@AIRBUS

AIRBUS S.A.S.
Customer Services
Technical Data Support and Services
31707 Blagnac Cedex
FRANCE

FAPE3

COMPONENT MAINTENANCE MANUAL

WITH
ILLUSTRATED PART LIST

AFT CARGO COMP DOOR

PN : D5237310000000
D5237310000200
D5237310000400
D5237310000600
D5237310000800
D5237310001000
D5237310001200
D5237310001400
D5237310002000

Issue: Nov 01/02 52-32-17 Rev: Jul 01/16

 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

HIGHLIGHTS

Revision No. 11 - Jul 01/16

LOCATIONS CHG DESCRIPTIONS OF CHANGE

CODE

HIGHLIGHTS
Page 1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

LIST OF EFFECTIVE CONTENT

Revision No. 11 - Jul 01/16

CONTENT CHG LAST REVISION

CODE DATE
INTRODUCTION
TASK 52-32-17-871-802-A01 Jul 01/16

DESCRIPTION AND OPERATION

TASK 52-32-17-870-803-A01 Jul 01/16
TASK 52-32-17-870-804-A01 Jul 01/16
FIGURE 52-32-17-991-001-A01 Jul 01/16
FIGURE 52-32-17-991-002-A01 Jul 01/16
FIGURE 52-32-17-991-003-A01 Jul 01/16
TASK 52-32-17-870-805-A01 Jul 01/16
FIGURE 52-32-17-991-004-A01 Jul 01/16
FIGURE 52-32-17-991-005-A01 Jul 01/16

TESTING AND FAULT ISOLATION

TASK 52-32-17-700-801-A01 Jul 01/16
Subtask 52-32-17-700-001-A01 Jul 01/16
Subtask 52-32-17-700-002-A01 Jul 01/16
Subtask 52-32-17-810-001-A01 Jul 01/16
Subtask 52-32-17-700-003-A01 Jul 01/16
FIGURE 52-32-17-991-006-A01 Jul 01/16

SCHEMATIC AND WIRING DIAGRAMS

TASK 52-32-17-878-806-A01 Jul 01/16
FIGURE 52-32-17-991-007-A01 Jul 01/16

DISASSEMBLY
TASK 52-32-17-000-801-A01 Jul 01/16
Subtask 52-32-17-000-001-A01 Jul 01/16
TASK 52-32-17-000-802-A01 Jul 01/16

L.E.C.
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COMPONENT MAINTENANCE MANUAL
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CONTENT CHG LAST REVISION

CODE DATE
Subtask 52-32-17-000-002-A01 Jul 01/16
TASK 52-32-17-000-803-A01 Jul 01/16
Subtask 52-32-17-000-003-A01 Jul 01/16
TASK 52-32-17-000-804-A01 Jul 01/16
Subtask 52-32-17-000-004-A01 Jul 01/16
TASK 52-32-17-000-805-A01 Jul 01/16
Subtask 52-32-17-000-005-A01 Jul 01/16
TASK 52-32-17-000-806-A01 Jul 01/16
Subtask 52-32-17-000-006-A01 Jul 01/16
TASK 52-32-17-000-807-A01 Jul 01/16
Subtask 52-32-17-000-007-A01 Jul 01/16
TASK 52-32-17-000-808-A01 Jul 01/16
Subtask 52-32-17-000-008-A01 Jul 01/16
TASK 52-32-17-000-808-B01 Jul 01/16
Subtask 52-32-17-000-019-A01 Jul 01/16
TASK 52-32-17-000-808-C01 Jul 01/16
Subtask 52-32-17-000-020-A01 Jul 01/16
TASK 52-32-17-000-809-A01 Jul 01/16
Subtask 52-32-17-000-009-A01 Jul 01/16
TASK 52-32-17-000-810-A01 Jul 01/16
Subtask 52-32-17-000-010-A01 Jul 01/16
TASK 52-32-17-000-811-A01 Jul 01/16
Subtask 52-32-17-000-011-A01 Jul 01/16
TASK 52-32-17-000-812-A01 Jul 01/16
Subtask 52-32-17-000-012-A01 Jul 01/16
TASK 52-32-17-000-813-A01 Jul 01/16
Subtask 52-32-17-000-013-A01 Jul 01/16
TASK 52-32-17-000-813-B01 Jul 01/16
Subtask 52-32-17-000-026-A01 Jul 01/16

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COMPONENT MAINTENANCE MANUAL
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CONTENT CHG LAST REVISION

CODE DATE
TASK 52-32-17-000-814-A01 Jul 01/16
Subtask 52-32-17-000-014-A01 Jul 01/16
TASK 52-32-17-000-815-A01 Jul 01/16
Subtask 52-32-17-000-015-A01 Jul 01/16
TASK 52-32-17-000-815-B01 Jul 01/16
Subtask 52-32-17-000-022-A01 Jul 01/16
TASK 52-32-17-000-815-C01 Jul 01/16
Subtask 52-32-17-000-023-A01 Jul 01/16
TASK 52-32-17-000-816-A01 Jul 01/16
Subtask 52-32-17-000-016-A01 Jul 01/16
TASK 52-32-17-000-817-A01 Jul 01/16
Subtask 52-32-17-000-017-A01 Jul 01/16
TASK 52-32-17-000-818-A01 Jul 01/16
Subtask 52-32-17-000-018-A01 Jul 01/16
Subtask 52-32-17-000-021-A01 Jul 01/16
TASK 52-32-17-000-818-B01 Jul 01/16
Subtask 52-32-17-000-024-A01 Jul 01/16
Subtask 52-32-17-000-025-A01 Jul 01/16

CLEANING
TASK 52-32-17-100-801-A01 Jul 01/16
Subtask 52-32-17-100-001-A01 Jul 01/16
Subtask 52-32-17-100-002-A01 Jul 01/16
Subtask 52-32-17-100-003-A01 Jul 01/16
Subtask 52-32-17-100-004-A01 Jul 01/16
Subtask 52-32-17-100-005-A01 Jul 01/16

INSPECTION/CHECK
TASK 52-32-17-200-801-A01 Jul 01/16
Subtask 52-32-17-210-001-A01 Jul 01/16

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COMPONENT MAINTENANCE MANUAL
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CONTENT CHG LAST REVISION

CODE DATE
Subtask 52-32-17-210-002-A01 Jul 01/16
Subtask 52-32-17-210-003-A01 Jul 01/16
Subtask 52-32-17-210-004-A01 Jul 01/16
FIGURE 52-32-17-991-008-A01 Jul 01/16
TASK 52-32-17-210-801-A01 Jul 01/16
Subtask 52-32-17-210-005-A01 Jul 01/16
Subtask 52-32-17-210-006-A01 Jul 01/16
Subtask 52-32-17-210-007-A01 Jul 01/16
FIGURE 52-32-17-991-009-A01 Jul 01/16
TASK 52-32-17-220-801-A01 Jul 01/16
Subtask 52-32-17-210-008-A01 Jul 01/16
TASK 52-32-17-210-802-A01 Jul 01/16
Subtask 52-32-17-210-009-A01 Jul 01/16
TASK 52-32-17-220-802-A01 Jul 01/16
Subtask 52-32-17-210-010-A01 Jul 01/16
FIGURE 52-32-17-991-010-A01 Jul 01/16

REPAIR
TASK 52-32-17-300-801-A01 Jul 01/16
Subtask 52-32-17-300-001-A01 Jul 01/16
Subtask 52-32-17-300-002-A01 Jul 01/16
Subtask 52-32-17-300-003-A01 Jul 01/16
FIGURE 52-32-17-991-011-A01 Jul 01/16
FIGURE 52-32-17-991-012-A01 Jul 01/16
FIGURE 52-32-17-991-013-A01 Jul 01/16
TASK 52-32-17-300-802-A01 Jul 01/16
Subtask 52-32-17-300-004-A01 Jul 01/16
Subtask 52-32-17-300-005-A01 Jul 01/16
Subtask 52-32-17-300-006-A01 Jul 01/16

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 @AIRBUS
COMPONENT MAINTENANCE MANUAL
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CONTENT CHG LAST REVISION

CODE DATE
TASK 52-32-17-300-803-A01 Jul 01/16
Subtask 52-32-17-300-007-A01 Jul 01/16
Subtask 52-32-17-300-008-A01 Jul 01/16
Subtask 52-32-17-300-009-A01 Jul 01/16
Subtask 52-32-17-300-012-A01 Jul 01/16
Subtask 52-32-17-300-013-A01 Jul 01/16
Subtask 52-32-17-300-014-A01 Jul 01/16
Subtask 52-32-17-300-015-A01 Jul 01/16
Subtask 52-32-17-300-016-A01 Jul 01/16
Subtask 52-32-17-300-017-A01 Jul 01/16

ASSEMBLY
TASK 52-32-17-400-801-A01 Jul 01/16
Subtask 52-32-17-400-001-A01 Jul 01/16
TASK 52-32-17-400-802-A01 Jul 01/16
Subtask 52-32-17-400-002-A01 Jul 01/16
TASK 52-32-17-400-803-A01 Jul 01/16
Subtask 52-32-17-400-003-A01 Jul 01/16
TASK 52-32-17-400-804-A01 Jul 01/16
Subtask 52-32-17-400-004-A01 Jul 01/16
TASK 52-32-17-400-805-A01 Jul 01/16
Subtask 52-32-17-400-005-A01 Jul 01/16
TASK 52-32-17-400-806-A01 Jul 01/16
Subtask 52-32-17-400-006-A01 Jul 01/16
TASK 52-32-17-400-807-A01 Jul 01/16
Subtask 52-32-17-400-007-A01 Jul 01/16
TASK 52-32-17-400-808-A01 Jul 01/16
Subtask 52-32-17-400-008-A01 Jul 01/16
TASK 52-32-17-400-808-B01 Jul 01/16

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 @AIRBUS
COMPONENT MAINTENANCE MANUAL
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CONTENT CHG LAST REVISION

CODE DATE
Subtask 52-32-17-400-026-A01 Jul 01/16
TASK 52-32-17-400-809-A01 Jul 01/16
Subtask 52-32-17-400-009-A01 Jul 01/16
TASK 52-32-17-400-810-A01 Jul 01/16
Subtask 52-32-17-400-010-A01 Jul 01/16
TASK 52-32-17-400-810-B01 Jul 01/16
Subtask 52-32-17-400-022-A01 Jul 01/16
TASK 52-32-17-400-810-C01 Jul 01/16
Subtask 52-32-17-400-023-A01 Jul 01/16
TASK 52-32-17-400-811-A01 Jul 01/16
Subtask 52-32-17-400-011-A01 Jul 01/16
TASK 52-32-17-400-811-B01 Jul 01/16
Subtask 52-32-17-400-019-A01 Jul 01/16
TASK 52-32-17-400-811-C01 Jul 01/16
Subtask 52-32-17-400-020-A01 Jul 01/16
TASK 52-32-17-400-812-A01 Jul 01/16
Subtask 52-32-17-400-012-A01 Jul 01/16
TASK 52-32-17-400-813-A01 Jul 01/16
Subtask 52-32-17-400-013-A01 Jul 01/16
TASK 52-32-17-400-814-A01 Jul 01/16
Subtask 52-32-17-400-014-A01 Jul 01/16
TASK 52-32-17-400-815-A01 Jul 01/16
Subtask 52-32-17-400-015-A01 Jul 01/16
TASK 52-32-17-400-816-A01 Jul 01/16
Subtask 52-32-17-400-016-A01 Jul 01/16
TASK 52-32-17-400-817-A01 Jul 01/16
Subtask 52-32-17-400-017-A01 Jul 01/16
Subtask 52-32-17-400-021-A01 Jul 01/16
TASK 52-32-17-400-817-B01 Jul 01/16

L.E.C.
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COMPONENT MAINTENANCE MANUAL
D5237310000000

CONTENT CHG LAST REVISION

CODE DATE
Subtask 52-32-17-400-024-A01 Jul 01/16
Subtask 52-32-17-400-025-A01 Jul 01/16
TASK 52-32-17-400-818-A01 Jul 01/16
Subtask 52-32-17-400-018-A01 Jul 01/16
TASK 52-32-17-800-801-A01 Jul 01/16
Subtask 52-32-17-820-001-A01 Jul 01/16
Subtask 52-32-17-820-002-A01 Jul 01/16
Subtask 52-32-17-820-003-A01 Jul 01/16
Subtask 52-32-17-820-004-A01 Jul 01/16
Subtask 52-32-17-820-005-A01 Jul 01/16
Subtask 52-32-17-820-006-A01 Jul 01/16
Subtask 52-32-17-820-007-A01 Jul 01/16
FIGURE 52-32-17-991-014-A01 Jul 01/16
FIGURE 52-32-17-991-015-A01 Jul 01/16
FIGURE 52-32-17-991-016-A01 Jul 01/16
FIGURE 52-32-17-991-017-A01 Jul 01/16
FIGURE 52-32-17-991-018-A01 Jul 01/16
FIGURE 52-32-17-991-019-A01 Jul 01/16
FIGURE 52-32-17-991-020-A01 Jul 01/16

FITS AND CLEARANCES

TASK 52-32-17-820-807-A01 Jul 01/16
TASK 52-32-17-820-808-A01 Jul 01/16
FIGURE 52-32-17-991-021-A01 Jul 01/16
FIGURE 52-32-17-991-022-A01 Jul 01/16
FIGURE 52-32-17-991-023-A01 Jul 01/16
FIGURE 52-32-17-991-024-A01 Jul 01/16

SPECIAL TOOLS,FIXTURES,EQUIPMENT AND CONSUMABLES

TASK 52-32-17-940-809-A01 Jul 01/16

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 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

CONTENT CHG LAST REVISION

CODE DATE
FIGURE 52-32-17-991-025-A01 Jul 01/16

STORAGE INCLUDING TRANSPORTATION

TASK 52-32-17-550-801-A01 Jul 01/16
Subtask 52-32-17-620-001-A01 Jul 01/16

ILLUSTRATED PARTS LIST

IPL Introduction
TASK 52-32-17-872-801-A01 Jul 01/16
VENDOR LIST Jul 01/16
Figure 01
FIGURE 52-32-17-991-801-001 Nov 01/08
Parts List Jul 01/16
Figure 02
FIGURE 52-32-17-991-802-001 Jul 01/16
Parts List Jul 01/16
Figure 03
FIGURE 52-32-17-991-803-001 Nov 01/08
Parts List Nov 01/08
Figure 04
FIGURE 52-32-17-991-804-001 Nov 01/08
Parts List Nov 01/08
Figure 05
FIGURE 52-32-17-991-805-001 Nov 01/08
Parts List Jul 01/16
Figure 08
FIGURE 52-32-17-991-808-001 Nov 01/08
Parts List Jul 01/16
Figure 09
FIGURE 52-32-17-991-809-001 Nov 01/08
Parts List Nov 01/08

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COMPONENT MAINTENANCE MANUAL
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CONTENT CHG LAST REVISION

CODE DATE
Figure 13
FIGURE 52-32-17-991-813-001 Nov 01/08
Parts List Nov 01/08
Figure 20
FIGURE 52-32-17-991-820-001 Nov 01/08
Parts List Nov 01/08
Figure 21
FIGURE 52-32-17-991-821-001 Nov 01/08
Parts List Nov 01/08
Figure 30
FIGURE 52-32-17-991-830-001 Nov 01/08
Parts List Jul 01/16
Figure 31
FIGURE 52-32-17-991-831-001 Nov 01/08
Parts List Jul 01/16
Figure 31A
FIGURE 52-32-17-991-831-A01 Nov 01/08
Parts List Jul 01/16
Figure 31B
FIGURE 52-32-17-991-831-B01 Jul 01/16
Parts List Jul 01/16
Figure 32
FIGURE 52-32-17-991-832-001 Nov 01/08
Parts List Nov 01/08
Figure 32A
FIGURE 52-32-17-991-832-A01 Nov 01/08
Parts List Nov 01/08
Figure 33
FIGURE 52-32-17-991-833-001 Nov 01/08

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COMPONENT MAINTENANCE MANUAL
D5237310000000

CONTENT CHG LAST REVISION

CODE DATE
Parts List Nov 01/08
Figure 34
FIGURE 52-32-17-991-834-001 Nov 01/08
Parts List Nov 01/08
Figure 40
FIGURE 52-32-17-991-840-001 Nov 01/08
Parts List Jul 01/16
Figure 41
FIGURE 52-32-17-991-841-001 Nov 01/08
Parts List Jul 01/16
Figure 41A
FIGURE 52-32-17-991-841-A01 Nov 01/08
Parts List Jul 01/16
Figure 41B
FIGURE 52-32-17-991-841-B01 Jul 01/16
Parts List Jul 01/16
Figure 44
FIGURE 52-32-17-991-844-001 Nov 01/08
Parts List Nov 01/08
Figure 50
FIGURE 52-32-17-991-850-001 Nov 01/08
Parts List Nov 01/08
Figure 60
FIGURE 52-32-17-991-860-001 Nov 01/08
Parts List Nov 01/08
Figure 62
FIGURE 52-32-17-991-862-001 Nov 01/08
Parts List Nov 01/08
Figure 63

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COMPONENT MAINTENANCE MANUAL
D5237310000000

CONTENT CHG LAST REVISION

CODE DATE
FIGURE 52-32-17-991-863-001 Nov 01/08
Parts List Nov 01/08
Figure 70
FIGURE 52-32-17-991-870-001 Nov 01/08
Parts List Nov 01/08
Figure 71
FIGURE 52-32-17-991-871-001 Nov 01/08
Parts List Nov 01/08
Figure 90
FIGURE 52-32-17-991-890-001 Nov 01/08
Parts List Nov 01/08
Figure 90A
FIGURE 52-32-17-991-890-A01 Nov 01/08
Parts List Nov 01/08
Figure 91
FIGURE 52-32-17-991-891-001 Nov 01/08
Parts List Nov 01/08
Figure 91A
FIGURE 52-32-17-991-891-A01 Nov 01/08
Parts List Nov 01/08
Figure 95
FIGURE 52-32-17-991-895-001 Nov 01/08
Parts List Nov 01/08
Figure 96
FIGURE 52-32-17-991-896-001 Nov 01/08
Parts List Nov 01/08
Figure 97
FIGURE 52-32-17-991-897-001 Nov 01/08
Parts List Nov 01/08

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COMPONENT MAINTENANCE MANUAL
D5237310000000

TABLE OF CONTENTS

INTRODUCTION
52-32-17-871-802-A01 Introduction

DESCRIPTION AND OPERATION

52-32-17-870-803-A01 General
52-32-17-870-804-A01 Description
52-32-17-870-805-A01 Operation

TESTING AND FAULT ISOLATION

52-32-17-700-801-A01 Test of the Proximity Switches 34WV and 12MJ

SCHEMATIC AND WIRING DIAGRAMS

52-32-17-878-806-A01 Wiring Diagram

DISASSEMBLY
52-32-17-000-801-A01 Removal of the Identification Plate, the Insulation and the Door
Seal
52-32-17-000-802-A01 Removal of the Door Fairing
52-32-17-000-803-A01 Removal and Disassembly of the Access Covers
52-32-17-000-804-A01 Removal of the Plugs, the Protective Plugs, the X-Stops and the
Adjusting Screws
52-32-17-000-805-A01 Removal of the Hand Lever Mechanism
52-32-17-000-806-A01 Disassembly of the Hand Lever Assembly
52-32-17-000-807-A01 Removal and Disassembly of the Adjustable Rods and the Drift
Pin Rods
52-32-17-000-808-A01 Removal and Disassembly of the Sequence Shaft
52-32-17-000-808-B01 Removal and Disassembly of the Sequence Shaft
52-32-17-000-808-C01 Removal and Disassembly of the Sequence Shaft
52-32-17-000-809-A01 Removal of the Vent Door Actuating Mechanism
52-32-17-000-810-A01 Removal and Disassembly of the Vent Door Assembly
52-32-17-000-811-A01 Removal of the Latching Mechanism Assemblies
52-32-17-000-812-A01 Disassembly of the Latching Hook Assemblies
52-32-17-000-813-A01 Removal and Disassembly of the Latching Shaft Assembly
52-32-17-000-813-B01 Removal and Disassembly of the Latching Shaft Assembly
52-32-17-000-814-A01 Removal and Disassembly of the Interlock Mechanism
52-32-17-000-815-A01 Removal of the Locking Shaft Assembly
52-32-17-000-815-B01 Removal of the Locking Shaft Assembly

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COMPONENT MAINTENANCE MANUAL
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52-32-17-000-815-C01 Removal of the Locking Shaft Assembly

52-32-17-000-816-A01 Removal of the Door Drainage
52-32-17-000-817-A01 Removal of the Door Sensors
52-32-17-000-818-A01 Removal of the Door Hinge Assemblies
52-32-17-000-818-B01 Removal of the Door Hinge Assemblies

CLEANING
52-32-17-100-801-A01 Cleaning

INSPECTION/CHECK
52-32-17-200-801-A01 Door Structure
52-32-17-210-801-A01 Check of the Door Mechanism and the Locking Mechanism
52-32-17-220-801-A01 Check of the Protective Treatment
52-32-17-210-802-A01 Check of the Electrical Equipment
52-32-17-220-802-A01 Visual Examination

REPAIR
52-32-17-300-801-A01 Reworking or Machining
52-32-17-300-802-A01 Protective Treatment
52-32-17-300-803-A01 Replacement of Parts

ASSEMBLY
52-32-17-400-801-A01 Installation of the Identification Plate, the Insulation and the Door
Seal
52-32-17-400-802-A01 Assembly and Installation of the Access Covers
52-32-17-400-803-A01 Installation of the X-Stops, the Protective Plugs, the Plugs and
the Adjusting Screws
52-32-17-400-804-A01 Assembly of the Hand Lever Assembly
52-32-17-400-805-A01 Installation of the Hand Lever Mechanism
52-32-17-400-806-A01 Assembly of the Latching Hook Assemblies
52-32-17-400-807-A01 Installation of the Latching Mechanism Assemblies
52-32-17-400-808-A01 Assembly and Installation of the Latching Shaft Assembly
52-32-17-400-808-B01 Assembly and Installation of the Latching Shaft Assembly
52-32-17-400-809-A01 Assembly and Installation of the Interlock Mechanism
52-32-17-400-810-A01 Installation of the Locking Shaft Assembly
52-32-17-400-810-B01 Installation of the Locking Shaft Assembly
52-32-17-400-810-C01 Installation of the Locking Shaft Assembly
52-32-17-400-811-A01 Assembly and Installation of the Sequence Shaft
52-32-17-400-811-B01 Assembly and Installation of the Sequence Shaft

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52-32-17-400-811-C01 Assembly and Installation of the Sequence Shaft

52-32-17-400-812-A01 Assembly and Installation of the Adjustable Rods and the Drift Pin
Rods
52-32-17-400-813-A01 Assembly and Installation of the Vent Door Assembly
52-32-17-400-814-A01 Installation of the Vent Door Actuating Mechanism
52-32-17-400-815-A01 Installation of the Door Sensors
52-32-17-400-816-A01 Installation of the Door Drainage
52-32-17-400-817-A01 Installation of the Door Hinge Assemblies
52-32-17-400-817-B01 Installation of the Door Hinge Assemblies
52-32-17-400-818-A01 Installation of the Door Fairing
52-32-17-800-801-A01 Adjustment

FITS AND CLEARANCES

52-32-17-820-807-A01 General
52-32-17-820-808-A01 Fits and Clearances

SPECIAL TOOLS,FIXTURES,EQUIPMENT AND CONSUMABLES

52-32-17-940-809-A01 Special Tools, Fixtures and Equipment List

STORAGE INCLUDING TRANSPORTATION

52-32-17-550-801-A01 Storage after Assembly

ILLUSTRATED PARTS LIST

52-32-17-872-801-A01 Introduction Illustrated Parts List (IPL)
VENDOR LIST
DETAILED PARTS LIST

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COMPONENT MAINTENANCE MANUAL
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LIST OF SERVICE BULLETINS

SB /AEB REV Included in State of TITLE
No. Revision Applicability
SB 52-1124 - - - DOORS - FWD AND AFT CARGO
COMPARTMENT DOORS - REPLACE
WATER DRAIN VALVE
01 no effect -
May 01/07
TABLE 1

SBL
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COMPONENT MAINTENANCE MANUAL
D5237310000000

INTRODUCTION

**For PN’s ALL

TASK 52-32-17-871-802-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
AF Across Flats
ATA Air Transport Association of America
ATLAS Abbreviated Test Language for All Systems
CMM Component Maintenance Manual
IPL Illustrated Parts List
MFR Manufacturer
MOD Modification
NO Number
PARA Paragraph

INTRO
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PMS Process and Materials Specification

PN Part Number
SB Service Bulletin
TBD To Be Determined
List of Abbreviations
TABLE 2

INTRO
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DESCRIPTION AND OPERATION

**For PN’s ALL

TASK 52-32-17-870-803-A01
General
1. The AFT 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 lock
and the unlock of the cargo door can carried out mechanically with the hand lever.
2. For data on the proximity switches see CMMV 32-10-03_08748 of the supplier ELDEC.
3. Technical Data (approx.):
Length: 2100 mm (82.7 in.)
Width : 1400 mm (55.2 in.)
Height: 720 mm (28.4 in.)
Weight: 101 kg (222.7 lb.)
Technical Data
TABLE 1

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TASK 52-32-17-870-804-A01
Description
1. Door Structure (See FIGURE 52-32-17-991-001-A and FIGURE 52-32-17-991-002-A).
A. The cargo door structure has:
- the frames and beams,
- the horizontal and vertical edge members,
- the inner and outer skin,
- the door seal,
- the fire protection lining,
- the fairing.
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. Sealants 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 FR58A and FR59A.
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 allows 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, provided 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 stop bolts are installed on the lower part of the cargo door. The adjustable stop
bolts 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
inner skin of the cargo door.
K. A drainage hose and two drainage valves are installed in the cargo door structure to drain the
condensed water.
L. The fire protection lining assy with integral insulation is made of prepeg. The insulation is made
of PE-foam material lined with self-adhesive. The fire protection lining assy is attached to the
inner skin of the cargo door with quick release fasteners.
M. The two part fairing made of CFRP is installed to the cargo door and gives aerodynamic
smoothness in the transition area of the wing and fuselage.

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2. Door Mechanism (See FIGURE 52-32-17-991-001-A and FIGURE 52-32-17-991-002-A).

A. The door mechanism is installed in the lower part of the cargo door and has:
- the handle mechanism,
- the latching mechanism,
- 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
assy, a door handle assy 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.
B. Latching Mechanism
(1) The Latching mechanism is installed in the lower part of the cargo door. The latching
shaft operates all latching hooks through shaft levers, spring units, bellcranks and links.
(2) 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
bellcrank.
(3) Safety cams, installed at the locking shaft, lock the latching hooks.
C. Interlock Mechanism
(1) 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.
(2) The interlock mechanism locks and unlocks the latching shaft.
D. Locking Mechanism
(1) The locking mechanism is installed parallel to the latching mechanism in the lower part of
the cargo door. The locking mechanism must be operated with the hand lever by a rod
connection at one end of the locking shaft.
(2) 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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E. Vent Door Mechanism

(1) At one end of the Locking shaft, there is a rod assy fitted to the vent door Lever of the
locking shaft which operates a bellcrank housing assy.
(2) The output shaft of the bellcrank housing assy moves the spring loaded vent door with a
connection rod assembly.
F. Target Mechanism
(1) The target mechanism of the door warning system is installed at the sequence shaft.
G. Drift Pin Mechanism
(1) 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 on the aircraft, closed and locked.
(2) The drift pin mechanism includes the control rods with the related bellcranks, the drift pin
lever on the locking shaft and the drift pins.
(3) Control rods transmit the movement of the locking shaft to retract or extend the drift pins.
3. Door Warning and Control System (See FIGURE 52-32-17-991-003-A and SCHEMATIC AND
WIRING DIAGRAM, TASK 52-32-17-878-806-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 34WV is installed adjacent the operating handle (Door Warning
System).
(2) The proximity switch 12MJ is installed to the frame near the target lever on the latching
shaft (Door Control System).

NOTE : For data of the proximity switches see CMMV 32-10-03_08748.

C. The target mechanism, the target lever for the proximity switch 32WV on the aircraft fuselage,
is installed on the frame. A rod assy 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
52-32-17-991-002-A. It consists of the four integrated windows and related green/red markings
on the safety 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. A cable harness for transmission of data of the door condition (LOCKED/UNLOCKED) to the
ECAM is installed in the door structure (See FIGURE 52-32-17-991-003-A ). For the wiring
diagram see TASK 52-32-17-878-806-A01.

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**For PN’s ALL

UPPER EDGE
MEMBER

HINGE
ASSEMBLIES A

ATTACHMENT
FITTINGS

COVER
VENT DOOR
DRIFT PIN/
VENT DOOR
MECHANISM

FIRE PROTECTION
LINING ASSEMBLY

DRIFT PIN
B
B
DRAINAGE
VALVE
B
B
FAIRING EGDE
MEMBER
B RETAINER
EXAMPLE
A
EXAMPLE
ADJUSTING
SCREW
INNER SKIN
DOOR
SEAL

SELF ADHESIVE
INSULATION MAT

FIRE PROTECTION
LINING ASSEMBLY QUICK RELEASE
FASTENER

F_CM_523217_1_0010101_01_00

AFT Cargo Compartment Door

FIGURE-52-32-17-991-001-A01

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**For PN’s ALL

A
PLUG INSTALLATION
A FOR HOISTING

BLANKING
PLUG

VENT
DOOR
BELLCRANK
HOUSING ASSY

SEQUENCE
SHAFT

A TARGET
MECHANISM
DOOR
HANDLE
LATCHING/LOCKING
MECHANISM
LATCHING
SHAFT

LOCKING
SHAFT LATCHING
HOOK
B INTERLOCK
MECHANISM
FLAP

ACCESS
PANEL

INDICATION
WINDOW
F_CM_523217_1_0020101_01_00

AFT Cargo Compartment Door

FIGURE-52-32-17-991-002-A01

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**For PN’s ALL

CONNECTOR
7516VC

7516VT

7518VP

34MV
PROXIMITY
SWITCH
7516VP

12MJ
PROXIMITY
SWITCH

F_CM_523217_1_0030101_01_00

Electric Equipment Installation

FIGURE-52-32-17-991-003-A01

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**For PN’s ALL

TASK 52-32-17-870-805-A01
Operation
1. When you push the flap of the handle mechanism into the cargo door, the flap mechanism unlocks
the door handle. (See FIGURE 52-32-17-991-004-A and FIGURE 52-32-17-991-005-A)
2. 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. (See FIGURE 52-32-17-991-004-A and FIGURE 52-32-17-991-005-A)
3. When you pull up the door handle to the stop position from the LATCHED to the UNLATCHED
position (126˚=fully open) (See FIGURE 52-32-17-991-004-A and FIGURE 52-32-17-991-005-A):
- the latching shaft moves to the unlatched position,
- the over-center linking locks break,
- the four latching hooks move through shaft levers, spring units, bellcranks and links to the
unlatched position.
4. When you press and move the lever of the interlock mechanism, the blockage of the latching shaft is
released. (See FIGURE 52-32-17-991-004-A and FIGURE 52-32-17-991-005-A)
5. When you move the door handle down from the fully open position (UNLATCHED) to the
LATCHED position (65˚). (See FIGURE 52-32-17-991-004-A and FIGURE 52-32-17-991-005-A)
- the latching shaft moves 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.
6. When you push the door handle of the handle mechanism down (until the door handle is smooth with
the 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). (See FIGURE 52-32-17-991-004-A
and FIGURE 52-32-17-991-005-A)

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**For PN’s ALL

UPPER EDGE
MEMBER

HINGE
ASSEMBLIES A

ATTACHMENT
FITTINGS

COVER
VENT DOOR
DRIFT PIN/
VENT DOOR
MECHANISM

FIRE PROTECTION
LINING ASSEMBLY

DRIFT PIN
B
B
DRAINAGE
VALVE
B
B
FAIRING EGDE
MEMBER
B RETAINER
EXAMPLE
A
EXAMPLE
ADJUSTING
SCREW
INNER SKIN
DOOR
SEAL

SELF ADHESIVE
INSULATION MAT

FIRE PROTECTION
LINING ASSEMBLY QUICK RELEASE
FASTENER

F_CM_523217_1_0040101_01_00

AFT Cargo Compartment Door

FIGURE-52-32-17-991-004-A01

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**For PN’s ALL

A
PLUG INSTALLATION
A FOR HOISTING

BLANKING
PLUG

VENT
DOOR
BELLCRANK
HOUSING ASSY

SEQUENCE
SHAFT

A TARGET
MECHANISM
DOOR
HANDLE
LATCHING/LOCKING
MECHANISM
LATCHING
SHAFT

LOCKING
SHAFT LATCHING
HOOK
B INTERLOCK
MECHANISM
FLAP

ACCESS
PANEL

INDICATION
WINDOW
F_CM_523217_1_0050101_01_00

AFT Cargo Compartment Door

FIGURE-52-32-17-991-005-A01

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TESTING AND FAULT ISOLATION

**For PN’s ALL

TASK 52-32-17-700-801-A01
Test of the Proximity Switches 34WV and 12MJ
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. Consumable Materials
REFERENCE DESIGNATION
03JBA1 Silicone base Grease-General Purpose - -
03HBD9 Synthetic Ester base Grease-General Purpose Low Temp -
Consumable Materials
TABLE 1

B. Fixtures, Tools, Test and Support Equipment

REFERENCE DESIGNATION
355M03213000 Cable Loom
355M03214000 Extension Cable Loom
Fixtures, Tools, Test and Support Equipment
TABLE 2

C.Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-000-803-A01 Removal and Disassembly of the Access Covers
TASK 52-32-17-400-802-A01 Assembly and Installation of the Access Covers
TASK 52-32-17-870-804-A01 Description
TASK 52-32-17-870-805-A01 Operation
FIGURE 52-32-17-991-006-A FIGURE 52-32-17-991-006-A-Test of the Electrical Resistance
Referenced Information
TABLE 3

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3. Procedure

WARNING : BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

CAUTION : USE ONLY THE SPECIFIED MATERIALS. MATERIALS WHICH ARE NOT
SPECIFIED, CAN CAUSE DAMAGE.

