPHIC 25-26-80-991-070-A01

25-26-80

PAGE 15 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE C. Double seat Business class (1) Seat in take of position :

660,1 (26")

1217,2 (47.92")

478,4 (18.85")

1514,2 (59.61")

1682,1 (66.22")

TECHNICAL DATA VALID FOR FFCL5-01WY SERIES FIGURE 15 / GRAPHIC 25-26-80-991-032-A01

25-26-80

PAGE 16 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE D. Double seat First class (1) Seat in take of position :

478.9 (18.85")

1199.6 (47.22")

546.6 (21.51")

xxx (xxx")

1599.27 (62.96")

TECHNICAL DATA VALID FOR FFCL5-02WY SERIES FIGURE 16 / GRAPHIC 25-26-80-991-071-A01

25-26-80

PAGE 17 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

PAGE INTENTIONALLY LEFT BLANK

25-26-80

PAGE 18 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 TESTING AND FAULT ISOLATION TASK 25-26-80-700-801-A01 1.

Testing A. General (1) The aim of the tests is to check the adjustments and the components of the seat parts or mechanisms, in the operating position. (2) The defective parts are repaired in workshops or are replaced by serviceable parts. B. Job set-up information (1) Referenced information REFERENCE

NAME

25-26-80-991-032-A01 25-26-80-991-033-A01 25-26-80-991-034-A01 25-26-80-991-035-A01 25-26-80-991-036-A01

Figure 1001 Figure 1002 Figure 1003 Figure 1004 Figure 1005

C. Procedure NOTE : Connect the seat to a power supply unit 115 V / 400 Hz to make powered tests. (1) Functional test with electrical controls (see Figure 1001) NOTE : Put the seat switch in "ON" position. 2

1

3

4

5

6

SEAT FUNCTION CONTROL UNIT FIGURE 1001 / GRAPHIC 25-26-80-991-033-A01

25-26-80

PAGE 1001 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 (a) Testing of seat back/bottom reclining displacement (see Figure 1002) ACTION

RESULT

Rearward displacement: push the button (2).

The reduction gear actuator runs and moves the seat to the bed position. In maximun rear position, the motor stops.

Forward displacement: push the button (1).

The reduction actuator runs and moves the seat to the take off position. In maximum forward position, the motor stops.

80°

SEAT BACK RECLINING DISPLACEMENT FIGURE 1002 / GRAPHIC 25-26-80-991-034-A01

25-26-80

PAGE 1002 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 (b) Testing of the legrest displacement (see Figure 1003) NOTE : If there are an unwanted item between the legrest and the seat, an overcurrent system stops the motor to prevent any damage. ACTION

RESULT

Upward displacement: push the button (5).

The reduction gear actuator runs and the legrest goes up. In the maximum upper position, the motor stops.

Downward displacement: push the button (6).

The reduction gear actuator runs and the legrest goes down. In the maximum down position, the motor stops.

90°

LEGREST DISPLACEMENT FIGURE 1003 / GRAPHIC 25-26-80-991-035-A01

25-26-80

PAGE 1003 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 (c) Testing of the lumbar rest displacement ACTION

RESULT

Push the button (3).

The reduction gear actuator runs and moves the seat back panel to the forward position. In maximum forward position the motor stops.

Push the button (4).

The reduction gear actuator runs and moves the seat back panel to the rearward position. In maximum rearward position, the motor stops.

(2) Functional test with mechanical controls (see Figure 1004) NOTE : The mechanical controls override the electrical controls if electrical components are defective.

LUMBAR REST SEAT BACK LEG REST

MECHANICAL CONTROLS FIGURE 1004 / GRAPHIC 25-26-80-991-036-A01

25-26-80

PAGE 1004 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 (a) Testing the seat back/bottom displacement ACTION

RESULT

Push the control lever.

The seat back/bottom operates correctly, without any excessive wedge or gap.

Release the control lever.

The reclining seat back/bottom stays in the desired position.

(b) Testing the legrest displacement ACTION

RESULT

Push the control lever.

The legrest operates correctly, without any excessive wedge or gap.

Release the control lever.

The legrest stays in the desired position.

(c) Testing of the lumbar rest displacement ACTION

RESULT

Push the control lever.

The seat bottom panel operates correctly, without any excessive wedge or gap.

Release the control lever.

The seat bottom panel stays in the desired position.

25-26-80

PAGE 1005 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE (d) Testing of the armrest displacement (see Figure 1005) RESULT

Push the command button.

Moves the armrest to the upper or lower position.

Release the command button.

The armrest stays in the upper or lower position.

181,7 (7.15")

ACTION

ARMREST DISPLACEMENT VALID FOR FFCLX-01WY SERIES FIGURE 1005 / GRAPHIC 25-26-80-991-037-A01

25-26-80

PAGE 1006 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 TASK 25-26-80-700-802-A01 2.

Fault Isolation NOTE : When corrective actions are done, examine the seat again and make sure that the fault is corrected. A. Electrical fault isolation (1) Electrical displacement control of the seat back/bottom

TROUBLE PROBABLE CAUSE The control button is operated, Motor not supplied or poor but the reduction gear actuator power supply. does not run.

CORRECTION Do a check of the circuit breaker. Do a check of the motor power supply.

Defective wiring or connector.

Do a check of the wiring and the connectors. Replace if necessary.

Defective actuator.

Replace the actuator.

Defective Electronic Control Unit

Replace the ECU.

The seat back/bottom is in the maximum position and the reduction gear actuator runs.

Defective actuator.

Replace the actuator.

The reduction gear actuator is power supplied, but the motor hums and does not run.

One cable of the motor is disconnected (circuit breaker opened).

Make sure that the plug is correctly connected. Reset the circuit breaker if necessary.

Reduction gear actuator clutching defective (circuit breaker opened).

Replace the reduction gear actuator. Reset the circuit breaker if necessary.

Unwanted materials jammed into the rollers slides, the rack and the reduction gear.

Clean the rollers slides, the rack and the reductor gear. Reset the circuit breaker if necessary.

25-26-80

PAGE 1007 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 (2) Electrical displacement control of the lumbar rest TROUBLE PROBABLE CAUSE The control button is operated, Motor not supplied or poor but the reduction gear actuator power supply. does not run.

CORRECTION Do a check of the circuit breaker. Do a check of the motor power supply.

The reduction gear actuator is power supplied, but the motor hums and does not run.

Defective wiring or connector.

Do a check of the wiring and the connectors. Replace if necessary.

Defective actuator.

Replace the actuator.

One cable of the motor is disconnected (circuit breaker opened)

Make sure that the plug is correctly connected. Reset the circuit breaker if necessary.

Unwanted materials jammed into the rollers track.

Clean the rollers track.

(3) Electrical displacement control of the legrest TROUBLE PROBABLE CAUSE The control button is operated, Motor not supplied or poor but the reduction gear actuator power supply. does not run.

CORRECTION Do a check of the circuit breaker. Do a check of the motor power supply

The reduction gear actuator is power supplied, but the motor hums and does not run.

Defective wiring or connector.

Do a check of the wiring and the connectors. Replace if necessary.

Defective actuator.

Replace the actuator.

One cable of the motor is disconnected (circuit breaker opened).

Make sure that the plug is correctly connected. Reset the circuit breaker if necessary.

Reduction gear actuator clutching defective (circuit breaker opened).

Replace the reduction gear actuator. Reset the circuit breaker if necessary.

Unwanted materials jammed on Clean the rack. Reset the the rack and the reduction gear. circuit breaker if necessary.

25-26-80

PAGE 1008 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 B. Mechanical fault isolation (1) Mechanical control of the seat back/bottom TROUBLE PROBABLE CAUSE The seat back/bottom reclining Defective control cable or to put entirety does not operate. out of order.

CORRECTION Replace or adjust the cable if necessary.

Reduction gear actuator clutching Remove and replace the defective. reduction gear actuator. Difficult sliding movement of seat back/bottom reclining entirety.

Jammed bearing.

Lubricate or replace the bearing if necessary.

Untightened bearing.

Correctly tighten the screw that holds the bearing.

Unwanted materials jammed into the bearing races or seat back rack.

Clean the bearing races or seat back rack.

(2) Mechanical control of the lumbar rest TROUBLE The lumbar rest entirety does not operate.

PROBABLE CAUSE Defective control cable or to put out of order.

CORRECTION Replace or adjust the cable if necessary.

Reduction gear actuator clutching Remove and replace the defective. reduction gear actuator. Difficult sliding movement of lumbar rest entirety.

Jammed bearing.

Lubricate or replace the bearing if necessary.

Untightened bearing.

Correctly tighten the screw that holds the bearing.

Unwanted materials jammed into the bearing tracks.

Clean the bearing tracks.

25-26-80

PAGE 1009 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE (3) Mechanical control of the legrest TROUBLE The legrest entirety does not operate.

PROBABLE CAUSE Defective cable or to put out of order.

CORRECTION Replace or adjust the cable if necessary.

Reduction gear actuator clutching Remove and replace the defective. reduction gear actuator. Attaching parts of the legrest too tightened.

Correctly tighten and lubricate.

(4) Mechanical control of the armrest Valid for FFCLX-01WY0X-01 TROUBLE The armrest displacement does not operate.

PROBABLE CAUSE Defective cable or to put out of order.

CORRECTION Replace or adjust the cable if necessary.

Unwanted materials jammed on the tube.

Clean the tube.

25-26-80

PAGE 1010 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE SCHEMATIC AND WIRING DIAGRAMS 1.

Wiring diagram effectivity

X X

X X X X

X X

X

X

X

ASS650

X X X X X X

ASS640

X X X X X X

HAR659

HAR647

X

HAR651

HAR644

X X

HAR650

HAR641

X

HAR640

Seat P/N FFCL4-01WY03-01 FFCL4-02WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 FFCL5-02WY01-01 FFCL5-02WY02-01

FFCL1-4J5010-01D

FFCL1-4G1001-05

WIRING DIAGRAM

X X X X X X

X X

X X

X X

25-26-80

PAGE 2001 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

SCHEMATIC DIAGRAM P/N: FFCL1-4G1001-05 VALID FOR FFCLX-01WY SERIES FIGURE 2001 / GRAPHIC 25-26-80-991-038-A01

25-26-80

PAGE 2002 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

SCHEMATIC DIAGRAM P/N: FFCL1-4J5010-01D VALID FOR FFCLX-02WY SERIES FIGURE 2002 / GRAPHIC 25-26-80-991-072-A01

25-26-80

PAGE 2003 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

WIRING DIAGRAM P/N: HAR 640 (SHEET 1 OF 2) VALID FOR FFCLX-01WY SERIES FIGURE 2003 / GRAPHIC 25-26-80-991-039-A01

25-26-80

PAGE 2004 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

WIRING DIAGRAM P/N: HAR 640 (SHEET 2 OF 2) VALID FOR FFCLX-01WY SERIES FIGURE 2004 / GRAPHIC 25-26-80-991-040-A01

25-26-80

PAGE 2005 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

WIRING DIAGRAM P/N: HAR 641 VALID FOR FFCLX-01WY SERIES FIGURE 2005 / GRAPHIC 25-26-80-991-041-A01

WIRING DIAGRAM P/N: HAR 644 FIGURE 2006 / GRAPHIC 25-26-80-991-042-A01

25-26-80

PAGE 2006 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

WIRING DIAGRAM P/N: HAR 647 FIGURE 2007 / GRAPHIC 25-26-80-991-043-A01

25-26-80

PAGE 2007 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

WIRING DIAGRAM P/N: HAR 650 (SHEET 1 OF 2) VALID FOR FFCLX-02WY SERIES FIGURE 2008 / GRAPHIC 25-26-80-991- 073 -A01

25-26-80

PAGE 2008 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

WIRING DIAGRAM P/N: HAR 650 (SHEET 2 OF 2) VALID FOR FFCLX-02WY SERIES FIGURE 2009 / GRAPHIC 25-26-80-991- 074 -A01

25-26-80

PAGE 2009 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

WIRING DIAGRAM P/N: HAR 651 VALID FOR FFCLX-02WY SERIES FIGURE 2010 / GRAPHIC 25-26-80-991- 075 -A01

25-26-80

PAGE 2010 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

WIRING DIAGRAM P/N: HAR 659 VALID FOR FFCLX-02WY SERIES FIGURE 2011 / GRAPHIC 25-26-80-991- 076 -A01

25-26-80

PAGE 2011 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

WIRING DIAGRAM P/N: ASS 640 (SHEET 1 OF 2) VALID FOR FFCLX-01WY SERIES FIGURE 2012 / GRAPHIC 25-26-80-991-044-A01

25-26-80

PAGE 2012 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

WIRING DIAGRAM P/N: ASS 640 (SHEET 2 OF 2) VALID FOR FFCLX-01WY SERIES FIGURE 2012 / GRAPHIC 25-26-80-991-045-A01

25-26-80

PAGE 2013 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

WIRING DIAGRAM P/N: ASS 650 (SHEET 1 OF 3) VALID FOR FFCLX-02WY SERIES FIGURE 2013 / GRAPHIC 25-26-80-991- 077 -A01

25-26-80

PAGE 2014 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

WIRING DIAGRAM P/N: ASS 650 (SHEET 2 OF 3) VALID FOR FFCLX-02WY SERIES FIGURE 2013 / GRAPHIC 25-26-80-991-078-A01

25-26-80

PAGE 2015 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

WIRING DIAGRAM P/N: ASS 650 (SHEET 3 OF 3) VALID FOR FFCLX-02WY SERIES FIGURE 2013 / GRAPHIC 25-26-80-991-079-A01

25-26-80

PAGE 2016 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 DISASSEMBLY TASK 25-26-80-000-801-A01 1.

General A. The overhaul instructions contained in this manual are usually used in mechanical overhaul workshops. If you not do a fully overhaul, it is not necessary to remove the seat from the aircraft. B. It is not recommended to disassemble welded, bonded, riveted assemblies unless there is a defect. If disassembly is necessary, refer to the chapter (6001) REPAIR. C. You must not usually remove identification plates. If it is necessary to remove them, you must first get approval from the manufacturer. D. It is not recommended to fully disassemble the seat. If you must repair, consult the manufacturer. If not, only disassemble what is necessary to do the repairs or to replace defective part (s). E. When these instructions are applied, don't disassemble those components which are in good condition after inspection unless their disassembly is necessary to get access to the defective part. F.

You must identify all the parts before the disassembly to prevent errors and to make the reassembly easier. NOTE : The degree of disassembly will not be more than necessary.

G. For the identification of damage or functional failure refer to: - Chapter (5001)

CHECKING.

- Chapter (1001)

TESTING AND FAULT ISOLATION.

TASK 25-26-80-000-802-A01 2.

Preliminary Steps A. Cut off the electrical power supply.

25-26-80

PAGE 3001 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-020-801-A01 3.

Removal of the headrest A. Reason for the job Self-explanatory. B. Job set-up information (1) Referenced information REFERENCE

25-26-80-991-002-A01 25-26-80-991-059-A01 25-26-80-991-018-A01

NAME Figure 1 (sheet 2 of 2) Figure 1A (sheet 2 of 2) Figure 14 (sheet 1 of 2)

C. Job set-up None. D. Procedure (refer to IPL figure 14) (1) Remove the screws (140) and the washer (150). (2) Remove the angle (130). (3) Remove the headrest (250, IPL Figure 1) or the headrest (210, IPL Figure 1A) from the seat back (70, IPL Figure 1 and Figure 1A).

25-26-80

PAGE 3002 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-030-801-A01 4.

Disassembly of the headrest A. Reason for the job Self-explanatory. B. Job set-up information (1) Referenced information REFERENCE

25-26-80-020-801-A01 25-26-80-991-003-A01 25-26-80-991-018-A01 25-26-80-991-019-A01 25-26-80-991-063-A01

NAME Removal of the headrest Figure 2 Figure 14 (sheet 1 of 3) Figure 14 (sheet 2 of 3) Figure 14 (sheet 3 of 3)

C. Job set-up Removal of the headrest (refer to TASK 25-26-80-020-801-A01). D. Procedure (refer to IPL Figure 14) valid for FFCLx-01WY SERIES, Business class (1) Remove the cover (70, IPL Figure 2) and the foam (80, IPL Figure 2) from the headrest. NOTE : Store these covers and foams in a dry, dust free area. (2) Remove the screws (20), the washers (30) and the spacer (35). (3) Remove the bracket (170). (4) Remove the screws (190) and the washers (200). (5) Remove the slide (180). (6) Remove the screws (220) and the nuts (230). (7) Remove the spring blade (210).

25-26-80

PAGE 3003 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE E. Procedure (refer to IPL Figure 14) valid for FFCLX-02WY SERIES, First class (1) Remove the cover (70, IPL Figure 2) and the foams (80, 90 and 100 IPL Figure 2) from the headrest. NOTE : Store these covers and foams in a dry, dust free area. (2) Remove the screws (20), and the washers (30). (3) Remove the bracket (170). (4) Remove the screws (190) and the washers (200). (5) Remove the slide (180). (6) Remove the screws (220) and the nuts (230). (7) Remove the spring blade (210). (8) Remove the screws (310) and the washers (320) (9) Remove the hinge (300), the RH headrest (350) and the LH headrest (360). (10) Remove the screws (260), the washers (270) and the nuts (280). (11) Remove the hinge (250) and the headrest central (340).

25-26-80

PAGE 3004 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-020-802-A01 5.

Removal of the cushions A. Reason for the job Self-explanatory. B. Job set-up information (1) Referenced information REFERENCE

25-26-80-991-003-A01 25-26-80-991-046-A01

NAME Figure 2 Figure 3001

C. Job set-up Removal of the headrest (refer to TASK 25-26-80-020-801-A01). D. Procedure (refer to IPL figure 2) CAUTION : THE VELCRO HAS AN IMPORTANT ATTACHING, TAKE PRECAUTIONS IN ORDER TO NOT CAUSE DAMAGE TO THE COVER. (1) Remove the cover (30) and the foam (40) from the seat back. (2) Remove the cover (10) and the foam (20) from the seat bottom. (3) Remove the cover (50) and the foam (60) from the legrest.

25-26-80

PAGE 3005 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE SUBTASK 25-26-80-020-001 (4) Removal of the belt (a) Open the clip (1, Figure 3001) and disengage the belt (2, Figure 3001). 2 1

REMOVAL OF THE BELT FIGURE 3001 / GRAPHIC 25-26-80-991-046-A01

25-26-80

PAGE 3006 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-020-803-A01 6.

Removal of the seat from the pallet A. Reason for the job Self-explanatory. B. Job set-up information (1) Tools, fixtures and equipment REFERENCE

Qty

64300FFCL1-01CX01-01

1

NAME Assembly tool

(2) Referenced information REFERENCE 25-26-80-020-801-A01 25-26-80-020-802-A01 25-26-80-991-015-A01 25-26-80-991-060-A01 25-26-80-991-017-A01 25-26-80-991-020-A01 25-26-80-991-022-A01 25-26-80-991-047-A01 25-26-80-991-048-A01

NAME Removal of the headrest Removal of the cushions Figure 12 (sheet 1 of 2) Figure 12A (sheet 1 of 2) Figure 13 Figure 15 (sheet 1 of 2) Figure 16 (sheet 1 of 2) Figure 3002 Figure 3003

C. Job set-up Removal of the headrest (refer to TASK 25-26-80-020-801-A01). Removal of the cushions (refer to TASK 25-26-80-020-802-A01). D. Procedure (1) Single seat (refer to Figure 3002) NOTE : The seats are symmetrical, this procedure gives the removal of the right seat. (a) Disconnect the connectors P17 from J17, P21 from J21, P20 from J20 and P22 from J22. (b) Remove the quick wiring support (270, IPL Figure 12) or the quick wiring support (360, IPL Figure 12A). (c) Push on the command button (1) and put the armrest (2) in upper position valid for FFCLx-01WY SERIES.

25-26-80

PAGE 3007 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE (d) Put the seat in the bed position with the button (3) of the mechanical override control (e) Remove the screws (50, IPL Figure 13) and the washers (60, IPL Figure 13). (f) Remove the front covering (40, IPL Figure 13). (g) Remove the shrouds (4) attached by Velcro tape. (h) Lift up the seat bottom panel (5) to get access to the seat attachment. (i)

Install the assembly tool (6) (P/N: 64300FFCL1-01CX01-01) to keep the seat in bed position.

(j)

Remove the screws (7) and the covers (8).

(k) Remove the screws (9), the washers (10) and the plates (11). (l)

Take the seat by the assembly tool (6) and the crossbeam tube (12) and remove it from the pallet.

25-26-80

PAGE 3008 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

6

12

5 4

2 1 7 8

9 10 11

3 13

9 10 11

REMOVAL OF THE SINGLE SEAT FIGURE 3002 / GRAPHIC 25-26-80-991-047-A01

25-26-80

PAGE 3009 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE (2) Double seat (refer to Figure 3003) NOTE : The seats are symmetrical, this procedure gives the removal of the left seat. (a) Disconnect the connectors P17 from J17, P21 from J21, P20 from J20 and P22 from J22. (b) Remove the quick wiring support (270, IPL Figure 12) or the quick wiring support (360, IPL Figure 12A). (c) Remove the screws ( 50, IPL Figure 13) and the washers (60, IPL Figure 13). (d) Remove the front covering (40, IPL Figure 13). (e) Push on the command button (1) and put the armrest (2) in upper position valid for FFCLX-01WY0X-01. (f) Put the seat in the bed position with the button (3) of the mechanical override control. (g) Remove the shrouds (4) attached by Velcro tape. (h) Lift up the seat bottom panel (5) to get access to the seat attachment. (i)

Install the assembly tool (6) (P/N: 64300FFCL1-01CX01-01) to keep the seat in bed position.

(j)

Remove the screws (710, IPL Figure 16 sheet 1), the washers (720, 730, IPL Figure 16 sheet 1) and the connector support (700, IPL Figure 16).

(k) Remove the screws (7) and the covers (8). (l)

Remove the screws (9), the washers (10) and the plates (11).

(m) Take the seat by the assembly tool (6) and the crossbeam tube (12) and remove it from the lower part.

25-26-80

PAGE 3010 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE 6

2

6 4 4

1

12 3

5 7 8

9 10 11

9 10 11

REMOVAL OF THE DOUBLE SEAT FIGURE 3003 / GRAPHIC 25-26-80-991-048-A01

25-26-80

PAGE 3011 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-030-802-A01 7.

Disassembly of the pallet A. Reason for the job Self-explanatory. B. Job set-up information (1) Referenced information REFERENCE

25-26-80-020-803-A01 25-26-80-991-020-A01 25-26-80-991-021-A01 25-26-80-991-022-A01 25-26-80-991-023-A01

NAME Removal of the seat from the pallet Figure 15 (sheet 1 of 2) Figure 15 (sheet 2 of 2) Figure 16 (sheet 1 of 2) Figure 16 (sheet 2 of 2)

C. Job set-up Removal of the seat from the pallet (refer to TASK 25-26-80-020-803-A01). D. Procedure (1) Single seat (refer to IPL Figure 15) (a) Remove the screws (500) and the washers (510). (b) Remove the stud locking front (490) and keep the shims (520). (c) Remove the screws (610) and the springs (600). (d) Remove the anti-rattle pins (590). (e) Remove the screws (650 and 660) and the washers (670 and 680). (f) Remove the cover supports (640). (g) Remove the screws (400). (h) Remove the fitting (390). (i)

Remove the screws (470) and the washers (480).

(j)

Remove the pin (460).

(k) Remove the screws (540 and 560). (l)

Remove the stops (530 and 550).

25-26-80

PAGE 3012 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE (m) Remove the screws (580). (n) Remove the position indicator (570). (2) Double seat (refer to IPL Figure 16) (a) Remove the screws (520) and the washers (530). (b) Remove the stud locking front (510) and keep the shims (400). (c) Remove the screws (620) and the springs (610). (d) Remove the anti-rattle pins (600). (e) Remove the screws (660 and 670) and the washers (680 and 690). (f) Remove the cover supports (650). (g) Remove the screws (570). (h) Remove the stops (560). (3) Disassembly of the equipped track (refer to IPL Figure 15 or Figure 16) NOTE : Procedure is the same for all equipped track. (a) Remove the screws (20) and the washers (30). (b) Remove the equipped track (10). (c) Remove the screws (80) and the washers (90). (d) Remove the rack (70). (e) Remove the screw (270) and the washer (280). (f) Remove the stop (260) from the track (290). (g) Remove the screws (220, 230 and 240) and the washers (250). (h) Remove the equipped track (210).

25-26-80

PAGE 3013 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-020-804-A01 8.

Removal of the armrest A. Reason for the job Self-explanatory. B. Job set-up information REFERENCE

25-26-80-020-801-A01 25-26-80-020-802-A01 25-26-80-991-002-A01 25-26-80-991-009-A01

NAME Removal of the headrest Removal of the cushions Figure 1 (sheet 2 of 2) Figure 8

C. Job set-up Removal fo the headrest. (refer to TASK 25-26-80-020-801-A01). Removal of the cushions (refer to TASK 25-26-80-020-802-A01). D. Procedure (refer to IPL Figure 1) NOTE : The seats are symmetrical, this procedure is for the right seat and valid for FFCLX--01WY SERIES, Business class. (1) Lift up the seat bottom (80, IPL Figure 8) and remove the screws (160 and 170) and the washer (180). (2) Remove the armrest (150).

25-26-80

PAGE 3014 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-030-803-A01 9.

Disassembly of the armrest A. Reason for the job Self-explanatory. B. Job set-up information REFERENCE

25-26-80-020-804-A01 25-26-80-991-010-A01 25-26-80-991-011-A01

NAME Removal of the armrest Figure 9 (sheet 1 of 2) Figure 9 (sheet 2 of 2)

C. Job set-up Removal fo the armrest. (refer to TASK 25-26-80-020-804-A01). D. Procedure (refer to IPL Figure 9) NOTE : Valid for FFCLX-01WY0X-01 SUBTASK 25-26-80-030-002-A01 (1) Removal of the shrouds (a) Remove the screw cap (530). (b) Remove the screw (500). (c) Remove the armcap (490). (d) Remove the screw (420). (e) Remove the outer shroud (410). (f) Remove the screws (470) and the nuts (480). (g) Remove the inner shroud (460). (h) Remove the screws (440 and 450). (i)

Remove the lower shroud (430).

25-26-80

PAGE 3015 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE SUBTASK 25-26-80-030-003-A01 (2) Disassembly of the armrest structure (a) Unlock the armrest, compress the gas cylinder (60), remove the pin (70), the shoulderd pin (90) and the washer (80). (b) Remove the structure (170) from the mobile structure (390) and keep the cylinder (60) and the spacer (100). (c) Remove the screws (20), the washers (30) and the self-locking nuts (40). (d) Remove the button (10). (e) Remove the screw (340) and the self-locking nut (350). (f) Remove the clamp (330). (g) Remove the screw (290) and disengage the control cable (310) from the lock support (230) and the lever (270). (h) Remove the screws (240), the washers (250) and the self-locking nuts (260). (i)

Remove the lock support (230).

(j)

Remove the cotter pin (190), the washer (200) and the shouldered pin (210).

(k) Remove the lever (270) and keep the spacer (220) and the washer (200). (l)

Remove the screws (120 and 160).

(m) Remove the track (110) and keep the stop (140).

25-26-80

PAGE 3016 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-020-805-A01 10. Removal of the legrest A. Reason for the job Self-explanatory. B. Job set-up information REFERENCE 25-26-80-020-801-A01 25-26-80-020-802-A01 25-26-80-991-009-A01 25-26-80-991-012-A01

NAME Removal of the headrest Removal of the cushions Figure 8 Figure 10

C. Job set-up Removal of the headrest. (refer to TASK 25-26-80-020-801-A01). Removal of the cushions (refer to TASK 25-26-80-020-802-A01). D. Procedure (refer to IPL Figure 10) NOTE : The seats are symmetrical, this procedure is for the right seat. (1) Lift up the seat bottom (80, IPL Figure 8). (2) Remove the cotter pin (250), the washer (240) and the shouldered pin (230) (3) Remove the articulation pin (290), the washer (310) and the spacer (300). (4) Remove the equipped legrest (280).

25-26-80

PAGE 3017 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-030-804-A01 11. Disassembly of the legrest A. Reason for the job Self-explanatory. B. Job set-up information REFERENCE 25-26-80-020-805-A01 25-26-80-991-012-A01

NAME Removal of the legrest Figure 10

Job set-up Removal of the legrest. (refer to TASK 25-26-80-020-805-A01). C. Procedure (refer to IPL Figure 10) (1) Remove the screws (380) and the washers (390). (2) Remove the yoke (370). (3) Remove the screws (350) and the washers (360). (4) Remove the LH arm (330) and the RH arm (340) from the panel (320). (5) Remove the screw (270). (6) Remove the angle (260).

25-26-80

PAGE 3018 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-020-806-A01 12. Removal of the seat back and the seat bottom A. Reason for the job Self-explanatory. B. Job set-up information REFERENCE 25-26-80-020-801-A01 25-26-80-020-802-A01 25-26-80-991-002-A01 25-26-80-991-015-A01 25-26-80-991-060-A01 25-26-80-991-004-A01 25-26-80-991-047-A01

NAME Removal of the headrest Removal of the cushions Figure 1 (sheet 2 of 2) Figure 12 (sheet 1 of 2) Figure 12A (sheet 1 of 2) Figure 3 Figure 3002

C. Job set-up Removal of the headrest. (refer to TASK 25-26-80-020-801-A01). Removal of the cushions (refer to TASK 25-26-80-020-802-A01). D. Procedure (refer to IPL Figure 1) NOTE : The seats are symmetrical, this procedure is for the right seat. (1) Put the seat in the bed position with the button (3, Figure 3002) of the mechanical override control installed on the structure. (2) Lift up the seat bottom panel (80) and mark the position of the gears. NOTE : The position must be the same at the reassembly. (3) Remove the cable clamps and disconnect the connector and the mechanical control cable of the lumbar rest actuator (120, IPL Figure 12 and Figure 12A). (4) Remove the cotter pins (130), the washer (100 and 120) and the pins (90 and 110). (5) Remove the ring retainer (340, IPL Figure 3) and the shouldered pin (330, IPL Figure 3). (6) Remove the seat back (70), the seat bottom (80) and keep the spacer (140).

