25-21-43

September 15, 2011

25-21-43 PRINTED IN USA

AmSafe, Inc. 1043 N 47th Ave. Phoenix, Arizona 85043 Phone: (602) 850-2850 Fax: (602) 850-2812

Aircraft Seat Belt Combination

FAG-9

Component Maintenance Manual

with illustrated parts list

Title page T-1

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September 15, 2011

25-21-43 Use or disclosure of information on this page is subject to the restrictions on the title page of this document

PROPRIETARY NOTICE

This document and the information disclosed herein are the proprietary data of AmSafe, Inc. Neither this document nor the information contained herein shall be used, reproduced or disclosed to others without the written authorization of AmSafe, Inc. except to the extent required for installation or maintenance of recipients equipment.

NOTICE FREEDOM OF INFORMATION ACT (5 USC 552) AND DISCLOSURE OF CONFIDENTIAL INFORMATION GENERALLY (18 USC 1905)

This document is being furnished in confidence by AmSafe, Inc. The information disclosed herein falls within exemption (b) (4) of 5 USC 552 and the prohibitions of 18 USC 1905.

TSO NOTICE

The conditions and tests required for TSO approval of this article are minimum performance standards. It is the responsibility of those desiring to install this article either on or within a specific type or class of aircraft to determine that the aircraft installation conditions are within the TSO standards. This article may be installed only if further evaluation by the applicant documents an acceptable installation and is approved by the administrator.

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MATERIALS HAZARD RATING CODE AmSafe Inc. uses the National Fire Protection Association system to identify the different levels of hazards that are caused by the use of a given material. A Hazard Code identifies three effects of a material on a person: health (eat, drink, touch, and breathe), fire (when and how it burns), and reactivity (chemical explosions). Also, each material is given a storage group for safety. Each code has three numbers and one letter (for example, 130D) as shown in the Hazard Code symbol below. The three numbers show the hazard levels for health, fire, and reactivity, in that sequence. The range of each number is 0 to 4. The higher the number, the more dangerous the hazard. You must be careful with any material that has a Hazard Code with a 2, 3, or 4. The one letter (A through E) in the code identifies a specific storage group that is applicable for the material. If applicable, the materials used for the procedures in this manual are given a Hazard Code. Get specific data on a material from the data sheet supplied by the manufacturer of the material. POSITION 1: HEALTH HAZARD POSITION 2: FIRE HAZARD

0 1 2 3 4

No important hazard IrritantUse with caution HazardousPrevent continued exposure, inhalation, and contact Dangerous hazardUse protective clothing together with protection to breathe Very bad hazardDo not breathe vapor or come in contact with liquid without approved special protection

0 1 2 3 4

Will not burn Must increase the temperature above 93.4C to burn Must increase the temperature above 37.8C to burn Fire and explosion hazard at ambient temperature Highly dangerous fire and explosion hazard

POSITION 3: REACTIVITY HAZARD POSITION 4: STORAGE

0 1 2 3 4

Usually stable Unstable if heated Violent chemical change is possible Dangerous explosion is possible Very bad explosion hazardquickly go out of the area if materials are exposed to fire

A B C D E

Acids Alkalis, cyanides Oxidizing agents Chlorinated hydrocarbons, flammable liquids, materials that are not flammable Neutral salts and others

Hazard rating page H-1

POSITION 3 REACTIVITY (YELLOW)

POSITION 4 STORAGE (WHITE)

POSITION 1 HEALTH (BLUE)

POSITION 2 FIRE (RED)

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RECORD OF REVISIONS

For each revision, put the revised pages in your manual and discard the superseded pages. Write the revision number and the date, date put in manual, and the incorporators initials in the applicable columns on the Record of Revisions. The initials AS show AmSafe Inc. is the incorporator. Revision Revision Date Put Revision Revision Date Put Number Date in Manual By Number Date in Manual By 1 Sep 1/83 at issue J. 2 Mar 1/90 at issue J. 3 Oct 12/95 at issue AS

4 Sept 15/11 at issue AS

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THIS PAGE INTENTIONALLY

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SERVICE BULLETIN LIST

FOR FAG-9

Service Identified Date Included Bulletin MOD in this Manual Description

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LIST OF EFFECTIVE PAGES

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SUBHEADING AND PAGE DATE SUBHEADING AND PAGE DATE Title Cleaning T-1/T-2 9/15/11 401/402 9/15/11 Hazard Rating Code Check H-1/HC-2 9/15/11 501/502 9/15/11 503/504 9/15/11 Record of Revisions 505/506 9/15/11 RR-1/RR-2 9/15/11 Record of Temporary Revisions Repair RTR-1/RTR-2 9/15/11 601/602 9/15/11 603/604 9/15/11 Service Bulletin List SBL-1/SBL-2 9/15/11 Assembly (Including Storage) 701/702 9/15/11 List of Effective Pages LEP-1/LEP-2 9/15/11 Fits and Clearances 801/802 9/15/11 Table of Contents TC-1/TC-2 9/15/11 Special Tools, Fixtures, and Equipment Introduction 901/902 9/15/11 INTRO-1 9/15/11 INTRO-2 9/15/11 Illustrated Parts Introduction INTRO-3 9/15/11 1 9/15/11 INTRO-4 9/15/11 2 9/15/11 Description and Operation Numerical Index 1 9/15/11 1 9/15/11 2 9/15/11 2 9/15/11 3 9/15/11 3 9/15/11 4 9/15/11 4 9/15/11 5 9/15/11 5 9/15/11 6 9/15/11 6 9/15/11 7 9/15/11 7 9/15/11 8 9/15/11 8 9/15/11 Testing and Fault Isolation 101/102 9/15/11 Disassembly 301/302 9/15/11

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LIST OF EFFECTIVE PAGES

SUBHEADING AND PAGE DATE

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Illustrated Parts List 1001 9/15/11 1002 9/15/11 1003 9/15/11 1004 9/15/11 1005 9/15/11 1006 9/15/11 1007 9/15/11 1008 9/15/11 1009 9/15/11 1010 9/15/11 1011 9/15/11 1012 9/15/11 1013 9/15/11 1014 9/15/11 1015 9/15/11 1016 9/15/11 1017 9/15/11 1018 9/15/11 1019 9/15/11 1020 9/15/11 1021 9/15/11 1022 9/15/11 1023 9/15/11 1024 9/15/11 1025 9/15/11

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TABLE OF CONTENTS _______Subheading_____________ Page DESCRIPTION AND OPERATION 1 TESTING AND FAULT ISOLATION 101

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AUTOMATIC TEST REQUIREMENTS (ATLAS) * N/A DISASSEMBLY 301 CLEANING 401 CHECK 501 REPAIR 601 ASSEMBLY (Including Storage) 701 FITS AND CLEARANCES* 801 SPECIAL TOOLS, FIXTURES, AND EQUIPMENT 901 ILLUSTRATED PARTS LIST INTRODUCTION 1 NUMERICAL INDEX 1 ILLUSTRATED PARTS LIST 1001 *Not applicable

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INTRODUCTION

How to use this Manual The instructions in this manual give the data necessary to do all recommended maintenance functions to put the Restraint System in serviceable condition. Standard maintenance procedures that technicians are thought to know are not given in this manual. Refer to the Table of Contents for a list of subheadings in this manual. The Table of Contents identifies those subheadings that are not applicable, that require no special instructions, or that are scheduled for a subsequent revision. To decrease the length of sentences and titles, complete part numbers are not always shown in this manual. A piece of the part number can show applicability to a specific assembly or component. Complete part numbers are always given in the parts list subheading. Refer to the introduction in the ILLUSTRATED PARTS LIST (or CATALOG) to find how to use that subheading. Related publications that are referred to in this manual are identified in the list that follows: Document Publication No. Abbreviations for Use on Drawings and in Text.* ASME Y 1.1 (1989) Standard Letter Symbols for Units of Measurement* ANSI / IEEE Std. 260 (1978) *Available from the American National Standard Institute, New York, NY. Warning, Cautions, Notes A. WARNING: Warning call attention to use of materials, processes, methods, procedures or limits which

must be followed precisely to avoid injury or death to persons. B, CAUTION: Cautions call attention to methods and procedures which must be followed to avoid damage

to equipment. C, Note: Notes call attention to method which make the job easier.

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Verification of these technical instructions is done by performance or by simulation of the necessary procedures. Checks of the manual by the engineering staff make sure the instructions and description data agree with the applicable engineering specifications and drawings and are accurate and sufficient. AmSafe Inc. will revise this manual as necessary to give current data.

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Abbreviations Weights and measurements in this manual are in both U.S. and S.I. (metric) values. The letter symbols for units of measurement and the abbreviations are the same as shown in ANSI/EEE Std 260 and ASME Y1.1 except as identified below. Abbreviation Definition APN AmSafe Inc. part number LF left foldout g standard gravity RF reference callouts

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DESCRIPTION AND OPERATION 1. General

This manual covers the two differing versions of the aircraft seat belt combination FAG-9 used by cabin crews as a safety belt. The aircraft seat belt combination FAG-9 will restrain the seat belt occupant safely in his seat in all flight attitudes, particularly in the event of a crash landing. The lap belt can not only be used in conjunction with the shoulder strap, but may also be used separately. The two aircraft seat belt combinations FAG-9 comprise the following versions: A. 1 automatic lap belt, Bagu FAG-9C and 2 automatic shoulder straps, Schugu FAG-9A

The attachment fittings used for the Bagu FAG-9C and Schugu FAG 9A are automatic inertia reels AGB-8C which are fitted to the end of each belt portion. The belt portions are fastened by means of a 2-point buckle assembly MS-1D.