Subtask 52-32-17-700-001-A01
A. Test of the Proximity Switches 34WV and 12MJ

NOTE : See TASK 52-32-17-870-804-A01, TASK 52-32-17-870-805-A01.

(1) Make sure that the access panel assembly is removed, see DISASSEMBLY TASK
52-32-17-000-803-A01.
(2) Prepare the doors checking tool for the test:

NOTE : See the AIRBUS 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.
(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 34WV and 12MJ.
(b) Install the connector P4 of the 355M03213000 Cable Loom to the connector P9 of
the 355M03214000 Extension Cable Loom .
(c) Connect the connector P1 of the cable loom 355M03213000 Cable Loom to the
connector J1 of the doors checking tool.
(d) Connect the connector P10 of the extension 355M03213000 Cable Loom to the
proximity switch 34WV or 12MJ for test.
(4) Do the test for the proximity switch 34WV 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 34WV, replace it.
ACTION RESULT
1 Move the handle in the LOCKED position. The red LED (DS23) comes on and indicates that
the TARGET is FAR.
2 Move the flap assembly in and pull the The red illuminated LED (DS23) for TARGET
handle out of its recess. NEAR goes off. 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 and Result
TABLE 4

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

(d) Disconnect the connector P10 from the proximity switch 34WV.
(e) Connect the plug connector to the proximity switch 34WV.
(5) Do the test for the proximity switch 12MJ as follows:
(a) Move the switch S6 in the ON position.
(b) If the red SENSOR LED NC (DS24) comes on and indicates a malfunction of the
proximity switch 12MJ, replace it.
ACTION RESULT
1 Move the handle in the LOCKED position. The red LED (DS22) comes on and indicates that
the TARGET is FAR.
2 Push the flap assembly in and pull the The red illuminated LED (DS22) for the TARGET
handle out of its recess. FAR stays on. When the handle is in the fully open
position, 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 and Result
TABLE 5

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

(d) Disconnect the connector P10 from the proximity switch 12MJ.
(e) Connect the plug connector to the proximity switch 12MJ.
(6) Disconnect the connector P1 from the connector J1 of the doors checking tool.

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(7) Disconnect the connector P9 from the connector P4 of the cable looms.
(8) Install the access panel assembly, see ASSEMBLY TASK 52-32-17-400-802-A01.

Subtask 52-32-17-700-002-A01
B. Test of the Electrical Circuit

NOTE : See TASK 52-32-17-870-804-A01, TASK 52-32-17-870-805-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 the electrical circuit
ACTION RESULT
1 Remove the connectors from the proximity -
switches 12MJ and 34WV.
2 Make a connection between the contacts -
11-12 and 15-16 of the connector 7516VC-
A.
3 Connect a continuity tester to the contacts Indication comes on the continuity tester.
A-B of the connectors for the proximity
switches 12MJ and 34WV.
4 Install the connectors to the proximity -
switches 12MJ and 34WV.
Action and Result
TABLE 6

Subtask 52-32-17-810-001-A01
C. Fault Isolation
(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 assembly 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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FAULT POSSIBLE CAUSE CORRECTION

2 You can move the hand a Damaged surfaces of the Replace the damaged parts.
lever assembly to the sequence cams 09-020, the
OPEN or CLOSED universal joint lock 08-240 and
position only with force. the universal joint latch 08-520.
b The sliding surfaces of the Apply the Material No. 03JBA1
sequence cams 09-020, the Silicone base Grease-General
universal joint lock 08-240 and Purpose - - to the sliding
the universal joint latch 08-520 surfaces.
are not lubricated.
c No grease between the sliding Apply the Material No.
surfaces of the shaft 08-250 03HBD9 Synthetic Ester base
and the sequence cams 09-020. Grease-General Purpose Low
Temp - to the lubrication
fitting 08-350 of the shaft
08-250.
d The actuating unit 08-040 is Replace the damaged actuating
damaged and has a leakage. unit 08-040.
e The rod assembly 08-160 is too Adjust the rod assembly
long or too short. 08-160.
f The rod assembly 08-600 is too Adjust the rod assembly
long or too short. 08-600.
3 The handle mechanism has a The thickness of the spacer Remove the hand lever
axial play and an axial washers 08-260, 08-270 must assembly and install new spacer
clearance. be increased. washers 08-260, 08-270.
4 You can not lock the hand a The bearing bolt 09-140 is Replace the damaged parts.
lever assembly with the broken.
handle flap 09-100 in the
CLOSED position.
5 The handle flap 09-100 is a The force of the spring 09-110 The spring 09-110 is weak or
not flush with the contour can not hold the handle flap broken. Replace the spring
of the hand lever assembly. 09-100 in position. 09-110.
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 and
bushes and the latching shaft. the bearing bushes, replace the
damaged parts.

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FAULT POSSIBLE CAUSE CORRECTION

b Not sufficient lubrication Apply the Material No.
between the bearing bushes and 03HBD9 Synthetic Ester base
the latching shaft. Grease-General Purpose Low
Temp - to the sliding surfaces
of the bearing bushes and the
latching shaft.
7 The locking shaft does not a Foreign objects between the Remove the locking shaft.
move easily. sliding surfaces of the bearing Examine the locking shaft and
bushes and the locking shaft. the bearing bushes, replace the
damaged parts.
b Not sufficient lubrication Apply the Material No.
between the bearing bushes and 03HBD9 Synthetic Ester base
the locking shaft. Grease-General Purpose Low
Temp - to the sliding surfaces
of the bearing bushes and the
locking shaft.
8 The drift pin mechanism a Not sufficient lubrication Apply the Material No.
does not move easily. between the bearing bushes and 03HBD9 Synthetic Ester base
the drift pins. Grease-General Purpose Low
Temp - to the sliding surfaces
of the bearing bushes and the
drift pins.
9 The interlock mechanism a The compression spring 44-040 Install a new compression
moves too easily. is broken or has lost its spring spring 44-040.
force.
10 Hard movement of the a Not sufficient lubrication of the Apply the Material No.
latching mechanism. latching mechanism. 03HBD9 Synthetic Ester base
Grease-General Purpose Low
Temp - to the lubrication
fittings 34-030 and 34-200 of
the latching mechanism.
Fault Isolation
TABLE 7

Subtask 52-32-17-700-003-A01
D. Test of the Electrical Resistance

NOTE : See FIGURE 52-32-17-991-006-A.

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(1) Test of the electrical resistance

ACTION RESULT
1 Connect the ohmmeter to the bonding lead The resistance must not be more than 0.1 mΩ.
and the structure near the attachment part.
2 Connect the ohmmeter near the bonding The resistance must not be more than 10.0 mΩ.
lead attachment on the structure.
Action and Result
TABLE 8

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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_523217_1_0060101_01_00

Test of the Electrical Resistance

FIGURE-52-32-17-991-006-A01

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SCHEMATIC AND WIRING DIAGRAMS

**For PN’s ALL

TASK 52-32-17-878-806-A01
Wiring Diagram
1. For the wiring diagram see FIGURE 52-32-17-991-007-A.

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AFT CARGO COMPARTMENT DOOR

2
R A
15 A R A
B A
5862−PF24 5865−PF24 B B
F B
B
16 G C
7518VP
7516VT 826 34WV−A
7516VC−A 154

7516VC−A
1
B C
G B
12 B
F B
1010−PF24 1008−PF24 R A
B A
R
11 A
12MJ−A
7516VP
7516VT

F_CM_523217_1_0070101_01_00

Wiring Diagram
FIGURE-52-32-17-991-007-A01

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DISASSEMBLY

**For PN’s ALL

TASK 52-32-17-000-801-A01
Removal of the Identification Plate, the Insulation and the Door Seal
1. General
A. Put the door in a support with the correct shape to prevent damage.

NOTE : See REPAIR TASK 52-32-17-300-803-A01 for the replacement of component parts
which have a permanent connection.
2. Job Set-up Information
A.Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-300-803-A01 Replacement of Parts
TASK 52-32-17-300-801-A01 Reworking or Machining
Referenced Information
TABLE 1

3. Procedure

Subtask 52-32-17-000-001-A01
A. Removal of the Identification Plate, the Insulation and the Door Seal

NOTE : See IPL_FIGURE_01, IPL_FIGURE_02.

NOTE : For the replacement of the identification plate 01-080, see REPAIR TASK
52-32-17-300-803-A01.
PRE MOD 34470K09330
(1) Remove the fire protection lining assembly 02-010 as follows:
(a) Release the studs 02-030 and remove the fire protection lining assembly 02-010 from
the door structure.

NOTE : It is only necessary to replace the lock washers 02-060, the spacers 02-040,
the washers 02-050 and the studs 02-030 from the fire protection lining
assembly 02-010 if they are damaged.

NOTE : It is only necessary to replace the insulation 02-020 from the fire protection
lining assembly 02-010 if it is damaged.

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NOTE : It is only necessary to replace the loop tape 02-085 and the hook tape
02-110 from the fire protection lining assembly 02-010 if it is damaged.
POST MOD 34470K09330
(1) Remove the fire protection lining assembly 02-010 as follows:
(a) Release the studs 02-030 and remove the fire protection lining assembly 02-010 from
the door structure.

NOTE : It is only necessary to replace the lock washers 02-060, the spacers 02-040,
the washers 02-050 and the studs 02-030 from the fire protection lining
assembly 02-010 if they are damaged.

NOTE : It is only necessary to replace the insulation 02-020 from the fire protection
lining assembly 02-010 if it is damaged.

NOTE : It is only necessary to replace the tape 02-085 and the tape 02-110 from
the fire protection lining assembly 02-010 if it is damaged.
ALL VARIANTS
(2) Remove the door seal 02-090 as follows:
(a) Remove the door seal 02-090 from the door structure.

NOTE : It is only necessary to replace the door seal 02-090 if it is damaged, see
REPAIR TASK 52-32-17-300-801-A01.

NOTE : It is only necessary to replace the bushings 02-100 from the door structure
if they are damaged, see REPAIR TASK 52-32-17-300-803-A01.

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**For PN’s ALL

TASK 52-32-17-000-802-A01
Removal of the Door Fairing
1. General
A. Put the door in a support with the correct shape to prevent damage.
-

NOTE : See REPAIR TASK 52-32-17-300-803-A01 for the replacement of component parts
which have a permanent connection.
2. Job Set-up Information
A.Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-300-803-A01 Replacement of Parts
Referenced Information
TABLE 1

3. Procedure

Subtask 52-32-17-000-002-A01
A. Removal of the Door Fairing

NOTE : See IPL_FIGURE_70, IPL_FIGURE_71.

(1) Remove the fairings 70-010 and 70-020 as follows:
(a) Remove the screws 70-030 and 70-050 and the washers 70-040 and remove the
fairings 70-010 and 70-020 from the fairing structure 70-060.
(b) Remove the sight glass 70-022 as follows:

NOTE : It is only necessary to replace the sight glass 70-022 if it is damaged.

1 Remove the nuts 70-028, the washers 70-026, the screws 70-024 and the sight
glass 70-022 from the fairing 70-020.
(2) Remove the fairing door web assemblies 71-130 and 71-160 as follows:

NOTE : It is only necessary to replace the riveted L-section assemblies 71-010, 71-020,
71-030 and 71-250, the connecting angle assembly 71-180 and the support plate
71-190 if they are damaged, see REPAIR TASK 52-32-17-300-803-A01.
(a) Make a mark to record the position of the door web assembly 71-130 in the X and Y
direction for the assembly procedure.

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(b) Remove the screws 71-110 and the washers 71-120, release the studs 71-140 and
remove the door web assembly 71-130.

NOTE : It is only necessary to replace the door web assembly 71-130 if it is

damaged, see REPAIR TASK 52-32-17-300-803-A01.

NOTE : It is only necessary to replace the studs 71-140 and the washers 71-150 if
they are damaged.
(c) Make a mark to record the position of the door web assembly 71-160 in the X and Y
direction for the assembly procedure.
(d) Remove the screws 71-110 and the washers 71-120 and remove the door web
assembly 71-160.

NOTE : It is only necessary to replace the door web assembly 71-160 if it is

damaged, see REPAIR TASK 52-32-17-300-803-A01.
(3) Remove the section assemblies 71-100, 71-170, 71-200 and 71-210 as follows:

NOTE : It is only necessary to replace the section assemblies 71-100, 71-170, 71-200 and
71-210 if they are damaged, see REPAIR TASK 52-32-17-300-803-A01.
(a) Make a mark to record the position of the section assemblies 71-100, 71-170, 71-200
and 71-210 in the X and Y direction for the assembly procedure.
(b) Remove the screws 71-240 and the washers 71-120 and remove the Z-section
assembly 71-170.
(c) Remove the screws 71-110 and the washers 71-120 and remove the lower L-section
71-100 and the L-section assembly 71-200.
(d) Release the studs 71-140 and remove the edge section assembly 71-210.

NOTE : It is only necessary to replace the studs 71-140 and the washers 71-220 if
they are damaged.

NOTE : It is only necessary to replace the plate 71-260 if it is damaged, see

REPAIR TASK 52-32-17-300-803-A01.

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**For PN’s ALL

TASK 52-32-17-000-803-A01
Removal and Disassembly of the Access Covers
1. General
A. Put the door in a support with the correct shape to prevent damage.
-

NOTE : See REPAIR TASK 52-32-17-300-803-A01 for the replacement of component parts
which have a permanent connection.
2. Job Set-up Information
A.Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-300-803-A01 Replacement of Parts
TASK 52-32-17-000-802-A01 Removal of the Door Fairing
Referenced Information
TABLE 1

3. Procedure

Subtask 52-32-17-000-003-A01
A. Removal and Disassembly of the Access Covers

NOTE : See IPL_FIGURE_03.

(1) Remove the access cover assembly 03-010 as follows:

NOTE : For the removal of the door fairing, see DISASSEMBLY TASK
52-32-17-000-802-A01.
(a) Release the studs 03-050, 03-060 and 03-070 and remove the access cover assembly
03-010 from the door structure.

NOTE : It is only necessary to replace the studs 03-050, 03-060 and 03-070, the
washers 03-080 and the tab washers 03-090 from the access cover assembly
03-010 if they are damaged.

NOTE : It is only necessary to replace the nut plates 03-100 and the receptacles
03-160 if they are damaged, see REPAIR TASK 52-32-17-300-803-A01.

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(2) Disassemble the access cover assembly 03-010 as follows:

(a) Remove the sight glasses 03-020 from the access cover assembly 03-010.

NOTE : It is only necessary to replace the sight glasses 03-020 if they are damaged.
1 Remove the nuts 03-040, the screws 03-030, the sheet 03-015 and remove the
sight glass 03-020 from the access cover assembly 03-010.
(3) Remove the access covers 03-110 as follows:

NOTE : It is only necessary to remove the access covers 03-110 if the drift pins are
damaged.
(a) Remove the screws 03-120 and remove the access cover 03-110 from the door
structure.
(4) Remove the access cover assembly 03-130 as follows:
(a) Remove the screws 03-140 and the washers 03-150 and remove the access cover
assembly 03-130 from the door structure.

NOTE : It is only necessary to replace the sealing section 03-135 from the access
cover 03-132 if it is damaged.

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**For PN’s ALL

TASK 52-32-17-000-804-A01
Removal of the Plugs, the Protective Plugs, the X-Stops and the Adjusting Screws
1. General
A. Put the door in a support with the correct shape to prevent damage.
-

NOTE : See REPAIR TASK 52-32-17-300-803-A01 for the replacement of component parts
which have a permanent connection.
2. Job Set-up Information
A.Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-300-803-A01 Replacement of Parts
Referenced Information
TABLE 1

3. Procedure

Subtask 52-32-17-000-004-A01
A. Removal of the Plugs, the Protective Plugs, the X-Stops and the Adjusting Screws

NOTE : See IPL_FIGURE_01, IPL_FIGURE_04.

(1) Remove the plugs 01-090 as follows:
(a) Remove the plugs 01-090 from the door structure.

NOTE : It is only necessary to replace the inserts 01-035 if they are damaged, see
REPAIR TASK 52-32-17-300-803-A01.
(2) Remove the adjusting screws 01-100 as follows:
(a) Release the tab washer 01-120 from the nut 01-110 and remove the adjusting screw
01-100, the nut 01-110 and the tab washer 01-120 from the door structure.
(b) Discard the tab washer 01-120.

NOTE : It is only necessary to replace the inserts 01-130 if they are damaged, see
REPAIR TASK 52-32-17-300-803-A01.
(3) Remove the protective plugs 04-020, 04-120 and 04-130 as follows:
(a) Remove the protective plugs 04-020, 04-120 and 04-130 from the door structure.

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(4) Remove the X-stops 04-030 and 04-100 as follows:

(a) Remove the nuts 04-070, the screws 04-050 and 04-080, the washers 04-060 and
04-090, the X-stops 04-030 and 04-100 and the adjusting plates 04-040, 04-041,
04-042, 04-043, 04-110, 04-111, 04-112, 04-113 from the door structure.

NOTE : Record the thickness of the adjusting plates 04-040, 04-041, 04-042,
04-043, 04-110, 04-111, 04-112, 04-113 for the assembly procedure.

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**For PN’s ALL

TASK 52-32-17-000-805-A01
Removal of the Hand Lever Mechanism
1. General
A. Put the door in a support with the correct shape to prevent damage.
-

NOTE : See REPAIR TASK 52-32-17-300-803-A01 for the replacement of component parts
which have a permanent connection.
2. Job Set-up Information
A.Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-300-803-A01 Replacement of Parts
Referenced Information
TABLE 1

3. Procedure

Subtask 52-32-17-000-005-A01
A. Removal of the Hand Lever Mechanism

NOTE : See IPL_FIGURE_08, IPL_FIGURE_95.

(1) Move the hand lever assembly 08-010 to the UNLOCKED position.
(2) Install a locally made bush and a nut (e.g. NAS 509-4) on the spring bolt 08-460. Turn the
nut until the compression spring 08-470 is completely compressed.

NOTE : The locally made bush must be made of aluminum or bronze and must have the
following dimensions:
Length: 12.0 mm (0.4724 in)
Inner 7.5 mm (0.2952 in)
Diameter:
Outer 13.0 mm (0.5118 in)
Diameter:
Technical Data
TABLE 2

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(3) Disconnect the rod assemblies 08-160 and 08-600 as follows:

(a) Remove and discard the cotter pin 08-170 from the nut 08-180.
(b) Remove the nut 08-180, the washer 08-190, the bolt 08-200, the washer 08-210 and
disconnect the rod assembly 08-160 from the lever 08-090.
(c) Remove and discard the cotter pin 08-540 from the nut 08-550.
(d) Remove the nut 08-550, the washer 08-560, the bolt 08-580, the washer 08-570 and
disconnect the rod assembly 08-600 from the universal joint assembly 08-510.
(4) Remove the shaft 08-250 and the hand lever assembly 08-010 as follows:
(a) Remove the bolts 08-140 and the lockwasher 08-150.
(b) Discard the lockwasher 08-150.
(c) Remove the shaft 08-250 and the spacer washers 08-260, 08-270, 08-271, 08-272,
08-273, 08-274, 08-275, 08-276, 08-277 and remove the hand lever assembly 08-010
from the door structure.

NOTE : Record the location and the thickness of the spacer washers 08-260, 08-270,
08-271, 08-272, 08-273, 08-274, 08-275, 08-276, 08-277 for the assembly
procedure.

NOTE : It is only necessary to replace the lubrication fitting 08-350 from the shaft
08-250 if it is damaged, see REPAIR TASK 52-32-17-300-803-A01.
(5) Remove and disassemble the lever assembly 08-020 as follows:
(a) Remove the nuts 08-110, the washers 08-120, the bolts 08-130 and the washers
08-120 from the bracket 08-030 and the door structure.
(b) Remove the nut 08-110, the washer 08-220 and the bolt 08-230 from the lever
08-090.

WARNING : THE LEVER ASSEMBLY IS INSTALLED WITH LOAD, REMOVE IT

CAREFULLY.
(c) Remove the lever assembly 08-020 from the shaft 08-360.
(d) Remove and discard the cotter pins 08-060 from the locating pins 08-050.
(e) Remove the washers 08-070, the locating pins 08-050 and the washers 08-080 and
disconnect the actuating unit 08-040 from the lever 08-090 and the bracket 08-030.

NOTE : It is only necessary to replace the bonded-in bearing 08-100 in the lever
08-090 if it is damaged, see REPAIR TASK 52-32-17-300-803-A01.
(6) Remove the compression spring 08-470 as follows:
(a) Remove the nut 08-110, the washer 08-120 and the bolt 08-450.

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WARNING : THE COMPRESSION SPRING IS INSTALLED WITH LOAD. REMOVE IT

CAREFULLY.
(b) Carefully remove the nut (e.g. NAS 509-4) from the spring bolt 08-460 and release
the tension of the compression spring 08-470.
(c) Remove the compression spring 08-470 from the spring bolt 08-460.
(d) Remove the spring bolt 08-460 from the roller lever 08-380.
(7) Remove the shaft 08-360 as follows:
(a) Remove the nut 08-110, the washer 08-220 and the bolt 08-230 from the universal
joint lock 08-240.
(b) Carefully remove the shaft 08-360 from the door structure and remove the universal
joint lock 08-240, the roller lever assembly 08-370 and the universal joint assembly
08-510.

NOTE : It is only necessary to replace the bonded-in bearing 08-590 in the universal
joint latch 08-520 if it is damaged, see REPAIR TASK 52-32-17-300-803-
A01.

NOTE : It is only necessary to replace the shouldered bushings 08-530 in the

universal joint latch 08-520 if they are damaged, see REPAIR TASK
52-32-17-300-803-A01.
(8) Disassemble the roller lever assembly 08-370 as follows:
(a) Remove and discard the cotter pin 08-TBD from the nut 08-410.
(b) Remove the nut 08-410, the washer 08-420 and the bolt 08-430, then remove the
roller 08-400 from the roller lever 08-380.

NOTE : It is only necessary to replace the shouldered bushings 08-390 in the roller
lever 08-380 if they are damaged, see REPAIR TASK 52-32-17-300-803-
A01.
(9) Remove the rod assemblies 08-160 and 08-600 as follows:
(a) Remove and discard the cotter pins 08-170 from the fork-end connection of the rod
assemblies 08-160 and 08-600.
(b) Remove the nuts 08-180, the washers 08-190, the bolts 08-200 and the washers
08-210 from the fork-end connection of the rod assemblies 08-160 and 08-600.
(c) Disconnect the fork-end of the rod assembly 08-160 from the locking shaft.
(d) Disconnect the fork-end of the rod assembly 08-600 from the latching shaft.
(10) Disassemble the rod assemblies 08-160 and 08-600 as follows:

NOTE : Measure and record the length of the rod assemblies 08-160 and 08-600 between
the centers of the rod ends, for the assembly procedure.

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WARNING : USE GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH

TIME YOU CUT LOCKWIRE DURING THE TASK, REMOVE AND
DISCARD IT (THE UNWANTED LOCKWIRE) IMMEDIATELY. LOOSE
LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND.
(a) Cut, remove and discard the lockwire from the nuts 95-030 and 95-040 and the
locking devices 95-050.
(b) Loosen the nuts 95-030 and 95-040.
(c) Remove the rod ends 95-010, 95-020 with the nuts 95-030 and 95-040 and the
locking devices 95-050 from the rod body.
(d) Remove the nuts 95-030 and 95-040 and the locking devices 95-050 from the rod ends
95-010, 95-020.
(11) Remove the catching hook 08-490 as follows:
(a) Remove the bolts 08-500, the washers 08-120 and remove the catching hook 08-490
and the sheet 08-480.

NOTE : Measure and record the thickness of the sheet 08-480 for the assembly
procedure.
(12) Remove the bolt 08-440 from the door structure as follows:
(a) Remove the nut 08-110, the washer 08-220 and the bolt 08-440 from the door
structure.

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**For PN’s ALL

TASK 52-32-17-000-806-A01
Disassembly of the Hand Lever Assembly
1. General
A. Put the door in a support with the correct shape to prevent damage.
-

NOTE : See REPAIR TASK 52-32-17-300-803-A01 for the replacement of component parts
which have a permanent connection.
2. Job Set-up Information
A.Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-300-803-A01 Replacement of Parts
Referenced Information
TABLE 1

3. Procedure

Subtask 52-32-17-000-006-A01
A. Disassembly of the Hand Lever Assembly

NOTE : See IPL_FIGURE_09.

(1) Disassemble the hand lever assembly 09-001 as follows:
(a) Remove the retaining rings 09-050, the washers 09-060, the bolts 09-040, the rollers
09-080 and remove the stop 09-030.

NOTE : It is only necessary to replace the bushings 09-070 if they are damaged, see
REPAIR TASK 52-32-17-300-803-A01.

NOTE : It is only necessary to replace the bonded-in insert 09-090 if it is damaged,

see REPAIR TASK 52-32-17-300-803-A01.
(b) Remove the bolts 09-190 and the washers 09-150 and remove the sequence cams
09-020.

NOTE : It is only necessary to replace the inserts 09-200 if they are damaged, see
REPAIR TASK 52-32-17-300-803-A01.
(c) Remove and discard the cotter pins 09-120 from the two ends of the bearing bolt
09-140.
(d) Remove the washers 09-130 and the bearing bolt 09-140 from the handle flap 09-100.

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(e) Remove and discard the cotter pins 09-120 from the two ends of the bearing bolt
09-160.

WARNING : THE SPRING IS INSTALLED WITH LOAD. REMOVE IT CAREFULLY.

(f) Remove the washers 09-150, the bearing bolt 09-160, the spring sleeve 09-170, the
spring 09-110 and the handle flap 09-100 from the hand lever 09-010.

NOTE : It is only necessary to replace the bushings 09-180 on the hand lever 09-010
and the handle flap 09-100 if they are damaged, see REPAIR TASK
52-32-17-300-803-A01.

NOTE : It is only necessary to replace the bonded sliding layer 09-210 from the
handle flap 09-100 if it is damaged.

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**For PN’s ALL

TASK 52-32-17-000-807-A01
Removal and Disassembly of the Adjustable Rods and the Drift Pin Rods
1. General
A. Put the door in a support with the correct shape to prevent damage.
-

NOTE : See REPAIR TASK 52-32-17-300-803-A01 for the replacement of component parts
which have a permanent connection.
2. Job Set-up Information
A. Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-300-803-A01 Replacement of Parts
TASK 52-32-17-000-808-A01 Removal and Disassembly of the Sequence Shaft
TASK 52-32-17-000-808-B01 Removal and Disassembly of the Sequence Shaft
TASK 52-32-17-000-808-C01 Removal and Disassembly of the Sequence Shaft
Referenced Information
TABLE 1

3. Procedure

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.

Subtask 52-32-17-000-007-A01
A. Removal and Disassembly of the Adjustable Rods and the Drift Pin Rods

NOTE : See IPL_FIGURE_13, IPL_FIGURE_95, IPL_FIGURE_96.

(1) Remove and disassemble the adjustable rod 13-260 as follows:
(a) Remove the adjustable rod 13-260 as follows:
1 Remove and discard the cotter pins 13-250.
2 Remove the nuts 13-230, the washers 13-240, the bolts 13-200 and the washers
13-210 and remove the adjustable rod 13-260.

NOTE : Measure and record the length of the adjustable rod 13-260 between
the center of the rod ends for the assembly procedure.

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(b) Disassemble the adjustable rod 13-260 as follows:

WARNING : USE GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE.

EACH TIME YOU CUT LOCKWIRE DURING THE TASK, REMOVE
AND DISCARD IT (THE UNWANTED LOCKWIRE) IMMEDIATELY.
LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND.
1 Cut, remove and discard the lockwire from the nuts 95-030 and 95-040 and the
locking washer 95-050.
2 Loosen the nuts 95-030 and 95-040.
3 Remove the clevis 95-010 and 95-020 with the nuts 95-030 and 95-040 and the
locking washer 95-050 from the rod body.
4 Remove the nuts 95-030 and 95-040 and the locking washer 95-050 from the
clevis 95-010 and 95-020.
5 Discard the locking washer 95-050.
(2) Remove the rod assemblies 13-080 and 13-270 as follows:
(a) Remove and discard the cotter pins 13-070 and 13-250.
(b) Remove the nuts 13-050 and 13-230, the washers 13-060 and 13-240, the bushings
13-040, the bolts 13-020 and 13-200 and the washers 13-210.
(c) Remove the rod assemblies 13-080 and 13-270, the washers 13-030 and 13-220 and
the drift pins 13-010 from the bellcrank assembly 13-090 and the link lever assembly
20-180.
(d) Do not disassemble the rod assemblies 13-080 and 13-270.

NOTE : It is only necessary to replace the rod assemblies 13-080 and 13-270 if they
are damaged.
(3) Remove the bellcrank assembly 13-090 as follows:
(a) Disconnect the fixed rod 40-010 from the link lever assembly 13-130, see
DISASSEMBLY TASK 52-32-17-000-808-A01TASK 52-32-17-000-808-B01TASK
52-32-17-000-808-C01.
(b) Remove the nuts 13-190 and 13-300, the sleeves 13-180 and 13-290 and the taper
pins 13-170 and 13-280.
(c) Remove the link lever assembly 13-130 from the beam-3 shaft 13-160.