25-26-80

PAGE 3019 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-030-805-A01 13. Disassembly of the seat back A. Reason for the job Self-explanatory. B. Job set-up information (1) Referenced information REFERENCE 25-26-80-020-806-A01 25-26-80-991-002-A01 25-26-80-991-058-A01 25-26-80-991-008-A01 25-26-80-991-015-A01 25-26-80-991-060-A01 25-26-80-991-017-A01 25-26-80-991-018-A01 25-26-80-991-019-A01

NAME Removal of the seat back and the seat bottom Figure 1 (sheet 1 of 2) Figure 1A (sheet 1 of 2) Figure 7 Figure 12 (sheet 1of 2) Figure 12A (sheet 1of 2) Figure 13 Figure 14 (sheet 1 of 3) Figure 14 (sheet 2 of 3)

C. Job set-up Removal of the seat back and the seat bottom (refer to TASK 25-26-80-020-806-A01). D. Procedure (refer to IPL Figure 7) (1) Remove the lateral shrouds (120 and 130, IPL Figure 13) attached by Velcro tape. (2) Remove the screws (140, IPL Figure 13). (3) Remove the seat back covering (110, IPL Figure 13). (4) Remove the screws (20). (5) Remove the mobile structure (10). (6) Remove the screws (40) and the washers (50). (7) Remove the roller tracks (30). (8) Remove the screws (70). (9) Remove the stops (60). (10) Remove the screw (90), the washer (100) and the spacer (110). (11) Remove the wiring supports (80).

25-26-80

PAGE 3020 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE (12) Remove the screws (260, IPL Figure 1) or (220, IPL Figure 1A) and the washers (270, IPL Figure 1) or or (230, IPL Figure 1A). (13) Remove the headrest fitting (10, IPL Figure 14) from the mobile structure (10). (14) Remove the screws (100, IPL Figure 14) and the washers (110, IPL Figure 14) and the spacers (120, IPL Figure 14). (15) Remove the shim (90, IPL Figure 14) from the fitting (10, IPL Figure 14). (16) Remove the screws (50, IPL Figure 14) and the self locking nuts (60, IPL Figure 14). (17) Remove the tracks (70 and 80, IPL Figure 14) from the fitting (10, IPL Figure 14) (18) Removal of the lumbar actuator (a) Disconnect the bonding braid of the lumbar rest actuator (120, IPL Figure12 and Figure 12A) and remove the screws (130, IPL Figure12 and Figure 12A) and the washers (140, IPL Figure12 and Figure 12A). (b) Remove the lumbar rest actuator (120, IPL Figure12 and Figure 12A). (19) Remove the screws (150). (20) Remove the hinge (140). (21) Remove the screws (170). (22) Remove the lower panel (160) and keep the spacers (180). (23) Remove the screws (310) and the washers (320). (24) Remove the panel (300). (25) Remove the screws (200) and the washers (210). (26) Remove the fitting (340 and 400) from the lower panel (190). (27) Remove the cotter pins (370 and 430), the washers (380 and 440) and the shouldered pins (360 and 420). (28) Remove the rollers (350 and 410).Remove the screws (260, 290), the washers (280) and the spacers (270). (29) Remove the wiring supports (250). (30) Remove the screws (230) and the washers (240). (31) Remove the connector supports (220).

25-26-80

PAGE 3021 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-030-806-A01 14. Disassembly of the seat bottom A. Reason for the job Self-explanatory. B. Job set-up information (1) Referenced information REFERENCE 25-26-80-020-806-A01 25-26-80-991-009-A01

NAME Removal of the seat back and the seat bottom Figure 8

C. Job set-up Removal of the seat back and the seat bottom (refer to TASK 25-26-80-020-806-A01). D. Procedure (refer to IPL Figure 8) (1) Remove the cotter pins (30), the washers (10, 20, 40) and the shouldered pins (50). (2) Remove the RH and LH fittings (60 and 70) and keep the washers (10). (3) Remove the screws (100) and the washers (110). (4) Remove the yokes (90) from the panel (120).

25-26-80

PAGE 3022 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-030-807-A01 15. Disassembly of the base A. Reason for the job Self-explanatory. B. Job set-up information (1) Referenced information REFERENCE 25-26-80-020-803-A01 25-26-80-020-805-A01 25-26-80-020-806-A01 25-26-80-991-004-A01 25-26-80-991-005-A01 25-26-80-991-006-A01 25-26-80-991-007-A01 25-26-80-991-012-A01 25-26-80-991-014-A01 25-26-80-991-016-A01 25-26-80-991-061-A01 25-26-80-991-017-A01

NAME Removal of the seat from the pallet Removal the legrest Removal the seat back and the seat bottom Figure 3 Figure 4 Figure 5 Figure 6 Figure 10 Figure 11 (sheet 2 of 2) Figure 12 (sheet 2 of 2) Figure 12A (sheet 2 of 2) Figure 13

C. Job set-up Removal of the seat from the pallet (refer to TASK 25-26-80-020-803-A01). Removal of the legrest (refer to TASK 25-26-80-020-805-A01). Removal of the seat back and the seat bottom (refer to TASK 25-26-80-020-806-A01). D. Procedure (refer to IPL Figure 3) (1) Remove the cable clamps (60, IPL Figure 11). (2) Disconnect the connectors and the bonding braids of the crossbeam actuator (70, IPL Figure 12 and Figure 12A) and of the legrest actuator (40, IPL Figure 12 and Figure 12A). (3) Remove the electrical wiring (refer to IPL Figure 12 and Figure 12A). (4) Disconnect the mechanical control cable of the electromagnet (130) of the crossbeam actuator (70, IPL Figure 12) and of the legrest actuator (40, IPL Figure 12 and Figure 12A). (5) Remove the screws (30, IPL Figure 13). (6) Remove the rear covering (20, IPL Figure 13).

25-26-80

PAGE 3023 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE SUBTASK 25-26-80-030-004-A01 (7) Disassembly of the legrest actuator mecanism (a) Remove the screws (20, IPL Figure 10) and the washers (30, IPL Figure 10). (b) Remove the legrest mecanism (10, IPL Figure 10) and the legrest actuator (40, IPL Figure 12 and Figure 12A) from the front crossbeam (230). (c) Remove the screws (50, IPL Figure 12 and Figure 12A) and the washers (60, IPL Figure 12 and Figure 12A). (d) Remove the actuator (40, IPL Figure 12 and Figure 12A) from the legrest mechanism (10, IPL Figure10). (e) Remove the spring pins (80 and 90, IPL Figure 10). (f) Remove the pin (70, IPL Figure 10) and keep the gear (100, IPL Figure 10), the bearing (110, IPL Figure10), and the spacer (160 and 180, IPL Figure 10). (g) Remove the screw (50, IPL Figure 10) and the stop (40, IPL Figure 10). (h) Remove the rack (60, IPL Figure 10). SUBTASK 25-26-80-030-005-A01 (8) Removal of the front crossbeam (a) Remove the screws (240 and 410) and the washers (250 and 430). (b) Remove the front crossbeam (230). SUBTASK 25-26-80-030-006-A01 (9) Disassembly of the front crossbeam (a) Remove the retainer rings (30) and the shouldered pins (20). (b) Remove the links (10). (c) Remove the retainer rings (50), the washers (70) and the shouldered pins (60). (d) Remove the elbowed links (80) and keep the rollers (40). (e) Remove the screws (270) and the washers (280). (f) Remove the bearings (260).

25-26-80

PAGE 3024 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE SUBTASK 25-26-80-030-007-A01 (10) Removal of the rear crossbeam (a) Remove the screws (190 and 210) and the washers (200 and 220). NOTE : If you remove the rear crossbeam before the seat back, mark the position of the gears. The position must be the same at the reassembly. (b) Remove the rear crossbeam (180). SUBTASK 25-26-80-030-008-A01 (11) Disassembly of the rear crossbeam (a) Remove the spring pins (480 and 490, IPL Figure 4) and slide the coupling bush (470, IPL Figure 4) from the actuator pin. (b) Remove the screws (80, IPL Figure 12 and Figure 12A), the spacers (90, IPL Figure 12 and Figure 12A), the washers (100, IPL Figure 12 and Figure 12A) and the self-locking nuts (110, IPL Figure 12 and Figure 12A). (c) Remove the actuator (70, IPL Figure 12 and Figure 12A) from the rear crossbeam (180). CAUTION : DO NOT DISASSEMBLE THE BEARING ASSY (40 AND 250). SUBTASK 25-26-80-030-009-A01 (12) Removal of the LH and RH fittings (a) Remove the screws (130, IPL Figure 11). (b) Remove the override system control (50, IPL Figure 11). (c) Disconnect the mechanical control cable. (d) Remove the screws (360, IPL Figure 5) and the washers (370, IPL Figure 5). (e) Remove the tube (80, IPL Figure 5) from the RH fitting (90, IPL Figure 5) and the LH fitting (270, IPL Figure 5). (f) Remove the screws (420) and the washers (430). (g) Remove the ECU support equipped (400) from the RH fitting (90, IPL Figure 5) and the LH fitting (270, IPL Figure 5).

25-26-80

PAGE 3025 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE SUBTASK 25-26-80-030-010-A01 (13) Disassembly of the LH and RH fittings (a) Remove the screw (110 and 290, refer to IPL Figure 5), the washer (130 and 310, refer to IPL Figure 5) and the bush (120 and 300, refer to IPL Figure 5). (b) Remove the belt fastener (100 and 280, refer to IPL Figure 5) and the belt (30, IPL Figure 1and Figure 1A). (c) Remove the screws (100), the washers (110) and the self-locking nuts (120). (d) Remove the electromagnet (90). SUBTASK 25-26-80-030-011-A01 (14) Disassembly of the ECU support equipped (a) Remove the screws (20, IPL Figure 12 and Figure 12A), the washers (30, IPL Figure 12 and Figure 12A). (b) Remove the ECU (10, IPL Figure 12 and Figure 12A). (c) Remove the screws (20 and 30, IPL Figure 6), the washers (40, IPL Figure 6). (d) Remove the support ECU (10, IPL Figure 6). (e) Remove the screws (90, IPL Figure 6), the washers (100, IPL Figure 6) and the spacers (110, IPL Figure 6). (f) Remove the connector support (80, IPL Figure 6).

25-26-80

PAGE 3026 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 CLEANING TASK 25-26-80-100-801-A01 1.

General A. You must clean the seat fully before you do inspections for defects. B. Cleaning removes accumulations and deposits of residue which can affect the performance of the equipment and leads to the repair. CAUTION : DURING THE CLEANING, PROTECT THE ACTUATOR, HARNESS, SWITCH AND RECLINE LOCK. DRY THE SEAT AFTER CLEANING.

TASK 25-26-80-100-802-A01 2.

Polycarbonate shroud A. Reason for the job Self-explanatory. B. Job set-up information (1) Consumables REFERENCE

Qty AR

NAME Soap

C. Job set-up None. D. Procedure CAUTION : DO NOT USE CHLORINATED SOLVENTS, METHYL ALCOHOL, ACETONE AND DETERGENTS MADE OF AMMONIA AGENTS OR ALKALINE TO CLEAN POLYCARBONATE SHROUD. STEAM CLEANING IS STRICTLY FORBIDDEN. THE USE OF THESE PRODUCTS OR PROCEDURES WILL AFFECT THE MATERIEL PROPERTY, THEN IT BECOMES BRITTLE (1) Be careful when you clean all plastics. Alcohol or bleaches based agents will never have to be used to clean any plastics materials. (2) All plastic surfaces should be cleaned with a mild soap (PH<7) and water solution. (3) Mix the soap with the water to get the desired concentration for cleaning purposes. (4) Apply the solution directly to the surface and rub with a clean cloth to loosen any dirt. (5) Flush with clear water, and then clean with a dry cloth.

25-26-80

PAGE 4001 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 TASK 25-26-80-100-803-A01 3.

General cleaning A. Reason for the job Self-explanatory. B. Job set-up information (1) Consumables REFERENCE

Qty

TURCO INTERIOR CLEANER

AR

NAME Detergent

C. Job set-up None. D. Procedure (1) For usual applications, mix approximately 1 part of "TURCO INTERIOR CLEANER" to 10 or 15 parts of water. (2) Apply with a sponge, cloth,... (3) Clean the surfaces with a soft, dry cloth. (4) Stubborn spots need application of more concentrated solution. NOTE : There are no limits of application. You must apply safety on all metals, high strength steel, painted surfaces, plastic surfaces and leather.

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PAGE 4002 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 TASK 25-26-80-100-804-A01 4.

Electrical parts A. Reason for the job Self-explanatory. B. Job set-up information (1) Consumables REFERENCE

1001 MIL-D-12491

Qty AR AR

NAME KF Spray Can F2 Solvent degreaser

C. Job set-up None. D. Procedure (1) Clean exterior of electrical parts with a cloth moist with solvent degreaser. (2) Remove tarnish from pins on connectors using a KF spray can.

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PAGE 4003 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 TASK 25-26-80-100-805-A01 5.

Seat cover A. Reason for the job Self-explanatory. B. Job set-up information (1) Consumables REFERENCE

Qty

TURCO INTERIOR CLEANER

AR AR AR AR AR AR AR AR AR AR AR

NAME Ammonia Benzene Carbon tetrachloride Denatured alcohol Deodorant spray Hydrogen peroxide Oleic acid Oxalic acid Soap Sodium hypchlorite solution Detergent

C. Job set-up Remove the foam from the cover. D. Procedure (1) Fabric cover For a complete cleaning of the fabric cover, EADS SOGERMA recommends the application of a dry cleaning treatment. NOTE : Before complete cleaning, apply hook velcro tapes on the velvet velcro tapes of cover to protect it. It is easier to clean fabric cover if you identify the stains before cleaning treatment. Below, you give a selection of recommended methods to remove stains. Make sure that all chemicals used are fully dry removed after cleaning. If a smelling still remains, you can use a deodorant spray. (a) Airsickness, Grease and Oil Apply detergent added with a little ammonia at a temperature of about 60°C (140°F). You can remove grease residue by local treatment with carbon tetrachloride.

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PAGE 4004 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 (b) Blood Clean with cold water and rub with a cloth wet with hydrogen peroxide. (c) Enamel, Paint and Lacquer Clean with one part Benzole to one part denatured alcohol. (d) General Dirt Apply detergent up to 60° C (140° F). (e) Ink Apply a solution of oxalic acid at 60° C (140° F) then flush fully with water and apply detergent and ammonia at 60° C (140° F). Oleic acid and ammonia followed by weak sodium hypchlorite solution can remove colored inks. (f) Mildew, Iron Mould You can remove some drainage marks if you apply detergent and ammonia at 60° C (140° F). You must apply oxalic acid followed by an ammonia treatment 60° C (140°F) on iron marks. (g) Urine Clean with detergent and water. (2) Leather cover CAUTION : NEVER USE A SOLVENT OR A DETERGENT ON LEATHER. Clean the leather with soap and water. (3) Mixed cover (fabric and leather) Not apply a dry cleaning treatment. When you clean the fabric, take precaution to not overflow the leather.

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PAGE 4005 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 TASK 25-26-80-100-806-A01 6.

Metal parts A. Reason for the job Self-explanatory. B. Job set-up information (1) Consumables REFERENCE

MIL-C-10578 PD680 type 1 SOCOSOLV 97T

Qty AR AR AR

NAME Corrosion removing compound White spirit Cleaner

C. Job set-up None. D. Procedure (1) Clean the metal parts with White Spirit. Rub with a dry lint-free cloth and let to dry in air. (2) Remove any stains or deposits remaining after application of White Spirit using a cloth soaked with SOCOSOLV 97T. (3) Remove any traces of corrosion with the corrosion removing compound. NOTE : switch and recline lock. dry the seat after cleaning.

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PAGE 4006 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 TASK 25-26-80-100-807-A01 7.

Seat belt A. Reason for the job Self-explanatory. B. Job set-up information (1) Consumables REFERENCE

AERO-CLEAN X-200

Qty AR

NAME Seat belt cleaner

C. Job set-up None. D. Procedure CAUTION : DO NOT USE A SOLVENT BASE AGENT OR CETONE BASE AGENTS. NOTE : The metallic parts shall be suitably masked to prevent ingress of the cleaning agent. (1) Use a standard mop and water with the mop or the sponge must always be kept clean.

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PAGE 4007 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 TASK 25-26-80-100-808-A01 8.

Leather A. Reason for the job Self-explanatory. B. Job set-up information (1) Consumables REFERENCE

Qty

Leather strong cleaner

AR

NAME Leather cleaner

C. Job set-up None. D. Procedure CAUTION : DON’T USE ANY DETERGENTS. (1) Interim cleaning For the interim cleaning, we recommend to use light soap water applied by a sponge or a soft cloth. Then wipe off the soap water with fresh water and dry with a soft cloth. (2) Main cleaning CAUTION : DON’T RUB WITH THE SPONGE. NOTE : This is a deep cleaning using cleaning fluids for leather. (a) Wet a sponge with the cleaner. (b) Clean the leather with lightly circular movements. (c) Dry up gently with a clean cloth. (d) Let dry for at least 30 minutes.

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PAGE 4008 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 INSPECTION/CHECK TASK 25-26-80-200-801-A01 1.

General A. To do all checks, refer to the check procedures. Record all damage you find to trace the frequency and in some conditions the reason and/or source. You must repair immediately all damage you find. B. Visually examine all hardware, detail parts, sub-assemblies and assemblies for the criteria that follows : (1) Wear, tears, fraying of fabric. (2) Good attachment and condition of Velcro tapes. (3) Tightening of screws and nuts. (4) Condition of structural parts. (5) Condition of welds and riveting. (6) Condition of paint and surface treatment. (7) Attachment and condition of identification plates. (8) Electrical wiring breaks or worn insulation. (9) Signs of overheating, arcing, corrosion or physical damage on electrical parts. C. Use a strong light and we recommend some means of magnification. Use an inspection mirror to examine all unexposed surfaces. D. Skilled personnel must perform all repair and, if no physical values are available, he can still measure the condition.

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PAGE 5001 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 TASK 25-26-80-210-801-A01 2.

Check Procedure A. Structure and lower parts Seat installed YES NO

- Examine the structure in general for evidence of scratches, cracks, holes and damages. - Examine damaged coating and other possible surface damages. - Examine if corrosion is present. - Examine the areas that are not easily accessible for prevent the corrosion.

X

X

X

X

X

X

X

X

B. Screwed and riveted connections Seat installed YES NO - Examine screwed and riveted connections for a firm seating

X

X

C. Label Seat installed YES NO - Examine the labels for a correct attachment and location

X

X

D. Electrical system Seat installed YES NO - Examine wires and electrical components for attachment, damage and overheating signs. - Examine the connections if they are clean. - Examine the connectors for loose, broken and missing pins or contacts sockets. - Examine the terminal lugs for firm connection on the wire ends. - Examine the sealing and the coating of the ground points.

25-26-80

X

X

X

X

X

X

X

X

X

X

PAGE 5002 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 E. Seat back Seat installed YES NO - Examine the good operation. - Examine the articulation for corrosion. - Examine the pinion for the correct condition and the shaft of the rear crossbeam.

F.

X

X

X

X

X

X

Base Seat installed YES NO

- Examine the pinion for the correct condition and the shaft of the rear crossbeam. - Examine the belt of the rear crossbeam

X

X

X

X

G. Armrest Seat installed YES NO - Examine the good articulation and locking. - Examine if it is clean.

X

X

X

X

H. Legrest Seat installed YES NO - Examine the good articulation and locking. - Examine the tracks for the correct condition. - Examine if it is clean.

25-26-80

X

X

X

X

X

X

PAGE 5003 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 TASK 25-26-80-200-802-A01 3.

Replacement of Parts A. After inspection of all items, make a list of defective parts to be replaced and those which need repair or a new protection. NOTE : It is mandatory to replace self locking nuts, lock washers and pins.

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PAGE 5004 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 REPAIR TASK 25-26-80-300-801-A01 1.

General A. In general, to repair the seat, refer to this procedure except for the riveted and welded parts. The manufacturer must repair damage on riveted or welded junctions

TASK 25-26-80-300-802-A01 2.

Metal Parts A. Reason for the job Self-explanatory. B. Job set-up information (1) Consumables REFERENCE

MIL-C-5541 S1590 TURCO 1495 VERT RAL 6001 404-12-70PX 404-12-71PR-7 404-12-864E 4080K201 414-12-9110 4635-3600 54614048PU66 6345-4502

Qty

NAME

AR AR AR AR AR AR AR AR AR AR AR AR AR

Abrasive paper Alodine 1200 Yellow primary paint Abrasive cloth for aluminum Bright glycero paint Grey paint Paint pantone 5C Beige braun paint Black paint White primary paint Green primary paint (PAC33) Glossed red paint Glossed red paint

C. Job set-up None. D. Procedure (1) Minor scratches Sand and polish minor scratches with an abrasive or crocus cloth (steel parts only) and with aluminum monoxide cloth (aluminum parts only). (2) Protection and painting You must protect all parts chemically (alodine, etc...) and paint them with yellow primary paint (S1590).

25-26-80

PAGE 6001 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-300-803-A01 3.

Decor location A. Reason for the job Self-explanatory. B. Job set-up information (1) Consumables REFERENCE

Qty

L25LR0093616360 01286-15 4080K201 404-12-864E

AR AR AR AR

NAME Leather LANTAL cognac Fabric GLIDE/RUM ROHI Black paint Beige braun paint

(2) Referenced information REFERENCE 25-26-80-991-049-A01

NAME FIGURE 6001

C. Job set-up None. D. Procedure None.

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PAGE 6002 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

L25LR0093616360

404-12-864E

01286-15

01286-15 404-12-864E 4080K201

01286-15

L25LR0093616360

VALID FOR FFCLX-01WY SERIES, BUSINESS CLASS

L25LR0093616360

404-12-864E

01286-15

01286-15 404-12-864E 4080K201

01286-15

DECOR VALID FOR FFCLX-02WY SERIES, FIRST CLASS FIGURE 6001 / GRAPHIC 25-26-80-991-049-A01

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PAGE 6003 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-300-804-A01 4.

Electrical parts A. Reason for the job Self-explanatory. B. Job set-up information (1) Consumables REFERENCE

Qty AR AR AR AR AR

4125-6407 CAF4 MIL-D-12491 NSA8420-2

NAME Abrasive paper Electrical bonding lacquer Sealant Solvent degreaser Lacing tapes

(2) Referenced information REFERENCE 25-26-80-991-050-A01 25-26-80-991-051-A01

NAME FIGURE 6002 FIGURE 6003

C. Job set-up None. D. Procedure (1) Cable tying procedure for routing cable attachments (a) Do a knot around the bundle (1) with the lacing tape (2) as shown on the figure. (b) Then do a simple terminal knot that will be cut (with scissors) to 6mm on the two ends of the lacing tape (2). (c) Put a drop of sealant (3) on the knots. NOTE : The operating temperature of the lacing tape is –55°C (-131°F) to +232°C (+450°F).

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PAGE 6004 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

CABLE TYING FIGURE 6002 / GRAPHIC 25-26-80-991-050-A01 (2) Bonding point (a) Remove the surface protection (Alodine, paint, bonding lacquer, etc..) from the contact zone with abrasive paper. (b) Clean the contact areas with a cloth moist with solvent degreaser. (c) Assemble the attachments of the bonding point (the nuts, the conductive bolts and screws, the bonding strap). (d) Apply electrical bonding lacquer (P/N: 4125-6407) on the bonding point.

BONDING POINT FIGURE 6003 / GRAPHIC 25-26-80-991-051-A01

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PAGE 6005 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-300-805-A01 5.

Repair procedure for leather A. Reason for the job Self-explanatory. B. Job set-up information (1) Consumables REFERENCE

Qty

EMFI 30055A

AR

NAME Adhesive

(2) Referenced information REFERENCE

NAME

25-26-80-991-052-A01 25-26-80-991-053-A01 25-26-80-991-054-A01

FIGURE 6004 FIGURE 6005 FIGURE 6006

C. Job set-up None. D. Procedure (1) Type of damage: Upholstery (Leather or “ultra leather” or fabric) is torn.

EXAMPLE OF A TYPICAL DAMAGE FIGURE 6004 / GRAPHIC 25-26-80-991-052-A01

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PAGE 6006 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE (2) Damage evaluation: Only the covering “skin” is torn, support or structure is safe. Damaged area must not exceed 100cm² (16sq.inch) see Fig. 6006. (3) Repair principle: Reposition the “skin” to avoid tear extension and to give a better aspect until the part is changed with a new one. (4) Repair material: - Adhesive EMFI 30055A, - Cleaner/degreaser product, - Adhesive tape (5) Repair process: (a) Trim all threads in excess. (b) Clean surface and gently degrease with solvent. (c) Bond “skin” in place.

THE SAME PART AFTER REPAIR FIGURE 6005 / GRAPHIC 25-26-80-991-053-A01

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PAGE 6007 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE Alternative repair method can be used by inserting a piece of tape (adhesive facing up) between skin and support (as shown on Fig. 6006).

tearing Adhesive tape Maxi. 100mm (4 in.)

Maxi. 100mm (4 in.)

FIGURE 6006 / GRAPHIC 25-26-80-991-054-A01

25-26-80

PAGE 6008 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-300-806-A01 6.

Velcro tape A. Reason for the job Self-explanatory. B. Job set-up information (1) Consumables REFERENCE

Qty

SOCOSOLV 97T

AR

NAME Cleaner

C. Job set-up None. D. Procedure (1) Velcro tape part number SD1-XXX-XXX-YZ

001: adhesive tape 002: none adhesive tape

001: hook tape 002: velvet tape

Y, width: 1 = 10mm 2 = 16mm 3 = 20mm 4 = 25mm 5 = 30mm 6 = 38mm 7 = 50mm 8 = 100mm

Z, color:

0 = white 1 = beige 2 = navy blue 3 = claret 4 = green 5 = black 6 = grey

(2) Replacement (a) Remove the "Velcro" tape. (b) Clean the traces of adhesive or of residues with SOCOSOLV 97T. (c) Install a new "Velcro" tape.

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PAGE 6009 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

PAGE INTENTIONALLY LEFT BLANK

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PAGE 6010 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 ASSEMBLY TASK 25-26-80-400-801-A01 1.

General A. Before assembly, be sure that you do CLEANING, CHECK and REPAIR operations for all parts. B. After replacement of a damaged or worn part, install the seat as we show in the paragraphs that follow. C. If possible, use new and original approved parts. D. Replace self-locking nuts and pins after a disassembly.

25-26-80

PAGE 7001 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 TASK 25-26-80-430-801-A01 2.

Assembly of the pallet A. Reason for the job Self-explanatory. B. Job set-up information (1) Referenced information REFERENCE

25-26-80-991-020-A01 25-26-80-991-021-A01 25-26-80-991-022-A01 25-26-80-991-023-A01

NAME Figure 15 (sheet 1 of 2) Figure 15 (sheet 2 of 2) Figure 16 (sheet 1 of 2) Figure 16 (sheet 2 of 2)

C. Job set-up None. D. Procedure (1) Assembly of the equipped track (refer to IPL Figure 15 or Figure 16) NOTE : Procedure is the same for all equipped track. (a) Install the stop (260) on the track (290) with the screws (270) and the washers (280). (b) Install the equipped track (210) on the equipped track (10) with the screws (220, 230 and 240) and the washers (250). (c) Install the rack (70) on the track (100) with the screws (80) and the washers (90). (d) Install the equipped track (10) on the lower part with the screws (20) and the washers (30). (2) Single seat (refer to IPL Figure 15) (a) Install the position indicators (570) on the pallet (790) with the screws (580). (b) Install the stops (530 and 550) on the pallet (790) with the screws (540 and 560). (c) Install the pin (460) with the screws (470) and the washers (480). (d) Install the fitting (390) with the screws (400). (e) Install the cover supports (640) with the screws (650 and 660) and the washers (670 and 680).

25-26-80

PAGE 7002 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01

(f) Install the anti-rattle pin (590) with the screws (610) and the springs (600). (g) Install the locking blocks (490) with the shim (520), the screws (500) and the washers (510). (3) Double seat (refer to IPL Figure 16) (a) Install the stops (560) on the pallet (750) with the screws (540 and 560). (b) Install the cover supports (650) with the screws (660 and 670) and the washers (680 and 690). (c) Install the anti-rattles pins (600) with the screws (620) and the springs (610). (d) Install the locking blocks (510) with the shims (400), the screws (520), and the washers (530).

25-26-80

PAGE 7003 FEV 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-430-802-A01 3.

Assembly of the base A. Reason for the job Self-explanatory. B. Job set-up information (1) Referenced information REFERENCE

25-26-80-820-001-A01 25-26-80-820-801-A01 25-26-80-991-004-A01 25-26-80-991-005-A01 25-26-80-991-006-A01 25-26-80-991-007-A01 25-26-80-991-012-A01 25-26-80-991-016-A01 25-26-80-991-061-A01 25-26-80-991-017-A01

NAME Electromagnet adjustment Actuator calibration Figure 3 Figure 4 Figure 5 Figure 6 Figure 10 Figure 12 (sheet 2 of 2) Figure 12A (sheet 2 of 2) Figure 13

C. Job set-up None. D. Procedure (refer to IPL Figure 3) SUBTASK 25-26-80-430-001-A01 (1) Assembly of the ECU support equipped (a) Install the connector support (80, IPL Figure 6) on the equipped support ECU (400) with the screws (90, IPL Figure 6), the washers (100, IPL Figure 6) and the spacers (110, IPL Figure 6). (b) Install the support ECU (10, IPL Figure 6) on the equipped support ECU (400) with the screws (20 and 30, IPL Figure 6) and the washers (40, IPL Figure 6). (c) Install the ECU (10, IPL Figure 12 and Figure 12A) on the support ECU (400) with the screws (20, IPL Figure 12 and Figure 12A) and the washers (30, IPL Figure 12 and Figure 12A). (d) Install the ECU (10, IPL Figure 12 and Figure 12A) on the support ECU (400) with the screws (20, IPL Figure 12 and Figure 12A) and the washers (30, IPL Figure 12 and Figure 12A).

