@airbus: Component Maintenance Manual With Illustrated Part List

@AIRBUS
AIRBUS S.A.S.
Customer Services
Technical Data Support and Services
31707 Blagnac Cedex
FRANCE
FAPE3
COMPONENT MAINTENANCE MANUAL

WITH
ILLUSTRATED PART LIST
FWD CARGO COMPARTMENT DOOR
PN : D5237300000000
D5237300000200
D5237300000400
D5237300000800
Issue: Nov 01/02 52-31-17 Rev: Jul 01/11

@AIRBUS
D5237300000000
HIGHLIGHTS
Revision No. 9 - Jul 01/11
LOCATIONS CHG DESCRIPTIONS OF CHANGE

CODE
HIGHLIGHTS
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LIST OF EFFECTIVE CONTENT
Revision No. 9 - Jul 01/11
CONTENT CHG LAST REVISION

CODE DATE
INTRODUCTION
TASK 52-31-17-871-801-A01 Nov 01/08
DESCRIPTION AND OPERATION

TASK 52-31-17-870-802-A01 Nov 01/08
TASK 52-31-17-870-803-A01 Nov 01/08
FIGURE 52-31-17-991-001-A01 Nov 01/08
FIGURE 52-31-17-991-002-A01 Nov 01/08
FIGURE 52-31-17-991-003-A01 Nov 01/08
TASK 52-31-17-870-804-A01 Nov 01/08
FIGURE 52-31-17-991-004-A01 Nov 01/08
FIGURE 52-31-17-991-005-A01 Nov 01/08
TESTING AND FAULT ISOLATION

TASK 52-31-17-700-801-A01 Jul 01/09
Subtask 52-31-17-700-001-A01 Nov 01/08
FIGURE 52-31-17-991-006-A01 Nov 01/08
TASK 52-31-17-700-802-A01 Nov 01/08
Subtask 52-31-17-700-002-A01 Nov 01/08
TASK 52-31-17-700-803-A01 Nov 01/08
Subtask 52-31-17-700-003-A01 Nov 01/08
FIGURE 52-31-17-991-007-A01 Nov 01/08
TASK 52-31-17-810-801-A01 Jul 01/11
Subtask 52-31-17-810-001-A01 Jul 01/11
SCHEMATIC AND WIRING DIAGRAMS

TASK 52-31-17-878-805-A01 Nov 01/08
FIGURE 52-31-17-991-008-A01 Nov 01/08
L.E.C.
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DISASSEMBLY
TASK 52-31-17-000-801-A01 Jul 01/11
Subtask 52-31-17-010-001-A01 Nov 01/08
TASK 52-31-17-000-802-A01 Jul 01/11
Subtask 52-31-17-000-012-A01 Nov 01/08
TASK 52-31-17-000-803-A01 Jul 01/11
Subtask 52-31-17-010-002-A01 Nov 01/08
TASK 52-31-17-000-804-A01 Jul 01/11
Subtask 52-31-17-010-003-A01 Nov 01/08
TASK 52-31-17-000-805-A01 Jul 01/11
Subtask 52-31-17-040-001-A01 Nov 01/08
TASK 52-31-17-000-806-A01 Jul 01/11
Subtask 52-31-17-000-002-A01 Nov 01/08
TASK 52-31-17-000-807-A01 Jul 01/11
Subtask 52-31-17-000-003-A01 Nov 01/08
TASK 52-31-17-000-808-A01 Jul 01/11
Subtask 52-31-17-010-004-A01 Nov 01/08
TASK 52-31-17-000-809-A01 Jul 01/11
Subtask 52-31-17-000-004-A01 Nov 01/08
TASK 52-31-17-000-810-A01 Jul 01/11
Subtask 52-31-17-010-011-A01 Nov 01/08
TASK 52-31-17-000-811-A01 Jul 01/11
Subtask 52-31-17-000-006-A01 Nov 01/08
TASK 52-31-17-000-812-A01 Jul 01/11
Subtask 52-31-17-040-007-A01 Nov 01/08
TASK 52-31-17-000-813-A01 Jul 01/11
Subtask 52-31-17-000-008-A01 Nov 01/08
TASK 52-31-17-000-814-A01 Jul 01/11
Subtask 52-31-17-000-009-A01 Nov 01/08
L.E.C.
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CODE DATE
TASK 52-31-17-000-815-A01 Jul 01/11
Subtask 52-31-17-010-005-A01 Nov 01/08
TASK 52-31-17-000-816-A01 Jul 01/11
Subtask 52-31-17-010-006-A01 Nov 01/08
TASK 52-31-17-000-817-A01 Jul 01/11
Subtask 52-31-17-010-007-A01 Nov 01/08
TASK 52-31-17-000-818-A01 Jul 01/11
Subtask 52-31-17-010-008-A01 Nov 01/08
CLEANING
TASK 52-31-17-100-801-A01 Jul 01/11
Subtask 52-31-17-100-001-A01 Jul 01/11
Subtask 52-31-17-100-002-A01 Jul 01/11
Subtask 52-31-17-100-003-A01 Jul 01/11
Subtask 52-31-17-100-004-A01 Jul 01/11
INSPECTION/CHECK
TASK 52-31-17-210-801-A01 Jul 01/11
Subtask 52-31-17-210-001-A01 Jul 01/11
FIGURE 52-31-17-991-009-A01 Nov 01/08
TASK 52-31-17-210-802-A01 Nov 01/08
Subtask 52-31-17-210-002-A01 Nov 01/08
TASK 52-31-17-210-803-A01 Nov 01/08
Subtask 52-31-17-210-003-A01 Nov 01/08
TASK 52-31-17-210-804-A01 Nov 01/08
Subtask 52-31-17-210-004-A01 Nov 01/08
TASK 52-31-17-210-805-A01 Nov 01/08
Subtask 52-31-17-210-005-A01 Nov 01/08
TASK 52-31-17-210-806-A01 Nov 01/08
Subtask 52-31-17-210-006-A01 Nov 01/08
L.E.C.
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CODE DATE
TASK 52-31-17-210-807-A01 Nov 01/08
Subtask 52-31-17-210-007-A01 Nov 01/08
TASK 52-31-17-210-808-A01 Nov 01/08
Subtask 52-31-17-210-008-A01 Nov 01/08
TASK 52-31-17-210-809-A01 Nov 01/08
Subtask 52-31-17-210-009-A01 Nov 01/08
TASK 52-31-17-210-810-A01 Nov 01/08
Subtask 52-31-17-210-010-A01 Nov 01/08
FIGURE 52-31-17-991-010-A01 Nov 01/08
REPAIR
TASK 52-31-17-300-801-A01 Jul 01/11
Subtask 52-31-17-300-001-A01 Nov 01/08
Subtask 52-31-17-300-002-A01 Jul 01/11
Subtask 52-31-17-300-003-A01 Jul 01/11
FIGURE 52-31-17-991-011-A01 Nov 01/08
FIGURE 52-31-17-991-012-A01 Nov 01/08
FIGURE 52-31-17-991-013-A01 Nov 01/08
TASK 52-31-17-300-802-A01 Jul 01/11
Subtask 52-31-17-300-004-A01 Jul 01/11
Subtask 52-31-17-300-005-A01 Jul 01/11
Subtask 52-31-17-300-006-A01 Jul 01/11
TASK 52-31-17-300-803-A01 Jul 01/11
Subtask 52-31-17-300-007-A01 Jul 01/11
Subtask 52-31-17-300-008-A01 Jul 01/11
Subtask 52-31-17-300-009-A01 Jul 01/11
Subtask 52-31-17-300-010-A01 Nov 01/08
Subtask 52-31-17-300-011-A01 Nov 01/08
Subtask 52-31-17-300-012-A01 Nov 01/08
L.E.C.
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CODE DATE
Subtask 52-31-17-300-013-A01 Nov 01/08
Subtask 52-31-17-300-014-A01 Nov 01/08
Subtask 52-31-17-300-015-A01 Jul 01/11
Subtask 52-31-17-300-016-A01 Jul 01/11
ASSEMBLY
TASK 52-31-17-400-801-A01 Jul 01/11
Subtask 52-31-17-410-001-A01 Jul 01/11
TASK 52-31-17-400-802-A01 Jul 01/11
Subtask 52-31-17-410-002-A01 Jul 01/11
TASK 52-31-17-400-803-A01 Jul 01/11
Subtask 52-31-17-410-003-A01 Jul 01/11
TASK 52-31-17-440-801-A01 Jul 01/11
Subtask 52-31-17-440-001-A01 Jul 01/11
TASK 52-31-17-400-804-A01 Jul 01/11
Subtask 52-31-17-410-004-A01 Jul 01/11
TASK 52-31-17-400-805-A01 Jul 01/11
Subtask 52-31-17-410-005-A01 Jul 01/11
TASK 52-31-17-400-806-A01 Jul 01/11
Subtask 52-31-17-440-002-A01 Jul 01/11
TASK 52-31-17-400-807-A01 Nov 01/08
Subtask 52-31-17-400-001-A01 Nov 01/08
TASK 52-31-17-400-808-A01 Jul 01/11
Subtask 52-31-17-400-002-A01 Jul 01/11
TASK 52-31-17-400-809-A01 Jan 01/09
Subtask 52-31-17-410-006-A01 Jan 01/09
TASK 52-31-17-400-810-A01 Nov 01/08
Subtask 52-31-17-400-003-A01 Nov 01/08
TASK 52-31-17-400-811-A01 Jul 01/11
L.E.C.
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CODE DATE
Subtask 52-31-17-400-004-A01 Jul 01/11
TASK 52-31-17-400-812-A01 Jul 01/11
Subtask 52-31-17-410-007-A01 Jul 01/11
TASK 52-31-17-400-813-A01 Jul 01/11
Subtask 52-31-17-400-005-A01 Jul 01/11
TASK 52-31-17-400-814-A01 Jul 01/11
Subtask 52-31-17-400-006-A01 Jul 01/11
TASK 52-31-17-400-815-A01 Jan 01/09
Subtask 52-31-17-410-008-A01 Jan 01/09
TASK 52-31-17-400-816-A01 Jul 01/11
Subtask 52-31-17-410-009-A01 Jul 01/11
TASK 52-31-17-400-817-A01 Jul 01/11
Subtask 52-31-17-410-010-A01 Jul 01/11
TASK 52-31-17-800-801-A01 Jan 01/09
Subtask 52-31-17-820-001-A01 Jan 01/09
FIGURE 52-31-17-991-014-A01 Jan 01/09
TASK 52-31-17-800-802-A01 Jan 01/09
Subtask 52-31-17-820-002-A01 Jan 01/09
FIGURE 52-31-17-991-015-A01 Jan 01/09
TASK 52-31-17-800-803-A01 Jan 01/09
Subtask 52-31-17-820-003-A01 Jan 01/09
FIGURE 52-31-17-991-016-A01 Jan 01/09
TASK 52-31-17-800-804-A01 Jan 01/09
Subtask 52-31-17-820-004-A01 Jan 01/09
FIGURE 52-31-17-991-017-A01 Jan 01/09
TASK 52-31-17-800-805-A01 Jan 01/09
Subtask 52-31-17-820-005-A01 Jan 01/09
FIGURE 52-31-17-991-018-A01 Jan 01/09
TASK 52-31-17-800-806-A01 Jan 01/09
L.E.C.
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CODE DATE
Subtask 52-31-17-820-006-A01 Jan 01/09
FIGURE 52-31-17-991-019-A01 Jan 01/09
TASK 52-31-17-800-807-A01 Jan 01/09
Subtask 52-31-17-820-007-A01 Jan 01/09
FIGURE 52-31-17-991-020-A01 Jan 01/09
FITS AND CLEARANCES

TASK 52-31-17-820-806-A01 Jul 01/11
FIGURE 52-31-17-991-021-A01 Nov 01/08
FIGURE 52-31-17-991-022-A01 Nov 01/08
FIGURE 52-31-17-991-023-A01 Nov 01/08
FIGURE 52-31-17-991-024-A01 Nov 01/08
SPECIAL TOOLS,FIXTURES,EQUIPMENT AND CONSUMABLES

TASK 52-31-17-940-807-A01 Nov 01/08
FIGURE 52-31-17-991-025-A01 Nov 01/08
STORAGE INCLUDING TRANSPORTATION

TASK 52-31-17-550-801-A01 Nov 01/08
Subtask 52-31-17-620-001-A01 Nov 01/08
Subtask 52-31-17-530-002-A01 Nov 01/08
Subtask 52-31-17-550-003-A01 Nov 01/08
Subtask 52-31-17-550-004-A01 Nov 01/08
Subtask 52-31-17-550-005-A01 Nov 01/08
ILLUSTRATED PARTS LIST

IPL Introduction
TASK 52-31-17-872-801-A01 Jul 01/11
VENDOR LIST Jul 01/10
Figure 01
FIGURE 52-31-17-991-801-001 Nov 01/08
Parts List Nov 01/08
L.E.C.
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CODE DATE
Figure 02
FIGURE 52-31-17-991-802-001 Nov 01/08
Figure 03
FIGURE 52-31-17-991-803-001 Nov 01/08
Figure 04
FIGURE 52-31-17-991-804-001 Nov 01/08
Figure 05
FIGURE 52-31-17-991-805-001 Nov 01/08
Figure 08
FIGURE 52-31-17-991-808-001 Nov 01/08
Figure 09
FIGURE 52-31-17-991-809-001 Nov 01/08
Figure 13
FIGURE 52-31-17-991-813-001 Nov 01/08
Figure 20
FIGURE 52-31-17-991-820-001 Nov 01/08
Figure 21
FIGURE 52-31-17-991-821-001 Nov 01/08
Figure 25
FIGURE 52-31-17-991-825-001 Nov 01/08
L.E.C.
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CODE DATE
Figure 30
FIGURE 52-31-17-991-830-001 Nov 01/08
Figure 31
FIGURE 52-31-17-991-831-001 Nov 01/08
Figure 32
FIGURE 52-31-17-991-832-001 Nov 01/08
Figure 33
FIGURE 52-31-17-991-833-001 Nov 01/08
Figure 34
FIGURE 52-31-17-991-834-001 Nov 01/08
Figure 40
FIGURE 52-31-17-991-840-001 Nov 01/08
Figure 44
FIGURE 52-31-17-991-844-001 Nov 01/08
Figure 50
FIGURE 52-31-17-991-850-001 Nov 01/08
Figure 60
FIGURE 52-31-17-991-860-001 Nov 01/08
Figure 62
L.E.C.
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CODE DATE
FIGURE 52-31-17-991-862-001 Nov 01/08
Figure 63
FIGURE 52-31-17-991-863-001 Nov 01/08
Figure 90
FIGURE 52-31-17-991-890-001 Nov 01/08
Figure 91
FIGURE 52-31-17-991-891-001 Nov 01/08
Figure 95
FIGURE 52-31-17-991-895-001 Nov 01/08
Figure 96
FIGURE 52-31-17-991-896-001 Nov 01/08
Figure 97
FIGURE 52-31-17-991-897-001 Nov 01/08
L.E.C.
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TABLE OF CONTENTS
INTRODUCTION
52-31-17-871-801-A01 Introduction

52-31-17-870-802-A01 General
52-31-17-870-803-A01 Description
52-31-17-870-804-A01 Operation

52-31-17-700-801-A01 Test of the Proximity Switches
52-31-17-700-802-A01 Test of the Electrical Circuit
52-31-17-700-803-A01 Test of The Electrical Resistance
52-31-17-810-801-A01 Fault Isolation

52-31-17-878-805-A01 Schematics and Wiring Diagram
DISASSEMBLY
52-31-17-000-801-A01 Removal of the Insulation and the Door Seal
52-31-17-000-802-A01 Removal and Disassembly of the Access Cover Assemblies
52-31-17-000-803-A01 Removal of the Plugs, the Adjusting Screws and the Protective
Plugs
52-31-17-000-804-A01 Removal of the Hand Lever Mechanism
52-31-17-000-805-A01 Disassembly of the Hand Lever Assembly
52-31-17-000-806-A01 Removal and Disassembly of the Drift Pin Rods
52-31-17-000-807-A01 Removal and Disassembly of the Sequence Shaft
52-31-17-000-808-A01 Removal of the Vent Door Mechanism
52-31-17-000-809-A01 Removal and Disassembly of the Vent Door Assembly
52-31-17-000-810-A01 Removal and Disassembly of the Gearbox Assembly
52-31-17-000-811-A01 Removal of the Latching Mechanism Assemblies
52-31-17-000-812-A01 Disassembly of the Latching Hook Assemblies
52-31-17-000-813-A01 Removal and Disassembly of the Latching Shaft Assembly
52-31-17-000-814-A01 Removal and Disassembly of the Interlock Mechanism
52-31-17-000-815-A01 Removal of the Locking Shaft Assembly
52-31-17-000-816-A01 Removal of the Cargo Door Drainage
52-31-17-000-817-A01 Removal of the Door Proximity Sensors
52-31-17-000-818-A01 Removal of the Hinge Assemblies
T.O.C.
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CLEANING
52-31-17-100-801-A01 Cleaning
INSPECTION/CHECK
52-31-17-210-801-A01 Door Structure
52-31-17-210-802-A01 Structure Components
52-31-17-210-803-A01 Door Seal
52-31-17-210-804-A01 Door Mechanism
52-31-17-210-805-A01 Locking Mechanism
52-31-17-210-806-A01 Protective Treatment
52-31-17-210-807-A01 Electrical Equipment
52-31-17-210-808-A01 Springs
52-31-17-210-809-A01 Placard
52-31-17-210-810-A01 Visual Examination
REPAIR
52-31-17-300-801-A01 Reworking or Machining
52-31-17-300-802-A01 Protective Treatment
52-31-17-300-803-A01 Replacement of Parts
ASSEMBLY
52-31-17-400-801-A01 Installation of the Insulation and the Door Seal
52-31-17-400-802-A01 Assembly and Installation of the Access Cover Assemblies
52-31-17-400-803-A01 Installation of the Plugs and the Protective Plugs
52-31-17-440-801-A01 Assembly of the Hand Lever Assembly
52-31-17-400-804-A01 Installation of the Hand Lever Mechanism
52-31-17-400-805-A01 Installation of the Latching Mechanism Assemblies
52-31-17-400-806-A01 Assembly of the Latching Hook Assemblies
52-31-17-400-807-A01 Assembly and Installation of the Latching Shaft Assembly
52-31-17-400-808-A01 Assembly and Installation of the Interlock Mechanism
52-31-17-400-809-A01 Installation of the Locking Shaft Assembly
52-31-17-400-810-A01 Assembly and Installation of the Sequence Shaft
52-31-17-400-811-A01 Assembly and Installation of the Drift Pin Rods
52-31-17-400-812-A01 Installation of the Vent Door Mechanism
52-31-17-400-813-A01 Assembly and Installation of the Vent Door Assembly
52-31-17-400-814-A01 Assembly and Installation of the Gearbox Assembly
52-31-17-400-815-A01 Installation of the Door Proximity Sensors
52-31-17-400-816-A01 Installation of the Cargo Door Drainage
T.O.C.
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52-31-17-400-817-A01 Installation of the Hinge Assemblies

52-31-17-800-801-A01 Adjustment of the Hand Lever Assembly
52-31-17-800-802-A01 Adjustment of the Latching Mechanism
52-31-17-800-803-A01 Adjustment of the Locking Mechanism
52-31-17-800-804-A01 Adjustment of the Drift Pin Mechanism
52-31-17-800-805-A01 Adjustment of the Interlock Mechanism
52-31-17-800-806-A01 Adjustment of the Skin Offset of the Vent Door assembly
52-31-17-800-807-A01 Adjustment of the Proximity Switches
FITS AND CLEARANCES

52-31-17-820-806-A01 Fits and Clearances

52-31-17-940-807-A01 Special Tool

52-31-17-550-801-A01 Storage after Assembly

52-31-17-872-801-A01 Introduction Illustrated Parts List (IPL)
VENDOR LIST
DETAILED PARTS LIST
T.O.C.
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LIST OF SERVICE BULLETINS
SB No REV No MOD No INCORP. TITLE

DATE
*** NO SB ***
SBL
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INTRODUCTION
**For PN’s ALL
TASK 52-31-17-871-801-A01
Introduction
1. General
A. This manual is written to the iSpec 2200 and in ASD Simplified Technical English (STE). The
international SI units of measurement are used in this manual, with imperial units shown in
parentheses.
B. The manual contains data about maintenance on the component in a workshop. It does not
contain data about maintenance on the component when it is installed in the aircraft.
C. Only approved persons with the necessary skills are permitted to do the maintenance procedures
in this manual.
D. Maintenance Task Oriented Support System (MTOSS) task and subtask identification is used in
this manual. The maintenance tasks and other data have special MTOSS numbers for Electronic
Data Processing (EDP). The user of the manual can ignore the MTOSS numbers.
E. This manual contains:
- Technical data for the component
- Maintenance and repair procedures about the component
- An Illustrated Parts List (IPL) with data for the component parts. Parts are identified in all
sections of the manual by the IPL-Figure and item number.
F. We verified the DISASSEMBLY, TESTING and ASSEMBLY procedures by simulation.
2. How to use the Manual
A. Make sure that the manual contains the information applicable to your component.
B. If you need to identify a part or find a part number, use the search function.
C. You must use the instructions in this manual for all the component maintenance. Read all the
applicable WARNINGS and CAUTIONS before you do the work on the component.
3. List of Abbreviations
ACM Abbreviated Component Maintenance Manual
AEB Airline Engineering Bulletin
ASD Aero Space and Defence Industries Association of Europe
AF Across Flats
ATA Air Transport Association of America
ATLAS Abbreviated Test Language for All Systems
CMM Component Maintenance Manual
CMS Component Maintenance Sheet
INTRO
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FIN Functional Item Number

IPC Illustrated Parts Catalog
IPL Illustrated Parts List
ID Inside Diameter
MFG Manufacturing
MFR Manufacturer
MOD Modification
MTOSS Maintenance Task Oriented Support System
NTF Non Textile Floor
OD Outside Diameter
PA Poly-Amide
PARA Paragraph
PC Poly-Carbonate
PMS Process and Materials Specification
PN Part Number
PU Poly-Urethane
PV Poly-Venyl-Fluorite
SB Service Bulletin
SERNO Serial Number
STE Simplified Technical English
TBD To Be Determined
List of Abbreviations
TABLE 1
INTRO
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**For PN’s ALL
TASK 52-31-17-870-802-A01
General
1. The FWD Cargo Compartment Door (referred to as cargo door) is installed on the lower right hand
side of the aircraft. Hinge assemblies at the top end attach the cargo door to the fuselage. The
locking and the unlocking operation of the cargo door is carried out mechanically with a hand lever.
2. For the data of the proximity switches refer to CMMV 32-10-03 of the supplier ELDEC.
3. Technical Data (approx.):
Width: 355 mm (14.0 in.)
Height: 2035 mm (52.2 in.)
Length: 1321 mm (80.1 in.)
Weight: 86 kg (189.6 lb.)
Technical Data
TABLE 1
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**For PN’s ALL
TASK 52-31-17-870-803-A01
Description
1. Door Structure (Refer to FIGURE 52-31-17-991-001-A and FIGURE 52-31-17-991-002-A)
A. The cargo door structure has:
- the frames and beams,
- the vertical and horizontal edge members,
- the inner and outer skin,
- the door seal,
- the fire protection lining.
B. The cargo door structure is made of aluminium sheet metal and machined parts. Rivets attach
the parts together to form a torsion resistant structure. Sealant on the mating surfaces of the
parts prevents corrosion and makes them pressure tight.
C. The attachment fittings for the hydraulic actuators on the inner side of the cargo door are part
of the upper ends of the FR25A and FR26A.
D. The outer skin has a cut-out for the vent door. The inner side of the vent door has a cover.
E. An access panel for the door mechanism is installed on the lower side of the cargo door
structure. Indication windows allow the visual checking of the locked/unlocked (green/red)
position of the safety cams of the locking shaft.
F. At the upper edge member and beam No. 1, replaceable hinge assemblies with bronze bushings,
are installed to fit the cargo door to the fuselage.
G. Three blanking plugs, made from plastic, are installed in the hoist fittings on the outer side of
the cargo door.
H. Four adjustable screws are installed on the lower part of the cargo door. The adjustable screws
stop the movement of the cargo door when it is in the closed position and in line with the
aircraft fuselage.
J. The door seal is made of fabric reinforced silicon rubber. Retainers attach the door seal to the
edge members of the cargo door.
K. A drainage hose and a drainage valve are installed in the cargo door structure to drain the
condensed water.
L. The fire protection lining assembly with integral insulation is made of prepreg. The insulation is
made of PE-foam material lined with self-adhesive. The fire protection lining assembly is
attached to the inner skin of the cargo door with quick release fasteners.
2. Door Mechanism (Refer to FIGURE 52-31-17-991-001-A and FIGURE 52-31-17-991-002-A)
A. The door mechanism is installed in the lower part of the cargo door and has:
- the handle mechanism.
- the latching mechanism.
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- the interlock mechanism.

- the locking mechanism.
- the vent door mechanism.
- the target mechanism.
- the drift pin mechanism.
(1) Handle Mechanism
(a) The handle mechanism is installed in the lower part of the cargo door and has a flap
assembly, a door handle assembly and a lever mechanism.
(b) The handle mechanism operates
- the locking mechanism with the vent door.
- the latching mechanism.
- the drift pin mechanism.
- the actuator system interlock and
- the door warning system.
(c) In the closed and locked position the hand lever is kept in a recess and is then in line
with the outer contour of the cargo door. A catch holds it in position. A spring-
loaded flap operates the catch.
(2) Latching Mechanism
(a) The latching mechanism is installed in the lower part of the cargo door. The latching
shaft operates all the latching hooks through shaft levers, spring units, bellcranks and
links.
(b) In the latching position, four over-center linking locks hold the latching hooks. There
is a stop to guarantee dead center at each latching hook between the latching hook
and the bell crank.
(c) Safety cams, installed at the locking shaft, lock the latching hooks.
(3) Interlock Mechanism
(a) The interlock mechanism is installed in the center of the lower part of the door. It
has a spring loaded strut, a connection rod, an interlock lever, a stop bolt and a roller
lever.
(b) The interlock mechanism locks and unlocks the latching shaft.
(4) Locking Mechanism
(a) The locking mechanism is installed parallel to the latching mechanism in the lower
part of the cargo door. The locking mechanism is operated with the hand lever by a
rod connection at one end of the locking shaft.
(b) Locking cams, painted with red and green markings, are installed on the locking shaft
to keep the latching hooks in the LOCKED position.
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(5) Vent Door Mechanism

(a) At one end of the locking shaft, there is a rod assembly fitted to the vent door lever
of the locking shaft which operates a gear box assembly.
(b) The output shaft of the gear box assembly moves the spring loaded vent door with a
connection rod assembly.
(6) Target Mechanism
(a) The target mechanism of the door warning system is installed at the sequence shaft
which is part of the vent door mechanism.
(7) Drift Pin Mechanism
(a) The drift pin mechanism, installed in the middle of the cargo door, makes sure that
no contour offset exists between the aircraft fuselage and the cargo door when the
cargo door is installed at the aircraft, closed and locked.
(b) The drift pin mechanism includes the control rods with the related bellcranks, the
drift pin lever on the locking shaft and the drift pins.
(c) Control rods transmit the movement of the locking shaft to retract or extend the drift
pins.
3. Door Warning and Control System (Refer to FIGURE 52-31-17-991-003-A and TASK
52-31-17-878-805-A01)
A. A cable harness for the transmission of the data of the door mode is installed in the door
structure.
B. Two proximity switches are installed in the cargo door.
(1) The proximity switch 28WV is installed adjacent to the door handle (Door Warning
System).
(2) The proximity switch 5MJ is installed to the frame near the target lever on the latching
shaft (Door Control System).
NOTE : For data of the proximity switches refer to CMMV 32-10-03.

C. The target mechanism with the target lever for the proximity switch 30WV, which is a part of
the aircraft fuselage, is installed on the frame. A rod assembly connects the target lever to the
locking shaft.
D. A direct visual locking indicator system is installed in the cargo door as shown in FIGURE
52-31-17-991-002-A. It has the four integrated windows and related green/red markings on the
locking cams of the locking shaft.
E. In addition the open vent door is an indication for an UNLOCKED position of the locking shaft.
4. Electrical Equipment Installation
A. Refer to FIGURE 52-31-17-991-003-A and TASK 52-31-17-878-805-A01.
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B. A cable harness for transmission of data of the door condition (LOCKED/UNLOCKED) to the
ECAM is installed in the door structure (Refer to FIGURE 52-31-17-991-003-A). For the wiring
diagram refer to TASK 52-31-17-878-805-A01.
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**For PN’s ALL
UPPER EDGE
MEMBER
HINGE
ASSEMBLIES A
ATTACHMENT
FITTINGS
FIRE PROTECTION
LINING ASSEMBLY
DRIFT PIN
MECHANISM
DRIFT PIN
COVER
B
VENT DOOR
B
DRAINAGE
VALVE B
B EGDE
MEMBER
B RETAINER
EXAMPLE SEQUENCE
A
SHAFT EXAMPLE
ADJUSTING
SCREW
INNER SKIN
DOOR
SEAL
SELF ADHESIVE
INSULATION MAT
FIRE PROTECTION
LINING ASSEMBLY QUICK RELEASE
FASTENER
F_CM_523117_1_0010101_01_00
FWD Cargo Compartment Door

FIGURE-52-31-17-991-001-A01
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**For PN’s ALL
A
A PLUG INSTALLATION
FOR HOISTING
BLANKING
PLUG
VENT
DOOR
GEARBOX
A TARGET
DOOR MECHANISM
HANDLE
LATCHING/LOCKING
MECHANISM
LATCHING
SHAFT
LOCKING
LATCHING
SHAFT
HOOK
INTERLOCK
B MECHANISM
FLAP
ACCESS
PANEL
INDICATION
WINDOW
F_CM_523117_1_0020101_01_00

FIGURE-52-31-17-991-002-A01
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**For PN’s ALL
CONNECTOR
1856VC
7526VT
7522VP
PROXIMITY
SWITCH
28WV
PROXIMITY
SWITCH
5MJ
F_CM_523117_1_0030101_01_00
Electrical Equipment Installation

FIGURE-52-31-17-991-003-A01
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**For PN’s ALL
TASK 52-31-17-870-804-A01
Operation
1. Refer to FIGURE 52-31-17-991-004-A and FIGURE 52-31-17-991-005-A.
2. When you push the flap of the handle mechanism into the cargo door, the flap mechanism unlocks
the door handle.
3. When you pull out the door handle (65˚), the locking shaft with the cams turns (red markings are
visible through the indication windows) in the direction UNLOCKED. The blockage of all the latching
hooks is released. At one end of the locking mechanism a cam on the sequence shaft moves in the
direction UNLOCKED. The blockage of the latching shaft releases, the vent door opens and the drift
pins retract.
4. When you pull up the door handle from LATCHED to the UNLATCHED position (126˚ = fully
open):
- the latching shaft turns.
- the over-center linking locks break.
- the four latching hooks moves through shaft levers, spring units, bellcranks and links to the
unlatched position.
5. When you press and move the lever of the interlock mechanism, the blockage of the latching shaft
releases.
6. When you move the door handle down from the fully open position (UNLATCHED) to the
LATCHED position (65˚)
- the latching shaft turns to the latched position.
- the shaft levers, spring units, bellcranks and links move the hook operating linkage to the over-
center position.
- all the latching hooks are engaged.
7. When you push the door handle of the handle mechanism 65˚ down (until the door handle is smooth
with outer contour of the cargo door), the locking shaft and the cams turn in the direction LOCKED
(the green markings are visible through the indication windows).
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**For PN’s ALL
UPPER EDGE
MEMBER
HINGE
ASSEMBLIES A
ATTACHMENT
FITTINGS
FIRE PROTECTION
LINING ASSEMBLY
DRIFT PIN
MECHANISM
DRIFT PIN
COVER
B
VENT DOOR
B
DRAINAGE
VALVE B
B EGDE
MEMBER
B RETAINER
EXAMPLE SEQUENCE
A
SHAFT EXAMPLE
ADJUSTING
SCREW
INNER SKIN
DOOR
SEAL
SELF ADHESIVE
INSULATION MAT
FIRE PROTECTION
LINING ASSEMBLY QUICK RELEASE
FASTENER
F_CM_523117_1_0040101_01_00

FIGURE-52-31-17-991-004-A01
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**For PN’s ALL
A
A PLUG INSTALLATION
FOR HOISTING
BLANKING
PLUG
VENT
DOOR
GEARBOX
A TARGET
DOOR MECHANISM
HANDLE
LATCHING/LOCKING
MECHANISM
LATCHING
SHAFT
LOCKING
LATCHING
SHAFT
HOOK
INTERLOCK
B MECHANISM
FLAP
ACCESS
PANEL
INDICATION
WINDOW
F_CM_523117_1_0050101_01_00

FIGURE-52-31-17-991-005-A01
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**For PN’s ALL
TASK 52-31-17-700-801-A01
Test of the Proximity Switches
1. General
A. This TESTING is a functional test of the electrical system.
B. This FAULT ISOLATION is limited to the door mechanism.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
REFERENCE DESIGNATION
355M03213000 Cable Loom
355M03214000 Extension Cable Loom
Fixtures, Tools, Test and Support Equipment
TABLE 1
B.Referenced Information
TASK 52-31-17-878-805-A01 Schematics and Wiring Diagram
FIGURE 52-31-17-991-006-A FIGURE 52-31-17-991-006-A-Electrical Equipment Installation
Referenced Information
TABLE 2
3. Procedure
Subtask 52-31-17-700-001-A01
A. Test of the Proximity Switches
NOTE : Refer to FIGURE 52-31-17-991-006-A and TASK 52-31-17-878-805-A01.

(1) Make sure that the access panel assembly is removed (Refer to DISASSEMBLY).
(2) Prepare the doors checking tool for the test:
NOTE : Refer to the AEROSPATIALE Ground Equipment Manual (GEM) for details and
function of the Doors Checking Tool.
(a) On the PROXIMITY DETECTOR ADJUSTMENT section put the switch S6 in the
ON position. The three red LEDs (DS22, DS23, DS24) stay off.
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(b) Press the LIGHT TEST pushbutton S5. The three red LEDs (DS22, DS23, DS24)
come on.
(c) Release the LIGHT TEST pushbutton S5. The three red LEDs (DS22, DS23, DS24)
go off.
(d) Put the switch S6 in the OFF position.
(3) Prepare the test.
(a) Disconnect the plug connectors from the proximity switches 28WV and 5MJ.
(b) Install the connector P4 of 355M03213000 Cable Loom to the connector P9 of
355M03214000 Extension Cable Loom.
(c) Connect the connector P1 of 355M03213000 Cable Loom to the connector J1 of the
doors checking tool.
(d) Connect the connector P10 of 355M03214000 Extension Cable Loom to the proximity
switch 28WV or 5MJ for test.
(4) Do the test for the proximity switch 28WV as follows:
(a) Move the switch S6 in the ON position.
(b) If the red SENSOR LED NC (DS24) comes on and indicates an malfunction of the
proximity switch 28WV, replace it.
ACTION RESULT
(1) Put the handle in the LOCKED position. The red LED (DS22) comes on and indicates that
the TARGET is FAR.
(2) Push the flap assy in and pull the handle The red illuminated LED (DS23) goes off.
out of its recess. The LED (DS22) comes on and indicates that the
TARGET is FAR.
(3) Move the handle back in the LOCKED The red illuminated LED (DS22) goes off and the
position. red LED (DS23) comes on and indicates that the
TARGET is NEAR.
Action Result Table
TABLE 3
(c) Move the switch S6 in the OFF position.

(d) Disconnect the connector P10 from the proximity switch 28WV.
(e) Connect the plug connector to the proximity switch 28WV.
(5) Do the test for the proximity switch 5MJ as follows:
(a) Move the switch S6 in the ON position.
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(b) If the red SENSOR LED NC (DS24) comes on and indicates an malfunction of the
proximity switch 5MJ, replace it.
ACTION RESULT
(1) Put the handle in the LOCKED position. The red LED (DS22) comes on and indicates that
the TARGET is FAR.
(2) Push the flap assy in and pull the handle The red illuminated LED (DS22) for the TARGET
out of its recess. FAR stays on, until the handle is in fully open
position. Then the red illuminated LED (DS22)
goes off.
(3) Move the handle back in the LOCKED The red illuminated LED (DS23) goes off and the
position. red LED (DS22) comes on and indicates that the
TARGET is FAR.
Action Result Table
TABLE 4
(c) Move the switch S6 in the OFF position.