NOTE : It is only necessary to replace the bonded-in bearing 13-150 on the link
lever 13-140 if it is damaged, see REPAIR TASK 52-32-17-300-803-A01.

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(d) Remove the beam-3 shaft 13-160 and the link lever assembly 13-100 from the door
structure.

NOTE : It is only necessary to replace the bonded-in bearings 13-120 from the link
lever 13-110 if it is damaged, see REPAIR TASK 52-32-17-300-803-A01.

NOTE : It is only necessary to replace the shouldered bushings 96-210 from the door
structure if they are damaged, see REPAIR TASK 52-32-17-300-803-A01.

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**For PN’s D5237310000000 D5237310000200 D5237310000400 D5237310000800

TASK 52-32-17-000-808-A01
Removal and Disassembly of the Sequence Shaft
1. General
A. Put the door in a support with the correct shape to prevent damage.
-

NOTE : See REPAIR for the replacement of component parts which have a permanent
connection.
2. Procedure

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.

Subtask 52-32-17-000-008-A01
A. Removal and Disassembly of the Sequence Shaft

NOTE : See IPL_FIGURE_13, IPL_FIGURE_31, IPL_FIGURE_40, IPL_FIGURE_41,

IPL_FIGURE_95.
(1) Remove and disassemble the bellcrank housing assembly 40-020 as follows:
(a) Remove the fixed rods 40-010 and 40-100 from the link lever assembly 13-130, the
lever assembly 41-240 and the levers 40-070 as follows:
1 Remove and discard the cotter pins 40-110 and 40-230.
2 Remove the nuts 40-120 and 40-210, the washers 40-130 and 40-220, the bolts
40-140 and 40-250 and the washers 40-150 and 40-240 and remove the fixed
rods 40-010 and 40-100.

NOTE : Measure and record the length of the fixed rod 40-010 between the
centers of the clevis 95-010 and 95-020 for the assembly procedure.

NOTE : It is only necessary to replace the bonded-in bearings 40-090 from the
levers 40-080 if they are damaged, see REPAIR .
(b) Disassemble the fixed rod 40-010 as follows:

WARNING : USE GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE.

EACH TIME YOU CUT LOCKWIRE DURING THE TASK, REMOVE
AND DISCARD IT (THE UNWANTED LOCKWIRE) IMMEDIATELY.
LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND.

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1 Cut and remove the lockwire from the nuts 95-030 and 95-040 and the locking
washers 95-050.
2 Loosen the nuts 95-030 and 95-040.
3 Remove the clevis 95-010 and 95-020 with the nuts 95-030 and 95-040 and the
locking washers 95-050 from the rod body.
4 Remove the nuts 95-030 and 95-040 and the locking washers 95-050 from the
clevis 95-010 and 95-020.
5 Discard the lockwire and the locking washers 95-050.
(c) Remove and disassemble the bellcrank housing assembly 40-020 as follows:
1 Remove the bolts 40-190, the washers 40-200 and remove the bellcrank housing
assembly 40-020 from the door structure.
2 Remove the nuts 40-170, the sleeves 40-180 and the taper pins 40-160.
3 Remove the beam-4 shaft 40-060 and the levers 40-080 from the beam-4 cover
40-030.

NOTE : It is only necessary to replace the shouldered bushings 40-050 from the
cover 40-040 if they are damaged, see REPAIR .
(2) Remove and disassemble the sequence shaft assembly 41-200 as follows:
(a) Remove and disassemble the link assembly 41-010 as follows:
1 Remove and discard the cotter pins 41-110 and 41-380.
2 Remove the nuts 41-100 and 41-360, the washers 41-090 and 41-370 and the
bolts 41-080 and 41-340.
3 Remove the link assembly 41-010, the sleeves 41-070 and 41-350 and the
bushing 41-230.
4 Release the tab washers 41-040 and loosen the nuts 41-030 and 41-050 and
remove the forks 41-020 and 41-060, the tab washers 41-040 and the nuts
41-030 and 41-050 from the rod 41-120.
5 Discard the tab washers 41-040.
(b) Remove the lever assembly 41-130 as follows:
1 Remove and discard the cotter pin 41-410.
2 Remove the nut 41-390, the washer 41-400 and the lever 41-140 from the fitting
support 41-170.

NOTE : It is only necessary to replace the shouldered bushings 41-150 and the
bushing 41-160 from the lever 41-140 if they are damaged, see
REPAIR .

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NOTE : It is only necessary to replace the riveted fitting support 41-170 if it is

damaged, see REPAIR .
(c) Remove the connecting rod assembly 41-440 as follows:
1 Remove and discard the cotter pins 41-410.
2 Remove the nuts 41-390, the washers 41-400, the bolts 41-430, the washers
41-420 and remove the connecting rod assembly 41-440 from the levers 41-330
and 31-060.

NOTE : It is only necessary to replace the bonded-in bearings 41-460 from the
connecting rod 41-450 if they are damaged, see REPAIR .
(d) Remove and disassemble the sequence shaft assembly 41-200 as follows:
1 Remove the nuts 41-300, the washers 41-290, the sleeves 41-280, the taper pins
41-270 and the rivet pins 41-320.

NOTE : Record the positions of the lever assembly 41-240, the locking cam
41-310 and the levers 41-220 and 41-330 for the assembly procedure.
2 Discard the rivet pins 41-320 and the nuts 41-300.
3 Remove the sequence shaft 41-210 with the lever assembly 41-240, the washer
41-335, the locking cam 41-310, the washer 41-335 and the levers 41-220 and
41-330.

NOTE : It is only necessary to replace the bonded-in bearing 41-260 from the
lever 41-250 if it is damaged, see REPAIR .

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**For PN’s D5237310000600 D5237310001000 D5237310001200 D5237310001400

TASK 52-32-17-000-808-B01
Removal and Disassembly of the Sequence Shaft
1. General
A. Put the door in a support with the correct shape to prevent damage.
-

NOTE : See REPAIR for the replacement of component parts which have a permanent
connection.
2. Procedure

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.

Subtask 52-32-17-000-019-A01
A. Removal and Disassembly of the Sequence Shaft

NOTE : See IPL_FIGURE_13, IPL_FIGURE_31A, IPL_FIGURE_40, IPL_FIGURE_41A,

IPL_FIGURE_95.
(1) Remove and disassemble the bellcrank housing assembly 40-020 as follows:
(a) Remove the fixed rods 40-010 and 40-100 from the link lever assembly 13-130, the
serrated lever assembly 41A-220 and the levers 40-070 as follows:
1 Remove and discard the cotter pins 40-110 and 40-230.
2 Remove the nuts 40-120 and 40-210, the washers 40-130 and 40-220, the bolts
40-140 and 40-250 and the washers 40-150 and 40-240 and remove the fixed
rods 40-010 and 40-100.

NOTE : Measure and record the length of the fixed rod 40-010 between the
centers of the clevis 95-010 and 95-020 for the assembly procedure.

NOTE : It is only necessary to replace the bonded-in bearings 40-090 from the
levers 40-080 if they are damaged, see REPAIR .
(b) Disassemble the fixed rod 40-010 as follows:

WARNING : USE GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE.

EACH TIME YOU CUT LOCKWIRE DURING THE TASK, REMOVE
AND DISCARD IT (THE UNWANTED LOCKWIRE) IMMEDIATELY.
LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND.

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1 Cut and remove the lockwire from the nuts 95-030 and 95-040 and the locking
washers 95-050.
2 Loosen the nuts 95-030 and 95-040
3 Remove the clevis 95-010 and 95-020 with the nuts 95-030 and 95-040 and the
locking washers 95-050 from the rod body.
4 Remove the nuts 95-030 and 95-040 and the locking washers 95-050 from the
clevis 95-010 and 95-020.
5 Discard the lockwire and the locking washers 95-050.
(c) Remove and disassemble the bellcrank housing assembly 40-020 as follows:
1 Remove the bolts 40-190, the washers 40-200 and remove the bellcrank housing
assembly 40-020 from the door structure.
2 Remove the nuts 40-170, the sleeves 40-180 and the taper pins 40-160.
3 Remove the beam-4 shaft 40-060 and the levers 40-080 from the beam-4 cover
40-030.

NOTE : It is only necessary to replace the shouldered bushings 40-050 from the
cover 40-040 if they are damaged, see REPAIR .
(2) Remove and disassemble the sequence shaft assembly 41A-200 as follows:
(a) Remove and disassemble the link assembly 41A-010 as follows:
1 Remove and discard the cotter pins 41A-110 and 41A-360.
2 Remove the nuts 41A-100 and 41A-340, the washers 41A-090 and 41A-290 and
the bolts 41A-080 and 41A-320.
3 Remove the link assembly 41A-010 with the sleeves 41A-070 and 41A-330 and
the bushing 41A-270.
4 Release the tab washers 41A-040 and loosen the nuts 41A-030 and 41A-050 and
remove the forks 41A-020 and 41A-060, the tab washers 41A-040 and the nuts
41A-030 and 41A-050 from the rod 41A-120.
5 Discard the tab washers 41A-040.
(b) Remove the lever assembly 41A-130 as follows:
1 Remove and discard the cotter pin 41A-390.
2 Remove the nut 41A-370, the washer 41A-380 and the lever 41A-140 from the
fitting support 41A-170.

NOTE : It is only necessary to replace the shouldered bushings 41A-150 and

the bushing 41A-160 from the lever 41A-140 if they are damaged, see
REPAIR .

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NOTE : It is only necessary to replace the riveted fitting support 41A-170 if it

is damaged, see REPAIR .
(c) Remove the connecting rod assembly 41A-440 as follows:
1 Remove and discard the cotter pins 41A-390.
2 Remove the nuts 41A-370, the washers 41A-380, the bolts 41A-400, the washers
41A-410 and remove the connecting rod assembly 41A-440 from the serrated
lever 41A-350 and the lever 31A-060.

NOTE : It is only necessary to replace the bonded-in bearings 41A-460 from

the connecting rod 41A-450 if they are damaged, see REPAIR .
(d) Remove and disassemble the sequence shaft assembly 41A-200 as follows:
1 Release the lockwasher 41A-430 and remove the screw 41A-420.
2 Discard the lockwasher 41A-430.
3 Remove the nuts 41A-300, the washers 41A-290 and the rivet pins 41A-280 and
41A-310.
4 Discard the rivet pins 41A-280 and 41A-310 and the nuts 41A-300.

NOTE : Record the position of the link lever 41A-260, the serrated lever
assembly 41A-220, the locking cam 41A-250 and the serrated lever
41A-350 for the assembly procedure.
5 Remove the sequence shaft 41A-210 with the serrated lever assembly 41A-220,
the locking cam 41A-250, the link lever 41A-260 and the serrated lever 41A-350.

NOTE : It is only necessary to replace the bonded-in bearing 41A-240 from the
serrated lever 41A-230 if it is damaged, see REPAIR .

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**For PN’s D5237310002000

TASK 52-32-17-000-808-C01
Removal and Disassembly of the Sequence Shaft
1. General
A. Put the door in a support with the correct shape to prevent damage.
-

NOTE : See REPAIR TASK 52-32-17-300-803-A01 for the replacement of component parts
which have a permanent connection.
2. Job Set-up Information
A.Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-300-803-A01 Replacement of Parts
Referenced Information
TABLE 1

3. Procedure

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.

Subtask 52-32-17-000-020-A01
A. Removal and Disassembly of the Sequence Shaft

NOTE : See IPL_FIGURE_13, IPL_FIGURE_31B, IPL_FIGURE_40, IPL_FIGURE_41B,

IPL_FIGURE_95.
(1) Remove and disassemble the bellcrank housing assembly 40-020 as follows:
(a) Remove the fixed rods 40-010 and 40-100 from the link lever assembly 13-130, the
serrated lever assembly 41B-220 and the levers 40-070 as follows:
1 Remove and discard the cotter pins 40-110 and 40-230.
2 Remove the nuts 40-120 and 40-210, the washers 40-130 and 40-220, the bolts
40-140 and 40-250 and the washers 40-150 and 40-240 and remove the fixed
rods 40-010 and 40-100.

NOTE : Measure and record the length of the fixed rod 40-010 between the
centers of the clevis 95-010 and 95-020 for the assembly procedure.

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NOTE : It is only necessary to replace the bonded-in bearings 40-090 from the
levers 40-080 if they are damaged, see REPAIR TASK
52-32-17-300-803-A01.
(b) Disassemble the fixed rod 40-010 as follows:

WARNING : USE GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE.

EACH TIME YOU CUT LOCKWIRE DURING THE TASK, REMOVE
AND DISCARD IT (THE UNWANTED LOCKWIRE) IMMEDIATELY.
LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND.
1 Cut and remove the lockwire from the nuts 95-030 and 95-040 and the locking
washers 95-050.
2 Loosen the nuts 95-030 and 95-040
3 Remove the clevis 95-010 and 95-020 with the nuts 95-030 and 95-040 and the
locking washers 95-050 from the rod body.
4 Remove the nuts 95-030 and 95-040 and the locking washers 95-050 from the
clevis 95-010 and 95-020.
5 Discard the lockwire and the locking washers 95-050.
(c) Remove and disassemble the bellcrank housing assembly 40-020 as follows:
1 Remove the bolts 40-190, the washers 40-200 and remove the bellcrank housing
assembly 40-020 from the door structure.
2 Remove the nuts 40-170, the sleeves 40-180 and the taper pins 40-160.
3 Remove the beam-4 shaft 40-060 and the levers 40-080 from the beam-4 cover
40-030.

NOTE : It is only necessary to replace the shouldered bushings 40-050 from the
cover 40-040 if they are damaged, see REPAIR TASK
52-32-17-300-803-A01.
(2) Remove and disassemble the sequence shaft assembly 41B-200 as follows:
(a) Remove and disassemble the link assembly 41B-010 as follows:
1 Remove and discard the cotter pins 41B-110 and 41B-360.
2 Remove the nuts 41B-100 and 41B-340, the washers 41B-090 and 41B-290 and
the bolts 41B-080 and 41B-320.
3 Remove the link assembly 41B-010 with the sleeves 41B-070 and 41B-330 and
the bushing 41B-270.
4 Release the tab washers 41B-040 and loosen the nuts 41B-030 and 41B-050 and
remove the forks 41B-020 and 41B-060, the tab washers 41B-040 and the nuts
41B-030 and 41B-050 from the rod 41B-120.
5 Discard the tab washers 41B-040.

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(b) Remove the lever assembly 41B-130 as follows:

1 Remove and discard the cotter pin 41B-390.
2 Remove the nut 41B-370, the washer 41B-380 and the lever 41B-140 from the
fitting support 41B-170.

NOTE : It is only necessary to replace the shouldered bushings 41B-150 and

the bushing 41B-160 from the lever 41B-140 if they are damaged, see
REPAIR TASK 52-32-17-300-803-A01.

NOTE : It is only necessary to replace the riveted fitting support 41B-170 if it

is damaged, see REPAIR TASK 52-32-17-300-803-A01.
(c) Remove the connecting rod assembly 41B-440 as follows:
1 Remove and discard the cotter pins 41B-390.
2 Remove the nuts 41B-370, the washers 41B-380, the bolts 41B-400, the washers
41B-410 and remove the connecting rod assembly 41B-440 from the serrated
lever 41B-350 and the lever 31B-060.

NOTE : It is only necessary to replace the bonded-in bearings 41B-460 from

the connecting rod 41B-450 if they are damaged, see REPAIR TASK
52-32-17-300-803-A01.
(d) Remove and disassemble the sequence shaft assembly 41B-200 as follows:
1 Release the lockwasher 41B-430 and remove the screw 41B-420.
2 Discard the lockwasher 41B-430.
3 Remove the nuts 41B-300 and 41B-470, the washers 41B-480, the bolt 41B-310
and the rivet pins 41B-280.
4 Discard the rivet pins 41B-280 and the nuts 41B-470.

NOTE : Record the position of the link lever 41B-260, the serrated lever
assembly 41B-220, the locking cam 41B-250 and the serrated lever
41B-350.
5 Remove the sequence shaft 41B-210 with the serrated lever assembly 41B-220,
the locking cam 41B-250, the link lever 41B-260 and the serrated lever 41B-350.

NOTE : It is only necessary to replace the bonded-in bearing 41B-240 from the
serrated lever 41B-230 if it is damaged, see REPAIR TASK
52-32-17-300-803-A01.

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**For PN’s ALL

TASK 52-32-17-000-809-A01
Removal of the Vent Door Actuating Mechanism
1. General
A. Put the door in a support with the correct shape to prevent damage.
-

NOTE : See REPAIR TASK 52-32-17-300-803-A01 for the replacement of component parts
which have a permanent connection.
2. Job Set-up Information
A.Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-300-803-A01 Replacement of Parts
Referenced Information
TABLE 1

3. Procedure

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.

Subtask 52-32-17-000-009-A01
A. Removal of the Vent Door Actuating Mechanism

NOTE : See IPL_FIGURE_13, IPL_FIGURE_20, IPL_FIGURE_95, IPL_FIGURE_96,

IPL_FIGURE_97.
(1) Remove the cover 20-240 as follows:
(a) Remove the nuts 20-270, the washers 20-260, the screws 20-250, the spacers 20-280
and the cover 20-240 from the door structure.
(2) Remove and disassemble the rod assembly 20-060 as follows:
(a) Remove the rod assembly 20-060 as follows:
1 Remove and discard the cotter pins 20-040.
2 Remove the nuts 20-050, the washers 20-030, the bolts 20-020 and 20-080, the
washers 20-030 and 20-070 and the rod assembly 20-060 from the vent door
assembly 20-010 and the link lever assembly 20-100.

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3 Measure and record the length of the rod assembly 20-060 between the centers
of the rod ends for the assembly procedure.

WARNING : USE GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH

TIME YOU CUT LOCKWIRE DURING THE TASK, REMOVE AND
DISCARD IT (THE UNWANTED LOCKWIRE) IMMEDIATELY. LOOSE
LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND.
(b) Disassemble the rod assembly 20-060 as follows:
1 Cut, remove and discard the lockwire from the nuts 95-030 and 95-040 and the
locking devices 95-050.
2 Loosen the nuts 95-030 and 95-040.
3 Remove the rod ends 95-010 and 95-020 with the nuts 95-030 and 95-040 and
the locking devices 95-050 from the rod body.
4 Remove the nuts 95-030 and 95-040 and the locking devices 95-050 from the
rod ends 95-010 and 95-020.
(3) Remove the rod assembly 20-150 as follows:
(a) Remove and discard the cotter pins 20-040.
(b) Remove the nuts 20-050, the washers 20-030, the bolts 20-080, the washers 20-070
and remove the rod assembly 20-150.
(c) Do not disassemble the rod assembly 20-150.
(4) Remove the bellcrank assembly 20-090 as follows:
(a) Remove the nuts 20-140, 20-310, the sleeves 20-130, 20-300, the taper pins 20-120,
20-290, the beam-3 shaft 20-110 and the link lever assemblies 20-100 from the door
structure.

NOTE : It is only necessary to replace the bonded-in bearings 20-107 from the link
levers 20-105 if they are damaged, see REPAIR TASK 52-32-17-300-803-
A01.
(5) Remove the bellcrank assembly 20-160 as follows:
(a) Remove and discard the cotter pin 20-040.
(b) Remove the nut 20-050, the washer 20-030, the bolt 20-080, the washer 20-070 and
the rod assembly 13-260 from the link lever assembly 20-180.
(c) Remove the nuts 20-210, 20-310, the sleeves 20-200, 20-300, the taper pins 20-190,
20-290, the beam-3 shaft 20-170, the link lever assemblies 20-180 and 20-220 and the
bush 20-230 from the door structure.

NOTE : It is only necessary to replace the bonded-in bearings 20-187 and 20-227
from the link levers 20-185 and 20-225 if they are damaged, see REPAIR
TASK 52-32-17-300-803-A01.

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NOTE : It is only necessary to replace the shouldered bushings 96-190 and 97-260
from the door structure if they are damaged, see REPAIR TASK
52-32-17-300-803-A01.

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**For PN’s ALL

TASK 52-32-17-000-810-A01
Removal and Disassembly of the Vent Door Assembly
1. General
A. Put the door in a support with the correct shape to prevent damage.
-

NOTE : See REPAIR TASK 52-32-17-300-803-A01 for the replacement of component parts
which have a permanent connection.
2. Job Set-up Information
A.Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-300-803-A01 Replacement of Parts
TASK 52-32-17-000-809-A01 Removal of the Vent Door Actuating Mechanism
Referenced Information
TABLE 1

3. Procedure

Subtask 52-32-17-000-010-A01
A. Removal and Disassembly of the Vent Door Assembly

NOTE : See IPL_FIGURE_20, IPL_FIGURE_21.

(1) Remove the vent door assembly 21-120 as follows:
(a) Remove the rod assembly 20-060 from the vent door assembly 21-120, see
DISASSEMBLY TASK 52-32-17-000-809-A01.
(b) Remove and discard the cotter pins 21-010.

WARNING : THE SPRINGS ARE INSTALLED WITH LOAD. REMOVE THEM

CAREFULLY.
(c) Remove the nuts 21-020 and the washers 21-030, 21-031 and 21-040.
(d) Remove the sleeves 21-060.
(e) Remove the bolts 21-080 and 21-110, the washers 21-030 and 21-070 and the sleeve
21-100.
(f) Remove the washers 21-030, 21-031 and 21-040 and record the number and position
of the washers 21-030, 21-031 and 21-040 for the assembly procedure.
(g) Remove the springs 21-050 and 21-090.

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(h) Remove the vent door assembly 21-120 from the door structure.
(2) Disassemble the vent door assembly 21-120 as follows:

NOTE : It is only necessary to replace the pressure relief flap seal 21-410 from the vent
door 21-130 if it is damaged.

NOTE : It is only necessary to replace the riveted retainers 21-420 and 21-430 from the
vent door 21-130 if they are damaged, see REPAIR TASK 52-32-17-300-803-
A01.
(a) Remove and discard the cotter pins 21-400.
(b) Remove the washers 21-160.
(c) Remove the spring bolts 21-390.
(d) Release the tab washers 21-230 and 21-350.
(e) Loosen the nuts 21-220 and 21-340 and remove the bolts 21-210 and 21-330, the tab
washers 21-230 and 21-350 and the nuts 21-220 and 21-340 from the actuator arms
21-240 and 21-360.
(f) Discard the tab washers 21-230 and 21-350.
(g) Remove the nuts 21-150, the washers 21-160, the screws 21-140 and 21-170, the
actuator arm 21-240, the bracket 21-300 and the actuator arm 21-360 the from the
vent door 21-130.

NOTE : It is only necessary to replace the bushings 21-190 and 21-320 and the
shouldered bushings 21-200, 21-250 and 21-370 from the actuator arm
assemblies 21-180 and 21-310 if they are damaged, see REPAIR TASK
52-32-17-300-803-A01.

NOTE : It is only necessary to replace the bushing 21-290 and the shouldered
bushing 21-280 from the bracket assembly 21-270 if they are damaged, see
REPAIR TASK 52-32-17-300-803-A01.

NOTE : It is only necessary to replace the inserts 21-260 and 21-380 from the
actuator arm assemblies 21-180 and 21-310 if they are damaged, see
REPAIR TASK 52-32-17-300-803-A01.

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**For PN’s ALL

TASK 52-32-17-000-811-A01
Removal of the Latching Mechanism Assemblies
1. General
A. Put the door in a support with the correct shape to prevent damage.
-

NOTE : See REPAIR TASK 52-32-17-300-803-A01 for the replacement of component parts
which have a permanent connection.
2. Job Set-up Information
A.Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-300-803-A01 Replacement of Parts
Referenced Information
TABLE 1

3. Procedure

Subtask 52-32-17-000-011-A01
A. Removal of the Latching Mechanism Assemblies

NOTE : See IPL_FIGURE_30, IPL_FIGURE_96, IPL_FIGURE_97.

NOTE : Do the steps that follow for each of the four latching mechanism assemblies 30-020
and 30-030.
(1) Remove the latching mechanism assemblies 30-020 and 30-030 as follows:
(a) Remove and discard the cotter pin 30-270 from the nut 30-280.
(b) Remove the nut 30-280, the washer 30-240, the bolt 30-230, 30-290, the washer
30-240 and the bushings 30-250 and 30-260.
(c) Remove and discard the cotter pin 30-050 from the nut 30-060.
(d) Remove the nut 30-060, the washer 30-070, the bolt 30-080, the washer 30-090, the
bushings 30-100 and 30-110 and the sleeve 30-120.
(e) Remove the nut 30-150, the washer 30-140, the bolt 30-130 and the washer 30-140.
(f) Remove and discard the cotter pin 30-180 from the nut 30-190.
(g) Remove the nut 30-190, the washer 30-170, the bolt 30-160, the washer 30-170, the
bushing 30-200 and the sleeve 30-210.

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(h) Remove the latching mechanism assemblies 30-020 and 30-030 from the door
structure.

NOTE : It is only necessary to replace the bushings 96-020 and 96-050 and the
shouldered bushings 96-030, 96-040, 96-060, 96-070 and 96-080 from the
frame assembly 96-010 if they are damaged, see REPAIR TASK
52-32-17-300-803-A01.

NOTE : It is only necessary to replace the bushings 97-020 and 97-050 and the
shouldered bushings 97-030, 97-040, 97-060 and 97-070 from the frame
assembly 97-010 if they are damaged, see REPAIR TASK
52-32-17-300-803-A01.

NOTE : It is only necessary to replace the bushings 96-100 and 96-130 and the
shouldered bushings 96-110, 96-120, 96-140 and 96-150 from the frame
assembly 96-090 if they are damaged, see REPAIR TASK
52-32-17-300-803-A01.

NOTE : It is only necessary to replace the bushings 97-090, 97-120 and 97-150 and
the shouldered bushings 97-100, 97-110, 97-130 and 97-140 from the frame
assembly 97-080 if they are damaged, see REPAIR TASK
52-32-17-300-803-A01.

NOTE : It is only necessary to replace the shouldered bushing 97-170 from the
forward frame segment 97-160 if it is damaged, see REPAIR TASK
52-32-17-300-803-A01.

NOTE : It is only necessary to replace the shouldered bushings 97-190 and 97-200
from the aft frame segment 97-180 if they are damaged, see REPAIR TASK
52-32-17-300-803-A01.

NOTE : It is only necessary to replace the inserts 96-170 from the door structure if
they are damaged, see REPAIR TASK 52-32-17-300-803-A01.

NOTE : It is only necessary to replace the inserts 97-210 and 97-240 from the door
structure if they are damaged, see REPAIR TASK 52-32-17-300-803-A01

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**For PN’s ALL

TASK 52-32-17-000-812-A01
Disassembly of the Latching Hook Assemblies
1. General
A. Put the door in a support with the correct shape to prevent damage.
-

NOTE : See REPAIR TASK 52-32-17-300-803-A01 for the replacement of component parts
which have a permanent connection.
2. Job Set-up Information
A.Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-300-803-A01 Replacement of Parts
Referenced Information
TABLE 1

3. Procedure

Subtask 52-32-17-000-012-A01
A. Disassembly of the Latching Hook Assemblies

NOTE : See IPL_FIGURE_33, IPL_FIGURE_34.

NOTE : Do the steps that follow for each of the four latching hook assemblies.
(1) Disassemble the latching hook mechanism 33-010, 34-010 as follows:
(a) Remove and discard the cotter pins 33-140, 34-140 from the nuts 33-120, 34-120.
(b) Remove the nuts 33-120, 34-120, the washers 33-130, 34-130, the bolts 33-080 and
33-150, 34-080 and 34-150 and the washers 33-090, 34-090.
(c) Disconnect the connecting link 33-070, 34-070 from the bellcrank assembly 33-160,
34-160 and the latching hook assembly 33-010, 34-010.
(d) Remove the bushings 33-100 and 33-110, 34-100 and 34-110 from the connecting link
33-070, 34-070.

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(e) Remove the sleeves 33-060, 34-060 from the latching hook assembly 33-010, 34-010
and the bellcrank assembly 33-160, 34-160.

NOTE : It is only necessary to replace the shouldered bushings 33-040 and 33-050,
34-040 and 34-050 and the lubrication fitting 33-030, 34-030 from the
latching hook 33-020, 34-020 if they are damaged, see REPAIR TASK
52-32-17-300-803-A01.
(f) Remove and discard the cotter pin 33-140, 34-140 from the nut 33-250, 34-250.
(g) Remove the nut 33-250, 34-250, the washer 33-220, 34-220, the bolt 33-210, 34-210,
the washer 33-220, 34-220, the bushing 33-240, 34-240 and remove the connecting
rod 33-260, 34-260 from the bellcrank 33-170, 34-170.

NOTE : It is only necessary to replace the bushing 33-180, 34-180, the shouldered
bushing 33-190, 34-190 and the lubrication fitting 33-200, 34-200 from the
bellcrank 33-170, 34-170 if they are damaged, see REPAIR TASK
52-32-17-300-803-A01.

NOTE : It is only necessary to replace the bushing 33-230, 34-230 from the
bellcrank 33-170, 34-170 if it is damaged, see REPAIR TASK
52-32-17-300-803-A01.
(h) Do not disassemble the connecting rod 33-260, 34-260.

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**For PN’s D5237310000000 D5237310000200 D5237310000400 D5237310000800

TASK 52-32-17-000-813-A01
Removal and Disassembly of the Latching Shaft Assembly
1. General
A. Put the door in a support with the correct shape to prevent damage.
-

NOTE : See REPAIR for the replacement of component parts which have a permanent
connection.
2. Job Set-up Information
A.Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-000-805-A01 Removal of the Hand Lever Mechanism
TASK 52-32-17-000-811-A01 Removal of the Latching Mechanism Assemblies
Referenced Information
TABLE 1

3. Procedure

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.

Subtask 52-32-17-000-013-A01
A. Removal and Disassembly of the Latching Shaft Assembly

NOTE : See IPL_FIGURE_32.

(1) Remove and disassemble the latching shaft 32-010 as follows:
(a) Make sure that the hand lever mechanism, see DISASSEMBLY TASK
52-32-17-000-805-A01 and the latching mechanism assemblies, see DISASSEMBLY
TASK 52-32-17-000-811-A01 are disconnected.
(b) Remove the nuts 32-050, the sleeves 32-040 and the taper pins 32-030 and 32-060.
(c) Remove the latching shaft 32-010, the shaft levers 32-020 and 32-070, the switch
lever 32-090, the hinged lever assembly 32-100 and the stop cam 32-080.

NOTE : Record the positions of the shaft levers 32-020 and 32-070 for the assembly
procedure.

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NOTE : It is only necessary to replace the bonded-in bearing 32-120 from the hinged
lever 32-110 if it is damaged, see REPAIR .

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**For PN’s D5237310000600 D5237310001000 D5237310001200 D5237310001400 D5237310002000

TASK 52-32-17-000-813-B01
Removal and Disassembly of the Latching Shaft Assembly
1. General
A. Put the door in a support with the correct shape to prevent damage.
-

NOTE : See REPAIR TASK 52-32-17-300-803-A01 for the replacement of component parts
which have a permanent connection.
2. Job Set-up Information
A.Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-300-803-A01 Replacement of Parts
TASK 52-32-17-000-805-A01 Removal of the Hand Lever Mechanism
TASK 52-32-17-000-811-A01 Removal of the Latching Mechanism Assemblies
Referenced Information
TABLE 1

3. Procedure

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.

