25-15-62-Rev3-Tr F04

132-SERIES

COMPONENT MAINTENANCE MANUAL WITH ILLUSTRATED PARTS LIST 132-SERIES PILOT & COPILOT SEAT F900 Revised : September 10, 2004

Pilot seat : 132051-100 132051-103 132051-113 132051-101 132051-111

Copilot seat: 132050-100 132050-103 132050-113 132050-101 132050-111

The seats listed above are certified to TSO C39 (a). Modification or installation of any components, including the covers and cushions, that are not OEM specified and certified will invalidate the TSO C39 (a) certification.

Information in this document is the property of SICMA AERO SEAT. This document, or parts thereof, may not be reproduced in any form without written authority from SICMA AERO SEAT.

Issued : Dassault F900 Sep 10/04 25-15-62 Title Page 132-SERIES

TEMPORARY REVISIONS N°.25-7 HIGHLIGHT

Remove and insert the affected pages as listed then complete the RECORD OF TEMPORARY REVISIONS in page II of CMM.

DESCRIPTION PAGE N° OF CHANGE

II Incorporated temporary revision N°.25-7 10034 Item 130 become item 62 10035 Item -61A P/N 132303-0 become P/N 132303-2, added new item 62 P/N 132303-01, item 100A P/N NAS679A4 become P/N NAS679A04,item 120 P/N 7002113 become P/N TAPK044BS,item 130A become item -130A,deleted P/N 132303-01 for item 130A and P/N 132303-02 for item - 131A. 10036 New pagination because change of place items.

PAGEpage 1/1 25-15-62 Mar 22/06 132-SERIES RECORD OF REVISIONS REV. TR. ISSUE DATE INSERTED REV. TR. ISSUE DATE INSERTED N°. N°.(*) DATE INSERTED BY N°. N°.(*) DATE INSERTED BY None 1997

1 Aug/97

2 Jan/00 .25-1 2000 .25-2 Oct/01 .25-3 Jan/02 .25-4 Nov/03 .25-5 Feb/04 .25-6 Mar/04 3 Sep/04 .25-7 Mar/06

Retain this record in the front of the manual. On receipt of revision, insert revised page in the manual and enter revision number, date inserted and initials. (*) Note : The temporary revisions are automatically integrated in the last revision. Record of Revisions EFFECTIVITY : Page I DASSAULT F900 25-15-62 Mar 22/06 132-SERIES RECORD OF TEMPORARY REVISIONS TEMPORARY PAGE ISSUE DATE BY DATE REMOVED BY REV. N°. NUMBER N.25-7 II Mar 22/06 N.25-7 10034 Mar 22/06 N.25-7 10035 Mar 22/06 N.25-7 10036 Mar 22/06

Record of Temporary Revisions EFFECTIVITY : Page II DASSAULT F900 25-15-62 Mar 22/06 132-SERIES RECORD OF TEMPORARY REVISIONS

Record of Temporary Revisions EFFECTIVITY : Page II DASSAULT F900 25-15-62 Mar 22/06 132-SERIES

SERVICE BULLETINS LIST

SERVICE DATE DESCRIPTION BULLETIN N∞. INCORPORATED SB132-25-001 April 13,99 Seat Bottom Modification for HUD Installation SB132-25-002 August 24,00 Fifth Strap Belt Installation SB132-25-003 January 23,02 Rear Cross Tube Change SB132-25-004 January 23,02 Seat Re-identification after Rear Cross Tube Evolution SB132-25-005 February 03,04 HUD, Harness Routing Securization SB132-25-005 May 02,04 Electrical Harness Routing issue 2 Securization

Service Bulletins List EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page III 132-SERIES

TABLE OF CONTENTS

PARAGRAPH TITLE PAGE RECORD OF REVISIONS I RECORD OF TEMPORARY REVISIONS II SERVICE BULLETINS LIST III TABLE OF CONTENTS IV LIST OF EFFECTIVE PAGES V INTRODUCTION VI 1. GENERAL VI 2. LAYOUT OF MANUAL VI 3. REVISIONS SERVICE VI 4. WARNINGS-CAUTIONS-NOTES VI 5. REQUIREMENTS VIa 6. LIST OF ABBREVIATIONS VIa DESCRIPTION AND OPERATION 1 1. GENERAL 1 2. GENERAL FIREBLOCKING INFORMATION 2 3. DESCRIPTION 3 4. OPERATION 7 5. DIMENSIONS 12 6. SEAT IDENTIFICATION PLACARD 14 TESTING AND TROUBLE SHOOTING 1001 1. GENERAL 1001 2. TESTING 1001 3. TROUBLE SHOOTING 1001 DISASSEMBLY 3001 1. GENERAL 3001 2. PROCEDURE 3001 CLEANING 4001 1. GENERAL 4001 2. LIST OF CLEANING MATERIALS AND USAGE 4001 3. PROCEDURES 4002

Table of Contents EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page IV 132-SERIES

TABLE OF CONTENTS PARAGRAPH TITLE PAGE CHECKS 5001 1. GENERAL 5001 2. VISUAL CHECKS 5001 3. POST-FLIGHT CHECKS 5001 4. CHECK INTERVAL 5002 5. CHECK PROCEDURES 5003 6. LUBRICATED PARTS 5005 7. REPLACEMENT OF THE PARTS 5006 REPAIR 6001 1. GENERAL 6001 2. LIST OF MATERIALS 6001 3. REPAIR PROCEDURE 6005 ASSEMBLY 7001 1. GENERAL 7001 2. LIST OF MATERIALS 7001 3. PROCEDURE 7005 FITS AND CLEARANCES 8001 1. TABLE OF FITS AND CLEARANCES 8001 SPECIAL TOOLS, FIXTURE AND EQUIPMENT 9001 1. GENERAL 9001 2. SPECIAL TOOLS 9001 3. SPECIAL EQUIPMENT 9001 ILLUSTRATED PARTS LIST 10001 1. INTRODUCTION 10001 2. ALPHANUMERICAL INDEX 10001 3. DETAILED PARTS LIST 10001 4. HOW TO USE THE PARTS LIST 10004 5. LIST OF VENDORS 10005 6. UPDATING 10007 ALPHANUMERICAL INDEX 10009 DETAILED PARTS LIST 10020 STORAGE 15001 1. STORAGE INSTRUCTION 15001

Table of Contents EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page IVaIVa 132-SERIES

LIST OF EFFECTIVE PAGES

SUBJECT PAGE DATE SUBJECT PAGE DATE Title Page Sep 10/04 Disassembly 3001 Sep 10/04 Record of Revisions I Sep 10/04 3002 Sep 10/04 3003 Sep 10/04 Record of Temporary II Sep 10/04 3004 Sep 10/04 Revisions 3005 Sep 10/04 Service Bulletins III Sep 10/04 3006 Sep 10/04 List 3007 Sep 10/04

Table of Contents IV Sep 10/04 Cleaning 4001 Sep 10/04 IVa Sep 10/04 4002 Sep 10/04 4003 Sep 10/04 List of Effective V Sep 10/04 4004 Sep 10/04 Pages Va Sep 10/04 4005 Sep 10/04 4006 Sep 10/04 Introduction VI Sep 10/04 VIa Sep 10/04 Recommended Checks 5001 Sep 10/04 VIb Sep 10/04 5002 Sep 10/04 VIc Sep 10/04 5003 Sep 10/04 VId Sep 10/04 5004 Sep 10/04 5005 Sep 10/04 Description and 1 Sep 10/04 5006 Sep 10/04 Operation 2 Sep 10/04 3 Sep 10/04 Repair 6001 Sep 10/04 4 Sep 10/04 6002 Sep 10/04 5 Sep 10/04 6003 Sep 10/04 6 Sep 10/04 6004 Sep 10/04 7 Sep 10/04 6005 Sep 10/04 8 Sep 10/04 6006 Sep 10/04 9 Sep 10/04 6007 Sep 10/04 10 Sep 10/04 6008 Sep 10/04 11 Sep 10/04 6009 Sep 10/04 12 Sep 10/04 13 Sep 10/04 Assembly (Storage) 7001 Sep 10/04 14 Sep 10/04 7002 Sep 10/04 7003 Sep 10/04 Testing and Trouble 1001 Sep 10/04 7004 Sep 10/04 Shooting 1002 Sep 10/04 7005 Sep 10/04 1003 Sep 10/04 7006 Sep 10/04 1004 Sep 10/04 7007 Sep 10/04 1005 Sep 10/04 7008 Sep 10/04 1006 Sep 10/04 7009 Sep 10/04 1007 Sep 10/04 7010 Sep 10/04 1008 Sep 10/04 1009 Sep 10/04 Fits and Clearances 8001 Sep 10/04 1010 Sep 10/04 8002 Sep 10/04 1011 Sep 10/04 8003 Sep 10/04

* The asterisk indicates pages changed, added or deleted F = Foldout Page List of Effective Pages EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page IVaV 132-SERIES

LIST OF EFFECTIVE PAGES

SUBJECT PAGE DATE SUBJECT PAGE DATE 8004 Sep 10/04 Structure Lower 10044 Sep 10/04 8005 Sep 10/04 10045 Sep 10/04 8006 Sep 10/04 10046 Sep 10/04 10047 Blank Special Tools, 9001 Sep 10/04 Headrest Assembly 10048 Sep 10/04 fixtures & Equipment 10049 Sep 10/04

Storage 15001 Sep 10/04 Illustrated 10001 Sep 10/04 15002 Sep 10/04 Parts List 10002 Sep 10/04 Sep 10/04 10003 Sep 10/04 10004 Sep 10/04 10005 Sep 10/04 10006 Sep 10/04 10007 Sep 10/04

Alphanumerical 10009 Sep 10/04 Index 10010 Sep 10/04 10011 Sep 10/04 10012 Sep 10/04 10013/10019 Blank

Detailed Parts List Pilot Seat Assembly 10020 Sep 10/04 10021 Sep 10/04 10022 Sep 10/04 10023 Sep 10/04 Covering Assembly 10024 Sep 10/04 10025 Sep 10/04 Armrest Assembly 10026 Sep 10/04 10027 Sep 10/04 10028 Sep 10/04 10029 Sep 10/04 10030 Sep 10/04 10031 Blank Lumbar Rest Assembly 10032 Sep 10/04 10033 Sep 10/04 Backrest Assembly 10034 Sep 10/04 10035 Sep 10/04 10036 Sep 10/04 10037 Blank Seat Structure 10038 Sep 10/04 10039 Sep 10/04 10040 Sep 10/04 10041 Sep 10/04 Level Assembly 10042 Sep 10/04 10043 Sep 10/04

* The asterisk indicates pages changed, added or deleted F = Foldout Page List of Effective Pages EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page IVaVa 132-SERIES DESCRIPTION AND OPERATION

INTRODUCTION

TASK 25-15-62-990-801 1. GENERAL This manual has been compiled in accordance with the requirements set out in ATA specification ATA2200. It is designed to provide sufficient information to enable a mechanic, who is unfamiliar with the product, to service, repair and inspect the unit. The unit is manufactured by: SICMA AERO SEAT (Societe Industrielle et Commerciale de Materiel Aeronautique). VENDOR CODE : VF0465 FACTORY : 7, RUE LUCIEN COUPET - 36100 ISSOUDUN, BP 69 FRANCE Telephone : (33) (0) 2 54 03 39 39 Telefax : (33) (0) 2 54 03 39 00 WEB Site : www.sicma.zodiac.com HEADQUARTER : 48 BOULEVARD GALLIENI - 92137 ISSY LES MOULINEAUX ,FRANCE Telephone : (33) (0) 1 41 23 25 25 Telefax : (33) (0) 1 41 23 25 26 Telefax numeris : (33) (0) 1 41 46 04 44 (Customer Support for North, Central and South America) SICMA AERO SEAT SERVICES INC. : 22030-20TH AVENUE S.E SUITE 102 BOTHELL SEATTLE-WASHINGTON 98021 U.S.A Telephone : (425) 806 2066 Telefax : (425) 806 2068 2. LAYOUT OF MANUAL This manual contains a general description, followed by data for maintenance, repair, disassembly and assembly of the unit. This is followed by an Illustrated Parts List which gives detailed information. 3. REVISIONS SERVICE This manual will be updated as required by revisions, Service Bulle- tin may be issued separately. Their effect on the manual will, however, be made evident by reissue of the Service Bulletins List as appropriate. 4. WARNINGS-CAUTIONS-NOTES These adjuncts to the text are expressed by the following headings:

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page VI 132-SERIES DESCRIPTION AND OPERATION

WARNING WARNINGS CALL ATTENTION FOR USE OF MATERIALS, PROCESSES, METHODS, PROCEDURES OR LIMITS WHICH MUST BE ADHERED TO PRECISELY IN ORDER TO AVOID ANY INJURY OR DEATH TO PERSONS.

CAUTION CAUTIONS CALL ATTENTIONS TO METHODS AND PROCEDURES WHICH MUST BE ADHERED TO IN ORDER TO AVOID DAMAGE TO EQUIPMENT.

NOTE Notes call attention to methods which make the job easier.

5. REQUIREMENTS Each seat assembly is designed to comply with the requirements defined in the following documents: DASSAULT Specification DTM 20502 DASSAULT Specification DTE 25.11.02 FAA Technical Standard Order (TSO) C 39 Revision (a) FAA Technical Standard Order (TSO) C 22 Revision (g) Federal Aviation Regulation Parts 25 and 121 NAS Specification 809

6. LIST OF ABBREVIATIONS The following abbreviations have been used in this IPL. Abbreviations : ABD Airbus Directives and Procedures A/C Aircraft ARM TAB Arm Table ASSY or AY Assembly ATA Air Transport Association of America AVU Audio Video Unit B/C Business Class B/O Breakover BACK Backrest BAG Baggage CMM Component Maintenance Manual CTL Central CTR Center CUS Cushion DBL Double DET BKDN Detail Breakdown DHPS Dual Headphone Power System DISC Disconnect DLVY Delivery

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page VIa 132-SERIES DESCRIPTION AND OPERATION DSEB Digital Seat Electronic Box DPCU Digital Passenger Control Unit EFFECT. Effective EPCU Electrical Passenger Control Unit EPML Emergency Path Marking Light EQU Equipped ESCUT Escutcheon EXTL External F Foldout Page FAA Federal Aviation Authority FAR Federal Aviation Regulations FB Fire Blocking F/C First Class FIG Figure FIX Fixing FLDG Folding F/R Front Row HAND Handicap HD Head HEX Hexagonal HMAR Hatch Mounted Armrest HZ Hertz IAT In Arm Table IFE In Flight Entertainement System INB Inboard INSTL Installation INTL Internal IPL Illustrated Parts List ISO International System Organisation ISPC In Seat Power Control ISPS In Seat Power Supply IVASEB Individual Video Seat Electronic Box IVCP Individual Video Cassette Player IVS Individual Video System JAA Joint Airworthiness Authority JAR Joint Airworthiness Requirements JAU Jack Audio Unit J-BOX Junction Box LATL Lateral LCD Liquid Cristal Display LED Light Emitting Diode LH Left-Hand L/R Lower MECS Multiple Envelop Convertible Seats MISCL Miscellaneous N/A Not Applicable

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page VIb 132-SERIES DESCRIPTION AND OPERATION NAR Narrow NAS National Aerospace Standard NHA Next Higher Assembly N∞ Number NP Not Procurable : If this is written after a description it means that this reference is not included in the set of drawings but constitutes a group of parts for illustration only. OPT Optional OUTBD Outboard PAX Passenger PC Polycarbonate PCH Personal Control Handset PCU Passenger Control Unit PJB Power Junction Box P/N Part Number PROX Proximity PSU Power Supply Unit PVT Pivot PVP Passenger Video Player QTY Quantity QUADR Quadruple RECL Recline REPLS Replaces REV Revision RF Reference : Indicates parts whose quantities are indicated in another part of the illustrated list. RH Right-Hand RJM Remote Jack Module RJU Remote Jack Unit SB Service Bulletin SDU Seat Demodular Unit SEB Seat Electronic Box SELF-SKIN Self-Skinning SET Seat Electronic Terminal SEU Seat Electronic Unit SGL Single SPCL Special S/S Shipset SST Stainless Steel STD Standard STRUCT Structure SVD Seat Video Display TBD To Be Determined

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page VIc 132-SERIES DESCRIPTION AND OPERATION T/C Tourist Class TCU Tape Control Unit TPL Triple TSO Technical Standard Order TSVD Touch Screen Video Display UEB Unit Electronic Box UPCU Universal Passenger Control Unit U/R Upper VASEB Video Audio Seat Electronic Box VDB Video Distribution Box VDU Video Display Unit VSEB Video Seat Electronic Box W/ With W/O Without ZTB Zone Telephony Box

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page VId 132-SERIES DESCRIPTION AND OPERATION DESCRIPTION AND OPERATION

TASK 25-15-62-870-801 1. GENERAL A. INTRODUCTION This manual contains maintenance and repair instructions for Pilot and Copilot seats type 132 manufactured by SICMA AERO SEAT. (1) The Pilot and Copilot seats are identical in design and operation; they only differ in the symmetrical arrangement of the controls and ashtray. (2) The two seats are fitted with adjustable armrests and seat backs, and can be adjusted for height and position in the fore and aft directions. (3) The seats are equipped with a multi point restraint system which is attached on the seat primary structure and the seat back.

NOTE: As an option, this reel can be provided with a manual control system.

(4) The overall dimensions and weights of the seats are as follows:

-weight :19.700 kg (43,430 lbs) -width :580 mm (22.83 inches) -depth :585 mm (23.03 inches) (seat back vertical) -height : 937 mm (36.89 inches) minimum, 1187 mm (46.73 inches) maximum.

B. CONFORMITY TO CERTIFICATION The numerous requirements for demonstrating that a "seat system" meets all the static and dynamic loads, the permanent deformation limitations, and the injury criteria, implies that individual elements of a seat system cannot be evaluated independently from each other. This difficulty translates into keeping the chain of structures and other essential features affecting the performance of the "seat system" intact as certificated. The performance of the components, the behavior of which are critical to the overall system, are numerous. These include, but are no limited to the seat belt, the bottom cushions, all padded components, the back cushions, the back structure, the seat back weight and vertical center of gravity, the total mass of the seat, any structural load path active in a primary or secondary fashion in restraining the occupant to the seat and the seat to the aircraft. Additionally, the seat back upright setting back (if any and degrees), aircraft track, rear pad, angle of the seat with respect to the aircraft axis, rotation of deployable items, all have significant impact on the certification.

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 1 132-SERIES DESCRIPTION AND OPERATION TASK 25-15-62-870-802 2. GENERAL FIREBLOCKING INFORMATION Fireblocking is the term used to describe the method or system of providing increased thermal protection for the foam in seat cushions. For that reason, the cushions, fireblocking liner and dress cover are considered to be a fireblocking system. Changes to any of the three components of the system can affect the thermal protection capability of that system. Two factors that affect capability are the cleanliness of all the components and the integrity of the fireblocking liner. Liners are made of materials, which, because of their chemical composition, provide inherent capability and do not depend on yarn or fabric treatments and coatings. Liners have no shelf life and their capability is not decreased by dry cleaning. Liner capability will be decreased by mechanical damage and, as stated above, will be influ- enced by the cleanliness of all components of the fireblocking system (cushion, liner and dress cover.) A. FIREBLOCKING LINER (1) Cleanliness : Slight discoloration, fading or color transfer from the dress cover to the fireblocking liner are normal and do not affect the capability of the liner system. Heavy stains, particularly petroleum products, should be removed using materials and methods currently listed for upholstery. Care should be taken not to soak the stain into the underlying cushion. Commercial dry cleaning is acceptable for removing large stains. If a liner is to be dry cleaned, be aware that liners have a large amount of hook Velcro and care should be taken to prevent them from damaging the liner or other covers and liners during the dry cleaning cycle. (2) Damage to Liners : The primary factor in liner capability is the mechanical integrity of the liner. The mechanical integrity is affected by wear holes and seams. If holes are being worn in liners, the structure should be made locally less abrasive. Dress sharp edges with a file or use glass tape. Tape may also be used elsewhere. - Generalized wear which results in a change of the liner surface texture, sheen or color is of no consequences as long as there is no hole through the liner. - Holes in the liner can degrade its capability but tests have been conducted that show that up to three (3) holes of 0.312 diameter still permit the liner to exceed minimum thermal performance requirements. The number and size of holes noted do not render the system nonflightworthy but the holes should be repaired at the next maintenance interval. B. REPAIR TO LINERS (1) Seams : Resew seam using same stitch pattern and stitch count used on other similar seams on the liner. Use only kevlar thread. (2) Holes : Must be patched, darning alone is not acceptable.