B. 1 lap belt, Bagu FAG-9D and 2 automatic shoulder straps, Schugu FAG-9D

The lap belt Bagu FAG-9D can be supplied with different fittings to suit the prevailing installation conditions. Seat attachment of the shoulder straps Schugu FAG-9D is by means of the automatic inertia reel AGB-8C. The belt portions are fastened by means of lugs inserted into a central rotary buckle.

2. Operation

A. Aircraft Seat Belt Combination Comprising Bagu FAG-9C and Schugu FAG-9A

(1) Lap Belt Bagu FAG-9C

The lap belt consists of a right-hand and a left-hand belt portion. The free end of the left-hand belt is fitted with a buckle MS-1 and the free end of the right hand belt with a lug. Buckle and lug are made from light-alloy and are used to centrally connect both belt portions.

The outer end of each lap belt portion is attached to an automatic inertia reel AGB-8C. The

automatic inertia reel AGB-8C also acts as a seat connection fitting. The lap belt itself is made from polyester webbing. When the lap belt is unfastened, both belt portions are rolled up by their perspective inertia

reels until only the fittings project from the recess in the seat. All lap belt portions are provided with an identification label indicating all relevant data.

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(2) Shoulder Straps Schugu FAG-9A

The shoulder straps also comprise a left-hand and a right-hand belt portion and are made from polyester webbing.

The free end of each strap is fitted with a sewn-in lug. Connection is by passing the lugs over the upper tongue of the right-hand lap belt lug and

inserting the lap belt lug into the MS-1 buckle. The upper end of each shoulder strap is separately attached to an automatic inertia reel

AGB-8C which also serves as seat attachment fitting. When the shoulder straps are unfastened, both strap portions are rolled up by their

respective automatic inertia reels until only the lugs project from the recess in the backrest. The right-hand shoulder strap is marked R and the left-hand shoulder strap L. All shoulder strap portions are provided with an identification label indicating all relevant data.

B. Aircraft Seat Belt Combination Comprising Bagu FAG-9D and Schugu FAG-9D

(1) Lap Belt Bagu FAG-9D

The lap belt consists of a right-hand and a left-hand belt portion and are made from polyester webbing. Depending on customer specification either the left-hand or right-hand portion of the lap belt is fitted with a fixed lug, and a rotary buckle, with the opposite belt portion provided with a suitable single lug. Rotary buckle and lugs provide a central fastening device for both belt portions. The other ends of the two lap belt portions are provided with sewn-in seat connection fittings. Each lap belt portion is provided with a sewn-in sliding buckle for length adjustment. Pulling direction for length adjustment is from rear to front for fastening. All lap belt portions are provided with an identification label indicating all relevant data.

(2) Shoulder Straps Schugu FAG-9D

The shoulder straps also comprise a left-hand and a right-hand belt portion and are made from polyester webbing.

The free end of each strap is fitted with a sewn-in lug for insertion into the rotary buckle. The upper end of each shoulder strap is separately attached to an automatic inertia reel AGB-8C which also serves as seat attachment fitting. When the shoulder straps are unfastened, both strap portions are rolled up by their respective automatic inertia reels until only the lugs project from the recess in the backrest. All shoulder strap portions are provided with an identification label indicating all relevant data.

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3. Functioning


Due to the automatic locking action of the inertia reels, the aircraft seat belt combination FAG-9, irrespective of the prevailing flight conditions, will safely restrain the occupant in his seat. As soon as the lap belt and shoulder straps are subjected to forward acceleration forces of at least 0.5 g and 1.5 g respectively, the inertia reels will automatically block any movement of the belts, thus preventing the body of the seat occupant from being thrown forward. As long as the acceleration forces do not reach the above values, the aircraft seat belt combination allows unrestricted normal movement of the seat occupant. When the seat belt combination is unfastened, both shoulder straps and lap belts are rolled up by their respective automatic inertia reels until only the lugs project from the recesses in the backrest.

B. Aircraft Seat Belt Combination Comprising Bagu FAG-9D and Schugu FAG-9D The aircraft seat belt combination FAG-9D, irrespective of the prevailing flight conditions, will safely restrain the occupant in his seat. As soon as the shoulder straps are subjected to forward acceleration forces of at least 1.5 g, the inertia reels will automatically block any movement of the straps, thus preventing the body of the seat occupant from being thrown forward. As long as the acceleration forces do not reach the above value, the automatic shoulder straps allow unrestricted normal movement of the seat occupant. When the seat belt combination is unfastened, both shoulder straps are rolled up by their respective automatic inertia reels until only the lugs project from the recesses in the backrest.

4. Applicable Specifications

A. Aircraft Seat Belt Combination Comprising Bagu FAG-9C and Schugu FAG-9A The applicable specification is the Design and Testing Specification for Inertia Reels AFG-17/72.


The applicable specification is the Airworthiness Requirements for Seat Belts (LFA), issue January 1973 and the Design and Testing Specification for Inertia Reels AFG-17/72.

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5. Technical Data


(1) Lap Belt Type: Aircraft seat belt Series: Bagu FAG-9C Design and AMSAFE, INCORPORATED Manufacture: 1043 NORTH 47th AVENUE, PHOENIX, ARIZONA 85043

Technical data: Max. length approx. 1400mm (55.12 in). Adjustment range for one belt portion approx. 600 mm (23.62 in.). Adjustment by means of automatic inertia reel. Webbing to data sheet AFG-5012. Fastening of seat belts by means of 2-point buckle assembly MS-1/D Total weight approx. 0.8 kg (1.76lb). Operating limits: Operating Temperature 219 to 344 K (-54 to 71C) (-65.2 to +159.8F). Rated strength 686.5 daN (1500 LB). Burning rate in accordance with FAR 25-853 (b-2). Application: Lap belt for aircraft occupants. The lap belt can be used Separately or in conjunction with the shoulder straps Schugu FAG-9A.

(2) Shoulder Straps

Type: Aircraft seat belt Series: Schugu FAG-9A Design and AMSAFE, INCORPORATED

Manufacture: 1043 NORTH 47th AVENUE, PHOENIX, ARIZONA 85043 Technical data: Max. length 1000 mm (39.37 in.) respectively 1150 mm (45.28 in.). Adjustment range approx. 1000 mm (39.4 in.). Adjustment by means of automatic inertia reel. Webbing to data sheet AFG-5012. Total weight approx. 0.73 kg (1.61 LB) (1 pair). Operating limits: Operating temperature 219 to 344 K (-54 to +71) (-65.2 to +159.8F). Rated strength 392.4 daN (882 LB). Burning rate in accordance with FAR 25.853 (b-2).

Application: Shoulder strap for aircraft occupants. The shoulder straps (used in pairs) are used in conjunction with the lap belt Bagu

FAG-9C.

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(1) Lap Belt Type: Aircraft seat belt Series: Bagu FAG-9C Design and AMSAFE, INCORPORATED Manufacture: 1043 NORTH 47th AVENUE, PHOENIX, ARIZONA 85043

Technical data: Max. length 1200 mm (47.2 in.) respectively 1100 mm (43.3 in.). Adjustment range approx. 660 mm (26.0 in.) respectively 500 mm (19.7 in.). Adjustment by means of sliding buckle. Pulling direction for adjustment from rear to front for fastening. Webbing to data sheet AFG-5030 Fastening of seat belt by means of rotary buckle. Total weight approx. 0.58 kg (1.28 lb). Operating limits: Operating temperature 219 to 344 K (-54 to +71C) (-65.2 to +159.8F). Rated strength 686.5 daN (1500 lb). Burning rate in accordance with FAR 25.853 (b-2). Application: Lap belt for aircraft occupants. The lap belt can be used Separately or in conjunction with the shoulder straps Schugu FAG-9D. (2) Shoulder Straps

Type: Aircraft seat belt Series: Schugu FAG-9D Design and AMSAFE, INCORPORATED

Manufacture: 1043 NORTH 47th AVENUE, PHOENIX, ARIZONA 85043 Technical data: Max. length (refer to the IPL) Adjustment range approx.1000 mm 39.4 in.). Adjustment by means of automatic inertia reel. Webbing to data sheet AFG-5012. Total weight approx. 0.76 kg (1.68 lb) (1 pair). Operating limits: Operating temperature 219 to 3144K (-54 to +71C) (-65.2 to +159.8F). Rated strength 392.4 daN (882 lb). Burning rate in accordance with FAR 25.853 (b-2). Application: Shoulder strap for aircraft occupants. The shoulder straps (used in pairs) are used in conjunction with the lap belt Bagu FAG-9D.

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6. Operation

A. Aircraft Seat Belt Combination Comprising Bagu FAG-9C and Schugu FAG-9A (1) Installation

The automatic inertia reels, acting as attachment fittings for the two lap belt portions and shoulder straps, are mounted on the seat in accordance with the installation instructions supplied by the seat manufacturer. The lap belt portion carrying the buckle MS-1 is to be installed on the left-hand side seen from the seated position. To ensure correct installation and operation the shoulder straps are marked R and L. Following installation all belt portions are to be subjected to a functional check observing the sequence given below: CAUTION: DO NOT ALLOW THE STRAPS TO BE WOUND UP UNRESTRAINED (a) When pulled slowly and uniformly, all belt portions must permit full extension without

any locking action occurring. When released, all belt portions must be fully retracted. (b) When a belt portion is withdrawn with a sudden jerk, the inertia reel must block the

movement of the belt at any point along its full length. When releasing the belt, the locking action must automatically be released.

(c) The lug of the lap belt is to be inserted into the buckle MS-1. The correct locking

action of the buckle is to be checked by applying tension to the lug ensuring that the lug is securely held by the latch block of the buckle.