Subtask 52-32-17-000-026-A01
A. Removal and Disassembly of the Latching Shaft Assembly

NOTE : See IPL_FIGURE_32A.

(1) Remove and disassemble the latching shaft 32A-020 as follows:
(a) Make sure that the hand lever mechanism, see DISASSEMBLY TASK
52-32-17-000-805-A01 and the latching mechanism assemblies, see DISASSEMBLY
TASK 52-32-17-000-811-A01 are disconnected.
(b) Remove the nuts 32A-130, the sleeves 32A-120 and the taper pins 32A-100 and
32A-110.

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(c) Remove the latching shaft 32A-020, the shaft levers 32A-030 and 32A-040, the switch
lever 32A-060, the hinged lever assembly 32A-070 and the stop cam 32A-050.

NOTE : Record the positions of the shaft levers 32A-030 and 32A-040 for the
assembly procedure.

NOTE : It is only necessary to replace the bonded-in bearing 32A-090 from the
hinged lever 32A-080 if it is damaged, see REPAIR TASK
52-32-17-300-803-A01.

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**For PN’s ALL

TASK 52-32-17-000-814-A01
Removal and Disassembly of the Interlock Mechanism
1. General
A. Put the door in a support with the correct shape to prevent damage.
-

NOTE : See REPAIR TASK 52-32-17-300-803-A01 for the replacement of component parts
which have a permanent connection.
2. Job Set-up Information
A.Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-300-803-A01 Replacement of Parts
Referenced Information
TABLE 1

3. Procedure

Subtask 52-32-17-000-014-A01
A. Removal and Disassembly of the Interlock Mechanism

NOTE : See IPL_FIGURE_44.

(1) Remove the interlock mechanism 44-090 as follows:

WARNING : THE COMPRESSION SPRING IS INSTALLED WITH LOAD. REMOVE IT

CAREFULLY.
(a) Compress the compression spring 44-040 and the spring sleeve assembly 44-010 to
decrease its length.
(b) Remove and discard the cotter pins 44-060 from the pins 44-050.
(c) Remove and discard the cotter pin 44-280 from the nut 44-240.
(d) Remove the nut 44-240, the washer 44-250, the bolt 44-270 and the washer 44-250.
(e) Remove and discard the cotter pin 44-060 from the nut 44-290.
(f) Remove the nut 44-290, the washer 44-070, the bolt 44-300 and the washer 44-220.
(g) Remove the bushings 44-230 and 44-260 and the interlock mechanism 44-090 from
the door structure.
(h) Remove the washer 44-070 and the pin 44-050.

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(i) Remove the washer 44-070, the pin 44-050, the spacers 44-080 and remove the spring
sleeve assembly 44-010 and the compression spring 44-040.

NOTE : It is only necessary to replace the pressed-in bushing 44-030 from the spring
sleeve 44-020 if it is damaged, see REPAIR TASK 52-32-17-300-803-A01.
(2) Disassemble the interlock mechanism 44-090 as follows:
(a) Remove the retaining ring 44-160, the pin 44-110 and the bolt 44-210.
(b) Remove the retaining rings 44-160, the pins 44-110 and the connecting rod 44-150
from the levers 44-100 and 44-170.
(c) Remove the adjusting screw 44-180, the nut 44-190 and the locking plate 44-200 from
the lever 44-170.
(d) Remove the retaining ring 44-120, the pin 44-130 and the roller 44-140 from the lever
44-100.

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**For PN’s D5237310000000 D5237310000200 D5237310000400 D5237310000800

TASK 52-32-17-000-815-A01
Removal of the Locking Shaft Assembly
1. General
A. Put the door in a support with the correct shape to prevent damage.
-

NOTE : See REPAIR for the replacement of component parts which have a permanent
connection.
2. Job Set-up Information
A.Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-000-805-A01 Removal of the Hand Lever Mechanism
TASK 52-32-17-000-810-A01 Removal and Disassembly of the Vent Door Assembly
TASK 52-32-17-000-807-A01 Removal and Disassembly of the Adjustable Rods and the Drift Pin
Rods
Referenced Information
TABLE 1

3. Procedure

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.

Subtask 52-32-17-000-015-A01
A. Removal of the Locking Shaft Assembly

NOTE : See IPL_FIGURE_31.

(1) Remove the locking shaft 31-010 as follows:
(a) Make sure that the hand lever mechanism, see DISASSEMBLY TASK
52-32-17-000-805-A01, the vent door mechanism, see DISASSEMBLY TASK
52-32-17-000-810-A01 and the drift pin mechanism, see DISASSEMBLY TASK
52-32-17-000-807-A01 are disconnected.

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(b) Remove the nuts 31-030, the washers 31-040, the sleeves 31-050, the taper pins
31-020 and the rivet pins 31-070.

NOTE : Identify and record the position of the locking cams 31-080 for the assembly
procedure.
(c) Discard the nuts 31-030 and the rivet pins 31-070.
(d) Remove the locking shaft 31-010 with the lever 31-060 and the hinged lever assembly
31-090.

NOTE : It is only necessary to replace the bonded-in bearing 31-110 from the hinged
lever 31-100 if it is damaged, see REPAIR .

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**For PN’s D5237310000600 D5237310001000 D5237310001200 D5237310001400

TASK 52-32-17-000-815-B01
Removal of the Locking Shaft Assembly
1. General
A. Put the door in a support with the correct shape to prevent damage.
-

NOTE : See REPAIR for the replacement of component parts which have a permanent
connection.
2. Job Set-up Information
A.Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-000-805-A01 Removal of the Hand Lever Mechanism
TASK 52-32-17-000-810-A01 Removal and Disassembly of the Vent Door Assembly
TASK 52-32-17-000-807-A01 Removal and Disassembly of the Adjustable Rods and the Drift Pin
Rods
Referenced Information
TABLE 1

3. Procedure

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.

Subtask 52-32-17-000-022-A01
A. Removal of the Locking Shaft Assembly

NOTE : See IPL_FIGURE_31A.

(1) Remove the locking shaft 31A-020 as follows:
(a) Make sure that the hand lever mechanism, see DISASSEMBLY TASK
52-32-17-000-805-A01, the vent door mechanism, see DISASSEMBLY TASK
52-32-17-000-810-A01 and the drift pin mechanism, see DISASSEMBLY TASK
52-32-17-000-807-A01 are disconnected.

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(b) Remove the nuts 31A-090, the washers 31A-100, the sleeves 31A-110, the taper pins
31A-080 and the rivet pins 31A-120.

NOTE : Identify and record the position of the locking cams 31A-070 for the
assembly procedure.
(c) Discard the nuts 31A-090 and the rivet pins 31A-120.
(d) Remove the locking shaft 31A-020 with the lever 31A-060 and the hinged lever
assembly 31A-030.

NOTE : It is only necessary to replace the bonded-in bearing 31A-050 from the
hinged lever 31A-040 if it is damaged, see REPAIR .

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**For PN’s D5237310002000

TASK 52-32-17-000-815-C01
Removal of the Locking Shaft Assembly
1. General
A. Put the door in a support with the correct shape to prevent damage.
-

NOTE : See REPAIR TASK 52-32-17-300-803-A01 for the replacement of component parts
which have a permanent connection.
2. Job Set-up Information
A. Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-300-803-A01 Replacement of Parts
TASK 52-32-17-000-805-A01 Removal of the Hand Lever Mechanism
TASK 52-32-17-000-810-A01 Removal and Disassembly of the Vent Door Assembly
TASK 52-32-17-000-807-A01 Removal and Disassembly of the Adjustable Rods and the Drift Pin
Rods
Referenced Information
TABLE 1

3. Procedure

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.

Subtask 52-32-17-000-023-A01
A. Removal of the Locking Shaft Assembly

NOTE : See IPL_FIGURE_31B.

(1) Remove the locking shaft 31B-020 as follows:
(a) Make sure that the hand lever mechanism, see DISASSEMBLY TASK
52-32-17-000-805-A01, the vent door mechanism, see DISASSEMBLY TASK
52-32-17-000-810-A01 and the drift pin mechanism, see DISASSEMBLY TASK
52-32-17-000-807-A01 are disconnected.

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(b) Remove the nuts 31B-090 and 31B-130, the washers 31B-100, the sleeves 31B-110,
the taper pins 31B-080 and the rivet pins 31B-120.

NOTE : Identify and record the position of the locking cams 31B-070 for the
assembly procedure.
(c) Discard the nuts 31B-130 and the rivet pins 31B-120.
(d) Remove the locking shaft 31B-020 with the lever 31B-060 and the hinged lever
assembly 31B-030.

NOTE : It is only necessary to replace the bonded-in bearing 31B-050 from the
hinged lever 31B-040 if it is damaged, see REPAIR TASK
52-32-17-300-803-A01.

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**For PN’s ALL

TASK 52-32-17-000-816-A01
Removal of the Door Drainage
1. General
A. Put the door in a support with the correct shape to prevent damage.
-

NOTE : See REPAIR TASK 52-32-17-300-803-A01 for the replacement of component parts
which have a permanent connection.
2. Job Set-up Information
A.Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-300-803-A01 Replacement of Parts
Referenced Information
TABLE 1

3. Procedure

Subtask 52-32-17-000-016-A01
A. Removal of the Door Drainage

NOTE : See IPL_FIGURE_50.

(1) Remove the hose 50-010 as follows:
(a) Cut and discard the cable ties 50-100.
(b) Remove the nut 50-140, the washer 50-130, the bolt 50-120 and remove the mount
50-110 from the door structure.
(c) Remove the hose 50-010 from the door structure.
PRE SB 52-1124
(4) Remove the basic valve 50-030 and the tube 50-090 (Detail A) as follows:
(a) Remove the nuts 50-060, the washers 50-050 and the screws 50-040.
(b) Remove the flange 50-080 with the tube 50-090 from the door structure.
(c) Remove the basic valve 50-030 from the valve retainer 50-020.
(d) Remove the valve retainer 50-020 from the door structure.
(5) Remove the basic valve 50-030 (Detail B) as follows:
(a) Remove the nuts 50-060, the washers 50-050 and the screws 50-070.

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(b) Remove the basic valve 50-030 from the valve retainer 50-020.
(c) Remove the valve retainer 50-020 from the door structure.
POST SB 52-1124
(4) Remove the valve 50-031 and the tube assembly 50-090 (Detail A) as follows:
(a) Remove the nuts 50-060, the washers 50-050 and the screws 50-040.
(b) Remove the flange 50-080 with the tube assembly 50-090 from the door structure.
(c) Remove the valve 50-031 from the valve retainer 50-020.
(d) Remove the valve retainer 50-020 from the door structure.
(5) Remove the valve 50-031 (Detail B) as follows:
(a) Remove the nuts 50-060, the washers 50-050 and the screws 50-070.
(b) Remove the valve 50-031 from the valve retainer 50-020.
(c) Remove the valve retainer 50-020 from the door structure.

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**For PN’s ALL

TASK 52-32-17-000-817-A01
Removal of the Door Sensors
1. General
A. Put the door in a support with the correct shape to prevent damage.
-

NOTE : See REPAIR TASK 52-32-17-300-803-A01 for the replacement of component parts
which have a permanent connection.
2. Job Set-up Information
A.Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-300-803-A01 Replacement of Parts
Referenced Information
TABLE 1

3. Procedure

Subtask 52-32-17-000-017-A01
A. Removal of the Door Sensors

NOTE : See IPL_FIGURE_62.

NOTE : The rectangular proximity sensors 62-010 are referred to as proximity switches 62-010
in this paragraph.
(1) Remove the door sensors as follows:
(a) Disconnect the electrical harness from the proximity switches 62-010.
(b) Install blanking caps on the electrical connectors.
(c) Remove the proximity switch 12MJ 62-010 (Detail B) as follows:
1 Remove the screws 62-030 and remove the proximity switch 62-010 from the
door structure.
(d) Remove the proximity switch 32WV 62-010 (Detail C) as follows:
1 Remove the nuts 62-060, the washers 62-070, the screws 62-050 and remove the
proximity switch 62-010 from the door structure.

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(e) Remove the targets 62-020 as follows:

1 Remove the nuts 62-060, the washers 62-070, the screws 62-030, 62-040 and
62-050, the washers 62-070 and remove the targets 62-020 from the door
structure.

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**For PN’s D5237310000000 D5237310000200 D5237310000400 D5237310000800

TASK 52-32-17-000-818-A01
Removal of the Door Hinge Assemblies
1. General
A. Put the door in a support with the correct shape to prevent damage.
-

NOTE : See REPAIR for the replacement of component parts which have a permanent
connection.
2. Procedure

Subtask 52-32-17-000-018-A01
A. Removal of the Door Hinge Assemblies

NOTE : See IPL_FIGURE_90.

(1) Remove the end fitting 90-010 as follows:
(a) Remove the nuts 90-120, the washers 90-110 and the screws 90-100 and remove the
end fitting 90-010 and the shims 90-090, 90-091, 90-092, 90-093, 90-094, 90-095,
90-096, 90-097, 90-098, 90-099, from the door structure 90-220.

NOTE : Measure and record the thickness of the shims 90-090, 90-091, 90-092,
90-093, 90-094, 90-095, 90-096, 90-097, 90-098, 90-099 for the assembly
procedure.
(2) Remove the hinge assemblies 90-020 and 90-050 as follows:
(a) Remove the nuts 90-120, 90-125 and 90-150, the washers 90-110, 90-115 and 90-140
and the screws 90-100, 90-105 90-130, 90-160, 90-170, 90-180, 90-190, 90-195,
90-200 and 90-210 and remove the hinge assemblies 90-020 and 90-050 from the door
structure 90-220.

NOTE : It is only necessary to replace the hinge assemblies 90-020 and 90-050 from
the door structure 90-220 if they are damaged. If you replace a hinge
assembly, you must measure and record the position and the thickness of
the hinge shims for the assembly procedure.

NOTE : It is only necessary to replace the bushings 90-040 from the outer hinge
90-030 if they are damaged, see REPAIR .

NOTE : It is only necessary to replace the bushings 90-070 and the shouldered
bushings 90-080 from the mid hinge 90-060 if they are damaged, see
REPAIR .

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Subtask 52-32-17-000-021-A01
B. Removal of the Door Hinge Assemblies

NOTE : See IPL_FIGURE_91.

(1) Remove the end fitting 91-080 as follows:
(a) Remove the nuts 91-120, the washers 91-110 and the screws 91-100 and remove the
end fitting 91-080 and the shims 91-090, 91-091, 91-092, 91-093, 91-094, 91-095,
91-096, 91-097, 91-098, 91-099.

NOTE : Measure and record the thickness of the shims 91-090, 91-091, 91-092,
91-093, 91-094, 91-095, 91-096, 91-097, 91-098, 91-099 for the assembly
procedure.
(2) Remove the hinge assemblies 91-010 and 91-050 as follows:
(a) Remove the nuts 91-120, 91-125 and 91-150, the washers 91-110, 91-115 and 91-140
and the screws 91-100, 91-105, 91-130, 91-160, 91-170, 91-180, 91-185, 91-190 and
91-200 and remove the hinge assemblies 91-010 and 91-050 from the door structure.

NOTE : It is only necessary to replace the hinge assemblies 91-010 and 91-050 from
the door structure if they are damaged. If you replace a hinge assembly, you
must measure and record the position and the thickness of the hinge shims
for the assembly procedure.

NOTE : It is only necessary to replace the bushings 91-070 from the outer hinge
91-060 if they are damaged, see REPAIR .

NOTE : It is only necessary to replace the bushings 91-030 and the shouldered
bushings 91-040 from the mid hinge 91-020 if they are damaged, see
REPAIR .

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D5237310000000

**For PN’s D5237310000600 D5237310001000 D5237310001200 D5237310001400 D5237310002000

TASK 52-32-17-000-818-B01
Removal of the Door Hinge Assemblies
1. General
A. Put the door in a support with the correct shape to prevent damage.
-

NOTE : See REPAIR TASK 52-32-17-300-803-A01 for the replacement of component parts
which have a permanent connection.
2. Job Set-up Information
A.Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-300-803-A01 Replacement of Parts
Referenced Information
TABLE 1

3. Procedure

Subtask 52-32-17-000-024-A01
A. Removal of the Door Hinge Assemblies

NOTE : See IPL_FIGURE_90A.

(1) Remove the end fitting 90A-010 as follows:
(a) Remove the nuts 90A-120, the washers 90A-110, the screws 90A-100 and remove the
end fitting 90A-010 and the shims 90A-090, 90A-091, 90A-092, 90A-093, 90A-094,
90A-095, 90A-096, 90A-097, 90A-098, 90A-099 from the door structure 90A-220.

NOTE : Measure and record the thickness of the shims 90A-090, 90A-091, 90A-092,
90A-093, 90A-094, 90A-095, 90A-096, 90A-097, 90A-098, 90A-099 for the
assembly procedure.
(2) Remove the hinge assemblies 90A-020 and 90A-050 as follows:
(a) Remove the nuts 90A-120, 90A-150 and 90A-155, the washers 90A-110, 90A-140 and
90A-145 and the screws 90A-100, 90A-130, 90A-160, 90A-170, 90A-175, 90A-180,
90A-185, 90A-190, 90A-200 and 90A-210 and remove the hinge assemblies 90A-020
and 90A-050 from the door structure 90A-220.

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NOTE : It is only necessary to replace the hinge assemblies 90A-020 and 90A-050
from the door structure 90A-220 if they are damaged. If you replace a hinge
assembly, you must measure and record the position and the thickness of
the hinge shims for the assembly procedure.

NOTE : It is only necessary to replace the bushings 90A-040 from the outer hinge
90A-030 if they are damaged, see REPAIR TASK 52-32-17-300-803-A01.

NOTE : It is only necessary to replace the bushings 90A-070 and the shouldered
bushings 90A-080 from the mid hinge 90A-060 if they are damaged, see
REPAIR TASK 52-32-17-300-803-A01.

Subtask 52-32-17-000-025-A01
B. Removal of the Door Hinge Assemblies

NOTE : See IPL_FIGURE_91A.

(1) Remove the end fitting 91A-080 as follows:
(a) Remove the nuts 91A-120, the washers 91A-110 and the screws 91A-100 and remove
the end fitting 91A-080 and the shims 91A-090, 91A-091, 91A-092, 91A-093,
91A-094, 91A-095, 91A-096, 91A-097, 91A-098, 91A-099.

NOTE : Measure and record the thickness of the shims 91A-090, 91A-091, 91A-092,
91A-093, 91A-094, 91A-095, 91A-096, 91A-097, 91A-098, 91A-099 for the
assembly procedure.
(2) Remove the hinge assemblies 91A-010 and 91A-050 as follows:
(a) Remove the nuts 91A-120, 91A-150 and 91A-155, the washers 91A-110, 91A-140 and
91A-145 and the screws 91A-100, 91A-130, 91A-160, 91A-165, 91A-170, 91A-175,
91A-180, 91A-190, 91A-200 and remove the hinge assemblies 91A-010 and 91A-050
from the door structure.

NOTE : It is only necessary to replace the hinge assemblies 91A-010 and 91A-050
from the door structure if they are damaged. If you replace a hinge
assembly, you must measure and record the position and the thickness of
the hinge shims for the assembly procedure.

NOTE : It is only necessary to replace the bushings 91A-070 from the outer hinge
91A-060 if they are damaged, see REPAIR TASK 52-32-17-300-803-A01.

NOTE : It is only necessary to replace the bushings 91A-030 and the shouldered
bushings 91A-040 from the mid hinge 91A-020 if they are damaged, see
REPAIR TASK 52-32-17-300-803-A01.

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CLEANING

**For PN’s ALL

TASK 52-32-17-100-801-A01
Cleaning
1. General
A. Make sure that all dirt, grease, sealant and cleaning agent is removed.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
08ABC1 Aqueous Cleaner-Aircraft Exterior Pressure Spraying -
14SBA1 Textile-Lint free Cotton -
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
08BBD1 Non Aqueous Cleaner-- Isopropyl Alcohol -
08AFA1 Aqueous Cleaner-Transparent Plastic - -
Consumable Materials
TABLE 1

B. Fixtures, Tools, Test and Support Equipment

REFERENCE DESIGNATION
vacuum cleaner
Fixtures, Tools, Test and Support Equipment
TABLE 2

3. Procedure

WARNING : BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

CAUTION : USE ONLY THE SPECIFIED CLEANING AGENTS. CLEANING AGENTS WHICH
ARE NOT SPECIFIED CAN CAUSE DAMAGE.

Subtask 52-32-17-100-001-A01
A. Clean the component parts which are painted
(1) Remove all the loose particles and other dirt with a vacuum cleaner or a soft brush.
(2) Remove old sealant and remaining dirt with a nonmetallic scraper.

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(3) Clean the component parts which are painted with the Material No. 08ABC1 Aqueous
Cleaner-Aircraft Exterior Pressure Spraying -.
(a) Use a soft brush or a clean Material No. 14SBA1 Textile-Lint free Cotton -.
(4) Remove the Material No. 08ABC1 Aqueous Cleaner-Aircraft Exterior Pressure Spraying -
with clean water.
(5) Dry the component parts which are painted with a clean Material No. 14SBA1 Textile-Lint
free Cotton - or a hot-air blower.

Subtask 52-32-17-100-002-A01
B. Clean the component parts which are not painted
(1) Remove all the loose particles and other dirt with a vacuum cleaner or a soft brush.
(2) Remove the remaining dirt with a nonmetallic scraper.
(3) Clean the component parts which are not painted with a clean Material No. 14SBA1
Textile-Lint free Cotton - made moist with the Material No. 08BBF1 Non Aqueous
Cleaner-- Methyl-Ethyl-Ketone -.
(a) Use a soft brush or a clean Material No. 14SBA1 Textile-Lint free Cotton - to dry the
components which are not painted.

Subtask 52-32-17-100-003-A01
C. Clean the Electrical Components
(1) Clean the electrical wiring with a clean Material No. 14SBA1 Textile-Lint free Cotton - and
the Material No. 08BBD1 Non Aqueous Cleaner-- Isopropyl Alcohol - or an equivalent
cleaning agent.
(2) Clean the electrical connectors with a clean Material No. 14SBA1 Textile-Lint free Cotton -
and the Material No. 08BBD1 Non Aqueous Cleaner-- Isopropyl Alcohol -.

Subtask 52-32-17-100-004-A01
D. Clean the Sight Glasses

NOTE : See IPL_FIGURE_03, IPL_FIGURE_70.

CAUTION : DO NOT RUB THE SURFACE WITH DRY CLOTH.

(1) Clean the sight glasses 03-020 and 70-022 with a weak soap solution.
(2) Dry the sight glasses 03-020 and 70-022 with a clean Material No. 14SBA1 Textile-Lint
free Cotton -.
(3) If more cleaning is required, clean the sight glasses 03-020 and 70-022 with the Material
No. 08AFA1 Aqueous Cleaner-Transparent Plastic - - and dry them with a clean Material
No. 14SBA1 Textile-Lint free Cotton -.

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Subtask 52-32-17-100-005-A01
E. Clean the Door Seal
(1) Clean the door seal with a weak soap solution.
(2) Dry the clean seals with a clean, dry, Material No. 14SBA1 Textile-Lint free Cotton - or
with dry compressed air.
(3) Apply Talcum powder to the door seal.

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INSPECTION/CHECK

**For PN’s ALL

TASK 52-32-17-200-801-A01
Door Structure
1. General
A. This check is a visual inspection of the component parts.
B. Do an approved nondestructive test if you think there is a crack which is not clearly visible.
C. See the Structural Repair Manual (SRM) for the repair of the door structure.
-

NOTE : See REPAIR TASK 52-32-17-300-803-A01 for the replacement of the permanently
attached parts.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
12ABC1 Corrosion Preventive Compound-Water Displacing Soft Film -
12ACC1 Corrosion Preventive Compound-Heavy Duty Soft Film -
Consumable Materials
TABLE 1

B. Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-300-803-A01 Replacement of Parts
TASK 52-32-17-300-801-A01 Reworking or Machining
PMS 01-02-43
FIGURE 52-32-17-991-008-A FIGURE 52-32-17-991-008-A-Visual Examination of the Surface
Protection and Locking Mechanism
Referenced Information
TABLE 2

3. Procedure

WARNING : BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

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CAUTION : THE LIMITS OF ALLOWABLE DAMAGE ARE ALWAYS RELATED TO THE

NOMINAL MATERIAL THICKNESS OF THE COMPONENT PARTS.

Subtask 52-32-17-210-001-A01
A. Check of the Door Structure for Damage.
(1) Do a check of the door structure for damage:
(a) For the Allowable Damage Limits (ADL) and the repair procedure see the Structural
Repair Manual (SRM).
(b) Make sure that all inner surfaces of the door structure have a protection of the
Material No. 12ABC1 Corrosion Preventive Compound-Water Displacing Soft Film -
see FIGURE 52-32-17-991-008-A, see PMS 01-02-43.
(c) Make sure that the outer surface of the door structure has a protection of the
Material No. 12ACC1 Corrosion Preventive Compound-Heavy Duty Soft Film -, see
FIGURE 52-32-17-991-008-A.

Subtask 52-32-17-210-002-A01
B. Structure Components

NOTE : See IPL_FIGURE_04, IPL_FIGURE_90, IPL_FIGURE_91 for the X-Stops and Hinges.

CAUTION : THE LIMITS ARE ALWAYS RELATED TO THE NOMINAL MATERIAL

THICKNESS.
(1) Do a check of structure components for cracks or corrosion.
(a) Cracks and corrosion are not permitted.
(b) See DISASSEMBLY and 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 (0.009 in).
(b) See REPAIR TASK 52-32-17-300-801-A01 for the removal of scratches or marks
which are in the limits.
(c) See DISASSEMBLY and ASSEMBLY for the replacement of the structure
components which have scratches or marks that are not in the limits.

Subtask 52-32-17-210-003-A01
C. Door Seal
(1) Do a check of the door seal for hardening, cracks, oil contamination and porosity.
(a) Hardening, cracks, oil contamination or porosity are not permitted.

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(b) See DISASSEMBLY and ASSEMBLY for the replacement of the door seal if there is
such damage.
(c) See REPAIR TASK 52-32-17-300-801-A01 for the removal of cracks.

Subtask 52-32-17-210-004-A01
D. Self-adhesive and Bonded Identification Plates

NOTE : See IPL_FIGURE_01.

(1) Do a check of the identification plate for readability and attachment.
(a) Loose or damaged identification plates are not permitted.
(b) See REPAIR TASK 52-32-17-300-803-A01 for the replacement of the damaged
identification plates.

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**For PN’s ALL

DOOR
SEAL

FR57A

DOOR
INSULATION

CORROSION PREVENTIVE CORROSION PREVENTIVE

(MATERIAL NO. 12ABC1) (MATERIAL NO. 12ACC1)

DOOR
STRUCTURE

DOOR SURFACE PROTECTION

LOCKING SHAFT

83

AREA OF RED MARKING

43
AREA OF GREEN MARKING

LOCKING CAM

TYPICAL DIRECT VISUAL LOCKING INDICATION

F_CM_523217_1_0080101_01_01

Visual Examination of the Surface Protection and Locking Mechanism

FIGURE-52-32-17-991-008-A01

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**For PN’s ALL

TASK 52-32-17-210-801-A01
Check of the Door Mechanism and the Locking Mechanism
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. See the Structural Repair Manual (SRM) for the door structure.
-

NOTE : See REPAIR TASK 52-32-17-300-803-A01 for the replacement of the permanently
attached parts.
2. Job Set-up Information
A.Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-300-803-A01 Replacement of Parts
TASK 52-32-17-300-801-A01 Reworking or Machining
TASK 52-32-17-820-808-A01 Fits and Clearances
FIGURE 52-32-17-991-009-A FIGURE 52-32-17-991-009-A-Test Data of the Torsion Spring
Referenced Information
TABLE 1

3. Procedure

CAUTION : THE LIMITS OF ALLOWABLE DAMAGE ARE ALWAYS RELATED TO THE

NOMINAL MATERIAL THICKNESS OF THE COMPONENT PARTS.

Subtask 52-32-17-210-005-A01
A. Door Mechanism
(1) Do a check of the component parts of the door mechanism for wear.
(a) See FITS AND CLEARANCES TASK 52-32-17-820-808-A01 for the wear limits.
(b) See DISASSEMBLY and ASSEMBLY for the replacement of component parts with
wear not in the limits.

Subtask 52-32-17-210-006-A01
B. Locking Mechanism

CAUTION : THE LIMITS ARE ALWAYS RELATED TO THE NOMINAL MATERIAL

THICKNESS.

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(1) Check for cracks.

(a) Cracks are not permitted.
(b) See DISASSEMBLY and 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 (0.009 in).
(b) See REPAIR TASK 52-32-17-300-801-A01 for the removal of the scratches, marks
and corrosion which are in the limits.
(c) See DISASSEMBLY and ASSEMBLY for the replacement of the parts which have
scratches, marks and corrosion that are not in the limits.
(3) Check for deformation.
(a) Deformation is not permitted.
(b) See DISASSEMBLY and ASSEMBLY for the replacement of the parts which have
deformation.
(4) Check for wear.
(a) See REPAIR for the repair of the parts which have wear.
(b) Make sure that the maximum outer diameter of the spring bolt 08-460 is not less than
6.25 mm (0.247 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.
(b) See DISASSEMBLY and ASSEMBLY for the replacement of the parts which have
other damage.

Subtask 52-32-17-210-007-A01
C. Springs
(1) Check for damage.
(a) Damage is not permitted.
(b) See DISASSEMBLY and ASSEMBLY for the replacement of the springs which have
damage.
(2) Check the spring data.
(a) For the test data see TABLE 2 and TABLE 3.
(b) For the torsion spring see FIGURE 52-32-17-991-009-A.

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(c) See DISASSEMBLY and ASSEMBLY for the replacement of the springs which have
test data that is not in the limits.
IPL FIG. ITEM FREE LENGTH TEST LENGTH LOAD daN (lbf.)
mm (in) mm (in)
IPL_FIGURE_08 Compression spring 61.0 45.20 22.43 - 29.70
08-470 (2.401) (1.780) (50.43 - 66.76)
IPL_FIGURE_44 Compression spring 98.0 78.0 6.07 - 8.09
44-040 (3.858) (3.071) (13.65 - 18.18)
Compression Spring Test Data
TABLE 2

IPL
Pos. Angle m.daN lbf.in
Figure Item
A IPL_FIGURE_09
Spring A1 68.90 deg. 0.018 - 0.022 1.60 - 1.94
09-110 A2 127.90 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

A1

A2

F_CM_523217_1_0090101_01_00

Test Data of the Torsion Spring

FIGURE-52-32-17-991-009-A01

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**For PN’s ALL

TASK 52-32-17-220-801-A01
Check of the Protective Treatment
1. General
A. See REPAIR for the replacement of the permanently attached parts.
-

NOTE : See REPAIR TASK 52-32-17-300-803-A01 for the replacement of the permanently
attached parts.
B. See the Structural Repair Manual (SRM) for the door structure.
2. Job Set-up Information
A.Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-300-803-A01 Replacement of Parts
TASK 52-32-17-300-802-A01 Protective Treatment
Referenced Information
TABLE 1

3. Procedure

Subtask 52-32-17-210-008-A01
A. Protective Treatment
(1) Check the structure components and the door mechanism for damaged protective
treatment.
(a) See REPAIR TASK 52-32-17-300-802-A01 for the repair of the protective treatment.