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 2 132-SERIES DESCRIPTION AND OPERATION - Patch must be of the same material as the liner. - Patch must be overlock stitched along its perimeter (not required for felts). - For cosmetic purposes and/or to prevent snagging, the hole may be darned prior to sewing the patch in place. - Patch may be on the outside or inside surface of the liner -Patch to be sewn on with the noted Kevlar thread using the same stitch pattern and stitch count as other seams on the liner. - Patch to be sized so that seams in the parent fabric that attach the patch are in undamaged parent fabric, preferably at least one-half damage diameter width from the edge of the damaged area. C. DRESS COVERS All previously stated considerations concerning dress covers remain in effect. In addition to appearance and sanitary considerations, the cleanliness of dress covers may affect the thermal performance of the fireblocking system. Cleaning intervals for dress covers should be evaluated to ensure against excess contamination buildup and transfer of contamination through to the fireblocking liner. NOTE: The fabric looses itís fireblocking capacity after twenty washings.

D. CUSHIONS The factors affecting the thermal performance of cushions are the density of the cushions and theirs cleanliness. Tests have shown that changes in cushion firmness (IFD / Identifi- cation Force Deflection) do not affect the thermal performance properties of the cushion. Heavy stains on cushions, particularly from petroleum products, should not be allowed to build up. Mild non-volatile, non-flamma- ble cleaners may be used gently on the surface of the cushion. Do not rub hard enough to break the skin of the foam. Because of the fire blocking layer, cushions can be expected to remain fairly clean. TASK 25-15-62-870-803 3. DESCRIPTION Subtask 25-15-62-870-001 A. GENERAL Each seat mainly comprises a lower structure and an upper structure, linked together by the arms and the box structure of the height adjustment system.

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 3 132-SERIES DESCRIPTION AND OPERATION Subtask 25-15-62-870-002 B. LOWER PRIMARY STRUCTURE The lower structure comprises : -the structure proper -the adjustment system. (1) Structure The structure mainly consits of two longitudinal members linked together by two cross members. Each longitudinal member is fitted with a fore and aft position locking system, a guide receiving the roller of the arm and two rollers which allow the seat to move along the aircraft rail. The rear cross member is provided with two welded lugs to carry the electrical actuator of the seat height adjustment system. This structure, which carries the entire seat, can be moved backwards and forwards along two rails fitted to the floor of the aircraft. (2) Height adjustment system

The height adjustment system mainly comprises : - a box structure which is hinged to the back of the seat pan structure at one end, while the other end slides upon rollers running within guide slots in the longitudinal members, -two arms which are hinged to the longitudinal members and also to the middle of the sides of the box structure. The free ends of the arms slide upon rollers running within guide slots in the side frames of the seat pan, -an electrical actuator secured to the rear cross member of the lower structure, the moving actuator rod being coupled to a tube integral with the lower end of the box structure through a crank pin. The crank pin is fitted with a grease nipple.

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Seat Description Figure 1

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Rear Items of Equipment Figure 2

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Subtask 25-15-62-870-003 C. UPPER STRUCTURE The upper structure comprises: - a sheet metal, - a backrest. (1) Sheet metal The structure consits of two light alloy side frames which are connected together by three tubes. A sheet metal support is secured to the front of the structure. On the LH side frame, for the pilot's seat, and on the RH side frame, for the co-pilot's seat, a support plate is fitted to carry : - the seat height adjustment control, - the backrest inclination adjustment control. The inertia reel control (OPTION) is secured to the RH side frame, for the pilot's seat, or to the LH side frame, for the copilot's seat. At the rear of the structure, two fittings are provided to secure the bearings around which the armrests are free to rotate. Each armrest comprises : - a cover, which envelopes the main support, (2) Backrest Of tubular construction, the backrest carries. The following parts are secured to the back of the backrest : - the inertia reel, - the pair of actuators which are used to adjust and to lock the backrest. Each actuator is integral with the backrest structure, to which it is secured by its clevis and its support. TASK 25-15-62-870-804 4. OPERATION Subtask 25-15-62-870-001 A. Adjustment of the seat height

The box structure is hinged to the seat pan at one end and hinged with the front crosspiece to the other end. The arms are hinged to the rear of the backward crosspiece and also to the middle of the sides of the box structure. Their free

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 7 132-SERIES DESCRIPTION AND OPERATION ends slide upon rollers running within slots in the side frames of the seat pan.

The electrical actuator is operated by means of the control switch. Extension or retraction of the actuator rod connected to the front crosspiece results in a change in the angle between the box structure and the arms, thus lowering or raising the seat. Subtask 25-15-62 -870-002 B. Fore and aft adjustment of the seat Operation of the control lever turns the locking tube, which raises both locking pins through the action of two fork arms ; the seat is then free to slide along its rails. When the control lever is released, both locking pins again engage in holes in the rail through the action of their return springs; the seat is then locked in position.

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Seat Adjustment Figure 3

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 9 132-SERIES DESCRIPTION AND OPERATION Subtask 25-15-62-870-003 C. Fore and aft adjustment of the armrest tops When the occupant of the seat depresses the control push button, both locking studs are withdrawn and the top of the armrest can be moved forward or rearward to the required position. The range of adjustment is limited by the movement of a pin within two elongated holes in the main support. When the seat occupant releases the pushbutton, he adjusts the top so that the two studs again enter the holes in the main support. The top of the armrest is then locked in the required position. Subtask 25-15-62-870-004 D. Adjustment of the armrest height (See Fig. 4) Pressure exerted upon the lateral pushbutton shifts the tab of the actuator through movement of the end of the lever integral with the push button. The actuator rod is then released and the seat occupant can move the armrest in the required direction. When the armrest is in the required position, the seat occupant releases the pushbutton, the actuator tab returns to its original position and the actuator rod is automatically locked inside the actuator body . During adjustment, the actuator rod is held in contact with the bearing through pressure exerted by the spring. The range of the adjustment of the armrest is limited by the stroke of the actuator rod, which is provided with a rubber bushing to cushion its contact with the actuator body. Subtask 25-15-62-870-005 E. Adjustment of the backrest inclination Operation of the mechanical inclination adjustment control opens the hydraulic circuit of the two actuators, allowing the seat occupant to select the required inclination by pressure exerted upon the backrest. When the seat occupant releases the mechanical control, the circuit is closed, thus clamping the actuators in position and retaining the backrest in the selected position.

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Armrest Height Adjustment Figure 4

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 11 132-SERIES DESCRIPTION AND OPERATION TASK 25-15-62-870-805 5. DIMENSIONS For seat dimensions refer to figures 5.

Dimensions Figure 5 (sheet 1)

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Dimensions Figure 5 (sheet 2)

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 13 132-SERIES DESCRIPTION AND OPERATION TASK 25-15-62-870-806 6. SEAT IDENTIFICATION PLACARD For seat identification placard refer to figure 6. Identification plate to be stuck on box structure assy. The TSO or QAC approval does not cover any electronic equipment such as the I.F.E. or its installation. The installer of the seat into the aircraft must substantiate these additional components.

P/N : 00-5008

NOTE: The identification plate P/N 00-5008 must be protected with self adhesive transparent plastic film P/N PDFILMPP100x65.

Identification Placard Figure 6

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TESTING AND TROUBLE SHOOTING

TASK 25-15-62-700-801 1. GENERAL A. The various incidents that may be encountered are listed below along with their probable causes. B. Defective parts should be repaired according chapter ´Repairª by approved workshops or may be replaced with serviceable elements. Care should be taken to use only approved parts, you may invalidate the TSO C39 (a) certification of the seat. 2. TESTING A. The tests consist in placing the chair in its operational position and checking the good working order of all its various components. B. Check all the correct lowering motion of the seating assembly in order to ensure that there are no friction points and that it operates without any problems. 3. TROUBLE SHOOTING A. The probable failures causes for this Pilot and Copilot could be due to a defective assembly or adjustement during the assembly of various sub-assemblies. B. An incorrect use could be a source of incidents. In all these cases, remove and replace the defective parts. C. The most frequently encountered failures during use of the seat are listed in the table below, as well as the probable causes and corresponding repairs to be performed. D. Having carried out the indicated repairs, try out the seat again in order to ensure that the fault no longer exists, according to the chapter ´Description and operationª.

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TROUBLE PROBABLE CAUSE CORRECTION The seat has seized up, The electrical actuator is defective. Check the electrical actuator and in the up and down position. replace if necessary. The actuator end fitting has seized up Check the actuator end fitting and or is defective. replace if necessary. The switch is defective. Check the switch and replace the switch. Electrical harness cut or wrongly con- Replace defective harness. nected. Check for correct functioning. Restraint System Reel does not Check shape good winding. function correctly. Inertia reel malfunctioning. Replace the inertia reel. Backrest has seized up. Defective actuator. Replace the actuator. Seized up or damaged mechanical Replace the control mechanism. control mechanism. Height adjustment is Button improperly adjusted. Tighten or loosen the front knob. impossible for armrest. Bearing improperly adjusted. Tighten or loosen screws. Seat recline button is broken Vibrations, shocks. Replace or adjust the recline away. button. Height adjustment is impossible Beta pins improperly adjusted. Adjust the beta pins. for headrest.

TROUBLE SHOOTING CHART Table 1001

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1.0 Make sure seat is in START full upright position

Visually inspect Check for wear, cuts, headrest tears & holes assembly

Is headrest No 1.1 assembly OK ?

Yes R & R* 9 / 5 thru 9 / 15 Make sure seat is in Check headrest full upright position adjustment

1.1

Is headrest No 1.2 adjustment OK ? Yes R & R* Visually inspect 9 / 5 Check for deterioration back cushion assy

1.2

Is back cushion No 1.3 assy OK ?

Yes R & R* Visually inspect 2 / 70 or 2 / 71 Check for wear, cuts, tears & holes covers & cushions assy *NOTE: Refer to IPL section to 1.3 Identify Figure-Item (# / #) Identified in remove and repair 1.A (R & R) block. Fault Isolation Flowchart - Seat Assembly Figure 102 (sheet 1)

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 1003 132-SERIES TESTING AND TROUBLE SHOOTING

1.A

Are covers & No 1.4 cushions OK ?

Yes R & R* 2 / 70 or 2 / 71 Visually inspect Check for wear, cuts, thru 2/60 or 2/61 tears & holes bottom cushion assembly

1.4

Is bottom No 1.5 cushion assy OK ? Yes R & R* 2 / 40 or 2 / 41

Check for damage & Visually inspect thru 2/50 or 2/51 missing parts armrest assembly

1.5

Are movable No 1.6 armrest assy OK ? Yes 2.0 R & R* 3 / 3 or Routine outlined in Detail Fault 3 / 4 section 2.0 to isolate Isolation of faulty parts for repar. movable armrest

1.6

1.B

*NOTE: Refer to IPL section to Identify Figure-Item (# / #) Identified in remove and repair Fault Isolation Flowchart - Seat Assembly (R & R) block. Figure 1002 (sheet 2)

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 1004 132-SERIES TESTING AND TROUBLE SHOOTING

1.B

Check for wear, cuts, Visually inspect tears & holes armrest cover

Is armrest No 1.7 cover OK ?

Yes R & R* 3 / 150 Check forfrays, cuts, Visually inspect breackage or other damage belts, straps & buckle.

1.7

Are belts, No 1.8 straps & buckles OK ?

Yes R & R* 1 / 30 thru Do extension / Check reel 1 / 70 retraction test & assembly check for locking / unlocking operation

1.8

1.C

*NOTE: Refer to IPL section to Identify Figure-Item (# / #) Identified in remove and repair (R & R) block. Fault Isolation Flowchart - Seat Assembly Figure 1002 (sheet 3)

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 1005 132-SERIES TESTING AND TROUBLE SHOOTING

1.C

Is reel No 1.9 assembly OK ? Yes R & R* 1 / 50 thru 1.C 1 / 70

3.0

Routine outlined in Detail Fault Isolation 1.9 section 3.0 to isolate of longitudinal faulty parts for repar. adjustment.

4.0

Routine outlined in Detail Fault Isolation section 4.0 to isolate of height faulty parts for repar. adjustment.

5.0

Routine outlined in Detail Fault Isolation section 5.0 to isolate of backrest faulty parts for repar. adjustment.

6.0

Routine outlined in Detail Fault Isolation section 6.0 to isolate of electrical faulty parts for repar. actuator.

END

*NOTE: Refer to IPL section to Identify Figure-Item (# / #) Identified in remove and Fault Isolation Flowchart - Seat assembly repair (R & R) block. Figure 1002 (sheet 4)

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 1006 132-SERIES TESTING AND TROUBLE SHOOTING

2.0 START

Lower armrest from the vertical position

Does armrest No 2.1 lower / raise easily Yes R & R* 3 / 60 thru Adjust knob so 3 / 91 both arms are at the lowest sitting

2.1 Knob turn

Does knob No 2.2 turn ?

Yes R & R* 3 / 340 thru No Does armrest 3 / 350 unlock/lock 2.3 easily Yes R & R* 2.2 3 / 180 thru 3 / 250 Return to inspection

*NOTE: Refer to IPL section to 2.3 Identify Figure-Item (# / #) Identified in remove and repair (R & R) block. Fault Isolation Flowchart - Movable armrest assembly Figure 1003

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 1007 132-SERIES TESTING AND TROUBLE SHOOTING

3.0 START

Operate longitudinal lever

R & R* Does control No 3.1 lever works 8 / 150 thru 3.1 easily 8 / 210 Yes

R & R* Does lever No 3.2 secure on shaft 8 / 160 thru 3.2 8 / 210 Yes

Does lever R & R* activate longi- No 3.3 8 / 60 thru 3.3 tudinal move 8 / 130 Yes

Does seat R & R* No 3.4 move 8 / 40 thru 8 / 50, 3.4 Fwd / Aft 8/310 thru 8/320 Yes

Does Fwd/Aft No R & R* 3.5 control lock in 3.5 8/120 thru 8/130 position Yes

Return to *NOTE: inspection Refer to IPL section to Identify Figure-Item (# / #) Identified in remove and repair (R & R) block. Fault Isolation Flowchart - Longitudinal Adjustment Figure 1004

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 1008 132-SERIES TESTING AND TROUBLE SHOOTING

4.0 START

Seat in the lower- position

Operate height adjuster control

Does seat R & R* No 4.1 move Up / 7 / 10 thru 4.1 Down 7 / 270 Yes

Does Up or No R & R* 4.2 intermediate 4.2 position keep 1/150 thru 1/160 Yes

Return to inspection

*NOTE: Refer to IPL section to Identify Figure-Item (# / #) Identified in remove and repair (R & R) block. Fault Isolation Flowchart - Height Adjustment Figure 1005

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 1009 132-SERIES TESTING AND TROUBLE SHOOTING

5.0 START

Operate backrest control pusher

R & R* Does backrest No 5.1 control works 6 / 380 thru 5.1 easily 6 / 520 Yes

R & R* Does backrest No 5 / 140 and 5.2 move «Fwd - 5.2 5 / 170 Aft» Yes

Return to inspection

*NOTE: Refer to IPL section to Identify Figure-Item (# / #) Identified in remove and repair (R & R) block. Fault Isolation Flowchart - Backrest assembly Adjustment Figure 1006

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 1010 132-SERIES TESTING AND TROUBLE SHOOTING

6.0 START

Seat in the lower- position

Operate height adjuster control

Does seat R & R* No 6.1 move Up / 7 / 10 thru 6.1 Down 7 / 270 Yes

Does Up or R & R* No 6.2 intermediate 1 / 150 thru 6.2 position keep 1 / 160 Yes

Return to inspection

*NOTE: Refer to IPL section to Identify Figure-Item (# / #) Identified in remove and repair (R & R) block. Fault Isolation Flowchart - Electrical Actuator Figure 1007

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 1011 132-SERIES DISASSEMBLY

DISASSEMBLY

TASK 25-15-62-000-801 1. GENERAL Complete disassembly of the seat assembly is neither anticipated nor recommended. The degree of disassembly carried out should not be more than necessary. For the identification of damage or functional failure refer to chapter 5001 RECOMMENDECK CHECKS and chapter 1001 TESTING AND TROUBLE SHOOTING.

CAUTION : DO NOT REMOVE RIVET-MOUNTED ASSEMBLIES OR COMPONENT PARTS UN- LESS DAMAGE NECESSITATES REPLACEMENT BY AN AVAILABLE PART. REPEATED REMOVAL AND REINSTALLATION OF RIVETS WILL CAUSE FATIGUE OF THE ADJACENT MATERIAL. DAMAGE IN THIS AREAS WILL REQUIRE REPLACEMENT OF THE NEXT HIGHER ASSEMBLY. REFER TO THE ILLUS- TRATED PARTS LIST WHICH CONTAINS A COMPLETE ENUMERATION OF THE AVAILABLE PARTS.

NOTE : After removal of the seat assembly from the aircraft, the use of a suitable frame to simulate the appropriate aircraft mounting provisions is recommended to facilitate maintenance and repair.

CAUTION : MOVING OR TRANSPORTING THE SEAT ASSEMBLIES BY SLIDING THEM ACROSS FLOOR SURFACES WILL DAMAGE THE TRACK ATTACHING FITTINGS OR MOUNT- ING SURFACES RESULTING IN EXCESSIVE WEAR TO THESE CRITICAL AREAS.

TASK 25-15-62-000-802 2. PROCEDURE A. GENERAL The following describes sequences of disassembly. Because of the similarities in Pilot & Co-pilot seats covered in this manual and for ease of explanation, only one type is described hereafter.

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 3001 132-SERIES DISASSEMBLY

NOTE : All parts should be marked before disassembly in order to facilitate easier subsequent assembly and to avoid any assembly errors.

B. SEQUENCES OF DISASSEMBLY

1. UPHOLSTERY 2.MISCELLANEOUS AFT COVERS 3.RESTRAINT SYSTEM 4.UPPER STRUCTURE 5.RECLINE ACTUATOR AND CONTROL 6.ELECTRICAL ASSEMBLY 7.ARMREST ASSEMBLY 8.BACKREST AND SEAT PAN 9.SEAT TO RAIL LOCKING 10.LOWER STRUCTURE ASSEMBLY 11.HEADREST ASSY

C. ACCOMPLISHMENT Subtask 25-15-62-020-001 (1) Removal of UPHOLSTERY (Ref. IPL, Fig. 2 & 9 ) (a) Ref. IPL, Fig. 2: Remove cushions (60&80) from their sup- ports. (b) Remove covers (50&70) from the cushions. (c) Ref. IPL, Fig. 9: Remove headrest cover (15) from the headrest cushion (10).

NOTE : The cushions are fixed with "VELCRO".