(d) When the cover of the buckle is lifted by more than 45 lug must be released so that

the lug can be withdrawn from the buckle. When released, the cover must automatically return to the closed position.

(2) Fastening

When fastening the aircraft seat belt combination proceed as follows: (a) In the seated position grasp the lug of the right-hand lap belt using the right hand and

pull the lug over to the center of the body. (b) Using the left hand pull down the right-hand shoulder strap and pass the lug over the

upper tongue of the lap belt lug. Place the thumb over the lug to prevent the lugs from separating.

(c) Using the left had pull down the left hand shoulder strap and pass the lug over the

upper tongue of the lap belt lug. Place the thumb over the lug to prevent the lugs from separating.

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(d) Using the left hand pull the buckle of the left-hand lap belt over the center of the body

and insert the lap belt lug into the buckle. Note: The buckle should be located at the center of the body when the automatic

inertia reels have taken up the slack in the belts. (d) Release CAUTION: DO NOT ALLOW THE STRAPS TO BE WOUND UP UNRESTRAINED. For the release of the aircraft seat belt combination lift the cover of the buckle by more than 45 so that the lug can be withdrawn from the buckle.

(d) Aircraft Seat Belt Combination Comprising Bagu FAG-9D and Schugu FAG-9D

(d) Installation

Installation of the lap belts is by means of seat connection fittings, whereas the shoulder straps are fitted to the seat by means of the automatic inertia reels. The installation is in accordance with the installation instructions supplied by the seat manufacturer. When in- stalling the lap belt ensure that in the seated position the lap belt portion carrying the rotary buckle is on the side of the seat which is facing the central gangway. In this position the release plate of the rotary buckle used for releasing the shoulder strap lugs must point upwards.

Following installation all belt portions are to be subjected to a functional check observing the sequence given below. CAUTION: DO NOT ALLOW THE STRAPS TO BE WOUND UP UNRESTRAINED.

(d) When pulled slowly and uniformly, the shoulder straps must permit full extension without any locking action occurring.

(b) When a shoulder strap is withdrawn with a sudden jerk, the inertia reel must block

the movement of the belt at any point along its full length. When releasing the belt, the locking action must automatically be released.

The loose lug of the lap belt is to be inserted into the lateral slot of the rotary buckle.

The two lugs of the shoulder straps are to be inserted into the upper slots of the rotary buckle. The correct locking action of the buckle is to be checked by pulling at the belts.

(d) Adjustability of the lap belt portions is to be checked by operating the sewn-in-sliding

buckles. CAUTION: DO NOT ALLOW THE STRAPS TO BE WOUND UP UNRESTRAINED.

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(e) The loose lugs must be released irrespective to the sense of rotation of the rotary disc of the buckle. Apart from this it must be possible to release the two shoulder strap lugs by pressing the release plate towards the front.

After rotation of the rotary disc it must automatically return to its initial position when released.

(2) Fastening When fastening the aircraft seat belt combination proceed as follows: In the seated position grasp the rotary buckle with one hand and position it over the center

of the body. Using the other hand bring over the lug of the opposite lap belt and insert the lug in the lateral slot of the rotary buckle. Adjust the length of the lap belt portions by

pulling at the free belt ends ensuring that the rotary buckle takes up a ventral position and that the lap belts pass over the pelvis.

Lengthening of the lap belt portions is by lifting the tongue on the sliding buckle while simultaneously pulling on the belt. Withdraw the shoulder straps from the inertia reels and insert the lugs in the upper slots of the rotary buckle between the rotary disc and the release plate. (3) Release CAUTION: DO NOT ALLOW THE STRAPS TO BE WOUND UP UNRESTRAINED. For the release of the aircraft seat belt combination turn the rotary disc of the buckle by approx. 45 in either direction to release the lugs.

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TESTING AND FAULT ISOLATION

1. GENERAL

No testing and trouble shooting is applicable when the aircraft seat belt combination is installed or removed in accordance with the instructions given under section Operation.

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DISASSEMBLY 1. Task

Before you disassemble the Restraint System, use TESTING AND FAULT ISOLATION to examine its condition or to find the most probable cause of its malfunction. This is to prevent disassembly that is not necessary. Do only those procedures of disassembly that are necessary to remove defective parts and to correct malfunctions. Damaged or unserviceable aircraft seat belt combinations are to be removed from the seat in accordance with the instructions supplied by the seat manufacturer and passed on for overhaul. When damaged, the following item may be removed from the aircraft seat belt combination: -Rotary buckles -Automatic inertia reels -Fitting and sliding buckles attached to webbing to data sheet AFG-5030 Repair/overhaul of aircraft seat belt combinations must only be carried out by the manufacturer of by Qualified agencies specially approved by the aviation authorities.

2. Equipment and Materials NOTE: Equivalent alternatives are permitted for the equipment and materials in this list. Spring plate 3 x 0.5 x 0.024 in (7.62 x 1.27 x 0.6 mm) Make locally 3. Procedure NOTE: Figure reference are to the IPL. A. Turn the handle on the rotary buckle assembly (10 or 30, IPL figure 1) to release the straps that are

not locked. B. Release the locked belt/strap (5, 15, 25 or 35) from the rotary buckle assembly (10 or 30).

(1) Put the spring plate behind the connector of the locked belt/strap.

(2) Insert the spring plate in the slot on the rotary buckle assembly (10 or 30) to release the pawl. (3) Remove the belt/strap and the spring plate from the rotary buckle.

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(1) Automatic Inertia Reel

(1) Removal of Automatic Inertia Reel for cleaning or replacing straps.

(a) Fully extend the strap, immobilize the spindle in this position, push the webbing end by

appr. 30 mm (1.18 in.) through the spindle slot, remove the pin to one side from the webbing loop , pull the strap out of the spindle slot and insert a suitable tool into the spindle slot to prevent the spindle from rotating.

(1) Dismantling of Automatic Inertia Reel for Repair.

(a) Refer to the relevant CMM 25-21-44

(1) Fitting and Sliding Buckles.

CAUTION: RESTITCHING AND/OR THE REPLACEMENT OF DAMAGED FITTINGS AND MS-1

BUCKLES ATTACHED TO WEBBING TO DATA SHEET AFG-5012 IS NOT PERMITTED. IN THIS CASE, THE DAMAGED FITTING AND/OR THE MS-1 BUCKLES AS WELL AS THE WEBBING, HAVE TO BE REPLACED.

(1) Remove fitting and/or sliding buckles by carefully opening the respective stitching.

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CLEANING

5. Task

To clean the aircraft seat belts, remove dirt and unwanted oil and grease. This helps the aircraft seat belts to last longer and prevents corrosion of the metal parts. Before you clean the aircraft seat belt, follow the instructions in the DISASSEMBLY section to remove the rotary buckle assembly and inertia reel assembly. The webbing is cleaned with fresh water and mild soap. The metal fittings are cleaned with a cloth moist with isopropyl alcohol. After you clean the assemblies and parts, protect them from moisture, dirt, or other contamination, Keep them protected until you do a visual check and assemble the aircraft seat belts.

2. Equipment and Materials WARNING: BEFORE YOU USE A MATERIAL, YOU MUST KNOW THE HAZARD CODE AND GET

THE NECESSARY PROTECTION. REFER TO THE PAGE ABOUT HAZARD CODES FOR MATERIALS IN THE FRONT OF THIS MANUAL.

NOTE: Equivalent alternatives are permitted for the equipment and materials in this list. Isopropyl Alcohol Optional source, HAZARD CODE 130D Mild Soap, Non-alkaline NILIN4M, Optional source Cloth, lint-free Optional source 3. Procedure CAUTIONS: 1. THE FIRST TIME A BELT IS WASHED, SHRINKAGE UP TO 15% MAY RESULT. SHINKAGE WILL DIMINISH WITH REPEATED WASHINGS. 2. THE DETERGENT MUST BE NON-ALKALINE. ALKALINE DETERGENT WILL

DAMAGE THE WEBBING COMPONENTS. 3. THE TEMPERATURE OF THE WATER IN THE WASHING MACHINE MUST NOT

EXCEED + 104 F (+ 40 C) (313.15K). WATER THAT IS TOO HOT WILL DAMAGE THE WEBBING COMPONENTS.

4. WHEN WASHING THE SEAT BELT, USE ADDITIONAL TEXTILE FILLLING

MATERIAL IN THE WASHING MACHINE OR PUT THE SEAT BELT INTO A SACKS.

5. MAKE SURE THAT THE LINE AND THE CLOTH WILL NOT LOOSEN IN THE

WASHING MACHINE. THIS WILL PREVENT DAMAGE CAUSE BY RUBBING IN THE MACHINE.

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A. Clean the webbing. (1) Use a piece of line to hold the connector halves. (2) Attach pieces of cloth to cover the metal fittings. (3) Wash the two connector halves in a mixture of the mild detergent and water. CAUTION: DO NOT DRY THE AIRCRAFT SEAT BELTS IN SUNLIGHT OR NEAR A SOURCE OF HEAT. (4) Dry the two connector halves in an are that has a good flow of air. (5) Inspect the dry aircraft seat belts. B. Clean the metal fittings with a lint-free cloth moist with isopropyl alcohol.

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INSPECTION/CHECK 1. General

Servicing of the aircraft seat belt combination is in accordance with the on condition principle and is governed by an inspection and servicing schedule. The equipment will remain in service until defects are noticed on the occasion of inspection or during use or until the service life has been expired.

A. Servicing Responsibility

Servicing of the aircraft seat belt combination is to be performed by qualified aircraft ground personnel or by authorized inspectors.