(d) Disconnect the connector P10 from the proximity switch 5MJ.
(e) Connect the plug connector to the proximity switch 5MJ.
(6) Disconnect the connector P1 from the connector J1 of the doors checking tool.
(7) Disconnect the connector P9 from the connector P4 of the cable looms.
(8) Install the access panel assembly (Refer to ASSEMBLY).
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**For PN’s ALL
CONNECTOR
1856VC
7526VT
7522VP
PROXIMITY
SWITCH
28WV
PROXIMITY
SWITCH
5MJ
F_CM_523117_1_0060101_01_00
Electrical Equipment Installation

FIGURE-52-31-17-991-006-A01
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**For PN’s ALL
TASK 52-31-17-700-802-A01
Test of the Electrical Circuit
1. General
continuity tester
TABLE 1
TASK 52-31-17-878-805-A01 Schematics and Wiring Diagram
TABLE 2
3. Procedure
Subtask 52-31-17-700-002-A01
A. Test of the Electrical Circuit
NOTE : Refer to TASK 52-31-17-878-805-A01.
NOTE : For this test you must use a continuity tester. If you find a failure, you must check all
connections for correct assembly.
(1) Test of the Electrical Circuit
ACTION RESULT
Remove the connectors from the proximity
switches 5MJ and 28WV
Make a connection between the contacts 1-
2 and 13-14 of the connector 1856VC-A.
Connect a continuity tester to the contacts Indication comes on the continuity tester.
A-B of the connectors for the proximity
switches 5MJ and 28WV.
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ACTION RESULT
Install the connectors to the proximity
switches 5MJ and 28WV.
Test of the Electrical Circuit
TABLE 3
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**For PN’s ALL
TASK 52-31-17-700-803-A01
Test of The Electrical Resistance
1. General
ohmmeter
TABLE 1
3. Procedure
Subtask 52-31-17-700-003-A01
A. Test of The Electrical Resistance
(1) Test of The Electrical Resistance
ACTION RESULT
(1) Connect the ohmmeterto the bonding lead The resistance must not be more than 0.1 mω.
and the structure near the attachment part.
(2) Connect the ohmmeternear the bonding lead The resistance must not be more than 10 mω.
attachment on the structure
Test of The Electrical Resistance
TABLE 2
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**For PN’s ALL
3 3
1 10.0m
2 0.1m
REMOVE THE SURFACE PROTECTION TO GET SUFFICIENT CONTACT.
3
REFER TO REPAIR FOR THE REPAIR OF THE PROTECTIVE TREATMENT.
F_CM_523117_1_0070101_01_00
Test of the Electrical Resistance

FIGURE-52-31-17-991-007-A01
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**For PN’s ALL
TASK 52-31-17-810-801-A01
Fault Isolation
1. General
A. This FAULT ISOLATION is limited to the door mechanism.
A. Consumable Materials
04-017 Silicone Grease
04-004 Synthetic Ester Based Grease High Pressure
Consumable Materials
TABLE 1
3. Procedure
Subtask 52-31-17-810-001-A01
A. Fault Isolation
WARNING : BE CAREFUL WHEN YOU USE MATERIAL NO. 04-017 SILICONE GREASE.
OBEY THE MATERIAL MANUFACTURER’S INSTRUCTIONS.
WARNING : BE CAREFUL WHEN YOU USE MATERIAL NO. 04-004 SYNTHETIC ESTER
BASED GREASE HIGH PRESSURE. OBEY THE MATERIAL
MANUFACTURER’S INSTRUCTIONS.
(1) Fault Isolation
FAULT POSSIBLE CAUSE CORRECTION
(1) You can not move the (a) Parts of the hand lever Examine the hand Lever
hand lever assy to the mechanism are damaged. mechanism and replace the
OPEN or CLOSED damaged parts.
position.
(b) Parts of the latching shaft are Examine the latching
damaged. mechanism and replace the
damaged parts.
(c) Parts of the locking shaft are Examine the locking mechanism
damaged. and replace the damaged parts.
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(2) You can move the hand (a) Damaged surfaces of the Replace the damaged parts.
lever assy to the OPEN sequence cams (9-20), the
and CLOSED position only universal joint lock (8-240) and
with high force. the universal joint assy (8-510).
(b) The sliding surfaces of the Apply Material No. 04-017
sequence cams (9-20), the Silicone Grease to the sliding
universal joint lock (8-240) and surfaces.
the universal joint assy (8-510)
are not lubricated.
(c) No grease between the sliding Apply Material No. 04-004
surfaces of the shaft (8-250) Synthetic Ester Based Grease
and the sequence cams (9-20). High Pressure to the lubrication
fitting (8-350) of the shaft
(8-250).
(d) The actuating unit (8-40) is Replace the damaged actuating
damaged and has a leakage. unit (8-40).
(e) The control rod is too long Adjust the control rod (8-160).
(8-160) or too short.
(f) The control rod (8-600) is too Adjust the control rod (8-600).
long or too short.
(3) The handle mechanism has (a) The thickness of the washers Remove the hand lever assy and
axial play and an axial (8-260, 270) must be increased. install new and washers (8-260,
gap. 270).
(4) You can not lock the hand (a) The bearing bolt (9-140) is Replace the damaged parts.
lever assy with the handle broken.
flap (9-100) in the
CLOSED position.
(5) The handle flap (9-100) is (a) The force of the spring (9-110)The spring (9-110) is weak or
not flush with the contour can not hold the handle flap broken. Replace the spring
of the hand lever assy. (9-100) in position. (9-110).
(6) The latching shaft does (a) Foreign objects between the - Remove the Latching shaft.
not move easily. sliding surfaces of the bearing- Examine the latching shaft
bushes and the latching shaft. and the bearing bushes,
replace the damaged parts.
(b) Not sufficient lubrication Apply Material No. 04-004
between the bearing bushes and Synthetic Ester Based Grease
the latching shaft. High Pressure to the sliding
surfaces of the bearing bushes
and the latching shaft.
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(7) (a)
(b)
(8) The drift pin mechanism (a) Not sufficient lubrication Apply Material No. 04-004
does not move easily. between the bearing bushes and Synthetic Ester Based Grease
sliding surfaces of the drift pins. High Pressure to the sliding
surfaces of the bearing bushes
and the drift pins.
(9) The interlock mechanism (a) The compression spring (44-40) Install a new compression spring
moves too easily. is broken or has Lost its spring (44-40).
force.
(10) Hard movement of the (a) Not sufficient Lubrication of the Apply Material No. 04-004
Latching mechanism. Latching mechanism. Synthetic Ester Based Grease
High Pressure to the
Lubrication fittings (34-30, 200)
of the latching mechanism.
Fault Isolation
TABLE 2
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**For PN’s ALL
TASK 52-31-17-878-805-A01
Schematics and Wiring Diagram
1. Schematics and Wiring Diagram
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**For PN’s ALL
FWD CARGO COMPARTMENT DOOR
2
R A
13 A R A
B A
5863−PF24 5864−PF24 B B
F B
B
14 G C
7526VT 7522VP 28WV−A
1856VC−A
1856VC−A
B 1
C
G B B
2 F B
1025−PF24 1023−PF24 R A
B A
1 A
R 5MJ−A
7526VT 7532VP
F_CM_523117_1_0080101_01_00
Wiring Diagram
FIGURE-52-31-17-991-008-A01
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DISASSEMBLY
**For PN’s ALL
TASK 52-31-17-000-801-A01
Removal of the Insulation and the Door Seal
1. General
CAUTION : IT IS NOT PERMITTED TO REPAIR OR REPLACE COMPONENTS THAT ARE

ASSEMBLED WITH TAPER PIN(S). IF YOU FIND A DEFECTIVE COMPONENT
THAT IS ASSEMBLED WITH TAPER PIN(S), YOU MUST REPLACE THE
ASSEMBLY.
-
NOTE : If necessary, refer to TASK 52-31-17-300-803-A01 for the replacement of the permanently
attached parts.
A. Refer to TESTING AND FAULT ISOLATION and CHECK for the necessary level of the
disassembly.
B. Put the cargo door in a well shaped support to prevent damage.
C. The Figure sequence of this section agrees with the related IPL. The Figures which are not used
are not included.
D. If a paragraph refers to one Figure, only the item number is given in brackets. If a paragraph
refers to more than one Figure, the Figure number and the item number are given in the
brackets.
NOTE : For the replacement of the identification plates refer to TASK 52-31-17-300-803-A01.
A.Referenced Information
TASK 52-31-17-300-803-A01 Replacement of Parts
TABLE 1
3. Procedure
Subtask 52-31-17-010-001-A01
A. Removal of the Insulation and the Door Seal
NOTE : Refer to IPL_FIGURE_02.
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(1) Remove the fire protection lining assembly (10).

(a) Disconnect the stud assemblies (80, 90) and remove the fire protection lining
assembly (10) from the door structure.
NOTE : Do not remove

- the insulation (20 thru 60) and the cling strips (70, 140) from the fire
protection lining assembly (10) unless a replacement is necessary,
- the bonded protective strip (130) from the fire protection lining
assembly (10) unless a replacement is necessary and
- the pressed-in bushes (160) from the cargo door structure unless a
replacement is necessary (Refer to TASK 52-31-17-300-803-A01).
NOTE : Do not disassemble the stud assemblies (80, 90).

(2) Remove the door seal (150).
NOTE : Do not remove the door seal (150) from the cargo door unless a replacement is
necessary.
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**For PN’s ALL
TASK 52-31-17-000-802-A01
Removal and Disassembly of the Access Cover Assemblies
1. General
-
attached parts.
disassembly.
are not included.
brackets.
TABLE 1
3. Procedure
Subtask 52-31-17-000-012-A01
A. Removal and Disassembly of the Access Cover Assemblies

(1) Remove the access cover assembly (10).
(a) Disconnect the studs (60, 90, 100) and remove the access cover assembly (10) from
the cargo door.
NOTE : Do not disassemble the stud assemblies (60, 90, 100) unless a replacement
is necessary.
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(2) Remove the access cover (110).
NOTE : Do not remove the access cover (110) unless a replacement of the drift pin parts
is necessary.
(a) Remove the screws (120) and remove the access cover (110).
(3) Remove the access cover assembly (130).
(a) Remove the screws (160) and the washers (170) and remove the access cover
assembly (140).
NOTE : Do not remove the self adhesive sealing section (150) from the access cover
(140) unless a replacement is necessary.
(4) Remove the sight glasses (30).
(a) Remove the nuts (50) and the screws (40) and remove the sheets (20) and the sight
glasses (30).
NOTE : Do not remove the sight glasses (30) unless a replacement is necessary.
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**For PN’s ALL
TASK 52-31-17-000-803-A01
Removal of the Plugs, the Adjusting Screws and the Protective Plugs
1. General
-
NOTE : If necessary, refer to REPAIR, TASK 52-31-17-300-803-A01, for the replacement of the
permanently attached parts.
disassembly.
are not included.
brackets.
NOTE : For the replacement of the identification plates refer to REPAIR, TASK
52-31-17-300-803-A01.
TABLE 1
3. Procedure
Subtask 52-31-17-010-002-A01
A. Removal of the Plugs, the Adjusting Screw and the Protective Plugs
NOTE : Refer to IPL_FIGURE_01 and IPL_FIGURE_04

(1) Remove the plugs (1-80).
NOTE : Do not remove the inserts (1-35) from the cargo door structure unless a repair or
a new installation is necessary (Refer to TASK 52-31-17-300-803-A01).
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(2) Remove the adjusting screws (1-90).
NOTE : Do not remove the adjusting screws (1-90) from the cargo door unless a repair or
a new installation is necessary.
NOTE : Do not remove the inserts (1-120) from the cargo door structure unless a repair
or a new installation is necessary (Refer to TASK 52-31-17-300-803-A01).
(3) Remove the protective plugs (4-20, 30) from the cargo door.
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**For PN’s ALL
TASK 52-31-17-000-804-A01
Removal of the Hand Lever Mechanism
1. General
-
NOTE : If necessary, refer to REPAIR, TASK 52-31-17-300-803-A01 for the replacement of the
disassembly.
are not included.
brackets.
52-31-17-300-803-A01.
TASK 52-31-17-300-802-A01 Protective Treatment
TASK 52-31-17-300-801-A01 Reworking or Machining
TABLE 1
3. Procedure
Subtask 52-31-17-010-003-A01
A. Removal of the Hand Lever Mechanism

(1) Move the hand lever assembly (10) to the UNLOCKED position.
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(2) Install a locally manufactured bush and a nut (e. g. NAS 509-4) at the spring bolt (460)
and turn the nut until the compression spring (470) is fully compressed.
NOTE : The locally manufactured bush must be made of aluminum or bronze and must
have the following dimensions:
- Length: 12.0 mm (0.4724 in.)
- Inner Diameter: 7.5 mm (0.2953 in.)
- Outer Diameter: 13.0 mm (0.5118 in.)
(3) Disconnect the control rods (160, 600).
(a) Remove and discard the cotter pin (170) from the nut (180).
(b) Remove the nut (180), the washer (190), the bolt (200) and the washer (210) and
disconnect the control rod (160) from the Lever (90).
(c) Remove and discard the cotter pin (540) from the nut (550).
(d) Remove the nut (550), the washer (560), the bolt (580) and the washer (570) and
disconnect the control rod (600) from the universal joint assembly (510).
(4) Remove the shaft (250) and the hand lever assembly (10).
(a) Remove the bolts (140) and the lock washer (150).
(b) Remove the shaft (250) and the spacer washers (260, 270) and remove the hand lever
assembly (10) from the cargo door.
(c) Identify the location and measure and record the thickness of the spacer washers
(260, 270).
NOTE : Do not remove the lubrication fitting (350) from the shaft (250) unless a
replacement is necessary (Refer to TASK 52-31-17-300-803-A01, TASK
52-31-17-300-802-A01, TASK 52-31-17-300-801-A01).
(5) Remove and disassemble the lever assembly (20).
(a) Remove the nuts (110), the bolts (130) and the washers (120) from the fitting (30)
and the door structure.
(b) Remove the nut (110), the washer (220) and the bolt (230) from the serrated lever
(90).
(c) Remove the serrated lever assembly (20) from the shaft (360).
(d) Remove and discard the cotter pins (60) from the location pins (50).
(e) Remove the washers (70), the location pins (50) and the washers (80) and disconnect
the actuating unit (40) from the serrated lever (90) and the fitting (30).
NOTE : Do not remove the bonded-in bearing (110) from the serrated lever (90)
unless a replacement is necessary (Refer to TASK 52-31-17-300-803-A01,
TASK 52-31-17-300-802-A01, TASK 52-31-17-300-801-A01).
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(6) Remove the compression spring (470).

(a) Remove the nut (110), the washer (120) and the bolt (450).
(b) Carefully remove the nut (e. g. NAS 509-4) from the spring bolt (460) and release the
tension of the compression spring (470).
(c) Remove the compression spring (470) from the spring bolt (460).
(7) Remove the shaft (360).
(a) Remove the nut (110), the washer (220) and the bolt (230) from the universal joint
lock (240).
(b) Carefully remove the shaft (360) from the door structure and remove the universal
joint lock (240), the roller lever assembly (370) and the universal joint assembly
(510).
NOTE : Do not remove the bonded-in bearing (590) and the pressed-in bushes (530)
from the universal joint latch (520) unless a replacement is necessary (Refer
to TASK 52-31-17-300-803-A01, TASK 52-31-17-300-802-A01, TASK
52-31-17-300-801-A01).
(c) Remove the nut (410), the washer (420) and the bolt (430) and remove the roller
(400) from the roller lever (380).
NOTE : Do not remove the pressed-in bushes (390) from the roller lever (380)
unless a replacement is necessary (Refer to TASK 52-31-17-300-803-A01,
TASK 52-31-17-300-802-A01, TASK 52-31-17-300-801-A01).
(8) Remove the control rods (160, 600).
(a) Record the position of the control rods (160, 600).
(b) Remove and discard the cotter pins (170) from the fork-end connection of the control
rods (160, 600).
(c) Remove the nuts (180), the washers (190), the bolts (200) and the washers (210)
from the fork-end connection of the control rods (160, 600).
(d) Disconnect the fork-end of the control rod (160) from the locking shaft.
(e) Disconnect the fork-end of the control rod (600) from the latching shaft.
(f) Measure and record the length of the control rods (160, 600) between the center of
the rod ends.
(g) Disassemble the control rods (160B, 600B) as follows (Refer to IPL_FIGURE_95):
1 Cut, remove and discard the lockwire from the nuts (30, 40) and the locking
devices (50).
2 Loosen the nuts (30, 40).
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3 Remove the rod ends (10A, 20A and 10B, 20B) with the nuts (30, 40) and the
locking devices (50) from the rod body.
4 Remove the nuts (30, 40) and the locking devices (50) from the rod ends (10A,
20A and 10B, 20B).
(9) Remove the catching hook (490).
(a) Remove the bolts (500) and the washers (120), and remove the catching hook (490)
and the shim (480).
(b) Measure and identify the thickness of the shim (480).
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**For PN’s ALL
TASK 52-31-17-000-805-A01
Disassembly of the Hand Lever Assembly
1. General
-
disassembly.
are not included.
brackets.
52-31-17-300-803-A01.
TABLE 1
3. Procedure
Subtask 52-31-17-040-001-A01
A. Disassembly of the Hand Lever Assembly

(1) Remove the retaining rings (50), the washers (60), the bolts (40) and the rollers (80) and
remove the stop (30).
NOTE : Do not remove the bonded-in bushes (70), the bonded-in insert (90) and the
insert (200), unless a replacement is necessary (Refer to REPAIR, TASK
52-31-17-300-801-A01).
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(2) Remove the bolts (190) and the washers (150) and remove the sequence cams (20).
(3) Remove and discard the cotter pins (120) from both ends of the bearing bolt (160).
(4) Remove the washers (130) and remove the bearing bolt (140).
WARNING : THE SPRING IS INSTALLED WITH LOAD.

(5) Remove the washers (150) and the bearing bolt (160), and collect the spring sleeve (170),
the spring (110) and the handle flap (100).
NOTE : Do not remove the bonded-in bushes (180) unless a replacement is necessary
(Refer to REPAIR, TASK 52-31-17-300-803-A01).
NOTE : Do not remove the bonded sliding layer (210) from the handle flap (100) unless a
replacement is necessary.
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**For PN’s ALL
TASK 52-31-17-000-806-A01
Removal and Disassembly of the Drift Pin Rods
1. General

ASSEMBLY.
-
attached parts.
disassembly.
are not included.
brackets.
TABLE 1
3. Procedure
Subtask 52-31-17-000-002-A01
A. Removal and Disassembly of the Drift Pin Rods

(1) Remove the rods (80).
(a) Remove and discard the cotter pins (70, 240).
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(b) Remove the nuts (50, 230), the washers (60, 210, 220) and the bolts (20, 200) and
remove the rods (80) and the washers (30).
NOTE : Do not disassemble the rods (80).

(2) Remove the drift pins (10) from the door structure.
(3) Remove the bellcrank assembly (90).
(a) Disconnect the the control rod from the lever (130).
1 Remove and discard the cotter pin (240).
2 Remove the nut (230), the bolt (200) and the washers (210, 220)
(b) Remove the nuts (190), the sleeves (180), the taper pins (170).
(c) Remove the Lever (130) from the beam 3-shaft (160).
NOTE : Do not remove the bonded-in bearing (150) from the Lever (140).
(d) Remove the beam 3-shaft (160) and the bellcrank (100) from the door structure.
NOTE : Do not remove the bonded-in bearings (120) from the bellcrank (110).
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**For PN’s ALL
TASK 52-31-17-000-807-A01
Removal and Disassembly of the Sequence Shaft
1. General

ASSEMBLY.
-
attached parts.
disassembly.
are not included.
brackets.
TABLE 1
3. Procedure
Subtask 52-31-17-000-003-A01
A. Removal and Disassembly of the Sequence Shaft

(1) Remove the control rods (10, 210).
(a) Remove and discard the cotter pins (60).
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(b) Remove the nuts (50), the bolts (20), the washers (30, 40) and remove the control
rods (10, 210).
NOTE : Do not disassemble the control rods (10, 210).

(2) Remove and disassemble the beam 4 cover assembly (70).
(a) Remove the bolts (190), the washers (200) and remove the beam 4 cover assembly
(70) from the door structure.
(b) Remove the nuts (180), the sleeves (170) and the taper pins (160).
(c) Remove the beam 4 shaft (150), the spacer sleeve (140) and the beam 4 levers (110)
from the beam 4 cover (80).
NOTE : Do not remove the bonded-in bearings (130) from the beam 4 levers (120)
and the pressed-in bushes (100) from the cover (90) unless a replacement is
necessary (Refer to TASK 52-31-17-300-803-A01).
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**For PN’s ALL
TASK 52-31-17-000-808-A01
Removal of the Vent Door Mechanism
1. General

ASSEMBLY.
-
attached parts.
disassembly.
are not included.
brackets.
TABLE 1
3. Procedure
Subtask 52-31-17-010-004-A01
A. Removal of the Vent Door Actuating Mechanism
NOTE : Refer to IPL_FIGURE_20 and IPL_FIGURE_25.
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(1) Remove the cover (20-10).

(a) Remove the nuts (20-20), the screws (20-40) and the washers (20-30) and remove the
cover (20-10) from the door structure.
(2) Remove the actuating rod (20-110).
(a) Remove the nut (25-160), the sleeve (25-150) and the taper pin (25-140).
(b) Remove and discard the cotter pins (20-80).
(c) Remove the nuts (20-90), the bolts (20-60, 120) and the washers (20-70, 130).
(d) Remove the actuating rod (20-110) with the Lever (25-120 and the plug (25-130)
from the vent door assembly (20-50) and the gear box assembly (20-220).
NOTE : Do not disassemble the actuating rod (20-110).

(3) Remove the connecting rod assembly (20-230).
(a) Remove and discard the cotter pins (20-80).
(b) Remove the nuts (20-90), the bolts (20-120) and the washers (20-70, 130) and
remove the connecting rod assembly (20-230).
NOTE : Do not remove the bonded-in bearings (20-250) from the connecting rod
(20-240) unless a replacement is necessary (Refer to TASK
52-31-17-300-803-A01).
(4) Remove the link assembly (20-260).
(a) Remove and discard the cotter pins (20-370, 450).
(b) Remove the nuts (20-360, 440), the bolts (20-330, 420), the washers (20-200, 350)
and the sleeve (20-430) and remove the link assembly (20-260) and the sleeves
(20-340, 430) from the gearbox assembly (20-220) and the lever assembly (20-380).
(c) Remove the lever assembly (20-380).
1 Remove and discard the cotter pin (20-80).
2 Remove the nut (20-90) and the washer (20-70) and remove the lever assembly
(20-380) from the fitting support (20-460).
NOTE : Do not remove the pressed-in bushes (20-410, 390) from the lever
(20-400) unless a replacement is necessary (Refer to TASK
52-31-17-300-803-A01).
NOTE : Do not remove the riveted fitting support (20-460) from the door
structure unless a replacement is necessary (Refer to TASK
52-31-17-300-803-A01).
(5) Disassemble the Link assembly (20-260).
(a) Release the tab washers (20-280) and loosen the nuts (20-290).
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(b) Remove the forks (20-270, 320), the tab washers (20-280) and the nuts (20-290)
from the rod (20-300).
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**For PN’s ALL
TASK 52-31-17-000-809-A01
Removal and Disassembly of the Vent Door Assembly
1. General

ASSEMBLY.
-
attached parts.
disassembly.
are not included.
brackets.
TABLE 1
3. Procedure
Subtask 52-31-17-000-004-A01
A. Removal and Disassembly of the Vent Door Assembly

(1) Remove the vent door assembly (100) as follows:
(a) Remove and discard the cotter pins (10).
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(b) Remove the nuts (20) and the washers (30).
WARNING : THE SPRINGS ARE INSTALLED WITH LOAD.

(c) Remove the sleeves (60).
(d) Remove the bolts (70), the washers (30) and the sleeve (90).
(e) Remove the washers (40) and identify the number of washers (40).
(f) Remove the springs (50, 80).
(g) Remove the vent door assembly (100) from the cargo door.
(2) Disassemble the vent door assembly (100).
NOTE : Do not remove unless a replacement is necessary (Refer to TASK

52-31-17-300-803-A01):
- the pressure-relief flap seal (170) from the vent door (200) unless a
replacement is necessary.
- the riveted retainers (180, 190) from the vent door (200).
- the nuts (130), the screws (110, 140) and the washers (120) from the vent
door (200).
- the riveted actuator arm assembly (220) and the arm assembly (350) from
the torsion box (330) and
- the pressed-in bushes (240, 250, 300, 310, 320, 370, 420) from the actuator
arms (230, 360) .
(a) Release the tab washers (270, 390).
(b) Loosen the nuts (280, 400) and remove the bolts (260, 380) with the tab washers
(270, 390) and the nuts (280, 400) from the actuator arm (230) and the arm (360).
(c) Remove the tab washers (270, 390) and the nuts (280, 400) from the bolts (260,
380).
NOTE : Do not remove the inserts (290, 410) from the actuator arm (230) and the
arm (360) unless a replacement is necessary (Refer to TASK
52-31-17-300-803-A01).
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**For PN’s ALL
TASK 52-31-17-000-810-A01
Removal and Disassembly of the Gearbox Assembly
1. General
-
attached parts.
disassembly.
are not included.
brackets.
TASK 52-31-17-000-808-A01 Removal of the Vent Door Mechanism
TABLE 1
3. Procedure
Subtask 52-31-17-010-011-A01
A. Removal and Disassembly of the Gearbox Assembly
NOTE : Make sure that the link assembly (20-260), the actuating rod (20-110) and the
connecting rod assembly (20-230) are disconnected from the gearbox assembly
(20-220) (Refer to TASK 52-31-17-000-808-A01).
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(1) Remove the gearbox assembly (20-220).

(a) Remove the nuts (25-160), the washers (25-270), the sleeves (25-280) and the taper
pins (25-290) from the lever (25-300) and the locking cam (25-310).
(b) Remove the lever (25-320) with the locking cam (25-310) and the lever (25-300) from
the axle assembly (25-210).
NOTE : Do not remove the pressed-in bush (25-330) from the lever (25-320) unless
a replacement is necessary (Refer to TASK 52-31-17-300-803-A01 ).
(c) Remove the lever (25-120) with the protective plug (25-130) from the shaft assembly
(25-70).
(d) Remove the protective plug (25-130) from the lever (25-120).
(e) Remove the nuts (20-180), the bolts (20-160) and the washers (20-170).
(f) Remove the bearing flange (20-140) from the door structure.
(g) Remove the bolts (20-190) and the washers (20-200) and remove the gearbox
assembly (20-220) with the shim (20-210) from the door structure.
(h) Remove the shim (20-210) from the gearbox assembly (20-220).
(i) Measure and identify the thickness of the shim (20-210).
NOTE : Do not remove the pressed-in bush (25-40) from the casing (25-20) unless a
(2) Disassemble the gearbox assembly (20-220).
(a) Remove the nuts (25-160), the washers (25-270) and the bolts (25-340) and remove
the cover assembly (25-180) and the shim (25-170) from the housing (25-10).
(b) Measure and identify the thickness of the shim (20-210).
NOTE : Do not remove the pressed-in bush (25-200) from the cover (25-190) unless
a replacement is necessary (Refer to TASK 52-31-17-300-803-A01).
(c) Remove the shaft assembly (25-70) from the housing assembly (25-10).
NOTE : Do not disassemble the shaft assembly (25-70) unless a replacement is

necessary.
(d) Remove the axle assembly (25-210) from the housing assembly (25-10).
NOTE : Observe the marks on the axle assembly (25-210).
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1 Remove the retaining ring (25--250) and the pin (25--240) from the bevel gear
(25-230).
NOTE : Do not remove the pressed-in bushes (25-40) and the riveted nuts
(25-50) from the casing (25-20) unless a replacement is necessary
(Refer to TASK 52-31-17-300-803-A01 ).
2 Remove the bevel gear (25-230), the thrust washer (25-260) and the axle
(25-220) from the housing assembly (25-10).
NOTE : Do not remove the pressed-in bushes (25-40) and the riveted nuts
(25-50) from the casing (25-20) unless a replacement is necessary
(Refer to TASK 52-31-17-300-803-A01).
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**For PN’s ALL
TASK 52-31-17-000-811-A01
Removal of the Latching Mechanism Assemblies
1. General

ASSEMBLY.
-
attached parts.
disassembly.
are not included.
brackets.
TABLE 1
3. Procedure
Subtask 52-31-17-000-006-A01
A. Removal of the Latching Mechanism Assemblies
NOTE : Do the steps which follow for each of the four latching mechanism assemblies (20,
30).
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(1) Remove and discard the cotter pin (270) from the nut (290).
(2) Remove the nut (290), the bolt (230, 280), the washers (240) and the bushes (250, 260).
(4) Remove the nut (60), the bolt (80), the washers (70, 90), and the sleeve (120).
(5) Remove the nut (150), the bolt (130) and the washers (140).
(7) Remove the nut (190), the bolt (160), the washers (170), and the sleeve (210).
(8) Remove the latching mechanism assemblies (20, 30) from the cargo door.
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**For PN’s ALL
TASK 52-31-17-000-812-A01
Disassembly of the Latching Hook Assemblies
1. General

ASSEMBLY.
-
attached parts.
disassembly.
are not included.
brackets.
NOTE : For the replacement of the identification plates refer to TASK 52-31-17-300-803-A01 .
TABLE 1
3. Procedure
Subtask 52-31-17-040-007-A01
A. Disassembly of the Latching Hook Assemblies
NOTE : Do the steps which follow for each of the four latching hook assemblies.
(1) Remove and discard the cotter pins (140) from the nuts (120).
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(2) Remove the nuts (120), the bolts (80, 150) and the washers (90, 130).
(3) Disconnect the linkage (70) from the bellcrank assembly (160) and from the latching hook
assembly (10).
(4) Remove the bushes (100, 110) from the linkage (70).
(5) Remove the sleeves (60) from the latching hook assembly (10) and from the bellcrank
assembly (160).
NOTE : Do not remove

- the pressed-in bushes (40, 50) from the latching hook (20) unless a
replacement is necessary (Refer to TASK 52-31-17-300-803-A01),
- the lubricating fitting (30) from the Latching hook (20) unless a replacement
is necessary,
- the pressed-in bushes (180, 190) from the bellcrank (170) unless a
replacement is necessary (Refer to TASK 52-31-17-300-803-A01) and
- the Lubricating fitting (200) from the bellcrank (170) unless a replacement is
necessary.
(7) Remove the nut (250), the bolt (210), the washers (220) and the bush (240) and remove
the connecting rod (260) from the bellcrank (170).
NOTE : Do not remove the pressed-in bush (230) from the bellcrank (170) unless a
NOTE : Do not disassemble the connecting rod (260).
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**For PN’s ALL
TASK 52-31-17-000-813-A01
Removal and Disassembly of the Latching Shaft Assembly
1. General

ASSEMBLY.
-
attached parts.
disassembly.
are not included.
brackets.
TASK 52-31-17-000-804-A01 Removal of the Hand Lever Mechanism
TASK 52-31-17-000-814-A01 Removal and Disassembly of the Interlock Mechanism
TABLE 1
3. Procedure
Subtask 52-31-17-000-008-A01
A. Removal and Disassembly of the Latching Shaft Assembly
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NOTE : Before you remove the latching shaft assembly, make sure that the hand lever
assembly (Refer to TASK 52-31-17-000-804-A01) and the locking mechanism
assemblies (Refer to TASK 52-31-17-000-814-A01) are disconnected.
(1) Remove the nuts (60), the sleeves (50) and the taper pins (40).
(2) Remove the Latching shaft (10), the shaft levers (30, 120), the switch Lever (110), the
hinged Lever assembly (70) and the cam stop (100).
NOTE : Do not remove the bonded-in bearing (90) from the hinged lever (80) unless a
NOTE : Identify the position of the shaft levers (30, 120).
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**For PN’s ALL
TASK 52-31-17-000-814-A01
Removal and Disassembly of the Interlock Mechanism
1. General
-
disassembly.
are not included.
brackets.
52-31-17-300-803-A01.
TABLE 1
3. Procedure
Subtask 52-31-17-000-009-A01
A. Removal and Disassembly of the Interlock Mechanism
WARNING : THE COMPRESSION SPRING IS INSTALLED WITH LOAD. REMOVE IT

CAREFULLY.
(1) Remove the interlock mechanism (90).
(a) Compress the compression spring (40) and the spring sleeve assembly (10) to decrease
its length.
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(b) Remove and discard the cotter pins (60) from the pins (50).
(c) Remove and discard the cotter pin (280) from the nut (290).
(d) Remove the nut (290), the bolt (260) and the washers (300).
(e) Remove the bushes (230, 270) and remove the interlock mechanism (90) from the
cargo door.
(f) Remove and discard the cotter pin (60) from the nut (240).
(g) Remove the nut (240), the bolt (250) and the washers (70, 220).
(h) Remove the pin (50) and the washer (70).
(i) Remove the washer (70), the pin (50) and the spacers (80) and remove the spring
sleeve assembly (10) and the compression spring (40).
NOTE : Do not remove the pressed-in bush (30) from the spring sleeve (20) unless a
replacement is necessary (Refer to REPAIR, TASK 52-31-17-300-803-A01).
(2) Disassemble the interlock mechanism (90).
(a) Remove the retaining ring (160) and the pin (110).
(b) Remove the retaining rings (160), the pins (110) and remove the connecting rod
(150) from the levers (100, 170).
(c) Remove the adjusting screw (180), the nut (190) and the Locking plate (200) from
the lever (170).
(d) Remove the retaining ring (120), the pin (130) and the roller (140) from the lever
(100).
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**For PN’s ALL
TASK 52-31-17-000-815-A01
Removal of the Locking Shaft Assembly
1. General

ASSEMBLY.
-
attached parts.
disassembly.
are not included.
brackets.
A. Referenced Information
TASK 52-31-17-000-804-A01 Removal of the Hand Lever Mechanism
TASK 52-31-17-000-809-A01 Removal and Disassembly of the Vent Door Assembly
TASK 52-31-17-000-806-A01 Removal and Disassembly of the Drift Pin Rods
TABLE 1
3. Procedure
Subtask 52-31-17-010-005-A01
A. Removal of the Locking Shaft Assembly
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NOTE : Before you remove the locking shaft assembly, make sure that the hand lever assembly
(Refer to TASK 52-31-17-000-804-A01), the vent door mechanism (Refer to TASK
52-31-17-000-809-A01) and the drift pin mechanism (Refer to TASK
52-31-17-000-806-A01) are disconnected.
(1) Remove the nuts (30), the washers (40), the sleeves (50), the taper pins (20) and the rivet
pins (120).
(a) Discard the nuts (30) and the rivet pins (120).
(2) Identify and record the position of the locking cams (130).
(3) Remove the locking shaft (10) with the lever (140), the lever assembly (90) and the hinged
lever assembly (60).
NOTE : Do not remove the bonded-in bearings (80, 110) from the lever (100) and the
hinged lever (70) unless a replacement is necessary (Refer to TASK
52-31-17-300-803-A01).
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**For PN’s ALL
TASK 52-31-17-000-816-A01
Removal of the Cargo Door Drainage
1. General

ASSEMBLY.
-
attached parts.
disassembly.
are not included.
brackets.
TABLE 1
3. Procedure
Subtask 52-31-17-010-006-A01
A. Removal of the Cargo Door Drainage

(1) Remove the hose (10).
(a) Cut and discard the cable ties (90).
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(b) Remove the nut (130), the bolt (110) and the washers (120) and remove the mount
(100) from the door structure.
(c) Remove the hose (10) from the cargo door.
(2) Remove the basic valve (30) and the tube assembly (80).
(a) Remove the nuts (60), the screws (40) and the washers (50).
(b) Remove the flange (70) with the tube assembly (80) and the valve retainer (20) with
the basic valve (30).
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**For PN’s ALL
TASK 52-31-17-000-817-A01
Removal of the Door Proximity Sensors
1. General

ASSEMBLY.
-
attached parts.
disassembly.
are not included.
brackets.
TABLE 1
3. Procedure
Subtask 52-31-17-010-007-A01
A. Removal of the Door Proximity Sensors
NOTE : The proximity sensors are referred to as proximity switches in this paragraph.
(1) Disconnect the electrical harness from the proximity sensors (10).
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(2) Install blanking caps at the electrical connectors.

(3) Remove the proximity sensor 5MJ (10, Detail C)
(a) Remove the nuts (60), the washers (50) and the screws (40) and remove the
proximity sensor (10) from the door structure.
(4) Remove the proximity sensor 28WV (10, Detail B).
(a) Remove the screws (40) and remove the proximity sensor (10) from the door
structure.
(5) Remove the targets (20).
(a) Remove the nuts (60), the washers (50) and the screws (40) and remove the targets
(20) from the door mechanism.
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**For PN’s ALL
TASK 52-31-17-000-818-A01
Removal of the Hinge Assemblies
1. General
-
NOTE : If necessary, refer to REPAIR, TASK 52-31-17-300-803-A01, for the replacement of the
disassembly.
are not included.
brackets.
52-31-17-300-803-A01.
TABLE 1
3. Procedure
Subtask 52-31-17-010-008-A01
A. Removal of the Hinge Assemblies

(1) Remove the end fittings (90-10, 91-60).
(a) Remove the nuts (90), the screws (70, 100) and the washers (80, 110) and remove
the end fittings (90-10, 91-60) and the shims (90-20, 91-50).
(b) Identify and record the thickness of the shims (90-20, 91-50).
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(2) Remove the hinge assemblies (90-30, 60), (91-10, 20).
NOTE : Do not remove the hinge assemblies (90-30, 60), (91-10, 20) from the door
structure unless a replacement is necessary. If you must remove a defective hinge
assembly, you must measure and identify the position and the thickness of the
hinge shims.
NOTE : Do not remove the bushes (90-50, 64,66), (91-14,16,40) from the hinges (90-40,
62), (91-12,30) unless a replacement is necessary (Refer to REPAIR, TASK
52-31-17-300-803-A01).
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CLEANING
**For PN’s ALL
TASK 52-31-17-100-801-A01
Cleaning
1. General
- Not applicable
11-001 Detergent
19-003 Lint-Free Cotton Cloth
11-003 Methyl-Ethyl-Ketone
11-010 Isopropyl Alcohol
11-019 Cabin Window Cleaner
TABLE 1
B. Fixtures, Tools, Test and Support Equipment

vacuum cleaner
TABLE 2
3. Procedure
Subtask 52-31-17-100-001-A01
A. Clean the Painted Component Parts as follows:
(1) Remove loose dirt with a vacuum cleaner or a soft brush.
(2) Remove old sealant and remaining dirt with a nonmetallic scraper.
WARNING : BE CAREFUL WHEN YOU USE MATERIAL NO. 11-001 DETERGENT. OBEY
THE MATERIAL MANUFACTURER’S INSTRUCTIONS.
CAUTION : USE ONLY THE SPECIFIED CLEANING AGENT (MATERIAL NO. 11-001).
(3) Clean the painted component parts with Material No. 11-001 Detergent.
(a) Use a soft brush or Material No. 19-003 Lint-Free Cotton Cloth.
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(4) Remove Material No. 11-001 Detergent with clean water.
(5) Dry component parts with Material No. 19-003 Lint-Free Cotton Cloth or a hot-air blower.
Subtask 52-31-17-100-002-A01
B. Clean the Component Parts which are not painted as follows:
(1) Remove loose dirt with a vacuum cleaner or a soft brush.
(2) Remove remaining dirt with a nonmetallic scraper.
WARNING : BE CAREFUL WHEN YOU USE MATERIAL NO. 11-003 METHYL-ETHYL-

KETONE. OBEY THE MATERIAL MANUFACTURER’S INSTRUCTIONS.
(3) Clean the component parts which are not painted with Material No. 11-003 Methyl-Ethyl-
Ketone.
(a) Use a soft brush or a clean Material No. 19-003 Lint-Free Cotton Cloth.
Subtask 52-31-17-100-003-A01
C. Clean the Electrical Components as follows:
WARNING : BE CAREFUL WHEN YOU USE MATERIAL NO. 11-010 ISOPROPYL

ALCOHOL. OBEY THE MATERIAL MANUFACTURER’S INSTRUCTIONS.
(1) Clean the electrical wiring with Material No. 11-010 Isopropyl Alcohol or an equivalent
cleaning agent.