Subtask 25-15-62-020-002 (2) Removal MISCELLANEOUS AFT COVERS (Ref. IPL, Fig. 5 & 1) (a) Ref. IPL, Fig. 5: Loosen screws (70), remove sleeves (10) then disengage backrest cover (20) from the backrest structure (260). (b) Ref. IPL, Fig. 1: Loosen screws (40&90), remove spacers (100) disengage side fairings (30&-31) from the lateral spreaders.

Subtask 25-15-62-020-003 (3) Removal of RESTRAINT SYSTEM (Ref. IPL, Fig. 5 & 1) (a) Ref. IPL, Fig. 5: Loosen screws (70), remove sleeves (10)

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 3002 132-SERIES DISASSEMBLY then disengage backrest cover (20) from the backrest structure(260). (b) (b)Ref. IPL, Fig. 1: Loosen aft nuts (70), remove screws (60) then disengage inertia reel (50) from the backrest structure. (c) Ref. IPL, Fig. 1: Loosen screws (40) then disengage inertia reel (50) from the seat structure. Subtask 25-15-62-020-004 (4) Removal UPPER STRUCTURE from the LOWER STRUCTURE (Ref. IPL, Fig. 6 & 7) (a) Ref. IPL, Fig. 6: Raise the seat to the up position. (b) Separate the connector from electrical actuator (160). (c) If necessary, remove the switch by unscrewing both screws. (d) Unscrew both nuts (90) securing the box structure to the upper structure. (e) Remove both screws (80) and recover both sleeve bushings (120). (f) Ref. IPL, Fig. 7: swing the upper structure through ap- proximately 45∞ in order to release upper rollers (230) from their guides.

Subtask 25-15-62-020-005 (5) Removal of BACKREST INCLINAISON ASSEMBLY (Ref. IPL, Fig. 6 and 5) (a) Raise the seat to the up position. (b) Tilt the backrest for forward. (c) Ref. IPL, Fig. 6: Disconnect the cable (400) from the actuator by loosening of the screw (-520)and by removal of the spring ring (510). For each actuator : (d) Ref. IPL, Fig. 5: unscrew nut (180) and remove screw (190), securing the hydrolock (200&210) to the backrest structure, (e) Unscrew both attaching screws (140) and release actuator (200) from the clevis, (f) Unscrew nut (160) and remove yoke (170) of hydrolock (200)&(210). (g) Remove lock-nut (160), (h) Ref. IPL, Fig. 6: remove backrest inclination adjustment control (380).

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 3003 132-SERIES DISASSEMBLY

Subtask 25-15-62-020-006 (6) Removal of ELECTRICAL ASSEMBLY (Ref. IPL, Fig. 1 and 8) (a) Raise the seat to the up position.

NOTE: Position some wooden shims inside the lower structure spars in order to block the rollers to be able to disengage the motor in safety (risk of shearing).

(b) Ref. IPL, Fig. 1: Separate the connector from electrical electrical jack (160). (c) Drive out plastic rivets (140) attaching loop clamps (130) and remove cable assembly (150). (d) Ref. IPL, Fig. 8:Measure the play between rollers (50) and the guide. (e) Count the number of screw threads visible on the grease end fitting of electrical jack (160). (f) Flatten the tab of the lock washer safety-locking the end fitting to the actuator rod, slacken the lock-nut and unscrew it by at least one full turn. (g) Remove both socket head cap screws (-380) securing electrical jack (160) to the rear cross tube. (h) Separate the actuator from its end fitting and remove the actuator. Subtask 25-15-62-020-007 (7) Removal of ARMREST ASSEMBLY (Ref. IPL, Fig. 1 and 3) Removal (Ref IPL, Fig. 1) (a) Unscrew attaching screw (90) and remove armrest assembly (80 or 81). (b) Recover hollow screw (100) and recover both washers (110). Disassembly (Ref IPL, Fig. 3) (a) Unscrew and remove the four screws (40). (b) Recover washers (50) and remove armrest cover (30). (c) Unscrew and remove screw (20) and recover knob (10). (d) Slacken lock-nut (350) and remove screw (340) complete with lock-nut (350). (e) Unscrew and remove screws (360) and recover control rod assembly (400).

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 3004 132-SERIES DISASSEMBLY (f) Remove screw (310), washer (320) and recover rubber bushing (330). (g) Remove retaining ring (370), washer (380) and recover spring (390). (h) Unscrew and remove screw (440) and washer (450); remove lever assembly (480). (j) Recover washers (460) and sleeve spacer (470). (k) On lever (480), remove spring pin (410), pin (420) and recover pushrod (430). (l) Unscrew screw (60) and remove hollow screw (70). (m) Recover washers (80) and fitting assembly (90). (n) Remove retaining rings (130) and remove pin (140). (p) By depressing lever assembly (240), slide the armrest assembly away from support assembly (300). (q) Unscrew pin (190), recover spring (200) and washers (210 or 220). (r) Remove screws (160 and 170), then recover upper armrest (150)

Subtask 25-15-62-020-008 (8) Removal of the BACKREST and SEAT PAN (Ref IPL, Fig. 5 and 6) (a) Separate the lower structure from the upper structure (see para. 4.). (b) Ref. IPL, Fig. 6: Disconnect the backrest inclination adjustment control (380),of the actuators. (c) Ref. IPL, Fig. 5: Unscrew both nuts (160) to release both actuators (200). (d) Disengage the clevis support from the seat pan structure . (e) Remove the inertia reel asembly (see para. 3.). (f) Unscrew both nuts (250) and recover washers (240). (g) Remove both hinge pins (220) and recover washers (230). (h) Separate the backrest from the seat pan.

Subtask 25-15-62-020-009 (9) Removal SEAT-TO-RAIL LOCKING assembly (Ref IPL, Fig. 8) (a) Raise the seat to the up position. On both sides : (b) Drive out spring pin (60) and recover the retaining ring:

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 3005 132-SERIES DISASSEMBLY remove ring (70), (c) Unscrew cross tube screw (90) and remove fork arm (80), (d) Unscrew both screws (110) and remove plate (100), (e) Remove locking pin (130) and spring (120), (f) Unscrew both screws (240) and recover both nuts (230), sleeve spacer (310) and roller (320), (g) Remove inner pad (280), outer pad (250) and bearing (270). (h) Remove cross tube assembly (220). (j) Unscrew and remove attaching screw (200) of control lever (180).

Subtask 25-15-62-020-010 (10) Removal of LOWER STRUCTURE (Ref IPL, Fig. 7 and 8) (a) Preliminary steps 1.Separate the lower structure from the upper structure (See para. 4.). 2.Remove the electrical actuator (See para. 6.). (b) Arm and box structure (Ref IPL, Fig. 8) - Arm 3. Ref. IPL, Fig. 8: Unscrew nut (10) and remove screw (20). 4. Withdraw the arm from the rear clevis lugs and remove sleeve spacer (30). 5. Ref. IPL, Fig. 7: Remove retaining ring (30) and central hinge pin (40) and sleeve (70). 6. Separate the arm from the box structure. 7. Unscrew upper pin (10) and remove roller (20). 8. Drive out spring pin (50) and remove the arm. 9. Carry out the same operations for the other arm, and recover the upper spacer (130). - Box structure 1. Remove both arms (see para. (b). 2. Hold the box structure vertically and remove one of the lower rollers from its guide by moving the box structure sideways. Remove the box structure assembly. 3. Ref. IPL, Fig. 8: Unscrew both pins (40) and remove rollers (50).

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 3006 132-SERIES DISASSEMBLY (c) Longitudinal members (Ref IPL, Fig. 8). 1. Unscrew both nuts (230), remove both screws (240) and recover roller (320) and both sleeve spacers (310). 2. Remove both rear pads (290 and 300).

3. Unscrew both screws (370) and remove rear cross tube (390). 4. Unscrew the four nuts (350) and recover screws (340). 5. Remove the front cross tube and both longitudinal members (330,420 and 421). Subtask 25-15-62-020-011 (11) Removal of HEADREST ASSY (Ref IPL, Fig. 9) (a) Disengage headrest assy (-1) from the sleeves of backrest structure.

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 3007 132-SERIES CLEANING CLEANING

TASK 25-15-62-100-801 1. GENERAL Thorough cleaning is essential to any close inspection to determine the presence, extent and location of possible defects. External surfaces and upholstery should be periodically checked and cleaned. The table below lists cleaning agents and materials for use on the seat assembly. TASK 25-15-62-100-802 2. LIST OF CLEANING MATERIALS AND USAGE

USAGE CLEANING AGENT

Metal, dirt and grime Soap and water (Ivory liquid soap), chlorinated dry cleaning solvent.

Metal, grease and oil Hexane, isopropyl alcohol, grain alcohol (ethanol). Chlorinated dry cleaning solvent.

Fabric backed vinyls Soap and water (Ivory liquid soap).

Polycarbonate/ABS fairing Soap and water only. dirt and grime

Leather Saddle soaps.

Sheepskin Soap such as Ivory liquid containing no enzymes and a neutral pH. Do not use Woolite.

CAUTION : DURING THE CLEANING, PROTECT THE ACTUATOR, HARNESS, SWITCH AND HYDROLOCK. DRY THE SEAT AFTER ANY CLEANING CLEANING MATERIALS AND USAGE TABLE 4001

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 4001 132-SERIES CLEANING TASK 25-15-62-100-803 3. PROCEDURE Subtask 25-15-62-100-001 A. POLYCARBONATE/ABS FAIRING (1) Extreme care should be taken in cleaning all plastics. Alcohol or bleaches based agent will never have to be used to clean any plastic materials. (2) All plastic surfaces should be cleaned with a mild soap (Ph<7) and water solution. (3) Mix soap with water to obtain the desired concentration according to the strength needed for cleaning purposes. (4) Apply the solution directly to the surface and rub with a clean cloth to loosen any dirts and debris. (5) Rinse with clear water, then wipe off with a dry cloth.

CAUTION :CLEANING AGENTS WITH CHLORINATED SOLVENTS, METHYLATED SPIRIT, ACETONE AND/ OR STRONG DETERGENTS WITH HIGH AMMONIAC OR ALKALINE CONTENTS ARE STRICTLY FORBIDDEN.

STEAM CLEANING IS STRICTLY FORBIDDEN. THE USE OF ABOVE MENTIONED PRODUCT OR PROCEDURE WILL AFFECT THE MATERIAL PROPERLY, WHEN IT BECOMES BRITTLE.

Subtask 25-15-62-100-002 B. UPHOLSTERY CLEANING PROCEDURES (SEAT COVERS AND LEATHERS) (1) Machine cleaning process (a) Identification and classification of the stains. The covers must be examined before cleaning in order to identify those having stains which will not be removed by machine cleaning and therefore submit them to a pre- cleaning. Machine cleaning can in fact alterate those stains and make their successive elimination quite dif- ficult. As general criteria remember that the following stains are not directly removed in the machine and therefore require a pre-cleaning: - coca cola, wine, blood, fruit, sweat, food. On the contrary, machine cleaning removes stains of : - coffee, fats, alcoholic drinks, some kinds of ink. Generally stains can be recognized as follows : - coffee and ink stains for their color and neat outline. - wine, coca cola, alcoholic drinks and sweat stains for their extensive and shaded out-line. - food and fat stains for their consistence.

Fruit and blood stains are not easily recognizable.

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 4002 132-SERIES CLEANING (b) Pre-cleaning

NOTE : Pre-cleaning is advisable in all cases of stains of uncertain nature

Pre-cleaning must be carried out as follows :

(2) Prepare a mixture of BC-2 Solugan, Perchlorethylene, water with a 1 : 0.5 : 0.5 ratio. Quantity : about 1 liter of mixture for 30 covers. For the mixture in a bucket and immerse the stained portion of cover rubbing the fabric energetically until the characteristic dirt of the stain has disappeared. Wring the fabric by hand and repeat the operation if necessary. (3) Prepare a mixture of Neptune, Perchlorethylene, water with a 1 : 1 : 1 ratio. Quantity : about 1 liter of mixture for 30 covers. Perform the pre-cleaning as described above. (a) Preparation of covers The adhesive stripes of all covers must be covered in order to avoid fraying of fabric at the end of the cleaning phase. (b) Preparation of the machine At least once a day it is necessary to perform the following operations: (4) to regenerate the perchlorethylene through distillation. (5) to add, directly in the reservoir, 1 liter of the pure additive used in pre-cleaning to every 100 liters of perchlorethilene. (a) Washing phase Before each load of covers add one of the following additives to the perchlorethilene, directly in the drum: (6) BC-2 Solugan :prepare a mixture of additive, alcohol, water in a ratio of 1 : 1 : 1, for 1,5 liter of mixture for each 40 Kg. of covers to be washed. (7) Neptune : prepare a mixture of additive, alcohol, water in a ratio of 1 : 1 : 1, for 1,5 liter of mixture for every 20 Kg. of covers to be washed. NOTE : The additive introduced in the drum must be the same as the one used for the pre-cleaning.

- Mix the perchlorethylene and the mixture before introducing the covers, in order to facilitate the dispersion of the additive in the solvent. - Load the drum with the covers, making sure that the adhesive stripes are covered. The quantity of covers must not be over 80 % of the machine maximum

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 4003 132-SERIES CLEANING operation load.-Wash for 5 minutes at room temperature.

- Centrifugate without exceeding 500 r.p.m. for 3 minutes. - Rinse for 5 minutes with pure solvent at room temperature. - Dry at a temperature not exceeding 60° C. (a) Control and repetition of treatment

After drying take the covers out and check them, one by one, to separate those which still have stains. These still having stains should be pre-washed once more following steps (1) b) and c). Following this they should be machine washed, together with another load of the same type. The second pre-wash is essential to avoid the stain becoming even more resistant to removal. (b) Ironing and final control The covers which have not been rejected must be ironed and subjected to a more rigorous checks to select and return to the cycle those still having stains.

(8) Dry cleaning process

NOTE : LANTAL wool or mohair fabrics, cleaned in accordance to the following recommendations can be dry cleaned up to 20 times without loosing the flame resistant properties.

(a) All hook (male) Velcro tapes must be covered with their counterpart (loop tape) to avoid any damages to the fabric during the dry cleaning process. (b) The covers should be sprayed with a detergent activator and left for about 20 minutes before loaded to the dry cleaning machine. Heavily stained areas should be slight- ly brushed with a soft brush. (c) For the dry cleaning process, please follow the instructions of the machine supplier. (d) About 70 to 80% of the covers should become clean during pre-treatment and dry cleaning - depending on the cleaning system and kind of stains. The spots still visible can be cleaned with a steam gun and then dry cleaning again. Before loaded to the dry cleaning machine, the fabric must be completely dry to avoid shrinkage.

CLEANING TABLE

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 4004 132-SERIES CLEANING

STAIN WHAT TO USE Alcohol, Liquors Use shampoo and then mop with methylated spirit. Beer Mop with tepid water (50∞ C max.) with 3% methylated spirit. Blood Mop with cold water. Then shampoo and use 5% ammonia. Butter, Oil, Sauce Mop with ethylic alcohol and perchlorethylene. Use shampoo and then 5% ammonia if stain remains. Chewing-gum Mop with acetone or perchlorethylene. Chocolate Mop with tepid water (50∞C max) or with 5% ammonia. Coffee, Tea Use shampoo and methylated spirit or 10% ammonia if stain remains. Egg Mop with 5% ammonia or methylated spirit, then use shampoo. Fruits, Food Mop with tepid water and then use shampoo. Glue, Paints Use ethylic alcohol or perchlorethylene. Then mop with tepid water or shampoo. Grass, Vegetables Moisten with methylated spirit. Ink, Coal Use absorbent paper then mop with a solution of 30% methylated spirit and 70% water. Use also lemon juice. Juice, Jam Mop with tepid water (50∞ C max.) if stain remains use ethylic alcohol or perchlorethylene. Mayonnaise, Use 10% ammonia and perchlorethylene. Ketchup, Mustard Then use shampoo. Milk, Ice cream, Use shampoo then mop with 5% ammonia or perchloreth- Cream ylene. Mud Let it dry up and then use vacuum-cleaner. Shoe polish, Use ethylic alcohol or perchlorethylene. Floor, Wax If stain remains use 5% ammonia or methylated spirit. Sugar Mop with tepid water. Then use shampoo. Tar Mop with methylated spirit or perchlorethylene, then use shampoo. Vomit, Urine, Mop with water and 50% vinegar or methylated spirit. Ordures Then use shampoo. Water Absorb with a cleaned cloth and let it dry up. Use shampoo or alcohol on eventual rings. Wax, Paraffin Put on the seat absorbent paper and iron it. Mop with perchlorethylene. Then use shampoo. Wine, Drinks Use a solution of 50 % vinegar then shampoo.

Subtask 25-15-62-100-003

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 4005 132-SERIES CLEANING C. METAL PARTS Moisten a clean, dry cloth with dry cleaning solvent and thoroughly, wipe metal parts completely clean. Degreasing of stainless steel and aluminium parts necessitates usage of trichloretane.

WARNING :USE SOLVENT-TYPES CLEANING AGENTS IN A WELL VENTILATED AREA. AVOID BREATHING SOLVENT VAPORS AND PROLONGED SOLVENT CONTACT WITH SKIN. OBSERVE APPROPRIATE FIRE PRECAUTIONS.

Subtask 25-15-62-100-004 D. LEATHERS Leathers should be cleaned with commercial saddle soaps. Do not use detergents or solvents type. Subtask 25-15-62-100-005 E. FABRIC-BACKED VINYLS

This type of material should be cleaned with a mild soap and water solution such as ivory liquid soap and wiped clean and dry. Do not use solvent-type cleaners.

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 4006 132-SERIES CHECKS

CHECKS

´THE FOLLOWING CHECKS MAY BE REPLACED WITH AN AIRLINES MAINTENANCE PROCEDURES APPROVED BY OWN LOCAL AUTHORITIESª

TASK 25-15-62-200-801 1. GENERAL This maintenance program is applicable to SICMA PILOT P/N 132051-XXX and COPILOT seat P/N 132050-XXX presently in operation. The aircraft must be electrically supplied (28 Vdc). For all operations describe below refer to the "DESCRIPTION AND OPERATION" chapter of the manual.

NOTE : If repair and/or overhaul of the seat assembly are necessary, refer to REPAIR chapter.

TASK 25-15-62-210-801 2. VISUAL CHECKS A. A preliminary inspection before initial cleaning will facilitate location of obvious defects. B. All hardware, piece parts, minor assemblies and minor subassem- blies are to be visually inspected using a strong light and preferably some means of magnification. C. Visually inspect parts for nicks, cracks, cuts, corrosion, crossed and stripped threads, scoring, excessive wear and defects that could impair efficient seat operation. NOTE : Excessive wear shall be defined by a visible deformation or deterioration of part that makes the equipment inoperative. If there is a doubt concerning the functioning of a part, replace it unless it is specified in the detail list as requiring specific repairs.

TASK 25-15-62-210-802 3. POST-FLIGHT CHECKS A. Check seat general status (leather or fabric upholstering). B. Check proper seat belt attach. C. Check proper electrical up and down seat operation. D. Check the armrest controls for correct operation.

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 5001 132-SERIES CHECKS E. Lower structure: (1) Check for absence of play in the hinges and for correct condition of the rollers. (2) Check the free sliding motion of the seat on the rails. (3) Check the rail locking control for correct operation, paying special attention to the locking studs and the return springs. Discard defective parts. (4) Height adjustment system Check the switch for correct operation. Make sure that the electrical actuator operates smoothly, without binding. Make sure that the actuator end fitting turns and slides freely. If the end fitting has seized-up, or if the screwthreads are damaged, replace it. F. Upper structure: (1) Check the backrest inclinaison control.Operate the actuators several times; they must operate smoothly, without binding. (2) Check the various items providing comfort and particularly : - the lumbar support of the backrest and the suspension springs. - the VELCRO strips,

- the springs, the protective covers and the sheet metal seat panel of the seat pan. Replace defective items. G. Restore the seat to normal position.