25-26-80

PAGE 7004 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE SUBTASK 25-26-80-430-002-A01 (2) Assembly of the LH and RH fitting (a) Install the electromagnet (90) on the LH fitting (270, IPL Figure 5) and RH fitting (90, IPL Figure 5) with the the screws (100), the washers (110) and the selflocking nuts (120). (b) Install the belt fasteners (100 and 280 IPL Figure 5) on the RH fitting (90, IPL Figure 5) and the LH fitting (270, IPL Figure 5) with the screws (110 and 280, IPL Figure 5), the washers (130 and 310, IPL Figure 5) and the bushs (120 and 300, IPL Figure 5). SUBTASK 25-26-80-430-003-A01 (3) Install of the LH and RH fitting (a) Connect the mechanical control cable of the override system control (50, IPL Figure 11). NOTE : For the adjustment of the electromagnet cable, refer to SUBTASK 25-26-80-820-001-A01, Chapter (8001) FITS AND CLEARANCES. (b) Install the override system control (50, IPL Figure 11) with the screws (13 IPL Figure 11). (c) Install the RH Fitting (90, IPL Figure 5) and the LH fitting (270, IPL Figure 5) on the equipped support ECU (400) with the screws (420) and the washers (430). (d) Install the tube (80, IPL figure 5) on the LH Fitting (270, IPL Figure 5) and the RH fitting (90, IPL Figure 5) with the screws (360, IPL Figure 5) and the washers (370, IPL Figure 5). SUBTASK 25-26-80-430-004-A01 (4) Assembly of the rear crossbeam CAUTION : DO NOT OPERATE THE GEAR OF THE ACTUATOR BEFORE THE INSTALLATION. CAUTION : AFTER ACTUATOR REPLACEMENT YOU MUST DO A SEAT ACTUATOR CALIBRATION (REFER TO TASK 25-26-80-820-802-A01). (a) Install the actuator (70, IPL Figure 12 and Figure 12A) on the rear crossbeam (180) with the screws (80, IPL Figure 12 and Figure 12A), the spacers (90, IPL Figure 12 and Figure 12A), the washers (100, IPL Figure 12 and Figure 12A) and the self-locking nuts (110, IPL Figure 12 and Figure 12A).

25-26-80

PAGE 7005 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE CAUTION : USE MARKS MADE DURING DISASSEMBLY, THE POSITION MUST BE THE SAME AT THE REASSEMBLY. (b) Slide the coupling bush (470, IPL Figure 4) on the bearing pin and attach it with the spring pins (480 and 490, IPL Figure 4). (5) Install the rear crossbeam (180) on the base structure (300) with the screws (190 and 210) and the washers (200 and 220). SUBTASK 25-26-80-430-005-A01 (6) Assembly of the front crossbeam (a) Install the bearing (260) on the front crossbeam (230) with the screws (270) and the washers (280). (b) Install the links (10) on the bearing (260) with the retainer rings (30) and the shouldered pins (20). (c) Install the elbowed links (80) and the rollers (40) on the links (10) with the retainer rings (50), the washers (70) and the shouldered pins (60). (7) Install the front crossbeam (230) on the base structure (300) with the screws (240 and 410) and the washers (250 and 430). SUBTASK 25-26-80-430-006-A01 (8) Assembly of the legrest actuator mecanism (a) Install the rack (60, IPL Figure 10) on the guide (120, IPL Figure 10) and install the stop (40, IPL Figure 10) with the screws (50, IPL Figure 10). (b) Install the gear (100, IPL Figure 10) in the bearing (110, IPL Figure 10). (c) Install in sequence on the pin (70, IPL Figure 10) and in the support (170, IPL Figure 10), the spacers (160 and 180, IPL Figure 10), the bearing (110, IPL Figure 10). (d) Install the spring pins (80 and 90, IPL Figure 10) on the pin (70, IPL Figure 10). (e) Install the legrest actuator (40, IPL Figure 12 and Figure 12A) on the legrest mecanism (10, IPL Figure 10) with the screws (50, IPL Figure 12 and Figure 12A) and the washers (60, IPL Figure 12 and Figure 12A). (f) Install the legrest mecanism (10, IPL Figure 10) and the legrest actuator (40, IPL Figure 12 and Figure 12A) on the front crossbeam (230) with the screws (20, IPL Figure 10) and the washers (30, IPL Figure 10).

25-26-80

PAGE 7006 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE (9) Install the rear covering (20, IPL Figure 13) with the screws (30, IPL Figure 13). (10) Connect the mechanical control cable of the electromagnet (130), the crossbeam actuator (70, IPL Figure 12 and Figure 12A) and the legrest actuator (40, IPL Figure 12 and Figure 12A). NOTE : For the adjustment of the electromagnet cable, refer to SUBTASK 25-26-80-820-001-A01, Chapter (8001) FITS AND CLEARANCES. (11) Install the electrical wiring and the cable clamps (refer to IPL Figure 12 and Figure 12A). (12) Connect the connector and the bonding braids of the crossbeam actuator (70, IPL Figure 12 and Figure 12A), the legrest actuator (40, IPL Figure 12 and Figure 12A).and the ECU (10, IPL Figure 12 and Figure 12A).

25-26-80

PAGE 7007 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 TASK 25-26-80-430-803-A01 4.

Assembly of the seat bottom A. Reason for the job Self-explanatory. B. Job set-up information (1) Referenced information REFERENCE

25-26-80-991-009-A01

NAME Figure 8

C. Job set-up None. D. Procedure (refer to IPL Figure 8) (1) Install the yokes (90) on the panel (120) with the screws (100) and the washers (110). (2) Install the RH and LH fittings (60 and 70) on the yokes (90) with the cotter pins (30), the washers (10, 20 and 40) and the shouldered pins (50).

25-26-80

PAGE 7008 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-430-804-A01 5.

Assembly of the seat back A. Reason for the job Self-explanatory. B. Job set-up information (1) Referenced information REFERENCE

25-26-80-820-801-A01 25-26-80-991-008-A01 25-26-80-991-014-A01 25-26-80-991-060-A01 25-26-80-991-017-A01 25-26-80-991-018-A01 25-26-80-991-019-A01

NAME Actuator calibration Figure 7 Figure 12 (sheet 1 of 2) Figure 12A (sheet 1 of 2) Figure 13 Figure 14 (sheet 1 of 3) Figure 14 (sheet 2 of 3)

C. Job set-up None. D. Procedure (refer to IPL Figure 7) (1) Install the connector support (200) on the lower panel (190) ith the screws (230) and the washers (240). (2) Install the wiring supports (250) on the lower panel (190) with the screws (260 and 290), the washers (280) and the spacers (270). (3) Install the rollers (350 and 410) on the fitting (340 and 400) with the cotter pins (370 and 430), the washers (380 and 440) and the pins (360 and 420). (4) Install the lower panel (190) on the fittings (340 and 400) with the screws (200) and the washers (210). (5) Install the fittings (340 and 400) on the upper panel (300) with the screws (310) and the washers (320). (6) Install the lower panel (160) on the fittings (340 and 400) with the screws (170) and the spacers (180). (7) Install the hinge (140) on the upper panel (300) with the screws (150). CAUTION : AFTER ACTUATOR REPLACEMENT YOU MUST DO A SEAT ACTUATOR CALIBRATION (REFER TO TASK 25-26-80-820-801-A01).

25-26-80

PAGE 7009 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE (8) Install the lumbar rest actuator (120, IPL Figure 12 and Figure 12A) on the lower panel (160) with the screws (130, IPL Figure 12 and Figure 12A) and the washers (140, IPL Figure 12 and Figure 12A) and connect the bonding braid. (9) Install the wiring supports (80) on the mobile structure (10) with the screws (90), the washers (100) and the spacers (110). (10) Install the tracks (70 and 80, IPL Figure 14) on the fitting (10, IPL Figure 14) with the screws (50, IPL Figure 14) and the self locking nuts (60, IPL Figure 14). (11) Install the shim (90, IPL Figure 14) on the fitting (10, IPL Figure 14) with the screws (100, IPL Figure 14) and the washers (110, IPL Figure 14) and the spacers (120, IPL Figure 14). (12) Install the headrest fitting (10, IPL Figure 14) on the fitting (10) with the screws (260, IPL Figure 1) and the washers (270, IPL Figure 1). (13) Install the stops (60) on the mobile structure (10) with the screws (70). (14) Install the roller tracks (30) with the screws (40) and the washers (50). (15) Install the mobile structure (10) on the hinge (140) with the screws (20). (16) Install the seat back covering (110, IPL Figure13) with the screws (140, IPL Figure 13) (17) Install the lateral shrouds (120 and 130, IPL Figure 13) attached by Velcro tape.

25-26-80

PAGE 7010 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-420-801-A01 6.

Installation of the seat back and the seat bottom on the base A. Reason for the job Self-explanatory. B. Job set-up information (1) Referenced information REFERENCE

25-26-80-430-802-A01 25-26-80-430-803-A01 25-26-80-430-804-A01 25-26-80-820-801-A01 25-26-80-991-002-A01 25-26-80-991-059-A01 25-26-80-991-004-A01 25-26-80-991-015-A01 25-26-80-991-060-A01 25-26-80-991-055-A01

NAME Assembly of the base Assembly of the seat bottom Assembly of the seat back Actuator calibration Figure 1 (sheet 2 of 2) Figure 1A (sheet 2 of 2) Figure 3 Figure 12 (sheet 1 of 2) Figure 12A (sheet 1 of 2) Figure 7001

C. Job set-up Assembly of the base (refer TASK 25-26-80-430-802-A01) Assembly of the seat bottom (refer TASK 25-26-80-430-803-A01) Assembly of the seat back (refer TASK 25-26-80-430-804-A01) D. Procedure (refer to IPL Figure 1 and Figure 1A) NOTE : The seats are symmetrical, this procedure is only for the right seat. (1) Install the seat back in the bed position and keep the seat in this position with the assembly tool (6, Figure 3002) PN 64300FFCL1-01CX01-01. (2) USE MARKS made DURING DISASSEMBLY, The position must be the same at the reassembly. (3) Put the seat bottom (80) on the seat and attach it on the seat back (70) with the washer (100) and the pins (90). (4) Install the link (80, IPL Figure 3) on the seat back (70) with the cotter pins (130), the washer (100 and 120), the spacer (140) and the pins (110). (5) Connect the connector and the mechanical control cable of the lumbar rest actuator (120, IPL Figure 12 and Figure 12A) and install the cable clamps.

25-26-80

PAGE 7011 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE NOTE : For the adjustment of the lumbar rest actuator, refer to SUBTASK 25-26-80-820-001-A01, Chapter (8001) FITS AND CLEARANCES. (6) Remove the assembly tool (6, Figure 7001). (7) Install the shrouds (4) attached by velcro tape.

25-26-80

PAGE 7012 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 TASK 25-26-80-430-805-A01 7.

Assembly of the legrest A. Reason for the job Self-explanatory. B. Job set-up information (1) Referenced information REFERENCE

25-26-80-991-012-A01

NAME Figure 10

C. Job set-up None. D. Procedure (refer to IPL Figure 10) (1) Install the angle (260) on the panel (320) with the screws (270). (2) Install the LH and RH fittings (330 and340) on the panel (320) with the screws (350) and the washers (360). (3) Install the yoke (370) on the panel (320) with the screws (380) and the washers (390).

25-26-80

PAGE 7013 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-420-802-A01 8.

Installation of the legrest on the base A. Reason for the job Self-explanatory. B. Job set-up information (1) Referenced information REFERENCE

25-26-80-430-802-A01 25-26-80-420-801-A01 25-26-80-430-805-A01 25-26-80-820-801-A01 25-26-80-991-002-A01 25-26-80-991-059-A01 25-26-80-991-012-A01 25-26-80-991-017-A01 25-26-80-991-055-A01

NAME Assembly of the base Installation of the seat back and the seat bottom on the base Assembly of the legrest Actuator calibration Figure 1 (sheet 2 of 2) Figure 1A (sheet 2 of 2) Figure 10 Figure 13 Figure 7001

C. Job set-up Assembly of the base (refer TASK. 25-26-80-430-802-A01) Installation of the seat back and the seat bottom on the base (refer TASK. 25-26-80-420801-A01) Assembly of the legrest (refer TASK. 25-26-80-430-805-A01) D. Procedure (refer to IPL Figure 10) (1) Lift up the seat bottom (80, IPL Figure 1 and Figure 1A). (2) Install the equipped legrest (280) on the base with the articulation pins (290), the washers (310) and the spacers (300). (3) Install the rack (60) on the yoke (370) with the cotter pins (250), the washers (240) and the shouldered pins (230). CAUTION : AFTER ACTUATOR REPLACEMENT YOU MUST DO A SEAT ACTUATOR CALIBRATION (REFER TO TASK 25-26-83-820-801-A01). (4) Pull on the button (16, Figure 7001) and check the correct unlocking of the legrest actuator. (5) Install the front covering (40, IPL Figure 13) with the screws (50, IPL Figure 13) and the washers (60, IPL Figure 13).

25-26-80

PAGE 7014 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-430-806-A01 9.

Assembly of the armrest NOTE : Valid for FFCLx-01WY SERIES, Business class A. Reason for the job Self-explanatory. B. Job set-up information (1) Consumables REFERENCE

Qty

LOCTITE 221

AR

NAME Anaerobic sealant

(2) Referenced information REFERENCE 25-26-80-991-010-A01 25-26-80-991-011-A01

NAME Figure 9 (sheet 1 of 2) Figure 9 (sheet 2 of 2)

C. Job set-up None. D. Procedure (refer to IPL Figure 9) (1) Assembly of the armrest structure (a) Install the track (110) and the stop (140) on the structure (170) with the screws (120 and 160). (b) Install the lever (270), the spacer (220) and the washer (200) on the mobile structure (390) with the cotter pin (190), the washer (200) and the shouldered pin (210). (c) Install the lock support (230) on the mobile structure (390) with the screws (240), the washers (250) and the self-locking nuts (260). (d) Install the control cable (310) on the lever (270) and install the pin (280) in the lock support (230) with the screw (290). (e) Install the clamp (330) on the mobile structure (390) with the screw (340 and the self-locking nut (350).

25-26-80

PAGE 7015 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE (f) Install the button (10) on the lever (270) with the screws (20), the washers (30) and the self-locking nuts (40). (g) Install the structure (170) on the mobile structure (390) and attach the cylinder (60) with the cotter pins (70), the washers (80), the spacers (100) and the shouldered pins (90). (2) Installation of the shrouds (a) Install the lower shroud (430) on the structure (170) with the screws (440 and 450). (b) Install the inner shroud (460) on the structure (390) with screws (470) and the nuts (480). (c) Install the outer shroud (410) with the screws (420). (d) Screws (420) are bonded with LOCTITE 221. (e) Install the armcap (490) with the screw (500). (f)

Screws (500) are bonded with LOCTITE 221.

(g) Install the screw cap (530).

25-26-80

PAGE 7016 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-420-803-A01 10. Installation of the armrest on the base NOTE :

Valid for FFCLx-01WY SERIES, Business class

A. Reason for the job Self-explanatory. B. Job set-up information (1) Referenced information REFERENCE 25-26-80-430-802-A01 25-26-80-420-801-A01 25-26-80-430-806-A01 25-26-80-991-002-A01 25-26-80-991-009-A01

NAME Assembly of the base Installation of the seat back and the seat bottom on the base Assembly of the armrest Figure 1 (sheet 2 of 2) Figure 8

C. Job set-up Assembly of the base (refer TASK 25-26-80-430-802-A01) Installation of the seat back and the seat bottom on the base (refer TASK 25-26-80-420801-A01) Assembly of the Armrest (refer TASK 25-26-80-430-806-A01) D. Procedure (refer to IPL Figure 1) (1) Lift up the seat bottom (80, IPL Figure 8). (2) Install the armrest (150) on the base (60) with the screws (160 and 170) and the washers (180).

25-26-80

PAGE 7017 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-420-804 11. Installation of the seat on the pallet A. Reason for the job Self-explanatory. B. Job set-up information (1) Tools, fixtures and equipment REFERENCE

Qty

64300FFCL1-01CX01-01

1

NAME Assembly tool

(2) Referenced information REFERENCE 25-26-80-430-801-A01 25-26-80-430-802-A01 25-26-80-420-801-A01 25-26-80-420-802-A01 25-26-80-420-803-A01 25-26-80-991-006-A01 25-26-80-991-020-A01 25-26-80-991-015-A01 25-26-80-991-060-A01 25-26-80-991-055-A01 25-26-80-991-056-A01

NAME Assembly of the pallet Assembly of the base Installation of the seat back and the seat bottom on the base Installation of the legrest on the base Installation of the armrest on the base Figure 5 Figure 15 (sheet 1 of 2) Figure 12 (sheet 1 of 2) Figure 12A (sheet 1 of 2) Figure 7001 Figure 7002

C. Job set-up Assembly of the pallet (refer TASK 25-26-80-430-801-A01) Assembly of the base (refer TASK 25-26-80-430-802-A01) Installation of the seat back and the seat bottom on the base (refer TASK 25-26-80-420801-A01) Installation of the legrest on the base (refer TASK 25-26-80-420-802-A01) Installation of the armrest on the base (refer TASK 25-26-80-420-803-A01) D. Procedure (1) Single seat (refer to figure 7001) (a) Make sure that the seat is in the bed position and the assembly tool (6) (P/N : 64300FFCL1-01CX01-01) correctly installed.

25-26-80

PAGE 7018 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE (b) Take the seat by the assembly tool (6) and the crossbeam tube (15) and engage the two rollers (140 and 320, IPL Figure 5) in the tracks of the pallet, then engage the middle and front rollers at the level of the plate (11) NOTE :

Use the button (3) of the mecanical override control to unlock the electromagnet and put the seat on the locking position.

(c) Install the plates (11) on the pallet with the screws (9) and the washers (10). (d) Install the covers (8) on the cover supports with the screws (7). (e) Remove the assembly tool (6) and manually (with mechanical control) move the seat back to the take-off position. (f) Install the quick wiring support (270, IPL Figure 12) or the quick wiring support (360, IPL Figure 12A). (g) Connect the connectors P17 from J17, P21 from J21, P20 from J20 and P22 from J22.

25-26-80

PAGE 7019 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01

6

12

5 4

2 7 8

1

9 10 11

3 13

9 10 11

INSTALLATION OF THE SINGLE SEAT FIGURE 7001 / GRAPHIC 25-26-80-991-055-A01

25-26-80

PAGE 7020 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 (2) Double seat (refer to figure 7002) NOTE : The seats are symmetrical, this procedure gives the installation of the left seat. (a) Make sure that the seat is in the bed position and the assembly tool (6) (P/N: 64300FFCL1-01CX01-01) correctly installed. (b) Take the seat by the assembly tool (6) and the crossbeam tube (15) and engage the two rear rollers (140 and 320, IPL Figure 5) in the tracks of the pallet then engage the middle and front rollers (140 and 320, IPL Figure 5) at the level of the plate (11). NOTE : Use the button (3) of the mechanical override control to unlock the electromagnet and put the seat in the locking postion. (c) Install the plates (11) on the tracks with the screws (10) and the washers (11). (d) Install the covers (8) on the cover supports with the screws (7). (e) Install the quick wiring support (270, IPL Figure 12). (f) Connect the connectors P17 from J17, P21 from J21, P20 from J20 and P22 from J22. NOTE : Check that the electrical wiring does not interfere with the tracks.

25-26-80

PAGE 7021 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 6

2

6 4 4

1

12 5

7 8

3

9 10 11

9 10 11

INSTALLATION OF THE DOUBLE SEAT FIGURE 7002 / GRAPHIC 25-26-80-991-056-A01

25-26-80

PAGE 7022 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 TASK 25-26-80-820-801-A01 12. Actuator calibration A. Reason for the job Self-explanatory. B. Job set-up information (1) Referenced information REFERENCE 25-26-80-420-801-A01 25-26-80-420-802-A01 25-26-80-420-803-A01

NAME Installation of the base on the pallet Installation of the seat back and the seat bottom on the base Installation of the legrest on the base

C. Job set-up Installation of the base on the pallet (refer to TASK 25-26-80-420-801-A01). Installation of the seat back and the seat bottom on the base (refer to TASK 25-26-80-420802-A01). Installation of the legrest on the base (refer to TASK 25-26-80-420-803-A01). D. Procedure NOTE : The calibration system gives the possibility at each actuator to have a reference in relation to a seat position. The useful range of each actuator shows an absolute distance. As it is possible to install the actuators in a perfect position where the operating range of the actuator corresponds perfectly to the useful range of movement of the seat, the calibration control must be used to give each actuator a relative reference (with respect to the seat). If an actuator is replaced, the complete calibration procedure must be done again (1) Move manually (not electrically) the seat to calibration position. (a) Put the seat in take-off position with the locking pins locked. (b) Put the legrest in vertical position (stowed). (c) Put the lumbar rest panel in fully retracted position. (2) Check all actuators are clutched. (3) Press the reset switch button, on ECU (labeled “reset” or “calib”) during at least 3 seconds. (4) Pull OFF the bracker on ECU.

25-26-80

PAGE 7023 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01

(5) Wait for 5 seconds, then push ON the breaker on ECU. (6) Check electrically that actuators do not hit mechanical endstops (no over current for example). NOTE : Do again the complete calibration procedure, in case of hitting actuator.

25-26-80

PAGE 7024 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-420-805-A01 13. Installation of the cushions A. Reason for the job Self-explanatory. B. Job set-up information (1) Referenced information REFERENCE

NAME

25-26-80-420-804-A01 25-26-80-991-079-A01 25-26-80-991-003-A01

Installation of the seat on the pallet Figure 7003 Figure 2

C. Job set-up Installation of the seat on the pallet (refer to TASK 25-26-80-420-804-A01). D. Procedure (refer to IPL Figure 4). SUBTASK 25-26-420-001-A01 (1) Install the belt (a) Open the clip (1) and engage the belt (2). 2

1

INSTALL THE BELT FIGURE 7003/ GRAPHIC 25-26-80-991-080-A01 SUBTASK 25-26-420-002-A01 (2) Install the cushions (a) Install the cover/foam (50 and 60) on the legrest. (b) Install the cover/foam (10 and 20) on the seat bottom. (c) Install the cover/foam (30 and 40) on the seat back.

25-26-80

PAGE 7025 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-430-807-A01 14. Assembly of the headrest A. Reason for the job Self-explanatory. B. Job set-up information (1) Referenced information REFERENCE 25-26-80-991-003-A01 25-26-80-991-018-A01 25-26-80-991-019-A01 25-26-80-991-063-A01

NAME Figure 2 Figure 14 (sheet 1 of 3) Figure 14 (sheet 2 of 3) Figure 14 (sheet 3 of 3)

C. Job set-up None. D. Procedure (refer to IPL Figure 14) valid for FFCLx-01WY SERIES, Business class (1) Install the spring blade (210) on the braket (170) with the screws (220) and the nuts (230). (2) Install the slides (180) on the braket (170) with the screws (190) and the washers (200). (3) Install the fitting (10) on the panel (240) with the screws (20), the washers (30) and the spacers (35). (4) Install the cover/foam (70 and 80, IPL Figure 2) on the headrest.

25-26-80

PAGE 7026 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE E. Procedure (refer to IPL Figure 14). Valid for FFCLx-02WY SERIES, First class (1) Install the hinge (250) and the headrest central (340) with the screws (260), the washers (270) and the nuts 5280). (2) Install the hinge (300), the headrest RH (350) and the headrest LH ( 360) with the screws (310), the washers (320). (3) Install spring blade (210) on the braket (170) with the screws (220) and the nuts (230). (4) Install the slides (180) on the braket (170) with the screws (190) and the washers (200). (5) Install the fitting (10) on the panel (240) with the screws (20) and the washers (30). (6) Install the cover/foam (70 and 80, IPL Figure 2) on the headrest.

25-26-80

PAGE 7027 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-420-806-A01 15. Installation of the headrest A. Reason for the job Self-explanatory. B. Job set-up information (1) Referenced information REFERENCE 25-26-80-420-805-A01 25-26-83-430-807-A01 25-26-80-991-001-A01 25-26-80-991-002-A01 25-26-80-991-058-A01 25-26-80-991-059-A01 25-26-80-991-018-A01

NAME Installation of the cushions Assembly of the headrest Figure 1 (sheet 1 of 2) Figure 1 (sheet 2 of 2) Figure 1A (sheet 1 of 2) Figure 1A (sheet 2 of 2) Figure 14 (sheet 1 of 2)

C. Job set-up Installation of the cushions (refer to TASK 25-26-80-420-805-A01). Assembly of the headrest (refer to TASK 25-26-80-430-807-A01). D. Procedure (refer to IPL Figure 1 and Figure 1A) (1) Install the headrest (250, IPL Figure 1) or the headrest (210, IPL Figure 1A) on the seat back (70, IPL Figure 1or Figure 1A). (2) Install the angle (130, IPL Figure 14) with the screws (140, IPL Figure 14) and the washers (150, IPL Figure 14).

25-26-80

PAGE 7028 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 FITS AND CLEARANCES TASK 25-26-80-820-802-A01 1.

General The torque values used are in accordance with standard maintenance practices unless otherwise specified.

TASK 25-26-80-820-803-A01 2.

Specific tightening torque value REFERENCE IPL – Fig. 15 – Item 610

NAME Screw

TORQUE VALUE m.daN in.lbf 0.4

25-26-80

36

PAGE 8001 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 TASK 25-26-80-820-804-A01 3.

Mechanical controls adjustment A. Reason for the job Self-explanatory. B. Job set-up information (1) Referenced information REFERENCE

25-26-83-991-057-A01

NAME Figure 8001

C. Job set-up None. D. Procedure (refer to Figure 8001) SUBTASK 25-26-80-820-001-A01 (1) Electromagnet adjustment (a) Pull on the button (1) and check the correct unlocking of the seat back/bottom actuator (4). Adjust the cable (5) if necessary. (b) Pull on the button (1) and adjust the nut (2) to get at the same time the unlocking of the electromagnets (3) and the seat back/bottom actuator (4). Adjust the cable (6, 7) if necessary. (c) Pull on the button (1) and check that the electromagnet (3) and the seat back/bottom actuator (4) unlock at the same time.

25-26-80

PAGE 8002 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01

3 6

2

4 7 1

5

3

MECHANICAL CONTROLS ADJUSTMENT FIGURE 8001 / GRAPHIC 25-26-80-991-057-A01

25-26-80

PAGE 8003 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01

PAGE INTENTIONALLY LEFT BLANK

25-26-80

PAGE 8004 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 SPECIAL TOOLS, FIXTURES, EQUIPMENT AND CONSUMABLES TASK 25-26-80-940-801-A01 1.

Special tools, fixtures and equipments A. General NOTE : Use equivalent alternatives for listed items. Part No.

Description

Suppliers code

64300FFCL1-01CX01-01 Assembly tool for first class seat

F4643

Page block where used 3001 7001

TID 2

B. Insertion and extraction tools for wired contacts These operations can be done with disposable plastic tool. White tip is for extraction and colored tip for insertion, tools are color-coded according to contact size. CONTACT SIZE AWG 22 20 16 12

TOOL COLOR CODE GREEN RED BLUE YELLOW

TOOL STANDARD NUMBER

VENDOR CODE

TID

M81969-14-01 OR (MS27534-22D) M81969-14-02 OR (MS27534-20) M81969-14-03 M81969-14-04

F0225

1

25-26-80

PAGE 9001 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 TASK 25-26-80-940-802-A01 2.

Consumables NOTE : Use equivalent alternatives for listed items.

Material No.

Designation and specification

01286-15 1001 404-12-70PX 404-12-71PR-7 404-12-864E 4080K201 4125-6407 414-12-9110 4635-3600 54614048PU66 6345-4502 AERO-CLEAN X-200 CAF4 EMFI 30055A G231N L25LR0093616360 Leather strong cleaner LOCTITE 221 MIL-C-10578 MIL-C-5541 MIL-D-12491

Ammonia Benzene Carbon tetrachloride Denatured alcohol Deodorant spray Hydrogen peroxide Oleic acid Oxalic acid Soap Sodium hypchlorite solution Abrasive paper Fabric GLIDE/RUM ROHI KF Spray Can F2 Grey paint Paint pantone 5C Beige braun paint Black paint Electrical bonding lacquer White primary paint Green primary paint (PAC33) Glossed red paint Glossed red paint Seat belt cleaner Sealant Adhesive Kraft paper Leather LANTAL cognac Leather cleaner Anaerobic sealant Corrosion removing compound Alodine 1200 Solvent degreaser

NSA8420-2 PD680 type 1 S1590 SOCOSOLV 97T

Lacing tapes White spirit Yellow primary paint Cleaner

Thermoweldable C-315

thermoweldable material

Suppliers code Page block or name and where used address Local purchase 4001 Local purchase 4001 Local purchase 4001 Local purchase 4001 Local purchase 4001 Local purchase 4001 Local purchase 4001 Local purchase 4001 Local purchase 4001 Local purchase 4001 Local purchase 6001 C8156 6001 F5517 4001 F9337 6001 F9337 6001 F9337 6001 F0883 6001 F1419 6001 F9337 6001 F1419 6001 F0883 6001 F1419 6001 S3102 4001 F0107 6001 F6599 6001 Local purchase 15001 S3859 6001 Local purchase 4001 F7121 7001 F3172 4001 F2865 6001 F5517 4001 6001 F5442 6001 F4233 4001 98502 6001 F6892 4001 6001 FAKH9 15001

25-26-80

PAGE 9002 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 Material No. TURCO 1495 TURCO INTERIOR CLEANER VERT RAL 6001

Designation and specification Abrasive cloth for aluminum Detergent Bright glycero paint

Suppliers code Page block or name and where used address F3172 6001 F3172 4001 F9337 6001

TASK 25-26-80-940-803-A01 3.