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**For PN’s ALL

TASK 52-32-17-210-802-A01
Check of the Electrical Equipment
1. General
A. This check is a visual inspection of the component parts.
B. Do an approved nondestructive test if you think there is a crack which is not visible.
C. See the Structural Repair Manual (SRM) for the repair of the door structure.
-

NOTE : See REPAIR TASK 52-32-17-300-803-A01 for the replacement of the permanently
attached parts.
2. Job Set-up Information
A.Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-300-803-A01 Replacement of Parts
TASK 52-32-17-300-801-A01 Reworking or Machining
Referenced Information
TABLE 1

3. Procedure

CAUTION : MAKE SURE THAT YOU ALWAYS USE THE NOMINAL MATERIAL THICKNESS
OF THE COMPONENT PARTS WHEN YOU CALCULATE THE LIMITS OF THE
ALLOWABLE DAMAGE.

Subtask 52-32-17-210-009-A01
A. Check of the Electrical Equipment for Damage
(1) Check the electrical harness for damaged attachment parts, chafe marks and other
damages.
(a) Chafe marks, damaged attachment parts or other damages are not permitted.
(b) See DISASSEMBLY and ASSEMBLY for the replacement of the damaged electrical
harness and attachment parts.
(2) Check electrical components for damage.
(a) Damage is not permitted.
(b) See DISASSEMBLY and ASSEMBLY for the replacement of the electrical
components.

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(3) Check bonding straps for damage, corrosion, attachment and torsion.
(a) Damage and corrosion are not permitted.
(b) See DISASSEMBLY and ASSEMBLY for the replacement of damaged bonding straps.
(c) See REPAIR TASK 52-32-17-300-801-A01 for the removal of corrosion on attachment
points.
(d) Damaged lacquer coating, incorrect attachment or torsion is not permitted.
(e) See ASSEMBLY for the correct installation of the bonding straps.

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**For PN’s ALL

TASK 52-32-17-220-802-A01
Visual Examination
1. General
A. Do an approved nondestructive test if you think there is a crack which is not clearly visible.
B. See REPAIR for the replacement of the permanently attached parts.
-

NOTE : See REPAIR TASK 52-32-17-300-803-A01 for the replacement of the permanently
attached parts.
C. See the Structural Repair Manual (SRM) for the door structure.
2. Job Set-up Information
A.Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-300-803-A01 Replacement of Parts
FIGURE 52-32-17-991-010-A FIGURE 52-32-17-991-010-A-Visual Examination of the Surface
Protection and Locking Mechanism
Referenced Information
TABLE 1

3. Procedure

Subtask 52-32-17-210-010-A01
A. Visual Examination

NOTE : See IPL_FIGURE_03, IPL_FIGURE_70.

(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 bushings for wear, scratches, corrosion and correct installation.
(4) Examine all nut plates for damaged threads, correct attachment and corrosion.
(5) Examine the hoist fittings for defective threads and corrosion.
(6) Examine the insulation for contamination and correct attachment.
(7) Make sure that the hoses, the water drain valves and holes are clean and not blocked.
(8) Examine the red painted areas of the hand lever assembly, the handle flap and the inside of
the vent door frame for damage.

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(9) Examine the lubrication fittings for damage.

(10) Examine the red and green markings on the locking cams for damage, see FIGURE
52-32-17-991-010-A.
(11) Examine the sight glasses for cracks and scratches.
(a) If there are cracks, replace the sight glass 03-020 and/or 70-022.
(b) If there are scratches on the sight glasses, find the dimensions of the damage:
- If the scratch is less than 10% of the sight glass thickness, then no action is
required
- If the scratch is more than 10% of the sight glass thickness, then replace the
sight glass.

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**For PN’s ALL

DOOR
SEAL

FR57A

DOOR
INSULATION

CORROSION PREVENTIVE CORROSION PREVENTIVE

(MAT. NO. 12ABC1) (MAT. NO. 12ACC1)

DOOR
STRUCTURE

DOOR SURFACE PROTECTION

LOCKING SHAFT

83

AREA OF RED MARKING

43
AREA OF GREEN MARKING

LOCKING CAM

TYPICAL DIRECT VISUAL LOCKING INDICATION

F_CM_523217_1_0100101_01_01

Visual Examination of the Surface Protection and Locking Mechanism

FIGURE-52-32-17-991-010-A01

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REPAIR

**For PN’s ALL

TASK 52-32-17-300-801-A01
Reworking or Machining
1. General
A. See CHECK and FITS AND CLEARANCES for the limits of the component parts.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
14SBA1 Textile-Lint free Cotton -
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
08ABC1 Aqueous Cleaner-Aircraft Exterior Pressure Spraying -
08BPA1 Non Aqueous Cleaner-Non structural use - -
06CMD9 Silicone Adhesive Sealant-General Purpose One part legacy
13XJA1 Laminate Repair Patch-Pax Door Seal - -
14HHB1 Film-Rubber Bonding Polyester Foil -
Consumable Materials
TABLE 1

B. Fixtures, Tools, Test and Support Equipment

REFERENCE DESIGNATION
abrasive cloth
Fixtures, Tools, Test and Support Equipment
TABLE 2

C.Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-300-802-A01 Protective Treatment
FIGURE 52-32-17-991-011-A FIGURE 52-32-17-991-011-A-Door Seal Repair
FIGURE 52-32-17-991-012-A FIGURE 52-32-17-991-012-A-Door Seal Repair
FIGURE 52-32-17-991-013-A FIGURE 52-32-17-991-013-A-Bonding Block
Referenced Information
TABLE 3

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3. Procedure

WARNING : BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

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.

Subtask 52-32-17-300-001-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 (0.23
in).
(2) Make the groove smooth with abrasive cloth.
(3) Burnish the surface with your hands or with a buffing wheel.
(4) Clean the reworked area with a clean Material No. 14SBA1 Textile-Lint free Cotton - made
moist with the Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(5) For the repair of the damaged paint work, see REPAIR TASK 52-32-17-300-802-A01.

Subtask 52-32-17-300-002-A01
B. Repair of Corrosion Damage
(1) Clean the corroded and the adjacent areas and remove the grease with the Material No.
08ABC1 Aqueous Cleaner-Aircraft Exterior Pressure Spraying -.
(2) Dry the wet areas with a clean Material No. 14SBA1 Textile-Lint free Cotton -.

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.

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(d) Clean the work area with a clean Material No. 14SBA1 Textile-Lint free Cotton -
made moist with the Material No. 08BBF1 Non Aqueous Cleaner-- 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 non-destructive test.

(6) Repair the damaged paint work, see REPAIR TASK 52-32-17-300-802-A01.
(7) Remove the masking material.

Subtask 52-32-17-300-003-A01
C. Repair of the Door Seal

CAUTION : MAKE SURE THAT THE SEAL IS TAGGED ”TO BE SUBJECTED TO A

FUSELAGE PRESSURIZATION CHECK” AFTER THE INSTALLATION OF THE
DOOR.

NOTE : See FIGURE 52-32-17-991-011-A, FIGURE 52-32-17-991-012-A, FIGURE

52-32-17-991-013-A.
(1) Remove the door seal from the seal retainer.
(2) Repair the chafe marks and cuts (maximum of 25.4 mm (1.0 in)) that are not in the
contact area as follows:

NOTE : See FIGURE 52-32-17-991-011-A.

(a) Drill a stop hole of 2 mm (0.078 in) dia. at each end of the cut.
(b) Apply pressure to the seal to open the cut.
(c) Make the face of the cut rough with 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.
(f) Clean the repair area with the Material No. 08BPA1 Non Aqueous Cleaner-Non
structural use - -.
(g) Dry the cleaned area with a clean Material No. 14SBA1 Textile-Lint free Cotton -.
(h) Apply a thin layer of the Material No. 06CMD9 Silicone Adhesive Sealant-General
Purpose One part legacy to the faces of the cut.

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(i) Press the faces of the cut together and let them to cure.
(j) Cut a piece of the Material No. 13XJA1 Laminate Repair Patch-Pax Door Seal - - the
same size as the repair area.
(k) Apply a thin layer of the Material No. 06CMD9 Silicone Adhesive Sealant-General
Purpose One part legacy 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 the Material No. 14HHB1 Film-Rubber Bonding
Polyester Foil - and install the seal in the wooden bonding block, see FIGURE
52-32-17-991-013-A.
(n) Use a clamp to compress the seal in the wooden bonding block. Keep the seal in the
bonding block for 24 hours.
(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/or cuts exceeding 25.4 mm (1.0 in) in the length or in the
contact area, by replacement of a section, see FIGURE 52-32-17-991-012-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.
(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.
(e) Clean the surface with the Material No. 08BPA1 Non Aqueous Cleaner-Non structural
use - -.
(f) Dry the cleaned area with a clean Material No. 14SBA1 Textile-Lint free Cotton -.
(g) Apply a thin coat of Material No. 06CMD9 Silicone Adhesive Sealant-General Purpose
One part legacy 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 the Material No. 13XJA1 Laminate Repair Patch-Pax Door Seal - - to
the size of the repair areas.

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(j) Apply a thin layer of the Material No. 06CMD9 Silicone Adhesive Sealant-General
Purpose One part legacy 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 the Material No. 14HHB1 Film-Rubber Bonding
Polyester Foil - and install the seal in the wooden bonding block, see FIGURE
52-32-17-991-013-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 until the seal is smooth.

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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 2.0 mm (0.078 in)

"W" = MAX LENGTH OF CUT 25.4 mm (1.0 in)
"X" = MIN REPAIR AREA AROUND CUT 10 mm (0.4 in)

REPLACEMENT
1 AREA IN WHICH THE FIRST LAYER TISSUE
OF REINFORCEMENT TISSUE IS REMOVED

F_CM_523217_1_0110101_01_01

Door Seal Repair

FIGURE-52-32-17-991-011-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

EXISTING
REPLACEMENT TISSUE DOOR SEAL LAYER OF TISSUE
REPLACEMENT
SECTION

"S" = MIN DISTANCE OF 50mm (1.97 in.) FROM

B−B
INFLATION HOLE
"T" = MIN REPAIR LENGTH OF 200mm (7.87 in.) 1
"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_523217_1_0120101_01_00

Door Seal Repair

FIGURE-52-32-17-991-012-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_523217_1_0130101_01_00

Bonding Block
FIGURE-52-32-17-991-013-A01

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**For PN’s ALL

TASK 52-32-17-300-802-A01
Protective Treatment
1. General
A. See CHECK and FITS AND CLEARANCES for the limits of the component parts.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
14SBA1 Textile-Lint free Cotton -
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
04CMA2 Wash Primer-- - Structure
04EAC2 Primer Polyurethane Paint-- Corrosion Inhibiting Structure
04JME4 Top Coat Polyurethane-- Grey Internal Structure
10ABC1 Surface Pretreatment-Light Alloys Chemical Conversion Yellow -
12ABE2 Corrosion Preventive Compound-Water Displacing Oily Film System
Consumable Materials
TABLE 1

B. Fixtures, Tools, Test and Support Equipment

REFERENCE DESIGNATION
abrasive cloth
Fixtures, Tools, Test and Support Equipment
TABLE 2

C. Referenced Information
REFERENCE DESIGNATION
PMS 01-02-08
PMS 01-02-43
Referenced Information
TABLE 3

3. Procedure

WARNING : BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

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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.

Subtask 52-32-17-300-004-A01
A. Repair of the Damaged Paint work
(1) Remove the damaged paint work with an abrasive cloth.
(2) Remove the paint dust.
(3) Clean the work area with a clean Material No. 14SBA1 Textile-Lint free Cotton - made
moist with the Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.

NOTE : Do not touch the cleaned area.

(4) Let the work area dry.
(5) Apply the Material No. 04CMA2 Wash Primer-- - Structure to the metal surface.
(6) Allow the Material No. 04CMA2 Wash Primer-- - Structure to dry.
(7) Apply the Material No. 04EAC2 Primer Polyurethane Paint-- Corrosion Inhibiting
Structure.
(8) Allow the Material No. 04EAC2 Primer Polyurethane Paint-- Corrosion Inhibiting Structure
to dry.
(9) Apply the Material No. 04JME4 Top Coat Polyurethane-- Grey Internal Structure.
(10) Allow the Material No. 04JME4 Top Coat Polyurethane-- Grey Internal Structure to dry.

Subtask 52-32-17-300-005-A01
B. Repair of the Anodized Surfaces
(1) Clean the work area with a clean Material No. 14SBA1 Textile-Lint free Cotton - made
moist with the Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.

CAUTION : MAKE SURE THAT THE COATING MATERIAL NO. 10ABC1 - SURFACE
PRETREATMENT - LIGHT ALLOYS CHEMICAL CONVERSION YELLOW
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 the Material No. 10ABC1 Surface Pretreatment-Light Alloys Chemical Conversion
Yellow - to the prepared area and let it work for 3 minutes, see PMS 01-02-08.
(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).

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Subtask 52-32-17-300-006-A01
C. Repair of the Corrosion Preventive
(1) Apply the Material No. 12ABE2 Corrosion Preventive Compound-Water Displacing Oily
Film System to the components, see PMS 01-02-43.

NOTE : Make sure that the existing drain holes are not blocked.

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**For PN’s ALL

TASK 52-32-17-300-803-A01
Replacement of Parts
1. General
A. See CHECK and FITS AND CLEARANCES for the limits of the component parts.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
14SBA1 Textile-Lint free Cotton -
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
06AAA1 Polysulfide Sealant-General Purpose Brushable -
06AAB1 Polysulfide Sealant-General Purpose Fillet -
04QAB2 Coating-- Flexible Structure
05ABF1 Retaining adhesive-Cylindrical fitting Medium strength Low viscosity -
06LCG9 Non Hardening Jointing Putty-Medium Temp. Area - -
05BAE1 Threadlocking Adhesive-- Medium strength -
05ABM1 Retaining adhesive-Cylindrical fitting High strength High viscosity -
05EML7 Epoxy Adhesive-- - Legacy 3
Consumable Materials
TABLE 1

B. Fixtures, Tools, Test and Support Equipment

REFERENCE DESIGNATION
nonmetallic scraper
Fixtures, Tools, Test and Support Equipment
TABLE 2

C. Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-940-809-A01 Special Tools, Fixtures and Equipment List
PMS 01-05-05
PMS 01-02-36
PMS 01-05-47
PMS 01-02-41
PMS 01-05-27
PMS 01-05-04

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REFERENCE DESIGNATION
PMS 01-05-45
PMS 01-04-24
Referenced Information
TABLE 3

3. Procedure

WARNING : BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

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.

Subtask 52-32-17-300-007-A01
A. Replacement of the Pressed-in Bushings

NOTE : The component parts with the pressed-in bushings are given in TABLE 4.

NOTE : If you find a damaged bushing in one hinge assembly, you must replace all bushes in
the hinge assembly. Use the locally made special tool, see TASK 52-32-17-940-809-
A01 for the replacement of the bushings in the hinge assemblies.
(1) Replace the pressed-in bushings as follows:
COMPONENT PART REPLACEMENT PART
IPL FIG. - ITEM
NAME NAME
--- Door Structure ---
02-100 --- Bushing
08-380 Roller Lever ---
08-390 --- Shouldered Bushing
08-520 Universal Joint Latch ---
08-530 --- Shouldered Bushing
21-240 Actuator Arm ---
21-190 --- Bushing
21-200 --- Shouldered Bushing
21-250 --- Shouldered Bushing
21-300 Bracket ---
21-280 --- Shouldered Bushing
21-290 --- Bushing

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COMPONENT PART REPLACEMENT PART

IPL FIG. - ITEM
NAME NAME
21-360 Actuator Arm ---
21-320 --- Bushing
21-370 --- Shouldered Bushing
33-020 Latching Hook ---
33-040 --- Shouldered Bushing
33-050 --- Shouldered Bushing
33-170 Bellcrank ---
33-180 --- Bushing
33-190 --- Shouldered Bushing
34-020 Latching Hook ---
34-040 --- Shouldered Bushing
34-050 --- Shouldered Bushing
34-170 Bellcrank ---
34-180 --- Bushing
34-190 --- Shouldered Bushing
40-040 Cover ---
40-050 --- Shouldered Bushing
41-140 Lever ---
41-150 --- Shouldered Bushing
41-160 --- Bushing
41A-140 Lever ---
41A-150 --- Shouldered Bushing
41A-160 --- Bushing
41B-140 Lever ---
41B-150 --- Shouldered Bushing
41B-160 --- Bushing
44-020 Spring Sleeve ---
44-030 --- Bushing
90-030 Outer Hinge ---
90-040 --- Bushing
90-060 Mid Hinge ---
90-070 --- Bushing
90-080 --- Shouldered Bushing
90A-030 Outer Hinge ---
90A-040 --- Bushing
90A-060 Mid Hinge ---
90A-070 --- Bushing
90A-080 --- Shouldered Bushing

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COMPONENT PART REPLACEMENT PART

IPL FIG. - ITEM
NAME NAME
91-020 Mid Hinge ---
91-030 --- Bushing
91-040 --- Shouldered Bushing
91-060 Outer Hinge ---
91-070 --- Bushing
91A-020 Mid Hinge ---
91A-030 --- Bushing
91A-040 --- Shouldered Bushing
91A-060 Outer Hinge ---
91A-070 --- Bushing
96-010 Frame Assembly ---
96-020 --- Bushing
96-030 --- Shouldered Bushing
96-040 --- Shouldered Bushing
96-050 --- Bushing
96-060 --- Shouldered Bushing
96-070 --- Shouldered Bushing
96-080 --- Shouldered Bushing
96-090 Frame Assembly ---
96-100 --- Bushing
96-110 --- Shouldered Bushing
96-120 --- Shouldered Bushing
96-130 --- Bushing
96-140 --- Shouldered Bushing
96-150 --- Shouldered Bushing
--- Door Structure ---
96-190 Shouldered Bushing
96-210 Shouldered Bushing
97-010 Frame Assembly ---
97-020 --- Bushing
97-030 --- Shouldered Bushing
97-040 --- Shouldered Bushing
97-050 --- Bushing
97-060 --- Shouldered Bushing
97-070 --- Shouldered Bushing

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COMPONENT PART REPLACEMENT PART

IPL FIG. - ITEM
NAME NAME
97-080 Frame Assembly ---
97-090 --- Bushing
97-100 --- Shouldered Bushing
97-110 --- Shouldered Bushing
97-120 --- Bushing
97-130 --- Shouldered Bushing
97-140 --- Shouldered Bushing
97-150 --- Bushing
97-160 Forward Frame Segment ---
97-170 --- Shouldered Bushing
97-180 Aft Frame Segment ---
97-190 --- Shouldered Bushing
97-200 --- Shouldered Bushing
--- Door Structure ---
97-260 --- Shouldered Bushing
Pressed-in Bushings
TABLE 4

CAUTION : DO NOT DAMAGE THE EDGES OF THE COMPONENT BORE.

(a) Remove the bushing from the component part with an applicable press-tool.
(b) Clean the bore in the component with a clean Material No. 14SBA1 Textile-Lint free
Cotton - made moist with the Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-
Ethyl-Ketone -.
(c) Let the component bore dry.
(d) Visually examine the component bore for damage.
(e) Install the new bushings, see PMS 01-05-05.

NOTE : You must install the new bushings with the Material No. 06AAA1
Polysulfide Sealant-General Purpose Brushable -.
(f) Examine the installed bushing for correct and satisfactory installation.
(g) Carefully remove the Material No. 06AAA1 Polysulfide Sealant-General Purpose
Brushable - from the surfaces of the component part and the bushing with a clean
Material No. 14SBA1 Textile-Lint free Cotton - made moist with the Material No.
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -, see PMS 01-02-36.
(h) Apply the Material No. 06AAB1 Polysulfide Sealant-General Purpose Fillet - to the
joint between the component bore and the bushing, see PMS 01-05-47.
(i) Let the Material No. 06AAB1 Polysulfide Sealant-General Purpose Fillet - dry.

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(j) Apply the Material No. 04QAB2 Coating-- Flexible Structure to the Material No.
06AAB1 Polysulfide Sealant-General Purpose Fillet -, see PMS 01-02-41.
(k) Let the Material No. 04QAB2 Coating-- Flexible Structure dry.

Subtask 52-32-17-300-008-A01
B. Replacement of the Bonded-in Bushings

NOTE : The component parts with bonded-in bushings are given in TABLE 5.
(1) Replace the bonded-in bushings as follows:
COMPONENT PART REPLACEMENT PART
IPL FIG. - ITEM
NAME NAME
09-030 Stop ---
09-070 --- Shouldered Bushing
09-010 Hand Lever ---
09-180 --- Bushing
09-100 Handle Flap ---
09-180 --- Bushing
Bonded-in Bushings
TABLE 5

(a) Heat the component parts to a maximum temperature of 120 deg. C (248 deg. F) to
soften the bond of the bushing.
(b) Remove the bushing with a suitable tool.
(c) Clean the component bore and the new bushing with a clean Material No. 14SBA1
Textile-Lint free Cotton - made moist with the Material No. 08BBF1 Non Aqueous
Cleaner-- Methyl-Ethyl-Ketone -.

NOTE : You must use a nonmetallic scraper to remove the unwanted Material No.
05ABF1 Retaining adhesive-Cylindrical fitting Medium strength Low
viscosity -.

CAUTION : DO NOT TOUCH THE BONDING SURFACES. CONTAMINATION CAN

CAUSE AN UNSATISFACTORY BOND.
(d) Dry the component bore and the bushing with a clean Material No. 14SBA1 Textile-
Lint free Cotton -.
(e) Install the new bushing, see PMS 01-05-27.

NOTE : You must install the bushing with the Material No. 05ABF1 Retaining
adhesive-Cylindrical fitting Medium strength Low viscosity -.

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(f) Apply the Material No. 04QAB2 Coating-- Flexible Structure to the space between
the bushing and the component part, see PMS 01-02-41.

Subtask 52-32-17-300-009-A01
C. Replacement of the Bonded-in Bearings

NOTE : The component parts with the bonded-in bearings are given in TABLE 6.
(1) Replace the bonded-in bearings as follows:
COMPONENT PART REPLACEMENT PART
IPL FIG. - ITEM
NAME NAME
08-090 Lever ---
08-100 --- Bearing
08-520 Universal Joint Latch ---
08-590 --- Bearing
13-110 Link Lever ---
13-120 --- Bearing
13-140 Link Lever ---
13-150 --- Bearing
20-105 Link Lever ---
20-107 --- Bearing
20-185 Link Lever ---
20-187 --- Bearing
20-225 Link Lever ---
20-227 --- Bearing
31-100 Hinged Lever ---
31-110 --- Bearing
31A-040 Hinged Lever ---
31A-050 --- Bearing
31B-040 Hinged Lever ---
31B-050 --- Bearing
32-110 Hinged Lever ---
32-120 --- Bearing
32A-080 Hinged Lever ---
32A-090 --- Bearing
40-080 Lever ---
40-090 --- Bearing
41-250 Lever ---
41-260 --- Bearing
41-450 Connecting Rod ---
41-460 --- Bearing
41A-230 Serrated Lever ---
41A-240 --- Bearing

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COMPONENT PART REPLACEMENT PART

IPL FIG. - ITEM
NAME NAME
41A-450 Connecting Rod ---
41A-460 --- Bearing
41B-230 Serrated Lever ---
41B-240 --- Bearing
41B-450 Connecting Rod ---
41B-460 --- Bearing
Bonded-in Bearings
TABLE 6

CAUTION : DO NOT DAMAGE THE EDGES OF THE COMPONENT BORE.

CAUTION : HANDLING OF SURFACE AFTER DEGREASING WILL IMPAIR

BONDING.
(a) Remove the bearing from the component with an applicable tool.
(b) Clean the component bore with a clean Material No. 14SBA1 Textile-Lint free Cotton
- made moist with the Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-
Ketone -.

NOTE : Use a wooden or a plastic scraper to remove the old Material No. 05ABF1
Retaining adhesive-Cylindrical fitting Medium strength Low viscosity -.
(c) Carefully clean the outer ring of the new bearing with a clean Material No. 14SBA1
Textile-Lint free Cotton -made moist with the Material No. 08BBF1 Non Aqueous
Cleaner-- Methyl-Ethyl-Ketone -.

CAUTION : DO NOT TOUCH THE BONDING SURFACES. CONTAMINATION CAN

CAUSE AN UNSATISFACTORY BOND.
(d) Install the bearing in the component, see PMS 01-05-27.

NOTE : You must install the bearing with the Material No. 05ABF1 Retaining
adhesive-Cylindrical fitting Medium strength Low viscosity -.
(e) When the bearing is installed, apply a small quantity of the Material No. 05ABF1
Retaining adhesive-Cylindrical fitting Medium strength Low viscosity - to the space
between the bearing and the component.
(f) Examine the bond and make sure that the bearing is correctly installed.
(g) Remove the unwanted Material No. 05ABF1 Retaining adhesive-Cylindrical fitting
Medium strength Low viscosity - from the bearing and the component with a clean
Material No. 14SBA1 Textile-Lint free Cotton - made moist with the Material No.
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.

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(h) Keep the parts at a room temperature for at least 30 minutes and let the part cure,
see PMS 01-05-27.

NOTE : Keep the component in such a position so that the bond can cure.
(i) Do not put a load on the bonded bearing until it has cured for 24 hours at room
temperature.
(j) Apply the Material No. 06AAB1 Polysulfide Sealant-General Purpose Fillet - to the
joint between the component bore and the bearing, see PMS 01-05-47.
(k) Let the Material No. 06AAB1 Polysulfide Sealant-General Purpose Fillet - dry.
(l) Apply the Material No. 04QAB2 Coating-- Flexible Structure to the Material No.
06AAB1 Polysulfide Sealant-General Purpose Fillet -, see PMS 01-02-41.
(m) Let the Material No. 04QAB2 Coating-- Flexible Structure dry.

Subtask 52-32-17-300-012-A01
D. Replacement of the Threaded Inserts

NOTE : The component parts with the threaded inserts are given in TABLE 7.
(1) Replace the threaded inserts as follows:
COMPONENT PART REPLACEMENT PART
IPL FIG. - ITEM
NAME NAME
--- Access Cover ---
01-130 --- Threaded Insert
09-020 Sequence Cam ---
09-200 --- Threaded Insert
--- Door Structure ---
96-170 --- Threaded Insert
--- Door Structure ---
97-210 --- Threaded Insert
97-240 -- Threaded Insert
Threaded Inserts
TABLE 7

(a) Replace the threaded inserts, see PMS 01-05-04.

Subtask 52-32-17-300-013-A01
E. Replacement of the HELI-COIL Threaded Inserts

NOTE : The component parts with the HELI-COIL threaded inserts are given in TABLE 8.

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(1) Replace the HELI-COIL threaded inserts as follows:

COMPONENT PART REPLACEMENT PART
IPL FIG. - ITEM
NAME NAME
--- Door Structure ---
01-035 --- Threaded Insert
21-180 Actuator Arm Assembly ---
21-260 --- Threaded Insert
21-310 Actuator Arm Assembly ---
21-380 --- Threaded Insert
HELI-COIL Threaded Inserts
TABLE 8

(a) Carefully remove the fractured inserts.

(b) Replace the HELI-COIL threaded inserts, see PMS 01-05-45.

NOTE : A HELI-COIL tool set is necessary for the replacement.

NOTE : You must use the Material No. 06LCG9 Non Hardening Jointing Putty-
Medium Temp. Area - - when you install the HELI-COIL threaded inserts,
see PMS 01-05-47.

Subtask 52-32-17-300-014-A01
F. Replacement of the Lubrication Fittings

NOTE : The component parts with the lubrication fittings are given in TABLE 9.
(1) Replace the lubrication fittings as follows:
COMPONENT PART REPLACEMENT PART
IPL FIG. - ITEM
NAME NAME
08-250 Shaft ---
08-350 --- Lubrication Fitting
33-020 Latching Hook ---
33-030 --- Lubrication Fitting
33-170 Bellcrank ---
33-200 --- Lubrication Fitting
34-020 Latching Hook ---
34-030 --- Lubrication Fitting
34-170 Bellcrank ---
34-200 --- Lubrication Fitting
Lubrication Fittings
TABLE 9

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(a) Remove the damaged or worn lubrication fitting from the component.
(b) Clean the component bore with a clean Material No. 14SBA1 Textile-Lint free Cotton
- made moist with the Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-
Ketone -.
(c) Apply the Material No. 05BAE1 Threadlocking Adhesive-- Medium strength - to the
thread of the lubrication fitting.
(d) Install the lubrication fitting on the component and tighten.

Subtask 52-32-17-300-015-A01
G. Replacement of the Bonded-in Insert

NOTE : The component part with the bonded-in insert is given in TABLE 10.
(1) Replace the bonded-in insert as follows:
COMPONENT PART REPLACEMENT PART
IPL FIG. - ITEM
NAME NAME
09-010 Hand lever ---
09-090 --- Insert
Bonded-in Insert
TABLE 10

(a) Remove the damaged insert from the component part with an applicable tool.
(b) Clean the component bore and the new insert with a clean Material No. 14SBA1
Textile-Lint free Cotton - made moist with the Material No. 08BBF1 Non Aqueous
Cleaner-- Methyl-Ethyl-Ketone -.

NOTE : You must use a nonmetallic scraper to remove the unwanted Material No.
05ABM1 Retaining adhesive-Cylindrical fitting High strength High viscosity
-.

CAUTION : DO NOT TOUCH THE BONDING SURFACES. CONTAMINATION CAN

CAUSE AN UNSATISFACTORY BOND.
(c) Dry the component bore and the bush with a clean Material No. 14SBA1 Textile-Lint
free Cotton -.
(d) Install the insert, see PMS 01-05-27.

NOTE : You must install the insert with the Material No. 05ABM1 Retaining
adhesive-Cylindrical fitting High strength High viscosity -.
(e) Apply the Material No. 04QAB2 Coating-- Flexible Structure to the space between
the insert and the component part, see PMS 01-02-41.

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Subtask 52-32-17-300-016-A01
H. Replacement of the Riveted Parts
(1) Replace the riveted parts as follows:
(a) Replace the riveted parts, see PMS 01-04-24.

Subtask 52-32-17-300-017-A01
J. Replacement of the Identification Plates
(1) Replace the self-adhesive identification plates as follows:

NOTE : The component parts with the self-adhesive identification plates are given in
TABLE 11.
COMPONENT PART REPLACEMENT PART
IPL FIG. - ITEM
NAME NAME
--- Door Structure ---
01-080A --- Identification Plate
01-080C --- Identification Plate
01-080D --- Identification Plate
Self-adhesive Identification Plate
TABLE 11

(a) Record the data of the used identification plate on the new identification plate.
(b) Remove the damaged or loose identification plate with a nonmetallic scraper.

CAUTION : DO NOT TOUCH THE BONDING SURFACES. CONTAMINATION CAN

CAUSE AN UNSATISFACTORY BOND.
(c) Clean the bonding area with a clean Material No. 14SBA1 Textile-Lint free Cotton -
made moist with the Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-
Ketone -.
(d) Remove the protection foil from the identification plate.
(e) Align and attach the identification plate on the cleaned bonding surface.
(2) Replace the bonded identification plates as follows:

NOTE : The component parts with the bonded identification plates are given in TABLE
12.

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COMPONENT PART REPLACEMENT PART

IPL FIG. - ITEM
NAME NAME
--- Door Structure ---
01-080B --- Identification Plate
Bonded Identification Plate
TABLE 12

(a) Write the data of the used identification plate on the new identification plate.
(b) Remove the damaged or loose identification plate with a nonmetallic scraper.