TASK 25-15-62-210-803 4. CHECK INTERVAL

Maximum Flight cycleshours Check Symbol Seat Installed Intermediate Check 1 400750 A Yes Intermediate Check 2 8001500 2A/B 2A Yes Intermediate Check 3 12002250 3A Yes Intermediate Check 4 16003000 4A/2B 4A Yes Intermediate Check 5 20003750 5A No Basic Check 1 40004500 C No Basic Check 2 80009000 2C No Basic Check 3 1200013500 3C No Basic Check 4 1600018000 4C No Basic Check 5 20000 5C No

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 5002 132-SERIES CHECKS TASK 25-15-62-210-804 5. CHECK PROCEDURES

CHECK INTERVALS A 2A3A4A5AC 2C3C4C5C Subtask 25-15-63-210-001 A Structure. Check the structure in general for evidence of 1 XXXXXXXXXX scratches, cracks, holes and various damages.

Check for damaged coating and for other 2 XXXXXXXXX possible surface damages.

3 Check if a corrosion is present. XXXXXXXXXX

Check the aeras that are not easely accessible 4 XXXXXXXXXX to prevent the corrosion.

Subtask 25-15-63-210-002 B Upholstery. Ckeck all the covers, condition of fabric, open 1 XXXXXXX seams and correct alignment of VELCRO tape

2 Replace the covers. XX

3 Ckeck all the cushions, density XXXX

4 Replace the cushions XX Subtask 25-15-63-210-003 C Termoformed fairing 1 Check the correct installation of all fairings. XXXXXXX

2 Check for surface imperfections. XXXXX

3 Replace the fairings. XX Subtask 25-15-63-210-004 D Screwed and riveted connections. Check screwed and riveted connections for a firm 1 XX sitting. Subtask 25-15-63-210-005 E Check placards for presence and attachment 1 Check placards for presence and attachment. XXXX XX Subtask 25-15-63-210-006 F Longitudinal Adjustment. 1 Clean the seat track from any residue or dust XXXXXXXXXX

Check proper operation of seat translation, move the 2 XXXXXXXXXX seat to its maximum forward and backward positions.

CHECK INTERVALS A 2A3A4A5AC 2C3C4C5C

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 5003 132-SERIES CHECKS

Ensure there is nothing interfere between the seat 3 XXXXXXXXXX track and the seat.

Check that the seat track locking pins ensure correctly 4 XXXXXXXXXX the seat stop while pushing aft/forward the seat.

Check the manual operation to disengage the locking 5 XXXXXXXXXX pins (part with the yellow paint). Subtask 25-15-63-210-007 G Height Adjustment. Check proper operation of the maximum up and down 1 XXXXXX positions by using the height adjustment switch.

Check proper operation of the maximum up and down 2 XXXXX positions by using the crank handle.

Subtask 25-15-63-210-008 H Seat belt attachment. 1 Check the seat belt attachment on the structure shaft. X XXXXX

2 Check the proper operation of the rotative buckle. X XXXXX

3 Check manually the operation of the seat belt reel. X XXXXX

4 Check manually the blocking of the seat belt reel. X XXXXX

Subtask 25-15-63-210-009 J Backrest adjustment. Check the proper operation of the backrest recline by 1 XXXXXX using the recline control.

Check the backrest recline to its maximum forward 2 XXXXX and backward positions by using the recline control.

Subtask 25-15-63-210-010 K Armrest adjustment. 1 Check the proper operation of the armrest. XXXXXX

2 Check the armrest to its maximum angle positions. XXXXX

CHECK INTERVALS A 2A3A4A5AC 2C3C4C5C

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 5004 132-SERIES CHECKS Subtask 25-15-63-210-011 L Electrical actuator assy. 1 Check the mechanical function of the switch. XXXXXX

Check wires and electrical components for 2 XXXXXX attachment, damage and overheating signs.

3 Check the connections for cleanliness. XXXXXXXXXX

Check the terminal plugs for firm connection on the 4 XXXXXX wire ends.

5 Check the sealing and the coating of the ground point. XXXXXX

TASK 25-15-62-200-802 6. LUBRICATED PARTS A. Some removed parts need to be lubricated with some grease ALVANIAG (see reference p7003 ´List of Materialsª) B. List of the lubricated parts and diagram (see below):

PART NUMBER NOMENCLATURE FIG. ITEM QTY 128500-24 YOKE 5 170 2 132100-06 SPACER,INTERNAL 8 310 8 132200-08 BUSHING,SLEEVE 6 120 2 132301-15 BUSHING 5 290 3 132500-01 PIN 7 40 2 132500-02 PIN,TREADED,HEADED 7 10 2 132500-03 PIN,TREADED,HEADED 8 40 2 132520-02 BUSHING,SLEEVE 7 70 1 132100-12 ROLLER,LH AFT 8 321 2 132100-09 LOCKING PIN 8 130 2 132100-04 ROLLER,RH AFT 8 320 2 132100-11 SHAFT,MOTOR 8 420 1 132200-74 SPRING 6 230 12 132200-05 RH FITTING 6 10 1 132200-06 LH FITTING 6 40 1 132400-04 YOKE 4 50 1 00-0521 HELICAL SPRING 3 200 1 394-10-310-07 SPRING 3 390 1 394-10-310-11 PIN 3 140 1 132275-010-0 PIN 3 141 1 376-100-19 BUSHING 8 30 2

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 5005 132-SERIES CHECKS

C. Electrical actuator assy : - perform visual checks of component in a well-illuminated area, using a magnification power of 10 or greater. - perform checks requirements in accordance with SICMA AERO SEAT Component Maintenance Manual ref.25-29-78. TASK 25-15-62-200-804 7. REPLACEMENT OF THE PARTS On completion of check procedure, draw up a list of defective parts to be replaced and parts requiring repair or new protection.

NOTE : If is necessary to replace the self-locking nuts, the locking washers and the pins.

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 5006 132-SERIES REPAIR

REPAIR

TASK 25-15-62-300-801 1. GENERAL Tolerance of scratches, cuts, nicks, dents, etc., on plastic and other components is established by the airline's own standards for aircraft interiors. Plastic components which have been cracked, must be replaced; they are considered "not repairable". Metal components which have been damaged, must be replaced; they are considered "not repairable". 2. LIST OF MATERIALS NOTE: Equivalent substitutes may be used for listed items.

MATERIAL IDENTIFICATION SOURCE APPLICATIONS

ADHESIVE AGOBOIS BT BOSTIK S.A. Solid wood, laminated white R.N. 19 panels, plating (within ( supersede 77170 COUBERT only) VINYL BT) FRANCE

ADHESIVE AGOBOIS PU BOSTIK S.A. Wood on all support color white R.N. 19 (at external) 77170 COUBERT FRANCE

ADHESIVE AGOPLAC DI BOSTIK S.A. Laminated on usual amber R.N. 19 support ( supersede 77170 COUBERT NEOPRENE DIR) FRANCE

ADHESIVE BONDMASTER ROUSSELOT Foam on cloth, foam on R 319R QUINCAILLERIE S.A. foam, foam on wood, color pink Bld de l'Europe foam on agglomerate, BP 184 foam on plywood, foam on 79304 BRESSUIRE Cedex metal FRANCE ADHESIVE LOCTITE n∞401 LOCTITE Corporation Elastomer, metal, plastic colorless 705, West Mountain Road Newington, Conn. 06111 U.S.A. ADHESIVE LOCTITE n∞416 LOCTITE Corporation Elastomer, metal, plastic colorless 705, West Mountain Road Newington, Conn. 06111 U.S.A.

Repair Materials Table 6001 (sheet 1)

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 6001 132-SERIES REPAIR MATERIAL IDENTIFICATION SOURCE APPLICATIONS ADHESIVE LOCTITE n∞421 LOCTITE Corporation Elastomer, metal, plastic clear colorless liquid 705, West Mountain Road Newington, Conn. 06111 U.S.A. ADHESIVE LOCTITE n∞601 LOCTITE Corporation Elastomer, metal, plastic green, fluorescent 705, West Mountain Road liquid Newington, Conn. 06111 U.S.A. ADHESIVE LOCTITE n∞638 LOCTITE Corporation Elastomer, metal, plastic green, fluorescent 705, West Mountain Road liquid Newington, Conn. 06111 U.S.A. ADHESIVE LOCTITE n∞648 LOCTITE Corporation Elastomer, metal, plastic green, fluorescent 705, West Mountain Road liquid Newington, Conn. 06111 U.S.A.

ADHESIVE M 890 BOSTIK S.A. Metal surface, PVC colorless R.N. 19 77170 COUBERT FRANCE

ADHESIVE METHYLENE ELF ATOCHEM S.A. Miscellaneous fairing, CHLORIDE 4 cours Michelet Cedex 42 cocktail table, 92091 PARIS LA DEFENCE 10 tray in polycarbonate only FRANCE

ADHESIVE MONTAPRENE BOSTIK S.A. Armcap, foam on sheet 2796 R.N. 19 metal ( supersede 77170 COUBERT Neoprene) FRANCE

ADHESIVE SILICOMET AS310 LOCTITE FRANCE Sealing, joint realization ( supersede 10 Avenue Eugene Gazeau Loctite 5366) BP 96 60304 SENLIS Cedex FRANCE

ADHESIVE SICOMET 7000 PIROT RUTARD Aluminium, steel, brass, colorless INDUSTRIE ABS fairing only (supersede 22, rue Combanaire OMNIFIT 7000) 36000 CHATEAUROUX FRANCE

ADHESIVE SICOMET 8300 PIROT RUTARD Aluminium, steel, brass INDUSTRIE 22, rue Combanaire 36000 CHATEAUROUX FRANCE

ADHESIVE TRANSPRENE K11 BOSTIK S.A. Leather, rubber, color amber R.N. 19 elastomer, wood, 77170 COUBERT composition material FRANCE Repair Materials Table 6001 (sheet 2)

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 6002 132-SERIES REPAIR MATERIAL IDENTIFICATION SOURCE APPLICATIONS

ADHESIVE TAPE ALUMINIUM FOIL 3M France Sealing of cavities TAPE Boulevard de l’Oise (Optional) 425 x 2 in 95006 CERGY PONTOISE Cedex FRANCE

ADHESIVE TAPE DOUBLE COATED 3M FRANCE Fairing, POLYESTER TAPE Boulevard de l’Oise structure armrest, 9490LE & 9495LE 95006 CERGY PONTOISE cocktail table High load and Cedex FRANCE Temperature Retaining

ADHESIVE TAPE DOUBLE COATED 3M FRANCE Fairing, TAPE Boulevard de l’Oise structure armrest, 9573 High 95006 CERGY PONTOISE cocktail table Performance Cedex FRANCE

CLEANER ISOPROPYL PROLABO metal surface, grease and ALCOHOL 54, rue Roger Salengro oil. BP 115 94126 FONTENAY-SOUS- BOIS Cedex FRANCE

CLEANER GRAIN PROLABO metal surface, grease and ALCOHOL 54, rue Roger Salengro oil. (ETHANOL) BP 115 94126 FONTENAY-SOUS- BOIS Cedex FRANCE

CLEANER SYDOL SID SOCIETE INDUSTRIELLE DE Miscellaneous fairing, DIFFUSION escutcheon hostess step, B.P. 118 step stirrup, 94003 CRETEIL Cedex ashtray, foodtray, FRANCE in arm table DE-RUSTER ARDROX 396/1 BRENT S.A. Rust point 280 rue J.B. Godin 02200 VILLENEUVE ST GER- MAIN FRANCE

GREASE ALVANIAG SHELL Greaser on technical seat 89, Bld Franklin Roosevelt 92564 RUEIL- MALMAISON FRANCE

LUBRICANT WD40 AEROSOL WD-40 COMPANY LTD Sliding mechanism P.O. Box 440, MILTON KEYNES, BUCKS MK113LF ENGLAND

Repair Materials Table 6001 (sheet 3)

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 6003 132-SERIES REPAIR MATERIAL IDENTIFICATION SOURCE APPLICATIONS

LUBRICANT WD40 LIQUID WD-40 COMPANY LTD Sliding mechanism P.O. Box 440, MILTON KEYNES, BUCKS MK113LF ENGLAND MASTIC Mastic DOW CORNING S.A. Sealing of cavities DOW CORNING 732 Parc Industriel - Zone C (optional) Clear B- 7180 Seneffe BELGIUM NON SLID material AF6/1472 AEROFLOOR LTD Pads covering (PIMPLE) 3 Commerce way, Whitehall Industrial Estate, CO2 8HR COLCHESTER NON SLID material AF6/1499 AEROFLOOR LTD Pads covering (3mm diameter 3 Commerce way, STUD) Whitehall Industrial Estate, CO2 8HR COLCHESTER SEALANT, High LOCTITE n∞290 LOCTITE Corporation Parts already assembled Temperature 705, West Mountain Road Retaining Newington, Conn. 06111 U.S.A. SEALANT, High LOCTITE n∞222 LOCTITE Corporation Brake filet for screw, nut, Temperature purple (low) 705, West Mountain Road shoulder shaft Retaining Newington, Conn. 06111 U.S.A. SEALANT, High LOCTITE n∞243 LOCTITE Corporation Brake filet for screw, nut, Temperature blue (normal) 705, West Mountain Road shoulder shaft Retaining Newington, Conn. 06111 U.S.A. SEALANT, High LOCTITE n∞270 or LOCTITE Corporation Brake filet for screw, nut, Temperature n∞2701 705, West Mountain Road shoulder shaft Retaining green (strong) Newington, Conn. 06111 U.S.A.

VELCRO SELF-GRIPPING APLIX S.A. Upholstery attachment, FASTENER TAPE ZA Les Relandières bottom sheet metal, (HOOK & LOOP RN 123 BP 850 Ligne backrest, legrest, beam, TYPE) 44850 CELLIERS bottom & backrest cover FRANCE

Repair Materials Table 6001 (sheet 4)

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 6004 132-SERIES REPAIR TASK 25-15-62-300-802 3. REPAIR PROCEDURE

NOTE : In addition to the following details, the operators could use the FAA standard AC43-13 ´Acceptable methods, techniques and practices - Aircraft Inspection and repairª as acceptable minor repair procedures after being submitted to Sicma Aero Seat then approved.

A. Scouring :

WARNING : USE SYDOL SID IN VENTILATED AREA WITH RUBBER GLOVES,AND GLASSES.

- To scour paint from metal parts, use SYDOL SID. B. Protection : - Before application, each part must to be cleaned thoroughly. - To protect zones not to be painted, use masking tape. C. VELCRO : In the event that any velcro which is bonded to metal or plastic has come loose it should be replaced. For best results remove the entire piece, clean the exposed surface (see chapter “CLEANING“, §3 “PROCEDURE“ page 4002) and wipe dry with clean cotton cloth. Install a new piece of velcro according to manufacturers instructions. D. Paint : Repaint each part after inspection according to assembly of colors to figure 6002. Some plastic part may be painted after repair. The spot repainting diameter can not exceed 1 inch. The coating must be submitted to SICMA for approval before using. E. Corrosion and protection : 1. Corrosion elimination : Sand lightly the corroded surfaces with an abrasive paper (grit P 600), until complete disappearing of the corrosion. If necessary use an abrasive paper (grit P 400) or less.

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 6005 132-SERIES REPAIR CAUTION : BE CAREFUL NOT TO DETERIORATE THE CORRODED PART BY A TOO IMPORTANT SANDING.

2.Treated surfaces protection : Protect the sandfaces with a anti-corrosive film. (ex. ARDROX 396/1) F. RIVETED ASSEMBLIES : (1) Removal : (a) It is recommended that a small center drill be used to provide a guide for a larger drill on top of the rivet, and the upper portion of the stem be drilled Small away to destroy the lock. Center drill a) (b) Drive out the rivet stem, using a tapered steel drift pin, or spent stem.

Drift pin b) (c) Drill nearly through the head of the rivet, using a drill the same size as the rivet shank. c)

(d) Break off rivet head, using a drift pin as a pry. d)

(e) Drive out the remaining rivet shank with a pin having a diameter equal to the rivet e) shank.

Figure 6001

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 6006 132-SERIES REPAIR

CAUTION : DO NOT DRILL COMPLETELY THROUGH THE RIVET SLEEVE TO REMOVE A RIVET AS THIS WILL TEND TO ENLARGE THE HOLE.

2.Rivet installation : Before installing new rivets, check the size of the hole to determine if the original fastener size may be reinstalled or if an oversize fastener will be required. Use the aircraft structural repair manual or FAA document EA-AC65-15A, "Airframe and Powerplant Mechanics Hand-book" to make this determination and install the new fastener in accordance with these documents. 3.Rivet Removal : (secondary structure only) Should it be necessary to remove any solid rivet, the work is to be accomplished in accordance with the aircraft structural repair manual or FAA document EA-AC5-15A, "Airframe and Powerplant Mechanics Handbook". Should it be necessary to remove any blind rivet, the work should be accomplished in accordance with the preceding recommended procedure as shown in figure 6001 (a thru e).

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 6007 132-SERIES REPAIR

Assembly of Colors Figure 6002 (sheet 1)

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 6008 132-SERIES REPAIR

ITEM NOMENCLATURE MATERIAL FINISH COLOR 5 STRUCTURE BASIC 2017 A PAINTING MAROON 357-7-301 10 COVERS FABRIC WHITE H001* 15 FAIRING MISCELLANEOUS PC FALMOUTH WHITE H041* 20 CONTROL PUSH BUTTON 2017 A ANODIZED NATURAL 4-08-00 25 ARMCAP FABRIC WHITE H001* 30 ASHTRAY SST BRUSHED NATUREL 01-220

(*) "Color code to be added at the end of the P/N for ordering" Assembly of Colors Figure 6002 (sheet 2)

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 6009 132-SERIES ASSEMBLY ASSEMBLY

TASK 25-15-62-400-801 1. GENERAL A. Before assembly, verify that the CLEANING, RECOMMENDED CHECKS and the REPAIR of all component parts have been carried out. B. After repair or replacement of any damaged or worn parts, reassemble the seat assembly following accepted workshop practices, noting the following detailed instructions. Use a tracking fixture to support the seat structure. C. Refer to the illustrations in the Illustrated Parts List for location, sequence, quantity and identification of assemblies, sub-assemblies and parts. These illustrations are also intended as a guide line for the assembly procedure. D. Whenever possible, replace low cost items during reassembly to prevent possible future maintenance work as a result of failure of these parts. E. The self-locking nuts and pins shall systematically be replaced after a dismantling operation. TASK 25-15-62-940-801 2. LIST OF MATERIALS:

NOTE : Equivalent replacement products may be used to replace those listed.