Suppliers list CAGE CODE

98502

C8156

F0107

F0225

F0883

F1419

F2865

F3172

F4233

F5442

NAMES AND ADDRESSES AKZO COATINGS INC AEROSPACE FINISHES DIVISION 434 W MEATS ST ORANGE, CA 92665, USA ROHI STOFFE GMBH SCHOENLINDERSTR 1 P.O. BOX 747 82538 GERETSRIED, GERMANY RHODIA CHIMIE 26 QUAI ALPHONSE LE GALLO 92100 BOULOGNE BILLANCOURT, FRANCE SOURIAU ET CIE SA DPT 13 RUE GALLIENI 92100 BOULOGNE BILLANCOURT, FRANCE CELOMER STE FRANCAISE DE PEINTURES E VERNIS SA PRODUITS LORY 75 BD WINSTON CHURCHILL 76052 LE HAVRE CEDEX , FRANCE PPG COATINGS SA 7 ALLEE DE LA PLAINE BP 87 76700 GONFREVILLE L'ORCHER, FRANCE NUFARM 28 BOULEVARD CAMELINAT BP 75 92230 GENNEVILLIERS, FRANCE TURCO FRANCE 161 RUE DE SILLY 92100 BOULOGNE BILLANCOURT, FRANCE SOLVADIS FRANCE LANGLOIS 3 RUE DE LA BUHOTIERE - BP 89152 35136 ST JACQUES DE LA LANDE, FRANCE EADS NORMALISATION STANDARD ASN 37 BOULEVARD DE MONTMORENCY 75016 PARIS, FRANCE

25-26-80

PAGE 9003 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 CAGE CODE F5517

F6599

F6892

F7121

F9337

FAKH9

S3102

S3859

NAMES AND ADDRESSES CRC INDUSTRIES FRANCE 12 BOULEVARD DES MARTYRS CHATEAUBRIAND BP 90028 95100 ARGENTEUIL, FRANCE EMFI SA 14 R DE LA FERME CLAUSS BP 30 67501 HAGUENAU CEDEX, FRANCE SOCOMOR SA ZI DU PRAT BP 3707 56000 VANNES, FRANCE HENKEL LOCTITE FRANCE 10 AVENUE EUGENE GAZEAU BP 400900 60300 SENLIS, FRANCE MANKIEWICZ FRANCE 16 RUE DE SOLFERINO 92100 BOULOGNE BILLANCOURT, FRANCE VALSEM RUELLE DE COMPIEGNE BP 30 60190 LACHELLE, FRANCE SIFRAG AG BAHNHOEHENWEG 70 BERN, SWITZERLAND LANTAL TEXTILES DORFGASSE 5 P.O. BOX 1330 LANGENTHAL, SWITZERLAND

25-26-80

PAGE 9004 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 STORAGE TASK 25-26-80-550-801-A01 1.

Storage A. Reason for the job Self-explanatory. B. Job set-up information (1) Consumables REFERENCE Thermoweldable C-315 G231N

Qty

NAME

AR AR

Thermoweldable material Kraft paper

C. Job set-up None. D. Procedure NOTE : The seat assembly is essentially corrosion resistant and no special treatment is necessary. (1) Do storage under the conditions that follow: (a) Attach the seat on a jig or a support, in an identical configuration to that of the aircraft to avoid distortions. (b) In a sheltered, ventilated place with a normal hygrometric degree (70 %). (c) Away from light (to prevent damage to fabrics and foams). (d) Wrap the seat in thermoweldable material (Specif. C315) or Kraft paper (Specif. G231N) or in a plastic bag. Use adhesive tape to close the wrapping. (e) Identify the seat and the revision or storage date on a placard or any suitable location on the wrapping. (f) Make every six months a visual inspection.

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PAGE 15001 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01

PAGE INTENTIONALLY LEFT BLANK

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PAGE 15002 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 ILLUSTRATED PARTS LIST TASK 25-26-80-950-801-A01 1.

Introduction A. General (1) The illustrated Parts List (IPL) shows the details of the equipment and lets easy provisioning of the spares necessary to the maintenance of this equipment. B. Ordered address (1) All components of this equipment can be ordered at the addresses indicated in the Price List. C. Use of the illustrated parts list (1) "Introduction" section The introduction contains all explanatory information for the individual sections necessary for use of this IPL. The introduction also contains a list of abbreviations used in the as well as a list of manufacturers' names and addresses. (2) "Alphanumerical Index" section This section contains a listing of part numbers of all items listed in the detailed parts list in Alphanumerical sequence with cross reference to respective Fig/item numbers as well as quantity per assy. - letters A through Z, except O (O to be considered as zero). - numerals 0 through 9. For subsequent rows, the order is : - a dash - letters A through Z, except O (O to be considered as zero). - numerals 0 through 9.

25-26-80

INTRO IPL PAGE 1 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 (3) "Illustrated Parts List" section The detailed parts list gives the list and the illustrations of parts making up the considered assembly. The different columns of the parts list pages are organized as follows: 1st column : Figure and item number 2nd column : Manufacturer's part number 3rd column : Airline part number (not used) 4th column : Indenture 5th column : Designation 6th column : Usage from to 7th column : Quantity per Assembly. (a) Figure and item number 1

Each illustration receives a figure number starting at 01 and carrying on in sequence.

2

Each illustration can be divided up into several folios.

3

When it is necessary to add figures, alphabetic indexes are added to the original figure, from A to Z, except I and O.

4

An item number is attributed to each part mentioned in the detailed parts list. Numbers start at 001A up to 999A per sequence of 10 by 10 or else in order to insert additional items.

5

Alternative parts have the same item as the initial part and are indexed.

6

To follow the evolution of the standard of parts or assemblies modification, items are indexed from B to Z, except I and O.

7

Non illustrated items are identified by a dash placed in front of the item.

(b) Manufacturer's part number This column indicates the original manufacturer's part number or the part manufacturer. (c) Airline part number This column is left blank, it is reserved for the airline.

25-26-80

INTRO IPL PAGE 2 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 (d) Indenture The designation is presented according to indentations indicating as follows the relation between the different components : 1 Assembly 2 Sub-assemblies 2 Attaching parts of the sub-assembly 3 Constitutive parts of the sub-assembly 3 Attaching parts of the sub sub-assembly 4 Constitutive parts of the sub sub-assembly etc. (e) Nomenclature The designation of the item can be followed by : - The CAGE manufacturer's code, - Cross-references indicating figures and items where this item is illustrated. - Attaching Parts Attaching parts are listed immediately below the assembly which they attach and preceding any detail parts of said assembly. They are listed in the same column as the assembly which they attach and are captioned “ATTACHING PARTS”. The XXX symbol shall follow the last item of the attaching parts as shown above. (f) Usage from to The interchangeability relation of constitutive parts according to the higher assembly is identified by the item number. This code is only valid for the assembly dealt with in the corresponding figure. Example : FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

NOMENCLATURE

USAGE FROM TO

UNITS PER ASSY

-

1A

PN1

1 ASSEMBLY 1

RF

-

1B

PN2

1 ASSEMBLY 2

RF

-

1C

PN3

1 ASSEMBLY 3

RF

10A

SPN1

2 SUB-ASSEMBLY 1

1AC

1

10B

SPN2

2 SUB-ASSEMBLY 2

1B

1

20A

SSPN1

3 SUB-SUB-ASSEMBLY 1

10A

1

20B

SSPN2

3 SUB-SUB-ASSEMBLY 2

10B

1

30A

SPN3

2 SUB-ASSEMBLY 3

25-26-80

1

INTRO IPL PAGE 3 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 (g) Units per assembly This column gives the number of parts required for an immediately higher assembly. If a same assembly or a same part appears in several figures, the quantity is only given in the first parts list; the RF abbreviation appears in the following parts list. If the quantity of a component is to be established as required (Ex.: seal, etc) the quantity is replaced by the term AR (as required). (4) How to use the Illustrated Parts List (a) When the part number is known : 1

Turn to the numerical index and find the part number.

2

The figure and item number on the illustration where the part appears are listed in the column to the right of the part number.

3

The corresponding item number in the accompanying parts list will give part number, description, assembly relationship and quantity required for that particular application.

(b) When the part number is not known : 1

Look through the illustrations and find the assembly of which the component is part, or look through the illustrations and identify the part by appearance. Note the item number in the exploded view and find part number, description and quantity required for that part.

25-26-80

INTRO IPL PAGE 4 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE (5) List of Abbreviations The following abbreviations are used in this IPL : ACMM

Abbreviated component maintenance manuel

AN

Army-Navy

AR

As Required. Indicates that an indefinite quantity is required

ASSY

Assembly

CAGE CODE Commercial and Government Entity Code CMM

Component Maintenance Manual

CSK

Countersunk

CTR

Central

DET

Detail

ECU

Electrical Control Unit

FIG

Figure

HEX.

Hexagonal

IND

Indenture

IPL

Illustrated Parts List

LH

Left Hand

MS

Military Standard

NAS

National Aerospace Standard

NHA

Next Higher Assembly

NP

Not Procurable. After any description means that this part number constitutes an assembly of breakdown parts not supplied as a whole. Although not procurable, a view of each assembly, sub-assembly, sub-sub-assembly, or small unit, exploded as necessary to show detail parts, is provided to illustrate each part in the detailed parts list. Illustrations of all parts will be technically correct in assembly installation relation ships. Only EADS SOGERMA repair shop can order (NP) parts for overhaul and repair.

NPV

Not Procurable Vendor at EADS SOGERMA but only at the supplier.

P/N

Part Number

Qty

Quantity

RF

Reference indicates those parts which have their quantity listed elsewhere in the Illustrated Parts List.

RH

Right Hand

25-26-80

INTRO IPL PAGE 5 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE D. Index of Vendors Parts manufactured by companies other than EADS SOGERMA are identified by an appropriate vendor code shown at the end of the line. CAGE CODE C4206

D8518

FA4Y6

FA5Z2

FB328

F0217

F0358

F0563

F1142

F1484

F3341

NAMES AND ADDRESSES IGUS GMBH SPICHER STRASSE 1A PO BOX 906123 51147 KOEL, GERMANY AIRBUS DEUTSCHLAND GMBH KREETSLAG 10 PO BOX 95 01 09 21129 HAMBURG, GERMANY ENGRENAGE HPC 58 CHEMIN DE LA BRUYERE 69 570 DARDILLY, FRANCE PGA ELECTRONIC SARL 112 RUE MONTAIGNE 36000 CHATEAUROUX, FRANCE ICAM 8 RUE DE L’ACADIE 91940 LES ULIS, FRANCE LABINAL 9 AVENUE FRANKLIN BP 218 78160 MONTIGNY LE BRETONNEUX, FRANCE PRECILEC SA 41 RUE GUYNEMER BP 239 89000 AUXERRE, FRANCE SCHAEFFLER FRANCE 93 ROUTE DE BITCHE BP 186 67500 HAGUENAU, FRANCE SCHERDEL HERCKELBOUT-DAWSON 56 RUE DU TILLOY BP 774 60000 BEAUVAIS, FRANCE MECALECTRO SA 8 RUE GALVANI BP 35 91300 MASSY, FRANCE HELLERMANNTYTON HELLERMANN CUBOPLASTIC-TYTON-RW D 2 RUE DES HETRES BP 130 78190 TRAPPES, FRANCE

25-26-80

INTRO IPL PAGE 6 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE CAGE CODE F4643

F5442

F6599

F7121

F8433

K0017

U4447

3KGA2

35FB9

NAMES AND ADDRESSES EADS SOGERMA ETABLISSEMENT DE ROCHEFORT ZI DE L’ARSENAL BP 60109 17303 ROCHEFORT, FRANCE EADS NORMALISATION STANDARD ASN 37 BOULEVARD DE MONTMORENCY 75016 PARIS, FRANCE EMFI SA 14 RUE DE LA FERME CLAUSS BP 30 67501 HAGUENEAU CEDEX, FRANCE HENKEL LOCTITE FRANCE 10 AVENUE EUGENE GAZEAU BP 400900 60300 SENLIS, FRANCE TRELLEBORG AIRAX ZI BESANCON BP 17 25320 CHEMAUDIN, FRANCE EMHART FASTENING TEKNOLOGIES 177 WALSALL ROAD, PERRY BARR BIRMINGHAM B42 1BP, UNITED KINGDOM SOUTHCO EUROPE LTD TOUCH POINT WAINWRIGHT ROAD K WARNDON WORCESTER WR4 9FA, UNITED KINGDOM IN SEAT SOLUTIONS LLC 11839 EAST SMITH AVENUE SANTA FE SPRINGS, CA 90670, USA AMSAFE INC DBA AMSAFE AVIATION 1043 N 47TH AVENUE PHOENIX AZ 85043-1817, USA

25-26-80

INTRO IPL PAGE 7 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE TASK 25-26-80-960-801-A01 2.

Equipment designator index EQUIPMENT DESIGNATION

J1 J1 J1 J100 J100 J2 J2 J200 J200 J22 J22 J3 J30 J4 J5 SL1 SL2 J5 P1 P10 P11 P12 P10 P10 P10 P100 P100 P11 P11 P11 P12 P12 P12 P17 P17 P2

PART NUMBER E65EAR5-640A E65EAR5-640A P81011A010 E65EAR5-640A E65EAR5-640A E65EAR5-640A E65EAR5-640A E65EAR5-640A E65EAR5-640A HAR644 HAR644 35016-00 E65EAR5-640A 33084-00 35016-00 SB5-300-001-01 SB5-300-001-01 35016-00 35016-00 HAR650 HAR650 HAR650 RSA012 RSA012 HAR640 HAR640 HAR65 RSA013 RSA013 HAR640 LSA011 LSA011 HAR640 HAR647 HAR647 HAR647

25-26-80

FIGURE

ITEM

12 12A 12A 12 12A 12 12A 12 12A 12 12A 12A 12A 12A 12A 3 3 12A 12A 12A 12A 12A 12 12A 12 12 12A 12 12A 12 12 12A 12 12 12A 12

010A 010A 220A 010A 010A 010A 010A 010A 010A 250A 340A 180A 010A 300A 180A 130A 130A 180A 180A 280A 280A 280A 070A 070A 220A 220A 280A 040A 040A 220A 120B 120A 220A 240A 330A 240A INTRO IPL PAGE 8 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE EQUIPMENT DESIGNATION P2 P20 P20 P200 P200 P200 P21 P21 P22 P22 P23 P23 P3 P24 P24 P4 P5 P300 B1-1 B1-2

PART NUMBER HAR647 HAR640 HAR650 HAR641 HAR651 M83723-60-214AN HAR641 HAR651 P81011A010 HAR640 HAR644 HAR644 33083-00 HAR644 HAR644 35016-00 HAR659 HAR659 HAR650 HAR650