B. Scope

After cleaning a visual examination of the webbing and fittings is to performed. Buckles and inertia reels are to be subjected to a functional check. If cleaning is not carried out regularly, these checks have to be performed at intervals not exceeding 12 months. In the case of malfunctions or if strength deterioration or impairment of operational safety cannot be excluded, the respective belt, together with its fittings, is to be removed and passed on for overhaul or must be discarded respectively. The defective belt is to be replaced by a serviceable one.

2. Equipment and Materials Item No. Designation Spec./P/N 1 Letterscales Commercial grade 2 Grease NATO G353 OR EQUIVALENT 3. Inspection Procedure A. Aircraft Seat Belt Combination Comprising Bagu FAG-9C and Schugu FAG-9A (1) Webbing and Fittings

(a) Deleted. (b) Visually examine the webbing for damaged stitching, injurious marks, broken fabric

threads, tears, chafe marks, residual contamination, dampness, wear, fusings serviceability and legibility of the inscriptions.

NOTE: Slight wear and roughening of the webbing may be ignored. Cut or worn

edges, however, make the webbing unserviceable.

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(c) Visually inspect the fittings for cracks, abrasion, corrosion, deformation, fractures, correct functioning of moveable parts, serviceability and surface finish conditions. (2) Inertia Reel CAUTION: DO NOT ALLOW THE STRAPS TO BE WOUND UP UNRESTRAINED. (a) Deleted. (b) Visually inspect the automatic inertia reel for external damage, secure fit of the two plastic

covers, deformation, cracks, abrasion, corrosion, fractures, completeness, serviceability and legibility of the inscriptions.

(c) After reassembling the automatic inertia reel withdraw the belt slowly and uniformly and

check that the belt permits full extension without any locking action occurring. When released, the belt must be fully retracted. (d) Withdraw the belt and check the correct locking action of the automatic inertia reel by

jerking the belt several times at various positions along its full length. (3) Buckle Assembly MS-1/D (a) Visually examine the buckle for cracks, abrasion, corrosion, serviceability, deformation,

fractures, surface finish condition and legibility of the inscriptions. (b) As a functional check insert the lug into the buckle MS-1 and apply tension to the lug

ensuring that the lug is securely held by the latch block. NOTE: The engagement of the latch block with the two rectangular recesses in the lug

is audible and can also be checked from the underside of the buckle. (c) Hold the buckle, lug inserted, in a vertical position with the lug pointing downwards. Lift the cover and allow the lug to fall clear of the buckle. The lug should be released at an

opening angle of the cover to approx. 45. (d) Open the cover to approx. 180 and press the latch block against it. When released, the latch block, under the action of the spring, must be forced against

both stops on the cover. Let the cover automatically return to the closed position. (e) When cleaning of the seat belts has been performed, open the buckle cover to 180 and

using a suitable brush, apply a thin coat of grease NATO-G353 to the portion of the torsion spring facing the latch block.

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B. Aircraft Seat Belt Combination Bagu FAG-9D and Schugu FAG-9D (1) Webbing, Fittings and Sliding Buckles

(d) Deleted.

(d) Visually examine the webbing for damaged stitching, injurious marks, broken fabric threads, tears, chafe marks, residual contamination, dampness, wear, fusings, service-

ability and legibility of the inscriptions. NOTE: Slight wear and roughening of the webbing may be ignored. Cut or worn

edges, however, make the webbing unserviceable.

(d) Visually check the fittings and sliding buckles for cracks, abrasion, corrosion, correct functioning of movable parts, serviceability and surface finish conditions.

(d) Automatic Inertia Reel

Follow the instructions as given under section INSPECTION/CHECK, paragraph 3.A. (2).

(d) Rotary Buckle

(d) Visually examine the rotary buckle for cracks, abrasion, corrosion, deformation, fractures, surface finish condition and legibility of the inscriptions.

(d) As a functional check insert all lugs into the rotary buckle and apply tension to the lugs

ensuring the lugs are securely held by the claws. NOTE: The engagement of the claw with the recess in the lug is audible.

(d) All lugs except the fixed one must be released by approx. 45 irrespective of the sense of rotation of the rotary disc of the buckle.

When released after operation the rotary disc of the buckle must automatically return to

within 3 of its initial position. (d) Insert the two lugs of the shoulder straps into the rotary buckle and hold the rotary buckle

in a vertical position with the shoulder straps pointing downwards. Press the release plate of the rotary buckle towards the front and allow the lugs to fall

clear.

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4. Inspection for Continued or Renewed Airworthiness A. General

Inspection of the restraint system is in accordance with the on condition principle and is governed by an inspection and servicing schedule. The restraint system may remain in service until defects are found upon inspection or in use. As a minimum, AmSafe recommends a yearly inspection of the restraint. system. The continued use of the restraint system is subject to the routine inspection interval of the airframe by conducting a functional inspection check of the restraint system in accordance with the procedures listed in the TESTING AND FAULT ISOLATION and CHECK sections of this CMM. The service life of the restraint system is subject to the periodic inspection of the restraint system while in service and depends on the service environment in which it is used and the degree of use over the installation period. This subsequently places the responsibility for the continued airworthiness of the restraint on the installer/operator since the flight times, usage, and operating environment will vary by operator. The frequency of the inspection interval should be adjusted appropriately by the installer/operator to ensure the continued airworthiness of the restraint. If the restraint is no longer usable based on the inspection for continued or renewed airworthiness, itthe restraint system must be discarded or returned to AmSafe or an AmSafe approved repair station for overhaul/repair.

(1) Inspection Intervals:

- Concurrently with the periodic aircraft inspection, but not later than every 42 months,

plus an admissible tolerance of 6 months. - After repairs or overhaul.

- After modifications requiring qualification testing.

- When the equipment is transferred to another owner or for any special reason.

- When the equipment has been overstressed, or if overstress is suspected.

- Concurrently with the aircraft inspection.

- After removal from storage.

(2) Deleted.

(3) Inspection Responsibility

Inspection of aircraft seat belt combinations must only be carried out by the manufacturer, or by agencies specially approved by the aviation authorities.

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B. Inspection Procedure for Aircraft Seat Belt Combination Comprising Bagu FAG-9C and Shugu FAG-9A (1) Webbing and Fittings Follow the instructions as given under section INSPECTION/CHECK, paragraph 3.A.(1). (2) Automatic Inertia Reel Follow the instructions as given under section INSPECTION/CHECK, paragraph 3.A.(2). (3) Buckle Assembly MS-1/D

(a) Follow the instructions as given under section INSPECTION/CHECK, paragraph 3.A.(2).

(b) Check the force required to open the buckle. For this purpose open the cover of the

buckle at right angles to the housing bottom and place the cover in this position on letterscales.

The force registered should be approx. 0.39 daN (.9lb). In addition to this check that with the buckle in the closed position the two studs of the

latch block are in contact with the housing bottom. Check also that the cover, within its idle travel of 10, is pressed against the spindle with sufficient spring force.

C. Inspection Procedure for Aircraft Seat Belt Combination Comprising Bagu FAG-9D and Shugu

FAG-9D (1) Webbing, Fittings and Sliding Buckles Follow the instructions as given under section INSPECTION/CHECK, paragraph 3.B.(1). (2) Automatic Inertia Reel Follow the instructions as given under section INSPECTION/CHECK, paragraph 3.A.(2). (3) Rotary Buckle Follow the instructions as given under section INSPECTION/CHECK, paragraph 3.B.(3). 5. Deleted.

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6. Certification When the inspection checks of the aircraft seat belts have been satisfactorily completed, the inspection stamp and inspection date are to be stamped on the webbing in the vicinity of the identification labels. The inspector has to prepare an inspection certificate in triplicate. If the aircraft seat belts fail the inspection checks, the inspector has to prepare an overhaul order, sign it and pass the respective belt on for overhaul.

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REPAIR / OVERHAUL 1. General

The repair/overhaul of aircraft seat belt combinations becomes necessary: - in the case of malfunctions, or if strength deterioration or impairment or operational safety cannot

be excluded. - in the event of defects found when using the seat belts in accordance with section DESCRIPTION

AND OPERATION, when inspecting the seat belts in accordance with section INSPECTION/CHECK.

CAUTION: RESTITCHING AND/OR THE REPLACEMENT OF DAMAGED FITTINGS AND MS-1

BUCKLES ATTACHED TO WEBBING TO DATA SHEET AFG-5012 IS NOT PERMITTED. IN THIS CASE, THE DAMAGED FITTING AND/OR THE MS-1 BUCKE AS WELL AS THE WEBBING HAVE TO BE REPLACED.

No special tools, fixtures or specific equipment is required for maintenance or overhaul work to be carried out on the seat belts. Standard tools are sufficient for these operations. 2. Repair/Overhaul Responsibility

Repair/overhaul of aircraft seat belt combinations must only be carried out by the manufacturer or by qualified agencies specially approved by the aviation authorities.

3. Equipment and Materials Item No. Designation Spec./P/N 1 Grease NATO G353 OR EQUIVALENT 2 Thread (For determination of E000207 P/N and color refer to IPL)

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4. Repair/Overhaul Instructions A. Restitching (Ref. Fig. 601) (1) Whenever fittings are to be replaced or the stitching of seams is broken, the old seam must be

carefully opened. The defective component is to be replaced by a serviceable one and the seam re-sewn.

(2) If a strap to data sheet 5030 is to be replaced, a new strap having the same dimensions is to

be used with the old strap serving as template. (3) Sewing of the lap belts is to be carried out in accordance with the stitching pattern shown in

Fig. 601.