MATERIAL IDENTIFICATION SOURCE APPLICATIONS

ADHESIVE AGOBOIS BT BOSTIK S.A. Solid wood, laminated white R.N. 19 panels, plating (within ( supersede 77170 COUBERT only) VINYL BT) FRANCE

ADHESIVE AGOBOIS PU BOSTIK S.A. Wood on all support color white R.N. 19 (at external) 77170 COUBERT FRANCE

ADHESIVE AGOPLAC DI BOSTIK S.A. Laminated on usual amber R.N. 19 support ( supersede 77170 COUBERT NEOPRENE DIR) FRANCE

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 7001 132-SERIES ASSEMBLY MATERIAL IDENTIFICATION SOURCE APPLICATIONS ADHESIVE LOCTITE n∞401 LOCTITE Corporation Elastomer, metal, plastic colorless 705, West Mountain Road Newington, Conn. 06111 U.S.A. ADHESIVE LOCTITE n∞416 LOCTITE Corporation Elastomer, metal, plastic colorless 705, West Mountain Road Newington, Conn. 06111 U.S.A. ADHESIVE LOCTITE n∞421 LOCTITE Corporation Elastomer, metal, plastic clear colorless liquid 705, West Mountain Road Newington, Conn. 06111 U.S.A. ADHESIVE LOCTITE n∞601 LOCTITE Corporation Elastomer, metal, plastic green, fluorescent 705, West Mountain Road liquid Newington, Conn. 06111 U.S.A. ADHESIVE LOCTITE n∞638 LOCTITE Corporation Elastomer, metal, plastic green, fluorescent 705, West Mountain Road liquid Newington, Conn. 06111 U.S.A. ADHESIVE LOCTITE n∞648 LOCTITE Corporation Elastomer, metal, plastic green, fluorescent 705, West Mountain Road liquid Newington, Conn. 06111 U.S.A.

ADHESIVE M 890 BOSTIK S.A. Metal surface, PVC colorless R.N. 19 77170 COUBERT FRANCE

ADHESIVE METHYLENE ELF ATOCHEM S.A. Miscellaneous fairing, CHLORIDE 4 cours Michelet Cedex 42 cocktail table, 92091 PARIS LA DEFENCE 10 tray in polycarbonate only FRANCE

ADHESIVE MONTAPRENE BOSTIK S.A. Armcap, foam on sheet 2796 R.N. 19 metal ( supersede 77170 COUBERT Neoprene) FRANCE

ADHESIVE SILICOMET AS310 LOCTITE FRANCE Sealing, joint realization ( supersede 10 Avenue Eugene Gazeau Loctite 5366) BP 96 60304 SENLIS Cedex FRANCE

ADHESIVE SICOMET 7000 PIROT RUTARD Aluminium, steel, brass, colorless INDUSTRIE ABS fairing only (supersede 22, rue Combanaire OMNIFIT 7000) 36000 CHATEAUROUX FRANCE

List of Materials Table 7001 (sheet 2)

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 7002 132-SERIES ASSEMBLY MATERIAL IDENTIFICATION SOURCE APPLICATIONS

ADHESIVE SICOMET 8300 PIROT RUTARD Aluminium, steel, brass INDUSTRIE 22, rue Combanaire 36000 CHATEAUROUX FRANCE

ADHESIVE TRANSPRENE K11 BOSTIK S.A. Leather, rubber, color amber R.N. 19 elastomer, wood, 77170 COUBERT composition material FRANCE

ADHESIVE TAPE ALUMINIUM FOIL 3M France Sealing of cavities TAPE Boulevard de l’Oise (Optional) 425 x 2 in 95006 CERGY PONTOISE Cedex FRANCE

ADHESIVE TAPE DOUBLE COATED 3M FRANCE Fairing, TAPE Boulevard de l’Oise structure armrest, 9573 High 95006 CERGY PONTOISE cocktail table Performance Cedex FRANCE

CLEANER ISOPROPYL PROLABO metal surface, grease and ALCOHOL 54, rue Roger Salengro oil. BP 115 94126 FONTENAY-SOUS- BOIS Cedex FRANCE

CLEANER GRAIN PROLABO metal surface, grease and ALCOHOL 54, rue Roger Salengro oil. (ETHANOL) BP 115 94126 FONTENAY-SOUS- BOIS Cedex FRANCE

CLEANER SYDOL SID SOCIETE INDUSTRIELLE DE Miscellaneous fairing, DIFFUSION escutcheon hostess step, B.P. 118 step stirrup, 94003 CRETEIL Cedex ashtray, foodtray, FRANCE in arm table

DE-RUSTER ARDROX 396/1 BRENT S.A. Rust point 280 rue J.B. Godin 02200 VILLENEUVE ST GER- MAIN FRANCE

GREASE ALVANIAG SHELL Greaser on technical seat 89, Bld Franklin Roosevelt 92564 RUEIL- MALMAISON FRANCE List of Materials Table 7001 (sheet 3)

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 7003 132-SERIES ASSEMBLY MATERIAL IDENTIFICATION SOURCE APPLICATIONS

LUBRICANT WD40 AEROSOL WD-40 COMPANY LTD Sliding mechanism P.O. Box 440, MILTON KEYNES, BUCKS MK113LF ENGLAND

NON SLID material AF6/1472 AEROFLOOR LTD Pads covering (PIMPLE) 3 Commerce way, Whitehall Industrial Estate, CO2 8HR COLCHESTER NON SLID material AF6/1499 AEROFLOOR LTD Pads covering (3mm diameter 3 Commerce way, STUD) Whitehall Industrial Estate, CO2 8HR COLCHESTER SEALANT, High LOCTITE n∞290 LOCTITE Corporation Parts already assembled Temperature 705, West Mountain Road Retaining Newington, Conn. 06111 U.S.A. SEALANT, High LOCTITE n∞222 LOCTITE Corporation Brake filet for screw, nut, Temperature purple (low) 705, West Mountain Road shoulder shaft Retaining Newington, Conn. 06111 U.S.A. SEALANT, High LOCTITE n∞243 LOCTITE Corporation Brake filet for screw, nut, Temperature blue (normal) 705, West Mountain Road shoulder shaft Retaining Newington, Conn. 06111 U.S.A. SEALANT, High LOCTITE n∞270 or LOCTITE Corporation Brake filet for screw, nut, Temperature n∞2701 705, West Mountain Road shoulder shaft Retaining green (strong) Newington, Conn. 06111 U.S.A.

List of Materials Table 7001 (sheet 4)

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 7004 132-SERIES ASSEMBLY TASK 25-15-62-400-802 3. PROCEDURE NOTE :In order to avoid errors during assembly, refer to the marking or numbering of the component parts. Following the replacement of worn or damaged parts reassemble the seat as follows :

Subtask 25-15-62-420-001 A. ASSEMBLY CAUTION :

DURING ASSEMBLY, DO NOT FORGET THAT THE FOLLOWING CONTROLS: - INERTIA REEL (OPTIONAL), - BACKREST RECLINING, - HEIGHT ADJUSTMENT, - TRACK LOCKING, ARE MOUNTED ON THE RIGHT FOR THE PILOT SEAT AND ON THE LEFT FOR THE COPILOT SEAT. Subtask 25-15-62-420-002 B. ASSEMBLY OF LOWER STRUCTURE (REF. IPL, FIG. 8 AND 7) 1. Longitudinal members (Ref. IPL, Fig. 8) (a) Secure the front cross member to both longitudinal members (420) and (421), using the four screws (340), and secure by nuts (350), (b) Secure the rear cross member (390) using both screws (370). On each longitudinal member: (c) -install both aft pads (290&300) and also both sleeve spacers (310) and rollers (320), (d) -Secure the assembly using both screws (240) and secure by nuts (230). 2. Arms and box structure (Ref. IPL, Fig. 8) Box structure Ref. IPL, Fig. 8: (a) Install both rollers (50) on the box structure, securing then with both pins (40). (b) Hold the box structure vertically and engage both rollers in their guide slots by turning the box structure. (c) Install both arms (see para. b).

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 7005 132-SERIES ASSEMBLY Arms Ref. IPL, Fig. 7: (d) Install the arm upon upper pin (100). (e) Secure the assembly by inserting pin (50). (f) Install roller (20) and secure it, using pin (10). (g) Insert central pin (40) into the box structure. (h) Secure the arm upon central pin (40), using retaining ring (30). (j) Perform the same operations for the second arm. Ref. IPL, Fig. 8: (k) Insert sleeve spacers (30) into the bores of both arms. (l) Secure both arms between the clevis lugs of the longitudinal members, using both screws (20) and nuts (10).

NOTE : Use new low cost items such as pins, screws, washers, nuts and tie-straps wherever possible during the reassembly procedures to prevent future repair requirements due to failure of these parts.

Subtask 25-15-62-420-003 C. ASSEMBLY SEAT-TO-RAIL LOCKING (REF. IPL, FIG. 8) (1) Secure control lever (180) to cross tube assembly (220). On each longitudinal member: (2) install bearing (270) in inner pad (280);install inner pad (280) and outer pad (250) upon the longitudinal menber. (3) secure the assembly using both screws (240), interposing both sleeve spacers (310) and rollers (320), (4) screw both nuts (230) over screws (240) and tighten them to secure the assembly, (5) insert cross tube assembly (220) between both bearings (270), (6) insert locking pin (130), complete with its spring (120), into the longitudinal member, (7) secure plate (100), using both screws (110), (8) install fork arms (80) upon cross tube assembly (220), (9) secure fork arms (80), using screws (90).

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 7006 132-SERIES ASSEMBLY NOTE : For a better accessibility and a correct monting, locate the seat at the end of the aircraft track then lift the lever to unlock and change the defective parts.

(10) install ring (70) and the retaining ring upon locking pin (130) then insert spring pin (60).

NOTE : Secure the attachment by using LOCTITE 222e on the thread of screws.

Subtask 25-15-62-420-004 D. ASSEMBLY OF THE BACKREST AND SEAT PAN (REF. IPL, FIG. 5, 6 AND 3) (1) Ref. IPL, Fig. 5: Install the backrest upon the seat pan. (2) Insert both hinge pins (220), fitting them with washers (230). (3) Install nuts (250) upon both hinge pins (220) and tighten them to secure the assembly. (4) Install the inertia reel assembly (see para. F). (5) Insert the threaded ends of hydrolocks (200 & 210) into yokes (170). (6) Secure the hydrolocks (200 & 210), using nuts (160) . (7) Ref. IPL, Fig. 6: Connect backrest inclination adjustment control assy (-380), to the hydrolock. (8) Ref. IPL, Fig. 3: Assemble the upper and lower structure (see para. J). Subtask 25-15-62-420-005 E. ASSEMBLY OF ARMREST ASSEMBLY (REF. IPL, FIG. 3) (1) Secure upper armrest (150) to slide (290), using screws (160 and 170). (2) While depressing lever (240), install slide (290) complete with lever (240) over support (300). (3) Install pin (190), spring (200) and washers (210 and 220). (4) Fit one retaining ring (130) to pin (140), insert this pin and then fit a second retaining ring (130). (5) Fit a washer (80) to both screw (60) and hollow screw (70). (6) Secure fitting (90), using screw (60) and hollow screw (70). (7) Fit pushrod (430) to lever (480), using pin (420) and spring pin (410).

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 7007 132-SERIES ASSEMBLY (8) After fitting sleeve spacer (470) to lever (480), secure the lever to support (300), using screw (440) complete with washer (450) and placing a washer (460)on each side of lever (480). (9) Place rubber bushing (330) upon control rod assembly (400) and secure it using screw (310) and washer (320) (10) At the opposite end, slide on spring (390) and install it using washer (380) and retaining ring (370). (11) Install the thus-assembled control rod assembly upon support (300) and secure it using screws (360).

NOTE : During this operation,observe the correct position of the tab of the control rod assembly relative to the end of cam bearing (490).

Subtask 25-15-62-420-006 F. ASSEMBLY OF RESTRAINT SYSTEM (REF. IPL, FIG. 1 AND 5) (1) Ref. IPL, Fig. 1: Secure reel assembly (50 to backrest structure, using the four screws (60) and secure by nuts (70). (2) Secure the belts to seat structure , using the two screws (40).

NOTE : The armrest fairing are fixed on the armrest structure by sticking.

(3) Ref. IPL, Fig. 5: Attach backrest fairing (130) with both screws (70) then place sleeves (10).

Subtask 25-15-62-420-007 G. ASSEMBLY OF ELECTRICAL ASSEMBLY (REF. IPL, FIG. 8 AND 1) Ref. IPL, Fig. 8: (1) Locate a shim washer, of suitable thickness to provide the play measured during disassembly, behind rollers (50 (minimum play of 0.5 mm (0.0196 in.)). (2) Offer up the actuator upon the grease end fitting and screw in actuator until both screws (380) can freely enter their holes in the actuator. (3) Screw in both screws (380) and tighten them to secure ; inject grease AIR 4222 into the hipple of the grease end fitting. Ref. IPL, Fig. 8: (4) Before tightening the nut, check the play between the guide slot of the longitudinal member and roller (50), and check the range of adjustment of the actuator .

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 7008 132-SERIES ASSEMBLY

(5) The end of the actuator operating range must be reached before the roller reaches the end of the guide slot; the play must be at least 0.5 mm (0.0196 in.)). (6) Tighten the lock-nut to a torque of 1.5 daN.m (11.06 ft.lb.). (7) Safety-lock the assembly by bending the tab of the tab washer through 90∞. Ref. IPL, Fig. 1: (8) Secure cable (150) underneath the structure of the seat pan using loop clamps (130) and secure by rivets (140). (9) Secure the control switch to its support, using both screws. (10) Make the various connections.

Subtask 25-15-62-420-008 H. ASSEMBLY OF RECLINE ACTUATOR AND CONTROL (REF. IPL, FIG. 5 AND 6) For each actuator (Ref. IPL, Fig. 5) (1) - install lock-nut (160) upon the threaded end of actuator (200). (2) - insert the threaded end of the actuator in yoke (170) and secure the yoke, using nuts (160). (3) - secure the assembly consisting of yoke (170) and actuator (200) to the clevis, using both attaching screws (140) . Ref. IPL, Fig. 6: (4) - secure the actuator to the backrest structure, using screw (190), fitted with nut (180). Ref. IPL, Fig. 5: (5) - tighten both washer (140) and both nuts (160), Ref. IPL, Fig. 6: (6) - secure and connect backrest inclination adjustment control assy (-380).

NOTE : Before installing actuator ensure that it is in the fully exended position.

Subtask 25-15-62-420-009 J. ASSEMBLY OF THE UPPER AND LOWER STRUCTURES (REF. IPL, FIG. 6) (1) Install the upper structure upon the lower structure, inserting the upper rollers of the arms in the guide slots of the seat pan.

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 7009 132-SERIES ASSEMBLY (2) Insert the free end of the box structure arms into support (70). (3) Locate sleeve bushings (130) and insert both hinge screws (80). (4) Secure both hinge screws (80) using nuts (90).

Subtask 25-15-62-420-010 K. ASSEMBLY OF MISCELLANEOUS AFT COVERS (REF. IPL, FIG. 1) (1) Attach the side fairings (30 & -31) on the lateral spreaders with screws (40 & 90) and spacers (100).

Subtask 25-15-62-420-011 L. ASSEMBLY OF UPHOLSTERY (REF. IPL, FIG. 2 & 9) (1) Ref. IPL, Fig. 2: Thread the bottom cover (10) on the bottom cushion (5) and fix on the bottom sheet metal. (2) Thread the backrest cover (20) on the backrest cushion (15) and fix on the backrest structure. (3) Ref. IPL, Fig. 9:Thread the headrest cover (15) on the headrest cushion (10) and fix on the backrest structure.

NOTE : The cushions are fixed with "VELCRO".

Subtask 25-15-62-420-012 M. ASSEMBLY OF HEADREST ASSEMBLY (REF. IPL, FIG. 9) (1) Install the headrest assy (-1) into the sleeves of backrest structure.

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 7010 132-SERIES FITS AND CLEARANCES FITS AND CLEARANCES

1. TABLE OF FITS AND CLEARANCES. A. Layout (1) The table of fit and clearances indicates the machining tolerances for new parts and the wear limits acceptable for a further period of operation. (2) The numbers in the first column indicate the position of the clearance or dimension to be measured. (3) The item numbers in the second column correspond to the item numbers in the IPL. B. Maximum permissible (Max. after wear) (1) "MAX. PERMISSIBLE" means the maximum wear limits. These limits are determined so that re-installed parts can be used for the period between two overhauls.

NOTE : During overhaul which gives the unit a new service life,and especially for parts ensuring precision guidance of moving components, the repair facility should endeavor to keep clearances within those of new parts.

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 8001 132-SERIES FITS AND CLEARANCES

Fits and Clearances Table 8001 (Sheet 1)

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 8002 132-SERIES FITS AND CLEARANCES

Fits and Clearances Table 8001 (Sheet 2)

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 8003 132-SERIES FITS AND CLEARANCES

Fits and Clearances Figure 8002 (Sheet 1)

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 8004 132-SERIES FITS AND CLEARANCES

Fits and Clearances Figure 8002 (Sheet 2)

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 8005 132-SERIES FITS AND CLEARANCES

Fits and Clearances Figure 8002 (sheet 3)

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 8006 132-SERIES SPECIAL TOOLS, FIXTURE AND EQUIPMENT

SPECIAL TOOLS, FIXTURE AND EQUIPMENT

TASK 25-15-62-940-801 1. GENERAL No special fixture or specific equipment are required for maintenance or overhaul work to be carried out on the seat. However, a fixture simulating aircraft seat-track locations is recommended for extensive seat maintenance conducted outside the aircraft. TASK 25-15-62-940-802 2. SPECIAL TOOLS No special tools or specific equipment are required for maintenance or repairs to the passenger. Standard tools are sufficient for these operations.

TASK 25-15-62-940-803 3. SPECIAL EQUIPMENT A. SICMA propose the Adjustment Bench P/N 03001-0-00 to be adjust the seat electrical motors.

B. SICMA propose the platform P/N D11-0029 to install the seat assy on the tracks.

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 9001 132-SERIES ILLUSTRATED PARTS LIST

ILLUSTRATED PARTS LIST

TASK 25-15-62-950-801 1. INTRODUCTION This illustrated parts list (IPL) contains the complete listing of all replaceable parts of the seat assy. The introduction contains all explanatory information for the individual sections as is necessary for the use of this IPL. The introduction also contains a list of abbreviations used in the detailed parts list as well as a list of manufacturer codes, together with manufacturer names and addresses. TASK 25-15-62-990-801 2. ALPHANUMERICAL INDEX This section contains a listing of part numbers of all items listed in the detailed parts list in alpha-numerical sequence with cross reference to respective Fig. / Item Nos. as well as units per assy. The order of precedence in beginning the part number arrangement at the extreme left-hand (first) position is as follows : - Letters A through Z ("0" to be considered as zero), - Numerals 0 through 9. For subsequent rows, the order is : - A dash, - Letters A through Z ("0" to be considered as zero), - Numerals 0 through 9. TASK 25-15-62-950-802 3. DETAILED PARTS LIST A. Column FIG. / ITEM : The first number in the first line of a page indicates the number of the figure illustrating the part, the second number indicates the item number by which the part is identifiable on the illustration. A dash placed before the item number indicates that the part is not illustrated. B. Column PART NUMBER : The part number column contains the original manufacturer part number. When standard parts are used, the standard part number is listed in this column. C. Column AIRLINE STOCK NO : This column is left blank for airline internal use.

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 10001 132-SERIES ILLUSTRATED PARTS LIST D. Column NOMENCLATURE : (1) Indenture System The indenture system shows the relationship of parts and assemblies to next higher, assemblies or installations, as follows : 1234567 Assembly or installation assembly RF number. Attaching parts for assembly or installation. *** .Detail parts for assembly .Sub-Assembly Attaching parts for sub-assembly *** ..Detail parts for sub-assembly ..Sub-sub-assembly Attaching parts for sub-sub-assembly *** ...Detailed parts for sub-sub-assembly etc. (2) Attaching Parts Attaching parts are captioned ATTACHING PARTS and are listed imme- diately following the parts attached. The *** symbol follows the last item of the attaching parts group. (3) Vendor Code Parts manufactured by companies other than SICMA are identified by an appropriate vendor code following the nomenclature. Vendor codes are in accordance with current issues of Federal Supply Codes for manufacturers Cataloguing Handbooks H4-1, H4-2 and H4-3 and are preceded by the letter "V". Standard parts such as AN, MS etc... are not identified by a vendor code. (4) SICMA code Under each attaching parts, we indicate the Sicma Part Number, in brackets.This P/N must be given when ordering these parts, together with the color code if applicable (Hxxx) from page 6009 (Assembly of colors). (5) Wires (Fig.1) All the AVIAC parts must be ordered directly from them.