25-26-80

FIGURE

ITEM

12A 12 12A 12 12A 12A 12 12A 12 12 12 12A 12A 12 12A 12A 12A 12A 12A 12A

330A 220A 280A 230A 320A 600A 230A 320A 160A 220A 250A 340A 310A 250A 340A 180A 290A 290A 280A 280A

INTRO IPL PAGE 9 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

PAGE INTENTIONALLY LEFT BLANK

25-26-80

INTRO IPL PAGE 10 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIGURE

ITEM

TOTAL REQUIRED

ABS0639-09

12 12A

490A 610A

2 2

ABS0639-50

12

500A

1

AN174-11A

16

410A

4

AN174-13A

16

520A

2

AN174-14A

3

100A

4

AN174-4A

5 5 12 12A

110A 290A 020A 020A

1 1 4 4

AN174-6A

1

170A

2

AN174H7A

1

160A

2

AN175-14A

12 12A

080A 080A

2 2

AN175-5A

10

200A

1

AN175-7A

12 12A

050A 050A

2 2

AN4-16A

5A 5A

110A 320A

1 1

AN525-10-18

9

450A

2

AN565A832H6

10

140A

2

AN960-10L

1 1 10 10

210A 270A 030A 360A

4 4 4 10

AN960-416L

1 5 5 5A 7 7 15 15 16 16

180A 130A 310A 330A 380A 440A 280A 370A 280A 370A

4 1 1 1 1 1 1 1 1 1

AN960-516L

3

070A

1

PART NUMBER

- ITEM NOT ILLUSTRATED

AIRLINE STOCK NUMBER

ALPHANUMERICAL INDEX PAGE 1 APR 15/09

25-26-80

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIGURE

ITEM

TOTAL REQUIRED

AN960-8

5 5 5 5A 5A 5A 9 10 14 15 15 15 15 16 16 16 16

250A 430A 470A 240A 450A 530A 030A 390A 110A 060A 090A 160A 190A 060A 090A 160A 190A

2 2 2 2 2 2 2 4 1 4 4 4 4 4 4 4 4

AN960-8L

3 5 5A 9 13

280A 500A 560A 250A 060A

4 1 1 4 4

AN960-816L

10

310A

2

030A 030A

1 1

PART NUMBER

AN960PD10

AIRLINE STOCK NUMBER

5 5A

AN960PD10L

13

100A

2

AN960PD516L

9 9

080A 200A

2 1

ASNA2733-01

13

150A

2

AT5-375-25

4 4

240A 450A

1 1

CA1710

15 16

600A 610A

2 2

CA1720

9

300A

1

D3Q1CC040020APA

11

130A

2

ET5-010-001-04

3

310A

1

ET5-010-002-01

11

030A

1

ET5-010-003-01

11

040A

1

ET5-010-005-01

13

070A

1

E6-10-420R50

14

250A

2

- ITEM NOT ILLUSTRATED

ALPHANUMERICAL INDEX PAGE 2 APR 15/09

25-26-80

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIGURE

ITEM

TOTAL REQUIRED

E6-10-440R50

14

300A

2

E65EAR5-640A

12 12A

010A 010A

1 1

1 1A

110A 110A

2 2

PART NUMBER

FFCL1-1A1151-20

AIRLINE STOCK NUMBER

FFCL1-1B0502-22

15

570A

1

FFCL1-1B0502-23

15

570B

1

FFCL1-1B0503-20

15 16

520A 400A

2 2

FFCL1-1B0512-20

15 16

260A 260A

1 1

FFCL1-1B0512-21

15 16

350A 350A

1 1

FFCL1-1B0514-20

15 16

460A 480A

2 2

FFCL1-1B0515-20

15 16

490A 510A

2 2

FFCL1-1B0516-20

15 16

420A -440A

1 1

FFCL1-1B0530-20

16

540B

2

FFCL1-1B0530-21

16

560B

2

FFCL1-1B0532-20

15 16

530A 540A

1 2

FFCL1-1B0532-21

15 16

550A 560A

1 2

FFCL1-1B0542-21

16

580A

1

FFCL1-1B0542-22

16

590A

1

FFCL1-1B0543-20

16

600A

2

FFCL1-1B0613-20

15

590A

2

FFCL1-1B0617-01

15 16

390A 390A

2 2

FFCL1-1B0618-20

15 16

410A -430A

1 1

- ITEM NOT ILLUSTRATED

ALPHANUMERICAL INDEX PAGE 3 APR 15/09

25-26-80

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE PART NUMBER

AIRLINE STOCK NUMBER

FIGURE

ITEM

TOTAL REQUIRED

FFCL1-1B0619-20

15 16

450A -470A

2 2

FFCL1-1B0632-01

15 16

010A 010A

1 2

FFCL1-1B0632-02

15 16

110A 110A

1 1

FFCL1-1B0633-01

15 16

100A 100A

1 1

FFCL1-1B0633-02

15 16

200A 200A

1 1

FFCL1-1B0634-01

16

650A

8

FFCL1-1B0635-20

15 16

620A 630A

2 4

FFCL1-1B0636-01

15 15 16 16

070A 170A 070A 170A

1 1 1 1

FFCL1-1B0637-20

15 15 16

040A 140B 040A

2 2 2

FFCL1-1B0637-21

15 16

140A 140A

2 2

FFCL1-1B0642-01

15

640A

4

FFCL1-1B0643-31

15

690A

1

FFCL1-1B0644-01

15

730A

1

FFCL1-1B0801-01

15

790A

1

FFCL1-1B0801-02

15

790B

1

FFCL1-1B0835-21

15 16

380A 380A

1 1

FFCL1-1B0848-01

16

750A

1

FFCL1-1B1101-01

3

230A

1

FFCL1-1B1111-01

3

290A

1

FFCL1-1B1121-01

3

260A

2

FFCL1-1B1203-01

3 4

180A -001A

1 RF

- ITEM NOT ILLUSTRATED

ALPHANUMERICAL INDEX PAGE 4 APR 15/09

25-26-80

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIGURE

ITEM

TOTAL REQUIRED

FFCL1-1B1212-01

4

460A

1

FFCL1-1B1221-01

4

010A

1

FFCL1-1B1222-20

12 12A

090A 090A

2 2

FFCL1-1B1231-01

4

040A

1

FFCL1-1B1231-02

4

250A

1

FFCL1-1B1233-01

4 4

070A 280A

1 1

FFCL1-1B1233-02

4 4

090A 300A

1 1

FFCL1-1B1245-20

4

470A

2

FFCL1-1B1256-20

4 4

150A 360A

1 1

FFCL1-1B1257-20

4 4

110A 320A

1 1

FFCL1-1B1258-20

4 4

210A 420A

1 1

FFCL1-1B1259-20

4 4

170A 380A

1 1

FFCL1-1B1268-20

4 4

130A 340A

1 1

FFCL1-1B1269-20

4 4

190A 400A

1 1

FFCL1-1B1292-20

3

035A

4

FFCL1-1B1304-03

3 5

300A -001A

1 RF

FFCL1-1B1304-04

3 5

300B -001B

1 RF

FFCL1-1B1311-20

5 5

120A 300A

1 1

FFCL1-1B1313-20

5 5 5A 5A

200A 380A 190A 400A

1 1 1 1

PART NUMBER

- ITEM NOT ILLUSTRATED

AIRLINE STOCK NUMBER

ALPHANUMERICAL INDEX PAGE 5 APR 15/09

25-26-80

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIGURE

ITEM

TOTAL REQUIRED

FFCL1-1B1327-20

6 12 12A

080A 150A 210A

1 1 1

FFCL1-1B1330-01

5 5A

040A 040A

1 1

FFCL1-1B1331-20

5 5A

080A 080A

1 1

FFCL1-1B1332-01

5 5 5A 5A

170A 350A 160A 370A

1 1 1 1

FFCL1-1B1333-20

5 5A

060A 060A

2 2

FFCL1-1B1335-20

5 5A

010A 010A

1 1

FFCL1-1B1335-21

5A

010B

1

FFCL1-1B1340-01

5 5A

520A 580A

1 1

FFCL1-1B1340-02

5A

580B

1

FFCL1-1B1350-01

5A

090A

1

FFCL1-1B1350-03

5

090A

1

FFCL1-1B1350-04

5

270A

1

FFCL1-1B1360-03

5

260A

1

FFCL1-1B1360-04

5

440A

1

FFCL1-1B1401-01

3

090A

2

FFCL1-1B1411-20

3

170A

1

FFCL1-1B1420-20

3

150A

1

FFCL1-1B1430-20

3

160A

1

FFCL1-1B1511-01

3

080A

1

FFCL1-1B1512-03

3

010A

2

FFCL1-1B1513-20

3 3

020A 060A

1 1

FFCL1-1B1514-01

3

085A

1

PART NUMBER

- ITEM NOT ILLUSTRATED

AIRLINE STOCK NUMBER

ALPHANUMERICAL INDEX PAGE 6 APR 15/09

25-26-80

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE PART NUMBER

AIRLINE STOCK NUMBER

FIGURE

ITEM

TOTAL REQUIRED

FFCL1-1B1522-20

1 1A

140A 140A

2 2

FFCL1-1B1530-20

3

040A

2

FFCL1-1B1610-20

5 5 5A 5A

150A 330A 140A 350A

1 1 1 1

FFCL1-1B1620-20

5 5 5A 5A

160A 340A 150A 360A

1 1 1 1

FFCL1-1B1630-20

3 3

020B 330A

1 2

FFCL1-1B1661-20

5 5 5A 5A

230A 410A 220A 430A

1 1 1 1

FFCL1-1B1670-20

5A

510A

1

FFCL1-1B1671-20

5 5A

450A 510B

1 1

FFCL1-1B1681-20

5 5A

480A 540A

1 1

FFCL1-1B1681-21

5A

540B

1

FFCL1-1C0002-01

1 1A 8

080A 080A -001A

1 1 RF

FFCL1-1C0022-01

8

090A

2

FFCL1-1C0024-20

8

010A

2

FFCL1-1C0028-20

8

020A

2

FFCL1-1C0030-01

8

080A

1

FFCL1-1C0031-01

8

120A

1

FFCL1-1C0032-01

8

060A

1

FFCL1-1C0032-02

8

070A

1

FFCL1-1D1051-20

10

230A

1

FFCL1-1D1224-20

10

370A

1

- ITEM NOT ILLUSTRATED

ALPHANUMERICAL INDEX PAGE 7 APR 15/09

25-26-80

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIGURE

ITEM

TOTAL REQUIRED

FFCL1-1D1225-20

10

290A

2

FFCL1-1D1226-20

10

300A

2

FFCL1-1D1234-01

10

320A

1

FFCL1-1D1323-01

10

110A

1

FFCL1-1D1325-20

10

130A

2

FFCL1-1D1327-20

10

100A

1

FFCL1-1D1328-20

10

060A

1

FFCL1-1D1329-20

10

040A

2

FFCL1-1D1330-20

10

160A

1

FFCL1-1D1338-20

10

120A

1

FFCL1-1D1344-20

10

170A

1

FFCL1-1D1345-20

10

070A

1

FFCL1-1D1346-20

10

150A

2

FFCL1-1D1347-01

10

190A

2

FFCL1-1E1136-01

7

300A

1

FFCL1-1E1137-20

7

140A

1

FFCL1-1E1144-20

7

180A

4

FFCL1-1E1147-01

7

190A

1

FFCL1-1E1153-20

7

030A

2

FFCL1-1E1156-20

7

060A

2

FFCL1-1E1180-20

1 1A

090A 090A

2 2

FFCL1-1E1181-20

1 1A

100A 100A

4 4

FFCL1-1E1246-01

12 12A

120B 120A

1 1

FFCL1-1F1010-01

1 9

150A -001A

1 RF

FFCL1-1F1010-02

1 9

150B -001B

1 RF

PART NUMBER

- ITEM NOT ILLUSTRATED

AIRLINE STOCK NUMBER

ALPHANUMERICAL INDEX PAGE 8 APR 15/09

25-26-80

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIGURE

ITEM

TOTAL REQUIRED

FFCL1-1F1217-01

9

170A

1

FFCL1-1F1217-02

9

170B

1

FFCL1-1F1218-20

9

540A

1

FFCL1-1F1231-20

9

230A

1

FFCL1-1F1232-20

9

280A

1

FFCL1-1F1234-20

9

220A

3

FFCL1-1F1241-20

9

050A

5

FFCL1-1F1245-20

9

100A

4

FFCL1-1F1248-20

9

320A

1

FFCL1-1F1249-20

9

520A

1

FFCL1-1F1250-01

9

390A

1

FFCL1-1F1250-02

9

390B

1

FFCL1-1F1253-20

9

140A

2

FFCL1-1F1254-31

9

150A

2

FFCL1-1F1271-20

9

370A

1

FFCL1-1F1272-20

9

270A

1

FFCL1-1F1272-21

9

270B

1

FFCL1-1F1315-20

9

360A

2

FFCL1-1F1351-20

9

010A

1

FFCL1-1F1351-21

9

010B

1

FFCL1-1G1014-01

1 1A 11

220A 180A -001A

1 1 RF

FFCL1-1G1014-02

1 1A 11

220B 180B -001B

1 1 RF

FFCL1-1J5010-01

1A 12A

190A -001A

1 RF

FFCL1-2A1007-01

1

010A

1

FFCL1-2A1007-02

1

020A

1

PART NUMBER

- ITEM NOT ILLUSTRATED

AIRLINE STOCK NUMBER

ALPHANUMERICAL INDEX PAGE 9 APR 15/09

25-26-80

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIGURE

ITEM

TOTAL REQUIRED

FFCL1-2A1106-01

1

050A

1

FFCL1-2A1106-02

1

050B

1

FFCL1-2B0522-31

15 16

760A 700A

1 2

FFCL1-2B0523-31

7

220A

1

FFCL1-2B0630-01

15 16

210A 210A

1 2

FFCL1-2B0630-02

15 16

300A 300A

1 2

FFCL1-2B0631-31

15 16

290A 290A

1 1

FFCL1-2B0801-01

1 15

290A -001A

1 RF

FFCL1-2B0801-02

1 15

290B -001B

1 RF

FFCL1-2B0844-01

1 16

300A -001A

1 RF

FFCL1-2B1005-01

1 3

060A -001A

1 RF

FFCL1-2B1005-02

1 3

060B -001B

1 RF

FFCL1-2B1314-03

3 13

350A 080A

1 2

FFCL1-2B1350-05

1

-280A

2

FFCL1-2B1350-07

1A

-240A

2

PART NUMBER

AIRLINE STOCK NUMBER

FFCL1-2B1704-03

13

010A

1

FFCL1-2B1704-04

13

010B

1

FFCL1-2B1710-01

13

065A

1

FFCL1-2B1744-03

13

020A

1

FFCL1-2B1750-01

13

160A

AR

FFCL1-2B1765-03

13

040A

1

FFCL1-2D1006-01

1 1A 10

190A 150A -001A

1 1 RF

- ITEM NOT ILLUSTRATED

ALPHANUMERICAL INDEX PAGE 10 APR 15/09

25-26-80

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIGURE

ITEM

TOTAL REQUIRED

FFCL1-2D1050-01

10

260A

1

FFCL1-2D1204-03

10

280A

1

FFCL1-2D1231-03

10

330A

1

FFCL1-2D1231-04

10

340A

1

FFCL1-2D1300-01

10

010A

1

FFCL1-2D1350-20

10

180A

1

FFCL1-2D1402-03

10

220A

1

FFCL1-2E1102-01

1 7

070A -001A

1 RF

FFCL1-2E1134-03

13

110A

1

FFCL1-2E1135-01

7

160A

1

FFCL1-2E1144-03

13

120A

1

FFCL1-2E1144-04

13

130A

1

FFCL1-2E1196-01

7

010A

1

FFCL1-2E1197-01

7

120A

1

FFCL1-2E1202-01

7

130A

1

FFCL1-2F1315-03

9

430A

1

FFCL1-2F1315-04

9

430B

1

FFCL1-2F1345-03

9

410A

1

FFCL1-2F1345-04

9

410B

1

FFCL1-2F1354-03

9

510A

1

FFCL1-2F1364-01

9

530A

1

FFCL1-2F1505-03

9

490A

1

FFCL1-2F1505-04

9

490B

1

FFCL1-2F1545-03

9

460A

1

FFCL1-2F1545-04

9

460B

1

FFCL1-2H1005-03

1 13

240A -001A

1 RF

PART NUMBER

- ITEM NOT ILLUSTRATED

AIRLINE STOCK NUMBER

ALPHANUMERICAL INDEX PAGE 11 APR 15/09

25-26-80

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE PART NUMBER

AIRLINE STOCK NUMBER

FIGURE

ITEM

TOTAL REQUIRED

FFCL1-2H1005-04

1 13

240B -001B

1 RF

FFCL1-2L1006-01

1 2

040A -001A

1 RF

FFCL1-2L1114-03

2

020A

1

FFCL1-2L1126-01

2

040A

1

FFCL1-2L1134-03

2

060A

1

FFCL1-2L1146-01

2

080A

1

FFCL1-2L1215-03

2

010A

1

FFCL1-2L1227-01

2

030A

1

FFCL1-2L1235-03

2

050A

1

FFCL1-2L1235-05

2

050B

1

FFCL1-2M1060-31

1

310A

1

FFCL1-2M1101-20

1 1A

320A 300A

1 1

FFCL1-2M1104-01

1 1A

320B 290A

1 1

FFCL1-2M1300-20

8

130A

1

FFCL1-2M1304-01

13

070B

1

FFCL1-3B1334-01

3 6

400A -001A

1 RF

FFCL1-3B1335-01

6

010A

1

FFCL1-3B1336-01

6

050A

1

FFCL1-3B1338-01

3 6

400B -001B

1 RF

FFCL1-4E1300-01

1 14

250A -001A

1 RF

FFCL1-4E1301-01

14

240A

1

FFCL1-4E1302-31

14

170A

1

FFCL1-4E1303-01

14

040A

1

FFCL1-4E1304-31

14

210A

1

- ITEM NOT ILLUSTRATED

ALPHANUMERICAL INDEX PAGE 12 APR 15/09

25-26-80

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIGURE

ITEM

TOTAL REQUIRED

FFCL1-4E1305-01

14

010A

1

FFCL1-4E1306-01

14

160A

1

FFCL1-4E1319-01

1A 14

210A -001B

1 RF

FFCL1-4E1320-01

14

240B

1

FFCL1-4E1321-01

14

330A

1

FFCL1-4E1322-01

14

340A

1

FFCL1-4E1323-01

14

360A

1

FFCL1-4E1323-02

14

350A

1

FFCL1-4G1001-01

1 12

230A -001A

1 RF

FFCL1-4L1240-01

2

070A

1

FFCL1-5A1007-01

1A

010A

1

FFCL1-5A1007-02

1A

020A

1

FFCL1-5A1106-01

1A

050A

1

FFCL1-5A1106-02

1A

050B

1

PART NUMBER

AIRLINE STOCK NUMBER

FFCL1-5B0514-31

15

460B

2

FFCL1-5B0522-31

15

760B

1

FFCL1-5B0632-01

15

010B

1

FFCL1-5B0632-02

15

110B

1

FFCL1-5B0643-01

12 12A

270A 360A

1 1

FFCL1-5B0800-01

1A 15

-260A -001C

1 RF

FFCL1-5B0800-02

1A 15

-260B -001D

1 RF

FFCL1-5B0801-01

15

790C

1

FFCL1-5B0801-02

15

790D

1

FFCL1-5B0840-01

1A 16

-270A -001B

1 RF

FFCL1-5B0841-01

16

750B

1

- ITEM NOT ILLUSTRATED

ALPHANUMERICAL INDEX PAGE 13 APR 15/09

25-26-80

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE PART NUMBER

AIRLINE STOCK NUMBER

FIGURE

ITEM

TOTAL REQUIRED

FFCL1-5B1000-01

1A 3

060A -001C

1 1

FFCL1-5B1000-02

1A 3

060B -001D

1 1

FFCL1-5B1300-01

3 5A

300C -001A

1 1

FFCL1-5B1300-02

3 5A

300D -001B

1 1

FFCL1-5B1312-01

5A

250A

1

FFCL1-5B1312-02

5A

460A

1

FFCL1-5B1350-02

5A

300A

1

FFCL1-5B1351-01

5A 5A

270A 480A

1 1

FFCL1-5B1352-01

5A 5A

100A 310A

1 1

FFCL1-5B1353-01

5A 5A

260A 470A

1 1

FFCL1-5B1711-01

13

010C

1

FFCL1-5B1711-02

13

010D

1

FFCL1-5E1000-31

7

450A

1

FFCL1-5E1010-01

7

480A

1

FFCL1-5E1011-01

3

390A

1

FFCL1-5E1100-01

1A 7

070A -001B

1 RF

FFCL1-5E1134-01

13

110B

1

FFCL1-5E1145-01

7

160B

1

FFCL1-5E1146-01

7

300B

1

FFCL1-5E1157-01

7

190B

1

FFCL1-5E1202-01

7

130B

1

FFCL1-5H1005-01

1A 13

200A -001C

1 RF

FFCL1-5H1005-02

1A 13

200B -001D

1 RF

- ITEM NOT ILLUSTRATED

ALPHANUMERICAL INDEX PAGE 14 APR 15/09

25-26-80

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE PART NUMBER

AIRLINE STOCK NUMBER

FIGURE

ITEM

TOTAL REQUIRED

FFCL1-5L1006-01

1A 2

040A -001B

1 RF

FFCL1-5L1050-01

2

090A

1

FFCL1-5L1060-01

2

100A

1

FFCL1-5L1125-01

2

020B

1

FFCL1-5L1130-01

2

040B

1

FFCL1-5L1135-01

2

030B

1

FFCL1-5L1140-01

2

080B

1

FFCL1-5L1145-01

2

070B

1

FFCL1-5L1225-01

2

010B

1

FFCL1-5M1060-31

1A

280A

1

FFCL4-01WY03-01

1

-001C

RF

FFCL4-02WY03-01

1A

-001C

RF

FFCL5-01WY01-01

1

-001A

RF

FFCL5-01WY02-01

1

-001B

RF

FFCL5-02WY01-01

1A

-001A

RF

FFCL5-02WY02-01

1A

-001B

RF

FFCL5-1B1113-01

3

320A

1

FFMU1-1B1307-01

5 5

100A 280A

1 1

FFMU1-1E1128-01

7

330A

1

FFMU1-1E1128-02

7

390A

1

FFMU1-1E1129-01

7

340A

1

FFMU1-1E1129-02

7

400A

1

FFMU1-1F1270-01

9

180A

1

FFMU1-1F1270-02

9

180B

1

FJEV1-1B2074-20

16

740A

4

FJEV1-2E1642-31

14

090A

1

FJEV1-2E1644-31

14

070A

1

- ITEM NOT ILLUSTRATED

ALPHANUMERICAL INDEX PAGE 15 APR 15/09

25-26-80

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIGURE

ITEM

TOTAL REQUIRED

FJEV1-2E1644-32

14

080A

1

FJEV1-2E1648-01

14

130A

1

FJPL1-1B0510-20

15

785A

2

FJPL1-1G1007-20

12 12A

170A 230A

2 2

G51NA

9

400A

AR

HAR640

12

220A

1

HAR641

12

230A

1

HAR644

12 12A

250A 340A

1 1

HAR647

12 12A

240A 330A

1 1

HAR650

12A

280A

1

HAR651

12A

320A

1

HAR659

12A

290A

1

H2P

9

330A

1

KRV26X

5 5 5A 5A

140A 320A 130A 340A

3 3 3 3

LFR50-5KDD4

9

130A

6

LFS20331-9-9-5V

9

110A

2

12

120A

1

PART NUMBER

LSA011

AIRLINE STOCK NUMBER

L23111-100AGL

1 1A

120A 120A

2 2

L23111-50AGL

5A

610A

4

L23111-60AGL

10

240B

1

MS16624-1046

4 4 4 4

120A 180A 330A 390A

1 2 1 2

14

060A

4

MS21042-08

- ITEM NOT ILLUSTRATED

ALPHANUMERICAL INDEX PAGE 16 APR 15/09

25-26-80

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIGURE

ITEM

TOTAL REQUIRED

MS21042-3

3 12 12A

380A 460A 580A

1 2 2

MS21042-4

3

120A

4

MS21042-5

12 12A

-110A -110A

2 2

MS21043-3

14

280A

4

MS24665-210

9 9 10

070A 190A 250A

2 1 1

MS24665-281

7 7

370A 430A

1 1

MS24665-285

1 1A 8

130A 130A 030A

2 2 2

PART NUMBER

AIRLINE STOCK NUMBER

MVS012

11

050A

1

M83723-60-214AN

12 12A

480A 600A

1 1

NAS1102-3-6

10

270A

2

NAS1149C0432R

5A 5A 5A

120A 290A 500A

1 2 2

NAS1149DN816J

5 12 12A 13

500B 140A 140A 060B

2 4 4 4

NAS1149DN832J

5 14

470B 110B

2 1

NAS1149DN832K

15 16 16

680A 690A 730A

4 1 2

NAS1149D0316J

13

100B

2

NAS1149D0332H

12 12A

450A 560A

6 6

NAS1149D0332J

14 14

270A 320A

8 4

NAS1149D0363H

5

030B

1

- ITEM NOT ILLUSTRATED

ALPHANUMERICAL INDEX PAGE 17 APR 15/09

25-26-80

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIGURE

ITEM

TOTAL REQUIRED

NAS1149D0416K

15

510A

2

NAS1149FN232P

12 12 12A

200A -210A -270A

4 4 4

NAS1149FN416P

12 12 12A

440A 520A 550A

4 6 4

NAS1149FN432P

6

100A

2

NAS1149FN632P

12A 15 16 16

570A 670A 680A 720A

1 4 1 2

NAS1149FN816P

7 11 11

050A 120A 120B

6 7 6

NAS1149FN832P

7 12 12 12A 12A 12A 14 14 15 15 15

500A 146A 200B 170A 200A 260A -125A 200A 710A 750A 780A

2 1 4 1 4 12 4 8 2 2 2

NAS1149F0332P

1A 1A 1A 3 3 3 3 3 4 4 4 6 6 6 7 7 7 7 7 7 7

170A 230A -250A 200A 250A 370A 430A 430B 030A 060A 270A 040A 070A 190A 100A 175A 210A 240A 280A 320A 470A

4 4 4 4 8 1 6 2 2 4 4 3 3 10 1 4 6 2 5 8 2

PART NUMBER

- ITEM NOT ILLUSTRATED

AIRLINE STOCK NUMBER

ALPHANUMERICAL INDEX PAGE 18 APR 15/09

25-26-80

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIGURE

ITEM

TOTAL REQUIRED

NAS1149F0332P (CONT’D)

7 7 8 12 12A 14 14 15 16

530A 560A 110A 430A 540A 030A 150A 480A 500A

1 1 6 6 6 4 2 2 1

NAS1149F0363P

15

720A

1

NAS1149F0432P

1 1 1 3 12 12A 15 15 15 15 16 16 16 16 16 16

180B 210B 270B 110A 030A 030A 030A 130A 250A 340A 030A 130A 250A 340A 420A 530A

4 4 4 4 4 4 6 6 5 5 6 6 5 5 4 2

NAS1149F0532P

3 10 12 12 12A 12A

220A 210A 060A 100A 060A 100A

2 1 2 4 2 4

NAS1351-02-6

12 12A

180A 240A

4 4

NAS1352-04-4

10

050A

2

NAS1352-06-12P

16

710A

2

NAS1352-08-10P

9

120A

8

NAS1801-06-4

12

190A

4

NAS1801-06-5

12A

530A

1

NAS1801-06-7

12 12A

190B 250A

4 4

NAS1801-08-10

14

190A

8

PART NUMBER

- ITEM NOT ILLUSTRATED

AIRLINE STOCK NUMBER

ALPHANUMERICAL INDEX PAGE 19 APR 15/09

25-26-80

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIGURE

ITEM

TOTAL REQUIRED

NAS1801-08-11

3

270A

4

NAS1801-08-13

9

020A

2

NAS1801-08-5

7

490A

2

NAS1801-08-6

9 12 12A

290A 130A 130A

1 4 4

NAS1801-08-7

15 15 16 16

050A 150A 050A 150A

4 4 4 4

NAS1801-08-8

5 5A 11 11 12A 15 15

490A 550A 090A 110B 190A 740A 770A

1 1 5 1 4 2 2

NAS1801-08-9

14 15

050A 700A

4 2

NAS1801-3-10

1 1A 3 6 7 10

260A 220A 410A 180A 520A 020A

4 4 2 1 1 4

NAS1801-3-11

4 4 4

020A 050A 260A

2 4 4

NAS1801-3-12

12

-370A

1

NAS1801-3-13

7 12 12A

090A -380B -470A

1 1 1

NAS1801-3-14

7 7 11 14

260A 550A 100A 020B

3 1 1 4

NAS1801-3-15

12 12A

400A 490A

1 1

NAS1801-3-17

6

140A

5

NAS1801-3-22

6

160A

2

PART NUMBER

- ITEM NOT ILLUSTRATED

AIRLINE STOCK NUMBER

ALPHANUMERICAL INDEX PAGE 20 APR 15/09

25-26-80

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIGURE

ITEM

TOTAL REQUIRED

NAS1801-3-24

6

170B

1

NAS1801-3-26

12 12A

410A 500A

1 1

NAS1801-3-28

7

170B

4

NAS1801-3-30

6

170A

1

NAS1801-3-5

7 7

230A 460A

2 2

NAS1801-3-6

7 7 7

200A 290A 310A

6 2 8

NAS1801-3-7

5A 10

600A 350A

4 10

NAS1801-3-8

6 6 6 12

020A 060A 150A -370B

3 3 1 1

NAS1801-3-9

3 3 5 5 5 5 5A 5A 5A 5A 12

190A 240A 180A 210A 360A 390A 170A 200A 380A 410A -380A

4 8 3 2 3 2 3 2 3 2 1

12A 14 14 14 14

-460A 020A 140A 260A 310A

1 4 2 4 4

5A 5A

280A 490A

2 2

NAS514P1032-14

12 12A

390A 480A

2 2

NAS514P1032-16

13

140A

6

NAS514P1032-22

7

070A

2

NAS514P1032-28

7

170A

4

PART NUMBER

NAS1801-4-11

- ITEM NOT ILLUSTRATED

AIRLINE STOCK NUMBER

ALPHANUMERICAL INDEX PAGE 21 APR 15/09

25-26-80

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIGURE

ITEM

TOTAL REQUIRED

NAS514P1032-8

9 9 9 15

420A 440A 470A 470B

1 2 2 2

NAS514P428-6

15

580A

2

NAS514P632-5

15

786A

2

NAS514P632-6

6 14

030A 220A

3 2

NAS514P832-10

9

500A

1

NAS514P832-12

13

030A

6

NAS514P832-14

9 9

160A 240A

4 4

NAS514P832-8

7 7

020A 150A

2 2

9 15 16

340A 630A 640A

1 4 2

NAS517-4-12

15 16

400A 570A

8 4

NAS517-4-9

15 15 16

540A 560A 550A

2 2 4

NAS600-13

6

090A

2

NAS600-19

12 12A

420A 510A

2 2

NAS600-6

12 12A

510A 520A

6 2

NAS601-6P

15 16

650A 660A

4 1

NAS602-10P

5 5A 7 15 15 16 16

460A 520A 040A 080A 180A 080A 180A

2 2 6 4 4 4 4

NAS602-14

14

100A

1

PART NUMBER

- ITEM NOT ILLUSTRATED

AIRLINE STOCK NUMBER

ALPHANUMERICAL INDEX PAGE 22 APR 15/09

25-26-80

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIGURE

ITEM

TOTAL REQUIRED

NAS602-6P

9 13 15 16

380A 050A 660A 670A

1 4 4 1

NAS602-7

10

380A

4

PART NUMBER

AIRLINE STOCK NUMBER

NAS602-7P

5 5 5A 5A

240A 420A 230A 440A

2 2 2 2

NAS602-8P

12 12A

145A 160A

1 1

NAS603-11

13

090A

2

200A 160A

4 4

NAS603-12

1 1A

NAS603-16

15 16

610A 620A

2 2

NAS603-7

3 3 15 16

360A 420A 470A 490A

1 4 2 1

NAS603-8

12 12A

280A 370A

2 2

NAS604-11

15 15 15 15 16 16 16 16

020A 120A 220A 310A 020A 120A 220A 310A

6 6 2 2 6 6 2 2

NAS604-18

15

500A

2

NAS604-28

15 15 16

230A 320A 230A

1 1 1

16

320A

1

15 15 16 16

240A 330A 240A 330A

2 2 2 2

NAS604-36

- ITEM NOT ILLUSTRATED

ALPHANUMERICAL INDEX PAGE 23 APR 15/09

25-26-80

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIGURE

ITEM

TOTAL REQUIRED

15 15 16 16

270A 360A 270A 360A

1 1 1 1

NAS623-3-3

8

100A

6

NAS623-3-6

5 5A

020A 020A

1 1

NAS6605-6

3

210A

2

NAS679A04

12 12A

-470A -590A

2 2

NAS679A06

9 14

350A 230A

1 2

NAS679A08

9 9

040A 260A

2 4

7 7 12 12A

350A 410A 144A 150A

1 1 2 2

9

480A

2

NSA5319-04-25

10

090A

3

NSA5319-04-30

4 4 15 16

230A 440A 430A -450A

1 1 1 1

NSA5319-05-25

4

480A

2

NSA5319-07-25

10

080A

3

NSA5319-08-25

4 4

160A 370A

1 1

NSA5319-08-35

4 4

220A 430A

1 1

NSA5319-08-40

4 4 4 4

140A 200A 350A 410A

1 1 1 1

NSA5319-09-25

4

490A

2

PART NUMBER

NAS604-8

NATR6

NSA5066-3-1

- ITEM NOT ILLUSTRATED

AIRLINE STOCK NUMBER

ALPHANUMERICAL INDEX PAGE 24 APR 15/09

25-26-80

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE PART NUMBER

NSA5319-12-50

AIRLINE STOCK NUMBER

FIGURE

5 5 5A 5A

ITEM

TOTAL REQUIRED

050A 070A 050A 070A

2 1 2 1

NSA5456-3-4

11 11

070A 070B

4 3

NSA5516-04ND

6 11 11

120A 080A 080B

4 10 8

NSA5527-03-04

12 12A 14

330A 420A 035A

3 3 4

NSA5527-03-05

7 7

110A 570A

1 1

NSA5527-03-06

11 14

140A 120A

1 1

NSA5527-03-08

6

210A

3

NSA5527-03-11

12 12A

350A 440A

1 1

NSA5527-03-12

12 12A

-340A -430A

2 2

NSA5527-03-16

6 6 7 12

110A 200A 270A -360A

2 6 3 1

NSA935401-04

11 11

060A 060B

2 4

NSA935401-05

12A

-450A

50

NSA935504-01

6 7 7 7 7 12 12A

130A 080A 250A 510A 540A 290A 380A

8 1 5 1 1 3 4

NSA935504-03

12 12A

300A 390A

1 1

NSA935513-05

12 12A

310A 400A

3 3

- ITEM NOT ILLUSTRATED

ALPHANUMERICAL INDEX PAGE 25 APR 15/09

25-26-80

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIGURE

ITEM

TOTAL REQUIRED

NSA935513-07

12 12A

320A 410A

1 1

PAF12070P11

4 4 4 4

080A 100A 290A 310A

2 2 2 2

P81011A010

12 12A

160A 220A

1 1

RSA012

12 12A

070A 070A

1 1

RSA013

12 12A

040A 040A

1 1

SB1-015-001-02

5A

590A

AR

SB1-015-001-04

5

530A

AR

SB3-011-107-01

9

310A

1

SB3-011-108-01

11

010A

1

SB3-011-108-02

11

020A

1

SB5-011-021-01

14

290A

2

SB5-300-001-01

3

130A

1

SR300A015040I

12 12A

-260A 350A

1 1

5 5A

510A 570A

1 1

PART NUMBER

TA1390

AIRLINE STOCK NUMBER

WJ200QMS38083AA

14

180A

4

22271BC030006L

3

140A

2

22719BC060024L

7 7

360A 420A

1 1

22719BC080027L

15 16

-440A -460A

1 1

22719BC080031L

9 9

090A -210A

2 1

22719BC100039L

8

050A

2

- ITEM NOT ILLUSTRATED

ALPHANUMERICAL INDEX PAGE 26 APR 15/09

25-26-80

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE PART NUMBER

AIRLINE STOCK NUMBER

FIGURE

ITEM

TOTAL REQUIRED

23111AG050LE

5 5 5 5 5A 5A 5A 5A

190A 220A 370A 400A 180A 210A 390A 420A

3 2 3 2 3 2 3 2

23111AG100LE

8

040A

4

23201AM0080T

3 3 3

030A 050A 340A

1 1 1

250-75N588539

9

060A

1

33083-00

12A

310A

1

33084-00

12A

300A

1

35016-00

12A

180A

1

504250-419-8167

1 1A

030A 030A

1 1

856AV52

3

130B

1

- ITEM NOT ILLUSTRATED

ALPHANUMERICAL INDEX PAGE 27 APR 15/09

25-26-80

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

PAGE INTENTIONALLY LEFT BLANK

ALPHANUMERICAL INDEX PAGE 28 APR 15/09

25-26-80

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01

DETAILED PART LIST

25-26-80

DPL 10001 FEV 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE 240

20

50 150 160 170 180

10

300

40 CUSHION ASSY : FFCL1-5L1006-01 COMPONENTS

30

FFCL1-5L1030-01 FFCL1-5L1020-01 FFCL1-5L1040-01 FFCL1-5L1050-01 FFCL1-5L1060-01 FFCL1-5L1120-01

310 FFCL1-5M1060-31

AIRBUS SPECIFICATION 2521 M1F 1000 00

FWD : DWN : UP : SIDE : AFT :

290

9.0 g 7.3 g 4.2 g 4.0 g 1.5 g

320 FFCL1-2M1104-01

FIRST CLASS SEAT (SHEET 1 OF 2) FIGURE 01 / GRAPHIC 25-26-80-991-001-A01

25-26-80

PAGE 10001-0 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

90 100

250 260 270

110 120 130 140

70 200 210

60 80

190

220 230

FIRST CLASS SEAT (SHEET 2 OF 2) FIGURE 01 / GRAPHIC 25-26-80-991-002-A01

25-26-80

PAGE 10001-1 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

1 -001A

FFCL5-01WY01-01

1 SEAT, SINGLE LH ASSY

RF

-001B

FFCL5-01WY02-01

1 SEAT, SINGLE RH ASSY

RF

-001C

FFCL4-01WY03-01

1 SEAT, DOUBLE CTR ASSY

RF

010A

FFCL1-2A1007-01

2 SEAT, EQUIPPED LH SIDE

1AC

1

020A

FFCL1-2A1007-02

2 SEAT, EQUIPPED RH SIDE

1BC

1

030A

504250-419-8167

3 BELT, ASSY (V 35FB9) SEE ACMM 25-24-57 FOR DET

1

040A

FFCL1-2L1006-01

3 CUSHION, ASSY (NP) SEE 252680-02, 001A FOR DET

1

050A

FFCL1-2A1106-01

3 STRUCTURE, LH EQUIPPED

(NP)

10A

1

050B

FFCL1-2A1106-02

3 STRUCTURE, LH EQUIPPED

(NP)

20A

1

060A

FFCL1-2B1005-01

4 BASE, LH ASSY (NP) SEE 252680-03, 001A FOR DET

50A

1

060B

FFCL1-2B1005-02

4 BASE, RH ASSY (NP) SEE 252680-03, 001B FOR DET

50B

1

070A

FFCL1-2E1102-01

4 SEAT BACK, ASSY SEE 252680-07, 001A FOR DET

1

080A

FFCL1-1C0002-01

4 SEAT BOTTOM, ASSY SEE 252680-08, 001A FOR DET

1

090A

FFCL1-1E1180-20

4 PIN

2

100A

FFCL1-1E1181-20

4 WASHER

4

110A

FFCL1-1A1151-20

4 PIN, ROD

2

120A

L23111-100AGL

4 WASHER

2

130A

MS24665-285

4 PIN, COTTER

2

140A

FFCL1-1B1522-20

4 SPACER

2

150A

FFCL1-1F1010-01

4 ARMREST, ASSY SEE 252680-09, 001A FOR DET

50A

1

150B

FFCL1-1F1010-02

4 ARMREST, ASSY SEE 252680-09, 001B FOR DET

50B

1

160A

AN174H7A

ATTACHING PARTS 4 SCREW, HEX. HEAD

2

170A

AN174-6A

4 SCREW, HEX. HEAD

2

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10001-2 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

1 180A

AN960-416L

4 DELETED, SUPSD BY ITEM 180B

4

180B

NAS1149F0432P

4 WASHER SUSPDS ITEM 180A XXX

4

190A

FFCL1-2D1006-01

4 LEGREST, ASSY SEE 252680-10, 001A FOR DET

1

200A

NAS603-12

ATTACHING PARTS 4 SCREW, TRUSS HEAD

4

210A

AN960-10L

4 DELETED, SUPSD BY ITEM 210B

4

210B

NAS1149F0432P

4 WASHER SUSPDS ITEM 210A XXX

4

220A

FFCL1-1G1014-01

4 CABLE, LH MECHANICAL ASSY SEE 252680-11, 001A FOR DET

50A

1

220B

FFCL1-1G1014-02

4 CABLE, RH MECHANICAL ASSY SEE 252680-11, 001B FOR DET

50B

1

230A

FFCL1-4G1001-01

4 CABLE, LH ELECTRICAL ASSY (NP) SEE 252680-12, 001A FOR DET

240A

FFCL1-2H1005-03

4 COVERING, LH ASSY SEE 252680-13, 001A FOR DET

50A

1

240B

FFCL1-2H1005-04

4 COVERING, RH ASSY SEE 252680-13, 001B FOR DET

50B

1

250A

FFCL1-4E1300-01

4 HEAD REST, ASSY SEE 252680-14, 001A FOR DET

260A

NAS1801-3-10

ATTACHING PARTS 4 SCREW, HEX. HEAD

4

270A

AN960-10L

4 DELETED, SUPSD BY ITEM 270B

4

270B

NAS1149F0432P

4 WASHER SUSPDS ITEM 270A XXX

4

-280A

FFCL1-2B1350-05

4 FITTING

2

290A

FFCL1-2B0801-01

2 PALLET, LH ASSY SEE 252680-15, 001A FOR DET

1A

1

290B

FFCL1-2B0801-02

2 PALLET, RH ASSY SEE 252680-15, 001B FOR DET

1B

1

1

1

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10001-3 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

NOMENCLATURE

USAGE FROM TO

UNITS PER ASSY

1 300A

FFCL1-2B0844-01

2 PALLET, CTR ASSY SEE 252680-16, 001A FOR DET

1C

1

310A

FFCL1-2M1060-31

2 LABEL, CUSHION

1

320A

FFCL1-2M1101-20

2 DELETED, SUPSD BY ITEM 320B

1

320B

FFCL1-2M1104-01

2 LABEL, LOAD SUSPDS ITEM 320A

1

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10001-4 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

PAGE INTENTIONALLY LEFT BLANK

25-26-80

PAGE 10001-5 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE 200

20 10 50 CUSHION ASSY : FFCL1-5L1006-01 COMPONENTS FFCL1-5L1030-01 FFCL1-5L1020-01 FFCL1-5L1040-01 FFCL1-5L1050-01 FFCL1-5L1060-01 FFCL1-5L1120-01

280 FFCL1-5M1060-31

40

AIRBUS SPECIFICATION 2521 M1F 1000 00

30

FWD : DWN : UP : SIDE : AFT :

9.0 g 7.3 g 4.2 g 4.0 g 1.5 g

290 FFCL1-2M1104-01

AIRBUS SPECIFICATION 2520 M1F 0100 00 CHAP:6.2.1 FWD:

9.0g

DWN:

7.3g

UP:

4.2g

SIDE:

4.0g

AFT:

1.5g

300 FFCL1-2M1101-20

FIRST CLASS SEAT (SHEET 1 OF 2) FIGURE 01A / GRAPHIC 25-26-80-991-058-A01

25-26-80

PAGE 10001A-0 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

90 100 210 220 230 110 120 130 140 70

80

60

150 160 170

180 190

FIRST CLASS SEAT (SHEET 2 OF 2) FIGURE 01A / GRAPHIC 25-26-80-991-059-A01

25-26-80

PAGE 10001A-1 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

1A -001A

FFCL5-02WY01-01

1 SEAT, SINGLE LH ASSY

RF

-001B

FFCL5-02WY02-01

1 SEAT, SINGLE RH ASSY

RF

-001C

FFCL4-02WY03-01

1 SEAT, DOUBLE CTR ASSY

RF

010A

FFCL1-5A1007-01

2 SEAT, EQUIPPED LH SIDE

1AC

1

020A

FFCL1-5A1007-02

2 SEAT, EQUIPPED RH SIDE

1BC

1

030A

504250-419-8167

3 BELT, ASSY (V 35FB9) SEE ACMM 25-24-57 FOR DET

1

040A

FFCL1-5L1006-01

3 CUSHION, ASSY (NP) SEE 252680-02, 001A FOR DET

1

050A

FFCL1-5A1106-01

3 STRUCTURE, LH EQUIPPED

(NP)