CAUTION : DO NOT TOUCH THE BONDING SURFACES. CONTAMINATION CAN

CAUSE AN UNSATISFACTORY BOND.
(c) Clean the bonding area with a clean Material No. 14SBA1 Textile-Lint free Cotton -
made moist with the Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-
Ketone -.
(d) Apply the Material No. 05EML7 Epoxy Adhesive-- - Legacy 3 to the bonding surface,
see the manufacturers instructions.
(e) Align and install the identification plate on the bonding surface.
(f) Remove the unwanted Material No. 05EML7 Epoxy Adhesive-- - Legacy 3 from the
edges of the identification plate, with a clean Material No. 14SBA1 Textile-Lint free
Cotton - made moist with the Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-
Ethyl-Ketone -.

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ASSEMBLY

**For PN’s ALL

TASK 52-32-17-400-801-A01
Installation of the Identification Plate, the Insulation and the Door Seal
1. General
A. See REPAIR section for the component parts which have a permanent connection.
B. Make sure that the drain valves and the drain holes are clean and have no blockages.
C. When no torque value is specified, a standard torque value is applicable.
-

NOTE : For the standard torque values, see PMS 01-05-66.

NOTE : Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to all surfaces of parts which move.
2. Job Set-up Information
A. Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-300-803-A01 Replacement of Parts
TASK 52-32-17-300-801-A01 Reworking or Machining
PMS 01-05-66
Referenced Information
TABLE 1

3. Procedure

WARNING : BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

CAUTION : USE ONLY THE SPECIFIED MATERIALS. MATERIALS WHICH ARE NOT
SPECIFIED, CAN CAUSE DAMAGE.

Subtask 52-32-17-400-001-A01
A. Installation of the Identification Plate, the Insulation and the Door Seal

NOTE : See IPL_FIGURE_01, IPL_FIGURE_02.

NOTE : For the replacement of the identification plate 01-080, see REPAIR TASK
52-32-17-300-803-A01.

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PRE MOD 34470K09330

(1) Install the fire protection lining assembly 02-010 as follows:
(a) Put the fire protection lining assembly 02-010 in position on the door structure and
tighten the studs 02-030.
POST MOD 34470K09330
(1) Install the fire protection lining assembly 02-010 as follows:
(a) Put the fire protection lining assembly 02-010 in position on the door structure and
tighten the studs 02-030.

WARNING : IF THE DOOR SEAL IS NOT INSTALLED IN THE CORRECT POSITION, THE
CABIN PRESSURE CAN DECREASE. THIS CAN RESULT IN A DISRUPTION
OF THE FLIGHT.
ALL VARIANTS
(2) Install the door seal 02-090 as follows:
(a) If removed, install the door seal 02-090 on the door structure, see REPAIR TASK
52-32-17-300-801-A01.

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**For PN’s ALL

TASK 52-32-17-400-802-A01
Assembly and Installation of the Access Covers
1. General
A. See REPAIR section for the component parts which have a permanent connection.
B. Make sure that the drain valves and the drain holes are clean and have no blockages.
C. When no torque value is specified, a standard torque value is applicable.
-

NOTE : For the standard torque values, see PMS 01-05-66.

NOTE : Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to all surfaces of parts which move.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
14SBA1 Textile-Lint free Cotton -
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
06AEA1 Polysulfide Sealant-Low Adhesion Brushable -
06AAA1 Polysulfide Sealant-General Purpose Brushable -
08BBD1 Non Aqueous Cleaner-- Isopropyl Alcohol -
05GBK1 Cyanoacrylate Adhesive-Non Structural One Part - Low viscosity
Small gaps -
06AAB1 Polysulfide Sealant-General Purpose Fillet -
Consumable Materials
TABLE 1

B. Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-400-818-A01 Installation of the Door Fairing
PMS 01-05-66
PMS 01-02-37
PMS 01-02-36
PMS 01-05-47
Referenced Information
TABLE 2

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3. Procedure

WARNING : BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

CAUTION : USE ONLY THE SPECIFIED MATERIALS. MATERIALS WHICH ARE NOT
SPECIFIED, CAN CAUSE DAMAGE.

Subtask 52-32-17-400-002-A01
A. Assembly and Installation of the Access Covers

NOTE : See IPL_FIGURE_03.

NOTE : For the installation of the door fairing, see ASSEMBLY TASK 52-32-17-400-818-A01.
(1) Install the access cover assembly 03-130 as follows:
(a) Install the access cover assembly 03-130 with the washers 03-150 and the screws
03-140 on the door structure.
(b) If the sealing section 03-135 was removed during the disassembly procedure, continue
as follows:
1 Clean the mating surface of the access cover 03-132 for the sealing section
03-135 with a clean Material No. 14SBA1 Textile-Lint free Cotton - made moist
with the Material No. 08BBD1 Non Aqueous Cleaner-- Isopropyl Alcohol -.
2 Cut the sealing section 03-135 to the length and remove the protection foil from
the sealing section 03-135.
3 Install the sealing section 03-135 on the access cover 03-132 and bond the ends
of the sealing section 03-135 together with the Material No. 05GBK1
Cyanoacrylate Adhesive-Non Structural One Part - Low viscosity Small gaps -.
4 Install the access cover assembly 03-130 with the washers 03-150 and the screws
03-140 on the door structure.
(c) Tighten the screws 03-140.
(2) Install the access covers 03-110 as follows:
(a) Clean the mating surfaces of the access cover 03-110 and the door structure and the
screws 03-120 with a clean Material No. 14SBA1 Textile-Lint free Cotton - made
moist with the Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
and let them dry.
(b) Apply the Material No. 06AEA1 Polysulfide Sealant-Low Adhesion Brushable - to the
mating surface of the access cover 03-110, see PMS 01-02-37.
(c) Apply the Material No. 06AAA1 Polysulfide Sealant-General Purpose Brushable - to
the shaft of the screws 03-120, see PMS 01-02-36.

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(d) Install the access cover 03-110 with the screws 03-120 on the door structure.
(e) Tighten the screws 03-120.
(3) Assemble the access cover assembly 03-010 as follows:
(a) If the sight glasses 03-020 were removed during the DISASSEMBLY procedure,
proceed as follows:
1 Clean the mating surfaces of the sheet 03-015 and the sight glass 03-020 with a
clean Material No. 14SBA1 Textile-Lint free Cotton - made moist with the
Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone - and let
them dry.
2 Apply the Material No. 06AAA1 Polysulfide Sealant-General Purpose Brushable -
to the mating surfaces of the sheet 03-015 and the sight glass 03-020, see PMS
01-02-36.
3 Apply the Material No. 06AAA1 Polysulfide Sealant-General Purpose Brushable -
to the shaft of the screws 03-030, see PMS 01-02-36)
4 Install the sight glass 03-020 with the sheet 03-015, the screws 03-030 and the
nuts 03-040 on the access cover assembly 03-010.
5 Tighten the nuts 03-040.
6 Apply the Material No. 06AAB1 Polysulfide Sealant-General Purpose Fillet - to
the space between the sheet 03-015, the sight glass 03-020 and the access cover
assembly 03-010, see PMS 01-05-47.
7 Let the Material No. 06AAB1 Polysulfide Sealant-General Purpose Fillet - dry.
(4) Install the access cover assembly 03-010.
(a) Install the access cover assembly 03-010 with the studs 03-050, 03-060 and 03-070 on
the door structure.

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**For PN’s ALL

TASK 52-32-17-400-803-A01
Installation of the X-Stops, the Protective Plugs, the Plugs and the Adjusting Screws
1. General
A. See REPAIR section for the component parts which have a permanent connection.
B. Make sure that the drain valves and the drain holes are clean and have no blockages.
C. When no torque value is specified, a standard torque value is applicable.
-

NOTE : For the standard torque values, see PMS 01-05-66.

NOTE : Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to all surfaces of parts which move.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
14SBA1 Textile-Lint free Cotton -
08BBD1 Non Aqueous Cleaner-- Isopropyl Alcohol -
06AAC1 Polysulfide Sealant-General Purpose Interfay -
06AAA1 Polysulfide Sealant-General Purpose Brushable -
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
06AAB1 Polysulfide Sealant-General Purpose Fillet -
Consumable Materials
TABLE 1

B. Referenced Information
REFERENCE DESIGNATION
PMS 01-05-66
PMS 01-02-36
PMS 01-05-47
Referenced Information
TABLE 2

3. Procedure

WARNING : BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

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CAUTION : USE ONLY THE SPECIFIED MATERIALS. MATERIALS WHICH ARE NOT
SPECIFIED, CAN CAUSE DAMAGE.

Subtask 52-32-17-400-003-A01
A. Installation of the X-Stops, the Protective Plugs, the Plugs and the Adjusting Screws

NOTE : See IPL_FIGURE_01, IPL_FIGURE_04.

(1) Install the X-stops 04-030 and 04-100 as follows:
(a) Clean the mating surfaces of the X-stops 04-030 and 04-100, the adjusting plates
04-040, 04-041, 04-042, 04-043, 04-110, 04-111, 04-112, 04-113 and the door
structure with a clean Material No. 14SBA1 Textile-Lint free Cotton - made moist
with the Material No. 08BBD1 Non Aqueous Cleaner-- Isopropyl Alcohol -.
(b) Apply the Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surfaces of the X-stops 04-030 and 04-100 and the adjusting plates 04-040,
04-041, 04-042, 04-043, 04-110, 04-111, 04-112, 04-113 , see PMS 01-02-36.
(c) Put the adjusting plates 04-040, 04-041, 04-042, 04-043, 04-110, 04-111, 04-112,
04-113 in position as recorded during the disassembly procedure.
(d) Apply the Material No. 06AAA1 Polysulfide Sealant-General Purpose Brushable - on
the screws 04-050 and 04-080, see PMS 01-02-36.
(e) Put the X-stops 04-030 and 04-100 in position on the adjusting plates 04-040, 04-041,
04-042, 04-043, 04-110, 04-111, 04-112, 04-113 and install the screws 04-050 and
04-080, the washers 04-060 and 04-090 and the nuts 04-070.
(f) Tighten the nuts 04-070.
(2) Install the protective plugs 04-020, 04-120 and 04-130 as follows:
(a) Clean the mating surfaces of the protective plugs 04-020, 04-120 and 04-130 and the
door structure with a clean Material No. 14SBA1 Textile-Lint free Cotton - made
moist with the Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(b) Install the protective plugs 04-020, 04-120 and 04-130 on the door structure.
(c) Apply the Material No. 06AAB1 Polysulfide Sealant-General Purpose Fillet - to the
space between the plugs 04-020, 04-120 and 04-130 and the door structure, see PMS
01-05-47.
(3) Install the adjusting screws 01-100 as follows
(a) Put the nuts 01-110 and the new tab washers 01-120 on the adjusting screws 01-100
and install the adjusting screws 01-100 on the door structure.

NOTE : Attach a tag that tells persons to adjust and safety the adjusting screws
01-100 after the final installation of the door on the aircraft.

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(4) Install the plugs 01-090 as follows:

(a) Clean the mating surfaces of the plugs 01-090 and the door structure with a clean
Material No. 14SBA1 Textile-Lint free Cotton - made moist with the Material No.
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(b) Install the plugs 01-090 in the door structure.

NOTE : Attach a tag that tells persons to install the plugs 01-090 flush with the
door skin after the final installation of the door on the aircraft.

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**For PN’s ALL

TASK 52-32-17-400-804-A01
Assembly of the Hand Lever Assembly
1. General
A. See REPAIR section for the component parts which have a permanent connection.
B. Make sure that the drain valves and the drain holes are clean and have no blockages.
C. When no torque value is specified, a standard torque value is applicable.
-

NOTE : For the standard torque values, see PMS 01-05-66.

NOTE : Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to all surfaces of parts which move.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
14SBA1 Textile-Lint free Cotton -
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
03HBD9 Synthetic Ester base Grease-General Purpose Low Temp -
Consumable Materials
TABLE 1

B. Referenced Information
REFERENCE DESIGNATION
PMS 01-05-66
PMS 01-05-44
Referenced Information
TABLE 2

3. Procedure

WARNING : BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

CAUTION : USE ONLY THE SPECIFIED MATERIALS. MATERIALS WHICH ARE NOT
SPECIFIED, CAN CAUSE DAMAGE.

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Subtask 52-32-17-400-004-A01
A. Assembly of the Hand Lever Assembly

NOTE : See IPL_FIGURE_09.

(1) Assemble the hand lever assembly 09-001 as follows:
(a) Clean the outer and inner surfaces of the spring sleeve 09-170 and the spring 09-110
with a clean Material No. 14SBA1 Textile-Lint free Cotton - made moist with the
Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(b) Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to the outer surface of the spring sleeve 09-170 and the spring 09-110.

WARNING : YOU MUST INSTALL TORSION SPRINGS WITH LOAD.

(c) Put the spring 09-110, the spring sleeve 09-170, the handle flap 09-100 and the
bearing bolt 09-160 in position on the hand lever 09-010 and install the washers
09-150.
(d) Safety the bearing bolt 09-160 with the new cotter pins 09-120, see PMS 01-05-44.
(e) Clean the bearing bolt 09-140 with a clean Material No. 14SBA1 Textile-Lint free
Cotton - made moist with the Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-
Ethyl-Ketone -.
(f) Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to the bearing bolt 09-140.
(g) Install the bearing bolt 09-140 and the washers 09-130 on the handle flap 09-100.
(h) Safety the bearing bolt 09-140 with the new cotter pins 09-120, see PMS 01-05-44.
(i) Put the sequence cams 09-020 in position on the hand lever 09-010 and install the
washers 09-150 and the bolts 09-190.
(j) Clean the shafts of the bolts 09-040 with a clean Material No. 14SBA1 Textile-Lint
free Cotton - made moist with the Material No. 08BBF1 Non Aqueous Cleaner--
Methyl-Ethyl-Ketone -.
(k) Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to the shafts of the bolts 09-040.
(l) Install the stop 09-030, the rollers 09-080, the bolts 09-040 and the washers 09-060.
(m) Safety the bolts 09-040 with the retaining rings 09-050.

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**For PN’s ALL

TASK 52-32-17-400-805-A01
Installation of the Hand Lever Mechanism
1. General
A. See REPAIR section for the component parts which have a permanent connection.
B. Make sure that the drain valves and the drain holes are clean and have no blockages.
C. When no torque value is specified, a standard torque value is applicable.
-

NOTE : For the standard torque values, see PMS 01-05-66.

NOTE : Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to all surfaces of parts which move.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
14SBA1 Textile-Lint free Cotton -
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
03HBD9 Synthetic Ester base Grease-General Purpose Low Temp -
03JBA1 Silicone base Grease-General Purpose - -
06AEA1 Polysulfide Sealant-Low Adhesion Brushable -
Consumable Materials
TABLE 1

B. Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-800-801-A01 Adjustment
PMS 01-05-66
PMS 01-05-44
PMS 01-05-03
PMS 01-02-37
Referenced Information
TABLE 2

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3. Procedure

WARNING : BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

CAUTION : USE ONLY THE SPECIFIED MATERIALS. MATERIALS WHICH ARE NOT
SPECIFIED, CAN CAUSE DAMAGE.

Subtask 52-32-17-400-005-A01
A. Installation of the Hand Lever Mechanism

NOTE : See IPL_FIGURE_08, IPL_FIGURE_95.

(1) Install the bolt 08-440 on the door structure as follows:
(a) Install the bolt 08-440, the washer 08-220 and the nut 08-110 on the door structure.
(2) Install the catching hook 08-490 as follows:
(a) Install the sheet 08-480 as recorded during the disassembly procedure.
(b) Put the catching hook 08-490 in position on the door structure and install the
washers 08-120 and the bolts 08-500.
(c) Adjust the catching hook 08-490, see ASSEMBLY TASK 52-32-17-800-801-A01.
(3) Assemble the rod assemblies 08-160 and 08-600 as follows:
(a) Install the nuts 95-030 and 95-040 and the locking devices 95-050 on the rod ends
95-010 and 95-020.
(b) Install the rod ends 95-010 and 95-020 with the nuts 95-030 and 95-040 and the
locking devices 95-050 on the rod body. Make sure that the length of the rod
assemblies 08-160 and 08-600 is the same as the length recorded during the
disassembly procedure.

NOTE : Do not safety the nuts 95-030 and 95-040 at this time. Attach a tag to tell
persons to safety the nuts 95-030 and 95-040 after adjustment.
(4) Install the rod assemblies 08-160 and 08-600 as follows:

NOTE : Install the rod assemblies 08-160 and 08-600 in the position as recorded during
the disassembly procedure.
(a) Clean the bolts 08-200 with a clean Material No. 14SBA1 Textile-Lint free Cotton -
made moist with the Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-
Ketone -.
(b) Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to the shaft of the bolts 08-200.
(c) Connect the fork-end of the rod assembly 08-600 on the latching shaft.

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(d) Install the washer 08-210, the bolt 08-200, the washer 08-190 and the nut 08-180 on
the rod assembly 08-600.
(e) Tighten the nut 08-180.
(f) Connect the fork-end of the rod assembly 08-160 on the locking shaft.
(g) Install the washer 08-210, the bolt 08-200, the washer 08-190 and the nut 08-180 on
the rod assembly 08-160.
(h) Tighten the nut 08-180.
(i) Safety the nuts 08-180 with the new cotter pins 08-170, see PMS 01-05-44.
(5) Assemble the roller lever assembly 08-370 as follows:
(a) Clean the bore of the roller 08-400 and the shaft of the bolt 08-430 with a clean
Material No. 14SBA1 Textile-Lint free Cotton - made moist with the Material No.
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(b) Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to the bore of the roller 08-400 and the shaft of the bolt 08-430.
(c) Install the roller 08-400 with the bolt 08-430, the washer 08-420 and the nut 08-410
on the roller lever 08-380.
(d) Tighten the nut 08-410.
(e) Make sure that the roller 08-400 turns freely.
(f) Safety the nut 08-410 with the new cotter pin 08-TBD, see PMS 01-05-44.
(6) Install the shaft 08-360 as follows:
(a) Clean the shaft 08-360 and the bushings 08-390 and 08-530 with a clean Material No.
14SBA1 Textile-Lint free Cotton - made moist with the Material No. 08BBF1 Non
Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(b) Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to the mating surfaces of the shaft 08-360 and the bushings 08-390 and
08-530.
(c) Install the shaft 08-360 on the door structure.
1 During the installation of the shaft 08-360 install the universal joint assembly
08-510, the roller lever assembly 08-370 and the universal joint lock 08-240 on
the shaft 08-360.

NOTE : Make sure that the attachment holes are aligned.

(d) Install the bolt 08-230, the washer 08-220 and the nut 08-110 on the universal joint
lock 08-240.

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(7) Install the compression spring 08-470 as follows:

(a) Clean the shaft of the spring bolt 08-460 with a clean Material No. 14SBA1 Textile-
Lint free Cotton - made moist with the Material No. 08BBF1 Non Aqueous Cleaner--
Methyl-Ethyl-Ketone -.
(b) Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to the shaft of the spring bolt 08-460.

WARNING : YOU MUST INSTALL THE COMPRESSION SPRING WITH LOAD.

(c) Install the compression spring 08-470 on the spring bolt 08-460.
(d) Install the spring bolt 08-460 with the compression spring 08-470 in the hole in the
door structure.
(e) Push the spring bolt 08-460 down against the compression spring 08-470.
(f) Install the locally manufactured bush and a mounting nut e.g. NAS509-4 on the
thread of the spring bolt 08-460 to compensate the load of the compression spring
08-470 for easy installation.
(g) Connect the spring bolt 08-460 with the bolt 08-450, the washer 08-120 and the nut
08-110 on the roller lever assembly 08-370.
(h) Tighten the nut 08-110.
(i) Remove the locally manufactured bush and the mounting nut.
(8) Assemble and install the lever assembly 08-020 as follows:
(a) Assemble the lever assembly 08-020 as follows:
1 Clean the locating pins 08-050 with a clean Material No. 14SBA1 Textile-Lint
free Cotton - made moist with the Material No. 08BBF1 Non Aqueous Cleaner--
Methyl-Ethyl-Ketone -.
2 Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose
Low Temp - to the locating pins 08-050.
3 Put the actuating unit 08-040 in position on the bracket 08-030 and the lever
08-090.
4 Install the washers 08-080, the locating pins 08-050 and the washers 08-070.
5 Safety the locating pins 08-050 with the new cotter pins 08-060, see PMS
01-05-44.

WARNING : YOU MUST INSTALL THE LEVER ASSEMBLY WITH LOAD.

(b) Install the lever assembly 08-020 as follows:
1 Clean the mating surfaces of the bracket 08-030 and the door structure with a
clean Material No. 14SBA1 Textile-Lint free Cotton - made moist with the
Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.

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2 Apply the Material No. 06AEA1 Polysulfide Sealant-Low Adhesion Brushable -

to the mating surface of the bracket 08-030, see PMS 01-02-37.
3 Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose
Low Temp - to the inner diameter of the lever 08-090.
4 Put the lever 08-090 in position on the shaft 08-360 and the bracket 08-030.
5 Make sure that the attachment holes in the lever 08-090 and in the shaft 08-360
are aligned
6 Attach the bracket 08-030 with the washers 08-120, the bolts 08-130, the
washers 08-120 and nuts 08-110 on the door structure.
7 Install the bolt 08-230, the washer 08-220 and the nut 08-110 in the lever
08-090 and the shaft 08-360.
(9) Connect the rod assemblies 08-160 and 08-600 as follows:
(a) Clean the shaft of the bolts 08-200 and 08-580 and the inner side of the fork-ends of
the rod assemblies 08-160 and 08-600 with a clean Material No. 14SBA1 Textile-Lint
free Cotton - made moist with the Material No. 08BBF1 Non Aqueous Cleaner--
Methyl-Ethyl-Ketone -.
(b) Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to the shaft of the bolts 08-200 and 08-580 and the inner side of the fork-
ends of the rod assemblies 08-160 and 08-600.
(c) Connect the rod assembly 08-600 with the washer 08-570, the bolt 08-580, the washer
08-560 and the nut 08-550 to the universal joint latch 08-520.
(d) Tighten the nut 08-550 and safety with the new cotter pin 08-540, see PMS
01-05-44.
(e) Connect the rod assembly 08-160 with the washers 08-210, the bolts 08-200, the
washers 08-190 and the nuts 08-180 to the lever 08-090.
(f) Tighten the nuts 08-180 and safety with the new cotter pins 08-170, see PMS
01-05-44.
(10) Install the hand lever assembly 08-010 and the shaft 08-250 as follows:
(a) Clean the outer surface of the shaft 08-250, the hand lever assembly 08-010, the roller
lever assembly 08-370 and the universal joint assembly 08-510 with a clean Material
No. 14SBA1 Textile-Lint free Cotton - made moist with the Material No. 08BBF1
Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(b) Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to the outer surface of the shaft 08-250.
(c) Apply the Material No. 03JBA1 Silicone base Grease-General Purpose - - to the
related contact surfaces of the hand lever assembly 08-010, the roller lever assembly
08-370 and the universal joint assembly 08-510.

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(d) Install the shaft 08-250, the spacer washers 08-260, 08-270, 08-271, 08-272, 08-273,
08-274, 08-275, 08-276, 08-277 and the hand lever assembly 08-010 on the door
structure.

NOTE : Use the location and the thickness of the spacer washers 08-260, 08-270,
08-271, 08-272, 08-273, 08-274, 08-275, 08-276, 08-277 as recorded during
the disassembly procedure.
(e) Measure and if necessary adjust the clearance ”A” between the hand lever assembly
08-010 and the door structure, see ASSEMBLY TASK 52-32-17-800-801-A01.
(f) Put the new lock washer 08-150 in position on the shaft 08-250.
(g) Tighten the bolts 08-140.
(h) Safety the bolts 08-140 with the lock washer 08-150, see PMS 01-05-03.
(i) Make sure that the hand lever assembly 08-010 is flush with the door surface.

NOTE : If the hand lever assembly 08-010 is not flush with the door surface, see
ASSEMBLY TASK 52-32-17-800-801-A01.

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**For PN’s ALL

TASK 52-32-17-400-806-A01
Assembly of the Latching Hook Assemblies
1. General
A. See REPAIR section for the component parts which have a permanent connection.
B. Make sure that the drain valves and the drain holes are clean and have no blockages.
C. When no torque value is specified, a standard torque value is applicable.
-

NOTE : For the standard torque values, see PMS 01-05-66.

NOTE : Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to all surfaces of parts which move.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
14SBA1 Textile-Lint free Cotton -
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
03HBD9 Synthetic Ester base Grease-General Purpose Low Temp -
Consumable Materials
TABLE 1

B. Referenced Information
REFERENCE DESIGNATION
PMS 01-05-66
PMS 01-05-44
Referenced Information
TABLE 2

3. Procedure

WARNING : BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

CAUTION : USE ONLY THE SPECIFIED MATERIALS. MATERIALS WHICH ARE NOT
SPECIFIED, CAN CAUSE DAMAGE.

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Subtask 52-32-17-400-006-A01
A. Assembly of the Latching Hook Assemblies

NOTE : See IPL_FIGURE_33, IPL_FIGURE_34.

(1) Assemble the latching hook mechanism 33-010, 34-010 as follows:
(a) Clean the mating surfaces of the sleeve 33-060, 34-060, the bushings 33-100 and
33-110, 34-100 and 34-110 and the bolt 33-150, 34-150 with a clean Material No.
14SBA1 Textile-Lint free Cotton - made moist with the Material No. 08BBF1 Non
Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(b) Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to the mating surfaces of the sleeve 33-060, 34-060, the bushings 33-100 and
33-110, 34-100 and 34-110 and the bolt 33-150, 34-150.
(c) Put the sleeve 33-060, 34-060 in position on the bellcrank assembly 33-160, 34-160.
(d) Put the bushings 33-100 and 33-110, 34-100 and 34-110 in position on the upper
fork-end of the connecting link 33-070, 34-070.
(e) Put the bellcrank assembly 33-160, 34-160 in position on the connecting link 33-070,
34-070.
(f) Install the washers 33-090 and 33-130, 34-090 and 34-130, the bolt 33-150, 34-150
and the nut 33-120, 34-120.
(g) Safety the nut 33-120, 34-120 with the new cotter pin 33-140, 34-140, see PMS
01-05-44.
(h) Put the eye-end of the connecting rod 33-260, 34-260 in position on the fork-end of
the bellcrank assembly 33-160, 34-160.
(i) Install the bushing 33-240, 34-240, the washer 33-220, 34-220, the bolt 33-210,
34-210, the washer 33-220, 34-220 and the nut 33-250, 34-250.
(j) Safety the nut 33-250, 34-250 with the new cotter pin 33-140, 34-140, see PMS
01-05-44.
(k) Clean the with a clean Material No. 14SBA1 Textile-Lint free Cotton - made moist
with the Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(l) Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to the mating surfaces of the sleeve 33-060, 34-060, the bushings 33-100 and
33-110, 34-100 and 34-110 and the bolt 33-080, 34-080.
(m) Install the sleeve 33-060, 34-060 on the latching hook assembly 33-010, 34-010.
(n) Install the bushings 33-100 and 33-110, 34-100 and 34-110 on the fork-end of the
connecting link 33-070, 34-070.
(o) Install the latching hook assembly 33-010, 34-010, the washers 33-090 and 33-130,
34-090 and 34-130, the bolt 33-080, 34-080 and the nut 33-120, 34-120.

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(p) Safety the nut 33-120, 34-120 with the new cotter pin 33-140, 34-140, see PMS
01-05-44.

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**For PN’s ALL

TASK 52-32-17-400-807-A01
Installation of the Latching Mechanism Assemblies
1. General
A. See REPAIR section for the component parts which have a permanent connection.
B. Make sure that the drain valves and the drain holes are clean and have no blockages.
C. When no torque value is specified, a standard torque value is applicable.
-

NOTE : For the standard torque values, see PMS 01-05-66.

NOTE : Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to all surfaces of parts which move.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
14SBA1 Textile-Lint free Cotton -
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
03HBD9 Synthetic Ester base Grease-General Purpose Low Temp -
Consumable Materials
TABLE 1

B. Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-800-801-A01 Adjustment
PMS 01-05-66
PMS 01-05-44
Referenced Information
TABLE 2

3. Procedure

WARNING : BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

CAUTION : USE ONLY THE SPECIFIED MATERIALS. MATERIALS WHICH ARE NOT
SPECIFIED, CAN CAUSE DAMAGE.

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Subtask 52-32-17-400-007-A01
A. Installation of the Latching Mechanism Assemblies

NOTE : See IPL_FIGURE_30.

(1) Install the latching mechanism assemblies 30-020 and 30-030 as follows:
(a) Clean the sleeve 30-210, the bushing 30-200 and the bolt 30-160 with a clean
Material No. 14SBA1 Textile-Lint free Cotton - made moist with the Material No.
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(b) Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to the mating surfaces of the sleeve 30-210, the bushing 30-200 and the bolt
30-160.
(c) Put the bushing 30-200 in position on the door structure and install the latching
mechanism assemblies 30-020 and 30-030 with the sleeve 30-210, the washer 30-170,
the bolt 30-160, the washer 30-170 and the nut 30-190.
(d) Tighten the nut 30-190.
(e) Safety the nut 30-190 with the new cotter pin 30-180, see PMS 01-05-44.
(f) Install the washer 30-140, the bolt 30-130, the washer 30-140 and the nut 30-150.
(g) Tighten the nut 30-150.
(h) Clean the sleeve 30-120, the bushings 30-100 and 30-110 and the bolt 30-080 with a
clean Material No. 14SBA1 Textile-Lint free Cotton - made moist with the Material
No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(i) Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to the mating surfaces of the sleeve 30-120, the bushings 30-100 and 30-110
and the bolt 30-080.
(j) Put the bushings 30-100 and 30-110 in position on the door structure and install the
latching mechanism assemblies 30-020 and 30-030, the sleeve 30-120, the washer
30-090, the bolt 30-080, the washer 30-070 and the nut 30-060.
(k) Tighten the nut 30-060.
(l) Safety the nut 30-060 with the new cotter pin 30-050, see PMS 01-05-44.
(m) Clean the bushings 30-250 and 30-260 and the bolt 30-230, 30-290 with a clean
Material No. 14SBA1 Textile-Lint free Cotton - made moist with the Material No.
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(n) Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to the mating surfaces of the bushings 30-250 and 30-260 and the bolt
30-230, 30-290.
(o) Install the bushings 30-250 and 30-260, the washer 30-240, the bolt 30-230, 30-290,
the washer 30-240 and the nut 30-280.

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(p) Tighten the nut 30-280.

(q) Safety the nut 30-280 with the new cotter pin 30-270, see PMS 01-05-44.
(r) Make sure that the upper dead center of the latching mechanism is correctly adjusted,
see ASSEMBLY TASK 52-32-17-800-801-A01.
(s) Make sure that the proximity switch 12MJ is correctly adjusted, see ASSEMBLY
TASK 52-32-17-800-801-A01.
(t) Make sure that the lower dead center of each latching mechanism is correctly
adjusted, see ASSEMBLY TASK 52-32-17-800-801-A01.

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**For PN’s D5237310000000 D5237310000200 D5237310000400 D5237310000800

TASK 52-32-17-400-808-A01
Assembly and Installation of the Latching Shaft Assembly
1. General
A. See REPAIR section for the component parts which have a permanent connection.
B. Make sure that the drain valves and the drain holes are clean and have no blockages.
C. When no torque value is specified, a standard torque value is applicable.
-

NOTE : For the standard torque values, see PMS 01-05-66.

NOTE : Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to all surfaces of parts which move.
2. Job Set-up Information
A. Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-400-807-A01 Installation of the Latching Mechanism Assemblies
TASK 52-32-17-400-805-A01 Installation of the Hand Lever Mechanism
PMS 01-05-66
Referenced Information
TABLE 1

3. Procedure

WARNING : BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

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.

Subtask 52-32-17-400-008-A01
A. Assembly and Installation of the Latching Shaft Assembly

NOTE : See IPL_FIGURE_32.