ALCOHOL. OBEY THE MATERIAL MANUFACTURER’S INSTRUCTIONS.
(2) Clean the electrical connectors with Material No. 11-010 Isopropyl Alcohol.
Subtask 52-31-17-100-004-A01
D. Clean the Sight Glasses as follows:
CAUTION : DO NOT RUB THE SURFACE WITH DRY CLOTH.

(1) Clean the sight glasses with a weak soap solution.
(2) Dry the sight glasses with clean, dry Material No. 19-003 Lint-Free Cotton Cloth .
(3) If more cleaning is required, clean the sight glasses with Material No. 11-019 Cabin
Window Cleaner and dry them with clean, dry Material No. 19-003 Lint-Free Cotton Cloth
.
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INSPECTION/CHECK
**For PN’s ALL
TASK 52-31-17-210-801-A01
Door Structure
1. General
A. This check is a visual inspection of the component parts and a check of the spring values.
B. Do an approved nondestructive test if you think there is a crack which is not clearly visible.
C. Refer to the Structural Repair Manual (SRM) for the door structure.
WARNING : BE CAREFUL WHEN YOU USE SOLVENTS/CLEANING AGENTS, SEALANTS AND

OTHER MATERIALS. OBEY THE MATERIAL MANUFACTURER’S INSTRUCTIONS
AND THE LOCAL REGULATIONS. MAKE SURE THAT THERE IS A GOOD FLOW
OF AIR THROUGH THE WORK AREA. DO NOT BREATHE THE FUMES. DO NOT
SMOKE. DO NOT USE THESE MATERIALS NEAR A FLAME, SPARKS OR
SOURCES OF HEAT. USE PROTECTIVE CLOTHING, GOGGLES AND GLOVES. IF
YOU GET ONE OF THESE MATERIALS ON YOUR SKIN OR IN YOUR EYES,
FLUSH IT AWAY WITH A FLOW OF CLEAN WATER. IF YOU GET ONE OF
THESE MATERIALS IN YOUR MOUTH, GET IMMEDIATE MEDICAL AID. IN
GENERAL, THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN
IRRITANTS.
NOTE : Refer to REPAIR, TASK 52-31-17-300-803-A01 for the replacement of the

15-005 Corrosion Preventive Temporary Protective Compound
TABLE 1
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FIGURE 52-31-17-991-009-A FIGURE 52-31-17-991-009-A-Visual Examination of the Surface
Protection and Locking Indication
TABLE 2
3. Procedure
Subtask 52-31-17-210-001-A01
A. Door Structure
(1) Check the door structure for damage.
(a) For the Permitted Damage Limits (PDL) and the repair procedure refer to the
(SRM).
WARNING : BE CAREFUL WHEN YOU USE MATERIAL NO. 15-005 CORROSION

PREVENTIVE TEMPORARY PROTECTIVE COMPOUND. OBEY THE
MATERIAL MANUFACTURER’S INSTRUCTIONS.
(b) Make sure that all inner surfaces of the cargo door have a protection of Material No.
15-005 Corrosion Preventive Temporary Protective Compound (Refer to FIGURE
52-31-17-991-009-A).

(c) Make sure that the outer surface, shown in FIGURE 52-31-17-991-009-A has a
protection of Material No. 15-007 Corrosion Preventive Temporary Protective
Compound.
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**For PN’s ALL
CARGO DOOR
SEAL
FR24A
CARGO DOOR
INSULATION
CORROSION PREVENTIVE CORROSION PREVENTIVE

(MAT. NO. 15−005) (MAT. NO. 15−007)
CARGO DOOR
STRUCTURE
CARGO DOOR SURFACE PROTECTION
LOCKING SHAFT
(REFER TO THE IPL−FIGURE 31)
83
AREA OF RED MARKING
43
AREA OF GREEN MARKING
LOCKING CAM, ITEM 130

TYPICAL DIRECT VISUAL LOCKING INDICATION

F_CM_523117_1_0090101_01_00
Visual Examination of the Surface Protection and Locking Indication

FIGURE-52-31-17-991-009-A01
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**For PN’s ALL
TASK 52-31-17-210-802-A01
Structure Components
1. General
NOTE : Refer to REPAIR, TASK 52-31-17-300-803-A01for the replacement of the

TABLE 1
3. Procedure
Subtask 52-31-17-210-002-A01
A. Structure Components
CAUTION : THE LIMITS ARE ALWAYS RELATED TO THE NOMINAL MATERIAL

THICKNESS.
NOTE : Refer to IPL_FIGURE_90 and IPL_FIGURE_91 for the Hinges

(1) Do a check of the structure components for cracks or corrosion.
(a) Cracks and corrosion are not permitted.
(b) Refer to DISASSEMBLY, ASSEMBLY for the replacement of the structure
components which have cracks and corrosion.
(2) Do a check of the structure components for scratches and marks.
(a) Scratches and marks are permitted up to a depth of 0.25 mm (0.01 in.)
(b) Refer to TASK 52-31-17-300-802-A01, TASK 52-31-17-300-801-A01 for the removal
of scratches or marks which are in the limits.
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(c) Refer to DISASSEMBLY, ASSEMBLY for the replacement of the structure

components which have scratches or marks that are not in the limits.
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**For PN’s ALL
TASK 52-31-17-210-803-A01
Door Seal
1. General

TABLE 1
3. Procedure
Subtask 52-31-17-210-003-A01
A. Door Seal
(1) Do a check of the door seat for hardening, cracks, oil contamination and porosity.
(a) Hardening, cracks, oil contamination or porosity is not permitted,
(b) Refer to DISASSEMBLY, ASSEMBLY for the replacement of the door seal if there is
such damage.
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**For PN’s ALL
TASK 52-31-17-210-804-A01
Door Mechanism
1. General
NOTE : Refer to TASK 52-31-17-300-803-A01 for the replacement of the permanently

attached parts.
TASK 52-31-17-820-806-A01 Fits and Clearances
TABLE 1
3. Procedure
Subtask 52-31-17-210-004-A01
A. Door Mechanism
(1) Do a check of the component parts of the door mechanism for wear.
(a) Refer to TASK 52-31-17-820-806-A01 for the wear limits.
(b) Refer to DISASSEMBLY, ASSEMBLY for the replacement of component parts with
wear not in the limits.
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**For PN’s ALL
TASK 52-31-17-210-805-A01
Locking Mechanism
1. General

TABLE 1
3. Procedure
Subtask 52-31-17-210-005-A01
A. Locking Mechanism
CAUTION : THE LIMITS ARE ALWAYS RELATED TO THE NOMINAL MATERIAL

THICKNESS.
(1) Check for cracks.
(a) Cracks are not permitted.
(b) Refer to DISASSEMBLY, ASSEMBLY for the replacement of the parts which have
cracks.
(2) Check for scratches, marks and corrosion.
(a) Scratches, marks and corrosion are permitted up to a depth of 0.25 mm (0.01 in.).
(b) Refer to REPAIR, TASK 52-31-17-300-802-A01, TASK 52-31-17-300-801-A01 for the
removal of the scratches, marks and corrosion which are in the Limits.
(c) Refer to DISASSEMBLY, ASSEMBLY for the replacement of the parts which have
scratches, marks and corrosion that are not in the Limits.
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(3) Check for deformation.

(a) Deformation is not permitted.
deformation.
(4) Check for wear.
(a) Refer to REPAIR, TASK 52-31-17-300-803-A01, TASK 52-31-17-300-802-A01, TASK
52-31-17-300-801-A01 for the repair of the parts which have wear.
(b) Make sure that the max. outer diameter of the spring bolt (8-460) is not less than
6.25 mm (0.2461 in.).
(c) Replace the parts which have dimensions that are not in the limits.
(5) Check for other damage.
(a) Other damage is not permitted.
other damage.
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**For PN’s ALL
TASK 52-31-17-210-806-A01
Protective Treatment
1. General
NOTE : Refer to TASK 52-31-17-300-803-A01 for the replacement of the permanently

attached parts.
TABLE 1
3. Procedure
Subtask 52-31-17-210-006-A01
A. Protective Treatment
(1) Check the structure components and the door mechanism for damaged protective
treatment.
(a) Refer to TASK 52-31-17-300-802-A01 for the repair of the protective treatment.
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**For PN’s ALL
TASK 52-31-17-210-807-A01
Electrical Equipment
1. General
2. Procedure
Subtask 52-31-17-210-007-A01
A. Electrical Equipment
(1) Check the electrical harness for damaged attachment parts, chafe marks and other damage.
(a) Chafe marks, damaged attachment parts or other damage are not permitted.
(b) Refer to DISASSEMBLY, ASSEMBLY for the replacement of the damaged electrical
harness and attachment parts.
(2) Check electrical components for damage.
(a) Damage is not permitted.
(b) Refer to DISASSEMBLY, ASSEMBLY for the replacement of the electrical
components.
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**For PN’s ALL
TASK 52-31-17-210-808-A01
Springs
1. General
NOTE : Refer to REPAIR, TASK 52-31-17-300-803-A01, for the replacement of the

TABLE 1
3. Procedure
Subtask 52-31-17-210-008-A01
A. Springs
(1) Check for damage.
(a) Damage is not permitted.
(b) Refer to DISASSEMBLY, ASSEMBLY for the replacement of the springs which have
damage.
(2) Check the spring data.
(a) For the test data refer to TABLE 2 and TABLE 3.
(b) For the torsion spring refer to Figure 1.
(c) Refer to DISASSEMBLY, ASSEMBLY for the replacement of the springs which have
test data that are not in the limits.
IPL ITEM FREE LENGTH TEST LENGTH LOAD
FIG.
mm (in.) mm (in.) daN (lbf.)
8 470 61.0 (2.402) 45.2 (1.780) 25.90-31.14 (50.43-66.76)
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IPL ITEM FREE LENGTH TEST LENGTH LOAD

FIG.
mm (in.) mm (in.) daN (lbf.)
44 40 98.0 (3.858) 78.0 (3.071) 7.08-13.10 (13.65-18.18)
Spring Test Data
TABLE 2
IPL
Figure Item Pos. Angle daNm Lbf. in.
A 9 110 A1 68.9 deg. 0.018-0.022 1.60-1.94
A2 127.9 deg. 0.032-0.040 2.84-3.54
Test Data of the Torsion Spring
TABLE 3
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**For PN’s ALL
TASK 52-31-17-210-809-A01
Placard
1. General
NOTE : Refer to REPAIR, TASK 52-31-17-300-803-A01, for the replacement of the

TABLE 1
3. Procedure
Subtask 52-31-17-210-009-A01
A. Self-adhesive and Bonded Identification Plates

(1) Check the identification plate for readability and attachment.
(a) Loose or damaged identification plates are not permitted.
(b) Refer to REPAIR, TASK 52-31-17-300-803-A01 for the replacement of the damaged
identification plates.
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**For PN’s ALL
TASK 52-31-17-210-810-A01
Visual Examination
1. General
NOTE : Refer to TASK 52-31-17-300-803-A01, TASK 52-31-17-300-802-A01, TASK

52-31-17-300-801-A01 for the replacement of the permanently attached parts.
FIGURE 52-31-17-991-010-A FIGURE 52-31-17-991-010-A-Visual Examination of the Surface
Protection and Locking Indication
TABLE 1
3. Procedure
Subtask 52-31-17-210-010-A01
A. Visual Examination
(1) Examine all screws, bolts, nuts and tapered pins for general condition, wear and other
damage.
(2) Examine all bearings for correct movement without play.
(3) Examine all bushes for wear, scratches, corrosion and correct installation.
(4) Examine all bonding leads for damage and corrosion.
(5) Examine all nut plates for damaged threads, correct attachment and corrosion.
(6) Examine the hoist fittings for defective threads and corrosion.
(7) Examine the insulation for contamination and correct attachment.
(8) Make sure that the hoses, the water drain valves and holes are clean and not blocked.
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(9) Examine the red painted areas of the hand lever assembly, the handle flap and the inside of
the vent door frame for damage.
(10) Examine the lubrication fittings for damage.
(11) Examine the red and green markings on the locking cams for damage (Refer to FIGURE
52-31-17-991-010-A).
(12) Examine the sight glasses installed to the access cover for damage.
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**For PN’s ALL
CARGO DOOR
SEAL
FR24A
CARGO DOOR
INSULATION
CORROSION PREVENTIVE CORROSION PREVENTIVE

(MAT. NO. 15−005) (MAT. NO. 15−007)
CARGO DOOR
STRUCTURE
CARGO DOOR SURFACE PROTECTION
LOCKING SHAFT
83
AREA OF RED MARKING
43
AREA OF GREEN MARKING
LOCKING CAM, ITEM 130

TYPICAL DIRECT VISUAL LOCKING INDICATION

F_CM_523117_1_0100101_01_00
Visual Examination of the Surface Protection and Locking Indication

FIGURE-52-31-17-991-010-A01
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REPAIR
**For PN’s ALL
TASK 52-31-17-300-801-A01
Reworking or Machining
1. General

IRRITANTS.
CAUTION : USE ONLY THE SPECIFIED MATERIALS. MATERIALS WHICH ARE NOT
SPECIFIED, CAN CAUSE DAMAGE.
CAUTION : AFTER THE REMOVAL OF THE DAMAGE THE COMPONENTS PARTS MUST BE
IN THE LIMITS. REFER TO CHECK FOR THE LIMITS.
-
NOTE : Refer to CHECK and FITS AND CLEARANCES for the limits of the component parts.
11-001 Detergent
11-016 Safety Solvent
08-004 Adhesive Sealant
05-024 Fabric
05-023 Polyterepthalate
TABLE 1
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abrasive cloth
TABLE 2
C.Referenced Information
FIGURE 52-31-17-991-011-A FIGURE 52-31-17-991-011-A-Door Seal Repair
FIGURE 52-31-17-991-012-A FIGURE 52-31-17-991-012-A-Door Seal Repair
FIGURE 52-31-17-991-013-A FIGURE 52-31-17-991-013-A-Bonding Block
TABLE 3
3. Procedure
Subtask 52-31-17-300-001-A01
A. Repair of Scratches and Marks
CAUTION : THE WIDTH OF THE GROOVE AFTER THE REPAIR MUST NOT BE MORE
THAN 6 MM (0.24 IN.).
(1) Remove the necessary material from the scratch or the mark to make a shallow groove.
NOTE : Do not remove more material than necessary and keep the width to 6 mm (0.24
in.).
(2) Make the groove smooth with abrasive cloth.
(3) Burnish the surface with your hands or with a buffing wheel.
(4) Repair the damaged paintwork as specified in TASK 52-31-17-300-802-A01.
Subtask 52-31-17-300-002-A01
B. Repair of Corrosion Damage
(1) Clean the corroded and the adjacent areas and remove the grease with Material No. 11-001
Detergent.
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(2) Dry the wet areas with clean, dry Material No. 19-003 Lint-Free Cotton Cloth.
NOTE : Before you start to repair the corrosion damage, approved persons must make an
analysis of the level of the corrosion damage.
(3) Remove the surface protection from the corroded area with an abrasive cloth.
(4) Remove the corroded material.
(a) Apply masking material around the corroded area.
(b) Remove the corrosion with a synthetic sponge and/or an abrasive cloth.
(c) Feather the material to the adjacent area, so that the transition to the work area is
smooth and without stress concentrations.

(d) Clean the work area with Material No. 11-003 Methyl-Ethyl-Ketone.
(e) Let the work area dry.
(5) Use a magnifying glass to make sure that all corroded material is removed and that there
are no cracks.
NOTE : It is important that all corroded material is removed before you continue the
work. The smallest corroded area can cause new extended corrosion damage.
NOTE : If you find a defect, you must do an approved nondestructive test.

(6) Repair the damaged paintwork as specified in TASK 52-31-17-300-802-A01.
(7) Remove the masking material.
Subtask 52-31-17-300-003-A01
C. Repair of the Cargo Door Seal
CAUTION : MAKE CERTAIN THAT THE SEAL IS TAGGED ’TO BE SUBJECTED TO A

FUSELAGE PRESSURIZATION CHECK’ AFTER INSTALLATION OF THE
DOOR.
NOTE : Refer to FIGURE 52-31-17-991-011-A, FIGURE 52-31-17-991-012-A, and FIGURE

52-31-17-991-013-A.
(1) Remove the cargo door seal from the seal retainer.
(2) Repair the chafe marks and cuts (maximum of 25.4 mm (1.0 in.)) and not in the contact
area (Refer to FIGURE 52-31-17-991-011-A) as follows:
(a) Drill a stop hole of 2 mm (0.08 in.) dia. at each end of the cut.
(b) Apply pressure to the seal to open the cut.
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(c) Make the face of the cut rough with an abrasive cloth.
(d) Carefully remove the first layer of the reinforced tissue from the door seal for a
distance of 10 mm (0.4 in.) around the cut.
(e) Prepare the surface of the repair area with a very fine abrasive cloth.
WARNING : BE CAREFUL WHEN YOU USE MATERIAL NO. 11-016 SAFETY

SOLVENT. OBEY THE MATERIAL MANUFACTURER’S INSTRUCTIONS.
(f) Clean the repair area with Material No. 11-016 Safety Solvent.
(g) Dry the cleaned area with Material No. 19-003 Lint-Free Cotton Cloth .
WARNING : BE CAREFUL WHEN YOU USE MATERIAL NO. 08-004 ADHESIVE

SEALANT. OBEY THE MATERIAL MANUFACTURER’S INSTRUCTIONS.
(h) Apply a thin coat of Material No. 08-004 Adhesive Sealant to the faces of the cut.
(i) Press the faces of the cut together and allow them to cure.
(j) Cut a piece of Material No. 05-024 Fabric to the size of the repair area.

(k) Apply a thin layer of Material No. 08-004 Adhesive Sealant to the repair area and fill
the stop holes.
(l) Install the prepared replacement tissue to the repair area so that it is as smooth as
the seal surface.
(m) Cover the repair area with a layer of Material No. 05-023 Polyterepthalate and install
the seal in the wooden bonding block (Refer to FIGURE 52-31-17-991-013-A).
(n) Compress the seal for 24 hours in the wooden bonding block with a clamp.
(o) Remove the bonding block and the special material from the repair area of the seal.
(p) Polish the repair area with very fine abrasive cloth to get a smooth surface of the seal.
(3) Repair the chafe marks and cuts exceeding 25.4 mm (1.0 in.) in the length or in the
contact area, by replacement of a section (Refer to FIGURE 52-31-17-991-012-A).
NOTE : The repair area must be s = minimum of 50 mm (1.97 in.) from the inflation
holes.
(a) Remove the damaged section of the seal.
(b) In straight and curved sections, cut the replacement section of the seal to the same
length as the removed section.
NOTE : Make sure that the quantity of the inflation holes are the same as in the
removed section.
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(c) Carefully remove the first layer of the tissue reinforcement from the ends of the seal
and the replacement sections over a length of 25.4 mm (1.0 in.).
(d) Make the surfaces of the repair areas rough with an abrasive cloth.
WARNING : BE CAREFUL WHEN YOU USE MATERIAL NO. 11-016 SAFETY

SOLVENT. OBEY THE MATERIAL MANUFACTURER’S INSTRUCTIONS.
(e) Clean the surface with Material No. 11-016 Safety Solvent.
(f) Dry the cleaned area with Material No. 19-003 Lint-Free Cotton Cloth .

(g) Apply a thin coat of Material No. 08-004 Adhesive Sealant to the ends of the seals
and the replacement sections.
(h) Press and hold the ends of the replacement section and the seal together and allow
them to cure.
(i) Cut a piece of Material No. 05-024 Fabric to the size of the repair areas.

(j) Apply a thin layer of Material No. 08-004 Adhesive Sealant to the contact surface of
the replacement tissue and the repair areas.
(k) Install the replacement tissue to the repair areas.
(l) Cover the repair area with a layer of Material No. 05-023 Polyterepthalate and install
the seal in the wooden bonding block (Refer to FIGURE 52-31-17-991-013-A).
(m) Compress the seal over a period of 24 hours in the wooden bonding block with a
clamp.
(n) Remove the bonding block and the special material from the repair area of the seal.
(o) Prepare the repair area with very fine abrasive cloth to get a smooth surface of the
seal.
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**For PN’s ALL
"V" B
C
C
"X"
B
CONTACT AREA SECTION

90 deg.
"W" B−B
"X"
"V" = DIA STOP HOLE 2.0mm (0.08 in.)

"W" = MAX LENGTH OF CUT 25.4mm (1.0 in.)
"X" = MIN REPAIR AREA AROUND CUT 10mm (0.4 in.)
REPLACEMENT
1 AREA IN WHICH THE FIRST LAYER TISSUE
OF REINFORCEMENT TISSUE IS REMOVED
F_CM_523117_1_0110101_01_00
Door Seal Repair

FIGURE-52-31-17-991-011-A01
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**For PN’s ALL
"S"
"T"
"U"
"U"
C
"Y"
A
"Y"
SECTION
EXISTING
C−C REPLACEMENT B
DOOR SEAL SECTION
C
REPLACEMENT
SECTION
B
EXISTING
REPLACEMENT TISSUE DOOR SEAL LAYER OF TISSUE
REPLACEMENT
SECTION
B−B
"S" = MIN DISTANCE OF 50mm (1.97 in.) FROM
INFLATION HOLE 1
"T" = MIN REPAIR LENGTH OF 200mm (7.87 in.)
"U" = MIN REPAIR LENGTH OF 200mm (7.87 in.)
FOR RADII
"Y" = MIN ABRADED LENGTH OF REPAIR
AREA 25.4mm (1.0 in.)
1 AREA IN WHICH THE FIRST LAYER

OF REINFORCEMENT TISSUE IS REMOVED SEAM
F_CM_523117_1_0120101_01_00
Door Seal Repair

FIGURE-52-31-17-991-012-A01
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**For PN’s ALL
19.4mm
(0.76 in.)
1.0mm rad.
(0.04 in. rad.)
UPPER
HALF
(0.55 in.)
(0.63 in.)
14.0mm
16.0mm
LOWER
HALF
1.5mm rad.
(0.06 in. rad.)
NOTE: THE BONDING BLOCK CAN BE MANUFACTURED FROM HARDWOOD.

USE THE DIMENSIONS AS DETAILED. LENGTH AS REQUIRED.
F_CM_523117_1_0130101_01_00
Bonding Block
FIGURE-52-31-17-991-013-A01
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**For PN’s ALL
TASK 52-31-17-300-802-A01
Protective Treatment
1. General

IRRITANTS.
-
16-020 Wash Primer
16-001 Anti Corrosion Primer (Polyurethane)
16-002 Polyurethane Topcoat Grey (for Internal Applic.)
13-002 Chemical Conversion Coating Yellow Aluminum
15-004 Corrosion Preventive Compound
TABLE 1
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abrasive cloth
TABLE 2
3. Procedure
Subtask 52-31-17-300-004-A01
A. Repair of Damaged Paintwork
(1) Remove the damaged paintwork with an abrasive cloth.
(2) Remove the paint dust.

(3) Clean the work area with Material No. 11-003 Methyl-Ethyl-Ketone.
NOTE : Do not touch the cleaned area.

(4) Let the work area dry.
WARNING : BE CAREFUL WHEN YOU USE MATERIAL NO. 16-020 WASH PRIMER. OBEY
(5) Apply 16-020 Wash Primer to the metal surface.
WARNING : BE CAREFUL WHEN YOU USE MATERIAL NO. 16-020 WASH PRIMER. OBEY
(6) Let the 16-020 Wash Primer dry.
WARNING : BE CAREFUL WHEN YOU USE MATERIAL NO. 16-001 ANTI CORROSION
PRIMER (POLYURETHANE). OBEY THE MATERIAL MANUFACTURER’S
INSTRUCTIONS.
(7) Apply Material No. 16-001 Anti Corrosion Primer (Polyurethane).
WARNING : BE CAREFUL WHEN YOU USE MATERIAL NO. 16-001 ANTI CORROSION
PRIMER (POLYURETHANE). OBEY THE MATERIAL MANUFACTURER’S
INSTRUCTIONS.
(8) Let the Material No. 16-001 Anti Corrosion Primer (Polyurethane) dry.
WARNING : BE CAREFUL WHEN YOU USE MATERIAL NO. 16-002 POLYURETHANE

TOPCOAT GREY (FOR INTERNAL APPLIC.). OBEY THE MATERIAL
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(9) Apply Material No. 16-002 Polyurethane Topcoat Grey (for Internal Applic.).
WARNING : BE CAREFUL WHEN YOU USE MATERIAL NO. 16-002 POLYURETHANE

TOPCOAT GREY (FOR INTERNAL APPLIC.). OBEY THE MATERIAL
(10) Let the Material No. 16-002 Polyurethane Topcoat Grey (for Internal Applic.) dry.
Subtask 52-31-17-300-005-A01
B. Repair of Anodized Surfaces

(1) Clean the area with Material No. 11-003 Methyl-Ethyl-Ketone.
WARNING : BE CAREFUL WHEN YOU USE MATERIAL NO. 13-002 CHEMICAL

CONVERSION COATING YELLOW ALUMINUM. OBEY THE MATERIAL
CAUTION : MAKE SURE THAT THE COATING MATERIAL NO. 13-002 - CHEMICAL
CONVERSION COATING YELLOW ALUMINUM DOES NOT GO INTO GAPS
OR BELOW FASTENERS WHERE YOU CANNOT MAKE IT NEUTRAL.
COATING WHICH YOU DO NOT MAKE NEUTRAL CAUSES NEW
CORROSION.
(2) Apply Material No. 13-002 Chemical Conversion Coating Yellow Aluminum to the prepared
area and let it work for 3 minutes.
(3) Make the area neutral with clean water.
(4) Dry the repaired area with warm air up to a maximum temperature of 60 deg. C (140 deg.
F).
Subtask 52-31-17-300-006-A01
C. Repair of Corrosion Preventive

PREVENTIVE COMPOUND. OBEY THE MATERIAL MANUFACTURER’S
INSTRUCTIONS.
(1) Apply Material No. 15-004 Corrosion Preventive Compound to the components.
NOTE : Make sure that the existing drain holes are not blocked.
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**For PN’s ALL
TASK 52-31-17-300-803-A01
Replacement of Parts
1. General

IRRITANTS.
-
09-013 Corrosion Inhibiting Brush Consistency
09-016 Corrosion Inhibiting Fillet Consistency
16-021 Flexible Polyurethane
08-029 Adhesive
08-007 Sealant, High Temperature
08-050 Adhesive
08-001 General Purpose Adhesive Honeycomb Filler
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07-023 Protective Coating, Transparent
TABLE 1

nonmetallic scraper
TABLE 2
C. Referenced Information
TASK 52-31-17-940-807-A01 Special Tool
PMS 01-05-05
PMS 01-05-27
PMS 01-05-04
PMS 01-05-45
PMS 01-02-41
TABLE 3
3. Procedure
Subtask 52-31-17-300-007-A01
A. Replacement of the Pressed-in Bushes
CAUTION : BE CAREFUL NOT TO CAUSE DAMAGE TO THE EDGES OF THE

COMPONENT BORE.
NOTE : The component parts with the pressed-in bushes are given in TABLE 4.
NOTE : If you find a damaged bush in one hinge assembly, you must replace all bushes in the
hinge assembly. Use the local manufactured special tool (Refer to TASK
52-31-17-940-807-A01) for the replacement of the bushes in the hinge assemblies.
(1) Remove the bush from the component part with an applicable press-tool.

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(2) Remove the grease and clean the component bore with Material No. 11-003 Methyl-Ethyl-
Ketone.
(3) Let the component bore dry.
(4) Visually examine the component bore for damage.
IPL FIGURE COMPONENT NAME OF COMPONENT BUSH ITEM
ITEM
2 -1A Fire Protection Installation 160
8 380 Roller Lever 390
8 520 Universal Joint Latch 530
44 20 Spring Sleeve 30
40 90 Cover 100
33,34 20 Latching Hook 40, 50
33,34 170 Bellcrank 180, 190, 230
20 400 Lever 390, 410
21 230 Actuator Arm 240, 250, 300, 310, 320
21 360 Arm 370, 420
25 190 Cover 200
25 20 Casing 30, 40
25 320 Lever 330
90 40 Outer Hinge 50
90 62 Inner Hinge 64,66
91 12 Mid Hinge 14,16
91 30 Outer Hinge 40
Pressed-in Bushes
TABLE 4

INHIBITING BRUSH CONSISTENCY. OBEY THE MATERIAL
(5) Install the new bush in accordance with PMS 01-05-05.
NOTE : You must install the bush with Material No. 09-013 Corrosion Inhibiting Brush
Consistency.
(6) Check the installed bush for correct and satisfactory installation.

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(7) Carefully remove Material No. 09-013 Corrosion Inhibiting Brush Consistency from the
surfaces of the component part and the bush with a cloth soaked in Material No. 11-003
Methyl-Ethyl-Ketone.

INHIBITING FILLET CONSISTENCY. OBEY THE MATERIAL
(8) Apply Material No. 09-016 Corrosion Inhibiting Fillet Consistency to the joint between the
component bore and the bush.

(9) Let the Material No. 09-016 Corrosion Inhibiting Fillet Consistency dry.
WARNING : BE CAREFUL WHEN YOU USE MATERIAL NO. 16-021 FLEXIBLE

POLYURETHANE. OBEY THE MATERIAL MANUFACTURER’S
INSTRUCTIONS.

(10) Apply Material No. 16-021 Flexible Polyurethane to Material No. 09-016 Corrosion
Inhibiting Fillet Consistency.

INSTRUCTIONS.
(11) Let the Material No. 16-021 Flexible Polyurethane dry.
Subtask 52-31-17-300-008-A01
B. Replacement of the Bonded-in Bushes
NOTE : The component part with the bonded-in bushes is given in TABLE 5.
(1) Bonded-in Bushes
IPL FIGURE COMPONENT ITEM NAME OF BUSH ITEM
COMPONENT
9 30 Stop 70
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IPL FIGURE COMPONENT ITEM NAME OF BUSH ITEM

COMPONENT
9 100 Handle Flap 180
Bonded-in Bushes
TABLE 5
(2) Heat the component part to a maximum temperature of 120 deg. C (248 deg. F) to soften
the bond of the bush.
(3) Press out the bush with a suitable tool.

WARNING : BE CAREFUL WHEN YOU USE MATERIAL NO. 08-029 ADHESIVE. OBEY
(4) Clean the component bore and the new bush with Material No. 11-003 Methyl-Ethyl-
Ketone.
NOTE : You must use a nonmetallic scraper to remove the unwanted Material No.
08-029 Adhesive.
CAUTION : DO NOT TOUCH THE BONDING SURFACES. CONTAMINATION CAN

CAUSE AN UNSATISFACTORY BOND.
(5) Dry the component bore and the bush with Material No. 19-003 Lint-Free Cotton Cloth .
(6) Install the new bush in accordance with PMS 01-05-27.
NOTE : You must install the bush with Material No. 08-029 Adhesive.

INSTRUCTIONS.
(7) Apply Material No. 16-021 Flexible Polyurethane to the gap between the bush and the
component part.
Subtask 52-31-17-300-009-A01
C. Replacement of the Bonded-in Bearings
NOTE : The component parts with the bonded-in bearings are given in TABLE 6.
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(1) Bonded-in Bearings

IPL FIGURE COMPONENT ITEM NAME OF BEARING ITEM
COMPONENT
8 90 Lever 100
8 520 Universal Joint Latch 590
31 100 Lever 110
31 700 Hinged Lever 80
32 80 Hinged Lever 90
40 120 Beam 4 Lever 130
13 110 Bellcrank 120
13 140 Lever 150
20 240 Connecting Rod 250
Bonded-in Bearings
TABLE 6
CAUTION : DO NOT DAMAGE EDGES OF COMPONENT BORE.

(2) Remove the bearing from the component with an applicable tool.

CAUTION : HANDLING OF SURFACE AFTER DEGREASING WILL IMPAIR BONDING.

(3) Clean the component bore with Material No. 11-003 Methyl-Ethyl-Ketone.
NOTE : Use a wooden or a plastic nonmetallic scraper to remove the old Material No.
08-029 Adhesive.

(4) Clean the outer ring of the new bearing with Material No. 11-003 Methyl-Ethyl-Ketone.
(5) Dry the parts in a warm air furnace. Alternatively, you can use hot air at a temperature of
30 to 40 deg. C (86 to 104 deg. F) and a relative humidity of 50 % for approx. 30 minutes.
(6) Install the bearing in the component in accordance with PMS 01-05-27.
NOTE : You must install the bearing with Material No. 08-029 Adhesive.
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(7) When the bearing is installed, apply a small quantity of Material No. 08-029 Adhesive to
the gap between the bearing and the component.
(8) Examine the bond and make sure that the bearing is correctly installed.
(9) Remove the unwanted Material No. 08-029 Adhesive from the bearing and the component
with clean Material No. 19-003 Lint-Free Cotton Cloth .
(10) Keep the parts at a room temperature for at least 30 minutes and let the part cure as it is
specified in PMS 01-05-27.
NOTE : Keep the component in such a position that the bond can cure.
(11) Do not put a load on the bonded bearing until it has cured for 24 hours at room
temperature.

(12) Carefully remove the unwanted Material No. 08-029 Adhesive with Material No. 19-003
Lint-Free Cotton Cloth soaked with Material No. 11-003 Methyl-Ethyl-Ketone.

(13) Apply Material No. 09-016 Corrosion Inhibiting Fillet Consistency to the joint between the
component bore and the bearing.

(14) Let Material No. 09-016 Corrosion Inhibiting Fillet Consistency dry.

INSTRUCTIONS.

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(15) Apply Material No. 16-021 Flexible Polyurethane to Material No. 09-016 Corrosion

INSTRUCTIONS.
(16) Let Material No. 16-021 Flexible Polyurethane dry.
Subtask 52-31-17-300-010-A01
D. Replacement of the Hinge Assembly
NOTE : A detailed procedure for the replacement will be issued later.

(1) TBD.
Subtask 52-31-17-300-011-A01
E. Replacement of Riveted Parts
(1) Replace the riveted parts in accordance with the standard riveting procedure.
Subtask 52-31-17-300-012-A01
F. Replacement of the Riveted Nuts
NOTE : The component parts with the riveted nuts are given in TABLE 7.
(1) Riveted Nut
IPL FIGURE COMPONENT ITEM NAME OF RIVETED NUT ITEM
COMPONENT
25 20 Casing 50
Riveted Nut
TABLE 7
(2) Drill out the rivets and remove the damaged riveted nut from the component part.
Subtask 52-31-17-300-013-A01
G. Replacement of Threaded Inserts
NOTE : The component parts with the threaded inserts are given in TABLE 8.
(1) Threaded Inserts
IPL FIGURE COMPONENT ITEM NAME OF INSERT ITEM
COMPONENT
1 --- Access Cover 120
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COMPONENT
9 --- Hand Lever Assembly 200
Threaded Inserts
TABLE 8
(2) Replace the threaded inserts in accordance with PMS 01-05-04.
Subtask 52-31-17-300-014-A01
H. Replacement of the HELI-COIL Threaded Inserts
NOTE : The component parts with the HELI-COIL threaded inserts are given in TABLE 9.
(1) HELI-COIL Threaded Inserts
IPL FIGURE COMPONENT ITEM NAME OF HELI-COIL INSERTS
COMPONENT ITEM
01 30 Structure Assy 35
21 230 Actuator Arm 290
21 360 Arm 410
HELI-COIL Threaded Inserts
TABLE 9
(2) Replace the HELI-COIL threaded inserts in accordance with PMS 01-05-45.
NOTE : Do the replacement with a HELI-COIL tool set.
NOTE : Remove the fractured parts of threaded inserts separately.
Subtask 52-31-17-300-015-A01
J. Replacement of the Lubrication Fittings
NOTE : The component parts with the lubrication fittings are given in TABLE 10.
(1) Lubrication Fittings
IPL FIGURE COMPONENT ITEM NAME OF LUBRICATION
COMPONENT FITTINGS ITEM
8 250 Shaft 350
33,34 20 Locking Hook 30
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IPL FIGURE COMPONENT ITEM NAME OF LUBRICATION

COMPONENT FITTINGS ITEM
33,34 170 Bellcrank 200
Lubrication Fittings
TABLE 10
(2) Remove the damaged or worn lubrication fitting from the component.

(3) Clean the component bore and remove the grease with Material No. 11-003 Methyl-Ethyl-
Ketone.
WARNING : BE CAREFUL WHEN YOU USE MATERIAL NO. 08-007 SEALANT, HIGH
TEMPERATURE. OBEY THE MATERIAL MANUFACTURER’S
INSTRUCTIONS.
(4) Apply Material No. 08-007 Sealant, High Temperature to the thread of the lubrication
fitting.
(5) Install the lubrication fitting to the component and tighten.
Subtask 52-31-17-300-016-A01
K. Replacement of the Bonded-in Insert
NOTE : The component part with the bonded-in insert is given in TABLE 11.
(1) Bonded-in Insert
COMPONENT
9 10 Hand Lever 90
Bonded-in Insert
TABLE 11
(2) Remove the damaged insert from the component part with an applicable tool.