10A

1

050B

FFCL1-5A1106-02

3 STRUCTURE, LH EQUIPPED

(NP)

20A

1

060A

FFCL1-5B1000-01

4 BASE, LH ASSY (NP) SEE 252680-03, 001A FOR DET

50A

1

060B

FFCL1-5B1000-02

4 BASE, RH ASSY (NP) SEE 252680-03, 001B FOR DET

50B

1

070A

FFCL1-5E1100-01

4 SEAT BACK, ASSY SEE 252680-07, 001A FOR DET

1

080A

FFCL1-1C0002-01

4 SEAT BOTTOM, ASSY SEE 252680-08, 001A FOR DET

1

090A

FFCL1-1E1180-20

4 PIN

2

100A

FFCL1-1E1181-20

4 WASHER

4

110A

FFCL1-1A1151-20

4 PIN, ROD

2

120A

L23111-100AGL

4 WASHER

2

130A

MS24665-285

4 PIN, COTTER

2

140A

FFCL1-1B1522-20

4 SPACER

2

150A

FFCL1-2D1006-01

4 LEGREST, ASSY SEE 252680-10, 001A FOR DET

1

160A

NAS603-12

170A

NAS1149F0332P

4 WASHER XXX

180A

FFCL1-1G1014-01

4 CABLE, LH MECHANICAL ASSY SEE 252680-11, 001A FOR DET

ATTACHING PARTS 4 SCREW, TRUSS HEAD

4 4 50A

1

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10001A-2 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

1A 180B

FFCL1-1G1014-02

4 CABLE, RH MECHANICAL ASSY SEE 252680-11, 001B FOR DET

190A

FFCL1-1J5010-01

4 CABLE, ELECTRICAL ASSY (NP) SEE 252680-12, 001A FOR DET

200A

FFCL1-5H1005-01

4 COVERING, LH ASSY SEE 252680-13, 001A FOR DET

50A

1

200B

FFCL1-5H1005-02

4 COVERING, RH ASSY SEE 252680-13, 001B FOR DET

50B

1

210A

FFCL1-4E1319-01

4 HEAD REST, ASSY SEE 252680-14, 001A FOR DET

220A

NAS1801-3-10

230A

NAS1149F0332P

4 WASHER XXX

4

-240A

FFCL1-2B1350-07

4 FITTING

2

-250A

NAS1149F0332P

4 WASHER

4

-260A

FFCL1-5B0800-01

2 PALLET, LH ASSY SEE 252680-15, 001A FOR DET

1A

1

-260B

FFCL1-5B0800-02

2 PALLET, RH ASSY SEE 252680-15, 001B FOR DET

1B

1

-270A

FFCL1-5B0840-01

2 PALLET, CTR ASSY SEE 252680-16, 001A FOR DET

1C

1

280A

FFCL1-5M1060-31

2 LABEL, CUSHION

290A

FFCL1-2M1104-01

2 LABEL, LOAD

1AB

1

300A

FFCL1-2M1101-20

2 LABEL, LOAD

1C

1

50B

1 1

1

ATTACHING PARTS 4 SCREW, HEX. HEAD

4

1

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10001A-3 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

70 80

90

100

30 40

10

20

50 60

CUSHION ASSEMBLY FIGURE 02 / GRAPHIC 25-26-80-991-003-A01

25-26-80

PAGE 10002-0 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

2 -001A

FFCL1-2L1006-01

1 CUSHION, ASSY (NP) SEE 252680-01, 040A FOR NHA

RF

-001B

FFCL1-5L1006-01

1 CUSHION, ASSY (NP) SEE 252680-01A, 040A FOR NHA

RF

010A

FFCL1-2L1215-03

2 COVER, SEAT BOTTOM

1A

1

010B

FFCL1-5L1225-01

2 COVER, SEAT BOTTOM

1B

1

020A

FFCL1-2L1114-03

2 FOAM, SEAT BOTTOM

1A

1

020B

FFCL1-5L1125-01

2 FOAM, SEAT BOTTOM

1B

1

030A

FFCL1-2L1227-01

2 COVER, SEAT BACK

1A

1

030B

FFCL1-5L1135-01

2 COVER, SEAT BACK

1B

1

040A

FFCL1-2L1126-01

2 FOAM, SEAT BACK

1A

1

040B

FFCL1-5L1130-01

2 FOAM, SEAT BACK

1B

1

050A

FFCL1-2L1235-03

2 COVER, LEG REST

1A

1

050B

FFCL1-2L1235-05

2 COVER, LEG REST

1B

1

060A

FFCL1-2L1134-03

2 FOAM, LEG REST

070A

FFCL1-4L1240-01

2 COVER, HEAD REST

1A

1

070B

FFCL1-5L1145-01

2 COVER, HEAD REST

1B

1

080A

FFCL1-2L1146-01

2 FOAM, HEAD REST

1A

1

080B

FFCL1-5L1140-01

2 FOAM, HEAD REST

1B

1

090A

FFCL1-5L1050-01

2 FOAM, REAR SEAT BACK

1B

1

100A

FFCL1-5L1060-01

2 FOAM, REAR HEAD REST

1B

1

1

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10002-1 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE 330 340 40 50

80

10

85

60 70 260

40 50

90 170

160

20 30 35

130

100 110 120

270 280

230 290

140

150

VIEW A

90

400

180

420 430

350 360 370 380

300

390 210 220

290 230

410 430

190 200

A

WARNING

320 310

240 250

RAISE LEG REST FULLY BEFORE REMOVING THE ACTUATOR

310

(STRAP UNDER TENSION) ET5-010-001-04

BASE ASSEMBLY FIGURE 03 / GRAPHIC 25-26-80-991-004-A01

25-26-80

PAGE 10003-0 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

3 -001A

FFCL1-2B1005-01

1 BASE, LH ASSY (NP) SEE 252680-01, 060A FOR NHA

RF

-001B

FFCL1-2B1005-02

1 BASE, RH ASSY (NP) SEE 252680-01, 060B FOR NHA

RF

-001C

FFCL1-5B1000-01

1 BASE, LH ASSY (NP) SEE 252680-01A, 060A FOR NHA

1

-001D

FFCL1-5B1000-02

1 BASE, RH ASSY (NP) SEE 252680-01A, 060B FOR NHA

1

010A

FFCL1-1B1512-03

2 LINK

2

020A

FFCL1-1B1513-20

ATTACHING PARTS 2 DELETED, SUPSD BY ITEM 020B

020B

FFCL1-1B1630-20

2 PIN, SHOULDERED SUPSDS ITEM 020A

(NP)

1

030A

23201AM0080T

2 RING, RETAINER XXX

(NP)

1

035A

FFCL1-1B1292-20

2 BUSH, SHOULDERED

(NP)

040A

FFCL1-1B1530-20

2 ROLLER

2

050A

23201AM0080T

ATTACHING PARTS 2 RING, RETAINER

1

060A

FFCL1-1B1513-20

2 PIN, SHOULDERED

1

070A

AN960-516L

2 WASHER XXX

1

080A

FFCL1-1B1511-01

2 LINK, ELBOWED

(NP)

1

085A

FFCL1-1B1514-01

2 LINK, ELBOWED

(NP)

1

090A

FFCL1-1B1401-01

2 ELECTROMAGNET, EQUIPPED

2

100A

AN174-14A

ATTACHING PARTS 2 SCREW, HEX. HEAD

4

110A

NAS1149F0432P

2 WASHER

4

120A

MS21042-4

2 NUT, SELF-LOCKING XXX

4

130A

SB5-300-001-01

3 ELECTROMAGNET SL1, SL2

(NP)

1

(NP)

1CD

4

1

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10003-1 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

3 130B

856AV52

3 ELECTROMAGNET

(NPV F1484)

1

140A

22271BC030006L

ATTACHING PARTS 3 SCREW, TRUSS HEAD XXX

(NP)

2

150A

FFCL1-1B1420-20

3 PIN, LOCKING (NP) BONDED WITH LOCTITE 221 MADE BY F7121

1

160A

FFCL1-1B1430-20

3 STOP, CABLE BONDED WITH LOCTITE 221 MADE BY F7121

1

170A

FFCL1-1B1411-20

3 SUPPORT

180A

FFCL1-1B1203-01

2 CROSSBEAM, REAR ASSY SEE 252680-04, 001A FOR DET

190A

NAS1801-3-9

200A

NAS1149F0332P

2 WASHER XXX

4

210A

NAS6605-6

2 SCREW, HEX. HEAD

2

220A

NAS1149F0532P

2 WASHER

2

230A

FFCL1-1B1101-01

2 CROSSBEAM, FRONT ASSY

(NP)

1

240A

NAS1801-3-9

ATTACHING PARTS 2 SCREW, HEX. HEAD

(NP)

8

250A

NAS1149F0332P

2 WASHER XXX

(NP)

8

260A

FFCL1-1B1121-01

3 BEARING

(NP)

2

270A

NAS1801-08-11

ATTACHING PARTS 3 SCREW, HEX. HEAD

(NP)

4

280A

AN960-8L

3 WASHER XXX

(NP)

4

290A

FFCL1-1B1111-01

3 CROSSBEAM, FRONT

(NP)

1

300A

FFCL1-1B1304-03

2 STRUCTURE, BASE ASSY (NP) SEE 252680-05, 001A FOR DET

1A

1

300B

FFCL1-1B1304-04

2 STRUCTURE, BASE ASSY (NP) SEE 252680-05, 001B FOR DET

1B

1

300C

FFCL1-5B1300-01

2 STRUCTURE, BASE ASSY (NP) SEE 252680-05, 001C FOR DET

1C

1

(NP)

1 1

ATTACHING PARTS 2 SCREW, HEX. HEAD

4

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10003-2 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

3 300D

FFCL1-5B1300-02

2 STRUCTURE, BASE ASSY (NP) SEE 252680-05, 001C FOR DET

1D

1

310A

ET5-010-001-04

2 LABEL, LEGREST

1AB

1

320A

FFCL5-1B1113-01

2 SHIM

(NP)

330A

FFCL1-1B1630-20

2 PIN, SHOULDERED

(NP)

1AB

2

340A

23201AM0080T

2 RING, RETAINER

(NP)

1AB

1

350A

FFCL1-2B1314-03

2 HOOK

1AB

1

360A

NAS603-7

ATTACHING PARTS 2 SCREW, TRUSS HEAD

1AB

1

370A

NAS1149F0332P

2 WASHER

1AB

1

380A

MS21042-3

2 NUT, SELF-LOCKING XXX

1AB

1

390A

FFCL1-5E1011-01

2 BRACKET

400A

FFCL1-3B1334-01

2 SUPPORT, ECU EQUIPPED (NP) SEE 252680-06, 001A FOR DET

1AC

1

400B

FFCL1-3B1338-01

2 SUPPORT, ECU EQUIPPED (NP) SEE 252680-06, 001B FOR DET

1BD

1

410A

NAS1801-3-10

ATTACHING PARTS 2 SCREW, HEX. HEAD

420A

NAS603-7

2 SCREW, TRUSS HEAD

1AB

4

430A

NAS1149F0332P

2 WASHER

1AB

6

430B

NAS1149F0332P

2 WASHER XXX

1CD

2

1

1

2

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10003-3 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE 280

370 250

340 350

290 360

300 310

260 270 450

320 330

460 290

380 390

20 30 10

430 420 410 440

400

80 90 100

110

130 140

480 490

470

70 80

160

470

50 60

480 490

150 90 100 240

120

200 190 40 170 180 210 220 230

REAR CROSSBEAM ASSEMBLY FIGURE 04 / GRAPHIC 25-26-80-991-005-A01

25-26-80

PAGE 10004-0 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

4 -001A

FFCL1-1B1203-01

1 CROSSBEAM, REAR ASSY SEE 252680-03, 180A FOR NHA

010A

FFCL1-1B1221-01

2 SUPPORT, ACTUATOR

1

020A

NAS1801-3-11

ATTACHING PARTS 2 SCREW, HEX. HEAD

2

030A

NAS1149F0332P

2 WASHER XXX

040A

FFCL1-1B1231-01

2 BEARING, ASSY

(NP)

1

050A

NAS1801-3-11

ATTACHING PARTS 2 SCREW, HEX. HEAD

(NP)

4

060A

NAS1149F0332P

2 WASHER XXX

(NP)

4

070A

FFCL1-1B1233-01

3 BEARING, EQUIPPED

080A

PAF12070P11

4 BUSH, SHOULDERED

090A

FFCL1-1B1233-02

3 BEARING, EQUIPPED

100A

PAF12070P11

4 BUSH, SHOULDERED

110A

FFCL1-1B1257-20

120A

RF

2

1 (NPV F0563)

2

(NP)

1

(NPV F0563)

2

3 PIN, SEAT BACK

(NP)

1

MS16624-1046

ATTACHING PARTS 3 RING XXX

(NP)

1

130A

FFCL1-1B1268-20

3 PULLEY, SEAT BACK

(NP)

1

140A

NSA5319-08-40

ATTACHING PARTS 3 PIN, SPRING XXX

(NPV F5442)

1

150A

FFCL1-1B1256-20

3 GEAR, SEAT BACK

(NP)

1

160A

NSA5319-08-25

ATTACHING PARTS 3 PIN, SPRING XXX

(NPV F5442)

1

170A

FFCL1-1B1259-20

3 PIN, BASE

(NP)

1

180A

MS16624-1046

ATTACHING PARTS 3 RING XXX

(NP)

2

190A

FFCL1-1B1269-20

3 PULLEY, BASE

(NP)

1

200A

NSA5319-08-40

ATTACHING PARTS 3 PIN, SPRING XXX

(NPV F5442)

1

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10004-1 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

4 210A

FFCL1-1B1258-20

3 GEAR, BASE

(NP)

1

220A

NSA5319-08-35

ATTACHING PARTS 3 PIN, SPRING

(NPV F5442)

1

230A

NSA5319-04-30

3 PIN, SPRING XXX

(NPV F5442)

1

240A

AT5-375-25

3 BELT

(NPV FA4Y6)

1

250A

FFCL1-1B1231-02

2 BEARING, ASSY

1

260A

NAS1801-3-11

ATTACHING PARTS 2 SCREW, HEX. HEAD

4

270A

NAS1149F0332P

2 WASHER XXX

280A

FFCL1-1B1233-01

3 BEARING, EQUIPPED

290A

PAF12070P11

4 BUSH, SHOULDERED

300A

FFCL1-1B1233-02

3 BEARING, EQUIPPED

310A

PAF12070P11

4 BUSH, SHOULDERED

320A

FFCL1-1B1257-20

330A

4 (NP)

1

(NPV F0563)

2

(NP)

1

(NPV F0563)

2

3 PIN, SEAT BACK

(NP)

1

MS16624-1046

ATTACHING PARTS 3 RING XXX

(NP)

1

340A

FFCL1-1B1268-20

3 PULLEY, SEAT BACK

(NP)

1

350A

NSA5319-08-40

ATTACHING PARTS 3 PIN, SPRING XXX

(NPV F5442)

1

360A

FFCL1-1B1256-20

3 GEAR, SEAT BACK

(NP)

1

370A

NSA5319-08-25

ATTACHING PARTS 3 PIN, SPRING XXX

(NPV F5442)

1

380A

FFCL1-1B1259-20

3 PIN, BASE

(NP)

1

390A

MS16624-1046

ATTACHING PARTS 3 RING XXX

(NP)

2

400A

FFCL1-1B1269-20

3 PULLEY, BASE

(NP)

1

410A

NSA5319-08-40

ATTACHING PARTS 3 PIN, SPRING XXX

(NPV F5442)

1

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10004-2 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

4 420A

FFCL1-1B1258-20

3 GEAR, BASE ATTACHING PARTS 3 PIN, SPRING

430A

NSA5319-08-35

440A

NSA5319-04-30

3 PIN, SPRING XXX

450A

AT5-375-25

3 BELT

460A

FFCL1-1B1212-01

2 CROSSBEAM, REAR

1

470A

FFCL1-1B1245-20

2 BUSH, COUPLING

2

480A

NSA5319-05-25

ATTACHING PARTS 2 PIN, SPRING

490A

NSA5319-09-25

2 PIN, SPRING XXX

1 (V F5442)

1

(V F5442)

1

(NPV FA4Y6)

1

(NPV F5442)

2

(NPV F5442)

2

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10004-3 FEB20 /09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 180 190

170

480 490 500 510

100

450

110 120 130

460 470 10 20 30 50

60 70

230 240 250

200

270 440

210 220 90 260

A 140 150 160

40 80 530

VIEW A

520

350 360 370

280

290 300 310

410

380

420 430

390 400

320 330 340

BASE STRUCTURE ASSEMBLY FIGURE 05 / GRAPHIC 25-26-80-991-006-A01

25-26-80

PAGE 10005-0 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

5 -001A

FFCL1-1B1304-03

1 STRUCTURE, BASE ASSY (NP) SEE 252680-03, 300A FOR NHA

RF

-001B

FFCL1-1B1304-04

1 STRUCTURE, BASE ASSY (NP) SEE 252680-03, 300B FOR NHA

RF

010A

FFCL1-1B1335-20

2 LEVER, CABLE

1

020A

NAS623-3-6

ATTACHING PARTS 2 SCREW, TRUSS HEAD

1

030A

AN960PD10

2 DELETED, SUPSD BY ITEM 030B

1

030B

NAS1149D0363H

2 WASHER SUPSDS ITEM 030A XXX

1

040A

FFCL1-1B1330-01

2 CROSSBEAM, UPPER

(NP)

1

050A

NSA5319-12-50

ATTACHING PARTS 2 PIN, SPRING XXX

(NPV F5442)

2

060A

FFCL1-1B1333-20

3 STOP, SEAT BACK

(NP)

2

070A

NSA5319-12-50

ATTACHING PARTS 3 PIN, SPRING XXX

(NPV F5442)

1

080A

FFCL1-1B1331-20

3 TUBE

(NP)

1

090A

FFCL1-1B1350-03

2 FITTING, RH EQUIPPED

(NP)

1

100A

FFMU1-1B1307-01

3 FASTENER, BELT

1

110A

AN174-4A

ATTACHING PARTS 3 SCREW, HEX. HEAD

1

120A

FFCL1-1B1311-20

3 BUSH (NP) BONDED WITH LOCTITE 241 MADE BY F7121

1

130A

AN960-416L

3 WASHER XXX

(NP)

1

140A

KRV26X

3 ROLLER

(NPV F0563)

3

150A

FFCL1-1B1610-20

160A

FFCL1-1B1620-20

ATTACHING PARTS 3 SUPPORT, ROLLER (NP) BONDED WITH LOCTITE 241 MADE BY F7121 3 SPACER XXX

(NP)

1

1

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10005-1 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

5 170A

FFCL1-1B1332-01

3 BUSH

(NP)

1

180A

NAS1801-3-9

ATTACHING PARTS 3 SCREW, HEX. HEAD

(NP)

3

190A

23111AG050LE

3 WASHER XXX

(NP)

3

200A

FFCL1-1B1313-20

3 STOP

(NP)

1

210A

NAS1801-3-9

ATTACHING PARTS 3 SCREW, HEX. HEAD

(NP)

2

220A

23111AG050LE

3 WASHER XXX

(NP)

2

230A

FFCL1-1B1661-20

3 STOP, CABLE WRAPPING

1

240A

NAS602-7P

ATTACHING PARTS 3 SCREW, TRUSS HEAD

2

250A

AN960-8

3 WASHER XXX

260A

FFCL1-1B1360-03

3 FITTING

(NP)

1

270A

FFCL1-1B1350-04

2 FITTING, LH EQUIPPED

(NP)

1

280A

FFMU1-1B1307-01

3 FASTENER, BELT

1

290A

AN174-4A

ATTACHING PARTS 3 SCREW, HEX. HEAD

1

300A

FFCL1-1B1311-20

3 BUSH (NP) BONDED WITH LOCTITE 241 MADE BY F7121

1

310A

AN960-416L

3 WASHER XXX

1

320A

KRV26X

3 ROLLER

330A

FFCL1-1B1610-20

340A

FFCL1-1B1620-20

3 SPACER XXX

350A

FFCL1-1B1332-01

3 BUSH

(NP)

1

360A

NAS1801-3-9

ATTACHING PARTS 3 SCREW, HEX. HEAD

(NP)

3

2

(V F0563)

ATTACHING PARTS 3 SUPPORT, ROLLER BONDED WITH LOCTITE 241 MADE BY F7121

3 1

1

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10005-2 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

5 370A

23111AG050LE

3 WASHER XXX

(NP)

3

380A

FFCL1-1B1313-20

3 STOP

(NP)

1

390A

NAS1801-3-9

ATTACHING PARTS 3 SCREW, HEX. HEAD

(NP)

2

400A

23111AG050LE

3 WASHER XXX

(NP)

2

410A

FFCL1-1B1661-20

3 STOP, CABLE WRAPPING

1

420A

NAS602-7P

ATTACHING PARTS 3 SCREW, TRUSS HEAD

2

430A

AN960-8

3 WASHER XXX

440A

FFCL1-1B1360-04

3 FITTING

450A

FFCL1-1B1671-20

2 STOP, CABLE WRAPPING

1

460A

NAS602-10P

ATTACHING PARTS 2 SCREW, TRUSS HEAD

2

470A

AN960-8

2 DELETED, SUPSD BY ITEM 470B

2

470B

NAS1149DN832J

2 WASHER SUPSDS ITEM 470A XXX

2

480A

FFCL1-1B1681-20

2 SUPPORT, CABLE WRAPPING

1

490A

NAS1801-08-8

ATTACHING PARTS 2 SCREW, HEX. HEAD

1

500A

AN960-8L

2 DELETED, SUPSD BY ITEM 500B

1

500B

NAS1149DN816J

2 WASHER SUPSDS ITEM 500A XXX

2

510A

TA1390

2 SPRING

520A

FFCL1-1B1340-01

2 SUPPORT, SEAL RIVETED WITH TLPD440BS MADE BY K0017

530A

SB1-015-001-04

3 SEAL BONDED WITH RTV108 MADE BY FB328

2 (NP)

(V F1142) (NP)

1

1 1

AR

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10005-3 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE 160

170 180

260 470 540 550 560 570

100 310 110 120 320 330

510 520 530 10 20 30 50

270 480

60 70

280 290 490 500

220 230 240

190

300 460

200 210 90 250

A 130 140 150

40 80 590 370 380 390

580

VIEW A

400 410 420

430 440 450 340 350 360 600 610

BASE STRUCTURE ASSEMBLY FIGURE 05A / GRAPHIC 25-26-80-991-060-A01

25-26-80

PAGE 10005A-0 APR15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

5A -001A

FFCL1-5B1300-01

1 STRUCTURE, BASE ASSY (NP) SEE 252680-03, 300C FOR NHA

1

-001B

FFCL1-5B1300-02

1 STRUCTURE, BASE ASSY (NP) SEE 252680-03, 300D FOR NHA

1

010A

FFCL1-1B1335-20

2 LEVER, CABLE

1A

1

010B

FFCL1-1B1335-21

2 LEVER, CABLE

1B

1

020A

NAS623-3-6

ATTACHING PARTS 2 SCREW, TRUSS HEAD

030A

AN960PD10

2 WASHER XXX

040A

FFCL1-1B1330-01

2 CROSSBEAM, UPPER

(NP)

1

050A

NSA5319-12-50

ATTACHING PARTS 2 PIN, SPRING XXX

(NPV F5442)

2

060A

FFCL1-1B1333-20

3 STOP, SEAT BACK

(NP)

2

070A

NSA5319-12-50

ATTACHING PARTS 3 PIN, SPRING XXX

(NPV F5442)

1

080A

FFCL1-1B1331-20

3 TUBE

(NP)

1

090A

FFCL1-1B1350-01

2 FITTING, RH EQUIPPED

(NP)

1

100A

FFCL1-5B1352-01

3 FASTENER, BELT

1

110A

AN4-16A

ATTACHING PARTS 3 SCREW, HEX. HEAD

1

120A

NAS1149C0432R

3 WASHER XXX

(NP)

1

130A

KRV26X

3 ROLLER

(NPV F0563)

3

140A

FFCL1-1B1610-20

150A

FFCL1-1B1620-20

3 SPACER XXX

(NP)

1

160A

FFCL1-1B1332-01

3 BUSH

(NP)

1

170A

NAS1801-3-9

ATTACHING PARTS 3 SCREW, HEX. HEAD

(NP)

3

1 1

ATTACHING PARTS 3 SUPPORT, ROLLER (NP) BONDED WITH LOCTITE 241 MADE BY F7121

1

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10005A-1 APR15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

5A 180A

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

23111AG050LE

3 WASHER XXX

(NP)

3

190A

FFCL1-1B1313-20

3 STOP

(NP)

1

200A

NAS1801-3-9

ATTACHING PARTS 3 SCREW, HEX. HEAD

(NP)

2

210A

23111AG050LE

3 WASHER XXX

(NP)

2

220A

FFCL1-1B1661-20

3 STOP, CABLE WRAPPING

1

230A

NAS602-7P

ATTACHING PARTS 3 SCREW, TRUSS HEAD

2

240A

AN960-8

3 WASHER XXX

250A

FFCL1-5B1312-01

3 FITTING

260A

FFCL1-5B1353-01

3 SHEET, BELT FITTING

1

270A

FFCL1-5B1351-01

3 FITTING, BELT

1

280A

NAS1801-4-11

ATTACHING PARTS 3 SCREW, HEX. HEAD

2

290A

NAS1149C0432R

3 WASHER XXX

300A

FFCL1-5B1350-02

2 FITTING, LH EQUIPPED

310A

FFCL1-5B1352-01

3 FASTENER, BELT

1

320A

AN4-16A

ATTACHING PARTS 3 SCREW, HEX. HEAD

1

330A

AN960-416L

3 WASHER XXX

340A

KRV26X

3 ROLLER

350A

FFCL1-1B1610-20

360A

FFCL1-1B1620-20

3 SPACER XXX

370A

FFCL1-1B1332-01

3 BUSH

(NP)

1

380A

NAS1801-3-9

ATTACHING PARTS 3 SCREW, HEX. HEAD

(NP)

3

2 (NP)

1

2 (NP)

1

1 (V F0563)

ATTACHING PARTS 3 SUPPORT, ROLLER BONDED WITH LOCTITE 241 MADE BY F7121

3 1

1

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10005A-2 APR15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

5A 390A

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

23111AG050LE

3 WASHER XXX

(NP)

3

400A

FFCL1-1B1313-20

3 STOP

(NP)

1

410A

NAS1801-3-9

ATTACHING PARTS 3 SCREW, HEX. HEAD

(NP)

2

420A

23111AG050LE

3 WASHER XXX

(NP)

2

430A

FFCL1-1B1661-20

3 STOP, CABLE WRAPPING

1

440A

NAS602-7P

ATTACHING PARTS 3 SCREW, TRUSS HEAD

2

450A

AN960-8

3 WASHER XXX

460A

FFCL1-5B1312-02

3 FITTING

470A

FFCL1-5B1353-01

3 SHEET, BELT FITTING

1

480A

FFCL1-5B1351-01

3 FITTING, BELT

1

490A

NAS1801-4-11

ATTACHING PARTS 3 SCREW, HEX. HEAD

2

500A

NAS1149C0432R

3 WASHER XXX

510A

FFCL1-1B1670-20

2 STOP, CABLE WRAPPING

1A

1

510B

FFCL1-1B1671-20

2 STOP, CABLE WRAPPING

1B

1

520A

NAS602-10P

ATTACHING PARTS 2 SCREW, TRUSS HEAD

530A

AN960-8

2 WASHER XXX

540A

FFCL1-1B1681-20

2 SUPPORT, CABLE WRAPPING

1A

1

540B

FFCL1-1B1681-21

2 SUPPORT, CABLE WRAPPING

1B

1

550A

NAS1801-08-8

ATTACHING PARTS 2 SCREW, HEX. HEAD

560A

AN960-8L

2 WASHER XXX

570A

TA1390

2 SPRING

580A

FFCL1-1B1340-01

2 SUPPORT, SEAL RIVETED WITH TLPD440BS MADE BY K0017

2 (NP)

1

2

2 2

1 1 (V F1142) (NP)

1 1A

1

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10005A-3 APR15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

5A 580B

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

(NP)

1B

UNITS PER ASSY

FFCL1-1B1340-02

2 SUPPORT, SEAL RIVETED WITH TLPD440BS MADE BY K0017

1

590A

SB1-015-001-02

3 SEAL BONDED WITH RTV108 MADE BY FB328

600A

NAS1801-3-7

2 SCREW, HEX. HEAD

4

610A

L23111-50AGL

2 WASHER

4

AR

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10005A-4 APR15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

PAGE INTENTIONALLY LEFT BLANK

25-26-80

PAGE 10005A-5 APR15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01

140 190

130

200

140 190

30

140 190

200

130

130

130 200

130 180 190

140 190

FWD

10

50

210

30

130 210

90 100

110

150 130 190

80 200

160 190

20 40

20 40

130

80

120

60 70

200

120

60 70

210

170 190

ECU SUPPORT ASSY FIGURE 06 / GRAPHIC 25-26-80-991-007-A01

25-26-80

PAGE 10006-0 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

6 -001A

FFCL1-3B1334-01

1 SUPPORT, ECU ASSY (NP) SEE 252680-03, 400A FOR NHA

RF

-001B

FFCL1-3B1338-01

1 SUPPORT, ECU ASSY (NP) SEE 252680-03, 400B FOR NHA

RF

010A

FFCL1-3B1335-01

2 SUPPORT, ECU

1

020A

NAS1801-3-8

ATTACHING PARTS 2 SCREW, HEX. HEAD

3

030A

NAS514P632-6

2 SCREW, CSK HEAD

3

040A

NAS1149F0332P

2 WASHER XXX

3

050A

FFCL1-3B1336-01

2 CROSSBEAM, ECU

(NP)