Stitching pattern: Stitching pattern: Automatically sewn seam, Automatically sewn seam, 72 stitches, comprising 72 stitches, comprising - 65 Stepping stitches - 67 Stepping stitches - 5 Overstitches - 3 Overstitches (Locking stitches) (Locking stitches) - 2 Attachment stitches - 2 Attachment stitches Thread: Refer to the IPL Thread: Refer to the IPL

Stitching pattern:

Automatically sewn seam, 29 stitches, comprising - 24 Stepping stitches - 3 Overstitches (Locking stitches) - 2 Attachment stitches Thread: Refer to the IPL

Stitching Patterns

Figure 601

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B. Automatic Inertia Reel Overhaul operations are to be performed in accordance with the instructions contained in the automatic inertia reel CMM 25-21-44. C. Buckles No provisions are made for the overhaul of the rotary buckle and for the MS-1/D buckle assembly, as overhaul would be uneconomical. Unserviceable buckles, plastic loops or lugs are to be replaced by serviceable ones.

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LEFT BLANK

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ASSEMBLY (INCLUDING STORAGE)

(3) Equipment and Materials Item No. Designation Spec./P/N 1. Spring tensioning tool (if required) AFG0185430 2. Sticker (if required) AFG012509 2. Assembly

(4) Fitting the Strap to the Automatic Inertia Reel (Ref. Fig. 701)

(5) Pass the looped end of the strap far enough through the smaller slot in the spindle so that the pin can be inserted into the webbing loop.

Ensure that the loose portion of the strap end E faces the spindle.

(6) Secure the strap by pulling the looped end into the insert ensuring that the pin lies inside the spindle circumference.

CAUTION: DO NOT ALLOW THE STRAP TO BE WOUND UP UNRESTRAINED.

(7) Remove the tool used to prevent the spindle from rotating and allow the strap to be slowly retracted.

NOTE: When rolling up the strap ensure that the loose portion of the strap end E

faces the spindle.

(8) Fitting the Strap to Replacement Automatic Inertia Reel (Ref. Fig. 701) NOTE: Automatic inertia reels supplied or returned without seat belt are dispatched with the

sticker, which is normally fitted to the return spring cover, accompanying the automatic inertia reel as a loose item and with the return spring in the relieved condition.

(9) Insert the spring tensioning tool, P/N AFG0185430, thought the hole in the return spring cover,

ensuring that the slot in the tool passes over the inner end of the return spring.

(10) Turn the tensioning tool clockwise against the stop and give 1 to 2 turns in the opposite direction and immobilize the spindle in this position.

(11) Pass the looped end of the strap far enough through the smaller slot in the spindle so that the

pin can be inserted into the webbing loop. Ensure that the loose portion of the strap end E faces the spindle.

(12) Secure the strap by pulling the looped end into the insert ensuring that the pin lies inside the spindle circumference.

CAUTION: DO NOT ALLOW THE STRAP TO BE WOUND UP UNRESTRAINED.

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(5) Remove the tensioning tool and allow the strap to be slowly retracted. NOTE: When rolling up the strap ensure that the loose portion of the strap end E

faces the spindle. (6) Close the opening in the return spring cover using the supplied sticker.

Strap Installation Figure 701

3. Storage

A. Aircraft seat belts are to be protected for dampness, direct sunlight, contamination and chemicals. Sealing of the seat belts in plastic foil etc. must be carried out under low humidity conditions.

B. Stored seat belts are to be inspected every 24 months. The inspection is to be performed as

outlined in chapter INSPECTION/CHECK, section 3. Inspection Procedure.

C. Prior to installation, stored seat belts taken from store are to be subjected to an inspection as outlined in chapter INSPECTION/CHECK, section 3. Inspection Procedure.

D. Deleted.

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FITS AND CLEARANCES

NOT APPLICABLE

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SPECIAL TOOLS, FIXTURES, AND EQUIPMENT

This subheading gives all the tools, fixtures, and equipment specified in other subheadings. They are necessary to do the maintenance on the Restraint System. The applicable subheading shows the materials used during maintenance. Am-Safe provides the data that follows so you can get all of the equipment listed, or you can substitute equivalent equipment. The code in parentheses is the Commercial And Government Entity (CAGE) code. Refer to table 901 for manufacturer location data. NOTE: Equivalent alternatives are permitted for the equipment in this list. This equipment can be fabricated locally per Figure 901.

Steel spring plate 0.024 in (0.06 mm) thickness.

Spring Plate Figure 901

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LEFT BLANK

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ILLUSTRATED PARTS LIST

INTRODUCTION 1. General The purpose of the Illustrated Parts List is to list the items necessary for the support of the unit. It may be

used for requisitioning, issuing and identifying parts. 2. Numerical Index The Numerical Index is a listing of all part numbers used in the Detailed Parts List. Classification is made from left to right side, each digit (letter, numerical) being considered separately. For the first left row the sequence is: - Letters A to Z ( except the O letter considered as zero) - Numerals 0 to 9 3. Detailed Parts List The detailed nomenclature gives the parts list and illustrations for components of the assembly

considered. To determine the next higher assembly for a part or assembly note the column in which the first word of the nomenclature begins; the first item directly above which appears on column to the left is the next higher assembly.

An example of the next higher assembly relationship, indicated by the indenture method, is as follows: 1234567 Assembly or Installation Assembly (RF) number Attaching parts for assembly or installation of R.F. Assembly *** Detail parts for assembly Sub-sub-assembly Attaching parts for sub-sub-assembly *** Detailed parts for sub-sub-assembly

I.P.L.Introduction page 1

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How to use this Illustrated Parts List If neither the part number nor the nomenclature is known, the part can be found by comparison with the

exploded view illustration. When located on the Illustration, the index number will refer to the line in the Illustrated Parts List with the part number and the nomenclature.

How to determine the applicable EFF CODE Part numbers covering parts that are only used in specific assemblies are followed by a letter symbol

indicated in the EFF CODE column. If applicable, an explanation of the letter symbols used is outlined below. In cases where the EFF

CODE column has been left blank, parts listed are common to all assemblies. 4. Vendor Codes and Addresses A part manufactured by a company other than Am-Safe is identified by a Vendor Code, following the

nomenclature. Vendor Codes and Addresses applicable to this I.P.L. will be found in Table I. If difficulty is experienced in obtaining vendor items, contact Am-Safe for assistance.

Code No Name Address 45402 Pacific Scientific Co. 22715 Saui Ranch Pky HTL/KIN Tech Div. P.O. Box 87019 Yorba Linda CA 92686 USA

Vendor Codes Table I

I.P.L. Introduction page 2

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PART NUMBER AIRLINE PART NO,

FIG. ITEM TTL REQ.

AFG000470 AFG011459 AFG011532 AFG011533 AFG011534 AFG011535 AFG011550 AFG011556 AFG012072 AFG012073 AFG012074 AFG012444 AFG012509 AFG012516 AFG012517 AFG012518 AFG012519 AFG012520 AFG012521 AFG012535 AFG012849 AFG013913

2 2 3 3 4 4 5 5 1 1 1 1 1 6 6 6 6 6 6 1 1 6 6 7 1 1 6 6 7 6 6 6 6 1 1 6 6 2 2 3 3 4 4 5 5 7

40 130 40 130 40 130 40 130 20 70 1 10 60 10 60 1 -1A -10A -60A -30 -80 -30 -80 -30 -40 -90 -40 -90 -40 -50A -100A 50 100 50 100 20 70 30 140 30 140 30 140 30 140 20

1 1 1 1 1 1 1 1 1 1 RF 1 1 1 1 RF RF 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1

Numerical index page 1

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FIG. ITEM TTL REQ.

AFG014140 AFG014141 AFG014544 AFG014620 AFG014621 AFG014622 AFG014623 AFG014878 AFG014879 AFG016995 AFG016996 AFG016997 AFG017015 AFG017016 AFG017017 AFG0174342 AFG0176076 AFG0306980 AFG0306998 AFG0307005 AFG0307010 AFG0307028 AFG0307033 AFG0307040 AFG0307058 AFG0307063 AFG0307070 AFG0307086 AFG0307093 AFG0307100 AFG0307115 AFG0307122 AFG0307138 AFG0308163 AFG0309843 AFG0310327 AFG0310340 AFG0318641 AFG0318659 AFG0318671 AFG0318687 AFG0318694 AFG0318700

7 2 3 2 2 3 3 7 7 2 2 2 3 3 3 7 7 7 7 4 4 4 5 5 5 7 7 2 2 2 3 3 3 4 4 5 5 7 7 7 7 7 4 4 4 5

1 1 1 10 90 10 80 10 50 -1A -10A -90A -1A -10A -80A -1A -10A -1B -10B 1 10 90 1 10 80 -1C -10C -1B -10B -90B -1B -10B -80B 20 150 20 150 -50B -50C -50A -1D -10D -1A -10A -90A -1A

RF RF RF 1 1 1 1 2 1 RF 1 1 RF 1 1 RF 2 RF 2 RF 1 1 RF 1 1 RF 2 RF 1 1 RF 1 1 1 1 1 1 1 1 1 RF 2 RF 1 1 RF


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FIG. ITEM TTL REQ.


5 5 7 7 2 2 2 3 3 3 7 7 3 3 7 7 7 7 4 4 4 5 5 5 7 7 2 2 2 3 2 4 3 5 7 7 7 7 4 4 4 5 5 5 7

-10A -80A -1E -10E -1C -10C -90C -1C -10C -80C -50D -50E -10D -80D -50F -50G -1F -10F -1B -10B -90B -1B -10B -80B -1G -10G -1D -10D -90D -1D 80 80 90 90 -50L -1H -10H -50H -1C -10C -90C -1C -10C -80C -1J

1 1 RF 2 RF 1 1 RF 1 1 1 1 1 1 1 1 RF 2 RF 1 1 RF 1 1 RF 2 RF 1 1 RF 1 1 1 1 1 RF 2 1 RF 1 1 RF 1 1 RF


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FIG. ITEM TTL REQ.