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(3) Clean the component bore and the new insert with Material No. 11-003 Methyl-Ethyl-
Ketone.
NOTE : You must use a nonmetallic scraper to remove the remaining Material No.
08-050 Adhesive.
CAUTION : DO NOT TOUCH THE BONDING SURFACES. CONTAMINATION CAN

CAUSE AN UNSATISFACTORY BOND.
(4) Dry the component bore and the bush with dry, clean Material No. 19-003 Lint-Free
Cotton Cloth .
(5) Install the insert in accordance with PMS 01-05-27.
NOTE : You must install the insert with Material No. 08-050 Adhesive.

INSTRUCTIONS.
(6) Apply Material No. 16-021 Flexible Polyurethane to the gap between the insert and the
component part.
PRE MOD 32337K7963
(7) Replacement of Identification Plates
(a) For the replacement of the self-adhesive identification plate refer to the TABLE 12.
IPL FIG. ITEM COMPONENT PART IDENTIFICATION
NAME PLATE ITEM
1 FWD Cargo 70A
Compartment Door
Self-adhesive Identification Plate
TABLE 12
1 Write down the data of the old door identification plate.

2 Transfer the data from the old identification plate to the new door identification
plate.
3 Remove the damaged or loose identification plate with a nonmetallic scraper.
WARNING : BE CAREFUL WHEN YOU USE MATERIAL NO. 11-003 METHYL-

ETHYL-KETONE. OBEY THE MATERIAL MANUFACTURER’S
INSTRUCTIONS.
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4 Clean the bonding area with Material No. 11-003 Methyl-Ethyl-Ketone.
CAUTION : DO NOT TOUCH THE BONDING SURFACES.

5 Remove the protection foil from the new identification plate.
6 Align and attach the new identification plate on the cleaned bonding area.
POST MOD 32337K7963
(7) Replacement of Identification Plates
(a) For the replacement of the bonded identification plate refer to TABLE 13.
IPL FIG. ITEM COMPONENT PART IDENTIFICATION
NAME PLATE ITEM
1 FWD Cargo 70B
Compartment Door
Bonded Identification Plate
TABLE 13
1 Write down the data of the old door identification plate.

2 Transfer the data from the old identification plate to the new door identification
plate.
3 Remove the damaged or loose identification plate with a nonmetallic scraper.
WARNING : BE CAREFUL WHEN YOU USE MATERIAL NO. 11-003 METHYL-

ETHYL-KETONE. OBEY THE MATERIAL MANUFACTURER’S
INSTRUCTIONS.
4 Clean the bonding area with Material No. 11-003 Methyl-Ethyl-Ketone,
WARNING : BE CAREFUL WHEN YOU USE MATERIAL NO. 08-001 GENERAL

PURPOSE ADHESIVE HONEYCOMB FILLER. OBEY THE
CAUTION : DO NOT TOUCH THE BONDING SURFACES.

5 Apply Material No. 08-001 General Purpose Adhesive Honeycomb Filler in
accordance with the manufacturer’s instruction to the bonding surface.
6 Align and install the identification plate on the bonding surface.
7 Remove the unwanted bonding material from the edges of the identification
plate.
WARNING : BE CAREFUL WHEN YOU USE MATERIAL NO. 07-023

PROTECTIVE COATING, TRANSPARENT. OBEY THE MATERIAL
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8 Apply Material No. 07-023 Protective Coating, Transparent to the edges of the
identification plate in accordance with PMS 01-02-41.
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ASSEMBLY
**For PN’s ALL
TASK 52-31-17-400-801-A01
Installation of the Insulation and the Door Seal
1. General
A. The figure and the item numbers used in the IPL are given in this assembly topic. Before the
assembly and the installation of each component of the Cargo Door, CHECK and REPAIR
procedures must be done.
B. If you must do a full assembly, you must do the subsequent procedures.
C. If it is necessary to install only a sub-assembly, find the procedure in the applicable lists and
illustrations. If it is necessary to install or connect sub-assemblies or components before you
start to assemble or install a sub-assembly, you will find cross-references in the text.
D. If a paragraph refers to one illustration only, only the item number is given in the brackets. If a
paragraph refers to more than one illustration, the illustration number and the item number are
given in the brackets.
E. When there is no torque value specified, use a standard torque value.
TABLE 1
3. Procedure
Subtask 52-31-17-410-001-A01
A. Installation of the Insulation and the Door Seal

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(1) Install the insulation.
NOTE : Before you install the insulation, make sure that Material No. 15-005 Corrosion
Preventive Temporary Protective Compound is applied to the inner surfaces of
the cargo door structure.
(a) Install the insulation at the cargo door and connect the insulation with the stud
assemblies (2-80, 90).
(2) Install the door seal (150).
WARNING : IF THE DOOR SEAL IS NOT INSTALLED IN THE CORRECT POSITION,

THE CABIN PESSURE CAN DECREASE. THIS CAN RESULT IN A
DISRUPTION OF THE FLIGHT.
(a) If you have removed the door seal (150) during the DISASSEMBLY or REPAIR
procedure, install it correctly in its retainer on the cargo door structure.
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**For PN’s ALL
TASK 52-31-17-400-802-A01
Assembly and Installation of the Access Cover Assemblies
1. General
09-018 Corrosion Inhibitinglow Adhesion Sealant
11-010 Isopropyl Alcohol
08-616
TABLE 1
B. Referenced Information
PMS 01-02-36
PMS 01-05-47
TABLE 2
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3. Procedure
Subtask 52-31-17-410-002-A01
A. Assembly and Installation of the Access Cover Assemblies

(1) Assemble the access cover assembly (10).
(a) If you have removed a damaged sight glass (30) during the DISASSEMBLY
procedure, proceed as follows:

1 Apply Material No. 09-013 Corrosion Inhibiting Brush Consistency at the mating
surfaces of the sheet (20) and the sight glass (30) (Refer to PMS 01-02-36).

2 Apply Material No. 09-013 Corrosion Inhibiting Brush Consistency on the shaft
of the screws (40)
NOTE : Refer to PMS 01-05-47.

3 Install the screws (40), the sight glasses (30), the sheets (20) and the nuts (50)
on the access cover (15).

4 Apply Material No. 09-016 Corrosion Inhibiting Fillet Consistency on the space
between the sheets (20), the sight glasses (30) and the access cover (15).

5 Let Material No. 09-016 Corrosion Inhibiting Fillet Consistency dry.
(2) Install the access cover assembly (10).
(a) Instal l the access cover assembly (10) on the cargo door and connect the studs (60,
90, 100).
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(3) Install the access cover assembly (130) with the washers (170) and the screws (160, 180)
at the cargo door.
(a) If you have removed the self adhesive sealing (150) during the DISASSEMBLY
procedure, continue as follows:

ALCOHOL. OBEY THE MATERIAL MANUFACTURER’S
INSTRUCTIONS.
1 Clean the installation surface for the self adhesive sealing (150) on the access
cover (140) with Material No. 11-010 Isopropyl Alcohol.
2 Cut the sealing (150) to the length and remove the protection foil from the
sealing (150).
3 Install the sealing (150) to the cover (140) and glue the ends of the sealing
(150) together with Material No. 08-616 .
(4) Install the access cover (110).

INHIBITINGLOW ADHESION SEALANT. OBEY THE MATERIAL
(a) Apply Material No. 09-018 Corrosion Inhibitinglow Adhesion Sealant on the
installation surface of the access cover (110).

(b) Apply Material No. 09-013 Corrosion Inhibiting Brush Consistency on the shaft of the
screws (120).
(c) Install the access cover (110) with the screws (120) on the cargo door.
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**For PN’s ALL
TASK 52-31-17-400-803-A01
Installation of the Plugs and the Protective Plugs
1. General
TABLE 1
3. Procedure
Subtask 52-31-17-410-003-A01
A. Installation of the Plugs and the Protective Plugs

(1) Install the plugs (1-80).
NOTE : Attach a tag that tells people, to install the plugs (1-80) flush with the cargo
door skin after the final installation of the cargo door on the aircraft.
(2) Install the protective plugs (4-20, 30)
(a) Install the protective plugs (4-20, 30) in the cargo door.
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(b) Apply Material No. 09-016 Corrosion Inhibiting Fillet Consistency to the space
between the plugs (4-20, 30) and the cargo door.
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**For PN’s ALL
TASK 52-31-17-440-801-A01
Assembly of the Hand Lever Assembly
1. General
TABLE 1
3. Procedure
Subtask 52-31-17-440-001-A01
A. Assembly of the Hand Lever Assembly
(1) Apply Material No. 04-004 Synthetic Ester Based Grease High Pressure to the outer surface
of the spring sleeve (170) and the spring (110).
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(2) Apply Material No. 04-004 Synthetic Ester Based Grease High Pressure to the bearing bolt
(140).
(3) Install the bearing bolt (140) and the washers (130) at the handle flap (100).
(4) Safety the bearing bolt (140) with the cotter pins (120).
WARNING : YOU MUST INSTALL THE SPRING WITH LOAD.

(5) Install the spring (110), the spring sleeve (170), the handle flap (100), the bearing bolt
(160) and the washers (150) on the hand lever (10).
(6) Safety the bearing bolt (160) with the cotter pins (120).
(7) Install the sequence cams (20) with the bolts (190) and the washers (150) on the hand
lever (10).
(8) Tighten the bolts (190).
(9) Apply Material No. 04-004 Synthetic Ester Based Grease High Pressure to the shafts of the
bolts (40).
(10) Install the stop (30), the rollers (80), the bolts (40) and the washers (60).
(11) Safety the bolts (40) with the retaining rings (50).
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**For PN’s ALL
TASK 52-31-17-400-804-A01
Installation of the Hand Lever Mechanism
1. General
04-017 Silicone Grease
TABLE 1
TASK 52-31-17-800-801-A01 Adjustment of the Hand Lever Assembly
TABLE 2
3. Procedure
Subtask 52-31-17-410-004-A01
A. Installation of the Hand Lever Mechanism
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(1) Install the catching hook (490).

(a) Install the shim (480) as recorded during the DISASSEMBLY procedure.
(b) Install the catching hook (490) with the washers (120) and the bolts (500) at the
cargo door.
(c) Tighten the bolts (500).
(d) Adjust the catching hook (490) (Refer to TASK 52-31-17-800-801-A01).
(2) Assemble the control rods (160B, 600B) as follows (Refer to IPL_FIGURE_95):
(a) Install the nuts (30, 40) and the locking devices (50) on the rod ends (10A, 20A and
10B, 20B).
(b) Install the rod ends (10A, 20A and 10B, 20B) with the nuts (30, 40) and the locking
devices (50) on the rod body. Make sure that the length is the same as the length
recorded in the DISASSEMBLY procedure.
NOTE : Do not safety the nuts (30, 40) at this time. Attach a tag which say
persons to safety the nuts (30, 40) after the adjustment.
(3) Install the control rods (160, 600).
WARNING : BE CAREFUL WHEN YOU USE MATERIAL NO. 04-004 SYNTHETIC

ESTER BASED GREASE HIGH PRESSURE. OBEY THE MATERIAL
(a) Apply Material No. 04-004 Synthetic Ester Based Grease High Pressure to the shaft of
the bolts (200).
(b) Connect the fork-end of the control rod (600) at the latching shaft.
(c) Install the washer (210), the bolt (200), the washer (190) and the nuts (180) at the
control rod (600). Tighten the nuts (180).
(d) Connect the fork-end of the control rod (160) on the locking shaft.
(e) Install the washer (210), the bolt (200), the washer (190) and the nuts (180) on the
control rod (160). Tighten the nuts (180).
(f) Safety the nuts (180) with the cotter pins (170).
(4) Assemble the roller lever assembly (370).

(a) Apply Material No. 04-004 Synthetic Ester Based Grease High Pressure to the bore of
the roller (400) and the shaft of the bolt (430).
(b) Install the roller (400) with the bolt (430), the washer (420) and the nut (410) on the
roller lever (380).
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(c) Make sure that the roller (400) turns freely.

(5) Install the shaft (360).

(a) Apply Material No. 04-004 Synthetic Ester Based Grease High Pressure to the mating
surfaces of the shaft (360) and the bushes (390, 530).
(b) Install the shaft (360) on the door structure.
1 During the installation of the shaft (360) install the universal joint assembly
(510), the roller lever assembly (370) and the universal joint lock (240) on the
shaft (360).
NOTE : Make sure that the attachment holes are aligned.

(c) Install the bolt (230), the washer (220) and the nut (110) at the universal joint lock
(240).
(6) Install the compression spring (470).

the spring bolt (460).
WARNING : YOU MUST INSTALL THE COMPRESSION SPRING WITH LOAD.

(b) Install the compression spring (470) on the spring bolt (460).
(c) Install the spring bolt (460) with the compression spring (470) at the hole in the
cargo door structure.
(d) Push the spring bolt (460) down against the compression spring (470).
(e) Install the locally manufactured bush and a mounting nut (e.g. NAS 509-4) on the
thread of the spring bolt (460) to compensate the load of the compression spring
(470) for easy installation.
(f) Connect the spring bolt (460) with the bolt (450), the washer (120) and the nut
(110) on the roller lever assembly (370).
(g) Tighten the nut (110).
(h) Remove the locally manufactured bush and the mounting nut.
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(7) Assemble and install the lever assembly (20).

(a) Assemble the lever assembly (20).

1 Apply Material No. 04-004 Synthetic Ester Based Grease High Pressure to the
locating pins (50).
2 Put the actuating unit (40) in position on the fitting (30) and the lever (90).
3 Install the washers (80), the locating pins (50) and the washers (70).
4 Safety the locating pins (50) with the cotter pins (60).
(b) Install the lever assembly (20).

1 Apply Material No. 09-018 Corrosion Inhibitinglow Adhesion Sealant to the
mating surface of the fitting (30).

2 Apply Material No. 04-004 Synthetic Ester Based Grease High Pressure to the
inner diameter of the lever (90).
WARNING : YOU MUST INSTALL THE LEVER ASSEMBLY WITH LOAD.

3 Put the lever (90) in position on the shaft (360) and the fitting (30) on the
4 Make sure that the attachment holes in the lever (90) and in the shaft (360) are
aligned.
5 Attach the fitting (30) with the washers (120), the bolts (130), the washers
(120) and nuts (110) on the cargo door structure.
6 Install the bolt (230), the washer (220) and the nut (110) at the lever (90) and
the shaft (360).
(c) Carefully remove the mounting nut from the spring bolt (460).

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(d) Apply Material No. 04-004 Synthetic Ester Based Grease High Pressure to the shaft of
the bolts (200, 580) and to inner side of the fork-ends of the control rods (160, 600)
(e) Connect the control rod (600) with the washer (570), the bolt (580), the washer
(560) and the nut (550) on the universal joint latch (520).
(f) Tighten the nut (550) and safety with the cotter pin (540).
(g) Connect the control rod (160) with the washers (210), the bolts (200), the washers
(190) and the nuts (180) on the lever (90).
(h) Tighten the nuts (180) and safety with the cotter pins (170).
(8) Install the hand lever assembly (10).

(a) Apply Material No. 04-004 Synthetic Ester Based Grease High Pressure to the outer
surface of the shaft (250).
WARNING : BE CAREFUL WHEN YOU USE MATERIAL NO. 04-017 SILICONE

GREASE. OBEY THE MATERIAL MANUFACTURER’S INSTRUCTIONS.
(b) Apply Material No. 04-017 Silicone Grease to the hand lever contact surfaces of the
hand lever (10), the roller lever assembly (370) and the universal joint assembly (510).
(c) Install the shaft (250), the spacer washers (260, 270) (as recorded during
DISASSEMBLY) and the hand lever assembly (10) on the cargo door.
(d) Measure and if necessary adjust the clearance ”A” between the hand lever assembly
(10) and the door structure (Refer to TASK 52-31-17-800-801-A01).
(e) Put the lock washer (150) in position on the shaft (250).
(f) Tighten the bolts (140).
(g) Safety the bolts (140) with the lock washers (150).
(h) Make sure that the hand lever assembly (10) is flush with the cargo door skin.
NOTE : If the hand lever assembly (10) is not flush with the cargo door skin, refer
to TASK 52-31-17-800-801-A01.
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**For PN’s ALL
TASK 52-31-17-400-805-A01
Installation of the Latching Mechanism Assemblies
1. General
TABLE 1
TASK 52-31-17-800-802-A01 Adjustment of the Latching Mechanism
TASK 52-31-17-800-807-A01 Adjustment of the Proximity Switches
TABLE 2
3. Procedure
Subtask 52-31-17-410-005-A01
A. Installation of the Latching Mechanism Assemblies (20, 30)
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(1) Apply Material No. 04-004 Synthetic Ester Based Grease High Pressure to the mating
surfaces of the sleeves (210) and the bolts (160).
(2) Install the sleeves (210), the latching mechanism assemblies (20, 30), the washers (170),
the bolts (160), the washers (170) and the nuts (190) at the cargo door.
(3) Safety the nuts (190) with the cotter pins (180).
(4) Install the washers (140), the bolts (130), the washers (140) and the nuts (150).
surfaces of the sleeves (120) and the bolts (80).
(6) Install the sleeves (120), the washers (90) the bolts (80), the washers (70) and the nuts
(60).
surfaces of the bushes (250, 260) and the bolts (230, 280).
(9) Install the bushes (250, 260), the washers (240), the bolts (230, 280), the washers (240)
and the nuts (290).
(11) Make sure that the upper dead center of the latching mechanism is correctly adjusted
(Refer to TASK 52-31-17-800-802-A01).
(12) Make sure that the proximity switch 5MJ is correctly adjusted (Refer to TASK
52-31-17-800-807-A01).
(13) Make sure that the lower dead center of each latching mechanism is correctly adjusted
(Refer to TASK 52-31-17-800-802-A01).
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**For PN’s ALL
TASK 52-31-17-400-806-A01
Assembly of the Latching Hook Assemblies
1. General
TABLE 1
3. Procedure
Subtask 52-31-17-440-002-A01
A. Assembly of the Latching Hook Assemblies

(1) Assemble the bellcrank assemblies (160) and the linkage (70).

surfaces of the sleeves (60), the bushes (100, 110) and the bolts (150).
(b) Put the sleeves (60) in position on the bellcrank assemblies (160).
(c) Put the bushes (100, 110) in position on the upper fork-end of the linkage (70).
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(d) Put the bellcrank assemblies (160) in position on the linkage (70).
(e) Install the washers (90), the bolts (150), the washers (130) and the nuts (120).
(2) Connect the connecting rod (260).

surfaces of the bushes (230, 240) and the bolts (210).
(b) Install the bushes (230) on the bellcrank assemblies (160).
(c) Install the bushes (240) and move the eye-end of the connecting rods (260) on the
fork-end of the bellcrank assemblies (160).
(d) Install the washers (220), the bolts (210), the washers (220) and the nuts (250).
(e) Tighten the nuts (250).
(3) Install the latching hook assemblies (10).

surfaces of the sleeves (60), the bushes (100, 110) and the bolt (80).
(b) Install the sleeves (60) at the locking hook assemblies (10).
(c) Install the bushes (100, 110) on the fork-end of the linkage (70).
(d) Install the latching hook assemblies (10), the washers (90), the bolts (80), the
washers (130) and the nuts (120).
(e) Safety the nuts (120) with the cotter pins (140).
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**For PN’s ALL
TASK 52-31-17-400-807-A01
Assembly and Installation of the Latching Shaft Assembly
1. General
TASK 52-31-17-400-805-A01 Installation of the Latching Mechanism Assemblies
TASK 52-31-17-400-804-A01 Installation of the Hand Lever Mechanism
TABLE 1
3. Procedure
Subtask 52-31-17-400-001-A01
A. Assembly and Installation of the Latching Shaft Assembly

(1) Put the hinged lever assembly (70), the stop cam (100), the switch lever (110) and the
shaft levers (30) in position and install the latching shaft (10).
NOTE : You must install the shaft levers (30) as identified during the DISASSEMBLY
procedure.
(2) Install the taper pins (40, 130), the sleeves (50) and the nuts (60).
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(3) Connect the latching mechanism (Refer to TASK 52-31-17-400-805-A01) and the hand
lever mechanism (Refer to TASK 52-31-17-400-804-A01) on the latching shaft assembly.
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**For PN’s ALL
TASK 52-31-17-400-808-A01
Assembly and Installation of the Interlock Mechanism
1. General
TABLE 1
TASK 52-31-17-800-805-A01 Adjustment of the Interlock Mechanism
TABLE 2
3. Procedure
Subtask 52-31-17-400-002-A01
A. Assembly and Installation of the Interlock Mechanism
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(1) Assemble the interlock mechanism (90).

the pin (130) and the bore of the roller (140).
(b) Install the roller (140) and the pin (130) on the lever (100).
(c) Safety the pin (130) with the retaining ring (120).
(d) Install the adjusting screw (180) with the nut (190) and the lock plate (200) on the
lever (170).
NOTE : Do not safety the nut (190) with the lock plate (200) at this time. Attach a
tag to say that the nut (190) must be safetied with the lock plate (200)
during the final adjustment of the cargo door on the aircraft.

(e) Apply Material No. 04-004 Synthetic Ester Based Grease High Pressure to the shaft of
the pins (110) and to the inner side of the fork fittings of the levers (100, 170).
(f) Install the levers (100, 170) with the pins (110) on the connecting rod (150).
(g) Safety the pins (110) with the retaining rings (160).

(h) Apply Material No. 04-004 Synthetic Ester Based Grease High Pressure to the shaft of
the pin (110) and to the inner side of the fork-end of the bolt (210).
(i) Install the bolt (210) with the pin (110) at the lever (170).
(j) Safety the pin (110) with the retaining ring (160).
(2) Install the interlock mechanism (90).

the bolt (210) and to the shaft of the spring sleeve (20).
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(b) Apply Material No. 04-004 Synthetic Ester Based Grease High Pressure to the outer
diameters of the bushes (230, 270) and to the shaft of the pin (50).
(c) Install the pin (50) and the washer (70).
(d) Safety the pin (50) with the cotter pin (60).
(e) Install the bush (270) and the interlock mechanism (90) at the cargo door structure.
1 Install the washer (300), the bolt (260), the washer (300) and the nut (290).
2 Safety the nut (290) with the cotter pin (280).
(f) Install the bush (230) at the interlock mechanism (90).
1 Install the washer (220), the bolt (250) the washer (70) and the nut (240).
2 Safety the nut (240) with the cotter pin (60).
(g) Install the spring sleeve assembly (10) with the compression spring (40) on the bolt
(210).
WARNING : YOU MUST INSTALL THE COMPRESSION SPRING WITH LOAD.

(h) Compress the compression spring (40) and the spring sleeve assembly (10) to decrease
its length.
(i) Install the pins (50) and the spacers (80) on the spring sleeve assembly (10) and on
the cargo door structure.
(j) Install the washers (70) and safety the pins (50) with the cotter pins (60).
(3) Adjust the interlock mechanism (90) (Refer to TASK 52-31-17-800-805-A01).
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**For PN’s ALL
TASK 52-31-17-400-809-A01
Installation of the Locking Shaft Assembly
1. General
A. Referenced Information
TASK 52-31-17-800-803-A01 Adjustment of the Locking Mechanism
TASK 52-31-17-400-804-A01 Installation of the Hand Lever Mechanism
TASK 52-31-17-400-812-A01 Installation of the Vent Door Mechanism
TASK 52-31-17-400-811-A01 Assembly and Installation of the Drift Pin Rods
TABLE 1
3. Procedure
Subtask 52-31-17-410-006-A01
A. Installation of the Locking Shaft Assembly
NOTE : After the installation of the locking shaft assembly, you must connect the following
items to the locking shaft (10):
- the hand lever mechanism (Refer to TASK 52-31-17-400-804-A01),
- the vent door mechanism (Refer to TASK 52-31-17-400-812-A01) and
- the drift pin mechanism (Refer to TASK 52-31-17-400-811-A01)
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(1) Put the hinged lever assembly (60) and the locking cams (130) in position as recorded
during the DISASSEMBLY procedure.
(2) Put the lever assembly (90) and the lever (140) in position and install the locking shaft
(10).
(3) Install the threaded pins (120), the taper pins (20), the sleeves (50), the washers (40) and
the nuts (30).
(4) Adjust the locking shaft assembly (Refer to TASK 52-31-17-800-803-A01).
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**For PN’s ALL
TASK 52-31-17-400-810-A01
Assembly and Installation of the Sequence Shaft
1. General
2. Procedure
Subtask 52-31-17-400-003-A01
A. Assembly and Installation of the Sequence Shaft

(1) Assemble the beam-4 cover assembly (70).
(a) Put the beam-4 levers (110) and the spacer sleeve (140) in position and install the
beam-4 shaft (150) on the beam-4 cover (80).
(b) Install the taper pins (160), the sleeves (170) and the nuts (180).
(2) Install the beam-4 cover assembly (70).
(a) Install the washers (200), the bolts (190) and the beam-4 cover assembly (70) at the
(3) Install the control rods (10, 210).
(a) Install the control rods (10, 210) with the washers (30), the bolts (20), the washers
(40) and the nuts (50).
(b) Safety the nuts (50) with the cotter pins (60).
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**For PN’s ALL
TASK 52-31-17-400-811-A01
Assembly and Installation of the Drift Pin Rods
1. General
TABLE 1
TASK 52-31-17-800-804-A01 Adjustment of the Drift Pin Mechanism
TABLE 2
3. Procedure
Subtask 52-31-17-400-004-A01
A. Assembly and Installation of the Drift Pin Rods
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(1) Install the bellcrank assembly (90).

(a) Put the lever (130) and the bellcrank (100) in position and install the beam-3 shaft
(160) on the cargo door structure.
(b) Install the taper pins (170), the sleeves (180) and the nuts (190).
(2) Install the drift pins (10) and the rods (80).

surfaces of the bushes (40), the bolts (20) and the drift pins (10).
(b) Install the bushes (40) and the washers (60) on the drift pins (10).
(c) Install the drift pins (10) on the cargo door structure.
NOTE : Make sure that the flattened side of the drift pins (10) show at the outer
side of the cargo door.
(d) Install the rods (80) on the drift pins (10) with the bolts (20), the washers (60) and
the nuts (50).
(e) Safety the nuts (50) with the cotter pins (70).
(f) Connect the control rod (10) with the washer (210), the bolt (200), the washer (220)
and the nut (230) on the lever (130).
(3) Adjust the drift pin mechanism (Refer to TASK 52-31-17-800-804-A01).
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**For PN’s ALL
TASK 52-31-17-400-812-A01
Installation of the Vent Door Mechanism
1. General
TABLE 1
TASK 52-31-17-800-806-A01 Adjustment of the Skin Offset of the Vent Door assembly
TABLE 2
3. Procedure
Subtask 52-31-17-410-007-A01
A. Installation of the Vent Door Mechanism
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(1) Assemble the link assembly (260).

(a) Install the tab washers (280), the nuts (290, 310) and the forks (270, 320) on the rod
(300).
NOTE : Make sure that you can see the thread of the forks (270, 320) through the
inspection hole of the rod (300).
NOTE : Do not tighten and safety the nuts (290, 310) at this time. Attach a tag to
say persons to tighten and safety the nuts after the final adjustment.
(b) Install the lever assembly (380), the sleeve (340), the bolt (330), the washer (350)
and the nut (360).
(c) Safety the nut (360) with the cotter pin (370).
(2) Install the link assembly (260).

(a) Apply Material No. 04-004 Synthetic Ester Based Grease High Pressure to the outer
diameter of the fitting support (460).
(b) Install the link assembly (260) on the gearbox assembly (220) with the sleeve (430),
the bolt (420) the washer (200) and the nut (440).
(c) Safety the nut (440) with the cotter pin (450).
(d) Install the link assembly (260) at the fitting support (460) with the washer (70) and
the nut (90).
(e) Safety the nut (90) with the cotter pin (80).
(3) Install the connecting rod assembly (230).

the bolts (120).
(b) Install the connecting rod assembly (230), the washers (130), the bolts (120), the
washers (70) and the nuts (90).
(c) Safety the nuts (90) with the cotter pins (80).
(4) Install the actuating rod (110).

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the bolts (60, 120).
(b) Install the actuating rod (110) on the fork-ends of the gearbox assembly (220) and
the vent door assembly (50).
(c) Install the bush (100), the washers (70, 130), the bolts (60, 120), the washers (70)
and the nuts (90).
(d) Safety the nuts (90) with the cotter pins (80).
(5) Adjust the skin offset of the vent door installation (50) (Refer to TASK 52-31-17-800-806-
A01)
(6) Install the cover (10).

(a) Apply Material No. 09-016 Corrosion Inhibiting Fillet Consistency to the installation
brackets of the cover (10) at the cargo door structure.
(b) Install the cover (10), the screws (40), the washers (30) and the nuts (20).
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**For PN’s ALL
TASK 52-31-17-400-813-A01
Assembly and Installation of the Vent Door Assembly
1. General
TABLE 1
TASK 52-31-17-800-806-A01 Adjustment of the Skin Offset of the Vent Door assembly
TABLE 2
3. Procedure
Subtask 52-31-17-400-005-A01
A. Assembly and Installation of the Vent Door Assembly
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(1) Assemble the vent door assembly (100).

(a) Install the nuts (280, 400) and the tab washers (270, 390) on the screws (260, 380).
(b) Install the screws (260, 380) with the nuts (280, 400) and the tab washers (270, 390)
on the actuator arm assembly (220) and the arm assembly (350).
NOTE : Do not tighten and safety the nuts (280, 400) at this time. Attach a tag to
say persons must tighten and safety the nuts (280, 400) after the
adjustment of the vent door assembly (Refer to TASK 52-31-17-800-806-
A01).
(c) Install the spring bolts (150) and the bushes (320, 420).
(d) Install the washers (120) at the spring bolts (150) and safety with the cotter pins
(160).
(2) Install the vent door assembly (100).

surfaces of the sleeves (60, 90), the bushes (240, 250, 370) and the shafts of the bolts
(70).
CAUTION : YOU MUST INSTALL THE SPRINGS WITH LOAD.

(b) Put the washers (30), the springs (50, 80), the sleeves (60, 90), the bolts (70) and
the vent door assembly (100) on the cargo door.
(c) Install and tighten the nuts (20).
(d) Safety the nuts (20) with the cotter pins (10).
(e) Install the actuating rod on the vent door assembly (100) (Refer to TASK
52-31-17-400-812-A01).
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**For PN’s ALL
TASK 52-31-17-400-814-A01
Assembly and Installation of the Gearbox Assembly
1. General
TABLE 1
TABLE 2
3. Procedure
Subtask 52-31-17-400-006-A01
A. Assembly and Installation of the Gearbox Assembly
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(1) Assemble the gearbox assembly (20-220).

(a) Apply Material No. 04-004 Synthetic Ester Based Grease High Pressure to the shaft
assembly (25-70), the axle assembly (25-210), the thrust washer (25-260), the bevel
gears (25-90, 230) and the pins (25-100, 240).
(b) Install the axle assembly (25-200) as follows:
NOTE : Observe the marks on the axle assembly (25-210).

1 Install the axle (25-220) in the housing assembly (25-10).
2 Install the thrust washer (25-260) at the axle (25-220).
3 Install the bevel gear (25-230) at the axle (25-220).
4 Install the pin (25-240) at the bevel gear (25-230) and the axle (25-220).
5 Safety the pin (2-240) with the retaining ring (5-250)
6 Make sure that you can move the axle assembly (25-200) easy.
(c) Install the shaft assembly (25-70) at the housing assembly (25-70).
NOTE : Make sure that the marks on the bevel gears (25-90, 230) align.
(d) Install the shim (25-170) as recorded during the DISASSEMBLY procedure on the
housing assembly (25-10).
(e) Put the cover assembly (25-180) with the bolts (340) and the washers (25-270) on
the housing assembly (25-10).
(f) Install and tighten the nuts (25-50).
(g) Make sure that the gear moves freely.
(h) If the gear does not move freely, remove the nuts (25-50), the washers (25-270), the
bolts (25-340) and the cover assembly (25-180).
(i) Adjust the movement of the gear with the shims (25-170).
(j) Do steps (b) thru (g) again.
(2) Install the gearbox assembly (20-220).
NOTE : Make sure that the link assembly (20-260), the actuating rod (20-110) and the
connecting rod assembly (20-230) will be connected on the levers (25-320, 120,
300) (Refer to TASK 52-31-17-400-812-A01) after the installation of the gearbox
assembly (20-220).
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(a) Apply Material No. 09-018 Corrosion Inhibitinglow Adhesion Sealant to the mating
surfaces of the shim (20-210).
(b) Install the shim (20-210) as recorded during the DISASSEMBLY procedure on the
gearbox assembly (20-220).
(c) Install the gearbox assembly (20-220) with the shim (20-210) on the cargo door
structure.
(d) Install the washers (20-200) and the bolts (20-190).
(e) Make sure that the gear of the gearbox assembly (20-220) moves freely and easily.

(f) Apply Material No. 09-018 Corrosion Inhibitinglow Adhesion Sealant to the mating
surfaces of the washers (20-170) and the bearing flange (20-140).
(g) Install the bearing flange (20-140), the washers (20-170), the bolts (20-160), the
washers (20-170) and the nuts (20-180).

(h) Apply Material No. 04-004 Synthetic Ester Based Grease High Pressure to the shaft of
the axle (25-80) and the shaft of the taper pin (25-140).
(i) Install the lever (25-120), the taper pin (25-140), the sleeve (25-150) and the nut
(25-160).
(j) Install the protective plug (25-130) on the lever (25-120).

(k) Apply Material No. 04-004 Synthetic Ester Based Grease High Pressure to the mating
surfaces of the lever (25-320).
(l) Install the lever (25-320) with the lever (25-300) and the locking cam (25-310) on the
axle (25-220).
(m) Install the taper pins (25-290), the sleeves (25-280), the washers (25-270) and the
nuts (25-160).
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**For PN’s ALL
TASK 52-31-17-400-815-A01
Installation of the Door Proximity Sensors
1. General
TASK 52-31-17-800-807-A01 Adjustment of the Proximity Switches
TABLE 1
3. Procedure
Subtask 52-31-17-410-008-A01
A. Installation of the Door Proximity Sensors
NOTE : Refer to IPL_FIGURE_09, IPL_FIGURE_20, IPL_FIGURE_32 and IPL_FIGURE_62.

(1) Install the targets (62-20).
(a) Install the targets (62-20), the screws (62-30, 40) the washers (62-50) and the nuts
(62-60) on:
- the lever assembly (20-380) of the vent door mechanism.
- the hand lever (9-10) and
- the lever (32-80) of the latching shaft assembly.
(2) Install the Proximity Switch 5MJ (62-10).
(a) Remove the blanking caps from the electrical connectors.
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(b) Install the proximity switch 5MJ (62-10), the washers (62-50) and the screws (62-40)
on the cargo door structure.
(c) Adjust the proximity switch 5MJ (62-10) (Refer to TASK 52-31-17-800-807-A01).
(3) Install the proximity switch 28WV (62-10).
(a) Remove the blanking caps from the electrical connectors.
(b) Install the proximity switch 28WV (62-10), the washers (62-50) and the screws
(62-40) on the cargo door structure.
(c) Adjust the proximity switch 28WV (62-10) (Refer to TASK 52-31-17-800-807-A01).
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**For PN’s ALL
TASK 52-31-17-400-816-A01
Installation of the Cargo Door Drainage
1. General
09-005 Corrosion Inhibitive Interfay Sealant
TABLE 1
3. Procedure
Subtask 52-31-17-410-009-A01
A. Installation of the Cargo Door Drainage

(1) Install the tube assembly (80).

INHIBITIVE INTERFAY SEALANT. OBEY THE MATERIAL
(a) Apply Material No. 09-005 Corrosion Inhibitive Interfay Sealant to the mating surfaces
of the retainer (20) and the flange (70).
(b) Install the retainer (20), the basic valve (30) and the tube assembly (80) with the
flange (70).
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(c) Install the washers (50), the screws (40) and the nuts (60).
(2) Install the hose (10).
(a) Install the mounts (100) with the washers (120), the bolts (110) and the nuts (130)
on the cargo door structure.
(b) Move the lower end of the hose (10) through the holes in the cargo door structure.
(c) Install the hose (10) on the tube assembly (80).
(d) Fasten the hose (10) on the tube assembly (80) and on the mount (100) with the
cable ties (90).
(e) Make sure that the cable ties (90) do not compress the diameter of the hose (10).
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**For PN’s ALL
TASK 52-31-17-400-817-A01
Installation of the Hinge Assemblies
1. General
16-021 Flexible Polyurethane
TABLE 1
TABLE 2
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3. Procedure
Subtask 52-31-17-410-010-A01
A. Installation of the Hinge Assemblies

(1) Install the fittings (90-10, 91-60).

(a) Apply Material No. 09-013 Corrosion Inhibiting Brush Consistency to the mating
surfaces of the shims (90-20, 91-50).
(b) Install the shims (90-20, 91-50), the fittings (90-10, 91-60), the screws (70, 100), the
washers (80, 110) and the nuts (90).

(c) Apply Material No. 09-016 Corrosion Inhibiting Fillet Consistency to the space
between:
- the door structure
- the hinge assemblies (90-30, 91-20) and
- the fittings (90-10, 91-60).

(d) Let Material No. 09-016 Corrosion Inhibiting Fillet Consistency dry.

INSTRUCTIONS.

(e) Apply Material No. 16-021 Flexible Polyurethane to Material No. 09-016 Corrosion

INSTRUCTIONS.
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(f) Let Material No. 16-021 Flexible Polyurethane dry.