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 10002 132-SERIES ILLUSTRATED PARTS LIST E. Column EFFECT CODE : The Effectivity Code column establishes parts relationship with units or assemblies which are essentially the same but have minor deviations. These units or assemblies are assigned reference letters such as A, B, C etc. If required, the succession will follow BA, CA, DA, EA, ...ZA, CB, DB, EB, ...ZB, DC, EC, FC, ...ZC, ED, FD, etc.Parts which are not common to all configurations but are associated with one or more of the coded lead items, carry the letter or letters assigned to the lead item with which it is associated. Where a part is common to all lead items, the effectivity column is left blank. The successive letters such as A,B,C,D,E are notified A-E. F. Column UNITS PER ASSY This column contains the quantity of a part required in the build sequence of only one sub-sub-assembly, sub-assembly, assembly, or installation level as applicable. Where items are listed for reference purpose, ´RFª is inserted. G. PARTS NUMBER CODIFICATION (1) Standard Parts Number Standard international standard Parts number is mentioned in Part Number column : i.e. NAS601-5 Internal Sicmaís standard Parts number codification is mentioned in Nomenclature column : (VINAS6015) like vendor code Thus, VINAS6015 = NAS601-5 VI means Screw EC means Nut POP means Pop Rivet R0 means Washer EE means Electrical Equipment RI means Rivet CI means Circlip CO means Collar etc. Examples : VIAN412A = AN4-12A R0AN960416 = AN960-416 These Parts number are two-way interchangeable. (2) Sicmaís Parts Number Standard Sicmaís Parts number codification is 2 digits - 6 digits - 3 digits - 1 digit : i.e. P/N XX-xxxXXX-xxx-X Thus, P/N XX-xxxXXX-xxx-X = P/N XX-xxxXXXAxxx-X Example : P/N 50-000610-024-0 = P/N 50-000610A024-0 These Parts number are two-way interchangeable.

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 10003 132-SERIES ILLUSTRATED PARTS LIST (3) Screws codification

SICMA reference with correspondence P/N Normalized of screw reference :

XXXX * MEANS THE THREAD AND THE LENGTH OF THE SCREW :

EXAMPLE : DIN912 1/4NF X 5/8 = CHC 1/4NF X 5/8

- 1/4NF (INCH VALUE) : THREAD DIAMETER

- X 5/8 (INCH VALUE) : LENGTH UNDER HEAD

. FOR SCREW BHC AND CHC (SEE DIMENSIONS A) . TOTAL LENGTH FOR SCREW FCH,HCBPL, HCBPT, HCBTT, HCBC (SEE DIMENSIONS B)

NOTE : These parts number are two-way interchangeable.

TASK 25-15-62-950-803 4. HOW TO USE THE PARTS LIST A. THE PART NUMBER IS KNOWN (1) Find the part number in the numerical index. Note figure and item number. (2) Turn to the figure. (3) Locate the part on illustration and in the parts list by item number. B. THE PART NUMBER IS UNKNOWN (1) Refer to figure 1 and look for the title of figure in which the part should be shown. (2) Note the figure number. (3) Turn to the illustration and find the part.

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 10004 132-SERIES ILLUSTRATED PARTS LIST (4) Refer to corresponding item number in the parts list. C. SEAT COLOR (1) Refer to color code section in CMM for color code example (xxx) page 6009. TASK 25-15-62-980-801 5. LIST OF VENDORS CODE NAME AND ADDRESS VD8286 DIN DEUTSCHES INSTITUT FUER NORMUNG E.V. KAMEKESTRASSE 2-8 50672 KOELN ALLEMAGNE VF0110 AFNOR (ASSOCIATION FRANCAISE DE NORMALISATION TOUR EUROPE 92049 PARIS LA DEFENSE CEDEX FRANCE VF0111 BNAE (BUREAU DE NORMALISATION DE LíAERONAUTIQUE ET DE LíESPACE) 199 R JEAN JACQUES ROUSSEAU 92138 ISSY LES MOULINEAUX FRANCE VF0217 PRECISION MECANIQUE LABINAL SA B.P. 64 78390 BOIS DíARCY FRANCE VF0224 SIMMONDS SA 9 R DES CRESSIONNIERES 72110 SAINT COSME EN VAIRAIS FRANCE VF0313 MECANINDUS SA 8 MAIL JOLIOT CURIE Z.I. VERT GALANT 95310 ST OUEN LíAUMONE FRANCE VF0344 GOUPILLE CANNELEE (LA) íL.G.C.í SA B.P. 4 49240 AVRILLE FRANCE VF0349 NOMEL SA TOUR FRANKLIN 92081 PARIS LA DEFENSE CEDEX 11 FRANCE VF0368 MANUFACTURE FRANCAISE DíOEILLETS METALLIQUES SA íM.F.O.M.í 12 R TRUILLOT 94203 IVRY CEDEX FRANCE

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 10005 132-SERIES ILLUSTRATED PARTS LIST CODE NAME AND ADDRESS VF0396 AVIAC TECHNOLOGIES 15-19,Rue Louise MICHEL 78200 MANTES-LA-VILLE FRANCE VF0465 SICMA (STE INDUSTRIELLE ET COMMERCIALE DE MATERIEL AERONAUTIQUE) 7 Rue LUCIEN COUPET 36100 ISSOUDUN FRANCE VF0712 RAYMOND SA 113 COURS BERRIAT 38028 GRENOBLE FRANCE VD8527 HELLERMANN PAUL COMPANY Electronic, Special tools Siemenstrasse 5 2080 PINNEBERG GERMANY VF3349 LA DAUPHINOISE SA (MANUFACTURE DíARTICLES METALLIQUES ET PLASTIQUES) 6-8 AV GENERAL DE GAULE 38800 PONT DE CLAIX FRANCE VK0017 TUCKER FASTENERS LTD WALSALL ROAD BIRMINGHAM B42 1BP ROYAUME-UNI V02953 P.L PORTER COMPANY 6355 DE SOTO AVENUE WOODLAND HILLS CALIFORNIA 91364 USA V45402 PACIFIC SCIENTIFIC CO KIN-TECH DIVISION 1346 S STATE COLLEGE BLVD 92803 ANAHEIN USA V72962 ESNA DIV OF AMERACE CORP 2330 VAUXHALL ROAD UNION NJ 07083 ETATS-UNIS V80205 NATIONAL AEROSPACE STANDARDS COMMITTEE AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA INC 1250 EYE ST NW WASHINGTON DC 20005 ETATS-UNIS V88044 AERONAUTICAL STANDARDS GROUP DEPT OF NAVY AIR FORCE ETATS-UNIS

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 10006 132-SERIES ILLUSTRATED PARTS LIST CODE NAME AND ADDRESS V96906 MILITARY STANDARDS PROMULGATED BY MILITARY DEPARTMENTS UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M ETATS-UNIS

TASK 25-15-62-950-804 6. UPDATING When an item is revised, added or deleted, a vertical stoke is shown in the RH margin on RH pages, LH margin on LH pages (the column ´date of issueª changes on the revisions page). The vertical stoke appears in the RH margin opposite the page number when all the item numbers are changed. Minor editorial revisions such as spelling errors, punctuation etc., are not recorded or otherwise identified.

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 10007 TASK 25-15-62-970-801 132-SERIES ALPHANUMERICAL INDEX AIRLINE AIRLINE PART NUMBER FIG. ITEM QTY PART NUMBER FIG. ITEM QTY STOCK N∞ STOCK N∞ AN3-14A 4 120A 2 MS20364-832A 7 180A 6 AN3-5A 1 60A 4 MS24693C2 6 -430A 1 AN3-6A 3 440A 1 MS24693C5 5 90A 2 6 150A 2 MS27039-0812 3 -21A 1 AN316-6R 4 40A 2 MS27039-0814 3 20A 1 5 160A 4 MS27039-0818 7 160A 6 AN4-10A 4 20A 1 MU7 3 -321A 1 AN4-13A 6 330A 1 NAS1149D0516K 3 210A 1 AN4-14A 6 310A 1 NAS1149F0332P 3 450A 1 AN4-15A 6 80A 4 NAS1149F0632P 5 -150A 4 AN4-3A 3 310A 1 NAS1149F0732P 3 380A 1 AN4-7A 5 190A 2 NAS1149F0763P 3 -381A 1 AN509-10R7 8 110A 4 NAS1149FN816P 3 -461A 1 AN515-832R6 4 170A 4 NAS514P832-5 3 -530A 8 AN520-10R14 8 90A 2 NAS514P832-6 3 170A 2 AN525-10R16 8 200A 1 NAS514P832-8 3 40A 4 AN525-832R7 5 280A 7 3 -171A 2 AN525-832R8 3 -441A 1 NAS517-4-11 6 20A 2 AN526-632R4 2 30A 2 6 50A 2 AN526-632R9 2 80A 2 NAS601-4 3 -260A 2 AN526-832R8 5 70A 2 NAS602-6 3 -41A 4 AN565B10-32H3 6 -520A 1 3 160A 2 AN565F10-32H8 6 -481A 1 NAS679A08 6 320A 1 AN960-10L 4 130A 2 NAS679A3 1 70A 4 AN960-616 5 240A 2 4 140A 2 AN960-8 7 170A 6 NAS679A4 4 30A 1 AN960-8L 4 180A 4 5 100A 2 AN960-916L 3 -362A 1 5 180A 2 CHC1-4NFx5-8 3 -311A 1 NAS679A6 5 250A 2 6 250A 2 NAS680A8 3 -270A 1 CHC8NCx3-8 6 300A 1 N∞4 3 50A 4 D2M1QV060020AL 3 -100A 1 PLT1M-M 1 -152 1 DELETED 6 -340A 6 -526A 1 E1-5x15EMCD 3 410A 1 TAPD036BS 6 -527A 1 E2-5x14EMCD 8 60A 2 TLPD419BS 6 190A 9 E3x20EMCD 4 100A 2 7 270A 2 E3x25EMCD 6 210A 2 TLPD424BS 5 30A 4 EC6PH135M 8 230A 8 5 50A 4 F52NTE048 6 30A 2 6 160A 7 6 60A 2 6 -161A 12 6 90A 4 TLPD429BS 6 170A 2 FGFB910124001N1 1 150A 1 7 250A 2 FGFB910124002N1 1 -151A 1 TLPD435BS 7 230A 3 G07-3x26S250 6 -211A 2 V1,5x15AC 3 -411A 1 G07-8x30A 6 270A 2 V39-101-06 6 460A 1 G072,5x14 8 160A 4 V39-101-07-3 6 470A 1 H3P 1 130A 2 V39-101-08-3 6 480A 1 JFGA070UL 3 320A 1 V39-101-12 6 490A 1 LKCRNATUREL 6 -525A 1 V40-101-13 6 500A 1 LL-01500-10 5 210A 1 V40-101-3 6 -440A 1 MECAE3x20 7 50A 2 V40-301 6 390A 2 7 110A 4 V40-600 6 410A 2 MM-2010-61 3 400A 1 V40-800 6 -420A 1 MM-2010-62 3 401A 1 V57-401 6 400A 1

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 10009 132-SERIES ALPHANUMERICAL INDEX AIRLINE AIRLINE PART NUMBER FIG. ITEM QTY PART NUMBER FIG. ITEM QTY STOCK N∞ STOCK N∞ V57-Y-401-600-0 6 -380A 1 132100-2 1 -211A 1 VELCR016-10A 6 -541A 1 8 -2A RF VELCR020-10A 6 -531A 1 132101 8 330A 1 00-0021-1 3 420A 1 132102-01 8 150A 1 00-0521 3 200A 1 132102-02 8 170A 1 00-2612 6 450A 1 132102-03 8 180A 1 00-3316 1 -220A 1 132102-04 8 190A 1 052141 1 140A 2 132102-05-1 8 220A 1 110-1166-13 1 30A 1 132102-05-2 8 -221A 1 110-1167-09 1 -31A 1 132102-06 8 210A 1 128100-37 8 20A 2 132102-1 8 -140A 1 128100-48 8 301A 1 132102-2 8 -141A 1 128100-49 8 300A 1 132103 8 -260A 1 128100-50 8 291A 1 132103-01 8 280A 1 128100-51 8 290A 1 132103-02 8 281A 1 128500-23 5 140A 4 132104 8 -261A 1 128500-24 5 170A 2 132105-2 8 390A 1 132-01 1 11A 1 132115-1 8 -360A 1 2 -1A RF 132200-01 6 370A 1 132-02 1 -12A 1 132200-02 6 -361A 1 2 -2A RF 132200-03 6 360A 1 132-03 2 10A 1 132200-04 6 -371A 1 9 -1A RF 132200-05 6 10A 1 132050-100 1 -2A RF 132200-06 6 40A 1 132050-101 1 -6A RF 132200-07 6 350A 2 132050-103 1 -4A RF 132200-08 6 120A 1 132050-111 1 -8A RF 132200-09 6 110A 2 132050-113 1 -10A RF 132200-1 1 190A 1 132051-00023 1 100A 1 6 -1A RF 3 70A 1 132200-12 6 200A 1 132051-00025 1 110A 2 132200-18 6 290A 1 3 80A 2 132200-19 6 -291A 1 132051-100 1 -1A RF 132200-2 1 -191A 1 132051-101 1 -5A RF 6 -2A RF 132051-103 1 -3A RF 132200-57 6 220A 12 132051-111 1 -7A RF 132200-58 6 130A 1 132051-113 1 -9A RF 132200-63 6 180A 1 132100-01 8 -400A 1 132200-64 6 -530A 1 132100-011 8 420A 1 132200-65 6 -540A 1 132100-012 8 410A 1 132200-70 6 -231A 12 132100-02 8 -401A 1 132200-72 6 -141 1 132100-021 8 421A 1 132200-74 6 230A 12 132100-03 8 100A 2 132200-75 2 90A 2 132100-04 8 320A 2 132203 6 240A 2 132100-05 8 250A 2 132204 6 -260A 1 132100-06 8 310A 8 132204-01 6 280A 1 132100-07 8 80A 2 132206-01 6 70A 2 132100-08 8 70A 2 132206-02 6 100A 2 132100-09 8 130A 2 132207 6 140A 1 132100-1 1 210A 1 132208-1 1 -192A 1 8 -1A RF 6 -3A RF 132100-10 8 270A 1 132208-2 1 -193A 1 132100-11 8 380A 2 6 -4A RF 132100-12 8 321A 2 132208-58 6 -131A 1

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 10010 132-SERIES ALPHANUMERICAL INDEX AIRLINE AIRLINE PART NUMBER FIG. ITEM QTY PART NUMBER FIG. ITEM QTY STOCK N∞ STOCK N∞ 132209-1 1 -194A 1 132375-125-2 3 -401B 1 6 -5A RF 132375-126-0 3 -510A 1 132209-2 1 -195A 1 132375-130-1 3 -30B 1 6 -6A RF 132375-130-2 3 -31B 1 132260 1 20A 1 132375-140-1 3 -550A 1 95A1132375-140-2 3 -551A 1 132300-01 5 230A 2 132380 1 -81A 1 132300-02 5 220A 2 3 -2A RF 132300-03 1 40A 2 132381 3 301A 1 132300-1 1 180A 1 132400-001 1 170A 1 5 -1A RF 4 -1A RF 132300-11 5 10A 2 132400-01 4 90A 2 132300-2 1 -181A 1 132400-02 4 60A 2 5 -2A RF 132400-03 4 80A 2 132301 5 260A 1 132400-04 4 50A 1 132301-09 5 300A 2 132400-20 4 10A 1 132301-15 5 290A 3 132401 4 110A 1 132301-20 5 270A 1 132402 4 290A 1 132302-1 5 20A 1 132403 4 190A 1 132302-2 5 40A 1 132403-01 4 230A 1 132303-0 5 -61A 1 132403-02 4 200A 1 132303-01 5 130A 1 132403-03 4 250A 1 132303-02 5 -131A 1 132403-04 4 240A 1 132303-03 5 110A 2 132403-05 4 280A 1 132303-1 5 -60A 1 132500 1 200A 1 132315-150-0 3 -560A 1 7 -1A RF 132370 1 80A 1 132500-01 7 40A 2 3 -1A RF 132500-02 7 10A 2 132371 3 300A 1 132500-03 8 40A 2 132371-31 3 350A 1 132500-04 7 20A 2 132371-32 3 340A 1 132500-05 8 50A 2 132374 3 150A 1 132500-25 5 200A 1 132375-000-1 1 -80B 1 132520 7 -60A 2 3 -3A RF 132520-01 7 90A 2 132375-000-2 1 -81B 1 132520-02 7 70A 1 3 -4A RF 132530 7 100A 1 132375-010-0 3 -141A 1 132530-01 7 130A 1 132375-100-1 3 300B 1 132530-02 7 120A 2 132375-100-2 3 301B 1 132540 7 -150A 1 132375-110-1 3 -291A 1 132540-01 7 200A 1 132375-110-2 3 -291B 1 132540-02 7 190A 2 132375-115-1 3 -481A 1 132550 7 140A 1 132375-115-2 3 -481B 1 132601 1 -120A 1 132375-116-0 3 -490A 1 132602 1 -121A 1 132375-118-0 3 -431A 1 132710 2 50A 1 132375-119-0 3 -11A 1 132712 2 -51A 1 132375-120-1 3 -90B 1 132720 2 70A 1 132375-120-2 3 -91B 1 132722 2 -71A 1 132375-122-1 3 -520A 1 132730-001 2 40A 1 132375-122-2 3 -521A 1 132732-001 2 -41A 1 132375-123-0 3 -341A 1 132740-001 2 60A 1 3 -540A 1 132742-001 2 -61A 1 132375-124-0 3 -500A 1 132780-1 2 20A 1 132375-125-1 3 -400B 1 132780-2 2 -21A 1

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 10011 132-SERIES ALPHANUMERICAL INDEX AIRLINE AIRLINE PART NUMBER FIG. ITEM QTY PART NUMBER FIG. ITEM QTY STOCK N∞ STOCK N∞ 132784-1 2 -20B 1 700-10SEP25/100 3 -363A 1 132784-2 2 -21B 1 7002113 5 120A 4 142760 9 10A 1 7133D10 3 -371A 1 147100-19 8 120A 2 7133D16 7 30A 2 21215ID3208A 4 210A 8 7133D5 6 510A 1 21217DE2406A 3 -280A 2 7144D5 3 -131A 2 22208BC050014L 8 340A 4 79A8F27470 5 80A 1 22208BC060012L 8 370A 2 8260 1 160A 1 22271BC060046L 8 240A 6 863100-09 3 370A 1 22271BC060048L 8 241A 2 8TA10BE 8 10A 2 23111AA030L 4 220A 8 23134DG080D 4 70A 2 23203AM0050T 3 130A 2 2B25A3X03 1 50A 1 341-710-03 4 260A 2 363-730-08 4 270A 1 376-100-19 8 30A 2 376-135-03 7 80A 2 376-143 7 210A 1 394-10-162 7 220A 1 394-10-165-03 7 260A 1 394-10-165-07 7 240A 1 394-10-310-07 3 390A 1 394-10-310-11 3 140A 1 394-10-310-14 3 -71A 1 394-10-310-15 1 90A 1 3 60A 1 394-10-310-32 3 -81A 2 394-10-310-35 3 230A 1 394-10-313-07 3 250A 1 394-10-317-07 3 -110A 2 394-10-354-07 3 360A 2 394-10-354-09 3 330A 1 394-10-354-10 3 -361A 1 394-10-370-15 3 10A 1 394-10-371-09 3 430A 1 394-10-371-11 3 460A 2 394-10-371-25 3 470A 1 394-10-372 3 90A 1 394-10-372-01 3 -120A 1 394-10-373 3 -180A 1 394-10-373-01 3 290A 1 394-10-373-06 3 220A 1 394-10-373-11 3 190A 1 394-10-376 3 30A 1 394-10-378 3 480A 1 394-10-379 3 240A 1 394-10-382 3 91A 1 394-10-382-01 3 -121A 1 394-10-386 3 31A 1 394-10-800-001 9 15A 1 394-13-200-12 4 150A 2 394-13-200-13 4 160A 2 5PH135M 8 350A 4