AFG0364937 AFG0364944 AFG0364951 AFG0364967 AFG0364974 AFG0364980 AFG0364997 AFG0365006 AFG0391349 AFG0396655 AFG0396660 AFG0414652 AFG0418778 AFG0452937 AFG0452944 AFG0452951 AFG0452967 AFG0452974 AFG0452980 AFG0454660 AFG0454678 AFG0454683 AFG0455063 AFG0455070 AFG0455086 AFG0455093 AFG0455100 AFG0455115 AFG0455122 AFG0455138 AFG0455145 AFG0455152 AFG0455168 AFG0455175 AFG0471650 AFG0471665 AFG0471672 AFG0471782 AFG0471790 AFG0471808 AFG0475798 AFG0475806 AFG0475811 AFG0476726 AFG0476731

7 7 2 2 2 3 3 3 7 7 7 7 7 7 4 5 7 2 3 7 7 7 4 4 5 5 2 2 3 3 7 7 7 7 7 7 7 7 7 7 7 7 7 7 7

-10J -50J -1E -10E -90E -1E -10E -80E -1K -10K -50K -1L -10L -1M -1D -1D -1N -1F -1F -1P -10P -50P -10D -90D -10D -80D -10F -90F -10F -80F -10M -50M -10N -50N -1Q -10Q -50Q -10R -1R -50R -1S -50S -10S -1T -10T

2 1 RF 1 1 RF 1 1 RF 2 1 RF 2 RF RF RF RF RF RF RF 2 1 1 1 1 1 1 1 1 1 2 1 2 1 RF 2 1 2 RF 1 RF 1 2 RF 2


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FIG. ITEM TTL REQ.


7 7 7 7 7 7 7 7 7 7 7 7 7 7 7 7 7 7 7 7 7 7 4 4 4 5 5 5 7 7 7 7 7 7 7 7 7 4 4 4 5 5 5

-50T -1U -10U -50U -1V -10V -50V -1W -10W -50W -1X -10X -50X -1Y -10Y -50Y -1Z -10Z -50Z -1AA -10AA -50AA -1E -10E -90E -1E -10E -80E -1AB -10AB -50AB -1AC -10AC -50AC -1AD -10AD -50AD -1F -10F -90F -1F -10F -80F

1 RF 2 1 RF 2 1 RF 2 1 RF 2 1 RF 2 1 RF 2 1 RF 2 1 RF 1 1 RF 1 1 RF 2 1 RF 2 1 RF 2 1 RF 1 1 RF 1 1


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PART NUMBER AIRLINE

PART NO, FIG. ITEM TTL

REQ. AFG0533462 AFG0533470 AFG0533485 AFG0533492 AFG0533509 AFG0533514 AFG0533521 AFG0533537 AFG0533544 AFG0533551 AFG0533567 AFG0533574 AFG0533580 AFG0533597 AFG0533605 AFG0570010 AFG0570027 AFG0570032 AFG0570040 AFG0570057 AFG0570062 AFG0570070 AFG0570085 AFG0570092 AFG0570109 AFG0570114 AFG0570121 AFG40691 170694 283227 442536

4 4 4 5 5 5 7 7 7 7 7 7 7 7 7 7 7 7 7 7 7 4 4 4 5 5 5 2 2 3 3 2 3 5 5 2 2 3 3 4 4 5 5

-1G -10G -90G -1G -10G -80G -1AE -10AE -50AE -1AF -10AF -50AF -1AG -10AG -50AG -1AH -10AH -50AH -1AJ -10AJ -50AJ -1H -10H -90H -1H -10H -80H 20 150 20 150 -50D -110D 50F 110D -50A -110A -50A -110A 50 110 50 110

RF 1 1 RF 1 1 RF 2 1 RF 2 1 RF 2 1 RF 2 1 RF 2 1 RF 1 1 RF 1 1 1 1 1 1 A/R AR AR AR AR AR AR AR AR AR AR AR


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FIG. ITEM TTL REQ.

448540 501911 501913 501932 502502 503749-1

2 2 3 3 4 4 5 5 5 5 5 5 2 2 3 3 2 2 3 3 4 4 5 5 2 2 3 3 4 4 5 5 2 2 3 3 4 4 5 5

-50B -110B -50B -110B -50B -110B -50B -110B -50F -50E -50A -110A 50 110 50 110 -50C -110C -50C -110C -50C -110C -50C -110C 70 100 70 100 70 100 70 100 60 120 60 120 -60A -120A -60A -120A

AR AR AR AR AR AR AR AR AR AR AR AR AR AR AR AR AR AR AR AR AR AR AR AR 1 1 1 1 1 1 1 1 AR AR AR AR AR AR AR AR


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FIG. ITEM TTL REQ.

503749-2 503749-3 503749-6 503749-7 503749-8 503749-10 503749-11

2 2 3 3 4 4 5 5 2 3 3 4 4 5 5 2 4 4 4 4 5 5 2 2 3 3 4 4 5 5 4 4 5 5 4 4 5 5 4 4 5 5

-60C -120C -60C -120C -60C -120C -60C -120C -120D -60D -120D -60D -120D -60D -120D -60D -50A -110A -60G -120G -60G -120G -60B -120B -60B -120B -60B -120B -60B -120B -60H -120H -60H -120H -60E -120E -60E -120E -60F -120F -60F -120F

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


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DETAILED PARTS LIST

Page 1001

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NOTE: Refer to figure 6 for proper shoulder straps.

Lap Belt, Bagu FAG-9C Figure 1

Page 1002

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FIG. ITEM

PART NUMBER

NOMENCLATURE 1234567

EFF CODE

UNITS PER ASSY

1- 1 10 20

-30 -40 50 60 70

-80 -90 100

AFG011532 AFG011533 AFG011459 AFG012444 AFG012509 AFG012520 AFG011534 AFG011459 AFG012444 AFG012509 AFG012521

LAP BELT, BAGU FAG-9C, SILVERGREY .BELT, LAP, RH ..REEL, INERTIA, AUTOMATIC, AGB-8C ..PIN ..STICKER (FOR INERTIA REEL COVER) ..BELT, LAP, RH .BELT, LAP, LH ..REEL, INERTIA, AUTOMATIC, AGB-8C ..PIN ..STICKER (FOR INERTIA REEL COVER) ..BELT, LAP, LH

RF 1 1 1 1 1 1 1 1 1 1

-ITEM NOT ILLUSTRATED

Page 1003

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Lap Belt, Bagu FAG-9D-13 (Buckle on RH Belt)

Figure 2

Page 1004

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FIG. ITEM

PART NUMBER


EFF CODE

UNITS PER ASSY

2- 1

-1A

-1B

-1C

-1D

-1E

-1F

10 -10A -10B -10C -10D -10E -10F

20 30 40 50

-50A

-50B

-50C

-50D

60

-60A -60B -60C -60D

70 80 90

-90A -90B -90C

AFG014141 AFG016995 AFG0307086 AFG0318769 AFG0334840 AFG0364951 AFG0452974 AFG014620 AFG016996 AFG0307093 AFG0318776 AFG0334857 AFG0364967 AFG0455100 AFG40691 AFG012849 AFG000470 501913 442536 448540 501932 179064 503749-1 503749-4 503749-7 503749-2 503749-3 502102 AFG0341279 AFG014621 AFG016997 AFG0307100 AFG0318781

LAP BELT, BAGU FAG-9D-13, SILVERGREY, BUCKLE ON RH BELT LAP BELT, BAGU FAG-9D-13, SILVERGREY, BUCKLE ON RH BELT LAP BELT, BAGU FAG-9D-13, BROWN, BUCKLE ON RH BELT LAP BELT, BAGU FAG-9D-13, SILVERGREY, BUCKLE ON RH BELT LAP BELT, BAGU FAG-9D-13, BLACK, BUCKLE ON RH BELT LAP BELT, BAGU FAG-9D-13, TAN, BUCKLE ON RH BELT LAP BELT, BAGU FAG-9D-13, NAVYBLUE, BUCKLE ON RH BELT .BELT, LAP, RH .BELT, LAP, RH .BELT, LAP, RH .BELT, LAP, RH .BELT, LAP, RH .BELT, LAP, RH .BELT, LAP, RH ..HOOK, SNAP ..BUCKLE, SLIDING ..LOOP, PLASTIC ..THREAD, NYLON, SILVER, E000207 ..THREAD, NYLON, BROWN, E000207 ..THREAD, NYLON, BLACK, E000207 ..THREAD, NYLON, LT.SANDSTONE E000207 ..THREAD, NYLON, LT. CASHMERE, E000207 ..WEBBING, SILVERGREY, AFG-5030 ..WEBBING, BROWN, AFG-5030 ..WEBBING, BLACK, AFG-5030 ..WEBBING, TAN, AFG-5030 ..WEBBING, NAVYBLUE, AFG-5030 ..LUG (V.45402, P/N 1101212) ..BUCKLE, ROTARY .BELT, LAP, LH .BELT, LAP, LH .BELT, LAP, LH .BELT, LAP, LH