(g) Install the hinge assemblies (90-30, 60), (91-10, 20).
NOTE : For the replacement of the hinge assemblies (90-30, 60), (91-10, 20) refer
to TASK 52-31-17-300-803-A01, TASK 52-31-17-300-802-A01, TASK
52-31-17-300-801-A01.
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**For PN’s ALL
TASK 52-31-17-800-801-A01
Adjustment of the Hand Lever Assembly
1. General
FIGURE 52-31-17-991-014-A FIGURE 52-31-17-991-014-A-Adjustment of the Hand Lever Assembly
TABLE 1
3. Procedure
Subtask 52-31-17-820-001-A01
A. Adjustment of the Hand Lever Assembly
NOTE : Refer to IPL_FIGURE_08 and IPL_FIGURE_09 and FIGURE 52-31-17-991-014-A
NOTE : The hand lever assembly (8-10) must be in the LOCKED position.
(1) Adjust the clearance ”A” (Refer to FIGURE 52-31-17-991-014-A).
(a) Check that the clearances ”A” have the same dimensions and are between 1.0 and 3.0
mm (0.0393 and 0.1181 in.), between the hand lever assembly (8-10) and the door
structure.
(b) If the clearances ”A” are not in the limits, change the positions and/or the quantity
of the spacer washers (8-260, 270 or 8-290 thru 340) to make the necessary
adjustment.
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(2) Adjust the clearance ”B” (flush clearance) between the hand lever assembly (8-10) and the
installed access cover (Refer to FIGURE 52-31-17-991-014-A).
(a) If the clearance ”B” is not correct, then do the subsequent steps:
1 Loosen the nut (8-110).
2 Adjust the clearance ”B” with the screw (8-440).
3 Tighten the nut (8-110).
(3) Adjust the catching hook (8-490) (Refer to FIGURE 52-31-17-991-014-A).
(a) Make sure that the bearing bolt (9-140) does not come into contact with the catching
hook (8-490).
(b) Make sure that the clearance ”C” between 0.3 and 0.7 mm (0.0118 and 0.0276 in.)
while the hand lever assembly (8-10) is flush with the door structure.
(c) If the clearance ”C” is not correct, then do the subsequent steps:
1 Remove the bolts (8-500), the washers (8-120), the catching hook (8-490) and
the shim (8-480).
2 Adjust the clearance with the shim (8-480).
3 Install the shim (8-480), the catching hook (8-490), the washers (8-120) and the
bolts (8-500).
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**For PN’s ALL
A
HAND LEVER
ASSY (8−10)
ACCESS COVER
"A"
"A" SPACER WASHER

(8−260, 270)
(8−290 THRU 340)
A B
B ADJUSTMENT OF
CLEARANCE "A"
D "C"
"C"
BEARING
BOLT
C
(9−140) D "B"
HAND LEVER
ASSY (8−10)
SHIM
(8−480) ADJUSTMENT OF
C HANDLE OFFSET "B"
CATCHING HOOK
(8−490) HAND LEVER
ASSY (8−10)
E
WASHER BEAM4
(8−120)
BOLT
(8−500) NUT
(8−110)
BOLT
(8−440)
DIMENSION IN mm (in.)
"A" 1.0 TO 3.0 (0.0393 TO 0.1181)
"B" 0.0 TO −1.0 (0.0000 TO −0.0394)
HAND LEVER
ASSY (8−10) "C" 0.3 TO 0.7 (0.0118 TO 0.0276)
F_CM_523117_1_0140101_01_00
Adjustment of the Hand Lever Assembly

FIGURE-52-31-17-991-014-A01
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**For PN’s ALL
TASK 52-31-17-800-802-A01
Adjustment of the Latching Mechanism
1. General
FIGURE 52-31-17-991-015-A FIGURE 52-31-17-991-015-A-Adjustment of the Latching Mechanism
TABLE 1
3. Procedure
Subtask 52-31-17-820-002-A01
A. Adjustment of the Latching Mechanism
NOTE : Refer to IPL_FIGURE_08, IPL_FIGURE_30, IPL_FIGURE_33, IPL_FIGURE_34,

IPL_FIGURE_40 and FIGURE 52-31-17-991-015-A
NOTE : Make sure tat the latching mechanism assemblies (30-20, 30) are in the LOCKED
position.
(1) Make sure that the hand lever assembly is flush with the door structure during the
adjustment procedure.
(2) Install the rigging pin (1) (PN TBD) through the rigging holes of the cargo door structure
and the bolt (30-230, 280) (upper dead center).
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(3) If you cannot install the rigging pin (1) (PN TBD) easily through the bolt (30-230, 280),
you must adjust the Length of the control rod (8-600) as follows:
(a) If necessary, cut and remove the lockwire from the safety devices.
(b) Loosen the two jam nuts.
(c) Turn the turnbuckle until you can install the rigging pin (1) (PN TBD) easily in the
bolt (30-230, 280).
(d) Tighten the jam nuts and safety them with lockwire to the safety devices.
(4) Adjust the length of the six connecting rods (33,34-260) as follows to make sure that the
lower over-centering is correct:
(a) If necessary, cut and remove the lockwire from the safety devices.
(c) Turn the turnbuckle until the back of the bellcrank assembly (33-160) touches the
bolt (30-130).
(d) Turn the turnbuckle back until you can move the rod easily.
(e) Make sure that you can install the rigging pin (2) (PN TBD) through the cargo door
structure and the bolt (33-150).
(f) If not, turn the turnbuckle until you can install the rigging pin (2) (PN TBD) easily.
(g) Tighten the jam nuts and safety them with lockwire at the safety devices.
(h) Make sure that you can turn the connecting rods (33,34-260).
(i) Remove the rigging pins (1,2) (PN TBD).
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**For PN’s ALL
A
EXAMPLE
LATCHING UNIT
JAM NUT
SAFETY DEVICE
CONTROL ROD
TURNBUCKLE
(8−600)
SAFETY DEVICE
JAM NUT
LATCHING SHAFT
RIGGING PIN
BOLT (30−230)
1 (1)
JAM NUT
SAFETY DEVICE CONNECTION
TURNBUCKLE ROD
(33, 34−260)
JAM NUT
SAFETY DEVICE
BOLT BELLCRANK ASSY
(30−130) (33, 34−160)
LOCKING SHAFT
BOLT (33, 34−150)
RIGGING PIN
(2)
1 THE RIGGING PIN (1) IS

ON FWD DOOR AT FR26A
F_CM_523117_1_0150101_01_00
Adjustment of the Latching Mechanism

FIGURE-52-31-17-991-015-A01
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**For PN’s ALL
TASK 52-31-17-800-803-A01
Adjustment of the Locking Mechanism
1. General
lockwire
TABLE 1
FIGURE 52-31-17-991-016-A FIGURE 52-31-17-991-016-A-Adjustment of the Locking Mechanism
TABLE 2
3. Procedure
Subtask 52-31-17-820-003-A01
A. Adjustment of the Locking Mechanism
NOTE : Refer to IPL_FIGURE_08, IPL_FIGURE_30, IPL_FIGURE_31, IPL_FIGURE_33 and

FIGURE 52-31-17-991-016-A.
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(1) Move the hand lever assembly away from the cargo door structure up to a position of 65
degree.
NOTE : Make sure that the latching hook assemblies (30-20, 30) remain in the latched
position.
(2) Measure the clearance between the locking cam (31-130) and the latching hook (33-20).
NOTE : The dimension of the clearance must be more than 2.0 mm (0.0787 in.).
(3) If the dimension is less than 2 mm (0.0787 in.) adjust the control rod (8-160) as follows:
(a) Cut, remove and discard the lockwire from the safety devices.
(c) Turn the turnbuckle until the dimension is correct.
(d) Tighten the jam nuts and safety them with lockwire to the locking devices.
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**For PN’s ALL
JAM NUT
LOCKING
DEVICE
TURNBUCKLE
LATCHING
SHAFT
CONTROL ROD
(8−160)
B
EXAMPLE
LOCKING CAM LOCKING

(31−130) SHAFT
TURNBUCKLE
LOCKING
DEVICE
JAM NUT
2.0mm
(0.0787 in.)
B
LATCHING
HOOK
(33, 34−20) LATCHING
MECHANISM ASSY
(30−20, 30)
F_CM_523117_1_0160101_01_00
Adjustment of the Locking Mechanism

FIGURE-52-31-17-991-016-A01
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**For PN’s ALL
TASK 52-31-17-800-804-A01
Adjustment of the Drift Pin Mechanism
1. General
lockwire
TABLE 1
FIGURE 52-31-17-991-017-A FIGURE 52-31-17-991-017-A-Adjustment of the Drift Pin Mechanism
TABLE 2
3. Procedure
Subtask 52-31-17-820-004-A01
A. Adjustment of the Drift Pin Mechanism
NOTE : Refer to IPL_FIGURE_13, IPL_FIGURE_40 and FIGURE 52-31-17-991-017-A.

(1) Make sure that the hand lever assembly is in the LOCKED position and in the recess of the
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(2) Install the rigging pin (3) (PN TBD) through the cargo door structure and the bellcrank
(13-100).
NOTE : This position gives an over-centering height of approx. 2.1 mm (0.083 in.) and
1.0 mm (0.0394 in.) on the bellcrank (13-100).
(3) If you cannot install the rigging pin (3) (PN TBD) easily into the bellcrank (13-100),
adjust the length of the control rod (40-10) as follows:
(c) Turn the turnbuckle until you can install the rigging pin (3) easily in the bellcrank
(13-100).
(d) Tighten the jam nuts and safety them with lockwire to the safety devices.
(4) Measure the distance ”Y” between the end of the extended drift pins (13-10) and the edge
members of the cargo door.
NOTE : Make sure that the distance ”Y” is between 34.7 and 37.7 mm (1.3661 and
1.4843 in.).
(5) Move the hand lever assembly to the UNLOCKED position.
(6) Make sure that the retracted drift pins are behind the skin edge of the cargo door.
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**For PN’s ALL
DEAD CENTER HEIGHT

A B 1.0mm (0.039 in.) ON
EXTENDED DRIFT PIN (13−10)
DEAD CENTER HEIGHT

2.1mm (0.083 in.) ON
EXTENDED DRIFT PIN (13−10)
A
BELLCRANK
B (13−100)
C
RIGGING PIN (3)
B
CONTROL ROD
EXAMPLE (40−10)
DRIFT PIN
(13−10)
D C
JAM NUT
SAFETY
CONTROL ROD DEVICE
D (40−10)
TURN
BUCKLE
SECTION
EXTENDED
D−D
"Y"
IN RETRACTED CONDITION
THE DRIFT PIN MUST BE
BEHIND THE SKIN EDGE
"Z" SKIN EDGE DIMENSION IN mm (in.)

"Y" 34.7 TO 37.7 (1.3661 TO 1.4843)
"Z" 5.0 (0.1969)
F_CM_523117_1_0170101_01_00
Adjustment of the Drift Pin Mechanism

FIGURE-52-31-17-991-017-A01
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**For PN’s ALL
TASK 52-31-17-800-805-A01
Adjustment of the Interlock Mechanism
1. General
FIGURE 52-31-17-991-018-A FIGURE 52-31-17-991-018-A-Adjustment of the Interlock Mechanism
TABLE 1
3. Procedure
Subtask 52-31-17-820-005-A01
A. Adjustment of the Interlock Mechanism

(1) Make sure that the hand lever assembly is in the UNLOCKED position.
(2) Measure the clearance ”Z” between the adjusting screw (44-180) and the stop cam
(32-100) of the latching shaft (32-10).
NOTE : The clearance ”Z” must be between 1.0 and 1.4 mm (0.0394 and 0.0551 in.).
(3) If the clearance ”Z” is not in the limits, adjust the clearance ”Z” as follows:
(a) Bend and release the lock plate (44-200).
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(b) Loosen the nut (44-190), remove the adjusting screw (44-180) from the lever
(44-170).
(c) Install a new lock plate (44-200) with the adjusting screw (44-180) and the nut
(44-190) on the lever (44-170).
(d) Adjust the adjusting screw (44-180) until the clearance ”Z” is correct.
(e) Tighten the nut (44-190) and safety it with the new lock plate (44-200).
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**For PN’s ALL
A
LATCHING SHAFT
(32−10)
STOP CAM
(32−100)
A
1.0 TO 1.4mm
(0.0394 TO 0.0551 in.)
B
ADJUSTING SCREW
(44−180)
ADJUSTING SCREW
(44−180)
NUT (44−190)
LOCK PLATE
(44−200)
LEVER (44−170)
F_CM_523117_1_0180101_01_00
Adjustment of the Interlock Mechanism

FIGURE-52-31-17-991-018-A01
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**For PN’s ALL
TASK 52-31-17-800-806-A01
Adjustment of the Skin Offset of the Vent Door assembly
1. General
lockwire
TABLE 1
FIGURE 52-31-17-991-019-A FIGURE 52-31-17-991-019-A-Adjustment of the Vent Door Assembly
TABLE 2
3. Procedure
Subtask 52-31-17-820-006-A01
A. Adjustment of the Skin Offset of the Vent Door assembly

(1) Make sure that the hand lever assembly is in the LOCKED position and in the recess of the
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(2) Measure the skin offset ”A” between the external contour of the vent door assembly
(20-50) and the cargo door skin.
(3) Make sure that the skin offset ”A” is be between 0.5 and 1.5 mm (0.0197 and 0.0591 in.).
(4) If the skin offset is not correct, adjust the length of the actuating rod (20-110) as follows:
(b) Loosen the jam nuts to release the turnbuckle.
(c) Turn the turnbuckle until the skin offset is correctly adjusted.
(d) Tighten the jam nuts and safety them with lockwire at the safety devices.
(5) Measure the clearance ”B” between the bolts (21-260, 380) and the stop of the vent door
frame.
NOTE : Make sure that the clearance ”B” is between 0.2 and 0.6 mm (0.0079 and
0.0236 in.).
(6) If the clearance ”B” is not correct, adjust the clearance as follows:
(a) Pull the hand lever assembly out of the recess until it is in the position (65 degree) to
open the vent door assembly (20-100).
(b) Bend the tab washers (21-270, 390) to release the nuts (21-280, 400).
(c) Loosen the nuts (21-280, 400) to release the bolts (21-260, 380).
(d) Remove the screws (21-260, 380) with the nuts (21-280, 400) and tab washers
(21-270, 390) from the actuator arm (21-220) and the arm (21-350).
(e) Discard the tab washers (21-270, 390).
(f) Install the screws (21-260, 380) with the nuts (21-280, 400) and the new tab, washers
(21-270, 390) on the actuator arm (21-220) and the arm (21-350).
NOTE : Make sure that the tab washers (21-270, 390) are correctly installed on the
actuator arm (21-220) and the arm (21-350).
(g) Close the vent door assembly (20-100) as follows:
1 Push the roller lever of the interlock mechanism to the outer side of the cargo
door to release the latching shaft.
2 Move the hand lever assembly down to the LOCKED position and push it into
the recess of the cargo door structure.
(h) Adjust the screws (21-260, 380) until the clearance ”B” is between 0.2 and 0.6 mm
(0.0079 and 0.0236 in.).
(i) Tighten the nuts (21-280, 400) and safety them with the tab washers (21-270, 390).
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**For PN’s ALL
A
ARM
(21−350)
B
TAB WASHER
(21−390)
ACTUATING ROD
(20−110) SAFETY
NUT
(21−400) DEVICE
TURNBUCKLE
SAFETY
BOLT DEVICE
(21−380)
ARM
(21−220) JAM NUT
B
TAB WASHER
(21−270) JAM NUT
NUT
(21−280) B
EXAMPLE
CLEARANCE CHECK OF VENT DOOR STOP
BOLT AND SKIN OFFSET CHECK
(21−260)
BOLT (21−260, 380)
VENT DOOR ASSY (21−100)
"B"
STOP
DIMENSION IN mm (in.) "A"
"A" 0.5 TO 1.5 (0.0197 TO 0.0591)
"B" 0.2 TO 0.6 (0.0079 TO 0.0236)

CARGO DOOR CONTOUR VENT DOOR CONTOUR
F_CM_523117_1_0190101_01_00
Adjustment of the Vent Door Assembly

FIGURE-52-31-17-991-019-A01
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**For PN’s ALL
TASK 52-31-17-800-807-A01
Adjustment of the Proximity Switches
1. General
FIGURE 52-31-17-991-020-A FIGURE 52-31-17-991-020-A-Adjustment of the Proximity Switches
TABLE 1
3. Procedure
Subtask 52-31-17-820-007-A01
A. Adjustment of the Proximity Switches
NOTE : Refer to IPL_FIGURE_44, IPL_FIGURE_32, IPL_FIGURE_62 and FIGURE

52-31-17-991-020-A.
(1) Make sure that the hand lever assembly is in the UNLOCKED position.
(2) Adjust the proximity switch 5MJ (62-10) installed near the locking shaft as follows:
(a) Move the hand lever assembly until you get a clearance between 1.0 and 1.4 mm
(0.0394 and 0.0551 in.) between the adjusting screw (44-180) and the stop cam
(32-100).
(b) Measure the clearance between the target (62-20) and the proximity switch 5MJ
(62-10) installed on the cargo door structure.
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(c) Make sure that the clearance is between 1.60 and 2.00 mm (0.0630 and 0.0787 in.).
(d) If the clearance is not correct, adjust the target (62-20) until you get the correct
clearance.
(e) If the adjusting screw (44-180) touches the stop cam (32-100), adjust the clearance
between the proximity switch 5MJ (62-10) and the target (32-20) to a maximum of
3.0 mm (0.1811 in.).
(3) Adjust the proximity switch 28WV (62-10) installed near the hand lever assembly as
follows:
(a) Make sure that the hand lever assembly is in the LOCKED position.
(b) Measure the clearance between the proximity switch 28WV (62-10) and the target
(62-20) installed on the hand lever assembly
(c) The clearance must be between 1.60 and 2.00 mm (0.0630 and 0.0787 in.):
(d) If the clearance is not correct, adjust the target (62-20) until you get the correct
clearance.
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**For PN’s ALL
"A"
B
PROXIMITY SWITCH
A 28WV
(62−10)
HAND LEVER ASSY
TARGET
(62−20)
PROXIMITY SWITCH 5MJ
(62−10)
"B"
TARGET
(62−20)
STOP CAM
(32−100)
"C"
ADJUSTING SCREW
(44−180)
DIMENSION IN mm (in.)
"A" 1.6 TO 2.0 (0.0630 TO 0.0787)
"B" 1.6 TO 2.0 (0.0630 TO 0.0787)
"C" 1.0 TO 1.4 (0.0394 TO 0.0551)
F_CM_523117_1_0200101_01_00
Adjustment of the Proximity Switches

FIGURE-52-31-17-991-020-A01
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FITS AND CLEARANCES
**For PN’s ALL
TASK 52-31-17-820-806-A01
Fits and Clearances
1. General
A. How to use the Fits and Clearances Table (See TABLE 1)
(1) A NOTE above the table gives the reference to the related CMM figure.
(2) Column 1 gives the location number (LOC NO.) of the part.
(3) Column 2 gives links to the IPL figure item numbers of the mating parts.
(4) Column 3 gives the dimensions and the assembly clearances of the original manufacturer
(MFR) limits.
(5) Column 4 gives the dimension limits and the maximum allowable clearance of the in-
service wear limits.
NOTE : It is necessary to replace the parts which are not in the limits (See
DISASSEMBLY, REPAIR and ASSEMBLY).
B. Sample of Fits and Clearances
NOTE : See FIGURE XXX

1 2 3 4
MFR LIMITS IN-SERVICE WEAR LIMITS
MATING MAX
IPL ASSEMBLY DIMENSION ALLOWABLE
LOC FIGURE DIMENSION CLEARANCE LIMITS CLEARANCES
NO. AND millimeters millimeters millimeters millimeters
ITEM NO. (inches) (inches) (inches) (inches)
MIN MAX MIN MAX MIN MAX
Sample
TABLE 1
2. Fits and Clearances
NOTE : Refer to FIGURE 52-31-17-991-021-A.
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MATING MAX
B1 OD 8-250 15.976 15.994 15.951
(0.6342) (0.6350) 0.006 0.042 (0.6279) 0.092
B2 ID 9-20 16.000 16.018 (0.0002) (0.0017) 16.043 (0.0036)
(0.6352) (0.6359) (0.6396)
C1 OD 8-360 19.972 19.993 19.941
(0.7863) (0.7871) 0.007 0.049 (0.7851) 0.111
C2 ID 8-390 20.000 20.021 (0.0003) (0.0019) 20.052 (0.0044)
(0.7874) (0.7882) (0.7894)
C1 OD 8-360 19.972 19.993 19.941
(0.7863) (0.7871) 0.007 0.049 (0.7851) 0.111
C3 ID 8-530 20.000 20.021 (0.0003) (0.0019) 20.052 (0.0044)
(0.7874) (0.7882) (0.7894)
Fits and Clearances
TABLE 2

MATING MAX
D1 OD 30-210 13.976 13.994 13.941
(0.5502) (0.5155) 0.006 0.042 (0.5489) 0.102
D2 ID 33,34 14.000 14.018 (0.0002) (0.0017) 14.043 (0.0040)
-180 (0.5512) (0.5519) (0.5529)
E1 OD 30-120 22.959 22.980 22.928
(0.8685) (0.8693) 0.020 0.062 (0.9027) 0.124
E2 ID 33,34 23.000 23.021 (0.0009) (0.0024) 23.052 (0.0049)
-40 (0.9055) (0.9063) (0.9076)
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MATING MAX
F1 OD 33-60 12.994 12.983 12.967
(0.5116) (0.5094) 0.017 0.024 (0.5105) 0.076
F2 ID 33-190 13.000 13.018 (0.0007) (0.0009) 13.043 (0.0030)
(0.5118) (0.5125) (0.5135)
G1 OD 33-60 12.994 12.983 12.967
(0.4761) (0.4757) 0.017 0.024 (0.5105) 0.076
G2 ID 33-50 13.000 13.018 (0.0007) (0.0009) 13.043 (0.0030)
(0.5118) (0.5125) (0.5135)
Fits and Clearances
TABLE 3

MATING MAX
B1 OD 40-150 19.980 19.993 19.960
(0.7866) (0.7871) 0.007 0.041 (0.7858) 0.092
B1 ID 40-100 20.000 20.021 (0.0003) (0.0016) 20.052 (0.0036)
(0.7874) (0.7882) (0.7894)
Fits and Clearances
TABLE 4
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MATING MAX
C1 OD FUSELG 10.857 10.900 10.400
HINGE (0.4274) (0.4291) (0.4094)
BOLT
0.300 0.860 1..100
C2 ID 90- 11.200 11.243
(0.0118) (0.0339)
11.500
(0.0433)
50, 64 (0.4409) (0.4426) (0.4528)
91-
14,40
D1 OD FUSELG 10.857 10.900 10.400
HINGE (0.4274) (0.4291) (0.4094)
0.300 0.860 1..100
BOLT
(0.0118) (0.0339) (0.0433)
D2 ID 90-66 11.200 10.900 11.500
91-16 (0.4409) (0.4426) (0.4528)
Fits and Clearances
TABLE 5
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**For PN’s ALL
A
A
B
C
B
SECTION
B2 B−B
B2
B1
SECTION
C−C
C1
C2 C3
F_CM_523117_1_0210101_01_00
Hand Lever Mechanism

FIGURE-52-31-17-991-021-A01
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**For PN’s ALL
A B
BOLD OF SECTION E−E
INSTALLED
IN OPPOSITE
DIRECTION
A
D
B
B
B F2 C
G2
E
SECTION D
F−F
G−G F1
G1
SECTION
E−E
C F
G
F
SECTION
E1 E2 D1 D2
D−D G
F_CM_523117_1_0220101_01_00
Latching Hook Assy

FIGURE-52-31-17-991-022-A01
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**For PN’s ALL
A
B
SECTION
B2
B−B B2
B1
F_CM_523117_1_0230101_01_00
Sequence Shaft
FIGURE-52-31-17-991-023-A01
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**For PN’s ALL
A
B
B
A
D
D
B
C
SECTION D2
C
D1
D−D
SECTION C2
C−C C1
F_CM_523117_1_0240101_01_00
Door Hinge
FIGURE-52-31-17-991-024-A01
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**For PN’s ALL
TASK 52-31-17-940-807-A01
Special Tool
1. Special Tools (See TABLE 1).
SUPPLIERS CODE
PART No. DESCRIPTION OR NAME AND WHERE USED TID
ADDRESS
355M03213000 Cable Loom TASK
52-31-17-700-801-
A01
355M03214000 Extension Cable Loom TASK
52-31-17-700-801-
A01
Special Tools, Fixtures and Equipment
TABLE 1
2. For the Tool set for the replacement of the bushes of the hinge assembly seeFIGURE
52-31-17-991-025-A.
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**For PN’s ALL
BOLT NUT 1 BUSH BOLT NUT 2 BUSH
REMOVAL OF THE BUSHES INSTALLATION OF THE BUSHES
THREAD
SECTION M8x1 DIA. X
A−A A
DIA. Y
AF 6.0
(0.236) A 3.0
(0.12)
40.0
15.0
(1.57)
(0.59)
25.0
(0.98)
65.0
(2.56)
110.0
(4.33)
NUT 1 NUT 2
THREAD THREAD
M8x1 M8x1
AF 17.0 AF 17.0
(0.67) (0.67)
5.0
15.0
(0.20)
(0.60)
15.0 DIA. Z
(0.60)
NOTE: DIMENSIONS IN MILLIMETERS (INCHES)
INNER DIA. OF BUSHES BOLT−DIA. X BOLT−DIA. Y NUT 2−DIA. Z

11.200 TO 11.243 11.0 TO 11.1 13.0 TO 13.1 13.0 TO 13.1
(0.4409 TO 0.4426) (0.397 TO 0.437) (0.476 TO 0.516) (0.476 TO 0.516)
F_CM_523117_1_0250101_01_00
Tool Set for the Replacement of the Bushes of the Hinge Assemblies
FIGURE-52-31-17-991-025-A01
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**For PN’s ALL
TASK 52-31-17-550-801-A01
Storage after Assembly
1. Reason for the Job
A. Self Explanatory
TASK 52-31-17-870-802-A01 General
TASK 52-31-17-870-803-A01 Description
TASK 52-31-17-870-804-A01 Operation
TABLE 1
3. Procedure
Subtask 52-31-17-620-001-A01
A. Preservation
(1) Make sure that you do the preservation procedure before you put the component in its
packing. The preservation procedure is given in the MIL-P-116 and/or MIL-P-25690A
Specification.
Subtask 52-31-17-530-002-A01
B. Packing
(1) Put the component in its initial container. Use the initial material for the protection of the
component.
(2) If the initial container is not available:
(a) Refer to TASK 52-31-17-870-802-A01, TASK 52-31-17-870-803-A01, TASK
52-31-17-870-804-A01 for the dimensions and weight of the component.
(b) Refer to ATA Specification 300. Use only approved materials for the protection of the
component.
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Subtask 52-31-17-550-003-A01
C. Identification Label
(1) Put the identification labels on the component and on the outside of the container. Make
sure that you can read the labels easily.
(2) The identification label must have all the related data of the component.
(3) The component is not approved for installation if there is no identification label attached to
it.
Subtask 52-31-17-550-004-A01
D. Storage
CAUTION : DO NOT KEEP THE CONTAINER NEAR FLUIDS THAT CAN CAUSE
CORROSION OR DAMAGE AND DO NOT KEEP IT NEAR SOURCES THAT
MAKE OZONE OR HEAT.
CAUTION : MAKE SURE THAT THERE IS NOT TOO MUCH WEIGHT ON THE
CONTAINER IF YOU USE THE STACK STORAGE METHOD. TOO MUCH
WEIGHT ON THE CONTAINER CAN CAUSE DAMAGE TO THE
COMPONENT.
(1) Keep the container in a clean, dry room with a good supply of air.
CAUTION : DO NOT KEEP THE COMPONENTS WITH RUBBER PARTS AT MORE

THAN + 20 DEG.C (+ 68 DEG.F).
(2) If components do not have rubber parts, keep the temperature of the room to between +18
and +28 deg. C (+64 and +82 deg. F). We recommend +18 deg. C (+64 deg. F).
(3) Keep the relative humidity to between 25 and 65 %.
(4) Put the containers where you can clearly read the identification label.
(5) Examine the condition and function of the component at specified times.
Subtask 52-31-17-550-005-A01
E. Condition Check and Functional Test
(1) Examine the condition and function of the component at specified times.
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INTRODUCTION
**For PN’s ALL
TASK 52-31-17-872-801-A01
Introduction Illustrated Parts List (IPL)
1. General
A. The procedure recommended for finding a part number, or details of a part are in paragraph 2
of this introduction.
B. The IPL contains:
- illustrations that show an exploded view of the parts,
- the related detailed Parts Lists.
C. The IPL is used to identify, to get, keep and issue replacement aircraft parts and units.
D. AIRBUS S.A.S. has no responsibility for parts and/or units deleted or revised as a result if
airline initiated modifications are included.
E. Part numbers shown in this document are written to Air Transport Association of America
(ATA) Specification ISPEC 2200.
F. Illustrations are applicable to more than one customer.
G. In the Detailed Parts List, each figure has its own page numbering system that starts at zero.
2. How to use the IPL
A. To find a Part Number (P/N) in a Figure or Illustration you can either:
- Enter the PN in the SEARCH tool within the AirN@v / Workshop. This will show you the
Figure or Figures where this appears. Click on your chosen Fig/Item number to go open the
Figure.
- Or refer to the Alph/Numeric Parts List and find the PN. In the Fig/Item column it will
show you all the figures where this PN exists, and the Item number. Click one of these to
open the Figure.
3. Plan of the IPL
A. Indenture System of the Detailed Parts List
(1) The indenture system shows how parts and assemblies relate to their next higher
assemblies (NHA) as follows:
1234567
Assembly
Attaching parts for assembly
.Detail parts for assembly
.Sub-assembly
..Detailed parts for sub-assembly
..Sub-sub-assembly
IPL INTRO
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...Detailed parts for sub-sub-assembly.

B. AIRBUS Part -- Numbering System
(1) The example that follows shows the identification of a part/assembly:
Basic Part Number L 57 4 6 0200 000 00
DRAWING NUMBER PARTS LIST DATA
AIRBUS Part -- Numbering System
TABLE 1
(1) L Aircraft A = AIRBUS A310/A300/A300-600 Aircraft

D = AIRBUS A320 Aircraft
F = AIRBUS A340 Aircraft
L = AIRBUS A380 Aircraft
NOTE: Initial aircraft type the part assembly was first used
on.
(2) 57 ATA Chapter Design and Manufacturing requirements of the above
breakdown will not always be the same as those in the
ATA Specification and the IPL.
(3) 4 ATA Section Changes with the ATA Chapter.
(4) 6 Drawing Responsibility The Engineering Department that is responsible for the
Design.
(5) 0200 Drawing Number The Drawing number.
(6) 000 Part or Assembly Part/assembly number.
(7) 00 Technical Specification Manufacturing or spares requirements suffix.
AIRBUS Part -- Numbering System
TABLE 2
C. Suffixes
SUFFIXES DEFINITION REMARKS
00 and 40 to 49 Production Part to drawing
The same as the Production Part.
01 to 39 Production Part not to drawing
50 Spare Part to drawing Spare part is not the same as the
51 to 59 Spare Part not to drawing Production Part
60 to 89 Spare Part not to drawing and not Number for Product Support
storable Breakout, but not for Production
99 Spare Part to drawing and not
storable
90 to 94 Specific Part for Repair Kits
IPL INTRO
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SUFFIXES DEFINITION REMARKS

95 to 98 Specific Part for Service Bulletin Kits
Suffixes
TABLE 3
D. D. Detailed composition for an IPL

Column 1 Column 2 Column 3 Column 4 Column 5
FIG-ITEM PART NUMBER 1234567 NOMENTLATURE USAGE UNIT
FROM TO PER
ASSY
1 -- 1A L5217605100000 ARM ASSY-SUPPORT EFF//NHA RF
1 -- 2A L5217605100100 ARM ASSY-SUPPORT EFF//NHA RF
10A L5217605100100 .SUPPORT ASSY (LH) ) (V2D671) 1
SEE 52-10-50-02 FOR DET
20A L5217605500300 .SUPPORT ASSY (RH) (V2D671) 1
SEE 52-10-50-02 FOR DET
*** L5217605501100 .SUPPORT ASSY (V2D671) SPARE
30A L5217609020000 .SHEET-BONDING (V2D671) 2
40A ABS0114T3-1 .BOLT V2D671) 18
50A NAS1149C0363R .WASHER (V80205) 21
60A L9247100502400 .STRAP-BONDING (V2D671) 3
90A L5217608620000 .BRACKET-DOOR (V2D671) 1
100A ABS0114T5-25 .BOLT (V2D671) 1
110A L5217608720000 .WASHER-TOOTHED (V2D671) 2
120A NAS1149C0532R .WASHER (V80205) 1
130A NAS1291C5M .NUT (V80205) 1
OPT TO H42-5 (V15653)
OPT TO PLH55M (VF0224)
OPT TO VN300D054
(V92215)
140A L5217605600000 .BRACKET ASSY (V2D671) 2
*** L5217605600200 .BRACKET ASSY (V2D671) SPARE
145A L5217605620000 ..BRACKET (V2D671) EFF/NHA 1
IPL INTRO
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Column 1 Column 2 Column 3 Column 4 Column 5

USED WITH L5217605600000
*** L5217605620200 ..BRACKET (V2D671) SPARE
150A MS21209F4-15 ..INSERT (V96906) EFF/NHA 1
USED WITH L5217605600000
160A L5217607600000 .BUMPER ASSY (LH) (V2D671) 1
170A L5217607600100 .BUMPER ASSY (RH) (V2D671) 1
180A L5217607800000 ..BRACKET ASSY (LH) (V2D671) 1
190A L5217607800100 ..BRACKET ASSY (RH) (V2D671) 1
200A L5217607820000 ...BRACKET (LH) (V2D671) 1
210A L5217607820100 ...BRACKET (RH) (V2D671) 1
220A D5237111620400 ...BUSHING-SHOULDERED (V2D671) 1
230A L5217608000000 ..STOP ASSY (V2D671) 1
240A L5217608120000 ...STOP (V2D671) 1
250A L5217608220000 ...SUPPORT (V2D671) 1
260A ABS0114T5-15 ..BOLT (V2D671) 1
270A NAS1291C5M ..NUT (V80205) 1
OPT TO H42-5 (V15653)
OPT TO PLH55M (VF0224)
OPT TO VN300D054
(V92215)
Detailed composition for an IPL
TABLE 4
(1) Help for the IPL-Page example

Column 1 Figure Number The figure number refers to its
related illustration. Modifications and
system variants can cause a different
figure. It will be added with a
sequential alpha-suffix, e.g. modified
versions of Figure 1 would be Figure
1A then Figure 1B and so on.
Non-Illustrated Parts The dash before an item number
shows it is not illustrated.
Item Number Initially, only every tenth number is
used for item numbers so that other
items can be added later.
IPL INTRO
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Column 2 AIRBUS Part AIRBUS manufactured parts e. g.