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90 100 110

11 20

180

170 70

50 81 80

60 11 190

40 160

30 150 130 210 200 140

Pilot Seat Assy Figure 1

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 10020 132-SERIES

DETAILED PARTS LIST UNITS AIRLINE EFFECT. FIG. ITEM PART NUMBER 1234567 NOMENCLATURE PER STOCK N∞ CODE ASSY. 1 -1A 132051-100 SEAT,PILOT,ASSEMBLY (LH) RF (WITH LUMBAR-REST) (OPTIONAL) -2A 132050-100 SEAT,COPILOT,ASSEMBLY (RH) RF (WITH LUMBAR-REST) (OPTIONAL) -3A 132051-103 SEAT,PILOT,ASSEMBLY (LH) RF (HUD-EASY VERSION) -4A 132050-103 SEAT,COPILOT,ASSEMBLY (RH) RF (HUD-EASY VERSION) -5A 132051-101 SEAT,PILOT,ASSEMBLY (LH) RF (HUD VERSION) -6A 132050-101 SEAT,COPILOT,ASSEMBLY (RH) RF (HUD VERSION) -7A 132051-111 SEAT,PILOT,ASSEMBLY (LH) RF (HUD VERSION) (WITH FIVE CROTCH STRAP) -8A 132050-111 SEAT,COPILOT,ASSEMBLY (RH) RF (HUD VERSION) (WITH FIVE CROTCH STRAP) -9A 132051-113 SEAT,PILOT,ASSEMBLY (LH) RF (HUD-EASY VERSION) (WITH FIVE CROTCH STRAP) -10A 132050-113 SEAT,COPILOT,ASSEMBLY (RH) RF (HUD-EASY VERSION) (WITH FIVE CROTCH STRAP) 11A 132-01 .COVERING,ASSEMBLY 1A 2A 1 (NOT PROCURABLE) SEE 251562-02 -001A FOR DET -12A 132-02 .COVERING,ASSEMBLY 3A 4A 5A 1 (NOT PROCURABLE) 6A 7A 8A SEE 251562-02 -002A FOR DET 9A 10A 20A 132260 .STRUCTURE,HEADREST 1 30A 110-1166-13 .STRAP,WEBBING (LH) 1A 3A 5A 1 (V45402) 7A 9A -31A 110-1167-09 .STRAP,WEBBING (RH) 2A 4A 6A 1 (V45402) 8A 10A ATTACHING PARTS 40A 132300-03 .SCREW,SHOULDERED 2 *** 50A 2B25A3X03 .REEL,INERTIAL (V45402) 1 ATTACHING PARTS 60A AN3-5A .SCREW (V88044) 4 70A NAS679A3 .NUT,PLAIN,HEXAGON (V80205) 4 *** 80A 132370 .ARMREST,ASSEMBLY (LH) 1A 2A 3A 1 SEE 251562-03 -001 FOR DET 5A 6A 7A 8A 9A 10A

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 10021 132-SERIES

DETAILED PARTS LIST UNITS AIRLINE EFFECT. FIG. ITEM PART NUMBER 1234567 NOMENCLATURE PER STOCK N∞ CODE ASSY. 1 -80B 132375-000-1 .EASY ARMREST,ASSY (LH) 4A 10A 1 SEE 251562-03 -004 FOR DET -81A 132380 .ARMREST,ASSEMBLY (RH) 1A 2A 4A 1 SEE 251562-03 -002 FOR DET 5A 6A 7A 8A 9A 10A -81B 132375-000-2 .EASY ARMREST,ASSY (RH) 3A 9A 1 SEE 251562-03 -003 FOR DET ATTACHING PARTS 90A 394-10-310-15 .SCREW 1 100A 132051-00023 .BOLT,INTERNALLY RELIEVED 1 BODY 110A 132051-00025 .WASHER 2 *** -120A 132601 .EQUIPMENT,ELECTRICAL (LH) 1A 3A 5A 1 7A 9A -121A 132602 .EQUIPMENT,ELECTRICAL (RH) 2A 4A 6A 1 8A 10A 130A H3P ..CLAMP,LOOP (VD8527) 2 ATTACHING PARTS 140A 052141 ..RIVET PLASTIC (VF0712) 2 *** 150A FGFB910124001N1 ..CABLE ASSEMBLY,SPECIAL 120A 1 PURPOSE,ELECTRICAL (LH) (VF0217) -151A FGFB910124002N1 ..CABLE ASSEMBLY,SPECIAL 121A 1 PURPOSE,ELECTRICAL (RH) (VF0217) -152 PLT1M-M ..COLLAR (C0PLT1M-M) 120A 1 121A *** 160A 8260 ..JACK,ELECTRICAL (VF0396) 1 170A 132400-001 .LUMBAR REST,ASSEMBLY 1A 2A 1 (OPTIONAL) SEE 251562-04 -001A FOR DET 180A 132300-1 .BACKREST,ASSEMBLY (LH) 1A 3A 5A 1 SEE 251562-05 -001A FOR DET 7A 9A -181A 132300-2 .BACKREST,ASSEMBLY (RH) 2A 4A 6A 1 SEE 251562-05 -002A FOR DET 8A 10A 190A 132200-1 .SEAT,STRUCTURE (LH) 1A 1 SEE 251562-06 -001A FOR DET -191A 132200-2 .SEAT,STRUCTURE (RH) 2A 1 SEE 251562-06 -002A FOR DET -192A 132208-1 .SEAT,STRUCTURE (LH) 3A 5A 1 SEE 251562-06 -003A FOR DET -193A 132208-2 .SEAT,STRUCTURE (RH) 4A 6A 1 SEE 251562-06 -004A FOR DET -194A 132209-1 .SEAT,HUD STRUCTURE (LH) 7A 9A 1 SEE 251562-06 -005A FOR DET

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 10022 132-SERIES

DETAILED PARTS LIST UNITS AIRLINE EFFECT. FIG. ITEM PART NUMBER 1234567 NOMENCLATURE PER STOCK N∞ CODE ASSY. 1 -195A 132209-2 .SEAT,HUD STRUCTURE (RH) 8A 10A 1 SEE 251562-06 -006A FOR DET 200A 132500 .LEVER,ASSEMBLY 1 SEE 251562-07 -001A FOR DET 210A 132100-1 .STRUCTURE,LOWER (LH) 1A 3A 5A 1 SEE 251562-08 -001A FOR DET 7A 9A -211A 132100-2 .STRUCTURE,LOWER (RH) 2A 4A 6A 1 SEE 251562-08 -002A FOR DET 8A 10A *** -220A 00-3316 .CROTCH STRAP 7A 8A 1 9A 10A

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 10023 132-SERIES

80 / 90

Covering Assembly Figure 2

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 10024 132-SERIES

DETAILED PARTS LIST UNITS AIRLINE EFFECT. FIG. ITEM PART NUMBER 1234567 NOMENCLATURE PER STOCK N∞ CODE ASSY. 2 -1A 132-01 COVERING,ASSEMBLY RF (NOT PROCURABLE) SEE 251562-01 -011A FOR NHA -2A 132-02 COVERING,ASSEMBLY RF (NOT PROCURABLE) SEE 251562-01 -012A FOR NHA 10A 132-03 .HEADREST ASSEMBLY 1 (NOT PROCURABLE) SEE 251562-09 -001A FOR DET 20A 132780-1 .FAIRING,SEAT (LH) 1 (PRE SB 132-25-001) -20B 132784-1 .FAIRING,SEAT (LH) 1 (POST SB 132-25-001) -21A 132780-2 .FAIRING,SEAT (RH) 1 (PRE SB 132-25-001) -21B 132784-2 .FAIRING,SEAT (RH) 1 (POST SB 132-25-001) ATTACHING PARTS 30A AN526-632R4 .SCREW (V88044) 2 (PRE SB 132-25-001) *** 40A 132730-001 .COVER,SEAT 1 (PRE SB 132-25-001) -41A 132732-001 .COVER,SEAT 1 (POST SB 132-25-001) 50A 132710 .FOAM,SEAT 1 (PRE SB 132-25-001) -51A 132712 .FOAM,SEAT 1 (POST SB 132-25-001) 60A 132740-001 .COVER,BACKREST 1 (PRE SB 132-25-001) -61A 132742-001 .COVER,BACKREST 1 (POST SB 132-25-001) 70A 132720 .FOAM,BACKREST 1 (PRE SB 132-25-001) -71A 132722 .FOAM,BACKREST 1 (POST SB 132-25-001) 80A AN526-632R9 .SCREW (V88044) 2 (PRE SB 132-25-001) 90A 132200-75 .SPACER 2

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 10025 132-SERIES

150

290

140 130 90 91 70 80 170

160 80 60 360 300 350 340 220 301 240 210 230 200 420 190 460 480 470 370 380 460 390 430 400 401 410 30 320 31 310 40 330 50 450 10

440 Figure20 3

Armrest Assembly Figure 3

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 10026 132-SERIES

DETAILED PARTS LIST UNITS AIRLINE EFFECT. FIG. ITEM PART NUMBER 1234567 NOMENCLATURE PER STOCK N∞ CODE ASSY. 3 -1A 132370 ARMREST,ASSEMBLY (LH) RF SEE 251562-01 -080A FOR NHA -2A 132380 ARMREST,ASSEMBLY (RH) RF SEE 251562-01 -081A FOR NHA -3A 132375-000-1 EASY ARMREST,ASSEMBLY(LH) RF SEE 251562-01 -080B FOR NHA -4A 132375-000-2 EASY ARMREST,ASSEMBLY(RH) RF SEE 251562-01 -081B FOR NHA 10A 394-10-370-15 .KNOB 1A 2A 1 -11A 132375-119-0 .BUTTON 3A 4A 1 ATTACHING PARTS 20A MS27039-0814 .SCREW (VIMS270390814) 1A 2A 1 -21A MS27039-0812 .SCREW (VIMS270390812) 3A 4A 1 *** 30A 394-10-376 .COVER (LH) 1A 1 -30B 132375-130-1 .COVER (LH) 3A 1 31A 394-10-386 .COVER (RH) 2A 1 -31B 132375-130-2 .COVER (RH) 4A 1 ATTACHING PARTS 40A NAS514P832-8 .SCREW,MACHINE (V80205) 1A 2A 4 -41A NAS602-6 .SCREW (VINAS6026) 3A 4A 4 50A N∞4 .WASHER,FINISHING (VF3349) 4 *** 60A 394-10-310-15 .SCREW 1 70A 132051-00023 .BOLT,INTERNALLY RELIEVED 1A 2A 1 BODY -71A 394-10-310-14 .BOLT,INTERNALLY RELIEVED 3A 4A 1 BODY 80A 132051-00025 .WASHER 1A 2A 2 -81A 394-10-310-32 .WASHER 3A 4A 2 90A 394-10-372 .FITTING,EQUIPPED (LH) 1A 1 -90B 132375-120-1 .FITTING,EQUIPPED (LH) 3A 1 91A 394-10-382 .FITTING,EQUIPPED (RH) 2A 1 -91B 132375-120-2 .FITTING,EQUIPPED (RH) 4A 1 -100A D2M1QV060020AL ..SCREW,CAP,SOCKET HEAD 1 (VF0110) -110A 394-10-317-07 ..BUSHING,SLEEVE 2 -120A 394-10-372-01 ..FITTING (LH) 90A 1 -121A 394-10-382-01 ..FITTING (RH) 91A 1 130A 23203AM0050T .RING,RETAINING (VF0111) 1A 2A 2 -131A 7144D5 .CIRCLIP (CI7144D5) 3A 4A 2 140A 394-10-310-11 .PIN,STRAIGHT,HEADLESS 1A 2A 1 -141A 132375-010-0 .PIN,STRAIGHT,HEADLESS 3A 4A 1 150A 132374 .UPPER ARMREST 1 ATTACHING PARTS 160A NAS602-6 .SCREW (V80205) 2 170A NAS514P832-6 .SCREW (V80205) 1A 2A 2 -171A NAS514P832-8 .SCREW (V80205) 3A 4A 2

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 10027 132-SERIES

DETAILED PARTS LIST UNITS AIRLINE EFFECT. FIG. ITEM PART NUMBER 1234567 NOMENCLATURE PER STOCK N∞ CODE ASSY. 3 *** -180A 394-10-373 .SLIDE,EQUIPPED 1 190A 394-10-373-11 ..PIN,THREADED,HEADED 1 200A 00-0521 ..SPRING,HELICAL, 1 COMPRESSION 210A NAS1149D0516K ..WASHER,FLAT 1 (R0AN960PD516L) 220A 394-10-373-06 ..WASHER,FLAT 1 230A 394-10-310-35 ..PIN,STRAIGHT,HEADLESS 1 240A 394-10-379 ..LEVER,EQUIPPED 1 250A 394-10-313-07 ...BUTTON 1 ATTACHING PARTS -260A NAS601-4 ...SCREW (V80205) 2 *** -270A NAS680A8 ..NUT,PLAIN,PLATE (V80205) 1 ATTACHING PARTS -280A 21217DE2406A ..RIVET,SOLID (VF0111) 2 *** 290A 394-10-373-01 ..SLIDE 1A 2A 1 -291A 132375-110-1 ..MAIN STRUCTURE EQU,LH 3A 1 -291B 132375-110-2 ..MAIN STRUCTURE EQU,RH 4A 1 *** 300A 132371 .SUPPORT,EQUIPPED (LH) 1A 1 300B 132375-100-1 .SUPPORT,EQUIPPED (LH) 3A 1 301A 132381 .SUPPORT,EQUIPPED (RH) 2A 1 301B 132375-100-2 .SUPPORT,EQUIPPED (RH) 4A 1 310A AN4-3A ..SCREW (V88044) 1 -311A CHC1-4NFx5-8 ..SCREW (VIDIN9121/4NFx5/8) 300B 1 301B 320A JFGA070UL ..WASHER,FLAT (VF0110) 300A 1 301A -321A MU7 ..WASHER (R0MU7) 300B 1 301B 330A 394-10-354-09 ..BUSHING,RUBBER 1 340A 132371-32 ..SCREW 300A 1 301A -341A 132375-123-0 ..THRUST 300B 1 301B 350A 132371-31 ..LOCK-NUT 1 360A 394-10-354-07 ..SCREW 300A 2 301A -361A 394-10-354-10 ..BOLT,SHOULDER 300B 1 301B -362A AN960-916L ..WASHER (R0AN960916L) 300B 1 301B -363A 700-10SEP25/100 ..SHIM (AD10AD12825/100) 300B 1 301B

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DETAILED PARTS LIST UNITS AIRLINE EFFECT. FIG. ITEM PART NUMBER 1234567 NOMENCLATURE PER STOCK N∞ CODE ASSY. 3 370A 863100-09 ..RING,RETAINING (VF0349) 300A 1 301A -371A 7133D10 ..CIRCLIP (CI7133D10) 300B 1 301B 380A NAS1149F0732P ..WASHER,FLAT (R0AN960716L) 300A 1 301A -381A NAS1149F0763P ..WASHER,FLAT (R0AN960716) 300B 1 301B 390A 394-10-310-07 ..SPRING,HELICAL, 1 COMPRESSION 400A MM-2010-61 ..CONTROL ROD (LH) 300A 1 (P/N SICMA: VE-MM201061) -400B 132375-125-1 ..CONTROL ROD (LH) 300A 1 401A MM-2010-62 ..CONTROL ROD (RH) 301A 1 (P/N SICMA: VE-MM201062) -401B 132375-125-2 ..CONTROL ROD (RH) 301B 1 410A E1-5x15EMCD ..PIN,SPRING (VF0313) 300A 1 301A -411A V1,5x15AC ..PIN,SPRING (GPV1-5x15AC) 300B 301B 420A 00-0021-1 ..PIN,STRAIGHT,HEADED 1 430A 394-10-371-09 ..TAPPET 300A 1 301A -431A 132375-118-0 ..CAMSHAFT 300B 1 301B 440A AN3-6A ..SCREW (V88044) 300A 1 301A -441A AN525-832R8 ..SCREW (VIAN525832R8) 300B 1 301B 450A NAS1149F0332P ..WASHER,FLAT (R0AN96010L) 1 460A 394-10-371-11 ..WASHER,FLAT 300A 2 301A -461A NAS1149FN816P ..WASHER,FLAT (R0AN9608L) 300B 1 301B 470A 394-10-371-25 ..SPACER,SLEEVE 1 480A 394-10-378 ..LEVER 300A 1 301A -481A 132375-115-1 ..UNLOCKING CAM,LH 300B 1 -481B 132375-115-2 ..UNLOCKING CAM,RH 301B 1 -490A 132375-116-0 ..CAM BEARING 300B 1 301B -500A 132375-124-0 ..SPACER,LONG 300B 1 301B -510A 132375-126-0 ..DRIVE SHAFT 300B 1 301B -520A 132375-122-1 ..END,LH CONTROL ROD 300B 1 -521A 132375-122-2 ..END,RH CONTROL ROD 301B 1 -530A NAS514P832-5 ..SCREW (VINAS514P8325) 300B 8 301B

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DETAILED PARTS LIST UNITS AIRLINE EFFECT. FIG. ITEM PART NUMBER 1234567 NOMENCLATURE PER STOCK N∞ CODE ASSY. 3 -540A 132375-123-0 ..STOP,ARMREST 300B 1 301B *** -550A 132375-140-1 .ARMCAP,LH LOWER 3A 1 -551A 132375-140-2 .ARMCAP,RH LOWER 4A 1 -560A 132315-150-0 .HOOK ASSY,LOWER ARMREST 3A 4A 1

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30 260

270 110 10 280

290 120 150

90 60 250 70

210 160 40 220 130 80 100 140 50 60 230 70 240 220 10 80 40 210

200

180 170 Lumbar Rest Assembly (Optional) Figure 4

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 10032 132-SERIES

DETAILED PARTS LIST UNITS AIRLINE EFFECT. FIG. ITEM PART NUMBER 1234567 NOMENCLATURE PER STOCK N∞ CODE ASSY. 4 -1A 132400-001 LUMBAR SUPPORT,ASSEMBLY RF (OPTIONAL) SEE 251562-01 -170A FOR NHA 10A 132400-20 .JACK,DUMMY 1 ATTACHING PARTS 20A AN4-10A .SCREW (V88044) 1 30A NAS679A4 .NUT,PLAIN,HEXAGON 1 (V80205) 40A AN316-6R .NUT,PLAIN,HEXAGON 2 (V88044) *** 50A 132400-04 .YOKE 1 ATTACHING PARTS 60A 132400-02 .SCREW,SHOULDER 2 70A 23134DG080D .WASHER,FLAT (VF0111) 2 *** 80A 132400-03 .SPACER,SLEEVE 2 90A 132400-01 .BUSHING 2 ATTACHING PARTS 100A E3x20EMCD .PIN,SPRING (VF0313) 2 *** 110A 132401 .TUBE ASSY 1 ATTACHING PARTS 120A AN3-14A .SCREW (V88044) 2 130A AN960-10L .WASHER,FLAT (V88044) 2 140A NAS679A3 .NUT,PLAIN,HEXAGON 2 (V80205) *** 150A 394-13-200-12 .SPACER 2 160A 394-13-200-13 .SPACER 2 170A AN515-832R6 .SCREW,MACHINE (V88044) 4 180A AN960-8L .WASHER,FLAT (V88044) 4 190A 132403 .LUMBAR SUPPORT ASSY 1 200A 132403-02 ..BAR 1 210A 21215ID3208A ..RIVET,SOLID (VF0111) 8 220A 23111AA030L ..WASHER,FLAT (VF0111) 8 230A 132403-01 ..BAR 1 240A 132403-04 ..CLOTH,ASSY 1 250A 132403-03 ..BAR 1 260A 341-710-03 ..SPRING,HELICAL,EXTENSION 2 270A 363-730-08 ..ROD 1 280A 132403-05 ..CLOTH,ASSY 1 290A 132402 .STRUCTURE 1