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(1) Assemble and install the latching shaft 32-010 as follows:

(a) Put the shaft levers 32-020 and 32-070, the stop cam 32-080, the switch lever 32-090
and the hinged lever assembly 32-100 in position on the latching shaft 32-010.

NOTE : Make sure that the shaft levers 32-020 and 32-070 are in the correct
position as recorded during the disassembly procedure.
(b) On the shaft lever 32-020 install the taper pins 32-030 and 32-060, the sleeves 32-040
and the nuts 32-050.
(c) On the shaft levers 32-070, the stop cam 32-080, the switch lever 32-090 and the
hinged lever assembly 32-100 install the taper pins 32-030, the sleeves 32-040 and the
nuts 32-050.
(d) Connect the latching mechanism assemblies, see ASSEMBLY TASK
52-32-17-400-807-A01 and the hand lever mechanism, see ASSEMBLY TASK
52-32-17-400-805-A01 on the latching shaft assembly 32-010.

Page 7024
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**For PN’s D5237310000600 D5237310001000 D5237310001200 D5237310001400 D5237310002000

TASK 52-32-17-400-808-B01
Assembly and Installation of the Latching Shaft Assembly
1. General
A. See REPAIR section for the component parts which have a permanent connection.
B. Make sure that the drain valves and the drain holes are clean and have no blockages.
C. When no torque value is specified, a standard torque value is applicable.
-

NOTE : For the standard torque values, see PMS 01-05-66.

NOTE : Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to all surfaces of parts which move.
2. Job Set-up Information
A. Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-400-807-A01 Installation of the Latching Mechanism Assemblies
TASK 52-32-17-400-805-A01 Installation of the Hand Lever Mechanism
PMS 01-05-66
Referenced Information
TABLE 1

3. Procedure

WARNING : BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

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.

Subtask 52-32-17-400-026-A01
A. Assembly and Installation of the Latching Shaft Assembly

NOTE : See IPL_FIGURE_32A.

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(1) Assemble and install the latching shaft 32A-020 as follows:

(a) Put the shaft levers 32A-030 and 32A-040, the stop cam 32A-050, the switch lever
32A-060, and the hinged lever assembly 32A-070 in position on the latching shaft
32A-020.

NOTE : Make sure that the shaft levers 32A-030 and 32A-040, are in the correct
position as recorded during the disassembly procedure.
(b) On the shaft lever 32A-030, install the taper pins 32A-100 and 32A-110, the sleeves
32A-120 and the nuts 32A-130.
(c) On the shaft levers 32A-040, the stop cam 32A-050, the switch lever 32A-060 and the
hinged lever assembly 32A-070, install the taper pins 32A-100, the sleeves 32A-120
and the nuts 32A-130.
(d) Connect the latching mechanism assemblies, see ASSEMBLY TASK
52-32-17-400-807-A01 and the hand lever mechanism, see ASSEMBLY TASK
52-32-17-400-805-A01 on the latching shaft assembly 32A-020.

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**For PN’s ALL

TASK 52-32-17-400-809-A01
Assembly and Installation of the Interlock Mechanism
1. General
A. See REPAIR section for the component parts which have a permanent connection.
B. Make sure that the drain valves and the drain holes are clean and have no blockages.
C. When no torque value is specified, a standard torque value is applicable.
-

NOTE : For the standard torque values, see PMS 01-05-66.

NOTE : Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to all surfaces of parts which move.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
14SBA1 Textile-Lint free Cotton -
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
03HBD9 Synthetic Ester base Grease-General Purpose Low Temp -
Consumable Materials
TABLE 1

B. Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-800-801-A01 Adjustment
PMS 01-05-66
PMS 01-05-44
Referenced Information
TABLE 2

3. Procedure

WARNING : BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

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Subtask 52-32-17-400-009-A01
A. Assembly and Installation of the Interlock Mechanism

NOTE : See IPL_FIGURE_44.

(1) Assemble the interlock mechanism 44-090 as follows:
(a) Clean the pin 44-130 and the roller 44-140 with a clean Material No. 14SBA1 Textile-
Lint free Cotton - made moist with the Material No. 08BBF1 Non Aqueous Cleaner--
Methyl-Ethyl-Ketone -.
(b) Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to the shaft of the pin 44-130 and the bore of the roller 44-140.
(c) Install the roller 44-140 and the pin 44-130 on the lever 44-100.
(d) Safety the pin 44-130 with the retaining ring 44-120.
(e) Install the adjusting screw 44-180 with the nut 44-190 and the locking plate 44-200
on the lever 44-170.

NOTE : Do not safety the nut 44-190 with the locking plate 44-200 at this time.
Attach a tag to say that the nut 44-190 must be safetied with the locking
plate 44-200 after the final adjustment of the door on the aircraft.
(f) Clean the pins 44-110 and the levers 44-100 and 44-170 with a clean Material No.
14SBA1 Textile-Lint free Cotton - made moist with the Material No. 08BBF1 Non
Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(g) Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to the shaft of the pins 44-110 and the inner side of the fork fittings of the
levers 44-100 and 44-170.
(h) Install the levers 44-100 and 44-170 with the pins 44-110 on the connecting rod
44-150.
(i) Safety the pins 44-110 with the retaining rings 44-160.
(j) Clean the pin 44-110 and the bolt 44-210 with a clean Material No. 14SBA1 Textile-
Lint free Cotton - made moist with the Material No. 08BBF1 Non Aqueous Cleaner--
Methyl-Ethyl-Ketone -.
(k) Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to the shaft of the pin 44-110 and the inner side of the fork-end of the bolt
44-210.
(l) Install the bolt 44-210 with the pin 44-110 on the lever 44-170.
(m) Safety the pin 44-110 with the retaining ring 44-160.

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(2) Install the interlock mechanism 44-090 as follows:

(a) Clean the bolt 44-210 and the shaft of the spring sleeve 44-020 with a clean Material
No. 14SBA1 Textile-Lint free Cotton - made moist with the Material No. 08BBF1
Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
(b) Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to the shafts of the bolt 44-210 and the spring sleeve 44-020.
(c) Clean the bushings 44-230 and 44-260 and the pin 44-050 with a clean Material No.
14SBA1 Textile-Lint free Cotton - made moist with the Material No. 08BBF1 Non
Aqueous Cleaner-- Methyl-Ethyl-Ketone -
(d) Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to the outer diameters of the bushings 44-230 and 44-260 and to the shaft of
the pin 44-050.
(e) Install the pin 44-050 and the washer 44-070.
(f) Safety the pin 44-050 with the new cotter pin 44-060, see PMS 01-05-44.
(g) Install the bushing 44-260 and the lever 44-170 on the door structure.
1 Install the washer 44-250, the bolt 44-270, the washer 44-250 and the nut
44-240.
2 Tighten the nut 44-240.
3 Safety the nut 44-240 with the new cotter pin 44-280, see PMS 01-05-44.
(h) Install the bushing 44-230 and the interlock mechanism 44-090 on the door structure.
1 Install the washer 44-220, the bolt 44-300 the washer 44-070 and the nut
44-290.
2 Tighten the nut 44-290.
3 Safety the nut 44-290 with the new cotter pin 44-060, see PMS 01-05-44.
(i) Install the spring sleeve assembly 44-010 with the compression spring 44-040 on the
bolt 44-210.

WARNING : YOU MUST INSTALL THE COMPRESSION SPRING WITH LOAD.

(j) Compress the compression spring 44-040 and the spring sleeve assembly 44-010 to
decrease its length.
(k) Install the pin 44-050 and the spacers 44-080 on the spring sleeve assembly 44-010
and on the door structure.
(l) Install the washer 44-070 and safety the pin 44-050 with the new cotter pin 44-060,
see PMS 01-05-44.
(3) Adjust the interlock mechanism 44-090, see ASSEMBLY TASK 52-32-17-800-801-A01.

Page 7029
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 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

**For PN’s D5237310000000 D5237310000200 D5237310000400 D5237310000800

TASK 52-32-17-400-810-A01
Installation of the Locking Shaft Assembly
1. General
A. See REPAIR section for the component parts which have a permanent connection.
B. Make sure that the drain valves and the drain holes are clean and have no blockages.
C. When no torque value is specified, a standard torque value is applicable.
-

NOTE : For the standard torque values, see PMS 01-05-66.

NOTE : Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to all surfaces of parts which move.
2. Job Set-up Information
A. Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-800-801-A01 Adjustment
TASK 52-32-17-400-805-A01 Installation of the Hand Lever Mechanism
TASK 52-32-17-400-813-A01 Assembly and Installation of the Vent Door Assembly
TASK 52-32-17-400-812-A01 Assembly and Installation of the Adjustable Rods and the Drift Pin
Rods
PMS 01-05-66
Referenced Information
TABLE 1

3. Procedure

WARNING : BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

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.

Page 7030
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Subtask 52-32-17-400-010-A01
A. Installation of the Locking Shaft Assembly

NOTE : See IPL_FIGURE_31.

NOTE : After the installation of the locking shaft assembly, you must connect the following
items to the locking shaft:
- The hand lever mechanism, see ASSEMBLY TASK 52-32-17-400-805-A01
- The vent door mechanism, see ASSEMBLY TASK 52-32-17-400-813-A01
- The drift pin mechanism, see ASSEMBLY TASK 52-32-17-400-812-A01.
(1) Install the locking shaft 31-010 as follows:
(a) Put the hinged lever assembly 31-090 and the locking cams 31-080 in position as
recorded during the DISASSEMBLY procedure.
(b) Put the lever 31-060 in position and install the locking shaft 31-010.
(c) Install the new rivet pins 31-070, the taper pins 31-020, the sleeves 31-050, the
washers 31-040 and the new nuts 31-030.
(2) Adjust the locking shaft assembly, see ASSEMBLY TASK 52-32-17-800-801-A01.

Page 7031
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

**For PN’s D5237310000600 D5237310001000 D5237310001200 D5237310001400

TASK 52-32-17-400-810-B01
Installation of the Locking Shaft Assembly
1. General
A. See REPAIR section for the component parts which have a permanent connection.
B. Make sure that the drain valves and the drain holes are clean and have no blockages.
C. When no torque value is specified, a standard torque value is applicable.
-

NOTE : For the standard torque values, see PMS 01-05-66.

NOTE : Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to all surfaces of parts which move.
2. Job Set-up Information
A. Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-800-801-A01 Adjustment
TASK 52-32-17-400-805-A01 Installation of the Hand Lever Mechanism
TASK 52-32-17-400-813-A01 Assembly and Installation of the Vent Door Assembly
TASK 52-32-17-400-812-A01 Assembly and Installation of the Adjustable Rods and the Drift Pin
Rods
PMS 01-05-66
Referenced Information
TABLE 1

3. Procedure

WARNING : BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

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.

Page 7032
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 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

Subtask 52-32-17-400-022-A01
A. Installation of the Locking Shaft Assembly

NOTE : See IPL_FIGURE_31A.

NOTE : After the installation of the locking shaft assembly, you must connect the following
items to the locking shaft:
- The hand lever mechanism, see ASSEMBLY TASK 52-32-17-400-805-A01
- The vent door mechanism, see ASSEMBLY TASK 52-32-17-400-813-A01
- The drift pin mechanism, see ASSEMBLY TASK 52-32-17-400-812-A01.
(1) Install the locking shaft 31A-020 as follows:
(a) Put the hinged lever assembly 31A-030 and the locking cams 31A-070 in position as
recorded during the DISASSEMBLY procedure.
(b) Put the lever 31A-060 in position and install the locking shaft 31A-020.
(c) Install the new rivet pins 31A-120, the taper pins 31A-080, the sleeves 31A-110, the
washers 31A-100 and the new nuts 31A-090.
(2) Adjust the locking shaft assembly, see ASSEMBLY TASK 52-32-17-800-801-A01.

Page 7033
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 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

**For PN’s D5237310002000

TASK 52-32-17-400-810-C01
Installation of the Locking Shaft Assembly
1. General
A. See REPAIR section for the component parts which have a permanent connection.
B. Make sure that the drain valves and the drain holes are clean and have no blockages.
C. When no torque value is specified, a standard torque value is applicable.
-

NOTE : For the standard torque values, see PMS 01-05-66.

NOTE : Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to all surfaces of parts which move.
2. Job Set-up Information
A. Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-800-801-A01 Adjustment
TASK 52-32-17-400-805-A01 Installation of the Hand Lever Mechanism
TASK 52-32-17-400-813-A01 Assembly and Installation of the Vent Door Assembly
TASK 52-32-17-400-812-A01 Assembly and Installation of the Adjustable Rods and the Drift Pin
Rods
PMS 01-05-66
Referenced Information
TABLE 1

3. Procedure

WARNING : BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

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.

Page 7034
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COMPONENT MAINTENANCE MANUAL
D5237310000000

Subtask 52-32-17-400-023-A01
A. Installation of the Locking Shaft Assembly

NOTE : See IPL_FIGURE_31B.

NOTE : After the installation of the locking shaft assembly, you must connect the following
items to the locking shaft:
- The hand lever mechanism, see ASSEMBLY TASK 52-32-17-400-805-A01
- The vent door mechanism, see ASSEMBLY TASK 52-32-17-400-813-A01
- The drift pin mechanism, see ASSEMBLY TASK 52-32-17-400-812-A01.
(1) Install the locking shaft 31B-070 as follows:
(a) Put the hinged lever assembly 31B-030 and the locking cams 31B-070 in position as
recorded during the DISASSEMBLY procedure.
(b) Put the lever 31B-060 in position and install the locking shaft 31B-020
(c) Install the new rivet pins 31B-120, the taper pins 31B-080, the sleeves 31B-110, the
washers 31B-100 and the new nuts 31B-130.
(2) Adjust the locking shaft assembly, see ASSEMBLY TASK 52-32-17-800-801-A01.

Page 7035
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

**For PN’s D5237310000000 D5237310000200 D5237310000400 D5237310000800

TASK 52-32-17-400-811-A01
Assembly and Installation of the Sequence Shaft
1. General
A. See REPAIR section for the component parts which have a permanent connection.
B. Make sure that the drain valves and the drain holes are clean and have no blockages.
C. When no torque value is specified, a standard torque value is applicable.
-

NOTE : For the standard torque values, see PMS 01-05-66.

NOTE : Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to all surfaces of parts which move.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
14SBA1 Textile-Lint free Cotton -
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
03HBD9 Synthetic Ester base Grease-General Purpose Low Temp -
Consumable Materials
TABLE 1

B.Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-400-812-A01 Assembly and Installation of the Adjustable Rods and the Drift Pin
Rods
PMS 01-05-66
PMS 01-05-44
PMS 01-05-03
Referenced Information
TABLE 2

3. Procedure

WARNING : BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

Page 7036
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

CAUTION : USE ONLY THE SPECIFIED MATERIALS. MATERIALS WHICH ARE NOT
SPECIFIED, CAN CAUSE DAMAGE.

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.

Subtask 52-32-17-400-011-A01
A. Assembly and Installation of the Sequence Shaft

NOTE : See IPL_FIGURE_31, IPL_FIGURE_40, IPL_FIGURE_41, IPL_FIGURE_95.

(1) Assemble and install the sequence shaft assembly 41-200 as follows:
(a) Assemble and install the sequence shaft assembly 41-200 as follows:
1 Install the sequence shaft 41-210 on the lever 41-220.
2 Install the lever assembly 41-240, the washer 41-335, the locking cam 41-310,
the washer 41-335 and the lever 41-330.

NOTE : You must install the lever assembly 41-240, the locking cam 41-310
and the levers 41-220 and 41-330 as recorded during the disassembly
procedure.
3 Install the new rivet pins 41-320, the taper pins 41-270, the sleeves 41-280, the
washers 41-290 and the new nuts 41-300.
(b) Install the connecting rod assembly 41-440 as follows:
1 Put the connecting rod assembly 41-440 in position on the levers 41-330 and
31-060 and install the washers 41-420, the bolts 41-430, the washers 41-400 and
the nuts 41-390.
2 Safety the nuts 41-390 with the new cotter pins 41-410, see PMS 01-05-44.
(c) Install the lever assembly 41-130 as follows:
1 Clean the surfaces of the fitting support 41-170 with a clean Material No.
14SBA1 Textile-Lint free Cotton - made moist with the Material No. 08BBF1
Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
2 Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose
Low Temp - to the shaft of the fitting support 41-170.
3 Install the lever 41-140, the washer 41-400 and the nut 41-390.
4 Safety the nut 41-390 with the new cotter pin 41-410, see PMS 01-05-44.

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D5237310000000

(d) Assemble and install the link assembly 41-010 as follows:

1 Install the new tab washers 41-040, the nuts 41-030 and 41-050 and the forks
41-020 and 41-060 on the rod 41-120, see PMS 01-05-03.
2 Make sure that you can see the thread of the shaft 41-120 through the
inspection holes in the forks 41-020 and 41-060.
3 Tighten the nuts 41-030 and 41-050 and safety with the tab washers 41-040, see
PMS 01-05-03.
4 Install the bushing 41-230, the link assembly 41-010 and the sleeves 41-070 and
41-350 on the lever 41-220 and the lever assembly 41-130.
5 Install the bolts 41-080 and 41-340, the washers 41-090 and 41-370, and the
nuts 41-100 and 41-360.
6 Safety the nuts 41-100 and 41-360 with the new cotter pins 41-110 and 41-380,
see PMS 01-05-44.
(2) Assemble and install the bellcrank housing assembly 40-020 as follows:
(a) Assemble and install the bellcrank housing assembly 40-020 as follows:
1 Put the levers 40-080 in position on the beam-4 cover 40-030 and install the
beam-4 shaft 40-060.
2 Install the taper pins 40-160, the sleeves 40-180 and the nuts 40-170.
3 Put the bellcrank housing assembly 40-020 in position on the door structure and
install the washers 40-200 and the bolts 40-190.
(b) Assemble the fixed rod 40-010 as follows:
1 Install the nuts 95-030 and 95-040 and the new locking washers 95-050 on the
clevis 95-010 and 95-020.
2 Install the clevis 95-010 and 95-020 with the nuts 95-030 and 95-040 and the
locking washers 95-050 on the rod body.

NOTE : Make sure that the distance between the clevis 95-010 and 95-020
centers is the same as recorded during the disassembly procedure.

NOTE : Do not safety the nuts 95-030 and 95-040 at this time. Attach a tag
to tell persons to safety the nuts 95-030 and 95-040 after the final
adjustment.
(c) Install the fixed rods 40-010 and 40-100 as follows:

NOTE : Before the installation of the fixed rod 40-010 at its upper end, you must
connect the drift pin mechanism, see ASSEMBLY TASK 52-32-17-400-812-
A01.

Page 7038
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COMPONENT MAINTENANCE MANUAL
D5237310000000

1 Put the fixed rods 40-010 and 40-100 in position and install the washers 40-150
and 40-240, the bolts 40-140 and 40-250, the washers 40-130 and 40-220 and
the nuts 40-120 and 40-210.
2 Safety the nuts 40-120 and 40-210 with the new cotter pins 40-110 and 40-230,
see PMS 01-05-44.

Page 7039
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

**For PN’s D5237310000600 D5237310001000 D5237310001200 D5237310001400

TASK 52-32-17-400-811-B01
Assembly and Installation of the Sequence Shaft
1. General
A. See REPAIR section for the component parts which have a permanent connection.
B. Make sure that the drain valves and the drain holes are clean and have no blockages.
C. When no torque value is specified, a standard torque value is applicable.
-

NOTE : For the standard torque values, see PMS 01-05-66.

NOTE : Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to all surfaces of parts which move.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
14SBA1 Textile-Lint free Cotton -
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
03HBD9 Synthetic Ester base Grease-General Purpose Low Temp -
Consumable Materials
TABLE 1

B.Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-400-812-A01 Assembly and Installation of the Adjustable Rods and the Drift Pin
Rods
PMS 01-05-66
PMS 01-05-03
PMS 01-05-44
Referenced Information
TABLE 2

3. Procedure

WARNING : BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

Page 7040
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

CAUTION : USE ONLY THE SPECIFIED MATERIALS. MATERIALS WHICH ARE NOT
SPECIFIED, CAN CAUSE DAMAGE.

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.

Subtask 52-32-17-400-019-A01
A. Assembly and Installation of the Sequence Shaft

NOTE : See IPL_FIGURE_31A, IPL_FIGURE_40, IPL_FIGURE_41A, IPL_FIGURE_95.

(1) Assemble and install the sequence shaft assembly 41A-200 as follows:
(a) Assemble and install the sequence shaft assembly 41A-200 as follows:
1 Install the sequence shaft 41A-210 on the serrated lever assembly 41A-220.
2 Install the link lever 41A-260, the serrated lever assembly 41A-220, the locking
cam 41A-250 and the serrated lever 41A-350.

NOTE : You must install the link lever 41A-260, the serrated lever assembly
41A-220, the locking cam 41A-250 and the serrated lever 41A-350 as
recorded during the disassembly procedure.
3 Install the new rivet pins 41A-280 and 41A-310, the washers 41A-290 and the
new nuts 41A-300.
4 Put the new lockwasher 41A-430 in position on the serrated lever 41A-350 and
install the screw 41A-420.
5 Tighten the screw 41A-420 and safety with the lockwasher 41A-430, see PMS
01-05-03.
(b) Install the connecting rod assembly 41A-440 as follows:
1 Put the connecting rod assembly 41A-440 in position on the serrated lever
41A-350 and the lever 31A-060 and install the washers 41A-410, the bolts
41A-400, the washers 41A-380 and the nuts 41A-370.
2 Safety the nuts 41A-370 with the new cotter pins 41A-390, see PMS 01-05-44.
(c) Install the lever assembly 41A-130 as follows:
1 Clean the surfaces of the fitting support 41A-170 with a clean Material No.
14SBA1 Textile-Lint free Cotton - made moist with the Material No. 08BBF1
Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
2 Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose
Low Temp - to the shaft of the fitting support 41A-170.
3 Install the lever 41A-140, the washer 41A-380 and the nut 41A-370.

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4 Safety the nut 41A-370 with the new cotter pin 41A-390, see PMS 01-05-44.
(d) Assemble and install the link assembly 41A-010 as follows:
1 Install the new tab washers 41A-040, the nuts 41A-030 and 41A-050 and the
forks 41A-020 and 41A-060 on the rod 41A-120, see PMS 01-05-03.
2 Make sure that you can see the thread of the rod 41A-120 through the
inspection holes in the forks 41A-020 and 41A-060.
3 Tighten the nuts 41A-030 and 41A-050 and safety with the tab washers
41A-040, see PMS 01-05-03.
4 Install the bushing 41A-270, the link assembly 41A-010 and the sleeves 41A-070
and 41A-330 on the link lever 41A-260 and the lever assembly 41A-130.
5 Install the bolts 41A-080 and 41A-320, the washers 41A-090 and 41A-290, and
the nuts 41A-100 and 41A-340.
6 Safety the nuts 41A-100 and 41A-340 with the new cotter pins 41A-110 and
41A-360, see PMS 01-05-44.
(2) Assemble and install the bellcrank housing assembly 40-020 as follows:
(a) Assemble and install the bellcrank housing assembly 40-020 as follows:
1 Put the levers 40-080 in position on the beam-4 cover 40-030 and install the
beam-4 shaft 40-060.
2 Install the taper pins 40-160, the sleeves 40-180 and the nuts 40-170.
3 Put the bellcrank housing assembly 40-020 in position on the door structure and
install the washers 40-200 and the bolts 40-190.
(b) Assemble the fixed rod 40-010 as follows:
1 Install the nuts 95-030 and 95-040 and the new locking washers 95-050 on the
clevis 95-010 and 95-020.
2 Install the clevis 95-010 and 95-020 with the nuts 95-030 and 95-040 and the
locking washers 95-050 on the rod body.

NOTE : Make sure that the distance between the clevis 95-010 and 95-020
centers is the same as recorded during the disassembly procedure.

NOTE : Do not safety the nuts 95-030 and 95-040 at this time. Attach a tag
to tell persons to safety the nuts 95-030 and 95-040 after the final
adjustment.
(c) Install the fixed rods 40-010 and 40-100 as follows:

NOTE : Before the installation of the fixed rod 40-010 at its upper end, you must
connect the drift pin mechanism, see ASSEMBLY TASK 52-32-17-400-812-
A01.

Page 7042
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D5237310000000

1 Put the fixed rods 40-010 and 40-100 in position and install the washers 40-150
and 40-240, the bolts 40-140 and 40-250, the washers 40-130 and 40-220 and
the nuts 40-120 and 40-210.
2 Safety the nuts 40-120 and 40-210 with the new cotter pins 40-110 and 40-230,
see PMS 01-05-44.

Page 7043
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

**For PN’s D5237310002000

TASK 52-32-17-400-811-C01
Assembly and Installation of the Sequence Shaft
1. General
A. See REPAIR section for the component parts which have a permanent connection.
B. Make sure that the drain valves and the drain holes are clean and have no blockages.
C. When no torque value is specified, a standard torque value is applicable.
-

NOTE : For the standard torque values, see PMS 01-05-66.

NOTE : Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to all surfaces of parts which move.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
14SBA1 Textile-Lint free Cotton -
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
03HBD9 Synthetic Ester base Grease-General Purpose Low Temp -
Consumable Materials
TABLE 1

B.Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-400-812-A01 Assembly and Installation of the Adjustable Rods and the Drift Pin
Rods
PMS 01-05-66
PMS 01-05-03
PMS 01-05-44
Referenced Information
TABLE 2

3. Procedure

WARNING : BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

Page 7044
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

CAUTION : USE ONLY THE SPECIFIED MATERIALS. MATERIALS WHICH ARE NOT
SPECIFIED, CAN CAUSE DAMAGE.

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.

Subtask 52-32-17-400-020-A01
A. Assembly and Installation of the Sequence Shaft

NOTE : See IPL_FIGURE_31B, IPL_FIGURE_40, IPL_FIGURE_41B, IPL_FIGURE_95.

(1) Assemble and install the sequence shaft assembly 41B-200 as follows:
(a) Assemble and install the sequence shaft assembly 41B-200 as follows:
1 Install the sequence shaft 41B-210 on the serrated lever assembly 41B-220.
2 Install the link lever 41B-260, the serrated lever assembly 41B-220, the locking
cam 41B-250 and the serrated lever 41B-350.

NOTE : You must install the link lever 41B-260, the serrated lever assembly
41B-220, the locking cam 41B-250 and the serrated lever 41B-350 as
recorded during the disassembly procedure.
3 Install the new rivet pins 41B-280 and the bolt 41B-310, the washers 41B-480
and the new nuts 41B-300 and 41B-470.
4 Put the new lockwasher 41B-430 in position on the serrated lever 41B-350 and
install the screw 41B-420.
5 Tighten the screw 41B-420 and safety with the lockwasher 41B-430, see PMS
01-05-03.
(b) Install the connecting rod assembly 41B-440 as follows:
1 Put the connecting rod assembly 41B-440 in position on the serrated lever
41B-350 and the lever 31B-060 and install the washers 41B-410, the bolts
41B-400, the washers 41B-380 and the nuts 41B-370.
2 Safety the nuts 41B-370 with the new cotter pins 41B-390, see PMS 01-05-44.
(c) Install the lever assembly 41B-130 as follows:
1 Clean the surfaces of the fitting support 41B-170 with a clean Material No.
14SBA1 Textile-Lint free Cotton - made moist with the Material No. 08BBF1
Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
2 Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose
Low Temp - to the shaft of the fitting support 41B-170.
3 Install the lever 41B-140, the washer 41B-380 and the nut 41B-370.

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4 Safety the nut 41B-370 with the new cotter pin 41B-390, see PMS 01-05-44.
(d) Assemble and install the link assembly 41B-010 as follows:
1 Install the new tab washers 41B-040, the nuts 41B-030 and 41B-050 and the
forks 41B-020 and 41B-060 on the rod 41B-120.
2 Make sure that you can see the thread of the rod 41B-120 through the
inspection holes in the forks 41B-020 and 41B-060.
3 Tighten the nuts 41B-030 and 41B-050 and safety with the tab washers
41B-040, see PMS 01-05-03.
4 Install the bushing 41B-270, the link assembly 41B-010 and the sleeves 41B-070
and 41B-330 on the link lever 41B-260 and the lever assembly 41B-130.
5 Install the bolts 41B-080 and 41B-320, the washers 41B-090 and 41B-290, and
the nuts 41B-100 and 41B-340.
6 Safety the nuts 41B-100 and 41B-340 with the new cotter pins 41B-110 and
41B-360, see PMS 01-05-44.
(2) Assemble and install the bellcrank housing assembly 40-020 as follows:
(a) Assemble and install the bellcrank housing assembly 40-020 as follows:
1 Put the levers 40-080 in position on the beam-4 cover 40-030 and install the
beam-4 shaft 40-060.
2 Install the taper pins 40-160, the sleeves 40-180 and the nuts 40-170.
3 Put the bellcrank housing assembly 40-020 in position on the door structure and
install the washers 40-200 and the bolts 40-190.
(b) Assemble the fixed rod 40-010 as follows:
1 Install the nuts 95-030 and 95-040 and the new locking washers 95-050 on the
clevis 95-010 and 95-020, see PMS 01-05-03.
2 Install the clevis 95-010 and 95-020 with the nuts 95-030 and 95-040 and the
locking washers 95-050 on the rod body.

NOTE : Make sure that the distance between the clevis 95-010 and 95-020
centers is the same as recorded during the disassembly procedure.

NOTE : Do not safety the nuts 95-030 and 95-040 at this time. Attach a tag
to tell persons to safety the nuts 95-030 and 95-040 after the final
adjustment.
(c) Install the fixed rods 40-010 and 40-100 as follows:

NOTE : Before the installation of the fixed rod 40-010 at its upper end, you must
connect the drift pin mechanism, see ASSEMBLY TASK 52-32-17-400-812-
A01.

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1 Put the fixed rods 40-010 and 40-100 in position and install the washers 40-150
and 40-240, the bolts 40-140 and 40-250, the washers 40-130 and 40-220 and
the nuts 40-120 and 40-210.
2 Safety the nuts 40-120 and 40-210 with the new cotter pins 40-110 and 40-230,
see PMS 01-05-44.

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**For PN’s ALL

TASK 52-32-17-400-812-A01
Assembly and Installation of the Adjustable Rods and the Drift Pin Rods
1. General
A. See REPAIR section for the component parts which have a permanent connection.
B. Make sure that the drain valves and the drain holes are clean and have no blockages.
C. When no torque value is specified, a standard torque value is applicable.
-

NOTE : For the standard torque values, see PMS 01-05-66.

NOTE : Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to all surfaces of parts which move.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
14SBA1 Textile-Lint free Cotton -
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
03HBD9 Synthetic Ester base Grease-General Purpose Low Temp -
Consumable Materials
TABLE 1

B. Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-400-811-A01 Assembly and Installation of the Sequence Shaft
TASK 52-32-17-400-811-B01 Assembly and Installation of the Sequence Shaft
TASK 52-32-17-400-811-C01 Assembly and Installation of the Sequence Shaft
TASK 52-32-17-800-801-A01 Adjustment
PMS 01-05-66
PMS 01-05-44
Referenced Information
TABLE 2

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3. Procedure

WARNING : BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

CAUTION : USE ONLY THE SPECIFIED MATERIALS. MATERIALS WHICH ARE NOT
SPECIFIED, CAN CAUSE DAMAGE.

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.

Subtask 52-32-17-400-012-A01
A. Assembly and Installation of the Adjustable Rods and the Drift Pin Rods

NOTE : See IPL_FIGURE_13, IPL_FIGURE_20, IPL_FIGURE_95.