L5217605600000
Standard Part A standard part such as AN, MS,
NAS ...., is not given a supplier code.
Column 3 See XX-XX-XX-XX for DET or NHA Identifies correctly:
- the location of the full breakdown
of a sub-assembly in the IPL
- the location of the NHA of the item
in the IPL.
Usage From To In the Usage From To field the
statement ”EFF//NHA” related to
an NHA. At the same time in the
Nomenclature Field under the
description of the Part A Statement
”Used With ***” will state the NHA
PNR.
Symmetrical Parts LH or RH identifies the left hand or
right hand position of the part. If a
part is only on one assembly, (LH
side) or (RH side) follows its name.
VENDOR CODE A supplier code is given to the parts
manufactured by firms other then
AIRBUS.
Non-Procurable Item (NP) Identifies an item that is not
supplied.
Column 4 Usage From To In the Usage From To field the
statement ”EFF//NHA” related to
an NHA. At the same time in the
Nomenclature Field under the
description of the Part A Statement
”Used With ***” will state the NHA
PNR.
Column 5 Quantity The number in the Units Per Assy
column shows the quantity of parts
used for each NHA or installation.
AR = as required
RF = reference (quantity shown in
the NHA figure).
Help for the IPL-Page example
TABLE 5
IPL INTRO
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E. Other Notes
(1) ORDER OVRLGTH MPN XXXXXXXXXX
- Identifies a part number with more than fifteen characters that cannot fit in the part
number column.
(2) SB XX-XXX
- Identifies the Service Bulletin (SB) which adds to or changes the Detailed Parts List.
When the SB number shown in the name column is related to an AIRWORTHINESS
DIRECTIVE (AD), the letters AD and its number are shown in parenthesis. Also they
will follow the SB number, for example: PRE SB XX XXX (AD XXXX), POST SB XX
XXX (AD XXXX), ADDED by SB XX XXX (AD XXXX), DELETED BY SB XX XXX
(AD XXX), etc.
(3) SEL FROM
- Identifies a group of alternative parts from which you can take the necessary ones.
(4) OVERSIZE/UNDERSIZE
- Identifies a part as oversize or undersize.
(5) OPT TO
- Identifies an optional part that is fully interchangeable with the initial part.
(6) ALT FROM PN XXXXXXXXXX
- Identifies an alternate part number (this is a part that is fully interchangeable with the
initial part after it has had a change(s)).
(7) BUY PN XXXXXXXXXX
- Identifies the replacement part for the part in the part number column.
(8) LM = LOCAL MANUFACTURE
- Identifies the part number of the basic material (e.g. for seals, hinge strips, extrusion
etc...) from which the part in the part number column is manufactured.
- Identifies the unit of measurement followed by the dimensions or quantity.
(9) SEE CMM OR ACMM
- Refer to the Component Maintenance Manual or Abbreviated Component Maintenance
Manual for the part listed in the Detailed Parts List.
(10) MADE FROM JXXXX, MADE BY VXXXXX, MM XXX
- Identifies a part that is made from bulk material e.g. seals extrusions etc. and, if
necessary, the unit of measurement and quantity.
(11) USED ON MPN
- Identifies the NHA for a part in the part number column. This is used when the NHA
is not clear from the Usage Code (almost the same assemblies with details that are not
the same but have a single breakdown).
IPL INTRO
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(12) VENDOR CODE

(a) These codes agree with the current issue of the Manufacturers Cataloging Handbook
H4/HB:
- Federal Supply Code for Manufacturing (FSCM) or Commercial and Government
Entity (CAGE) code (United States and Canada only).
- NATO Supply Code for Manufacturers (NSCM) codes (does not include United
States and Canada)
(b) The letter ’V’ comes before the vendors code. For suppliers with no official code,
AIRBUS has given a provisional code. These codes are identified in the supplier table
by the information ”DUMMY CODE”.
NOTE : Suppliers who manufacture parts for which AIRBUS S.A.S. has an exclusive
sale right are not given a vendor code.
- AIRBUS standard parts (Prefix DAN, NSA etc...) are given the supplier code of
the seller of the parts. If there is more than one seller, a dummy supplier code
VT0000 is assigned to the related P/N. In this case, the additional cross-
reference table gives, for each P/N the various supplier codes and their own P/N
if applicable.
NOTE : All relevant Supplier Codes are shown in the ’Vendors Name and Code
List’, which is a part of the IPL INTRO.
IPL INTRO
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VENDOR LIST
CODE NAME AND ADDRESS

V01673 AIRDROME PARTS CO/3251 AIRPORT WAY/CA 90801/1867/LONG BEACH/USA
V04348 LAWRENCE ENGINEERING AND SUPPLY INC/”500 SO/ FLOWER ST, POB
30”/CA-91503/BURBANK/USA
V04795 HONEYWELL INTERNATIONAL INC/DIV HARDWARE PRODUCT GROUP/875W
ELLIOT RD SUITE 106/AZ-85284/TEMPE/USA
V06329 ASC INTERNATIONAL INCORPORATED/1227 CORPORATE DR
WEST/TX-76005/ARLINGTON/USA
V06383 PANDUIT CORP/17301 RIDGELAND/IL 60477-3048/TINLEY PARK/USA
V06725 AIR INDUSTRIES CORP/12570 KNOTT ST/CA 92641-3932/GARDEN GROVE/USA
V08748 ELDEC CORPORATION/16700 13TH AVE WEST/WA 98046/LYNNWOOD/USA
V10630 ANILLO INDUSTRIES INC/2090 N GLASSELL/CA 92667/ORANGE/USA
V11815 TEXTRON INC/PO BOX 1224 E WARNER AVE/CA 92707-0157/USA
V13899 HYDRO FITTING MFG CORP/733 E EDNA PLACE/CA 91722-3246/PO BOX
1558/COVINA/USA
V14283 AMPHENOL AEROSPACE/7077 CONSOLIDATED WAY/CA 92121/SAN DIEGO/USA
V15653 KAYNAR TECHNOLOGIES INC/KAYNAR DIV/800 S STATE COLLEGE BLVD/CA
92631/FULLERTON/USA
V17140 AEROSPACE PRODUCTS COMPAGNY/123 N.PINE
STREET/IN-46206/INDIANAPOLIS/USA
V1ER65 3-V FASTENERS/1651 B.MARKET STREET/CA-91720/CORONA/USA
V1NVY1 THE MEXMIL COMPANY/2865 SOUTH PULLMAN STREET/92705/SANTA ANA/USA
V1V757 WESCO AIRCRAFT HARDWARE CORP/27727 AVE
SCOTT/91355/VALENCIA,CA/USA
V27238 BRISTOL INDUSTRIES/630 EAST LAMBERT ROAD/CA 92821-4119/USA
V29372 ALCOA GLOBAL FASTENERS INC/DBA ALCOA FASTENING SYSTEMS DIV TRIDAIR
PRODUCTS/3000 W LOMITA BLVD/CA 90505-5103/TORRANCE/USA
V32664 AEROMETALS INC/11362 MONIER PARK PL BLDG 3B/CA 95742/RANCHO
CORDOVA/USA
V42C51 MIDI PYRENNES PLASTIQUES/Z I ESCALQUENS/31320/CASTANET/FR
V49367 AMPHENOL CORP/AMPHENOL AEROSPACE,PYLE-NATIONAL CONNECTORS/40-60
DELAWARE AVE/13838/SIDNEY,NY/USA
V52828 REPUBLIC FASTENER MFG CORP/1300 RANCHO CONEJO BLVD/CA
91320-1405/NEWBURY PARK/USA
IPL INTRO
Page 8
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@AIRBUS
D5237300000000

V56563 ALATEC PRODUCTS INC/21123 NORDHOFF ST/CA
91311-2344/2344/CHATSWORTH/USA
V56878 SPS TECHNOLOGIES INC/AEROSPACE AND INDUSTRIAL PRODUCTS
DIV/HIGHLAND AVENUE/PA 19046-2299/JENKINTOWN/USA
V57336 STEWARD INDUSTRIES INC/5210 14TH AVENUE NW/WA
98107-3729/SEATTLE/USA
V57983 GREER INDUSTRIES INC/2659 GRAVEL STREET/TX 76117-0249/14249/FORT
WORTH/USA
V59730 THOMAS AND BETTS CORP/HWY 218 S/IA 52240/IOWA CITY/USA
V5N982 BURBANK AIRCRAFT SUPPLY INC/2525 W 190TH
ST/CA-90504-6002/TORRANCE/USA
V60119 THE MONADNOCK COMPANY/18301 E.ARENTH AVE/CA-91749/CITY OF
INDUSTRY/USA
V60516 WEST COAST AEROSPACE INC/220 WEST E
STREET/CA-90744/WILMINGTON/USA
V60996 AERO FASTENER INC/507 300 UNION ST/01085/WESTFIELD,MA/USA
V69289 ORKAL INDUSTRIES LLC/333 WESTBURY AVE/11514/CARLE PLACE,NY/USA
V6D833 D AND D BEAN CO/701 SEVENTH ST/80631/GREELEY,CO/USA
V70347 AMERICAN AVIATION/180 VARICK STREET/NY-10014/NEW YORK/USA
V71286 FAIRCHILD CORP/CAMLOC PRODUCTS DIV FAIRCHILD FASTENER GROUP/3012
W LOMITA BLVD/CA 90505/TORRANCE/USA
V72962 HARVARD INDUSTRIES INC/PO BOX 3 WERNER WAY SUITE 210/NJ 08833/USA
V73197 HI-SHEAR CORP/PO BOX 2600 SKYPARK DR/CA 90505/USA
V75237 KAYNAR TECHNOLOGIES INC/MICRODOT DIV/190 W CROWTHER AVE/CA
92670/PLACENTIA/USA
V80205 NATIONAL AEROSPACE STANDARDS/(STANDARDISATION OFFICE.REFER TO
OPT VENDORS)/1725 DE SALES N W/WA-20036/WASHINGTON/USA
V80539 SPS TECHNOLOGIES INC AEROSPACE INDUSTRIAL PROD/2701 S HARBOR
BLVD/CA 92702-1259/1259/SANTA ANA/USA
V81343 SOCIETY OF AUTOMOTIVE ENGINEERS INC/(STANDARDISATION OFFICE.REFER
TO OPT VENDORS)/400 COMMONWEALTH DR/PA
15096-0001/WARRENDALE/USA
V81349 MILITARY SPECIFICATIONS/(STANDARDISATION OFFICE.REFER TO OPT
VENDORS)
V81482 SIMMONDS PRECISION PRODUCTS INC/CO-OPERATIVE INDUSTRIES DIV/100
OAKDALE RD/NJ 07930/CHESTER/USA
IPL INTRO
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V83324 REXNORD INC ROSAN DIV/3130 W HARWARD STREET/CA 92799/25225/SANTA
ANA/USA
V84114 AMERICAN STEEL CO/103 PARK AVENUE/PA-16117/ELLWOOD CITY/USA
V88044 AERONAUTICAL STANDARDS GROUP,DEPT OF NAVY AND
AIR/FORCE(STANDARDISATION OFFICE.REFER TO OPT
VENDORS)/MA-89536/SILVER SPRINGS/USA
V8K160 UNIREX INC/9310 EAST 37TH SREET NORTH/KS-67226/WICHITA/USA
V8Z507 CALIFORNIA SCREW PRODUCTS CORP/14957 GWENCHRIS
AVENUE/CA-90723/PARAMOUNT/USA
V91345 MILLER DIAL CORP/4400 N TEMPLE CITY BLVD/CA 91734/EL MONTE/USA
V92215 FAIRCHILD FASTENERSS INC/PO BOX 3000 W LOMITA BLVD/CA 90505-5103/USA
V92595 AUTOMATIC SCREW MACHINE/709 2ND AVENUE S.E/AL-35602/DECATURE/USA
V94931 BENDIX INTERNATIONAL/1633 BROADWAY/NY-10019/NEW YORK/USA
V952D1 SOURIAU-CLUSES/Z.I. DES GRANDS PRES/74301/CLUSES CEDEX/F
V96906 MILITARY STANDARDS PROMULGATED/(STANDARDISATION OFFICE.REFER TO
OPT VENDORS)/1321 FOURTEENTH STREET,N.W/WA-20005/WASHINGTON
D.C/USA
V97464 INDUSTRIAL RETAINING RING CO/57 CORDIER ST/NJ-07111/IRVINGTON, NJ/USA
V97928 DEUTSCH FASTENER CORP/3969 PARAMOUNT BLVD/CA
90712-4193/LAKEWOOD/USA
VB0014 ADB NV/585 LEUVENSESTEENWEG/1930/ZAVENTEN/BEL
VB0128 SONACA SA PARC INDUSTRIEL/5 ROUTE NATIONALE/6200/GOSSELIES/BEL
VB1395 TECHNICAL AIRBORNE COMPONENTS SA/PARC INDUSTRIEL DES HAUTS-SARTS
5 AVE/4040/HERSTAL/BEL
VC0258 BINDER GOTTLIEB GMBH UND CO BANDWEBEREI/BAHNHOF STRASSE
19/71088/POSTFACH 20/HOLZGERLINGEN/GER
VC0259 PANDUIT GMBH/STEINMUEHL STRASSE 14/61352/BAD HOMBURG/GER
VC0474 ILLBRUCK GMBH/BURSCHEIDER STRASSE 454/51381/LEVERKUSEN/GER
VC1711 THEYSON FRIEDRICH/JF KENNEDY STRASSE 48/38228/SALZGITTER/GER
VC3471 GLENAIR ELECTRIC GMBH/HOLZWEG 32A/61440/POSTFACH
4147/OBERURSEL/GER
VC3753 WULFMEYER RUDOLF AIRCRAFT INTERIOR GMBH & CO. KG/FRANKENRING
15/170263/LANGENHAGEN/GER
VC4293 ALCOA FASTENING SYSTEMS/FAIRCHILD FASTENERS EUR.-VSD GMBH/STEVEN
3/31135/101320/HILDESHEIM/GER
IPL INTRO
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VC4344 FROELICH GMBH/FRIEDRICH-EBERT-STR.209/37520/OSTERODE/D
VC4863 SCHWARZ/IM UNTEREN RIED 7/75382/ALTHENGSTETT/D
VC5543 INTERTURBINE LOGISTIK GMBH/KISDORFER WEG
36-38/24568/KALTENKIRCHEN/D
VC5729 HONEYWELL HPG/LADEMANNBOGEN 128/22339/HAMBURG,/D
VC7009 DUDEINS AEROSPACE GMBH/HOEKERWEG 270/40231/DUESSELDORF/GER
VC7100 ICORE INTERNATIONAL GMBH/FRIEDBERGER STRASSE 2/61350/BAD
HOMBURG/GER
VC7239 NMB MINEBA GMBH/SIEMENSTRASSE 30/63225/LANGEN/GER
VC7839 ROSWITHA WILDE TRADING/HOEHERWEG 270/40231/DUESSELDORF/D
VD0680 FAIRCHILD FATENERS EUROPE/CAMLOC GMBH/INDUSTRIES STRASSE
6/65779/POSTFACH 180/KELKHEIM/GER
VD1283 HUCK INTERNATIONAL GMBH/AN DER UNTEREN SOESE
26/37520/OSTERODE/GER
VD8090 SEEGER ORBIS GMBH/WIESBADENER STRASSE 243-247/61462/POSTFACH
1460/KOENIGSTEIN/GER
VD8286 DIN DEUTSCHES INSTITUT FUER NORMUNG E V/(STANDARDISATION OFFICE
REFER TO OPT VENDORS)/KAMEKE STRASSE 2-8/50672/KOELN/GER
VD8442 NORMENSTELLE LUFTFAHRT/(STANDARDISATION OFFICE.REFER TO OPT
VENDORS)/DREIMORGEN STRASSE 8/70771/LEINFELDEN ECHTERDINGEN/GER
VD8485 STABILUS GMBH/WALLERSHEIMER WEG 100/56070/POSTFACH
2029/KOBLENZ/GER
VD8518 DEUTSCHE AEROSPACE AIRBUS GMBH/KREETSLAG 10/21129/POSTFACH
950109/HAMBURG/GER
VD8527 HELLERMANN PAUL GMBH/SIEMENS STRASSE 5/25421/PINNEBERG/GER
VF0095 ATELIERS DE LA HAUTE-GARONNE ETS AURIOL/ZI DE
FLOURENS/31130/BALMA/FR
VF0188 BLANC AERO INDUSTRIES/193,RUE DEN BERCY,TOUR GAMMA A/75582/PARIS
CEDEX.12/FR
VF0189 MESSIER-DOWTY SA/ZONE AERONAUTIQUE LOUIS BREGUET/78142/VELIZY
VILLACOUBLAY/FR
VF0215 ESPA.SA/2 R DE BALZAC/75008/PARIS/FR
VF0222 SKF AEROSPACE FRANCE/1 AVENUE MARC SEGUIN/26241/BP 29/ST VALLIER
CEDEX/FR
VF0224 SIMMONDS SA/9 RUE DES CRESSONNIERES/72110/ST COSME EN VAIRAIS/FR
IPL INTRO
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VF0225 SOURIAU/9 RUE DE LA PORTE DE BUC/78000/VERSAILLES/FR
VF0236 BLANC AERO INDUSTRIES/18-20 RUE SAINT-HILAIRE/95310/ST QUEN
L’AUMONE/FR
VF0347 3M FRANCE/BD DE L’OISE/95006/CERGY PONTOISE CEDEX/FR
VF0355 CAILLAU SARL/28 RUE ERNEST RENAN/92134/BP 82/ISSY LES MOULINEAUX
CEDEX/FR
VF0394 AIR-LB STE SA/240 RUE GABRIEL PERI/92700/COLOMBES/FR
VF0434 D M G DECOLLETAGE GENERAL MODERNE/1 RUE GERBIER/75011/PARIS/FR
VF0564 PLASTIC OMNIUM SA/3 RUE DU PARC/92305/LEVALLOIS-PERRET/FR
VF0582 SUPERFLEXIT SA/58 BOULEVARD GALLIENI/92130/ISSY LES MOULINEAUX/FR
VF1983 DEUTSCH CIE SA/17 RUE LAVOISIER/27091/117/EVREUX CEDEX 9/FR
VF2094 S N E P SA/ZI DE SURVAURE/42602/84/MONTBRISSON CEDEX/FR
VF2538 JEHIER SA/BP 29.ROUTE DE SAINT-LEZIN/49120/CHEMILLE/FR
VF2693 LEGRAND SA/128 AVENUE DE LATTRE DE TASSIGNY/87000/LIMOGES/FR
VF3132 ITT COMPOSANTS ET INSTRUMENTS DIV CONN CANNON/157 RUE DES
BLAINS/92220/BAGNEUX/FR
VF3341 HELLERMANNTYTON CABLE MANAGEMENT PRODUCTS/MINIPARC DU MANET/2
R DES HETRES/78190/TRAPPES/FR
VF4240 HUBER ET CIE / ETS/ SA/19,RUE DE MALAKOFF/92320/CHATILLON/FR
VF4250 CONNECTRAL SA/29 RUE DES BAS ROGERS/92150/SURESNES/FR
VF5442 EADS NORMALISATION STANDARD ASN/REFER TO OPT VENDORS/37
BOULEVARD DE MONTMORENCY/75781/PARIS/FR
VF6101 AERAZUR /DIV EQUIPEMENTS AERONAUTIQUES SA/2 R MAURICE
MALLET/92137/ISSY LES MOULINEAUX CEDEX/FR
VF6162 AMPHENOL SOCAPEX/948 PROMENADE DE L’ARVE/74311/THYEZ CEDEX/FR
VF6167 HUCK FRANCE SA/US PAR VIGNY/95450/CLOS D’ASSEVILLE/FR
VF7395 DECOUPAGE INDUSTRIEL DE PRECISION SARL/ZI DE
FERRIERES/45210/FERRIERES EN GATINAIS/FR
VF7411 MECAERO SA/BLVD DU GRAND CASTAING/31120/PORTET SUR GARONNE/FR
VF7756 NORMAERO SARL/270 RUE DE L’ABBAYE/82000/MONTAUBAN/FR
VF8612 MATRIX SC FRANCE/29 CHS JULES CESAR/95300/CERGY PONTOISE CEDEX/FR
VF8982 SA G.ESTEVE/8 RUE CLAUDE GONIN ZI DE MONTAUDRAN/31400/TOULOUSE/FR
VF9211 L,HOTELLIER/4 RUE HENRI POINCARE/92167/ANTONY CEDEX/FR
IPL INTRO
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D5237300000000

VFAPE3 AIRBUS SAS (FOR ORDERING REFER TO SUPPLIER CODE)/1 ROND-POINT
MAURICE BELLONTE/31707/BLAGNAC/FRA
VH1822 STORK FOKKER AESP BV/INDUSTRIEWEG 4/3351 LB/1/PAPENDRECHT/NL
VH2776 AIR PARTS INTERNATIONAL BV/KALKOVENWEG 12/2401/255/LK ALPHEN AD
RIJN/NL
VH6173 HI-SHEAR CORP/EUROPEAN OFFICE/OOST/SCHIPHOL/HOL
VI9005 A E C M A/(STANDARDISATION OFFICE.REFER TO OPT VENDORS)/88 BLVD
MALESHERBES/75008/PARIS/FR
VK0316 ITT CANNON UK/JAYS CLOSE VIABLES INDUSTRIAL ESTATE/RG22
4BW/BASINGSTOKE HANTS/GB
VK0653 DOWTY ELECTRONIC COMPONENTS LTD/KINGSDITCH LANE/GL51
9PG/CHELTENHAM GL0S/UK
VK0654 MESSIER DOWTY LTD/CHELTENHAM ROAD EAST CHURCHDOWN/GL2
9QH/GLOUCESTER/GB
VK0685 ICORE INTERNATIONAL LTD/LEIGH ROAD SLOUGH TRADING ESTATE/SL1
4BB/SLOUGH BERKS/GB
VK0720 HELLERMANN TYTON/1 ROBESON WAY/ALTRINCHAM ROAD/M22
4TY/WYTHENSHAWE MANCHESTER/UK
VK1678 FAIRCHILD FASTENERS UK LTD/UNIT 6/22 BARDON INDUSTRIAL ESTATE/LE67
1TE/BARDON HILL, COALVILLE/UK
VK4130 WILD MANUFACTURING GROUP LTD/FLOODGATE STREET/B5
5SJ/BIRMINGHAM/GB
VK4975 LENTERN /AIRCRAFT/ LTD/MAIN ROAD/SS5 4JJ/HAWKWELL HOCKLEY
ESSEX/UK
VK5269 SKF (U.K) LTD AEROSPACE DIVISION/108 STRODE ROAD/BS21 6QQ/CLEVEDON
AVON/UK
VK5673 S P S TECHNOLOGIES LTD/T J BROOKS DIVISION/191 BARKBY ROAD TROON
INDUST0IAL ESTATE/LE4 9HX/LEICESTER/GB
VK6405 MICRODOT AEROSPACE LTD/BLACKTHORN ROAD/SL3 0AG/COLNEBROOK
SLOUGH BERKS/UK
VK7766 BRITISH STANDARDS INSTITUTION/(STANDARDISATION OFFICE.REFER TO OPT
VENDORS)/2 PARK STREET/W1A 2BS/LONDON/GB
VK8753 LINREAD NORTHBRIDGE/AIRCRAFT PRODUCT DIVISION/CROSSGATE ROAD
PARK FARM INDUSTRIAL ESTATE/B98 7TD/28/REDDITCH WORCS/UK
VR1120 SATAIR/AMAGER LANDEVEJ 147A/KASTRUP,2770/DK
VS0352 NIPPON MINIATURE BEARING COMPANY LTD/00389/TOKYO/JAP
IPL INTRO
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VS5540 ULTRA PRECISION SA/MONTHEY/CH
VU1598 BRITISH AEROSPACE AIRCRAFT GROUP/WEYBRIDGE-BRISTOL DIVISION/FILTON
HOUSE/BS99 7AR/BRISTOL/GB
VU1653 SOCIETY OF BRITISH AEROSPACE COMPANIES LTD/(STANDARDISATION
OFFICE.REFER TO OPT VENDORS)/29 KING STREET/SW1Y 6RD/LONDON/GB
VU7388 SMITHS AEROSPACE ACTUATION SYSTEMS/(FORMERLY DOWTY AEROSPACE
HYDRAULICS)/ARLE COURT/GL51 0TP/CHELTENHAM GLOUCESTER/GB
IPL INTRO
Page 14
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@AIRBUS
D5237300000000
DETAILED PARTS LIST
Page 10001
52-31-17 Jul 01/11
@AIRBUS
D5237300000000
C
60
10
120 B
110
100
90
B 50
C
A
A C
70
A
30
35
40
20
80
F_PL_523117_01_0_01_00
DOOR ASSY-CARGO COMPARTMENT,FWD

Figure 01 / FIGURE-52-31-17-950-801-01
Page 10001-0
52-31-17 Jul 01/11
@AIRBUS
D5237300000000
FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01 - 001A D5237300000000 DOOR ASSY-CARGO COMPARTMENT,FWD VFAPE3 RF
01 - 001B D5237300000200 DOOR ASSY-CARGO COMPARTMENT,FWD VFAPE3 RF
01 - 001C D5237300000400 DOOR ASSY-CARGO COMPARTMENT,FWD VFAPE3 RF
01 - 001D D5237300000800 DOOR ASSY-CARGO COMPARTMENT,FWD VFAPE3 RF
01 010A D2587113000060 . PROTECTION INSTL-FIRE VFAPE3 001
used on 001A, 001B, 001C, 001D
SEE 52-31-17-020 FOR DET
01 020A D5237300200060 . COVER-ACCESS VFAPE3 001
used on 001A, 001B, 001C, 001D
SEE 52-31-17-030 FOR DET
01 030A D5237301000060 . STRUCTURE ASSY VFAPE3 001
used on 001A, 001B, 001C, 001D
SEE 52-31-17-040 FOR DET
01 035A MS21209F1215P . INSERT V96906 003
Optional Vendor Code 04795, 06329, 60996, 8K160,
C4293, C5543, C5729, K6405
used on 001A, 001B, 001C, 001D
01 040A D5237305000060 . MECHANISM ASSY-DOOR VFAPE3 001
used on 001A, 001B, 001C, 001D
SEE 52-31-17-050 FOR DET
01 050A D5237300000061 . HOUSING-VALVE VFAPE3 001
used on 001A, 001B, 001C
SEE 52-31-17-500 FOR DET
01 050B D5237300000061 . HOUSING-VALVE VFAPE3 001
used on 001D
SEE 52-31-17-500 FOR DET
01 - 051A D5237300000061 . HOUSING-VALVE VFAPE3 001
used on 001B, 001C
SEE 52-31-17-500 FOR DET, POST SB 52-1124
01 060A D9209031103061 . ELECTRICAL SYSTEM VFAPE3 001
used on 001A
SEE 52-31-17-600 FOR DET
01 060B D9209031103061 . ELECTRICAL SYSTEM VFAPE3 001
used on 001B, 001C, 001D
SEE 52-31-17-600 FOR DET
01 070A NSA9117-23 . PLATE-IDENTIFICATION VF5442 001
NSA9117-23D F5442
Optional Vendor Code FAPE3
used on 001A, 001B
01 070B NSA9117-62 . IDENTIFICATION PLATE VF5442 001
Optional Vendor Code FAPE3
- ITEM NOT ILLUSTRATED
Page 10001-1
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@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
used on 001C, 001D
01 080A D5237121720000 . PLUG VFAPE3 003
OPT TO ABS0411PF1210 FAPE3
used on 001A, 001B, 001C, 001D
01 090A D5237113420000 . SCREW-ADJUSTING VFAPE3 004
used on 001A, 001B, 001C, 001D
01 100A NAS509-5C . NUT V80205 004
Optional Vendor Code 92595
used on 001A, 001B, 001C, 001D
01 110A SP112G . WASHER-TAB VK7766 004
OPT TO 5310999480982 K4975
Optional Vendor Code 04795, C5543, C5729, F7395,
K4130
used on 001A, 001B, 001C, 001D
01 120A NSA5054-5 . INSERT VF5442 004
OPT TO K8000-5 K6405
OPT TO SR314L0036 83324
Optional Vendor Code 04795, C5543, C5729, K6405
used on 001A, 001B, 001C, 001D
Page 10001-2
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@AIRBUS
D5237300000000
70
A 1 B
F
F 140 130
E
140
C D
F 70
120
C 80
D 90
E 110
40 50 60 10
160
100
160 30
B
A C
150
NOTE: 20
1 TYPICAL INSTALLATION
F_PL_523117_02_0_01_00
PROTECTION INSTL-FIRE
Figure 02 / FIGURE-52-31-17-950-802-01
Page 10002-0
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@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
02 - 001A D2587113000060 PROTECTION INSTL-FIRE VFAPE3 RF
used on 010A (523117010)
SEE 52-31-17-010 FOR NHA
02 010A D2587113200000 . LINING ASSY-FIRE PROTECTION VFAPE3 001
used on 001A
REFER TO SIL 25-135 ((FAR 25-856))
02 020A D2587113320000 .. INSULATION VFAPE3 001
Optional Vendor Code 1NVY1
used on 010A
REFER TO SIL 25-135 ((FAR 25-856))
used on 010A
REFER TO SIL 25-135 ((FAR 25-856))
used on 010A
REFER TO SIL 25-135 ((FAR 25-856))
used on 010A
REFER TO SIL 25-135 ((FAR 25-856))
used on 010A
REFER TO SIL 25-135 ((FAR 25-856))
used on 010A
REFER TO SIL 25-135 ((FAR 25-856))
02 080A NSA55131-007 .. STUD VF5442 013
OPT TO 2700-7S K1678
OPT TO J710-7N F9211
Optional Vendor Code 04795, C5543, C5729
used on 010A
02 090A NSA55131-005 .. STUD VF5442 001
OPT TO 2700-5S K1678
OPT TO J710-5N F9211
used on 010A
Page 10002-1
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@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
02 100A NAS1149C0532R .. WASHER V80205 014
Optional Vendor Code 04795, 60996, 8K160, C5543,
C5729
used on 010A
02 110A D2587115820200 .. SPACER VFAPE3 014
used on 010A
02 120A NSA55144-001 .. WASHER-LOCK VF5442 014
OPT TO 1127722 60119
OPT TO 2600SW K1678
Optional Vendor Code 04795, 71286, C5543, C5729,
D0680
used on 010A
02 130A NSA939510AN .. STRIP-PROTECTIVE VF5442 AR
USE AS REQUIRED, REQUIRED LENGTH 60 MM
OPT TO G51NA F3341
Optional Vendor Code C5543, F3341
used on 010A
02 140A DAN98S1B .. STRIP-CLING VFAPE3 001
REQUIRED LENGTH 400 MM
ABS1133D020 FAPE3
OPT TO 6TBD501284 C0258
Optional Vendor Code C0258, C3753, C5543
used on 010A
02 - 145A DAN98S1A . STRIP-CATCH VFAPE3 AR
ABS1133C020 FAPE3
OPT TO 6TBD501282 C0258
Optional Vendor Code C0258, C3753, C5543
used on 001A
02 150A D5237300120000 . SEAL-DOOR VFAPE3 001
used on 001A
02 160A D5237112720000 . BUSHING VFAPE3 004
used on 001A
Page 10002-2
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@AIRBUS
D5237300000000
110
A
B
10
15
A F
120
A G
F
B
C
D D
C
E C 40
C 30
F
E 20
C
E
F 50
G 160
170 D TO F
60 D
180 90 E 190
100 F
200
140 80
130
150 70
F_PL_523117_03_0_01_00
COVER-ACCESS
Figure 03 / FIGURE-52-31-17-950-803-01
Page 10003-0
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
03 - 001A D5237300200060 COVER-ACCESS VFAPE3 RF
used on 020A (523117010)
SEE 52-31-17-010 FOR NHA
03 010A D5237300200000 . COVER ASSY-ACCESS VFAPE3 001
used on 001A
03 015A D5237300220000 .. COVER-ACCESS VFAPE3 001
used on 010A
03 020A D5237124220000 .. SHEET VFAPE3 004
used on 010A
03 030A D5237124120200 .. GLASS-SIGHT VFAPE3 004
used on 010A
03 040A NAS1102-06-6 .. SCREW V80205 008
K8753
used on 010A
03 050A MS21042L06 .. NUT V96906 008
OPT TO AS8600B U1653
OPT TO H14L06 15653
OPT TO RH30A06 52828
OPT TO RM52LH3324-62 72962
OPT TO T98S632 11815
OPT TO VN300A62 92215
C5543, C5729
used on 010A
03 060A ABS0691-020 .. STUD VFAPE3 010
OPT TO 1604S41-020BP D0680
OPT TO DV691-020 C4863
used on 010A
03 070A ABS0604-4 .. WASHER VFAPE3 017
OPT TO CA21077-4 D0680
OPT TO SS604-4 C4863
used on 010A
03 080A ABS0692-01 .. WASHER-TAB VFAPE3 017
OPT TO 1604W50-1BP D0680
OPT TO H200S C4863
used on 010A
Page 10003-1
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
03 090A ABS0691-015 .. STUD VFAPE3 003
OPT TO 1604S41-015BP D0680
OPT TO DV691-015 C4863
used on 010A
03 100A ABS0691-010 .. STUD VFAPE3 004
OPT TO 1604S41-010BP D0680
OPT TO DV691-010 C4863
used on 010A
03 110A D5237288000200 . COVER-ACCESS VFAPE3 002
used on 001A
03 120A NAS1102E08-8 . SCREW V80205 004
Optional Vendor Code F0188, K8753
used on 001A
03 130A D5237173600200 . COVER ASSY-ACCESS VFAPE3 001
used on 001A
03 140A D5237173620200 .. COVER-ACCESS VFAPE3 001
used on 130A
03 150A D5347504521600 .. SECTION-SEALING VFAPE3 002
used on 130A
03 160A NAS1100E3-8 . SCREW V80205 018
Optional Vendor Code 1ER65, 8Z507, F0188, F7411,
K8753
used on 001A
03 170A NAS1149C0332R . WASHER V80205 018
Optional Vendor Code 04795, 5N982, 60996, 8K160,
C5543, C5729
used on 001A
03 180A NAS1102E3-7 . SCREW V80205 002
K8753
used on 001A
03 190A ABS0368-01 . RECEPTACLE VFAPE3 017
OPT TO 1604R02-1 71286
OPT TO HN368-01 C4863
Optional Vendor Code 04795, C5543, C5729, D0680
used on 001A
03 200A DIN65399-2400BF . RIVET VD8286 034
used on 001A
Page 10003-2
52-31-17 Jul 01/11
@AIRBUS
D5237300000000
10
B 20
30
30
20
30
F_PL_523117_04_0_01_00
STRUCTURE ASSY
Figure 04 / FIGURE-52-31-17-950-804-01
Page 10004-0
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
04 - 001A D5237301000060 STRUCTURE ASSY VFAPE3 RF
used on 030A (523117010)
SEE 52-31-17-010 FOR NHA
04 010A D5237301000061 . HINGE INSTL VFAPE3 001
used on 001A
SEE 52-31-17-900 FOR DET
04 020A D5237127620000 . PLUG-PROTECTIVE VFAPE3 002
used on 001A
04 030A D5237127620200 . PLUG-PROTECTIVE VFAPE3 003
used on 001A
04 - 040A D5237301000063 . BUSHING INSTL-DOOR STRUCTURE VFAPE3 001
used on 001A
SEE 52-31-17-960 FOR DET
Page 10004-1
52-31-17 Jul 01/11
@AIRBUS
D5237300000000
20
30
60
10
40
50
F_PL_523117_05_0_01_00
MECHANISM ASSY-DOOR
Figure 05 / FIGURE-52-31-17-950-805-01
Page 10005-0
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
05 - 001A D5237305000060 MECHANISM ASSY-DOOR VFAPE3 RF
used on 040A (523117010)
SEE 52-31-17-010 FOR NHA
05 010A D5237305000061 . LEVER ASSY-HAND VFAPE3 001
used on 001A
SEE 52-31-17-080 FOR DET
05 - 013A D5237305000073 . LEVER ASSY-HAND VFAPE3 001
used on 001A
SEE 52-31-17-080 FOR DET
05 - 015A D5237305000074 . LEVER ASSY-HAND VFAPE3 001
used on 001A
SEE 52-31-17-080 FOR DET
05 020A D5237305000062 . ROD AND PIN-DRIFT VFAPE3 001
used on 001A
SEE 52-31-17-130 FOR DET
05 - 025A D5237305000075 . ROD AND PIN-DRIFT VFAPE3 001
used on 001A
SEE 52-31-17-130 FOR DET
05 030A D5237305000063 . DOOR ASSY-VENT VFAPE3 001
used on 001A
SEE 52-31-17-200 FOR DET
05 040A D5237305000064 . MECHANISM ASSY-LOCKING VFAPE3 001
used on 001A
SEE 52-31-17-300 FOR DET
05 050A D5237305000065 . MECHANISM-INTERLOCK VFAPE3 001
used on 001A
SEE 52-31-17-440 FOR DET
05 060A D5237305000066 . SHAFT-SEQUENCE VFAPE3 001
used on 001A
SEE 52-31-17-400 FOR DET
05 - 063A D5237305000076 . SHAFT-SEQUENCE VFAPE3 001
used on 001A
SEE 52-31-17-400 FOR DET
05 - 065A D5237305000077 . SHAFT-SEQUENCE VFAPE3 001
used on 001A
SEE 52-31-17-400 FOR DET
Page 10005-1
52-31-17 Jul 01/11
@AIRBUS
D5237300000000
120
30 130
60
A 70 110
120
350
20 80 60
50 70
140
250 80
A 40
150
80
260 50
360 80
230 60
510 70
90
260 270 520 530
370 530 60
100
410 70
420 110
400 220
270 570 200
240 580
380 210
230 170
390 180
190
430 110 590
120
390 540
550 600 160
560
110
220 450
490
480
460
170 200
180 210
190
120
500
200
210
470
10 440
170
180
110 190
220
F_PL_523117_08_0_01_00
LEVER ASSY-HAND
Figure 08 / FIGURE-52-31-17-950-808-01
Page 10008-0
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
08 - 001A D5237305000061 LEVER ASSY-HAND VFAPE3 RF
used on 010A (523117050)
SEE 52-31-17-050 FOR NHA
08 - 001B D5237305000073 LEVER ASSY-HAND VFAPE3 RF
used on 013A (523117050)
SEE 52-31-17-050 FOR NHA
08 - 001C D5237305000074 LEVER ASSY-HAND VFAPE3 RF
used on 015A (523117050)
SEE 52-31-17-050 FOR NHA
08 010A D5237177000000 . LEVER ASSY-HAND VFAPE3 001
used on 001A, 001B, 001C
SEE 52-31-17-090 FOR DET
08 020A D5237178000000 . LEVER ASSY VFAPE3 001
used on 001A, 001B, 001C
08 030A D5237177620000 .. FITTING VFAPE3 001
used on 020A
08 040A ASNA2151-08 .. ACTUATING UNIT VF5442 001
OPT TO 192953 D8485
used on 020A
08 050A F5237136720200 .. PIN-LOCATING VFAPE3 002
used on 020A
08 060A MS24665-86 .. PIN-COTTER V96906 004
Optional Vendor Code 04795, 06329, 60996, 84114,
8K160, C5543, C5729
used on 020A
08 070A NAS1149C0463R .. WASHER V80205 004
C5729
used on 020A
08 080A NAS1149C0432R .. WASHER V80205 004
C5729
used on 020A
08 090A D5237179620000 .. LEVER VFAPE3 001
used on 020A
08 100A MS14102-4K .. BEARING V96906 001
Optional Vendor Code 04795, C5543, C5729, C7239,
K5269, S0352
used on 020A
08 110A NAS1291C3M . NUT V80205 007
OPT TO H42-3 15653
Page 10008-1
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@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
F0224
used on 001A, 001B, 001C
08 120A NAS1149C0332R . WASHER V80205 009
C5543, C5729
used on 001A, 001B, 001C
08 130A NSA5031-3-5 . BOLT VF5442 003
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001A, 001B, 001C
08 140A NSA5031-3-2 . BOLT VF5442 002
ABS0114T3-2 FAPE3
F0188, F6167, F7411, K5673, K8753
used on 001A, 001B, 001C
08 150A D5237179820000 . WASHER-LOCK VFAPE3 001
used on 001A, 001B, 001C
08 160A D5237176820000 . ROD-CONTROL VFAPE3 001
OPT TO B322104-003 F0222
OPT TO R24359 B1395
used on 001A
08 160B R24359 . ROD ASSY VB1395 001
OPT TO D5237176820000 FAPE3
OPT TO D5237176820200 FAPE3
used on 001B
SEE 52-31-17-950 FOR DET
08 160C B322104-003 . ROD ASSY VF0222 001
OPT TO D5237176820000 FAPE3
used on 001C
08 170A MS24665-151 . PIN-COTTER V96906 003
8K160, C5543, C5729
used on 001A, 001B, 001C
08 180A NSA5059E4 . NUT VF5442 003
OPT TO 73783CM8-428 56878
F0188
used on 001A, 001B, 001C
08 190A NAS1149C0463R . WASHER V80205 003
C5729
Page 10008-2
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
used on 001A, 001B, 001C
08 200A NSA5031-4D11 . BOLT VF5442 003
F0188, F6167, F7411, K5673, K8753
used on 001A, 001B, 001C
08 210A NAS1149C0432R . WASHER V80205 003
C5729
used on 001A, 001B, 001C
08 220A NAS1149C0363R . WASHER V80205 003
8K160, C5543, C5729
used on 001A, 001B, 001C
08 230A NSA5031-3-17 . BOLT VF5442 002
F0188, F6167, F7411, K5673, K8753
used on 001A, 001B, 001C
08 240A D5237179120000 . LOCK-UNIVERSAL JOINT VFAPE3 001
used on 001A, 001B, 001C
08 250A D5237179720200 . SHAFT VFAPE3 001
used on 001A, 001B, 001C
08 260A D5237179922000 . WASHER-SPACER VFAPE3 002
used on 001A, 001B, 001C
selfrom, THICKNESS 3.8 MM
used on 001A, 001B, 001C
08 - 271A D5237179920600 . WASHER-SPACER VFAPE3 AR
selfrom, USE AS REQUIRED, THICKNESS 3.6 MM
used on 001A, 001B, 001C
used on 001A, 001B, 001C
used on 001A, 001B, 001C
used on 001A, 001B, 001C
used on 001A, 001B, 001C
Page 10008-3
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
used on 001A, 001B, 001C
used on 001A, 001B, 001C
08 350A MS15001-1 . FITTING-LUBRICATION V96906 001
AS15001-1 81343
Optional Vendor Code 06329, 13899, 5N982, 60996,
8K160, C5543, C5729
used on 001A, 001B, 001C
08 360A D5237179520000 . SHAFT VFAPE3 001
used on 001A, 001B, 001C
08 370A D5237178500000 . LEVER ASSY-ROLLER VFAPE3 001
used on 001A, 001B, 001C
08 380A D5237178420000 .. LEVER-ROLLER VFAPE3 001
used on 370A
08 390A D5237178320000 .. BUSHING-SHOULDERED VFAPE3 002
used on 370A
08 400A D5237178620000 .. ROLLER VFAPE3 001
used on 370A
08 410A NAS1291C3M .. NUT V80205 001
OPT TO H42-3 15653
F0224
used on 370A
08 420A NAS1149C0332R .. WASHER V80205 001
C5543, C5729
used on 370A
08 430A NSA5042C04-150 .. BOLT VF5442 001
Optional Vendor Code 04795, C5543, F0095, F0188,
F7411, K4975, K5673, K8753
used on 370A
08 440A NAS428C3A7 . BOLT V80205 001
OPT TO D5237164820000 FAPE3
used on 001A, 001B, 001C
08 450A NSA5042C04-185 . BOLT VF5442 001
Optional Vendor Code 04795, C5543, F0095, F0188,
F7411, K4975, K5673, K8753
used on 001A, 001B, 001C
Page 10008-4
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
08 460A D5237178920000 . BOLT-SPRING VFAPE3 001
used on 001A, 001B, 001C
08 470A D5237178820000 . SPRING-COMPRESSION VFAPE3 001
used on 001A, 001B, 001C
08 480A A5217236820000 . SHIM VFAPE3 001
used on 001A, 001B, 001C
08 490A D5237176320000 . HOOK-CATCHING VFAPE3 001
used on 001A, 001B, 001C
08 500A NAS6703-5 . BOLT V80205 002
8K160, C5543, C5729, K8753
used on 001A, 001B, 001C
08 510A D5237179000200 . JOINT ASSY-UNIVERSAL VFAPE3 001
used on 001A
08 510B D5237179000200 . JOINT ASSY-UNIVERSAL VFAPE3 001
used on 001B
08 510C D5237179000200 . JOINT ASSY-UNIVERSAL VFAPE3 001
used on 001C
08 520A D5237179220000 .. LATCH-UNIVERSAL JOINT VFAPE3 001
used on 510A, 510B, 510C
used on 510A, 510B, 510C
08 540A MS24665-153 .. PIN-COTTER V96906 001
8K160, C5543, C5729
used on 510A, 510B, 510C
08 550A NSA5059C4 .. NUT VF5442 001
OPT TO TE9925-4 72962
OPT TO THCR54 F0224
Optional Vendor Code 04795, C5543, C5729, F0188
used on 510A, 510B, 510C
08 560A NAS1149C0463R .. WASHER V80205 001
C5729
used on 510A, 510B, 510C
08 570A NAS1149C0432R .. WASHER V80205 001
C5729
used on 510A, 510B, 510C
Page 10008-5
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
08 580A NSA5031-4D11 .. BOLT VF5442 001
F0188, F6167, F7411, K5673, K8753
used on 510A, 510B, 510C
08 590A MS14102-4K .. BEARING V96906 001
K5269, S0352
used on 510A, 510B, 510C
08 600A D5237176720200 .. ROD-CONTROL VFAPE3 001
OPT TO B322104-012 F0222
OPT TO R24358 B1395
used on 510A
08 600B R24358 .. ROD ASSY VB1395 001
OPT TO D5237176720000 FAPE3
OPT TO D5237176720200 FAPE3
OPT TO D5237176720400 FAPE3
used on 510B
SEE 52-31-17-950 FOR DET
08 600C B322104-012 .. ROD ASSY VF0222 001
OPT TO D5237176720200 FAPE3
used on 510C
Page 10008-6
52-31-17 Jul 01/11
@AIRBUS
D5237300000000
200 200
20
20
150
190
50
60
150 70
190
80
30
70
40
50 40
60
70 150
80
120 110
10
70
120 170
90
120
160
180
120
130
180
140
180
150
130
180
180
210
100
F_PL_523117_09_0_01_00
LEVER ASSY-HAND
Figure 09 / FIGURE-52-31-17-950-809-01
Page 10009-0
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
09 - 001A D5237177000000 LEVER ASSY-HAND VFAPE3 RF
used on 010A (523117080)
SEE 52-31-17-080 FOR NHA
09 010A D5237177120000 . LEVER-HAND VFAPE3 001
used on 001A
09 020A D5237178220000 . CAM-SEQUENCE VFAPE3 002
used on 001A
09 030A D5237178120000 . STOP VFAPE3 001
used on 001A
09 040A D5237177820200 . BOLT VFAPE3 002
used on 001A
09 050A NSA5321-6 . RING-RETAINING VF5442 002
OPT TO ST6 D8090
used on 001A
09 060A D5237152220000 . WASHER VFAPE3 002
used on 001A
09 070A D5237153220000 . BUSHING-SHOULDERED VFAPE3 004
used on 001A
09 080A D5237177920200 . ROLLER VFAPE3 002
used on 001A
09 090A D5227246920000 . INSERT VFAPE3 001
used on 001A
09 100A D5237177220000 . FLAP-HANDLE VFAPE3 001
used on 001A
09 110A D5237177320000 . SPRING VFAPE3 001
used on 001A
09 120A MS24665-153 . PIN-COTTER V96906 004
8K160, C5543, C5729
used on 001A
09 130A NAS1149C0363R . WASHER V80205 002
8K160, C5543, C5729
used on 001A
09 140A D5237177520200 . BOLT-BEARING VFAPE3 001
used on 001A
09 150A NAS1149C0332R . WASHER V80205 008
C5543, C5729
used on 001A
Page 10009-1
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
09 160A D5237177520000 . BOLT-BEARING VFAPE3 001
used on 001A
09 170A D5237180420000 . SLEEVE-SPRING VFAPE3 001
used on 001A
09 180A D5237136720000 . BUSHING VFAPE3 006
used on 001A
09 190A NSA5031-3-3 . BOLT VF5442 006
F0188, F6167, F7411, K5673, K8753
used on 001A
09 200A NSA5054-3 . INSERT VF5442 006
OPT TO K8000-3 K6405
OPT TO M45932-1-9AL 81349
used on 001A
09 210A D5237110220600 . LAYER-SLIDING VFAPE3 001
used on 001A
Page 10009-2
52-31-17 Jul 01/11
@AIRBUS
D5237300000000
A 10
A 20
50
40
60
70
80
200
210
30
220
230 120 130
240 140 190
190 150
180 180
110
100
120 160
90
50
60 40 170
70 20
170
10
80 200
210
220
230
240
220
230
240
30
200
210
F_PL_523117_13_0_01_00
ROD AND PIN-DRIFT