A B C D E F G A B C D E F G A,B,D C E,G F G A,B,D C E F G A B C D

RF RF RF RF RF RF RF 1 1 1 1 1 1 1 1 1 1 AR AR AR AR AR AR AR AR AR AR 1 1 1 1 1 1

-ITEM NOT ILLUSTRATED Page 1005

FAG-9

September 15, 2011


FIG. ITEM

PART NUMBER


EFF CODE

UNITS PER ASSY

2- -90D -90E -90F 100 110

-110A

-110B

-110C

-110D

120

-120A -120B -120C -120D

130 140 150

AFG0334862 AFG0364974 AFG0455115 502102 501913 442536 448540 501932 179064 503749-1 503749-4 503749-7 503749-2 503749-3 AFG000470 AFG012849 AFG40691

.BELT, LAP, LH

.BELT, LAP, LH

.BELT, LAP, LH

..LUG (V.45402, P/N 1101212)

..THREAD, NYLON, SILVER, E000207 ..THREAD, NYLON, BROWN, E000207 ..THREAD, NYLON, BLACK, E000207 ..THREAD, NYLON, LT.SANDSTONE E000207 ..THREAD, NYLON, LT. CASHMERE, E000207 ..WEBBING, SILVERGREY, AFG-5030 ..WEBBING, BROWN, AFG-5030 ..WEBBING, BLACK, AFG-5030 ..WEBBING, TAN, AFG-5030 ..WEBBING, NAVYBLUE, AFG-5030 ..LOOP, PLASTIC ..BUCKLE, SLIDING ..HOOK, SNAP

E F G A,B,D C E,G F G A,B,D C E F G

1 1 1 1 AR AR AR AR AR AR AR AR AR AR 1 1 1


Page 1006

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September 15, 2011



LEFT BLANK

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September 15, 2011



Lap Belt, Bagu FAG-9D-13 (Buckle on LH Belt)

Figure 3

Page 1008

FAG-9

September 15, 2011


FIG. ITEM

PART NUMBER


EFF CODE

UNITS PER ASSY

3- 1

-1A

-1B

-1C

-1D

-1E

-1F

10 -10A -10B -10C -10D -10E -10F

20 30 40 50

-50A

-50B

-50C

-50D

60

-60A -60B -60C -60D

70 80

-80A -80B -80C

AFG014544 AFG017015 AFG0307115 AFG0318799 AFG0334870 AFG0364980 AFG0452980 AFG014622 AFG017016 AFG0307122 AFG0318807 AFG0334201 AFG0364997 AFG0455122 AFG40691 AFG012849 AFG000470 501913 442536 448540 501932 179064 503749-1 503749-4 503749-7 503749-2 503749-3 502102 AFG014623 AFG017017 AFG0307138 AFG0318812

LAP BELT, BAGU FAG-9D-13, SILVERGREY, BUCKLE ON LH BELT LAP BELT, BAGU FAG-9D-13, SILVERGREY, BUCKLE ON LH BELT LAP BELT, BAGU FAG-9D-13, BROWN, BUCKLE ON LH BELT LAP BELT, BAGU FAG-9D-13, SILVERGREY, BUCKLE ON LH BELT LAP BELT, BAGU FAG-9D-13, BLACK, BUCKLE ON LH BELT LAP BELT, BAGU FAG-9D-13, TAN, BUCKLE ON LH BELT LAP BELT, BAGU FAG-9D-13, NAVYBLUE, BUCKLE ON LH BELT .BELT, LAP, RH .BELT, LAP, RH .BELT, LAP, RH .BELT, LAP, RH .BELT, LAP, RH .BELT, LAP, RH .BELT, LAP, RH ..HOOK, SNAP ..BUCKLE, SLIDING ..LOOP, PLASTIC ..THREAD, NYLON, SILVER, E000207 ..THREAD, NYLON, BROWN, E000207 ..THREAD, NYLON, BLACK, E000207 ..THREAD, NYLON, LT.SANDSTONE E000207 ..THREAD, NYLON, LT. CASHMERE, E000207 ..WEBBING, SILVERGREY, AFG-5030 ..WEBBING, BROWN, AFG-5030 ..WEBBING, BLACK, AFG-5030 ..WEBBING, TAN, AFG-5030 ..WEBBING, NAVYBLUE, AFG-5030 ..LUG (V.45402, P/N 1101212) .BELT, LAP, LH .BELT, LAP, LH .BELT, LAP, LH .BELT, LAP, LH

A B C D E F G A B C D E F G A,B,D C E,G F G A,B,D C E F G A B C D

RF RF RF RF RF RF RF 1 1 1 1 1 1 1 1 1 1 AR AR AR AR AR AR AR AR AR AR 1 1 1 1 1


Page 1009

FAG-9

September 15, 2011


FIG. ITEM

PART NUMBER


EFF CODE

UNITS PER ASSY

3- -80D -80E -80F

90 100 110

-110A

-110B

-110C

-110D

120

-120A -120B -120C -120D

130 140 150

AFG0334217 AFG0365006 AFG0455138 AFG0341284 502102 501913 442536 448540 501932 179064 503749-1 503749-4 503749-7 503749-2 503749-3 AFG000470 AFG012849 AFG40691

.BELT, LAP, LH

.BELT, LAP, LH

.BELT, LAP, LH

..BUCKLE, ROTARY

..LUG (V.45402, P/N 1101212)

..THREAD, NYLON, SILVER, E000207 ..THREAD, NYLON, BROWN, E000207 ..THREAD, NYLON, BLACK, E000207 ..THREAD, NYLON, LT.SANDSTONE E000207 ..THREAD, NYLON, LT. CASHMERE, E000207 ..WEBBING, SILVERGREY, AFG-5030 ..WEBBING, BROWN, AFG-5030 ..WEBBING, BLACK, AFG-5030 ..WEBBING, TAN, AFG-5030 ..WEBBING, NAVYBLUE, AFG-5030 ..LOOP, PLASTIC ..BUCKLE, SLIDING ..HOOK, SNAP

E F G A,B,D C E,G F G A,B,D C E F G

1 1 1 1 1 AR AR AR AR AR AR AR AR AR 1 1 1


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September 15, 2011



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September 15, 2011



Lap Belt, Bagu FAG-9D-26 (Buckle on RH Belt) Figure 4

Page 1012

FAG-9

September 15, 2011


FIG. ITEM

PART NUMBER


EFF CODE

UNITS PER ASSY

4- 1

-1A

-1B

-1C

-1D

-1E

-1F

-1G

-1H

10 -10A -10B -10C -10D -10E -10F -10G -10H

20 30 40 50

-50A

-50B

-50C

-50D

-50E

-50F

60

AFG0307005 AFG0318671 AFG0334766 AFG0364862 AFG0452944 AFG0530052 AFG0533404 AFG0533462 AFG0570070 AFG0307010 AFG0318687 AFG0334773 AFG0364870 AFG0455063 AFG0530068 AFG0533410 AFG0533470 AFG0570085 AFG0308163 AFG012849 AFG000470 442536 501913 448540 501932 179064 501911 283227 503749-4

LAP BELT, BAGU FAG-9D-26, BROWN, BUCKLE ON RH BELT LAP BELT, BAGU FAG-9D-26, SILVERGREY, BUCKLE ON RH BELT LAP BELT, BAGU FAG-9D-26, BLACK, BUCKLE ON RH BELT LAP BELT, BAGU FAG-9D-26, TAN, BUCKLE ON RH BELT LAP BELT, BAGU FAG-9D-26, NAVYBLUE, BUCKLE ON RH BELT LAP BELT, BAGU FAG-9D-26, PEPPERDUST, BUCKLE ON RH BELT LAP BELT, BAGU FAG-9D-26, RASIN, BUCKLE ON RH BELT LAP BELT, BAGU FAG-9D-26, DARKGREY, BUCKLE ON RH BELT LAP BELT, BAGU FAG-9D-26, BURGUNDY, BUCKLE ON RH BELT .BELT, LAP, RH .BELT, LAP, RH .BELT, LAP, RH .BELT, LAP, RH .BELT, LAP, RH .BELT, LAP, RH .BELT, LAP, RH .BELT, LAP, RH .BELT, LAP, RH ..FITTING, MOUNTING ..BUCKLE, SLIDING ..LOOP, PLASTIC ..THREAD, NYLON, BROWN, E000207 ..THREAD, NYLON, SILVER, E000207 ..THREAD, NYLON, BLACK, E000207 ..THREAD, NYLON, LT.SANDSTONE E000207 ..THREAD, NYLON, LT. CASHMERE, E000207 ..THREAD, NYLON, RED TM6, E000207 ..THREAD, NYLON, CHARCOAL, E000207 ..WEBBING, BROWN, AFG-5030

A B C D E F G H J A B C D E F G H J A B,F C,E,G, H,J D,F F G,J H A

RF RF RF RF RF RF RF RF RF 1 1 1 1 1 1 1 1 1 1 1 1 AR AR AR AR AR AR AR AR


FAG-9

September 15, 2011


FIG. ITEM

PART NUMBER


EFF CODE

UNITS PER ASSY

4- 60 -60A -60B -60C

-60D -60E -60F -60G -60H

70 80 90

-90A -90B -90C -90D -90E -90F -90G -90H 100 110

-110A

-110B -110C

-110D

120

-120A -120B -120C -120D -120E -120F -120G -120H

130 140 150

503749-4 503749-1 503749-7 503749-2 503749-3 503749-10 503749-11 503749-6 503749-8 502102 AFG0341279 AFG0307028 AFG0318694 AFG0334789 AFG0364885 AFG0455070 AFG0530075 AFG0533427 AFG0533485 AFG0570092 502102 442536 501913 448540 501932 179064 503749-4 503749-1 503749-7 503749-2 503749-3 503749-10 503749-11 503749-6 503749-8 AFG000470 AFG012849 AFG030816