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62 10 90 80 120

260 110

100

50 190 280 180 40

200 210 300

290 70 260 160 170 140 160 20 270 250 240 220 230

Backrest Assembly Figure 5 Temporary Revisions N°.25-7 EFFECTIVITY : Mar 22/06 Dassault F900 25-15-62 Page 10034 132-SERIES

DETAILED PARTS LIST UNITS AIRLINE EFFECT. FIG. ITEM PART NUMBER 1234567 NOMENCLATURE PER STOCK N° CODE ASSY. 5 -1A 132300-1 BACKREST,ASSEMBLY (LH) RF SEE 251562-01 -180A FOR NHA -2A 132300-2 BACKREST,ASSEMBLY (RH) RF SEE 251562-01 -181A FOR NHA 10A 132300-11 .SLEEVE 2 20A 132302-1 .SIDE,ASSEMBLY 1 ATTACHING PARTS 30A TLPD424BS .RIVET,BLIND (VK0017) 4 *** 40A 132302-2 .SIDE,ASSEMBLY 1 ATTACHING PARTS 50A TLPD424BS .RIVET,BLIND (VK0017) 4 *** -60A 132303-1 .COVER,ASSEMBLY (LH) 1A 1 -61A 132303-2 .COVER,BARE (RH) 2A 1 (WITHOUT OPENING ASHTRAY) (ONE WAY INTERCH WITH P/N 132303-0) 62A 132303-01 ..COVER,BARE (LH) 60A 1 (WITH OPENING ASHTRAY) 70A AN526-832R8 .SCREW (V88044) 2 *** 80A 79A8F27470 ..ASHTRAY (EQ79A8F27470) 60A 1 ATTACHING PARTS 90A MS24693-C5 ..SCREW (V96906) 60A 2 100A NAS679A04 ..NUT,PLAIN,HEXAGON 60A 2 (V80205) *** 110A 132303-03 ..BRACKET,ANGLE 60A 2 ATTACHING PARTS 120A TAPK044BS ..RIVET,BLIND (VK0017) 60A 4 *** 130A DELETED ..COVER (LH) 60A (REPLACED BY P/N ITEM 62A) -131A DELETED ..COVER (RH) 61A (OLD P/N 132303-02 REPLACED BY P/N ITEM -61A) 140A 128500-23 .SCREW 4 -150A NAS1149F0632P .WASHER (R0AN960616L) 4 160A AN316-6R .NUT,PLAIN,HEXAGON 4 (V88044) 170A 128500-24 .YOKE 2 180A NAS679A4 .NUT,PLAIN,HEXAGON 2 (V80205) 190A AN4-7A .SCREW (V88044) 2 200A 132500-25 .HYDROLOCK EQUIPPED 1 SIDE RIGHT

Temporary Revisions N°.25-7 EFFECTIVITY : Mar 2/06 Dassault F900 25-15-62 Page 10035 132-SERIES

DETAILED PARTS LIST UNITS AIRLINE EFFECT. FIG. ITEM PART NUMBER 1234567 NOMENCLATURE PER STOCK N° CODE ASSY. 5 210A LL-01500-10 .HYDROLOCK (V02953) 1 (P/N SICMA : VE-LL0150010) SIDE LEFT 220A 132300-02 .PIN 2 ATTACHING PARTS 230A 132300-01 .WASHER 2 240A AN960-616 .WASHER,FLAT (V88044) 2 250A NAS679A6 .NUT,PLAIN,HEXAGON (V80205) 2 *** 260A 132301 .STRUCTURE 1 270A 132301-20 ..SHEET METAL 1 ATTACHING PARTS 280A AN525-832R7 ..SCREW (V88044) 7 *** 290A 132301-15 ..BUSHING,SLEEVE 3 300A 132301-09 ..BOSS 2 (WELDED ON STRUCTURE)

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400 390 510 80 110 100 40 70 90 50 90 60 120 130 280 80

370 30 180

350 10 220 20 230 330 270

170 360 140 250 410 160 210 190 460 310 150 290 450 200 470 480 490 300 500 320 470

Seat Structure Figure 6

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DETAILED PARTS LIST UNITS AIRLINE EFFECT. FIG. ITEM PART NUMBER 1234567 NOMENCLATURE PER STOCK N∞ CODE ASSY. 6 -1A 132200-1 SEAT,STRUCTURE (LH) RF SEE 251562-01 -190A FOR NHA -2A 132200-2 SEAT,STRUCTURE (RH) RF SEE 251562-01 -191A FOR NHA -3A 132208-1 SEAT,STRUCTURE (LH) RF SEE 251562-01 -192A FOR NHA -4A 132208-2 SEAT,STRUCTURE (RH) RF SEE 251562-01 -193A FOR NHA -5A 132209-1 SEAT,HUD STRUCTURE (LH) RF SEE 251562-01 -194A FOR NHA -6A 132209-2 SEAT,HUD STRUCTURE (RH) RF SEE 251562-01 -195A FOR NHA 10A 132200-05 .FITTING 1 ATTACHING PARTS 20A NAS517-4-11 .SCREW (V80205) 2 30A F52NTE048 .NUT,SELF-LOCKING,HEXAGON 2 (V72962) *** 40A 132200-06 .FITTING 1 ATTACHING PARTS 50A NAS517-4-11 .SCREW (V80205) 2 60A F52NTE048 .NUT,SELF-LOCKING,HEXAGON 2 (V72962) *** 70A 132206-01 .SUPPORT 2 ATTACHING PARTS 80A AN4-15A .SCREW (V88044) 4 90A F52NTE048 .NUT,SELF-LOCKING,HEXAGON 4 (V72962) *** 100A 132206-02 ..BUSHING 2 110A 132200-09 .SPACER,SLEEVE 2 120A 132200-08 .BUSHING,SLEEVE 1 130A 132200-58 .CLOTH 1A 2A 1 -131A 132208-58 .CLOTH 3A 4A 5A 1 6A 140A 132207 .SUPPORT 1 -141 132200-72 .SHEET METAL FOR SPRINGS 3A 4A 5A 1 6A ATTACHING PARTS 150A AN3-6A .SCREW (V88044) 2 160A TLPD424BS .RIVET,BLIND (VK0017) 7 -161A TLPD424BS .RIVET,BLIND (VK0017) 12 (PRE SB 132-25-001) 170A TLPD429BS .RIVET,BLIND (VK0017) 2 *** 180A 132200-63 .SHEET METAL 1 ATTACHING PARTS

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DETAILED PARTS LIST UNITS AIRLINE EFFECT. FIG. ITEM PART NUMBER 1234567 NOMENCLATURE PER STOCK N∞ CODE ASSY. 6 190A TLPD419BS .RIVET,BLIND (VK0017) 9 *** 200A 132200-12 .TUBE 1 ATTACHING PARTS 210A E3x25EMCD .PIN,SPRING (VF0313) 1A 2A 2 -211A G07-3x26S250 .PIN,GROOVED (VF0344) 3A 4A 5A 2 6A *** 220A 132200-57 .TUBING 12 230A 132200-74 .SPRING,HELICAL,EXTENSION 12 (PRE SB 132-25-001) -231A 132200-70 .SPRING,HELICAL,EXTENSION 12 (POST SB 132-25-001) 240A 132203 .TUBE 2 ATTACHING PARTS 250A CHC1-4NFx5-8 .SCREW,CAP,SOCKET HEAD 2 (VD8286) *** -260A 132204 .TUBE,ASSY 1 ATTACHING PARTS 270A G07-8x30A .PIN,GROOVED,HEADED 2 (VF0344) *** 280A 132204-01 ..TUBE ASSY 1 290A 132200-18 .SUPPORT (LH) 1A 3A 5A 1 -291A 132200-19 .SUPPORT (RH) 2A 4A 6A 1 ATTACHING PARTS 300A CHC8NCx3-8 .SCREW,CAP,SOCKET HEAD 1 (VD8286) 310A AN4-14A .SCREW (V88044) 1 320A NAS679A08 .NUT,PLAIN,HEXAGON 1 (V80205) *** 330A AN4-13A .SCREW (V88044) 1 -340A DELETED .WASHER,FLAT (V88044) (AN960-416L) 350A 132200-07 .SPACER 2 360A 132200-03 .CROSS,LEFT (LH) 1A 3A 5A 1 -361A 132200-02 .CROSS,LEFT (RH) 2A 4A 6A 1 370A 132200-01 .CROSS,RIGHT (LH) 1A 3A 5A 1 -371A 132200-04 .CROSS,RIGHT (RH) 2A 4A 6A 1 -380A V57-Y-401-600-0 .CONTROL,ASSY (BACKREST) 1 390A V40-301 ..END 2 400A V57-401 ..CONTROL CABLE,LONG 1 410A V40-600 ..CONTROL CABLE,SHORT 2 -420A V40-800 ..DIVIDER 1 -430A MS24693C2 ...SCREW (VIMS24693C2) 1 -440A V40-101-3 ..PUSHER ASSY 1

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DETAILED PARTS LIST UNITS AIRLINE EFFECT. FIG. ITEM PART NUMBER 1234567 NOMENCLATURE PER STOCK N∞ CODE ASSY. 6 450A 00-2612 ...PUSHER BODY EQUIPPED 1 460A V39-101-06 ...SPRING 1 470A V39-101-07-3 ...GUIDE 1 480A V39-101-08-3 ...BUTTON 1 -481A AN565F10-32H8 ...SCREW,BUTTON (V88044) 1 (P/N SICMA : VIAN565F1032H8) 490A V39-101-12 ...WASHER, WAVY 1 500A V40-101-13 ...WASHER, FLAT 1 ATTACHING PARTS 510A 7133D5 .CIRCLIP (CI7133D5) 1 -520A AN565B10-32H3 .SCREW (V88044) 1 (P/N SICMA : VIAN565B1032H3) -525A LKCRNATUREL .TIE-WRAP PLASTIC BASE 1 (P/N SICMA: EELKCRNATUREL) -526A PLT1M-M .COLLAR 1 (P/N SICMA: C0PLT1M-M) -527A TAPD036BS .RIVET,BLIND 1 (P/N SICMA: P0PTAPD036BS) *** -530A 132200-64 .VELCR0,HOOK 1 (WIDTH 20, LENGTH 360) (PRE SB 132-25-001) (FIXING ON ITEM 280) -531A VELCR020-10A .VELCR0,HOOK 1 (WIDTH 20, LENGTH 360) (POST SB 132-25-001) -540A 132200-65 .VELCR0,HOOK 1 (WIDTH 16, LENGTH 360) (PRE SB 132-25-001) -541A VELCR016-10A .VELCR0,HOOK 1 (WIDTH 16, LENGTH 360) (POST SB 132-25-001)

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240 250 230 220

140

270 260

160 170

180

30 130 70 120 70 40

110

210 90 80 200 20 190 10

Lever Assembly Figure 7

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DETAILED PARTS LIST UNITS AIRLINE EFFECT. FIG. ITEM PART NUMBER 1234567 NOMENCLATURE PER STOCK N∞ CODE ASSY. 7 -1A 132500 LEVER,ASSEMBLY RF SEE 251562-01 -200A FOR NHA 10A 132500-02 .PIN,THREADED,HEADED 2 20A 132500-04 .ROLLER,LINEAR-ROTARY 2 MOTION 30A 7133D16 .CIRCLIP (VF0405) 2 40A 132500-01 .PIN 2 50A MECAE3x20 .PIN,SPRING (GPMECAE3x20) 2 -60A 132520 .ARM,ASSY 2 70A 132520-02 ..BUSHING,SLEEVE 1 80A 376-135-03 ..BUSHING,SLEEVE 2 90A 132520-01 ..ARM 2 100A 132530 .PIN, UPPER 1 110A MECAE3x20 .PIN,SPRING (GPMECAE3x20) 4 120A 132530-02 ..END PIECE 2 130A 132530-01 ..PIN,HOLLOW 1 140A 132550 .BOX 1 -150A 132540 ..PIN 1 ATTACHING PARTS 160A MS27039-0818 ..SCREW (V80205) 6 170A AN960-8 ..WASHER,FLAT (V88044) 6 180A MS20364-832A ..NUT,SELF-LOCKING,HEXAGON 6 (V96906) *** 190A 132540-02 ...END PIECE 2 200A 132540-01 ...PIN,HOLLOW 1 210A 376-143 ..CRANKPIN,OPERATION 1 220A 394-10-162 ..STRAP,WEBBING,EQUIPPED 1 ATTACHING PARTS 230A TLPD435BS ..RIVET,BLIND (VK0017) 3 *** 240A 394-10-165-07 ..BRACKET,ANGLE 1 ATTACHING PARTS 250A TLPD429BS ..RIVET,BLIND (VK0017) 2 *** 260A 394-10-165-03 ..HOOK 1 ATTACHING PARTS 270A TLPD419BS ..RIVET,BLIND (VK0017) 2

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Lower Structure Figure 8

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DETAILED PARTS LIST UNITS AIRLINE EFFECT. FIG. ITEM PART NUMBER 1234567 NOMENCLATURE PER STOCK N∞ CODE ASSY. 8 -1A 132100-1 STRUCTURE, LOWER (LH) RF SEE 251562-01 -210A FOR NHA -2A 132100-2 STRUCTURE, LOWER (RH) RF SEE 251562-01 -211A FOR NHA 10A 8TA10BE .NUT,SELF-LOCKING,HEXAGON 2 NYLSTOP DIA 8 (VF0224) 20A 128100-37 .SCREW 2 30A 376-100-19 .SPACER,SLEEVE 2 40A 132500-03 .PIN,THREADED,HEADED 2 50A 132500-05 .ROLLER,LINEAR-ROTARY 2 MOTION 60A E2-5x14EMCD .PIN,SPRING (VF0313) 2 70A 132100-08 .RING 2 80A 132100-07 .FORK ARM 2 ATTACHING PARTS 90A AN520-10R14 .SCREW (V88044) 2 *** 100A 132100-03 .PLATE 2 ATTACHING PARTS 110A AN509-10R7 .SCREW (V88044) 4 *** 120A 147100-19 .SPRING,HELICAL, 2 COMPRESSION 130A 132100-09 .LOCKING PIN 2 -140A 132102-1 .CROSS TUBE,ASSY (LH) 1A 1 -141A 132102-2 .CROSS TUBE,ASSY (RH) 2A 1 150A 132102-01 ..KNOB,LOCKING 1 160A G072,5x14 ..PIN,SPRING 4 (GPG072-5x14S250) 170A 132102-02 ..END PIECE 1 180A 132102-03 ..LEVER 1 190A 132102-04 ..END PIECE 1 ATTACHING PARTS 200A AN525-10R16 ..SCREW (V88044) 1 210A 132102-06 ..WASHER 1 *** 220A 132102-05-1 ..CROSS TUBE (LH) 140A 1 -221A 132102-05-2 ..CROSS TUBE (RH) 141A 1 230A EC6PH135M .NUT,SELF-LOCKING,HEXAGON 8 NYLSTOP DIA 6 (VF0224) 240A 22271BC060046L .SCREW (VF0111) 6 241A 22271BC060048L .SCREW (VF0111) 2 250A 132100-05 .PAD 2 -260A 132103 .PAD,ASSY (LH) 1 -261A 132104 .PAD,ASSY (RH) 1 270A 132100-10 ..BEARING 1 280A 132103-01 ..PAD (LH) 260A 1 281A 132103-02 ..PAD (RH) 261A 1

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DETAILED PARTS LIST UNITS AIRLINE EFFECT. FIG. ITEM PART NUMBER 1234567 NOMENCLATURE PER STOCK N∞ CODE ASSY. 8 290A 128100-51 .PAD (LH) 1 291A 128100-50 .PAD (RH) 1 300A 128100-49 .PAD (LH) 1 301A 128100-48 .PAD (RH) 1 310A 132100-06 .SPACER,SLEEVE 8 320A 132100-04 .ROLLER,LINEAR-ROTARY 2 MOTION (LH) 321A 132100-12 .ROLLER,LINEAR-ROTARY 2 MOTION (RH) 330A 132101 .CROSS TUBE 1 ATTACHING PARTS 340A 22208BC050014L .SCREW (VF0111) 4 350A 5PH135M .NUT,SELF-LOCKING,HEXAGON 4 NYLSTOP DIA 5 (VF0224) *** -360A 132115-1 .CROSS TUBE,ASSY 1 ATTACHING PARTS 370A 22208BC060012L .SCREW (VF0111) 2 *** 380A 132100-11 ..SCREW,CAP,SOCKET HEAD 2 390A 132105-2 ..CROSS TUBE 1 -400A 132100-01 .MEMBER, ASSY (LH) 1 -401A 132100-02 .MEMBER, ASSY (RH) 1 410A 132100-012 ..BUSHING,SLEEVE 1 420A 132100-011 ..MEMBER (LH) 400A 1 421A 132100-021 ..MEMBER (RH) 401A 1

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Headrest Assembly Figure 9

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DETAILED PARTS LIST UNITS AIRLINE EFFECT. FIG. ITEM PART NUMBER 1234567 NOMENCLATURE PER STOCK N∞ CODE ASSY. 9 -1A 132-03 HEADREST ASSEMBLY RF (NOT PROCURABLE) SEE 251562-02 -010A FOR NHA 5A 132260 .HEADREST STRUCTURE EQU 1 *** 10A 142760 .HEADREST FOAM 1 15A 394-10-800-001 .HEADREST COVER 1 (COLOR : WHITE)

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STORAGE

TASK 25-15-62-550-801 1. STORAGE INSTRUCTIONS Subtask 25-15-62-550-001 A. GENERAL (1) The seat is essentially corrosion resistant and special preservation is not required.

CAUTION : AVOID PLACING THE SEAT ON CONCRETE GROUND OR ON STEEL SURFACES WHICH ARE NOT PROTECTED AGAINST CORROSION.

Subtask 25-15-62-550-002 B. PRESERVATION (1) Set the armrests to the down position. (2) Tilt the backrest forward. (3) Lightly grease the hinge points with grease AIR 4222. (4) Using a soft cloyh moistened with aliphatic naphta, grade F, clean the external parts of the seat.

EFFECTIVITY : Sep 10/04 Dassault F900 25-15-62 Page 15001 132-SERIES STORAGE Subtask 25-15-62-550-003 C. PROCEDURES (1) For prolonged storage, wrap seat assembly in waterproof wrapping paper or a plastic cover. (2) Identify seat assembly part number and date of overhaul on a tag or in a convenient location on the seat assembly wrapper. (3) Store seat assembly in cool, dry place away from sunlight and heat sources. (4) After a year of storage, check all the seat systems as described in "CHECKS" and "TESTING" sections of this manual.

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