Figure 13 / FIGURE-52-31-17-950-813-01
Page 10013-0
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
13 - 001A D5237305000062 ROD AND PIN-DRIFT VFAPE3 RF
used on 020A (523117050)
SEE 52-31-17-050 FOR NHA
13 - 001B D5237305000075 ROD AND PIN-DRIFT VFAPE3 RF
used on 025A (523117050)
SEE 52-31-17-050 FOR NHA
13 010A D5237157120200 . PIN-DRIFT VFAPE3 002
used on 001A, 001B
13 020A NAS1303-11D . BOLT V80205 002
NAS6603D11 80205
Optional Vendor Code F0188, F7411, K8753
used on 001A, 001B
13 030A D5237156420000 . WASHER VFAPE3 002
used on 001A, 001B
13 040A D5237151620000 . BUSHING VFAPE3 002
used on 001A, 001B
13 050A NSA5059E3 . NUT VF5442 002
OPT TO 73783CM8-328 56878
F2094
used on 001A, 001B
13 060A NAS1149C0332R . WASHER V80205 002
C5543, C5729
used on 001A, 001B
13 070A MS24665-88 . PIN-COTTER V96906 002
8K160, C5543, C5729
used on 001A, 001B
13 080A D5237305720000 . ROD VFAPE3 002
used on 001A
13 080B R25259 . ROD ASSY VB1395 002
used on 001B
SEE 52-31-17-950 FOR DET
13 090A D5237159200000 . BELLCRANK ASSY VFAPE3 001
used on 001A, 001B
13 100A D5237159700000 .. BELLCRANK VFAPE3 001
used on 090A
13 110A D5237159720000 ... BELLCRANK VFAPE3 001
used on 100A
Page 10013-1
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
13 120A MS14102-4K ... BEARING V96906 002
K5269, S0352
used on 100A
13 130A D5237159600000 .. LEVER VFAPE3 001
used on 090A
13 140A D5237159620000 ... LEVER VFAPE3 001
used on 130A
13 150A MS14102-4K ... BEARING V96906 001
K5269, S0352
used on 130A
13 160A D5237103220200 .. SHAFT-BEAM 3 VFAPE3 001
used on 090A
13 170A AN386-2-8A .. PIN-TAPER V88044 002
used on 090A
13 180A D5237180220000 .. SLEEVE VFAPE3 002
used on 090A
13 190A NAS1291C3M .. NUT V80205 002
OPT TO H42-3 15653
F0224
used on 090A
13 200A NSA5031-4D11 . BOLT VF5442 003
F0188, F6167, F7411, K5673, K8753
used on 001A, 001B
13 210A NAS1149C0432R . WASHER V80205 003
C5729
used on 001A, 001B
13 220A NAS1149C0463R . WASHER V80205 003
C5729
used on 001A, 001B
13 230A NSA5059E4 . NUT VF5442 003
OPT TO 73783CM8-428 56878
F0188
used on 001A, 001B
Page 10013-2
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
13 240A MS24665-151 . PIN-COTTER V96906 003
8K160, C5543, C5729
used on 001A, 001B
Page 10013-3
52-31-17 Jul 01/11
@AIRBUS
D5237300000000
10 A 1
30
A 40
20
30
160
B 170 B
140
230
250
120 170
180 240
130
220
70
80
110 90
190
200
210 250
50
430 70
80
90 120 120
420 130 130
270
200 280 70
440 290 80
450
90
300
260
60
70 280 470
310 460
330 390
320
100
70 350 480
80 360
90 370
70 340
NOTE: 80 410
90 390 400
1 TYPICAL INSTALLATION
380
F_PL_523117_20_0_01_00
DOOR ASSY-VENT
Figure 20 / FIGURE-52-31-17-950-820-01
Page 10020-0
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
20 - 001A D5237305000063 DOOR ASSY-VENT VFAPE3 RF
used on 030A (523117050)
SEE 52-31-17-050 FOR NHA
20 010A D5237166120200 . COVER VFAPE3 001
used on 001A
20 020A NAS1291C3M . NUT V80205 004
OPT TO H42-3 15653
F0224
used on 001A
20 030A NAS1149C0332R . WASHER V80205 008
C5543, C5729
used on 001A
20 040A NAS1100E3-7 . SCREW V80205 004
Optional Vendor Code 1ER65, 8Z507, F0188, F7411,
K8753
used on 001A
used on 001A
SEE 52-31-17-210 FOR DET
20 060A NSA5031-4D16 . BOLT VF5442 001
F0188, F6167, F7411, K5673, K8753
used on 001A
20 070A NAS1149C0463R . WASHER V80205 006
C5729
used on 001A
20 080A MS24665-151 . PIN-COTTER V96906 005
8K160, C5543, C5729
used on 001A
20 090A NSA5059E4 . NUT VF5442 005
OPT TO 73783CM8-428 56878
F0188
used on 001A
20 100A D5237141420000 . BUSHING VFAPE3 001
used on 001A
20 110A A5217544023000 . ROD-ACTUATING VFAPE3 001
OPT TO R21362 B1395
OPT TO TDF13228-10 F0222
Page 10020-1
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
used on 001A
20 120A NSA5031-4D11 . BOLT VF5442 003
F0188, F6167, F7411, K5673, K8753
used on 001A
20 130A NAS1149C0432R . WASHER V80205 003
C5729
used on 001A
20 140A D5237291720000 . FLANGE-BEARING VFAPE3 001
used on 001A
20 160A NAS6703-3 . BOLT V80205 003
8K160, C5543, C5729, K8753
used on 001A
20 170A NAS1149C0363R . WASHER V80205 006
8K160, C5543, C5729
used on 001A
20 180A NAS1291C3M . NUT V80205 003
OPT TO H42-3 15653
F0224
used on 001A
20 190A NAS6703-5 . BOLT V80205 004
8K160, C5543, C5729, K8753
used on 001A
20 200A NAS1149C0332R . WASHER V80205 005
C5543, C5729
used on 001A
20 210A D5237167220000 . SHIM VFAPE3 001
used on 001A
20 220A D5237160200600 . GEARBOX ASSY VFAPE3 001
used on 001A
SEE 52-31-17-250 FOR DET
20 230A D5237180300200 . ROD ASSY-CONNECTING VFAPE3 001
used on 001A
20 240A D5237180320200 .. ROD-CONNECTING VFAPE3 001
used on 230A
Page 10020-2
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
20 250A MS14102-4K .. BEARING V96906 002
K5269, S0352
used on 230A
20 260A D5237150100400 . LINK ASSY VFAPE3 001
used on 001A
20 270A D5237153120200 .. FORK VFAPE3 001
used on 260A
20 280A SP108D .. WASHER-TAB VK7766 002
used on 260A
20 290A NAS509L3C .. NUT V80205 001
8K160, 92595, C5543, C5729
used on 260A
20 300A D5237152820000 .. ROD VFAPE3 001
used on 260A
20 310A NAS509-3C .. NUT V80205 001
8K160, 92595, C5543, C5729
used on 260A
20 320A D5237152620200 .. FORK VFAPE3 001
used on 260A
20 330A NSA5031-3D7 .. BOLT VF5442 001
F0188, F6167, F7411, K5673, K8753
used on 260A
20 340A D5237153420200 .. SLEEVE VFAPE3 001
used on 260A
20 350A NAS1149C0332R .. WASHER V80205 001
C5543, C5729
used on 260A
20 360A NSA5059C3 .. NUT VF5442 001
OPT TO H53173-3 15653
OPT TO TE9925-3 72962
OPT TO THCR53 F0224
used on 260A
20 370A MS24665-88 .. PIN-COTTER V96906 001
8K160, C5543, C5729
Page 10020-3
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
used on 260A
20 380A D5237153500200 .. LEVER ASSY VFAPE3 001
used on 260A
20 390A D5237153720000 ... BUSHING-SHOULDERED VFAPE3 002
used on 380A
20 400A D5237152420200 ... LEVER VFAPE3 001
used on 380A
20 410A D5237153320000 ... BUSHING VFAPE3 001
used on 380A
20 420A NSA5031-3D7 . BOLT VF5442 001
F0188, F6167, F7411, K5673, K8753
used on 001A
20 430A D5237153420200 . SLEEVE VFAPE3 001
used on 001A
20 440A NSA5059E3 . NUT VF5442 001
OPT TO 73783CM8-328 56878
F2094
used on 001A
20 450A MS24665-88 . PIN-COTTER V96906 001
8K160, C5543, C5729
used on 001A
20 460A D5237111920000 . SUPPORT-FITTING VFAPE3 001
used on 001A
20 470A DAN5-5-5 . PIN-RIVET VD8518 002
OPT TO ABS0250A5-5 FAPE3
OPT TO F0N2-1196-5-5 56878
OPT TO HL10VDF5-5 92215
Optional Vendor Code 04795, 56878, 73197, C5543,
C5729, D1283, F0188, K5673
used on 001A
20 480A NSA5075-5 . COLLAR VF5442 002
OPT TO DAN11-5 D8518
OPT TO F0N2-1181-5 H1822
OPT TO HL70AA5 92215
C5729, R1120
used on 001A
Page 10020-4
52-31-17 Jul 01/11
@AIRBUS
D5237300000000
A 190
100
110 200
170 A
180
380
400 390
410
30 120
70 160
90 420
120
370 130
140
360
370 420 350
110 150
60 260
280
80 10 270
20 220 290
10 30 230
20 150
30
40 320
50
60
30
40
250
120
130
30
240 70 330
320 300
120 310 210
160
F_PL_523117_21_0_01_00
DOOR ASSY-VENT
Figure 21 / FIGURE-52-31-17-950-821-01
Page 10021-0
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
21 - 001A D5237163500860 DOOR ASSY-VENT VFAPE3 RF
used on 050A (523117200)
SEE 52-31-17-200 FOR NHA
21 010A MS24665-300 . PIN-COTTER V96906 002
8K160, C5543, C5729
used on 001A
21 020A NSA5059E6 . NUT VF5442 002
OPT TO 73783CM8-624 56878
F0188
used on 001A
21 030A NAS1149C0632R . WASHER V80205 AR
USE AS REQUIRED, USAGE RANGE FROM 5 TO 8
C5729
used on 001A
21 040A NAS1149C0616R . WASHER V80205 AR
USE AS REQUIRED, USAGE RANGE FROM 4 TO 5
C5729
used on 001A
21 050A D5237166620100 . SPRING VFAPE3 001
used on 001A
21 060A D5237166320200 . SLEEVE VFAPE3 002
used on 001A
21 070A NSA5031-6D38 . BOLT VF5442 002
Optional Vendor Code 04795, C5543, D1283, F0188,
F6167, F7411, K5673, K8753
used on 001A
21 080A D5237166620000 . SPRING VFAPE3 001
used on 001A
21 090A D5237166320400 . SLEEVE VFAPE3 001
used on 001A
used on 001A
21 110A NSA5030-4-26 .. SCREW VF5442 004
ASNA2001V4-26 F5442
F0188, F6167, F7411, K5673, K8753
used on 100A
Page 10021-1
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
21 120A NAS1149C0463R .. WASHER V80205 010
C5729
used on 100A
21 130A NAS1291C4M .. NUT V80205 006
OPT TO 180003-5 60119
OPT TO PLH504M F0224
used on 100A
21 140A NSA5030-4-27 .. SCREW VF5442 002
ASNA2001V4-27 F5442
F0188, F6167, F7411, K5673, K8753
used on 100A
21 150A D5237165220200 .. BOLT-SPRING VFAPE3 002
used on 100A
21 160A MS24665-86 .. PIN-COTTER V96906 002
8K160, C5543, C5729
used on 100A
21 170A D5237163920200 .. SEAL-PRESSURE RELIEF FLAP VFAPE3 001
used on 100A
21 180A D5237163820500 .. RETAINER VFAPE3 001
used on 100A
21 190A D5237163820400 .. RETAINER VFAPE3 001
used on 100A
21 200A D5237163620400 .. DOOR-VENT VFAPE3 001
used on 100A
21 210A D5237164700000 .. BOX ASSY-TORSION VFAPE3 001
used on 100A
21 220A D5237164000200 ... ARM ASSY-ACTUATOR VFAPE3 001
used on 210A
21 230A D5237164120200 .... ARM-ACTUATOR VFAPE3 001
used on 220A
21 240A D5237165420200 .... BUSHING-SHOULDERED VFAPE3 001
used on 220A
21 250A D5237165620200 .... BUSHING VFAPE3 001
used on 220A
21 260A NAS428C3A7 .... BOLT V80205 001
OPT TO D5237164820000 FAPE3
used on 220A
Page 10021-2
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
21 270A SP108D .... WASHER-TAB VK7766 001
used on 220A
21 280A MS35650-304 .... NUT V96906 001
Optional Vendor Code 04795, 06329, 1V757, 57983,
69289, C5543, C5729
used on 220A
21 290A MS21209F1-20 .... INSERT V96906 001
C4293, C5543, C5729, K6405
used on 220A
used on 220A
21 310A D5237164320000 .... BUSHING VFAPE3 001
used on 220A
used on 220A
21 330A D5237164520000 ... BOX-TORSION VFAPE3 001
used on 210A
21 - 340A LN9198-4000CF ... RIVET VD8442 AR
USE AS REQUIRED, DETERMINE LENGTH ON
INSTALLATION
EN6081D5 I9005
used on 210A
21 350A D5237165000200 ... ARM ASSY VFAPE3 001
used on 210A
21 360A D5237165120200 .... ARM VFAPE3 001
used on 350A
21 370A D5237165620200 .... BUSHING VFAPE3 002
used on 350A
21 380A NAS428C3A7 .... BOLT V80205 001
OPT TO D5237164820000 FAPE3
used on 350A
21 390A SP108D .... WASHER-TAB VK7766 001
used on 350A
21 400A MS35650-304 .... NUT V96906 001
Optional Vendor Code 04795, 06329, 1V757, 57983,
69289, C5543, C5729
used on 350A
Page 10021-3
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
21 410A MS21209F1-20 .... INSERT V96906 001
C4293, C5543, C5729, K6405
used on 350A
used on 350A
Page 10021-4
52-31-17 Jul 01/11
@AIRBUS
D5237300000000
140
130
A
120
A
150
160
80
70
40
10
20
340
160 50
270 60
280
280
160 240
270 220 90
280 210 40
110
280
300
330
290
290
230 200
250
290 260
100
310 30
290 160
320 270
170
190
180
F_PL_523117_25_0_01_00
GEARBOX ASSY
Figure 25 / FIGURE-52-31-17-950-825-01
Page 10025-0
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
25 - 001A D5237160200600 GEARBOX ASSY VFAPE3 RF
used on 220A (523117200)
SEE 52-31-17-200 FOR NHA
25 010A D5237162000400 . HOUSING ASSY VFAPE3 001
used on 001A
25 020A D5237162120000 .. CASING VFAPE3 001
used on 010A
used on 010A
25 040A D5237162520200 .. BUSHING VFAPE3 002
used on 010A
25 050A NAS1792A3-1 .. NUT-PLATE V80205 004
OPT TO AJCR93M13 F0224
OPT TO F50733-3-1 15653
OPT TO NSA5103-3 F5442
OPT TO RF160A3-1 52828
C5543, C5729, U1598
used on 010A
25 060A DIN65399-2400BF .. RIVET VD8286 AR
INSTALLATION
used on 010A
25 070A D5237161500400 . SHAFT ASSY VFAPE3 001
used on 001A
25 080A D5237161620600 .. AXLE VFAPE3 001
used on 070A
25 090A D5237160720200 .. GEAR-BEVEL VFAPE3 001
used on 070A
25 100A D5237160820000 .. PIN VFAPE3 001
used on 070A
25 110A MS16624-4025 .. RING-RETAINING V96906 001
C5729
used on 070A
25 120A D5237161420200 . LEVER VFAPE3 001
used on 001A
25 130A DAN157-13 . PLUG-PROTECTIVE VD8518 001
OPT TO TL4-163 C1711
used on 001A
Page 10025-1
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
25 140A AN386-2-8A . PIN-TAPER V88044 001
used on 001A
25 150A D5237180220000 . SLEEVE VFAPE3 001
used on 001A
25 160A NAS1291C3M . NUT V80205 008
OPT TO H42-3 15653
F0224
used on 001A
25 170A D5237160320000 . SHIM VFAPE3 001
used on 001A
25 180A D5237163000800 . COVER ASSY VFAPE3 001
used on 001A
25 190A D5237163120400 .. COVER VFAPE3 001
used on 180A
used on 180A
25 210A D5237160500200 . AXLE ASSY VFAPE3 001
used on 001A
25 220A D5237160620200 .. AXLE VFAPE3 001
used on 210A
25 230A D5237160720200 .. GEAR-BEVEL VFAPE3 001
used on 210A
25 240A D5237160820000 .. PIN VFAPE3 001
used on 210A
25 250A MS16624-4025 .. RING-RETAINING V96906 001
C5729
used on 210A
25 260A D5237167420000 . WASHER-THRUST VFAPE3 001
MODIFIED FROM D5237167420200 MADE BY
FAPE3
FAPE3
FAPE3
FAPE3
FAPE3
used on 001A
Page 10025-2
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
25 270A NAS1149C0332R . WASHER V80205 007
C5543, C5729
used on 001A
25 280A D5237167320000 . SLEEVE VFAPE3 004
used on 001A
25 290A AN386-1-9A . PIN-TAPER V88044 004
F0434
used on 001A
25 300A D5237176920000 . LEVER VFAPE3 001
used on 001A
25 310A D5237151220800 . CAM-LOCKING VFAPE3 001
used on 001A
25 320A D5237167620200 . LEVER VFAPE3 001
used on 001A
25 330A D5237153320000 . BUSHING VFAPE3 001
used on 001A
25 340A NSA5031-3-3 . BOLT VF5442 003
F0188, F6167, F7411, K5673, K8753
used on 001A
Page 10025-3
52-31-17 Jul 01/11
@AIRBUS
D5237300000000
40
10
B
A A TO C
A
C 170
180
190
240
270 140
290 150
260
200
C 230
AB 280 210
240
250
220 B
220 B 110
160
170 120 80 B
90 B
130
140 AC 90
100
AC 80
20 AC 50
50 30 B 60 AC
60 B 70
70
F_PL_523117_30_0_01_00
MECHANISM ASSY-LOCKING
Figure 30 / FIGURE-52-31-17-950-830-01
Page 10030-0
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
30 - 001A D5237305000064 MECHANISM ASSY-LOCKING VFAPE3 RF
used on 040A (523117050)
SEE 52-31-17-050 FOR NHA
30 010A D5237305100000 . SHAFT ASSY-LOCKING VFAPE3 001
used on 001A
SEE 52-31-17-310 FOR DET
30 020A D5237149000000 . LATCHING MECHANISM ASSY VFAPE3 003
used on 001A
SEE 52-31-17-330 FOR DET
30 030A D5237149000200 . LATCHING MECHANISM ASSY VFAPE3 001
used on 001A
SEE 52-31-17-340 FOR DET
30 040A D5237305400000 . SHAFT ASSY-LATCHING VFAPE3 001
used on 001A
SEE 52-31-17-320 FOR DET
30 050A MS24665-370 . PIN-COTTER V96906 004
8K160, C5543, C5729
used on 001A
30 060A NSA5059E10 . NUT VF5442 004
OPT TO 73783CM8-1018 56878
used on 001A
30 070A NAS1149C1032R . WASHER V80205 004
C5729
used on 001A
30 080A D5237144120000 . BOLT VFAPE3 004
used on 001A
30 090A D5237140120000 . WASHER VFAPE3 004
used on 001A
used on 001A
used on 001A
30 120A D5237144220200 . SLEEVE VFAPE3 004
used on 001A
30 130A NAS6705U42 . BOLT V80205 004
F7411, K8753
used on 001A
Page 10030-1
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
30 140A NAS1149C0532R . WASHER V80205 008
C5729
used on 001A
30 150A NAS1291C5M . NUT V80205 004
OPT TO H42-5 15653
OPT TO PLH55M F0224
OPT TO VN300D054 92215
F0224
used on 001A
30 160A NSA5031-7D42 . BOLT VF5442 004
Optional Vendor Code 04795, C5543, D1283, F0188,
F6167, F7411, K5673, K8753
used on 001A
30 170A NAS1149C0763R . WASHER V80205 008
C5729
used on 001A
30 180A MS24665-300 . PIN-COTTER V96906 004
8K160, C5543, C5729
used on 001A
30 190A NSA5059E7 . NUT VF5442 004
OPT TO 73783CM8-720 56878
used on 001A
used on 001A
30 210A D5237144420400 . SLEEVE VFAPE3 004
used on 001A
30 220A D5237140120400 . WASHER VFAPE3 002
used on 001A
30 230A D5237144520200 . BOLT VFAPE3 001
used on 001A
30 240A NAS1149C0432R . WASHER V80205 008
C5729
used on 001A
30 250A D5237141320400 . BUSHING VFAPE3 004
used on 001A
30 260A D5237141420000 . BUSHING VFAPE3 004
used on 001A
Page 10030-2
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
30 270A MS24665-151 . PIN-COTTER V96906 004
8K160, C5543, C5729
used on 001A
30 280A NSA5031-4D16 . BOLT VF5442 003
F0188, F6167, F7411, K5673, K8753
used on 001A
30 290A NSA5059E4 . NUT VF5442 004
OPT TO 73783CM8-428 56878
F0188
used on 001A
Page 10030-3
52-31-17 Jul 01/11
@AIRBUS
D5237300000000
A
A 130
30
40
20
20
120
120
80
50
30
50 40
70 130
60
30
40
20
20
120
120 10
30
110 40
130
50 30 50
30 40
30
40 40 50
50
100
90
130
120 30 140
40
120 20
20
120
120
F_PL_523117_31_0_01_00
SHAFT ASSY-LOCKING
Figure 31 / FIGURE-52-31-17-950-831-01
Page 10031-0
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
31 - 001A D5237305100000 SHAFT ASSY-LOCKING VFAPE3 RF
used on 010A (523117300)
SEE 52-31-17-300 FOR NHA
31 010A D5237305220000 . SHAFT-LOCKING VFAPE3 001
used on 001A
31 020A AN386-1-10A . PIN-TAPER V88044 006
F0434
used on 001A
31 030A NAS1291C3M . NUT V80205 014
OPT TO H42-3 15653
F0224
used on 001A
31 040A NAS1149C0332R . WASHER V80205 014
C5543, C5729
used on 001A
31 050A D5237167320000 . SLEEVE VFAPE3 006
used on 001A
31 060A D5237150300000 . LEVER ASSY-HINGED VFAPE3 001
used on 001A
31 070A D5237150320000 .. LEVER-HINGED VFAPE3 001
used on 060A
31 080A MS14102-4K .. BEARING V96906 001
K5269, S0352
used on 060A
31 090A D5237150200600 . LEVER ASSY VFAPE3 001
used on 001A
31 100A D5237150220600 .. LEVER VFAPE3 001
used on 090A
31 110A MS14103-4K .. BEARING V96906 001
S0352
used on 090A
31 120A DAN15-6-18 . PIN-RIVET VD8518 008
OPT TO HL20PB6-18 73197
used on 001A
31 130A D5237151221000 . CAM-LOCKING VFAPE3 004
used on 001A
Page 10031-1
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
31 140A D5237176920000 . LEVER VFAPE3 001
used on 001A
Page 10031-2
52-31-17 Jul 01/11
@AIRBUS
D5237300000000
A
70
60 50 80
60
90
50
40
40
30
40
40
50
60 30
40
50
60
50
40
60
40 100
50
50
60
60
40
10
130
30
50 120
60
40 50
60
40
50 40
60 110
50
60
50
60
F_PL_523117_32_0_01_00
SHAFT ASSY-LATCHING
Figure 32 / FIGURE-52-31-17-950-832-01
Page 10032-0
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
32 - 001A D5237305400000 SHAFT ASSY-LATCHING VFAPE3 RF
used on 040A (523117300)
SEE 52-31-17-300 FOR NHA
32 010A D5237305520000 . SHAFT-LATCHING VFAPE3 001
used on 001A
32 030A D5237150620000 . LEVER-SHAFT VFAPE3 003
used on 001A
32 040A AN386-2-13A . PIN-TAPER V88044 011
F0434
used on 001A
32 050A D5237180220000 . SLEEVE VFAPE3 012
used on 001A
32 060A NAS1291C3M . NUT V80205 012
OPT TO H42-3 15653
F0224
used on 001A
32 070A D5237150500000 . LEVER ASSY-HINGED VFAPE3 001
used on 001A
32 080A D5237150520000 .. LEVER-HINGED VFAPE3 001
used on 070A
32 090A MS14102-4K .. BEARING V96906 001
K5269, S0352
used on 070A
32 100A D5237141920200 . CAM-STOP VFAPE3 001
used on 001A
32 110A D5237143220200 . LEVER-SWITCH VFAPE3 001
used on 001A
32 120A D5237150620200 . LEVER-SHAFT VFAPE3 001
used on 001A
32 130A AN386-2-12A . PIN-TAPER V88044 001
F0434
used on 001A
Page 10032-1
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D5237300000000
110
100 A
120
A 130
140
110
100
120
130
140
90
150
70
260
160 90
170
80 60
190
180
60
50
140
220
250
240
210 230
220 190
40
200
50
30 20
10
F_PL_523117_33_0_01_00
LATCHING MECHANISM ASSY

Figure 33 / FIGURE-52-31-17-950-833-01
Page 10033-0
52-31-17 Jul 01/11
@AIRBUS
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1234567 FROM PER
TO ASSY
33 - 001A D5237149000000 LATCHING MECHANISM ASSY VFAPE3 RF
used on 020A (523117300)
SEE 52-31-17-300 FOR NHA
33 010A D5237143500000 . HOOK ASSY-LATCHING VFAPE3 001
used on 001A
33 020A D5237143620000 .. HOOK-LATCHING VFAPE3 001
used on 010A
33 030A MS15001-1 .. FITTING-LUBRICATION V96906 001
AS15001-1 81343
8K160, C5543, C5729
used on 010A
used on 010A
used on 010A
33 060A D5237140320200 . SLEEVE VFAPE3 002
used on 001A
33 070A D5237185320000 . LINK-CONNECTING VFAPE3 001
used on 001A
33 080A D5237140420200 . BOLT VFAPE3 001
used on 001A
33 090A NAS1149C0732R . WASHER V80205 002
C5729
used on 001A
used on 001A
used on 001A
33 120A NSA5059C5 . NUT VF5442 002
OPT TO TE9925-5 72962
OPT TO THCR55 F0224
used on 001A
33 130A NAS1149C0532R . WASHER V80205 002
C5729
used on 001A
33 140A MS24665-153 . PIN-COTTER V96906 003
8K160, C5543, C5729
Page 10033-1
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TO ASSY
used on 001A
33 150A D5237140420000 . BOLT VFAPE3 001
used on 001A
used on 001A
used on 160A
33 180A D5237142320200 .. BUSHING VFAPE3 001
used on 160A
used on 160A
AS15001-1 81343
8K160, C5543, C5729
used on 160A
33 210A NSA5031-4D16 . BOLT VF5442 001
F0188, F6167, F7411, K5673, K8753
used on 001A
33 220A NAS1149C0432R . WASHER V80205 002
C5729
used on 001A
33 230A D5237141320400 . BUSHING VFAPE3 001
used on 001A
33 240A D5237141420000 . BUSHING VFAPE3 001
used on 001A
33 250A NSA5059C4 . NUT VF5442 001
OPT TO TE9925-4 72962
OPT TO THCR54 F0224
used on 001A
33 260A D5237180120000 . ROD-CONNECTING VFAPE3 001
OPT TO B322104-013 F0222
OPT TO R24225 B1395
used on 001A
Page 10033-2
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@AIRBUS
D5237300000000
100
110 A
150
A 90
100
110
80
90
120
130
140
70
260
160 120
170 130
140 60
190
180
60
50
140
220
250
240
210 230
220 190
40
200
50
30 20
10
F_PL_523117_34_0_01_00
LATCHING MECHANISM ASSY