1

060A

NAS1801-3-8

ATTACHING PARTS 2 SCREW, HEX. HEAD

(NP)

3

070A

NAS1149F0332P

2 WASHER XXX

(NP)

3

080A

FFCL1-1B1327-20

2 SUPPORT, CONNECTOR

(NP)

1

090A

NAS600-13

ATTACHING PARTS 2 SCREW, TRUSS HEAD

(NP)

2

100A

NAS1149FN432P

2 WASHER

(NP)

2

110A

NSA5527-03-16

2 SPACER XXX

(NPV F5442)

2

120A

NSA5516-04ND

2 CLAMP

(NPV F5442)

4

130A

NSA935504-01

2 SUPPORT, WIRING

(NPV F5442)

8

140A

NAS1801-3-17

2 SCREW, HEX. HEAD

(NP)

5

150A

NAS1801-3-8

2 SCREW, HEX. HEAD

(NP)

1

160A

NAS1801-3-22

2 SCREW

(NP)

2

170A

NAS1801-3-30

2 SCREW, HEX. HEAD

(NP)

1A

1

170B

NAS1801-3-24

2 SCREW, HEX. HEAD

(NP)

1B

1

180A

NAS1801-3-10

2 SCREW

(NP)

1

190A

NAS1149F0332P

2 WASHER

(NP)

10

200A

NSA5527-03-16

2 SPACER

(V F5442)

6

210A

NSA5527-03-08

2 SPACER

(V F5442)

3

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10006-1 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE VALID FOR FFCL1-2E1102-01

140 150

300 310 320

160 170 180 130

220 230 240

250 260 270 280 10 20

A 250 260 270 280

190 200 210 390 400

30 40 50

330 340 410 420 430 440

350

360 370 380

VALID FOR FFCL1-5E1100-01

120

VIEW A

60 80 70

90 100 110

70 60

250 280 290

480

570 510

540

550 560

520 530

490 500

460 450 470

SEAT BACK ASSEMBLY FIGURE 07 / GRAPHIC 25-26-80-991-008-A01

25-26-80

PAGE 10007-0 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

7 -001A

FFCL1-2E1102-01

1 SEAT BACK, ASSY SEE 252680-01, 070A FOR NHA

RF

-001B

FFCL1-5E1100-01

1 SEAT BACK, ASSY SEE 252680-01A, 070A FOR NHA

RF

010A

FFCL1-2E1196-01

2 STRUCTURE, MOBILE EQUIPPED

1

020A

NAS514P832-8

ATTACHING PARTS 2 SCREW, CSK HEAD XXX

2

030A

FFCL1-1E1153-20

3 TRACK, ROLLER

(NP)

2

040A

NAS602-10P

ATTACHING PARTS 3 SCREW, TRUSS HEAD

(NP)

6

050A

NAS1149FN816P

3 WASHER XXX

(NP)

6

060A

FFCL1-1E1156-20

3 STOP

(NP)

2

070A

NAS514P1032-22

ATTACHING PARTS 3 SCREW, CSK HEAD XXX

(NP)

2

080A

NSA935504-01

3 SUPPORT, WIRING

(NPV F5442)

1

090A

NAS1801-3-13

ATTACHING PARTS 3 SCREW, HEX. HEAD

(NP)

1

100A

NAS1149F0332P

3 WASHER

(NP)

1

110A

NSA5527-03-05

3 SPACER XXX

(NPV F5442)

1

120A

FFCL1-2E1197-01

3 STRUCTURE, MOBILE

(NP)

1

130A

FFCL1-2E1202-01

2 STRUCTURE, STATIC EQUIPPED

(NP)

1A

1

130B

FFCL1-5E1202-01

2 STRUCTURE, STATIC EQUIPPED

(NP)

1B

1

140A

FFCL1-1E1137-20

3 HINGE

1

150A

NAS514P832-8

ATTACHING PARTS 3 SCREW, CSK HEAD XXX

2

160A

FFCL1-2E1135-01

3 PANEL, STATIC UPPER

130A

1

160B

FFCL1-5E1145-01

3 PANEL, STATIC LOWER

130B

1

170A

NAS514P1032-28

ATTACHING PARTS 3 SCREW, CSK HEAD

130A

4

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10007-1 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

7 170B

NAS1801-3-28

3 SCREW, HEX. HEAD

130B

4

175A

NAS1149F0332P

3 WASHER

130B

4

180A

FFCL1-1E1144-20

3 SPACER XXX

190A

FFCL1-1E1147-01

3 PANEL, STATIC LOWER

130A

1

190B

FFCL1-5E1157-01

3 PANEL, STATIC LOWER

130B

1

200A

NAS1801-3-6

ATTACHING PARTS 3 SCREW, HEX. HEAD

210A

NAS1149F0332P

3 WASHER XXX

6

220A

FFCL1-2B0523-31

3 SUPPORT, CONNECTOR

1

230A

NAS1801-3-5

ATTACHING PARTS 3 SCREW, HEX. HEAD

2

240A

NAS1149F0332P

250A

NSA935504-01

3 SUPPORT, WIRING

260A

NAS1801-3-14

ATTACHING PARTS 3 SCREW, HEX. HEAD

270A

NSA5527-03-16

3 SPACER

(V F5442)

3

280A

NAS1149F0332P

3 WASHER

(NP)

5

290A

NAS1801-3-6

3 SCREW, HEX. HEAD XXX

300A

FFCL1-1E1136-01

3 PANEL, STATIC UPPER

130A

1

300B

FFCL1-5E1146-01

3 PANEL, STATIC UPPER

130B

1

310A

NAS1801-3-6

ATTACHING PARTS 3 SCREW, HEX. HEAD

320A

NAS1149F0332P

3 WASHER XXX

330A

FFMU1-1E1128-01

3 FITTING, LH EQUIPPED

(NP)

1

340A

FFMU1-1E1129-01

4 FITTING

(NP)

1

350A

NATR6

4 ROLLER

(V F0563)

1

360A

22719BC060024L

ATTACHING PARTS 4 PIN, SHOULDERED

4

6

WASHER XXX

2 (V F5442)

5 3

2

8 8

1

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10007-2 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

7 370A

MS24665-281

4 PIN, COTTER

1

380A

AN960-416L

4 WASHER XXX

1

390A

FFMU1-1E1128-02

3 FITTING, RH EQUIPPED

(NP)

1

400A

FFMU1-1E1129-02

4 FITTING

(NP)

1

410A

NATR6

4 ROLLER

(NPV F0563)

1

420A

22719BC060024L

ATTACHING PARTS 4 PIN, SHOULDERED

(NP)

1

430A

MS24665-281

4 PIN, COTTER

(NP)

1

440A

AN960-416L

4 WASHER XXX

(NP)

1

450A

FFCL1-5E1000-31

3 SUPPORT, RELAXOR

130B

1

460A

NAS1801-3-5

ATTACHING PARTS 3 SCREW, HEX. HEAD

130B

2

470A

NAS1149F0332P

3 WASHER XXX

130B

2

480A

FFCL1-5E1010-01

3 SUPPORT, RELAXOR CABLE

130B

1

490A

NAS1801-08-5

ATTACHING PARTS 3 SCREW, HEX. HEAD

130B

2

500A

NAS1149FN832P

3 WASHER XXX

130B

2

510A

NSA935504-01

4 SUPPORT, CABLE

520A

NAS1801-3-10

ATTACHING PARTS 4 SCREW, HEX. HEAD

530A

NAS1149F0332P

4 WASHER XXX

540A

NSA935504-01

4 SUPPORT, CABLE

550A

NAS1801-3-14

ATTACHING PARTS 4 SCREW, HEX. HEAD

1

560A

NAS1149F0332P

4 WASHER

1

570A

NSA5527-03-05

4 SPACER XXX

(V F5442)

1 1 1

(V F5442)

(V F5442)

1

1

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10007-3 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01

130

TAKE CARE LATERAL FURNITURE DURING MAINTENANCE

130

80 120

60

30 40 50

70

90 100 110 20

90 100 110

10

30 40 50

SEAT BOTTOM ASSEMBLY FIGURE 08 / GRAPHIC 25-26-80-991-009-A01

25-26-80

PAGE 10008-0 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

8 -001A

FFCL1-1C0002-01

1 SEAT BOTTOM, ASSY SEE 252680-01, 080A FOR NHA SEE 252680-01A, 080A FOR NHA

010A

FFCL1-1C0024-20

2 WASHER

(NP)

2

020A

FFCL1-1C0028-20

2 WASHER

(NP)

2

030A

MS24665-285

2 PIN, COTTER

2

040A

23111AG100LE

2 WASHER

4

050A

22719BC100039L

2 PIN, SHOULDERED

2

060A

FFCL1-1C0032-01

2 FITTING, RH

(NP)

1

070A

FFCL1-1C0032-02

2 FITTING, LH

(NP)

1

080A

FFCL1-1C0030-01

2 PANEL, SEAT BOTTOM ASSY

(NP)

1

090A

FFCL1-1C0022-01

3 YOKE

2

100A

NAS623-3-3

ATTACHING PARTS 3 SCREW, TRUSS HEAD

6

110A

NAS1149F0332P

3 WASHER XXX

120A

FFCL1-1C0031-01

3 PANEL

130A

FFCL1-2M1300-20

3 LABEL

RF

6 (NP)

1 1

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10008-1 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01

410 420

10 20 30 40

490 500 520

510

130

180

190 200 220

170 50 430 440 450

360 360

240 250 260

290 280

230

130

300

ARMREST ASSEMBLY (SHEET 1 OF 2) FIGURE 09 / GRAPHIC 25-26-80-991-010-A01

25-26-80

PAGE 10009-0 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01

530

390

460 470 480

150 160

320 140 150 110 120

80 100

370 380

100

310

70

90

60 400

540

330 270 340 350

ARMREST ASSEMBLY (SHEET 2 OF 2) FIGURE 09 / GRAPHIC 25-26-80-991-011-A01

25-26-80

PAGE 10009-1 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

9 -001A

FFCL1-1F1010-01

1 ARMREST, ASSY SEE 252680-01, 150A FOR NHA

RF

-001B

FFCL1-1F1010-02

1 ARMREST, ASSY SEE 252680-01, 150B FOR NHA

RF

010A

FFCL1-1F1351-20

2 BUTTON

1A

1

010B

FFCL1-1F1351-21

2 BUTTON

1B

1

020A

NAS1801-08-13

ATTACHING PARTS 2 SCREW, HEX. HEAD

2

030A

AN960-8

2 WASHER

2

040A

NAS679A08

2 NUT, SELF-LOCKING XXX

2

050A

FFCL1-1F1241-20

2 SPACER BONDED WITH LOCTITE 221 MADE BY F7121

5

060A

250-75N588539

2 CYLINDER, GAS

1

070A

MS24665-210

ATTACHING PARTS 2 PIN, COTTER

2

080A

AN960PD516L

2 WASHER

2

090A

22719BC080031L

2 PIN, SHOULDERED

2

100A

FFCL1-1F1245-20

2 SPACER XXX

4

110A

LFS20331-9-9-5V

2 TRACK LFS20331-9-9-5V IS RF CODE FOR LFS20/331-9/9.5VA

120A

NAS1352-08-10P

ATTACHING PARTS 2 SCREW, SOCKET HEAD XXX

130A

LFR50-5KDD4

2 ROLLER

140A

FFCL1-1F1253-20

150A

(V F8433)

(V F0563)

2

8 (V F0563)

6

2 STOP

(NP)

2

FFCL1-1F1254-31

2 STOP

(NP)

2

160A

NAS514P832-14

ATTACHING PARTS 2 SCREW, CSK HEAD XXX

(NP)

4

170A

FFCL1-1F1217-01

2 STRUCTURE

(NP)

1A

1

170B

FFCL1-1F1217-02

2 STRUCTURE

(NP)

1B

1

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10009-2 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

9 180A

FFMU1-1F1270-01

2 CONTROL, ASSY

1A

1

180B

FFMU1-1F1270-02

2 CONTROL, ASSY

1B

1

190A

MS24665-210

ATTACHING PARTS 2 PIN, COTTER

1

200A

AN960PD516L

2 WASHER

1

-210A

22719BC080031L

2 PIN, SHOULDERED

1

220A

FFCL1-1F1234-20

2 SPACER

(NP)

3

230A

FFCL1-1F1231-20

3 SUPPORT, LOCK

(NP)

1

240A

NAS514P832-14

2 SCREW, CSK HEAD

4

250A

AN960-8L

2 WASHER

4

260A

NAS679A08

2 NUT, SELF-LOCKING XXX

4

270A

FFCL1-1F1272-20

3 LEVER

(NP)

170A

1

270B

FFCL1-1F1272-21

3 LEVER

(NP)

170B

1

280A

FFCL1-1F1232-20

3 PIN

(NP)

290A

NAS1801-08-6

ATTACHING PARTS 3 SCREW, HEX. HEAD XXX

300A

CA1720

3 SPRING

310A

SB3-011-107-01

3 CABLE, CONTROL

320A

FFCL1-1F1248-20

2 SHIM BONDED WITH EMFI30055A MADE BY F6599

330A

H2P

2 CLAMP

340A

NAS514P832-8

ATTACHING PARTS 2 SCREW, CSK HEAD

350A

NAS679A06

2 NUT, SELF-LOCKING XXX

360A

FFCL1-1F1315-20

2 SPACER BONDED WITH EMFI30055A MADE BY F6599

370A

FFCL1-1F1271-20

2 SPACER

1 1

(V F1142)

1 1

(NP)

1

(V F3341)

1 1 1

(NP)

2

1

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10009-3 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

9 380A

NAS602-6P

ATTACHING PARTS 2 SCREW, TRUSS HEAD XXX

390A

FFCL1-1F1250-01

2 STRUCTURE, MOBILE

(NP)

1A

1

390B

FFCL1-1F1250-02

2 STRUCTURE, MOBILE

(NP)

1B

1

400A

G51NA

2 GROMMET

410A

FFCL1-2F1345-03

2 SHROUD, OUTER

1A

1

410B

FFCL1-2F1345-04

2 SHROUD, OUTER

1B

1

420A

NAS514P1032-8

430A

FFCL1-2F1315-03

2 SHROUD, LOWER

1A

1

430B

FFCL1-2F1315-04

2 SHROUD, LOWER

1B

1

440A

NAS514P1032-8

ATTACHING PARTS 2 SCREW, CSK HEAD

450A

AN525-10-18

2 SCREW, TRUSS HEAD XXX

460A

FFCL1-2F1545-03

2 SHROUD, INNER

1A

1

460B

FFCL1-2F1545-04

2 SHROUD, INNER

1B

1

470A

NAS514P1032-8

480A

NSA5066-3-1

2 NUT XXX

490A

FFCL1-2F1505-03

2 ARMCAP, LEATHER ARMREST

1A

1

490B

FFCL1-2F1505-04

2 ARMCAP, LEATHER ARMREST

1B

1

500A

NAS514P832-10

ATTACHING PARTS 2 SCREW, CSK HEAD XXX

510A

FFCL1-2F1354-03

1

(V F3341)

AR

ATTACHING PARTS 2 SCREW, CSK HEAD BONDED WITH LOCTITE 221 MADE BY F7121 XXX

1

2 2

ATTACHING PARTS 2 SCREW, CSK HEAD BONDED WITH LOCTITE 221 MADE BY F7121

2

(V F5442)

2 SHROUD, CONTROL BUTTON BONDED WITH EMFI30055A MADE BY F6599

2

1 1

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10009-4 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

9 520A

FFCL1-1F1249-20

2 SHIM BONDED WITH EMFI30055A MADE BY F6599

(NP)

1

530A

FFCL1-2F1364-01

2 CAP, ARMREST SCREW

1

540A

FFCL1-1F1218-20

2 STOP

1

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10009-5 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01

40 50

60 70

190 200 210

80 90

150

130 140 10

290 310 190 200 210

170

160 110 100 120 380 390 370

180 220

230 240 250

300 350 360

330

280 320

340

20 30 10

260

270

LEGREST CABLE ASSEMBLY FIGURE 10 / GRAPHIC 25-26-80-991-012-A01

25-26-80

PAGE 10010-0 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

10 -001A

FFCL1-2D1006-01

1 LEGREST, ASSY SEE 252680-01, 190A FOR NHA SEE 252680-01A, 150A FOR NHA

010A

FFCL1-2D1300-01

2 MECHANISM, LEGREST EQUIPPED

020A

NAS1801-3-10

030A

AN960-10L

2 WASHER XXX

040A

FFCL1-1D1329-20

3 STOP

(NP)

2

050A

NAS1352-04-4

ATTACHING PARTS 3 SCREW, HEX. SOCKET HEAD XXX

(NP)

2

060A

FFCL1-1D1328-20

3 RACK

(NP)

1

070A

FFCL1-1D1345-20

3 PIN

(NP)

1

080A

NSA5319-07-25

ATTACHING PARTS 3 PIN, SPRING

(NPV F5442)

3

090A

NSA5319-04-25

3 PIN, SPRING XXX

(NPV F5442)

3

100A

FFCL1-1D1327-20

3 GEAR

(NP)

1

110A

FFCL1-1D1323-01

3 BEARING, EQUIPPED

(NP)

1

120A

FFCL1-1D1338-20

4 GUIDE, RACK

1

130A

FFCL1-1D1325-20

4 BUSH BONDED WITH LOCTITE 638 MADE BY F7121

2

140A

AN565A832H6

4 SCREW, HEADLESS

2

150A

FFCL1-1D1346-20

3 BEARING (NP) BONDED WITH LOCTITE 638 MADE BY F7121

2

160A

FFCL1-1D1330-20

3 SPACER

(NP)

1

170A

FFCL1-1D1344-20

3 SUPPORT

(NP)

1

180A

FFCL1-2D1350-20

3 SPACER

(NP)

1

190A

FFCL1-1D1347-01

3 SPACER

(NP)

2

RF

1

ATTACHING PARTS 2 SCREW, HEX. HEAD

4 4

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10010-1 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

10 ATTACHING PARTS 3 SCREW, HEX. HEAD

200A

AN175-5A

210A

NAS1149F0532P

3 WASHER XXX

220A

FFCL1-2D1402-03

2 LEGREST, ASSY

(NP)

1

230A

FFCL1-1D1051-20

3 PIN, SHOULDERED

(NP)

1

240B

L23111-60AGL

3 WASHER

(NP)

1

250A

MS24665-210

3 PIN, COTTER

(NP)

1

260A

FFCL1-2D1050-01

3 ANGLE

1

270A

NAS1102-3-6

3 SCREW, CSK HEAD

2

280A

FFCL1-2D1204-03

3 LEGREST, EQUIPPED

290A

FFCL1-1D1225-20

4 PIN, ARTICULATION

2

300A

FFCL1-1D1226-20

4 SPACER

2

310A

AN960-816L

4 WASHER

2

320A

FFCL1-1D1234-01

4 PANEL

1

330A

FFCL1-2D1231-03

4 FITTING, LH

1

340A

FFCL1-2D1231-04

4 FITTING, RH

1

350A

NAS1801-3-7

4 SCREW, HEX. HEAD

10

360A

AN960-10L

4 WASHER

10

370A

FFCL1-1D1224-20

4 YOKE

1

380A

NAS602-7

ATTACHING PARTS 4 SCREW, TRUSS HEAD

4

390A

AN960-8

4 WASHER XXX

(NP)

1 1

(NP)

1

4

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10010-2 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01

PAGE INTENTIONALLY LEFT BLANK

25-26-80

PAGE 10010-3 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01

80 120

70 80 120

70 80 120

80 110

70 80

10

100 120 140

90 120 90 120

MECHANICAL CABLE ASSEMBLY (SHEET 1 OF 2) FIGURE 11 / GRAPHIC 25-26-80-991-013-A01

25-26-80

PAGE 10011-0 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01

80 80

90 120 20 130

40

30

R

50

L

60

MECHANICAL CABLE ASSEMBLY (SHEET 2 OF 2) FIGURE 11 / GRAPHIC 25-26-80-991-014-A01

25-26-80

PAGE 10011-1 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

11 -001A

FFCL1-1G1014-01

1 CABLE, LH MECHANICAL ASSY (NP) SEE 252680-01, 220A FOR NHA SEE 252680-01A, 180A FOR NHA

RF

-001B

FFCL1-1G1014-02

1 CABLE, RH MECHANICAL ASSY (NP) SEE 252680-01, 220B FOR NHA SEE 252680-01A, 180B FOR NHA

RF

010A

SB3-011-108-01

2 CABLE, ELECTROMAGNET CONTROL

1

020A

SB3-011-108-02

2 CABLE, ELECTROMAGNET CONTROL

1

030A

ET5-010-002-01

2 LABEL, SEAT BACK CONTROL

1

040A

ET5-010-003-01

2 LABEL, CONTROL

1

050A

MVS012

2 CONTROL, OVERRIDE SYSTEM

(V F0217)

060A

NSA935401-04

2 CLAMP

(V F5442)

1A

2

060B

NSA935401-04

2 CLAMP

(V F5442)

1B

4

070A

NSA5456-3-4

2 SUPPORT, CLAMP (V F5442) RIVETED WITH TLPD429BS MADE BY K0017

1A

4

070B

NSA5456-3-4

2 SUPPORT, CLAMP (V F5442) RIVETED WITH TLPD429BS MADE BY K0017

1B

3

080A

NSA5516-04ND

2 CLAMP

(V F5442)

1A

10

080B

NSA5516-04ND

2 CLAMP

(V F5442)

1B

8

090A

NAS1801-08-8

2 SCREW, HEX. HEAD

100A

NAS1801-3-14

2 SCREW, HEX. HEAD

1A

1

110B

NAS1801-08-8

2 SCREW, HEX. HEAD

1B

1

120A

NAS1149FN816P

2 WASHER

7

120B

NAS1149FN816P

2 WASHER

6

130A

D3Q1CC040020APA

2 SCREW, HEX. SOCKET HEAD

2

140A

NSA5527-03-06

2 SPACER

1

5

(V F5442)

1A

1

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10011-2 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01

PAGE INTENTIONALLY LEFT BLANK

25-26-80

PAGE 10011-3 FEV 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

130 140

144 145 146

120

220

350 410 430

270

ELECTRICAL CABLE ASSEMBLY (SHEET 1 OF 2) FIGURE 12 / GRAPHIC 25-26-80-991-015-A01

25-26-80

PAGE 10012-0 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE 310

310

230

310

320 20 30

290 330 390 460 70 80 90 100

10

B

450 150 340 420 440

A

290 330 390 460

40 50 60

VIEW A

280 450

240

VIEW B

330 400 430

500 510 520

490 510 520

480

160

300

250

180 190 200 210

ELECTRICAL CABLE ASSEMBLY (SHEET 2 OF 2) FIGURE 12 / GRAPHIC 25-26-80-991-016-A01

25-26-80

PAGE 10012-1 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

12 -001A

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

FFCL1-4G1001-01

1 CABLE, ELECTRICAL ASSY SEE 252680-01, 230A FOR NHA

010A

E65EAR5-640A

2 UNIT, (V F0358) ELECTRICAL CONTROL SEE CMM 25-29-92 FOR DET J100, J1, J2

020A

AN174-4A

030A

NAS1149F0432P

2 WASHER XXX

4

040A

RSA013

2 ACTUATOR (V F0358) SEE CMM 25-29-20 FOR DET P11

1

050A

AN175-7A

2 SCREW, HEX. HEAD

2

060A

NAS1149F0532P

2 WASHER

2

070A

RSA012

2 ACTUATOR (V F0358) SEE CMM 25-29-20 FOR DET P10

1

080A

AN175-14A

ATTACHING PARTS 2 SCREW, HEX. HEAD

2

090A

FFCL1-1B1222-20

2 SPACER

2

100A

NAS1149F0532P

2 WASHER

4

MS21042-5

2 NUT, SELF-LOCKING XXX

2

120A

LSA011

2 DELETED, SUPSD BY ITEM 120B

1

120B

FFCL1-1E1246-01

2 ACTUATOR SUSPDS ITEM 120A MODIFIED P/N FROM LSA011, MADE BY F0358 SEE CMM 25-29-78 FOR DET P12

1

130A

NAS1801-08-6

140A

NAS1149DN816J

2 WASHER XXX

144A

NATR6

3 ROLLER

-110A

RF

ATTACHING PARTS 2 SCREW, HEX. HEAD

1

4

ATTACHING PARTS 2 SCREW, HEX. HEAD

4 4 (V F0563)

2

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10012-2 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

12 ATTACHING PARTS 3 SCREW, TRUSS HEAD

145A

NAS602-8P

146A

NAS1149FN832P

3 WASHER XXX

1

150A

FFCL1-1B1327-20

2 SUPPORT, CONNECTOR

1

160A

P81011A010

2 SWITCH P22

170A

FJPL1-1G1007-20

2 SUPPORT

2

180A

NAS1351-02-6

2 SCREW, HEX. SOCKET HEAD

4

190A

NAS1801-06-4

2 DELETED

4

190B

NAS1801-06-7

2 SCREW, HEX. HEAD

4

200A

NAS1149FN232P

2 DELELED

4

200B

NAS1149FN832P

2 WASHER

4

-210A

NAS1149FN232P

2 DELETED

4

220A

HAR640

2 HARNESS, ACTUATOR (V F0358) P100, P10, P12, P11, P20, P22

1

230A

HAR641

2 HARNESS, LIGHT P200, P21

(V F0358)

1

240A

HAR647

2 HARNESS, POWER P2, P17

(V F0358)

1

250A

HAR644

2 HARNESS, SWITCH P23, P24, J22

(V F0358)

1

SR300A015040I

2 CHAIN, SUPPORT WIRING

1

270A

FFCL1-5B0643-01

2 QUICK, SUPPORT WIRING

1

280A

NAS603-8

2 SCREW, TRUSS HEAD

2

290A

NSA935504-01

2 SUPPORT, WIRING

(V F5442)

3

300A

NSA935504-03

2 SUPPORT, WIRING

(V F5442)

1

310A

NSA935513-05

2 SUPPORT, WIRING

(V F5442)

3

320A

NSA935513-07

2 SUPPORT, WIRING

(V F5442)

1

330A

NSA5527-03-04

2 SPACER

(V F5442)

3

-340A

NSA5527-03-12

2 SPACER

(V F5442)

2

-260A

1

(V FA5Z2)

1

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10012-3 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

12 350A

NSA5527-03-11

2 SPACER

(V F5442)

1

-360A

NSA5527-03-16

2 SPACER

(V F5442)

1

-370A

NAS1801-3-12

2 DELETED, SUPSD BY ITEM 370B

1

-370B

NAS1801-3-8

2 SCREW, HEX. HEAD SUPSDS ITEM 370A

1

-380A

NAS1801-3-9

2 DELETED, SUPSD BY ITEM 380B

1

-380B

NAS1801-3-13

2 SCREW, HEX. HEAD SUPSDS ITEM 380A

1

390A

NAS514P1032-14

2 SCREW, CSK HEAD

2

400A

NAS1801-3-15

2 SCREW, HEX. HEAD

1

410A

NAS1801-3-26

2 SCREW, HEX. HEAD

1

420A

NAS600-19

2 SCREW, TRUSS HEAD

2

430A

NAS1149F0332P

2 WASHER

6

440A

NAS1149FN416P

2 WASHER

4

450A

NAS1149D0332H

2 WASHER

6

460A

MS21042-3

2 NUT, SELF-LOCKING

2

-470A

NAS679A04

2 NUT, SELF-LOCKING

2

480A

M83723-60-214AN

2 PLUG

(V 96906)

1

490A

ABS0639-09

2 PLUG, SUB-D09

(V D8518)

2

500A

ABS0639-50

2 PLUG, SUB-D50

(V D8518)

1

510A

NAS600-6

2 SCREW, TRUSS HEAD

6

520A

NAS1149FN416P

2 WASHER

6

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10012-4 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01

PAGE INTENTIONALLY LEFT BLANK

25-26-80

PAGE 10012-5 FEV 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

130 140

150 160 170 120

310 220 290

ELECTRICAL CABLE ASSEMBLY (SHEET 1 OF 3) FIGURE 12A / GRAPHIC 25-26-80-991-061-A01

25-26-80

PAGE 10012A-0 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE 400

300 520 550 610

A 320

210 430 510 550 590

330

460 560

VIEW A

280 600

VIEW B

380 420 480 580

520 550 610

410 390 420 490 540

220 230 240 250 260 360 340 380 470 530 560 570

ELECTRICAL CABLE ASSEMBLY (SHEET 2 OF 3) FIGURE 12A / GRAPHIC 25-26-80-991-062-A01

25-26-80

PAGE 10012A-1 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

ELECTRICAL CABLE ASSEMBLY (SHEET 3 OF 3) FIGURE 12A / GRAPHIC 25-26-80-991-063-A01

25-26-80

PAGE 10012A-2 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

12A -001A

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

FFCL1-1J5010-01

1 CABLE, ELECTRICAL ASSY (NP) SEE 252680-01A, 230A FOR NHA

RF

010A

E65EAR5-650A

2 UNIT, (V F0358) ELECTRICAL CONTROL SEE CMM 25-29-92 FOR DET J100, J200, J300, J1, J2

1

020A

AN174-4A

030A

NAS1149F0432P

2 WASHER XXX

4

040A

RSA013

2 ACTUATOR (V F0358) SEE CMM 25-29-20 FOR DET P11

1

050A

AN175-7A

060A

NAS1149F0532P

2 WASHER XXX

2

070A

RSA012

2 ACTUATOR (V F0358) SEE CMM 25-29-20 FOR DET P10

1

080A

AN175-14A

ATTACHING PARTS 2 SCREW, HEX. HEAD

2

090A

FFCL1-1B1222-20

2 SPACER

2

100A

NAS1149F0532P

2 WASHER

4

MS21042-5

2 NUT, SELF-LOCKING XXX

2

120A

FFCL1-1E1246-01

2 ACTUATOR MODIFIED P/N FROM LSA011, MADE BY F0358 SEE CMM 25-29-78 FOR DET P12

1

130A

NAS1801-08-6

140A

NAS1149DN816J

2 WASHER XXX

150A

NATR6

3 ROLLER

-110A

ATTACHING PARTS 2 SCREW, HEX. HEAD

4

ATTACHING PARTS 2 SCREW, HEX. HEAD

2

ATTACHING PARTS 2 SCREW, HEX. HEAD

4 4 (V F0563)