..WEBBING, BROWN, AFG-5030

..WEBBING, SILVERGREY, AFG-5030

..WEBBING, BLACK, AFG-5030

..WEBBING, TAN, AFG-5030

..WEBBING, NAVYBLUE, AFG-5030

..WEBBING, PEPPERDUST, AFG-5030

..WEBBING, RASIN, AFG-5030

..WEBBING, DARKGREY, AFG-5030

..WEBBING, BURGUNDY, AFG-5030

..LUG (V.45402, P/N 1101212)

..BUCKLE, ROTARY

.BELT, LAP, LH

.BELT, LAP, LH

.BELT, LAP, LH

.BELT, LAP, LH

.BELT, LAP, LH

.BELT, LAP, LH

.BELT, LAP, LH

.BELT, LAP, LH

.BELT, LAP, LH

..LUG (V.45402, P/N 1101212)

..THREAD, NYLON, BROWN, E000207

..THREAD, NYLON, SILVER, E000207 ..THREAD, NYLON, BLACK, E000207 ..THREAD, NYLON, LT.SANDSTONE E000207 ..THREAD, NYLON, LT. CASHMERE, E000207 ..WEBBING, BROWN, AFG-5030 ..WEBBING, SILVERGREY, AFG-5030 ..WEBBING, BLACK, AFG-5030 ..WEBBING, TAN, AFG-5030 ..WEBBING, NAVYBLUE, AFG-5030 ..WEBBING, PEPPERDUST, AFG-5030 ..WEBBING, RASIN, AFG-5030 ..WEBBING, DARKGREY, AFG-5030 ..WEBBING, BURGUNDY, AFG-5030 ..LOOP, PLASTIC ..BUCKLE, SLIDING ..FITTING, MOUNTING

A B C D E F G H J A B C D E F G H J A B C,E,G H,J D,F G A B C D E F G H J

AR AR AR AR AR AR AR AR AR 1 1 1 1 1 1 1 1 1 1 1 1 AR AR AR AR AR AR AR AR AR AR AR AR AR AR 1 1 1


FAG-9

September 15, 2011



LEFT BLANK

Page 1015

FAG-9

September 15, 2011



Lap Belt, Bagu FAG-9D-26 (Buckle on LH Belt) Figure 5

Page 1016

FAG-9

September 15, 2011


FIG. ITEM

PART NUMBER


EFF CODE

UNITS PER ASSY

5- 1

-1A

-1B

-1C

-1D

-1E

-1F

-1G

-1H

10 -10A -10B -10C -10D -10E -10F -10G -10H

20 30 40 50

-50A

-50B

-50C

-50D

-50E

-50F

60

-60A -60B

AFG0307033 AFG0318700 AFG0334796 AFG0364892 AFG0452951 AFG0530080 AFG0533432 AFG0533492 AFG0570109 AFG0307040 AFG0318716 AFG0334804 AFG0364909 AFG0455086 AFG0530098 AFG0533440 AFG0533509 AFG0570114 AFG0308163 AFG012849 AFG000470 442536 501913 448540 501932 179064 501911 283227 503749-4 503749-1 503749-7

LAP BELT, BAGU FAG-9D-26, BROWN, BUCKLE ON LH BELT LAP BELT, BAGU FAG-9D-26, SILVERGREY, BUCKLE ON LH BELT LAP BELT, BAGU FAG-9D-26, BLACK, BUCKLE ON LH BELT LAP BELT, BAGU FAG-9D-26, TAN, BUCKLE ON LH BELT LAP BELT, BAGU FAG-9D-26, NAVYBLUE, BUCKLE ON LH BELT LAP BELT, BAGU FAG-9D-26, PEPPERDUST, BUCKLE ON LH BELT LAP BELT, BAGU FAG-9D-26, RASIN, BUCKLE ON LH BELT LAP BELT, BAGU FAG-9D-26, DARKGREY, BUCKLE ON LH BELT LAP BELT, BAGU FAG-9D-26, BURGUNDY, BUCKLE ON LH BELT .BELT, LAP, RH .BELT, LAP, RH .BELT, LAP, RH .BELT, LAP, RH .BELT, LAP, RH .BELT, LAP, RH .BELT, LAP, RH .BELT, LAP, RH .BELT, LAP, RH ..FITTING, MOUNTING ..BUCKLE, SLIDING ..LOOP, PLASTIC ..THREAD, NYLON, BROWN, E000207 ..THREAD, NYLON, SILVER, E000207 ..THREAD, NYLON, BLACK, E000207 ..THREAD, NYLON, LT.SANDSTONE E000207 ..THREAD, NYLON, LT. CASHMERE, E000207 ..THREAD, NYLON, RED TM6, E000207 ..THREAD, NYLON, CHARCOAL, E000207 ..WEBBING, BROWN, AFG-5030 ..WEBBING, SILVERGREY, AFG-5030 ..WEBBING, BLACK, AFG-5030

A B C D E F G H J A B C D E F G H J A B C,E,G, H,J D,F E G,J H A B C

RF RF RF RF RF RF RF RF RF 1 1 1 1 1 1 1 1 1 1 1 1 AR AR AR AR AR AR AR AR AR AR


FAG-9

September 15, 2011


FIG. ITEM

PART NUMBER


EFF CODE

UNITS PER ASSY

5- -60C -60D -60E -60F -60G -60H

70 80

-80A -80B -80C -80D -80E -80F -80G -80H

90 100 110

-110A

-110B -110C

-110D

-110E

-110D

120

-120A -120B -120C -120D -120E -120F -120G -120H

130 140 150

503749-2 503749-3 503749-10 503749-11 503749-6 503749-8 502102 AFG0307058 AFG0318723 AFG0334810 AFG0364914 AFG0455093 AFG0530104 AFG0533457 AFG0533514 AFG0570121 AFG0341284 502102 442536 501913 448540 501932 179064 501911 283227 503749-4 503749-1 503749-7 503749-2 503749-3 503749-10 503749-11 503749-6 503749-8 AFG000470 AFG012849 AFG0308163

..WEBBING, TAN, AFG-5030

..WEBBING, NAVYBLUE, AFG-5030

..WEBBING, PEPPERDUST, AFG-5030

..WEBBING, RASIN, AFG-5030

..WEBBING, DARKGREY, AFG-5030

..WEBBING, BURGUNDY, AFG-5030

..LUG (V.45402, P/N 1101212)

.BELT, LAP, LH

.BELT, LAP, LH

.BELT, LAP, LH

.BELT, LAP, LH

.BELT, LAP, LH

.BELT, LAP, LH

.BELT, LAP, LH

.BELT, LAP, LH

.BELT, LAP, LH

..BUCKLE, ROTARY

..LUG (V.45402, P/N 1101212)

..THREAD, NYLON, BROWN E000207 ..THREAD, NYLON, SILVER, E000207 ..THREAD, NYLON, BLACK, E000207 ..THREAD, NYLON, LT.SANDSTONE, E000207 ..THREAD, NYLON, LT. CASHMERE, E000207 ..THREAD, NYLON, RED TM6, E000207 ..THREAD, NYLON, CHARCOAL, E000207 ..WEBBING, BROWN, AFG-5030 ..WEBBING, SILVERGREY, AFG-5030 ..WEBBING, BLACK, AFG-5030 ..WEBBING, TAN, AFG-5030 ..WEBBING, NAVYBLUE, AFG-5030 ..WEBBING, PEPPERDUST, AFG-5030 ..WEBBING, RASIN, AFG-5030 ..WEBBING, DARKGREY, AFG-5030 ..WEBBING, BURGUNDY, AFG-5030 ..LOOP, PLASTIC ..BUCKLE, SLIDING ..FITTING, MOUNTING

D E F G H J A B C D E F G H J A B C,E,G H,J D,F E G,J H A B C D E F G H J

AR AR AR AR AR AR 1 1 1 1 1 1 1 1 1 1 1 1 AR AR AR AR AR AR AR AR AR AR AR AR AR AR AR AR 1 1 1


FAG-9

September 15, 2011



LEFT BLANK

Page 1019

FAG-9

September 15, 2011


NOTE: Refer to figure 1 for proper lap belt.

Shoulder Strap, Schugu FAG-9A Figure 6

Page 1020

FAG-9

September 15, 2011


FIG. ITEM

PART NUMBER


EFF CODE

UNITS PER ASSY

6- 1

-1A

10 -10A

20 -30 -40 50

-50A 60

-60A 70

-80 -90 100

-100A

AFG011556 AFG012072 AFG011535 AFG012073 AFG012535 AFG012444 AFG012509 AFG012518 AFG012516 AFG011550 AFG012074 AFG012535 AFG012444 AFG012509 AFG012519 AFG012517

SHOULDER STRAP, SCHUGU FAG-9A, SILVERGREY SHOULDER STRAP, SCHUGU FAG-9A, SILVERGREY .STRAP, SHOULDER, RH .STRAP, SHOULDER, RH ..REEL, INERTIA, AUTOMATIC, AGB-8C ..PIN ..STICKER, (FOR INERTIA REEL COVER) ..STRAP, SHOULDER, RH ..STRAP, SHOULDER, RH ..STRAP, SHOULDER, LH ..STRAP, SHOULDER, LH ..REEL, INERTIA, AUTOMATIC, AGB-8C ..PIN ..STICKER, (FOR INERTIA REEL COVER) ..STRAP, SHOULDER, LH ..STRAP, SHOULDER, LH

A B A B A B A B A B

RF RF 1 1 1 1 1 1 1 1 1 1 1 1 1 1


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