Figure 34 / FIGURE-52-31-17-950-834-01
Page 10034-0
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
34 - 001A D5237149000200 LATCHING MECHANISM ASSY VFAPE3 RF
used on 030A (523117300)
SEE 52-31-17-300 FOR NHA
34 010A D5237143500000 . HOOK ASSY-LATCHING VFAPE3 001
used on 001A
34 020A D5237143620000 .. HOOK-LATCHING VFAPE3 001
used on 010A
AS15001-1 81343
8K160, C5543, C5729
used on 010A
used on 010A
used on 010A
34 060A D5237140320200 . SLEEVE VFAPE3 002
used on 001A
34 070A D5237185320000 . LINK-CONNECTING VFAPE3 001
used on 001A
34 080A D5237140420200 . BOLT VFAPE3 001
used on 001A
34 090A NAS1149C0732R . WASHER V80205 002
C5729
used on 001A
used on 001A
used on 001A
34 120A NSA5059C5 . NUT VF5442 002
OPT TO TE9925-5 72962
OPT TO THCR55 F0224
used on 001A
34 130A NAS1149C0532R . WASHER V80205 002
C5729
used on 001A
34 140A MS24665-153 . PIN-COTTER V96906 003
8K160, C5543, C5729
Page 10034-1
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1234567 FROM PER
TO ASSY
used on 001A
34 150A D5237140420000 . BOLT VFAPE3 001
used on 001A
used on 001A
used on 160A
34 180A D5237142320200 .. BUSHING VFAPE3 001
used on 160A
used on 160A
AS15001-1 81343
8K160, C5543, C5729
used on 160A
34 210A NSA5031-4D16 . BOLT VF5442 001
F0188, F6167, F7411, K5673, K8753
used on 001A
34 220A NAS1149C0432R . WASHER V80205 002
C5729
used on 001A
34 230A D5237141320400 . BUSHING VFAPE3 001
used on 001A
34 240A D5237141420000 . BUSHING VFAPE3 001
used on 001A
34 250A NSA5059C4 . NUT VF5442 001
OPT TO TE9925-4 72962
OPT TO THCR54 F0224
used on 001A
34 260A D5237180120000 . ROD-CONNECTING VFAPE3 001
OPT TO B322104-013 F0222
OPT TO R24225 B1395
used on 001A
Page 10034-2
52-31-17 Jul 01/11
@AIRBUS
D5237300000000
A
150
70
80
90 100
100
140 180
110 160
120 170
130
130
110
190 120
200
20
160 30
170
180
40
50
60
10
40
210 50
60
20
30
40 20
50 30
60
F_PL_523117_40_0_01_00
SHAFT-SEQUENCE
Figure 40 / FIGURE-52-31-17-950-840-01
Page 10040-0
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
40 - 001A D5237305000066 SHAFT-SEQUENCE VFAPE3 RF
used on 060A (523117050)
SEE 52-31-17-050 FOR NHA
40 - 001B D5237305000076 SHAFT-SEQUENCE VFAPE3 RF
used on 063A (523117050)
SEE 52-31-17-050 FOR NHA
40 - 001C D5237305000077 SHAFT-SEQUENCE VFAPE3 RF
used on 065A (523117050)
SEE 52-31-17-050 FOR NHA
OPT TO B322104-002 F0222
OPT TO R24364 B1395
used on 001A, 001B, 001C
40 020A NSA5031-4D11 . BOLT VF5442 003
F0188, F6167, F7411, K5673, K8753
used on 001A, 001B, 001C
40 030A NAS1149C0432R . WASHER V80205 003
C5729
used on 001A, 001B, 001C
40 040A NAS1149C0463R . WASHER V80205 003
C5729
used on 001A, 001B, 001C
40 050A NSA5059E4 . NUT VF5442 003
OPT TO 73783CM8-428 56878
F0188
used on 001A, 001B, 001C
40 060A MS24665-151 . PIN-COTTER V96906 003
8K160, C5543, C5729
used on 001A, 001B, 001C
40 070A D5237159800000 . COVER ASSY-BEAM 4 VFAPE3 001
used on 001A, 001B, 001C
40 080A D5237159900000 .. COVER-BEAM 4 VFAPE3 001
used on 070A
40 090A D5237159920000 ... COVER VFAPE3 001
used on 080A
Page 10040-1
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@AIRBUS
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1234567 FROM PER
TO ASSY
40 100A D5237162320000 ... BUSHING-SHOULDERED VFAPE3 002
used on 080A
40 110A D5237162700200 .. LEVER-BEAM 4 VFAPE3 002
used on 070A
40 120A D5237162720200 ... LEVER-BEAM 4 VFAPE3 001
used on 110A
40 130A MS14103-4K ... BEARING V96906 001
S0352
used on 110A
40 140A D5237162820000 .. SLEEVE-SPACER VFAPE3 001
used on 070A
40 150A D5237162620000 .. SHAFT-BEAM 4 VFAPE3 001
used on 070A
40 160A AN386-2-8A .. PIN-TAPER V88044 002
used on 070A
40 170A D5237180220000 .. SLEEVE VFAPE3 002
used on 070A
40 180A NAS1291C3M .. NUT V80205 002
OPT TO H42-3 15653
F0224
used on 070A
40 190A NSA5031-3-3 . BOLT VF5442 004
F0188, F6167, F7411, K5673, K8753
used on 001A, 001B, 001C
40 200A NAS1149C0332R . WASHER V80205 004
C5543, C5729
used on 001A, 001B, 001C
OPT TO B322104-006 F0222
used on 001A
40 210B R24365 . ROD ASSY VB1395 001
used on 001B
SEE 52-31-17-950 FOR DET
40 210C B322104-006 . ROD ASSY VF0222 001
OPT TO D5237161720000 FAPE3
used on 001C
Page 10040-2
52-31-17 Jul 01/11
@AIRBUS
D5237300000000
A
280
60 290
70 300
50
A 270 60
260 70 60
300 70
240
110
160
210
50
220
250
40
180
190
200 80
30
20
170 80 10
110 230
160 90
100
110
160
130
150
120 140
F_PL_523117_44_0_01_00
MECHANISM-INTERLOCK
Figure 44 / FIGURE-52-31-17-950-844-01
Page 10044-0
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
44 - 001A D5237305000065 MECHANISM-INTERLOCK VFAPE3 RF
used on 050A (523117050)
SEE 52-31-17-050 FOR NHA
44 010A D5237145500000 . SLEEVE ASSY-SPRING VFAPE3 001
used on 001A
44 020A D5237145620000 .. SLEEVE-SPRING VFAPE3 001
used on 010A
44 030A D5237145820400 .. BUSHING VFAPE3 001
used on 010A
44 040A D5237148220000 . SPRING-COMPRESSION VFAPE3 001
used on 001A
44 050A MS20392-3T49 . PIN V96906 002
Optional Vendor Code 04795, 06329, 6D833, 70347,
C5543, C5729, F0188, H2776
used on 001A
44 060A MS24665-151 . PIN-COTTER V96906 003
8K160, C5543, C5729
used on 001A
44 070A NAS1149C0463R . WASHER V80205 003
C5729
used on 001A
used on 001A
44 090A D5237145000400 . MECHANISM-INTERLOCK VFAPE3 001
used on 001A
44 100A D5237147620200 .. LEVER VFAPE3 001
used on 090A
44 110A D5237148320400 .. PIN VFAPE3 003
used on 090A
44 120A MS16624-5018-1 .. RING-RETAINING V96906 001
C5729
used on 090A
44 130A D5237147820000 .. PIN VFAPE3 001
used on 090A
44 140A D5237147720000 .. ROLLER VFAPE3 001
used on 090A
44 150A D5237179420000 .. ROD-CONNECTING VFAPE3 001
used on 090A
Page 10044-1
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
44 160A NSA5321-6 .. RING-RETAINING VF5442 003
OPT TO ST6 D8090
used on 090A
44 170A D5237146620400 .. LEVER VFAPE3 001
used on 090A
44 180A D5237113420400 .. SCREW-ADJUSTING VFAPE3 001
used on 090A
44 190A NAS509-5C .. NUT V80205 001
used on 090A
44 200A A5217026320200 .. PLATE-LOCKING VFAPE3 001
used on 090A
44 210A D5237146120200 .. BOLT VFAPE3 001
used on 090A
44 220A NAS1149C0432R . WASHER V80205 001
C5729
used on 001A
44 230A D5237145821000 . BUSHING VFAPE3 001
used on 001A
44 240A NSA5059E4 . NUT VF5442 001
OPT TO 73783CM8-428 56878
F0188
used on 001A
44 250A NAS1304-23D . BOLT V80205 001
NAS6604D23 80205
used on 001A
44 260A NAS1306-22D . BOLT V80205 001
NAS6606D22 80205
C5729, F0188, K8753
used on 001A
44 270A D5237145821200 . BUSHING VFAPE3 001
used on 001A
44 280A MS24665-300 . PIN-COTTER V96906 001
8K160, C5543, C5729
used on 001A
Page 10044-2
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
44 290A NSA5059E6 . NUT VF5442 001
OPT TO 73783CM8-624 56878
F0188
used on 001A
44 300A NAS1149C0663R . WASHER V80205 002
70347, 8K160, C5543, C5729
used on 001A
Page 10044-3
52-31-17 Jul 01/11
@AIRBUS
D5237300000000
A
40
50
20
30
80
70
50
60
90
90
100
120
130 110
10
120
F_PL_523117_50_0_01_00
HOUSING-VALVE
Figure 50 / FIGURE-52-31-17-950-850-01
Page 10050-0
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
50 - 001A D5237300000061 HOUSING-VALVE VFAPE3 RF
used on 050A (523117010)
SEE 52-31-17-010 FOR NHA
50 - 001B D5237300000061 HOUSING-VALVE VFAPE3 RF
used on 050B (523117010)
SEE 52-31-17-010 FOR NHA
50 - 001C D5237300000061 HOUSING-VALVE VFAPE3 RF
used on 051A (523117010)
POST SB 52-1124
SEE 52-31-17-010 FOR NHA
50 010A DAN79-07 . HOSE VFAPE3 001
REQUIRED LENGTH 400 MM
Optional Vendor Code C5543
used on 001A, 001B, 001C
50 020A ABS0341-1-01 . RETAINER-VALVE VFAPE3 001
OPT TO 140N2021-1H 57336
used on 001A, 001B, 001C
50 030A ABS0341-2-01 . VALVE-BASIC VFAPE3 001
OPT TO 140N2022S2 57336
used on 001A
50 030B ABS0341-2-02 . VALVE VFAPE3 001
OPT TO 140N2022S1 57336
used on 001B
50 - 031A ABS0341-2-02 . VALVE VFAPE3 002
OPT TO 140N2022S1 57336
used on 001C
POST SB 52-1124
50 040A NAS1100E08-12 . SCREW V80205 002
used on 001A, 001B, 001C
50 050A NAS1149CN832R . WASHER V80205 004
OPT TO 7283A04-230 B0014
C5729
used on 001A, 001B, 001C
Page 10050-1
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
50 060A NAS1291C08M . NUT V80205 002
OPT TO 180003-08 60119
OPT TO FN1014M832 56878
OPT TO H42L08 K6405
OPT TO RMLH3858-82 72962
OPT TO T99C832M 11815
OPT TO VN300D82 92215
C5543, C5729, H2776
used on 001A, 001B, 001C
50 070A D5237127320000 . FLANGE VFAPE3 001
used on 001A, 001B, 001C
50 080A D5237127200000 . TUBE ASSY VFAPE3 001
used on 001A, 001B, 001C
50 090A NSA935401-04 . TIE-CABLE VF5442 002
OPT TO 32015 F2693
OPT TO 32254 F2693
OPT TO PLT1-5I30 06383
OPT TO SST1-5I30 06383
OPT TO T30RHS D8527
used on 001A, 001B, 001C
50 100A NSA935504-01 . MOUNT VF5442 001
OPT TO 00326110059 F0394
Optional Vendor Code 04795, 42C51, C5543, C5729
used on 001A, 001B, 001C
50 110A NAS1303-3 . BOLT V80205 001
NAS6603-3 80205
used on 001A, 001B, 001C
50 120A NAS1149C0332R . WASHER V80205 002
C5543, C5729
used on 001A, 001B, 001C
50 130A NAS1291C3M . NUT V80205 001
OPT TO H42-3 15653
F0224
used on 001A, 001B, 001C
Page 10050-2
52-31-17 Jul 01/11
@AIRBUS
D5237300000000
20
A A
230
240
50
B
10
280
B C
300
280 200
270
280 190
210
220
60 220
G C 240
290
300 260 250
290
290
E
300 D 300
300
F
150
110
310
320 140
F G 184
110 F
182
D E
120 F 80
170 G
80 G D
70
180 E
F_PL_523117_60_0_01_00
ELECTRICAL SYSTEM
Figure 60 / FIGURE-52-31-17-950-860-01
Page 10060-0
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
60 - 001A D9209031103061 ELECTRICAL SYSTEM VFAPE3 RF
used on 060A (523117010)
SEE 52-31-17-010 FOR NHA
60 - 001B D9209031103061 ELECTRICAL SYSTEM VFAPE3 RF
used on 060B (523117010)
SEE 52-31-17-010 FOR NHA
60 010A D9299741100000 . HARNESS-CABLE,4611VB VFAPE3 001
used on 001A, 001B
60 020A EN2997SE61624AN .. CONNECTOR-PLUG VI9005 001
EN2997SE61624CN I9005
OPT TO 6TBD100550 14283
OPT TO 85333ES16-24PNL F0225
OPT TO 9836SE16-24PNL F1983
OPT TO E0442SE16-24PNA F5442
used on 010A
60 - 030A EN3155-018M2018 .. CONTACT VI9005 014
OPT TO 006-0044-20A F1983
OPT TO 050-0001-2018 14283
OPT TO 330-7587-000 F3132
OPT TO 8522-2349A F0225
OPT TO B6320 S5540
used on 010A
60 - 040A E0616BB2000 .. PLUG-SEALING VF5442 010
OPT TO 8522-389A F0225
OPT TO NSA938153BB2000 F5442
OPT TO SB2034 F0225
used on 010A
60 050A E0115A12-16-3 .. ELBOW VF5442 001
OPT TO T9312-12 K0685
used on 010A
60 - 052A NSA935401-03 .. TIE-CABLE VF5442 010
OPT TO 32012 F2693
OPT TO 32251 F2693
OPT TO PLT1M30 06383
OPT TO SST1M30 06383
OPT TO T18RHS D8527
Page 10060-1
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
D8527
used on 010A
60 - 054A DAN79-05 .. HOSE VFAPE3 AR
Optional Vendor Code C4344, C5543
used on 010A
60 060A D9299741000000 . HARNESS-CABLE,4610VB VFAPE3 001
used on 001A, 001B
60 070A E0052R8B3ASNE .. CONNECTOR-PLUG VF5442 001
OPT TO 1260A11-8-3ASN F6162
OPT TO 1260A11-8-98SDN F6162
OPT TO 6TBD101465 F0225
OPT TO 6TBD101466 F1983
OPT TO 7TBD101554 F1983
OPT TO 7TBD102262 F0225
OPT TO E0052R8B98SNE F5442
OPT TO EN3646A6083ADN I9005
OPT TO MBL16A8-3AS 14283
OPT TO MBL16A8-98S F8612
OPT TO PVW6R8-3ASN57 F3132
OPT TO PVW6R8-98SN57 F3132
used on 060A
60 080A ABS0638B08 .. BACKSHELL-CONNECTOR VFAPE3 003
OPT TO GK5440 C3471
used on 060A
60 - 090A NSA938152SA2000 .. CONTACT-SOCKET VF5442 006
EN3155-019F2018 I9005
OPT TO 004-0142-20 F1983
OPT TO 006-0055-20A F1983
OPT TO 031-7741-000 F3132
OPT TO 050-1001-2018 14283
OPT TO 0603-34-2031 F1983
OPT TO 6TBD100463 49367
OPT TO 8520-292 F0225
OPT TO DF06A055-20B F1983
Optional Vendor Code 04795, 14283, C5543, C5729
used on 060A
Page 10060-2
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
60 - 100A E0616BB2000 .. PLUG-SEALING VF5442 024
OPT TO 8522-389A F0225
OPT TO NSA938153BB2000 F5442
OPT TO SB2034 F0225
used on 060A
60 110A ABS0638A08 .. BACKSHELL-CONNECTOR VFAPE3 003
OPT TO GK5430 C3471
used on 060A
60 120A E0073-8-3AT .. SEAL-PRESSURE VF5442 001
OPT TO DTP07-8-3AK F1983
OPT TO PVW77-8-98-57 K0316
used on 060A
60 - 130A NSA934701BU2000 .. PLUG-BLIND VF5442 002
OPT TO DF90-006-20 F1983
Optional Vendor Code D8518
used on 060A
60 140A A5217240234400 .. WASHER-SPECIAL VFAPE3 002
used on 060A
60 - 142A NSA935401-03 .. TIE-CABLE VF5442 030
OPT TO 32012 F2693
OPT TO 32251 F2693
OPT TO T18RHS D8527
D8527
used on 060A
60 150A D9269000400200 .. BLOCK-TERMINAL VFAPE3 001
used on 060A
SEE 52-31-17-630 FOR DET
Page 10060-3
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
60 - 160A NSA937910EA2000 .. CONTACT-PIN VF5442 004
OPT TO 001104-200-02 F0394
OPT TO 001104-210-02 F0394
OPT TO 020-0008-20 F1983
OPT TO 1104A20 F0394
OPT TO 123-0001-20 F1983
OPT TO 1841-1-5620 F1983
OPT TO 8550-239A F0225
OPT TO EN3155-016M2018 I9005
OPT TO SB2029 F0225
F0394, F1983
used on 060A
60 170A E0073-8-3AT .. SEAL-PRESSURE VF5442 001
OPT TO DTP07-8-3AK F1983
OPT TO PVW77-8-98-57 K0316
used on 060A
60 180A E0052R8B3ASNE .. CONNECTOR-PLUG VF5442 001
OPT TO 1260A11-8-3ASN F6162
OPT TO 1260A11-8-98SDN F6162
OPT TO 6TBD101465 F0225
OPT TO 6TBD101466 F1983
OPT TO 7TBD101554 F1983
OPT TO 7TBD102262 F0225
OPT TO E0052R8B98SNE F5442
OPT TO EN3646A6083ADN I9005
OPT TO MBL16A8-3AS 14283
OPT TO MBL16A8-98S F8612
OPT TO PVW6R8-3ASN57 F3132
OPT TO PVW6R8-98SN57 F3132
used on 060A
60 182A D9249550220000 .. WASHER VFAPE3 002
used on 060A
60 184A D9249550120000 .. PLATE-MOUNTING VFAPE3 002
used on 060A
60 - 186A NSA935805-04 .. ELECTRICAL CONDUIT VF5442 AR
INSTALLATION
Page 10060-4
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
OPT TO C10000-0-0-08 81482
OPT TO GC100-04 F0564
OPT TO SC001-0-0-04 K0685
OPT TO SF001-00-00-04 F6101
Optional Vendor Code C5543
used on 060A
60 190A NSA935807-12 . CLAMP VF5442 001
OPT TO 50011-12 F6101
F0355
used on 001A, 001B
60 200A NSA5527-03-03 . SPACER VF5442 001
used on 001A, 001B
60 210A NAS1096-2-29 . SCREW V80205 001
NAS1801-08-29 80205
K8753
used on 001A, 001B
60 220A NAS1149DN816K . WASHER V80205 003
C5729
used on 001A, 001B
60 230A NSA935808-01 . WASHER VF5442 001
OPT TO 3732-109 C7100
OPT TO 50012-1-31 F6101
OPT TO 715120001 F0355
used on 001A, 001B
60 240A MS21042L08 . NUT V96906 003
OPT TO AS8600C K4975
OPT TO BH21042L08 27238
OPT TO EH14L08 15653
OPT TO H14L08 15653
OPT TO RH30A08 52828
OPT TO RM52LH3324-82 72962
OPT TO T98S832 11815
OPT TO VN300A82 92215
8K160, C5543, C5729
used on 001A, 001B
Page 10060-5
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
60 250A NSA5527-03-01 . SPACER VF5442 002
Optional Vendor Code F8982
used on 001A, 001B
60 260A NAS1096-2-14 . SCREW V80205 002
NAS1801-08-14 80205
K8753
used on 001A, 001B
60 270A NSA935513-07 . MOUNT VF5442 001
OPT TO TY5K7HS D8527
used on 001A, 001B
60 280A NSA935513-05 . MOUNT VF5442 010
used on 001A, 001B
60 290A NSA935513-01 . MOUNT-CABLE VF5442 007
OPT TO TY5K1HSNAT K0720
used on 001A, 001B
60 300A NSA931025-03A . LABEL VF5442 005
F0347, F4240
used on 001A, 001B
60 310A NAS1100-08-8 . SCREW V80205 004
used on 001A, 001B
60 320A NAS1149CN832R . WASHER V80205 004
OPT TO 7283A04-230 B0014
C5729
used on 001A, 001B
60 - 330A D9239125400460 . SENSOR INSTL-DOOR VFAPE3 001
used on 001A
SEE 52-31-17-620 FOR DET
60 - 330B D9239125400460 . SENSOR INSTL-DOOR VFAPE3 001
used on 001B
SEE 52-31-17-620 FOR DET
Page 10060-6
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
60 - 340A NSA935401-03 . TIE-CABLE VF5442 050
OPT TO 32012 F2693
OPT TO 32251 F2693
OPT TO T18RHS D8527
D8527
used on 001A, 001B
Page 10060-7
52-31-17 Jul 01/11
@AIRBUS
D5237300000000
B
C A
A
20
50 50
C 60 60
10
40
40
50
60
B
10
20
30
30
40
50 20
60
F_PL_523117_62_0_01_00
SENSOR INSTL-DOOR
Figure 62 / FIGURE-52-31-17-950-862-01
Page 10062-0
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
62 - 001A D9239125400460 SENSOR INSTL-DOOR VFAPE3 RF
used on 330A (523117600)
SEE 52-31-17-600 FOR NHA
62 - 001B D9239125400460 SENSOR INSTL-DOOR VFAPE3 RF
used on 330B (523117600)
SEE 52-31-17-600 FOR NHA
62 010A 8-484-01 . SENSOR-PROXIMITY,RECTANGULAR V08748 002
REPLACED BY PN 8-933-01
8-933-01 08748
OPT TO 666000077 K0654
OPT TO ABS0121-10 FAPE3
used on 001A
REFER TO SIL 32-093
62 010B 8-933-01 . SENSOR-PROXIMITY,RECTANGULAR V08748 002
OPT TO 201655069 K0654
OPT TO H10468642SC U7388
used on 001B
62 020A 8-368-04 . TARGET V08748 003
OPT TO 666000078 K0654
used on 001A, 001B
62 030A NAS1096-3-8 . SCREW V80205 004
NAS1801-3-8 80205
F7411, K8753
used on 001A, 001B
62 040A NAS1096-3-7 . SCREW V80205 006
NAS1801-3-7 80205
Optional Vendor Code F0188, K8753
used on 001A, 001B
62 050A NAS1149C0332R . WASHER V80205 008
C5543, C5729
used on 001A, 001B
62 060A NAS1291C3M . NUT V80205 008
OPT TO H42-3 15653
F0224
Page 10062-1
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
used on 001A, 001B
Page 10062-2
52-31-17 Jul 01/11
@AIRBUS
D5237300000000
20
40
30
20
10
F_PL_523117_63_0_01_00
BLOCK-TERMINAL
Figure 63 / FIGURE-52-31-17-950-863-01
Page 10063-0
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
63 - 001A D9269000400200 BLOCK-TERMINAL VFAPE3 RF
used on 150A (523117600)
SEE 52-31-17-600 FOR NHA
63 010A NSA937901RB0100 . RAIL VF5442 001
F1983
used on 001A
63 020A NSA937901S . END-CLAMPS VF5442 002
OPT TO 00110201060 F0394
OPT TO 020-0020-00 F1983
used on 001A
63 030A NSA937901M20-01 . MODULE VF5442 002
OPT TO 00111520103 F0394
OPT TO 208-2B01 F4250
OPT TO 8559E2001 F0225
OPT TO FMJ11E20-01K F1983
used on 001A
63 040A NSA937901M20-09 . MODULE VF5442 002
OPT TO 00111520903 F0394
OPT TO 208-2B09 F4250
OPT TO 8559E2009 F0225
OPT TO FMJ11E20-09K F1983
used on 001A
Page 10063-1
52-31-17 Jul 01/11
@AIRBUS
D5237300000000
30
50 40
C A 190
200
120
150
120
A 120 180 170
B
210
70
130
140 100
C
70
140
130
160 90
140
110
80
90
80 140
90 100 90
160
110
10
64 66
20
90
B
110 60
210
62 200 170
70
90
110
140
160 100
140
160
80
90
90
110
F_PL_523117_90_0_01_00
HINGE INSTL
Figure 90 / FIGURE-52-31-17-950-890-01
Page 10090-0
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
90 - 001A D5237301000061 HINGE INSTL VFAPE3 RF
used on 010A (523117040)
SEE 52-31-17-040 FOR NHA
90 010A D5237114720500 . FITTING-END VFAPE3 001
used on 001A
90 020A D5237120220600 . SHIM VFAPE3 001
used on 001A
90 030A D5237114001500 . HINGE ASSY VFAPE3 001
used on 001A
90 040A D5237114120900 .. HINGE-OUTER VFAPE3 001
used on 030A
90 050A D5237113820600 .. BUSHING VFAPE3 005
used on 030A
used on 001A
90 062A D5237303320100 .. HINGE-INNER VFAPE3 001
used on 060A
90 064A D5237113820600 .. BUSHING VFAPE3 008
used on 060A
used on 060A
90 070A NSA5030-3-9 . SCREW VF5442 012
ASNA2001V3-9 F5442
F0188, F6167, F7411, K5673, K8753
used on 001A
90 080A NAS1149C0363R . WASHER V80205 012
8K160, C5543, C5729
used on 001A
90 090A NAS1291C3M . NUT V80205 035
OPT TO H42-3 15653
F0224
used on 001A
90 100A NSA5030-3-8 . SCREW VF5442 012
ASNA2001V3-8 F5442
F0188, F6167, F7411, K5673, K8753
used on 001A
Page 10090-1
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
90 110A NAS1149C0332R . WASHER V80205 023
C5543, C5729
used on 001A
90 120A NSA5030-4-9 . SCREW VF5442 005
ASNA2001V4-9 F5442
F0188, F6167, F7411, K5673, K8753
used on 001A
90 130A NAS1149C0432R . WASHER V80205 008
C5729
used on 001A
90 140A NAS1291C4M . NUT V80205 020
OPT TO 180003-5 60119
used on 001A
90 150A NSA5030-4-11 . SCREW VF5442 001
ASNA2001V4-11 F5442
F0188, F6167, F7411, K5673, K8753
used on 001A
90 160A NAS1149C0463R . WASHER V80205 012
C5729
used on 001A
90 170A NSA5030-4-12 . SCREW VF5442 008
ASNA2001V4-12 F5442
F0188, F6167, F7411, K5673, K8753
used on 001A
90 180A NSA5030-4-10 . SCREW VF5442 001
ASNA2001V4-10 F5442
F0188, F6167, F7411, K5673, K8753
used on 001A
90 190A NSA5030-4-8 . SCREW VF5442 001
ASNA2001V4-8 F5442
F0188, F6167, F7411, K5673, K8753
used on 001A
Page 10090-2
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
90 200A NAS1154-11 . SCREW V80205 004
used on 001A
90 210A NSA5030-3-7 . SCREW VF5442 011
ASNA2001V3-7 F5442
F0188, F6167, F7411, K5673, K8753
used on 001A
90 - 220A D52373010000CTD . STRUCTURE-DOOR VFAPE3 001
used on 001A
SEE 52-31-17-910 FOR DET
Page 10090-3
52-31-17 Jul 01/11
@AIRBUS
D5237300000000
16
A
210
150
120
A 180
B
C
90 70
110 14
10
130
140 100
12
130
140
80
90
90
C 70 110
20 B
40 30
200
190 70
100 100
170
210 120
80 120
90 150
120
180
60
50
90 90
110 110
140
80 160
90
130
140
90
110
140 130
160 140
F_PL_523117_91_0_01_00
STRUCTURE-DOOR
Figure 91 / FIGURE-52-31-17-950-891-01
Page 10091-0
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
91 - 001A D52373010000CTD STRUCTURE-DOOR VFAPE3 RF
used on 220A (523117900)
SEE 52-31-17-900 FOR NHA
used on 001A
91 012A D5237303320000 .. HINGE-MID VFAPE3 001
used on 010A
91 014A D5237113820600 .. BUSHING VFAPE3 008
used on 010A
used on 010A
used on 001A
91 030A D5237114120800 .. HINGE-OUTER VFAPE3 001
used on 020A
91 040A D5237113820600 .. BUSHING VFAPE3 005
used on 020A
91 050A D5237120220600 . SHIM VFAPE3 001
used on 001A
91 060A D5237114720400 . FITTING-END VFAPE3 001
used on 001A
91 070A NSA5030-3-9 . SCREW VF5442 012
ASNA2001V3-9 F5442
F0188, F6167, F7411, K5673, K8753
used on 001A
91 080A NAS1149C0363R . WASHER V80205 012
8K160, C5543, C5729
used on 001A
91 090A NAS1291C3M . NUT V80205 035
OPT TO H42-3 15653
F0224
used on 001A
91 100A NSA5030-3-8 . SCREW VF5442 012
ASNA2001V3-8 F5442
F0188, F6167, F7411, K5673, K8753
used on 001A
Page 10091-1
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
91 110A NAS1149C0332R . WASHER V80205 023
C5543, C5729
used on 001A
91 120A NSA5030-4-9 . SCREW VF5442 007
ASNA2001V4-9 F5442
F0188, F6167, F7411, K5673, K8753
used on 001A
91 130A NAS1149C0432R . WASHER V80205 014
C5729
used on 001A
91 140A NAS1291C4M . NUT V80205 020
OPT TO 180003-5 60119
used on 001A
91 150A NSA5030-4-11 . SCREW VF5442 003
ASNA2001V4-11 F5442
F0188, F6167, F7411, K5673, K8753
used on 001A
91 160A NAS1149C0463R . WASHER V80205 006
C5729
used on 001A
91 170A NSA5030-4-12 . SCREW VF5442 004
ASNA2001V4-12 F5442
F0188, F6167, F7411, K5673, K8753
used on 001A
91 180A NSA5030-4-10 . SCREW VF5442 003
ASNA2001V4-10 F5442
F0188, F6167, F7411, K5673, K8753
used on 001A
91 190A NSA5030-4-8 . SCREW VF5442 001
ASNA2001V4-8 F5442
F0188, F6167, F7411, K5673, K8753
used on 001A
Page 10091-2
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
91 200A NAS1154-11 . SCREW V80205 002
used on 001A
91 210A NSA5030-3-7 . SCREW VF5442 011
ASNA2001V3-7 F5442
F0188, F6167, F7411, K5673, K8753
used on 001A
Page 10091-3
52-31-17 Jul 01/11
@AIRBUS
D5237300000000
001A
10A 30 40 20A
50 50
001B
10B 30 40 20B
50 50
001C
10C 20C
001D
10D 20D
F_PL_523117_95_0_01_00
ROD ASSY
Figure 95 / FIGURE-52-31-17-950-895-01
Page 10095-0
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
95 - 001A R24359 ROD ASSY VB1395 RF
OPT TO D5237176820000 FAPE3
OPT TO D5237176820200 FAPE3
used on 160B (523117080)
SEE 52-31-17-080 FOR NHA
95 - 001B R24358 ROD ASSY VB1395 RF
OPT TO D5237176720000 FAPE3
OPT TO D5237176720200 FAPE3
OPT TO D5237176720400 FAPE3
used on 600B (523117080)
SEE 52-31-17-080 FOR NHA
95 - 001C R25259 ROD ASSY VB1395 RF
used on 080B (523117130)
SEE 52-31-17-130 FOR NHA
95 - 001D R24365 ROD ASSY VB1395 RF
used on 210B (523117400)
SEE 52-31-17-400 FOR NHA
95 010A E5072-4SL5K111 . ROD END VB1395 001
used on 001A
95 010B E5990-4SL5K111 . ROD END VB1395 001
used on 001B
95 010C E4143 . ROD END VB1395 001
used on 001C
95 010D E4116-4S5-111 . CLEVIS VB1395 001
used on 001D
95 020A E5072-4S5K111 . ROD END VB1395 001
used on 001A
95 020B E5990-4S5K111 . ROD END VB1395 001
used on 001B
95 020C E4144 . ROD END VB1395 001
used on 001C
95 020D E4116-4S5-111 . CLEVIS VB1395 001
used on 001D
95 030A NAS509L5C . NUT V80205 001
8K160, 92595, C5543, C5729
used on 001A, 001B
95 040A NAS509-5C . NUT V80205 001
used on 001A, 001B
Page 10095-1
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
95 050A NAS1193K5C . LOCKING DEVICE V80205 002
C5543, C5729, H2776
used on 001A, 001B
Page 10095-2
52-31-17 Jul 01/11
@AIRBUS
D5237300000000
D A B
40 A
C 120 B
80 A 60 A
140 B
B A
70 20 A
A
B
150 100 B
30 A
110 B
E A
50 40 A
B
130 120 B
20 A
100 B
160 C
200
D 180
160
F_PL_523117_96_0_01_00
BUSHING INSTL-DOOR STRUCTURE

Figure 96 / FIGURE-52-31-17-950-896-01
Page 10096-0
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
96 - 001A D5237301000063 BUSHING INSTL-DOOR STRUCTURE VFAPE3 RF
used on 040A (523117040)
SEE 52-31-17-040 FOR NHA
96 - 010A D5237302000060 . FRAME ASSY-FR25 (NP) 001
used on 001A
96 020A D5237112920200 .. BUSHING VFAPE3 002
used on 001A
used on 001A
used on 001A
96 050A D5237112820200 .. BUSHING VFAPE3 001
used on 001A
used on 001A
used on 001A
used on 001A
96 - 090A D5237302100060 . FRAME ASSY-FR25A (NP) 001
used on 001A
96 100A D5237112920200 .. BUSHING VFAPE3 002
used on 001A
used on 001A
used on 001A
96 130A D5237112820200 .. BUSHING VFAPE3 001
used on 001A
used on 001A
used on 001A
96 160A D5237112720000 .. BUSHING VFAPE3 002
used on 001A
96 - 170A D5237303700060 . BEAM-CTR,4 (NP) 001
used on 001A
96 180A NSA5054-3 .. INSERT VF5442 004
OPT TO K8000-3 K6405
OPT TO M45932-1-9AL 81349
used on 001A
Page 10096-1
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
96 - 190A D5237171800060 . BEAM-CTR,3E (NP) 001
used on 001A
used on 001A
96 - 210A D5237301000064 . BUSHING INSTL-DOOR STRUCTURE VFAPE3 001
used on 001A
SEE 52-31-17-970 FOR DET
Page 10096-2
52-31-17 Jul 01/11
@AIRBUS
D5237300000000
A B
150 B
40 A
C 110 B
D
60 A
130 B
B
A
70 A 20 A
140 B 90 B
30 A
100 B
50 A 40 A
120 B 110 B
20 A
90 B
D
210
C
200
230
170
190
240
F_PL_523117_97_0_01_00
BUSHING INSTL-DOOR STRUCTURE

Figure 97 / FIGURE-52-31-17-950-897-01
Page 10097-0
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
97 - 001A D5237301000064 BUSHING INSTL-DOOR STRUCTURE VFAPE3 RF
used on 210A (523117960)
SEE 52-31-17-960 FOR NHA
97 - 010A D5237302200060 . FRAME ASSY-FR26 (NP) 001
used on 001A
97 020A D5237112920200 .. BUSHING VFAPE3 002
used on 001A
used on 001A
used on 001A
97 050A D5237112820200 .. BUSHING VFAPE3 001
used on 001A
used on 001A
used on 001A
97 - 080A D5237302300060 . FRAME ASSY-FR26A (NP) 001
used on 001A
97 090A D5237112920200 .. BUSHING VFAPE3 002
used on 001A
used on 001A
used on 001A
97 120A D5237112820200 .. BUSHING VFAPE3 001
used on 001A
used on 001A
used on 001A
97 150A D5237179320000 .. BUSHING VFAPE3 001
used on 001A
97 - 160A D5237174700060 . SEGMENT-FRAME,FWD (NP) 001
used on 001A
used on 001A
97 - 180A D5237174800060 . SEGMENT-FRAME,AFT (NP) 001
used on 001A
used on 001A
Page 10097-1
52-31-17 Jul 01/11
@AIRBUS
D5237300000000

1234567 FROM PER
TO ASSY
used on 001A
97 210A NSA5054-3 .. INSERT VF5442 002
OPT TO K8000-3 K6405
OPT TO M45932-1-9AL 81349
used on 001A
97 - 220A D5237174200260 . BEAM-4 (NP) 001
used on 001A
97 230A D5237178720000 .. BUSH-GUIDE VFAPE3 001
used on 001A
97 240A NSA5054-3 .. INSERT VF5442 001
OPT TO K8000-3 K6405
OPT TO M45932-1-9AL 81349
used on 001A
Page 10097-2
52-31-17 Jul 01/11

@airbus: Component Maintenance Manual With Illustrated Part List

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@AIRBUS

COMPONENT MAINTENANCE MANUAL

FWD CARGO COMPARTMENT DOOR

Issue: Nov 01/02 52-31-17 Rev: Jul 01/11

Revision No. 9 - Jul 01/11

LOCATIONS CHG DESCRIPTIONS OF CHANGE

LIST OF EFFECTIVE CONTENT

Revision No. 9 - Jul 01/11

CONTENT CHG LAST REVISION

DESCRIPTION AND OPERATION

TESTING AND FAULT ISOLATION

SCHEMATIC AND WIRING DIAGRAMS

CONTENT CHG LAST REVISION

CONTENT CHG LAST REVISION

CONTENT CHG LAST REVISION

CONTENT CHG LAST REVISION

CONTENT CHG LAST REVISION

CONTENT CHG LAST REVISION

FITS AND CLEARANCES

SPECIAL TOOLS,FIXTURES,EQUIPMENT AND CONSUMABLES

STORAGE INCLUDING TRANSPORTATION

ILLUSTRATED PARTS LIST

CONTENT CHG LAST REVISION

CONTENT CHG LAST REVISION

CONTENT CHG LAST REVISION

DESCRIPTION AND OPERATION

TESTING AND FAULT ISOLATION

SCHEMATIC AND WIRING DIAGRAMS

52-31-17-400-817-A01 Installation of the Hinge Assemblies

FITS AND CLEARANCES

SPECIAL TOOLS,FIXTURES,EQUIPMENT AND CONSUMABLES

STORAGE INCLUDING TRANSPORTATION

ILLUSTRATED PARTS LIST

LIST OF SERVICE BULLETINS

SB No REV No MOD No INCORP. TITLE

**For PN’s ALL

FIN Functional Item Number

DESCRIPTION AND OPERATION

**For PN’s ALL

**For PN’s ALL

- the interlock mechanism.

(5) Vent Door Mechanism

NOTE : For data of the proximity switches refer to CMMV 32-10-03.

**For PN’s ALL

FWD Cargo Compartment Door

**For PN’s ALL

FWD Cargo Compartment Door

**For PN’s ALL

Electrical Equipment Installation

**For PN’s ALL

**For PN’s ALL

FWD Cargo Compartment Door

**For PN’s ALL

FWD Cargo Compartment Door

TESTING AND FAULT ISOLATION

**For PN’s ALL

NOTE : Refer to FIGURE 52-31-17-991-006-A and TASK 52-31-17-878-805-A01.

(c) Move the switch S6 in the OFF position.