2

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10012A-3 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

12A ATTACHING PARTS 3 SCREW, TRUSS HEAD

160A

NAS602-8P

1

170A

NAS1149FN832P

3 WASHER XXX

180A

35016-00

2 BOX, MASSAGE J3, J5, P1, P4

190A

NAS1801-08-8

200A

NAS1149FN832P

2 WASHER XXX

4

210A

FFCL1-1B1327-20

2 SUPPORT, CONNECTOR

1

220A

P81011A010

2 SWITCH J1

230A

FJPL1-1G1007-20

2 SUPPORT

2

240A

NAS1351-02-6

2 SCREW, HEX. SOCKET HEAD

4

250A

NAS1801-06-7

2 SCREW, HEX. HEAD

4

260A

NAS1149FN832P

2 WASHER

12

-270A

NAS1149FN232P

2 WASHER

4

280A

HAR650

2 HARNESS, ACTUATOR (V F0358) B1-1, B1-2, P10, P11, P12 P20, P100

1

290A

HAR659

2 HARNESS, ACTUATOR P5, P300

(V F0358)

1

300A

33084-00

2 HARNESS, SEAT BOTTON (V 3KGA2) J4

1

310A

33083-00

2 HARNESS, SEAT BACK P3

(V 3KGA2)

1

320A

HAR651

2 HARNESS, LIGHT P200, P21

(V F0358)

1

330A

HAR647

2 HARNESS, POWER P2, P17

(V F0358)

1

340A

HAR644

2 HARNESS, SWITCH P23, P24, J22

(V F0358)

1

350A

SR300A015040I

2 CHAIN, SUPPORT WIRING

1

360A

FFCL1-5B0643-01

2 QUICK, SUPPORT WIRING

1

25-26-80

PAGE 10012A-4 APR 15/09

1 (V 3KGA2)

ATTACHING PARTS 2 SCREW, HEX. HEAD

1

4

(V FA5Z2)

1

- ITEM NOT ILLUSTRATED

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

12A 370A

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

NAS603-8

2 SCREW, TRUSS HEAD

2

380A

NSA935504-01

2 SUPPORT, WIRING

(V F5442)

4

390A

NSA935504-03

2 SUPPORT, WIRING

(V F5442)

1

400A

NSA935513-05

2 SUPPORT, WIRING

(V F5442)

3

410A

NSA935513-07

2 SUPPORT, WIRING

(V F5442)

1

420A

NSA5527-03-04

2 SPACER

(V F5442)

3

-430A

NSA5527-03-12

2 SPACER

(V F5442)

2

440A

NSA5527-03-11

2 SPACER

(V F5442)

1

-450A

NSA935401-05

2 CLAMP

(V F5442)

50

-460A

NAS1801-3-9

2 SCREW, HEX. HEAD

1

-470A

NAS1801-3-13

2 SCREW, HEX. HEAD

1

480A

NAS514P1032-14

2 SCREW, CSK HEAD

2

490A

NAS1801-3-15

2 SCREW, HEX. HEAD

1

500A

NAS1801-3-26

2 SCREW, HEX. HEAD

1

510A

NAS600-19

2 SCREW, TRUSS HEAD

2

520A

NAS600-6

2 SCREW, TRUSS HEAD

2

530A

NAS1801-06-5

2 SCREW, HEX. HEAD

1

540A

NAS1149F0332P

2 WASHER

6

550A

NAS1149FN416P

2 WASHER

4

560A

NAS1149D0332H

2 WASHER

6

570A

NAS1149FN632P

2 WASHER

1

580A

MS21042-3

2 NUT, SELF-LOCKING

2

-590A

NAS679A04

2 NUT, SELF-LOCKING

2

600A

M83723-60-214AN

2 PLUG P200

(V 96906)

1

610A

ABS0639-09

2 PLUG, SUB-D09

(V D8518)

2

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10012A-5 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE 110

65

150

70B

Blank button to unlock backrest seat pan depth motion R : button to unlock backrest recline and seat tracking motion

110 140

L : button to unlock legrest motion

VALID FOR 001A AND 001B 160

120 130

ON 70A

80 90 100

OFF VALID FOR 001C AND 001D

20 30

10

40 50 60

COVERING LH ASSEMBLY FIGURE 13 / GRAPHIC 25-26-80-991-017-A01

25-26-80

PAGE 10013-0 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

13 -001A

FFCL1-2H1005-03

1 COVERING, LH ASSY (NP) SEE 252680-01, 240A FOR NHA

RF

-001B

FFCL1-2H1005-04

1 COVERING, RH ASSY (NP) SEE 252680-01, 240B FOR NHA

RF

-001C

FFCL1-5H1005-01

1 COVERING, LH ASSY (NP) SEE 252680-01A, 200A FOR NHA

RF

-001D

FFCL1-5H1005-02

1 COVERING, RH ASSY (NP) SEE 252680-01A, 200B FOR NHA

RF

010A

FFCL1-2B1704-03

2 COVERING, INNER

1A

1

010B

FFCL1-2B1704-04

2 COVERING, INNER

1B

1

010C

FFCL1-5B1711-01

2 COVERING, INNER

1C

1

010D

FFCL1-5B1711-02

2 COVERING, INNER

1D

1

020A

FFCL1-2B1744-03

2 COVERING, REAR

030A

NAS514P832-12

040A

FFCL1-2B1765-03

050A

NAS602-6P

060A

AN960-8L

2 WASHER

1CD

4

060B

NAS1149DN816J

2 WASHER XXX

1AB

4

065A

FFCL1-2B1710-01

2 SUPPORT, LABEL BONDED WITH 30055A MADE BY F6599

1AB

1

070A

ET5-010-005-01

2 LABEL, SWITCH

1CD

1

070B

FFCL1-2M1304-01

2 LABEL

1AB

1

080A

FFCL1-2B1314-03

2 HOOK

1AB

2

1

ATTACHING PARTS 2 SCREW, CSK HEAD BONDED WITH LOCTITE 221 MADE BY F7121 XXX

6

2 COVERING, FRONT RIVETED WITH TLPD639BS MADE BY K0017

1

ATTACHING PARTS 2 SCREW, TRUSS HEAD BONDED WITH LOCTITE 221 MADE BY F7121

4

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10013-1 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

NOMENCLATURE

USAGE FROM TO

UNITS PER ASSY

13 ATTACHING PARTS 2 SCREW, TRUSS HEAD BONDED WITH LOCTITE 221 MADE BY F7121

090A

NAS603-11

1AB

2

100A

AN960PD10L

2 DELETED

2

100B

NAS1149D0316J

2 WASHER XXX

2

110A

FFCL1-2E1134-03

2 COVERING, SEAT BACK

1AB

1

110B

FFCL1-5E1134-01

2 COVERING, SEAT BACK

1CD

1

120A

FFCL1-2E1144-03

2 COVERING, RH SIDE

1

130A

FFCL1-2E1144-04

2 COVERING, LH SIDE

1

140A

NAS514P1032-16

2 SCREW, CSK HEAD

6

150A

ASNA2733-01

2 PLUG BONDED WITH 30055A MADE BY F6599

1AB

2

160A

FFCL1-2B1750-01

2 EDGE RING BONDED WITH AQUABIND MADE BY FA2L9

1AB

AR

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10013-2 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

PAGE INTENTIONALLY LEFT BLANK

25-26-80

PAGE 10013-3 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE VALID FOR 001A 240 130 140 150

50 35

B

20 30

A

210 10 40

VALID FOR 001B

HEADREST ASSEMBLY (SHEET 1 OF 3) FIGURE 14 / GRAPHIC 25-26-80-991-018-A01

25-26-80

PAGE 10014-0 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

Detail A 170

220 230

190 200 190 200

180

160

Detail B

70

90

80

60

100 110 120

HEADREST ASSEMBLY (SHEET 2 OF 3) FIGURE 14 / GRAPHIC 25-26-80-991-019-A01

25-26-80

PAGE 10014-1 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

310 320 300 300

340 360

290 290

260 270 280 250 350 320

HEADREST ASSEMBLY (SHEET 3 OF 3) FIGURE 14 / GRAPHIC 25-26-80-991-064-A01

25-26-80

PAGE 10014-2 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

14 -001A

FFCL1-4E1300-01

1 HEAD REST, ASSY SEE 252680-01, 250A FOR NHA

RF

-001B

FFCL1-4E1319-01

1 HEAD REST, ASSY SEE 252680-01A, 210A FOR NHA

RF

010A

FFCL1-4E1305-01

2 FITTING, HEADREST

020A

NAS1801-3-9

ATTACHING PARTS 2 SCREW, HEX. HEAD

1B

4

020B

NAS1801-3-14

2 SCREW, HEX. HEAD

1A

4

030A

NAS1149F0332P

2 WASHER

035A

NSA5527-03-04

2 SPACER XXX

040A

FFCL1-4E1303-01

3 FITTING

1

050A

NAS1801-08-9

ATTACHING PARTS 3 SCREW, HEX. HEAD

4

060A

MS21042-08

3 NUT, SELF-LOCKING XXX

4

070A

FJEV1-2E1644-31

3 TRACK

1

080A

FJEV1-2E1644-32

3 TRACK

1

090A

FJEV1-2E1642-31

3 SHIM

1

100A

NAS602-14

3 SCREW, TRUSS HEAD

1

110A

AN960-8

3 DELETED

1

110B

NAS1149DN832J

3 WASHER

1

120A

NSA5527-03-06

3 SPACER

-125A

NAS1149FN832P

3 WASHER

4

130A

FJEV1-2E1648-01

2 ANGLE

1

140A

NAS1801-3-9

ATTACHING PARTS 2 SCREW, HEX. HEAD

2

150A

NAS1149F0332P

2 WASHER XXX

2

160A

FFCL1-4E1306-01

2 SUPPORT, MOBILE EQUIPPED

1

170A

FFCL1-4E1302-31

3 BRACKET

1

180A

WJ200QMS38083AA

3 SLIDE

1

4 (V F5442)

(V F5442)

(V C4206)

1A

4

1

4

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10014-3 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

14 ATTACHING PARTS 3 SCREW, HEX. HEAD BONDED WITH LOCTITE 243 MADE BY F7121

190A

NAS1801-08-10

8

200A

NAS1149FN832P

3 WASHER XXX

8

210A

FFCL1-4E1304-31

3 SPRING BLADE

1

220A

NAS514P632-6

ATTACHING PARTS 3 SCREW, CSK HEAD

2

230A

NAS679A06

3 NUT, SELF-LOCKING XXX

240A

FFCL1-4E1301-01

2 PANEL, HEADREST

1A

1

240B

FFCL1-4E1320-01

2 PANEL, HEADREST

1B

1

250A

E6-10-420R50

3 HINGE

1B

2

260A

NAS1801-3-9

ATTACHING PARTS 3 SCREW, HEX. HEAD

1B

4

270A

NAS1149D0332J

3 WASHER

1B

8

280A

MS21043-3

3 NUT, SELF-LOCKING XXX

1B

4

290A

SB5-011-021-01

3 STRAP

1B

2

300A

E6-10-440R50

3 HINGE

1B

2

310A

NAS1801-3-9

ATTACHING PARTS 3 SCREW, HEX. HEAD

1B

4

320A

NAS1149D0332J

3 WASHER XXX

1B

4

330A

FFCL1-4E1321-01

3 SUPPORT, MOBIL

1B

1

340A

FFCL1-4E1322-01

3 HEADREST, CTR

1B

1

350A

FFCL1-4E1323-02

3 HEADREST, RH

1B

1

360A

FFCL1-4E1323-01

3 HEADREST, LH

1B

1

2

(V U4447)

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10014-4 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

PAGE INTENTIONALLY LEFT BLANK

25-26-80

PAGE 10014-5 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

230 250 210 290

240 250

240 250

330 340

310 340

270

310 340

280

360 370 350

260

300 380

220 250 320 340

550 560

10 20 30

40 50 60

70 80 90

40 50 60

740 750

B

770 780 730 530 540

A

570 580

760

100

640

650 660 670 680

790

690 700 710 720

620 630 786

785 110 120 130

PALLET ASSEMBLY (SHEET 1 OF 2) FIGURE 15 / GRAPHIC 25-26-80-991-020-A01

25-26-80

PAGE 10015-0 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01

500 510

500 510

VIEW A

610

520 490 590 600

180 190 180 190

180 190 180 190 170 150 160 140 200 140

VIEW B 410

430 390

420

470 480 470 480

400 450

460

PALLET ASSEMBLY (SHEET 2 OF 2) FIGURE 15 / GRAPHIC 25-26-80-991-021-A01

25-26-80

PAGE 10015-1 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

15 -001A

FFCL1-2B0801-01

1 PALLET, LH ASSY SEE 252680-01, 290A FOR NHA

RF

-001B

FFCL1-2B0801-02

1 PALLET, RH ASSY SEE 252680-01, 290B FOR NHA

RF

-001C

FFCL1-5B0800-01

1 PALLET, LH ASSY SEE 252680-01A, 260A FOR NHA

RF

-001D

FFCL1-5B0800-02

1 PALLET, RH ASSY SEE 252680-01A, 260B FOR NHA

RF

010A

FFCL1-1B0632-01

2 TRACK, EQUIPPED

(NP)

1AB

1

010B

FFCL1-5B0632-01

2 TRACK, EQUIPPED

(NP)

1CD

1

020A

NAS604-11

ATTACHING PARTS 2 SCREW, TRUSS HEAD

(NP)

6

030A

NAS1149F0432P

2 WASHER XXX

(NP)

6

040A

FFCL1-1B0637-20

3 PLATE

2

050A

NAS1801-08-7

ATTACHING PARTS 3 SCREW, HEX. HEAD

4

060A

AN960-8

3 WASHER XXX

4

070A

FFCL1-1B0636-01

3 RACK

1

080A

NAS602-10P

ATTACHING PARTS 3 SCREW, TRUSS HEAD

4

090A

AN960-8

3 WASHER XXX

100A

FFCL1-1B0633-01

3 TRACK

(NP)

110A

FFCL1-1B0632-02

2 TRACK, EQUIPPED

(NP)

1AB

1

110B

FFCL1-5B0632-02

2 TRACK, EQUIPPED

(NP)

1CD

1

120A

NAS604-11

ATTACHING PARTS 2 SCREW, TRUSS HEAD

130A

NAS1149F0432P

2 WASHER XXX

140A

FFCL1-1B0637-21

3 PLATE

110A

2

140B

FFCL1-1B0637-20

3 PLATE

110B

2

4 1

6 6

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10015-2 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

15 ATTACHING PARTS 3 SCREW, HEX. HEAD

150A

NAS1801-08-7

4

160A

AN960-8

3 WASHER XXX

4

170A

FFCL1-1B0636-01

3 RACK

1

180A

NAS602-10P

ATTACHING PARTS 3 SCREW, TRUSS HEAD

4

190A

AN960-8

3 WASHER XXX

200A

FFCL1-1B0633-02

3 TRACK

(NP)

1

210A

FFCL1-2B0630-01

2 TRACK, REAR EQUIPPED

(NP)

1

220A

NAS604-11

ATTACHING PARTS 2 SCREW, TRUSS HEAD

2

230A

NAS604-28

2 SCREW, TRUSS HEAD

1

240A

NAS604-36

2 SCREW, TRUSS HEAD

2

250A

NAS1149F0432P

2 WASHER XXX

5

260A

FFCL1-1B0512-20

3 STOP

270A

NAS604-8

ATTACHING PARTS 3 SCREW, TRUSS HEAD

280A

AN960-416L

3 WASHER XXX

290A

FFCL1-2B0631-31

3 TRACK, REAR

(NP)

1

300A

FFCL1-2B0630-02

2 TRACK, REAR EQUIPPED

(NP)

1

310A

NAS604-11

ATTACHING PARTS 2 SCREW, TRUSS HEAD

2

320A

NAS604-28

2 SCREW, TRUSS HEAD

1

330A

NAS604-36

2 SCREW, TRUSS HEAD

2

340A

NAS1149F0432P

2 WASHER XXX

5

350A

FFCL1-1B0512-21

3 STOP

360A

NAS604-8

ATTACHING PARTS 3 SCREW, TRUSS HEAD

4

(NP)

1 1 1

(NP)

1 1

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10015-3 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

15 370A

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

AN960-416L

3 WASHER XXX

1

380A

FFCL1-1B0835-21

3 TRACK, REAR

390A

FFCL1-1B0617-01

2 FITTING, EQUIPPED

2

400A

NAS517-4-12

ATTACHING PARTS 2 SCREW, CSK HEAD XXX

8

410A

FFCL1-1B0618-20

3 YOKE

(NP)

1

420A

FFCL1-1B0516-20

3 BLOCK, LOCKING REAR

(NP)

1

430A

NSA5319-04-30

3 PIN, SPRING

(NPV F5442)

1

-440A

22719BC080027L

3 PIN, SHOULDERED

1

450A

FFCL1-1B0619-20

3 BUSH, SHOULDERED

2

460A

FFCL1-1B0514-20

2 PIN, SHEAR

1AB

2

460B

FFCL1-5B0514-31

2 PIN, SHEAR

1CD

2

470A

NAS603-7

1AB

2

470B

NAS514P1032-8

2 SCREW, CSK HEAD BONDED WITH LOCTITE 221 MADE BY F7121

1CD

2

480A

NAS1149F0332P

2 WASHER XXX

1AB

2

490A

FFCL1-1B0515-20

2 STUD, LOCKING FRONT

500A

NAS604-18

510A

NAS1149D0416K

2 WASHER XXX

520A

FFCL1-1B0503-20

2 SHIM

(NP)

2

530A

FFCL1-1B0532-20

2 STOP, LONG

(NP)

1

(NP)

ATTACHING PARTS 2 SCREW, TRUSS HEAD BONDED WITH LOCTITE 221 MADE BY F7121

1

2

ATTACHING PARTS 2 SCREW, TRUSS HEAD BONDED WITH LOCTITE 221 MADE BY F7121

2

2

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10015-4 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

15 ATTACHING PARTS 2 SCREW, CSK HEAD BONDED WITH LOCTITE 221 MADE BY F7121 XXX

540A

NAS517-4-9

550A

FFCL1-1B0532-21

560A

NAS517-4-9

570A

FFCL1-1B0502-22

2 INDICATOR, POSITION

1A

1

570B

FFCL1-1B0502-23

2 INDICATOR, POSITION

1B

1

580A

NAS514P428-6

ATTACHING PARTS 2 SCREW, CSK HEAD XXX

2

590A

FFCL1-1B0613-20

2 PIN, ANTI-RATTLE

2

600A

CA1710

2 SPRING

610A

NAS603-16

2 SCREW, TRUSS HEAD

2

620A

FFCL1-1B0635-20

2 COVER

2

630A

NAS514P832-8

640A

FFCL1-1B0642-01

2 SUPPORT, COVER

650A

NAS601-6P

ATTACHING PARTS 2 SCREW, TRUSS HEAD

4

660A

NAS602-6P

2 SCREW, TRUSS HEAD

4

670A

NAS1149FN632P

2 WASHER

4

680A

NAS1149DN832K

2 WASHER XXX

4

690A

FFCL1-1B0643-31

2 SUPPORT, WIRING

1

700A

NAS1801-08-9

ATTACHING PARTS 2 SCREW, HEX. HEAD

2

710A

NAS1149FN832P

2 WASHER

2

2 STOP, LONG

2

(NP)

1

ATTACHING PARTS 2 SCREW, CSK HEAD BONDED WITH LOCTITE 221 MADE BY F7121 XXX

2

(V F1142)

ATTACHING PARTS 2 SCREW, CSK HEAD BONDED WITH LOCTITE 221 MADE BY F7121 XXX

2

4

(NP)

4

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10015-5 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

15 720A

PART NUMBER

AIRLINE PART NUMBER

I N D

NOMENCLATURE

USAGE FROM TO

UNITS PER ASSY

NAS1149F0363P

2 WASHER XXX

1

730A

FFCL1-1B0644-01

2 SUPPORT, CONNECTOR

1

740A

NAS1801-08-8

ATTACHING PARTS 2 SCREW, HEX. HEAD

2

750A

NAS1149FN832P

2 WASHER XXX

760A

FFCL1-2B0522-31

2 SUPPORT, CONNECTOR EQUIPPED

1AB

1

760B

FFCL1-5B0522-31

2 SUPPORT, CONNECTOR EQUIPPED

1CD

1

770A

NAS1801-08-8

ATTACHING PARTS 2 SCREW, HEX. HEAD

780A

NAS1149FN832P

2 WASHER XXX

785A

FJPL1-1B0510-20

2 COVER

1CD

2

786A

NAS514P632-5

ATTACHING PARTS 2 SCREW, CSK HEAD XXX

1CD

2

790A

FFCL1-1B0801-01

2 PALLET

1A

1

790B

FFCL1-1B0801-02

2 PALLET

1B

1

790C

FFCL1-5B0801-01

2 PALLET

1C

1

790D

FFCL1-5B0801-02

2 PALLET

1D

1

2

2 2

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10015-6 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE

PAGE INTENTIONALLY LEFT BLANK

25-26-80

PAGE 10015-7 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01 240 240 250 250 230 250

270

210 290

330 340

310 340

280 260

310 340

360 370 350 300 380

220 250 320 340

40 50 60

590

70 80 90

10 20 30

630 640

480 490 500 560 570 740

700 710 720 730

390 410 420

100 650 660 670 680 690

110 120 130

A

750 580

CENTRAL PALLET ASSEMBLY (SHEET 1 OF 2) FIGURE 16 / GRAPHIC 25-26-80-991-022-A01

25-26-80

PAGE 10016-0 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01

180 190 180 190 180 190 180 190 170

170 180 190

150 160 140

200 140

VIEW A 620 520 530 520 530 600 610 400 510

CENTRAL PALLET ASSEMBLY (SHEET 2 OF 2) FIGURE 16 / GRAPHIC 25-26-80-991-023-A01

25-26-80

PAGE 10016-1 FEB 20/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

16 -001A

FFCL1-2B0844-01

1 PALLET, CTR ASSY SEE 252680-01, 300A FOR NHA

RF

-001B

FFCL1-5B0840-01

1 PALLET, CTR ASSY SEE 252680-01A, 270A FOR NHA

RF

010A

FFCL1-1B0632-01

2 TRACK, EQUIPPED

(NP)

2

020A

NAS604-11

ATTACHING PARTS 2 SCREW, TRUSS HEAD

(NP)

6

030A

NAS1149F0432P

2 WASHER XXX

(NP)

6

040A

FFCL1-1B0637-20

3 PLATE

2

050A

NAS1801-08-7

ATTACHING PARTS 3 SCREW, HEX. HEAD

4

060A

AN960-8

3 WASHER XXX

4

070A

FFCL1-1B0636-01

3 RACK

1

080A

NAS602-10P

ATTACHING PARTS 3 SCREW, TRUSS HEAD

4

090A

AN960-8

3 WASHER XXX

100A

FFCL1-1B0633-01

3 TRACK

(NP)

1

110A

FFCL1-1B0632-02

2 TRACK, EQUIPPED

(NP)

1

120A

NAS604-11

ATTACHING PARTS 2 SCREW, TRUSS HEAD

130A

NAS1149F0432P

2 WASHER XXX

6

140A

FFCL1-1B0637-21

3 PLATE

2

150A

NAS1801-08-7

ATTACHING PARTS 3 SCREW, HEX. HEAD

4

160A

AN960-8

3 WASHER XXX

4

170A

FFCL1-1B0636-01

3 RACK

1

180A

NAS602-10P

ATTACHING PARTS 3 SCREW, TRUSS HEAD

4

190A

AN960-8

3 WASHER XXX

4

6

4

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10016-2 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

16 200A

FFCL1-1B0633-02

3 TRACK

(NP)

1

210A

FFCL1-2B0630-01

2 TRACK, REAR EQUIPPED

(NP)

2

220A

NAS604-11

ATTACHING PARTS 2 SCREW, TRUSS HEAD

2

230A

NAS604-28

2 SCREW, TRUSS HEAD

1

240A

NAS604-36

2 SCREW, TRUSS HEAD

2

250A

NAS1149F0432P

2 WASHER XXX

5

260A

FFCL1-1B0512-20

3 STOP

270A

NAS604-8

ATTACHING PARTS 3 SCREW, TRUSS HEAD

280A

AN960-416L

3 WASHER XXX

290A

FFCL1-2B0631-31

3 TRACK, REAR

(NP)

1

300A

FFCL1-2B0630-02

2 TRACK, REAR EQUIPPED

(NP)

2

310A

NAS604-11

ATTACHING PARTS 2 SCREW, TRUSS HEAD

2

320A

NAS604-28

2 SCREW, TRUSS HEAD

1

330A

NAS604-36

2 SCREW, TRUSS HEAD

2

340A

NAS1149F0432P

2 WASHER XXX

5

350A

FFCL1-1B0512-21

3 STOP

360A

NAS604-8

ATTACHING PARTS 3 SCREW, TRUSS HEAD

370A

AN960-416L

3 WASHER XXX

380A

FFCL1-1B0835-21

3 TRACK, REAR

390A

FFCL1-1B0617-01

2 FITTING, EQUIPPED

400A

FFCL1-1B0503-20

2 SHIM

410A

AN174-11A

ATTACHING PARTS 2 SCREW, HEX. HEAD

420A

NAS1149F0432P

2 WASHER XXX

(NP)

1 1 1

(NP)

1 1 1

(NP)

1 2 1A

2 4 4

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10016-3 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

UNITS PER ASSY

16 -430A

FFCL1-1B0618-20

3 YOKE

(NP)

1

-440A

FFCL1-1B0516-20

3 BLOCK, LOCKING REAR

(NP)

1

-450A

NSA5319-04-30

3 PIN, SPRING

(NPV F5442)

1

-460A

22719BC080027L

3 PIN, SHOULDERED

1

-470A

FFCL1-1B0619-20

3 BUSH, SHOULDERED

2

480A

FFCL1-1B0514-20

2 PIN, SHEAR

2

490A

NAS603-7

500A

NAS1149F0332P

2 WASHER XXX

1

510A

FFCL1-1B0515-20

2 STUD, LOCKING FRONT

2

520A

AN174-13A

530A

NAS1149F0432P

2 WASHER XXX

2

540A

FFCL1-1B0532-20

2 DELETED

2

540B

FFCL1-1B0530-20

2 STOP, LONG

550A

NAS517-4-9

560A

FFCL1-1B0532-21

2 DELETED

560B

FFCL1-1B0530-21

2 STOP, LONG

570A

NAS517-4-12

580A

FFCL1-1B0542-21

2 INDICATOR, LEFT POSITION

1

590A

FFCL1-1B0542-22

2 INDICATOR, RIGHT POSITION

1

600A

FFCL1-1B0543-20

2 PIN, ANTI-RATTLE

2

ATTACHING PARTS 2 SCREW, TRUSS HEAD BONDED WITH LOCTITE 221 MADE BY F7121

1

ATTACHING PARTS 2 SCREW, HEX. HEAD BONDED WITH LOCTITE 221 MADE BY F7121

2

(NP)

ATTACHING PARTS 2 SCREW, CSK HEAD BONDED WITH LOCTITE 221 MADE BY F7121 XXX

ATTACHING PARTS 2 SCREW, CSK HEAD BONDED WITH LOCTITE 221 MADE BY F7121 XXX

2 4

2 (NP)

2 4

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10016-4 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-0xWY SERIES FFCL5-0xWY SERIE FIG-ITEM

16 610A

PART NUMBER

AIRLINE PART NUMBER

I N D

USAGE FROM TO

NOMENCLATURE

(V F1142)

UNITS PER ASSY

CA1710

2 SPRING

2

620A

NAS603-16

2 SCREW, TRUSS HEAD

2

630A

FFCL1-1B0635-20

2 COVER

4

640A

NAS514P832-8

650A

FFCL1-1B0634-01

2 SUPPORT, COVER

660A

NAS601-6P

ATTACHING PARTS 2 SCREW, TRUSS HEAD

1

670A

NAS602-6P

2 SCREW, TRUSS HEAD

1

680A

NAS1149FN632P

2 WASHER

1

690A

NAS1149DN832K

2 WASHER XXX

1

700A

FFCL1-2B0522-31

2 SUPPORT, CONNECTOR EQUIPPED

2

710A

NAS1352-06-12P

ATTACHING PARTS 2 SCREW, HEX. SOCKET HEAD

2

720A

NAS1149FN632P

2 WASHER

2

730A

NAS1149DN832K

2 WASHER XXX

2

740A

FJEV1-1B2074-20

2 SUPPORT, SWITCH CONNECTOR

4

750A

FFCL1-1B0848-01

2 PALLET

1A

1

750B

FFCL1-5B0841-01

2 PALLET

1B

1

ATTACHING PARTS 2 SCREW, CSK HEAD BONDED WITH LOCTITE 221 MADE BY F7121 XXX

2

(NP)

8

- ITEM NOT ILLUSTRATED

25-26-80

PAGE 10016-5 APR 15/09

EADS SOGERMA COMPONENT MAINTENANCE MANUAL FFCL4-01WY03-01 FFCL5-01WY01-01 FFCL5-01WY02-01

PAGE INTENTIONALLY LEFT BLANK

25-26-80

PAGE 10016-6 FEV 20/09