(1) Install the bellcrank assembly 13-090 as follows:
(a) Put the link lever assemblies 13-100 and 13-130 in position and install the beam-3
shaft 13-160 on the door structure.
(b) Install the taper pins 13-170 and 13-280, the sleeves 13-180 and 13-290 and the nuts
13-190 and 13-300.
(c) Tighten the nuts 13-190 and 13-300.
(2) Install the rod assemblies 13-080 and 13-270 as follows:
(a) Clean the mating surfaces of the bushings 13-040, the bolts 13-020 and the drift pins
13-010 with a clean Material No. 14SBA1 Textile-Lint free Cotton - made moist with
the Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(b) Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to the mating surfaces of the bushings 13-040, the bolts 13-020 and the drift
pins 13-010.
(c) Install the drift pins 13-010 on the door structure.

NOTE : Make sure that the flattened side of the drift pins 13-010 show at the outer
side of the door structure.
(d) Put the rod assemblies 13-080 and 13-270 and the washers 13-030 and 13-220 in
position on the drift pins 13-010, the bellcrank assembly 13-090 and the link lever
assembly 20-180.
(e) Install the washers 13-210, the bolts 13-200 and 13-020, the bushings 13-040, the
washers 13-060 and 13-210 and the nuts 13-050 and 13-230.

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(f) Safety the nuts 13-050 and 13-230 with the new cotter pins 13-070 and 13-250, see
PMS 01-05-44.
(3) Assemble and install the adjustable rod 13-260 as follows:
(a) Assemble the adjustable rod 13-260 as follows:
1 Install the nuts 95-030 and 95-040 and the locking devices 95-050 on the clevis
95-010 and 95-020.
2 Install the clevis 95-010 and 95-020 with the nuts 95-030 and 95-040 and the
locking devices 95-050 on the rod body. Make sure that the length is the same
as the length recorded during the disassembly procedure.

NOTE : Do not tighten and safety the nuts 95-030 and 95-040 at this time.
Attach a tag to tell persons to safety the nuts 95-030 and 95-040 after
the adjustment.
(b) Install the adjustable rod 13-260 as follows:
1 Clean the threads of the bolts 13-200 with a clean Material No. 14SBA1 Textile-
Lint free Cotton - made moist with the Material No. 08BBF1 Non Aqueous
Cleaner-- Methyl-Ethyl-Ketone -.
2 Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose
Low Temp - to the shafts of the bolts 13-200.
3 Put the adjustable rod 13-260 in position on the bellcrank assembly 13-090 and
install the washers 13-210, the bolts 13-200, the washers 13-240 and the nuts
13-230.

NOTE : Do not tighten and safety the nuts 13-230 at this time. Attach a tag
to say that persons must tighten and safety the nuts 13-230 after the
adjustment of the drift pin mechanism, see ASSEMBLY TASK
52-32-17-800-801-A01.
4 Install the fixed rod 40-010 on the link lever assembly 13-130, see ASSEMBLY
TASK 52-32-17-400-811-A01TASK 52-32-17-400-811-B01TASK
52-32-17-400-811-C01.
5 Adjust the drift pin mechanism, see ASSEMBLY TASK 52-32-17-800-801-A01.

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**For PN’s ALL

TASK 52-32-17-400-813-A01
Assembly and Installation of the Vent Door Assembly
1. General
A. See REPAIR section for the component parts which have a permanent connection.
B. Make sure that the drain valves and the drain holes are clean and have no blockages.
C. When no torque value is specified, a standard torque value is applicable.
-

NOTE : For the standard torque values, see PMS 01-05-66.

NOTE : Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to all surfaces of parts which move.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
14SBA1 Textile-Lint free Cotton -
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
03HBD9 Synthetic Ester base Grease-General Purpose Low Temp -
Consumable Materials
TABLE 1

B. Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-400-814-A01 Installation of the Vent Door Actuating Mechanism
TASK 52-32-17-800-801-A01 Adjustment
PMS 01-05-66
PMS 01-05-44
Referenced Information
TABLE 2

3. Procedure

WARNING : BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

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CAUTION : USE ONLY THE SPECIFIED MATERIALS. MATERIALS WHICH ARE NOT
SPECIFIED, CAN CAUSE DAMAGE.

Subtask 52-32-17-400-013-A01
A. Assembly and Installation of the Vent Door Assembly

NOTE : See IPL_FIGURE_21.

(1) Assemble the vent door assembly 21-120 as follows:
(a) Install the nuts 21-220 and 21-340 and the new tab washers 21-230 and 21-350 on
the bolts 21-210 and 21-330.
(b) Install the bolts 21-210 and 21-330 with the nuts 21-220 and 21-340 and the tab
washers 21-230 and 21-350 on the actuator arms 21-240 and 21-360.

NOTE : Do not tighten and safety the nuts 21-220 and 21-340 at this time. Attach
a tag to tell persons to tighten and safety the nuts 21-220 and 21-340 after
the adjustment of the vent door assembly, see ASSEMBLY TASK
52-32-17-800-801-A01.
(c) Put the actuator arms 21-240 and 21-360 in position on the vent door 21-130 and
install the screws 21-140 and 21-170, the washers 21-160 and the nuts 21-150.
(d) Tighten the nuts 21-150.
(e) Put the bracket assembly 21-270 in position on the vent door 21-130 and install the
screws 21-140, the washers 21-160 and the nuts 21-150.
(f) Tighten the nuts 21-150.
(g) Put the spring bolts 21-390 in position on the actuator arms 21-240 and 21-360 and
install the washers 21-160 and safety with the new cotter pins 21-400, see PMS
01-05-44.
(2) Install the vent door assembly 21-120 as follows:
(a) Clean the sleeves 21-060 and 21-100, the bushings 21-190, 21-200 and 21-320 and the
shafts of the bolts 21-080 and 21-110 with a clean Material No. 14SBA1 Textile-Lint
free Cotton - made moist with the Material No. 08BBF1 Non Aqueous Cleaner--
Methyl-Ethyl-Ketone -.
(b) Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to the mating surfaces of the sleeves 21-060 and 21-100, the bushings 21-190,
21-200 and 21-320 and the shafts of the bolts 21-080 and 21-110.

WARNING : YOU MUST INSTALL THE SPRINGS WITH LOAD.

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(c) Install the washers 21-030, 21-031, 21-040 and 21-070, the springs 21-050 and
21-090, the sleeves 21-060 and 21-100, the bolts 21-080 and 21-110 and the vent
door assembly 21-120 on the door structure.

NOTE : Use the number and position of the washers 21-030, 21-031 and 21-040 as
recorded during the disassembly procedure.
(d) Install the nuts 21-020.
(e) Tighten the nuts 21-020 and safety with the new cotter pins 21-010, see PMS
01-05-44.
(f) Install the rod assembly 20-060 on the vent door assembly 21-120, see ASSEMBLY
TASK 52-32-17-400-814-A01.

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**For PN’s ALL

TASK 52-32-17-400-814-A01
Installation of the Vent Door Actuating Mechanism
1. General
A. See REPAIR section for the component parts which have a permanent connection.
B. Make sure that the drain valves and the drain holes are clean and have no blockages.
C. When no torque value is specified, a standard torque value is applicable.
-

NOTE : For the standard torque values, see PMS 01-05-66.

NOTE : Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to all surfaces of parts which move.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
14SBA1 Textile-Lint free Cotton -
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
03HBD9 Synthetic Ester base Grease-General Purpose Low Temp -
06AAB1 Polysulfide Sealant-General Purpose Fillet -
Consumable Materials
TABLE 1

B. Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-800-801-A01 Adjustment
PMS 01-05-66
PMS 01-05-44
PMS 01-05-47
Referenced Information
TABLE 2

3. Procedure

WARNING : BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

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CAUTION : USE ONLY THE SPECIFIED MATERIALS. MATERIALS WHICH ARE NOT
SPECIFIED, CAN CAUSE DAMAGE.

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.

Subtask 52-32-17-400-014-A01
A. Installation of the Vent Door Actuating Mechanism

NOTE : See IPL_FIGURE_13, IPL_FIGURE_20, IPL_FIGURE_95.

(1) Install the bellcrank assembly 20-160 as follows:
(a) Clean the outer diameter of the beam 3-shaft 20-170 and the shaft of the bolts
20-080 with a clean Material No. 14SBA1 Textile-Lint free Cotton - made moist with
the Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(b) Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to the outer diameter of the beam 3-shaft 20-170 and the shaft of the bolts
20-080.
(c) Put the link lever assemblies 20-180 and 20-220, the bush 20-230 and the beam 3-
shaft 20-170 in position on the door structure and install the taper pins 20-190,
20-290, the sleeves 20-200, 20-300 and the nuts 20-210, 20-310.
(d) Tighten the nuts 20-210, 20-310.
(e) Put the rod assembly 13-260 in position on the link lever assembly 20-180 and install
the washer 20-070, the bolt 20-080, the washer 20-030 and the nut 20-050.
(f) Tighten the nut 20-050 and safety with the new cotter pin 20-040, see PMS
01-05-44.
(2) Install the bellcrank assembly 20-090 as follows:
(a) Clean the outer diameter of the beam 3-shaft 20-110 with a clean Material No.
14SBA1 Textile-Lint free Cotton - made moist with the Material No. 08BBF1 Non
Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(b) Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to the outer diameter of the beam 3-shaft 20-110.
(c) Install the link lever assemblies 20-100 and the beam 3-shaft 20-110 with the taper
pins 20-120, 20-290, the sleeves 20-130, 20-300 and the nuts 20-140, 20-310.
(d) Tighten the nuts 20-140, 20-310.

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(3) Install the rod assembly 20-150 as follows:

(a) Clean the shaft of the bolts 20-080 with a clean Material No. 14SBA1 Textile-Lint
free Cotton - made moist with the Material No. 08BBF1 Non Aqueous Cleaner--
Methyl-Ethyl-Ketone -.
(b) Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to the shaft of the bolts 20-080.
(c) Put the rod assembly 20-150 in position on the bellcrank assemblies 20-090 and
20-160 and install the washers 20-070, the bolts 20-080, the washers 20-030 and the
nuts 20-050.
(d) Safety the nuts 20-050 with the new cotter pins 20-040, see PMS 01-05-44.
(4) Assemble and install the rod assembly 20-060 as follows:
(a) Assemble the rod assembly 20-060 as follows:
1 Install the nuts 95-030 and 95-040 and the locking devices 95-050 on the rod
ends 95-010 and 95-020.
2 Install the rod ends 95-010 and 95-020 with the nuts 95-030 and 95-040 and the
locking devices 95-050 on the rod body.
3 Make sure that the length is as recorded during the DISASSEMBLY procedure.

NOTE : Do not safety the nuts 95-030 and 95-040 at this time. Attach a tag
to tell persons to safety the nuts 95-030 and 95-040 after the
adjustment of the vent door assembly, see ASSEMBLY TASK
52-32-17-800-801-A01.
(b) Install the rod assembly 20-060 as follows:
1 Clean the shaft of the bolts 20-020 and 20-080 with a clean Material No.
14SBA1 Textile-Lint free Cotton - made moist with the Material No. 08BBF1
Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
2 Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose
Low Temp -to the shaft of the bolts 20-020 and 20-080.
3 Install the rod assembly 20-060 the washers 20-030 and 20-070, the bolts 20-020
and 20-080, the washers 20-030 and the nuts 20-050.

NOTE : Do not tighten and safety the nuts 20-050 at this time. Attach a tag
to tell persons that they must tighten and safety the nuts 20-050 after
the adjustment of the vent door assembly, see ASSEMBLY TASK
52-32-17-800-801-A01.
(5) Adjust the skin offset of the vent door assembly 20-010 as follows:
(a) Adjust the skin offset of the vent door assembly 20-010, see ASSEMBLY TASK
52-32-17-800-801-A01.

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(6) Install the cover 20-240 as follows:

(a) Clean the cover 20-240 and the door structure with a clean Material No. 14SBA1
Textile-Lint free Cotton - made moist with the Material No. 08BBF1 Non Aqueous
Cleaner-- Methyl-Ethyl-Ketone -.
(b) Apply the Material No. 06AAB1 Polysulfide Sealant-General Purpose Fillet - to the
mating surfaces of the cover 20-240 and the door structure, see PMS 01-05-47.
(c) Put the spacers 20-280 in position and install the cover 20-240, the screws 20-250,
the washers 20-260 and the nuts 20-270.
(d) Tighten the nuts 20-270.
(e) Remove the unwanted Material No. 06AAB1 Polysulfide Sealant-General Purpose
Fillet - with a clean Material No. 14SBA1 Textile-Lint free Cotton - made moist with
the Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.

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**For PN’s ALL

TASK 52-32-17-400-815-A01
Installation of the Door Sensors
1. General
A. See REPAIR section for the component parts which have a permanent connection.
B. Make sure that the drain valves and the drain holes are clean and have no blockages.
C. When no torque value is specified, a standard torque value is applicable.
-

NOTE : For the standard torque values, see PMS 01-05-66.

NOTE : Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to all surfaces of parts which move.
2. Job Set-up Information
A. Referenced Information
REFERENCE DESIGNATION
TASK 52-32-17-800-801-A01 Adjustment
PMS 01-05-66
Referenced Information
TABLE 1

3. Procedure

WARNING : BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

Subtask 52-32-17-400-015-A01
A. Installation of the Door Sensors

NOTE : See IPL_FIGURE_62.

NOTE : The rectangular proximity sensors 62-010 are referred to as proximity switches 62-010
in this paragraph.
(1) Install the door sensors as follows:
(a) Install the targets 62-020 as follows:
1 Put the targets 62-020 in position on the door structure and install the washers
62-070, the screws 62-030, 62-040 and 62-050, the washers 62-070 and the nuts
62-060.

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(b) Install the proximity switch 12MJ 62-010 (Detail B) as follows:

1 Remove the blanking caps from the electrical connectors.
2 Put the proximity switch 62-010 in position on the door structure and install the
screws 62-030.
3 Adjust the proximity switch 62-010, see ASSEMBLY TASK 52-32-17-800-801-
A01.
(c) Install the proximity switch 32WV 62-010 (Detail C) as follows:
1 Remove the blanking caps from the electrical connectors.
2 Put the proximity switch 62-010 in position on the door structure and install the
screws 62-050, the washers 62-070 and the nuts 62-060.
3 Adjust the proximity switch 62-010, see ASSEMBLY TASK 52-32-17-800-801-
A01.

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**For PN’s ALL

TASK 52-32-17-400-816-A01
Installation of the Door Drainage
1. General
A. See REPAIR section for the component parts which have a permanent connection.
B. Make sure that the drain valves and the drain holes are clean and have no blockages.
C. When no torque value is specified, a standard torque value is applicable.
-

NOTE : For the standard torque values, see PMS 01-05-66.

NOTE : Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to all surfaces of parts which move.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
14SBA1 Textile-Lint free Cotton -
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
06AAC1 Polysulfide Sealant-General Purpose Interfay -
Consumable Materials
TABLE 1

B. Referenced Information
REFERENCE DESIGNATION
PMS 01-05-66
PMS 01-02-36
Referenced Information
TABLE 2

3. Procedure

WARNING : BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

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Subtask 52-32-17-400-016-A01
A. Installation of the Door Drainage

NOTE : See IPL_FIGURE_50.

PRE SB 52-1124
(1) Install the tube 50-090 and the basic valve 50-030 (Detail A) as follows:
(a) Clean the mating surfaces of the valve retainer 50-020, the flange 50-080 and the
door structure with a clean Material No. 14SBA1 Textile-Lint free Cotton - made
moist with the Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(b) Apply the Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surfaces of the valve retainer 50-020 and the flange 50-080, see PMS
01-02-36.
(c) Put the valve retainer 50-020 in position on the door structure.
(d) Install the basic valve 50-030 in the valve retainer 50-020.
(e) Put the tube 50-090 with the flange 50-080 in position and install the screws 50-040,
the washers 50-050 and the nuts 50-060.
(f) Tighten the nuts 50-060.
(2) Install the basic valve 50-030 (Detail B) as follows:
(a) Clean the mating surfaces of the valve retainer 50-020 and the door structure with a
clean Material No. 14SBA1 Textile-Lint free Cotton - made moist with the Material
No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(b) Apply the Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surface of the valve retainer 50-020, see PMS 01-02-36.
(c) Put the valve retainer 50-020 in position on the door structure.
(d) Install the basic valve 50-030 in the valve retainer 50-020.
(e) Install the screws 50-070, the washers 50-050 and the nuts 50-060.
(f) Tighten the nuts 50-060.
POST SB 52-1124
(1) Install the tube assembly 50-090 and the valve 50-031 (Detail A) as follows:
(a) Clean the mating surfaces of the valve retainer 50-020, the flange 50-080 and the
door structure with a clean Material No. 14SBA1 Textile-Lint free Cotton - made
moist with the Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
(b) Apply the Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surfaces of the valve retainer 50-020 and the flange 50-080, see PMS
01-02-36.
(c) Put the valve retainer 50-020 in position on the door structure.

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(d) Install the valve 50-031 in the valve retainer 50-020.

(e) Put the tube assembly 50-090 with the flange 50-080 in position and install the
screws 50-040, the washers 50-050 and the nuts 50-060.
(f) Tighten the nuts 50-060.
(2) Install the valve 50-031 (Detail B) as follows:
(a) Clean the mating surfaces of the valve retainer 50-020 and the door structure with a
clean Material No. 14SBA1 Textile-Lint free Cotton - made moist with the Material
No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
(b) Apply the Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surface of the valve retainer 50-020, see PMS 01-02-36.
(c) Put the valve retainer 50-020 in position on the door structure.
(d) Install the valve 50-031 in the valve retainer 50-020.
(e) Install the screws 50-070, the washers 50-050 and the nuts 50-060.
(f) Tighten the nuts 50-060.
ALL VARIANTS
(3) Install the hose 50-010 as follows:
(a) Install the mount 50-110, the bolt 50-120, the washer 50-130 and the nut 50-140 on
the door structure.
(b) Tighten the nut 50-140.
(c) Move the lower end of the hose 50-010 through the holes in the door structure.
(d) Install the hose 50-010 on the tube assembly 50-090.
(e) Attach the hose 50-010 to the tube assembly 50-090 and the mount 50-110 with the
new cable ties 50-100.

NOTE : Make sure that the cable ties 50-100 do not compress the diameter of the
hose 50-010.

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**For PN’s D5237310000000 D5237310000200 D5237310000400 D5237310000800

TASK 52-32-17-400-817-A01
Installation of the Door Hinge Assemblies
1. General
A. See REPAIR section for the component parts which have a permanent connection.
B. Make sure that the drain valves and the drain holes are clean and have no blockages.
C. When no torque value is specified, a standard torque value is applicable.
-

NOTE : For the standard torque values, see PMS 01-05-66.

NOTE : Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to all surfaces of parts which move.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
14SBA1 Textile-Lint free Cotton -
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
06AAA1 Polysulfide Sealant-General Purpose Brushable -
06AAB1 Polysulfide Sealant-General Purpose Fillet -
04QAB2 Coating-- Flexible Structure
04SAB2 Varnish Polyurethane-- Marking Structure
Consumable Materials
TABLE 1

B. Referenced Information
REFERENCE DESIGNATION
PMS 01-05-66
PMS 01-02-36
PMS 01-05-47
PMS 01-02-41
PMS 01-05-67
Referenced Information
TABLE 2

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3. Procedure

WARNING : BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

CAUTION : USE ONLY THE SPECIFIED MATERIALS. MATERIALS WHICH ARE NOT
SPECIFIED, CAN CAUSE DAMAGE.

Subtask 52-32-17-400-017-A01
A. Installation of the Door Hinge Assemblies

NOTE : See IPL_FIGURE_90.

(1) Install the end fitting 90-010 as follows:
(a) Clean the mating surfaces of the shims 90-090, 90-091, 90-092, 90-093, 90-094,
90-095, 90-096, 90-097, 90-098, 90-099 with a clean Material No. 14SBA1 Textile-
Lint free Cotton - made moist with the Material No. 08BBF1 Non Aqueous Cleaner--
Methyl-Ethyl-Ketone -.
(b) Apply the Material No. 06AAA1 Polysulfide Sealant-General Purpose Brushable - to
the mating surfaces of the shims 90-090, 90-091, 90-092, 90-093, 90-094, 90-095,
90-096, 90-097, 90-098, 90-099, see PMS 01-02-36.

NOTE : Use the thickness of the shims 90-090, 90-091, 90-092, 90-093, 90-094,
90-095, 90-096, 90-097, 90-098, 90-099 as recorded during the disassembly
procedure.
(c) Install the shims 90-090, 90-091, 90-092, 90-093, 90-094, 90-095, 90-096, 90-097,
90-098, 90-099, the end fitting 90-010, the screws 90-100, the washers 90-110 and
the nuts 90-120.
(d) Apply the Material No. 06AAB1 Polysulfide Sealant-General Purpose Fillet - to the
space between the end fitting 90-010, see PMS 01-05-47.
(e) Let the Material No. 06AAB1 Polysulfide Sealant-General Purpose Fillet - dry.
(f) Apply the Material No. 04QAB2 Coating-- Flexible Structure to the Material No.
06AAB1 Polysulfide Sealant-General Purpose Fillet -, see PMS 01-02-41.
(g) Let the Material No. 04QAB2 Coating-- Flexible Structure dry.
(2) Install the hinge assemblies 90-020 and 90-050 as follows:
(a) Clean the mating surfaces of the hinge shims, the hinge assemblies 90-020 and 90-050
and the door structure 90-220 with a clean Material No. 14SBA1 Textile-Lint free
Cotton -made moist with the Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-
Ethyl-Ketone -.

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(b) Apply the Material No. 06AAA1 Polysulfide Sealant-General Purpose Brushable - to
the mating surfaces of the hinge shims and the hinge assemblies 90-020 and 90-050,
see PMS 01-02-36

NOTE : Use the thickness of the hinge shims as recorded during the disassembly
procedure.
(c) Put the hinge shims and the hinge assemblies 90-020 and 90-050 in position on the
door structure 90-220.
(d) Apply the Material No. 06AAA1 Polysulfide Sealant-General Purpose Brushable - to
the shaft of the screws 90-100, 90-105, 90-130, 90-160, 90-170, 90-180, 90-190,
90-195, 90-200 and 90-210, see PMS 01-02-36.
(e) Install the screws 90-100, 90-105, 90-130, 90-160, 90-170, 90-180, 90-190, 90-195,
90-200 and 90-210, the washers 90-110, 90-115 and 90-140 and the nuts 90-120,
90-125 and 90-150.
(f) Tighten the nuts 90-120, 90-125 and 90-150.
(g) Torque the screws 90-210 to 2.0 m.daN (14.751 lbf.ft).
(h) Put marks on the screws 90-210 and the door structure 90-220 with the Material No.
04SAB2 Varnish Polyurethane-- Marking Structure for identification as torqued, see
PMS 01-05-67.

Subtask 52-32-17-400-021-A01
B. Installation of the Door Hinge Assemblies

NOTE : See IPL_FIGURE_91.

(1) Install the end fitting 91-080 as follows:
(a) Clean the mating surfaces of the shims 91-090, 91-091, 91-092, 91-093, 91-094,
91-095, 91-096, 91-097, 91-098, 91-099 with a clean Material No. 14SBA1 Textile-
Lint free Cotton - made moist with the Material No. 08BBF1 Non Aqueous Cleaner--
Methyl-Ethyl-Ketone -.
(b) Apply the Material No. 06AAA1 Polysulfide Sealant-General Purpose Brushable - to
the mating surfaces of the shims 91-090, 91-091, 91-092, 91-093, 91-094, 91-095,
91-096, 91-097, 91-098, 91-099, see PMS 01-02-36.

NOTE : Use the thickness of the shims 91-090, 91-091, 91-092, 91-093, 91-094,
91-095, 91-096, 91-097, 91-098, 91-099 as recorded during the disassembly
procedure.
(c) Install the shims 91-090, 91-091, 91-092, 91-093, 91-094, 91-095, 91-096, 91-097,
91-098, 91-099, the end fitting 90-010, the screws 91-100, the washers 91-110 and
the nuts 91-120.

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(d) Apply the Material No. 06AAB1 Polysulfide Sealant-General Purpose Fillet - to the
space between the end fitting 91-080, see PMS 01-05-47.
(e) Let the Material No. 06AAB1 Polysulfide Sealant-General Purpose Fillet - dry.
(f) Apply the Material No. 04QAB2 Coating-- Flexible Structure to the Material No.
06AAB1 Polysulfide Sealant-General Purpose Fillet -, see PMS 01-02-41.
(g) Let the Material No. 04QAB2 Coating-- Flexible Structure dry.
(2) Install the hinge assemblies 91-010 and 91-050 as follows:
(a) Clean the mating surfaces of the hinge shims, the hinge assemblies 91-010 and 91-050
and the door structure with a clean Material No. 14SBA1 Textile-Lint free Cotton -
made moist with the Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-
Ketone -.
(b) Apply the Material No. 06AAA1 Polysulfide Sealant-General Purpose Brushable - to
the mating surfaces of the hinge shims and the hinge assemblies 91-010 and 91-050,
see PMS 01-02-36

NOTE : Use the thickness of the hinge shims as recorded during the disassembly
procedure.
(c) Put the hinge shims and the hinge assemblies 91-010 and 91-050 in position on the
door structure.
(d) Apply the Material No. 06AAA1 Polysulfide Sealant-General Purpose Brushable - to
the shaft of the screws 91-100, 91-105, 91-130, 91-160, 91-170, 91-180, 91-185,
91-190 and 91-200, see PMS 01-02-36.
(e) Install the screws 91-100, 91-105, 91-130, 91-160, 91-170, 91-180, 91-185, 91-190
and 91-200, the washers 91-110, 91-115 and 91-140 and the nuts 91-120, 91-125 and
91-150.
(f) Tighten the nuts 91-120, 91-125 and 91-150.
(g) Torque the screws 91-200 to 2.0 m.daN (14.751 lbf.ft).
(h) Put marks on the screws 91-200 and the door structure with the Material No.
04SAB2 Varnish Polyurethane-- Marking Structure for identification as torqued, see
PMS 01-05-67.

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**For PN’s D5237310000600 D5237310001000 D5237310001200 D5237310001400 D5237310002000

TASK 52-32-17-400-817-B01
Installation of the Door Hinge Assemblies
1. General
A. See REPAIR section for the component parts which have a permanent connection.
B. Make sure that the drain valves and the drain holes are clean and have no blockages.
C. When no torque value is specified, a standard torque value is applicable.
-

NOTE : For the standard torque values, see PMS 01-05-66.

NOTE : Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to all surfaces of parts which move.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
14SBA1 Textile-Lint free Cotton -
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
06AAA1 Polysulfide Sealant-General Purpose Brushable -
06AAB1 Polysulfide Sealant-General Purpose Fillet -
04QAB2 Coating-- Flexible Structure
04SAB2 Varnish Polyurethane-- Marking Structure
Consumable Materials
TABLE 1

B. Referenced Information
REFERENCE DESIGNATION
PMS 01-05-66
PMS 01-02-36
PMS 01-05-47
PMS 01-02-41
PMS 01-05-67
Referenced Information
TABLE 2

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3. Procedure

WARNING : BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

CAUTION : USE ONLY THE SPECIFIED MATERIALS. MATERIALS WHICH ARE NOT
SPECIFIED, CAN CAUSE DAMAGE.

Subtask 52-32-17-400-024-A01
A. Installation of the Door Hinge Assemblies

NOTE : See IPL_FIGURE_90A.

(1) Install the end fitting 90A-010 as follows:
(a) Clean the mating surfaces of the shims 90A-090, 90A-091, 90A-092, 90A-093,
90A-094, 90A-095, 90A-096, 90A-097, 90A-098, 90A-099 with a clean Material No.
14SBA1 Textile-Lint free Cotton - made moist with the Material No. 08BBF1 Non
Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(b) Apply the Material No. 06AAA1 Polysulfide Sealant-General Purpose Brushable - to
the mating surfaces of the shims 90A-090, 90A-091, 90A-092, 90A-093, 90A-094,
90A-095, 90A-096, 90A-097, 90A-098, 90A-099, see PMS 01-02-36.

NOTE : Use the thickness of the shims 90A-090, 90A-091, 90A-092, 90A-093,
90A-094, 90A-095, 90A-096, 90A-097, 90A-098, 90A-099 as recorded
during the disassembly procedure.
(c) Install the shims 90A-090, 90A-091, 90A-092, 90A-093, 90A-094, 90A-095, 90A-096,
90A-097, 90A-098, 90A-099, the end fitting 90A-010, the screws 90A-100, the
washers 90A-110 and the nuts 90A-120.
(d) Apply the Material No. 06AAB1 Polysulfide Sealant-General Purpose Fillet - to the
space between the end fitting 90A-010, see PMS 01-05-47.
(e) Let the Material No. 06AAB1 Polysulfide Sealant-General Purpose Fillet - dry.
(f) Apply the Material No. 04QAB2 Coating-- Flexible Structure to the Material No.
06AAB1 Polysulfide Sealant-General Purpose Fillet -, see PMS 01-02-41.
(g) Let the Material No. 04QAB2 Coating-- Flexible Structure dry.
(2) Install the hinge assemblies 90A-020 and 90A-050 as follows:
(a) Clean the mating surfaces of the hinge shims, the hinge assemblies 90A-020 and
90A-050 and the door structure 90A-220 with a clean Material No. 14SBA1 Textile-
Lint free Cotton -made moist with the Material No. 08BBF1 Non Aqueous Cleaner--
Methyl-Ethyl-Ketone -.

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(b) Apply the Material No. 06AAA1 Polysulfide Sealant-General Purpose Brushable - to
the mating surfaces of the hinge shims and the hinge assemblies 90A-020 and
90A-050, see PMS 01-02-36

NOTE : Use the thickness of the hinge shims as recorded during the disassembly
procedure.
(c) Put the hinge shims and the hinge assemblies 90A-020 and 90A-050 in position on the
door structure 90A-220.
(d) Apply the Material No. 06AAA1 Polysulfide Sealant-General Purpose Brushable - to
the shaft of the screws 90A-100, 90A-130, 90A-160, 90A-170, 90A-175, 90A-180,
90A-185, 90A-190, 90A-200 and 90A-210, see PMS 01-02-36.
(e) Install the screws 90A-100, 90A-130, 90A-160, 90A-170, 90A-175, 90A-180, 90A-185,
90A-190, 90A-200 and 90A-210, the washers 90A-110, 90A-140 and 90A-145 and the
nuts 90A-120, 90A-150 and 90A-155.
(f) Tighten the nuts 90A-120, 90A-150 and 90A-155.
(g) Torque the screws 90A-210 to 2.0 m.daN (14.751 lbf.ft).
(h) Put marks on the screws 90A-210 and the door structure 90A-220 with the Material
No. 04SAB2 Varnish Polyurethane-- Marking Structure for identification as torqued,
see PMS 01-05-67.

Subtask 52-32-17-400-025-A01
B. Installation of the Door Hinge Assemblies

NOTE : See IPL_FIGURE_91A.

(1) Install the end fitting 91A-080 as follows:
(a) Clean the mating surfaces of the shims 91A-090, 91A-091, 91A-092, 91A-093,
91A-094, 91A-095, 91A-096, 91A-097, 91A-098, 91A-099 with a clean Material No.
14SBA1 Textile-Lint free Cotton - made moist with the Material No. 08BBF1 Non
Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(b) Apply the Material No. 06AAA1 Polysulfide Sealant-General Purpose Brushable - to
the mating surfaces of the shims 91A-090, 91A-091, 91A-092, 91A-093, 91A-094,
91A-095, 91A-096, 91A-097, 91A-098, 91A-099, see PMS 01-02-36.

NOTE : Use the thickness of the shims 91A-090, 91A-091, 91A-092, 91A-093,
91A-094, 91A-095, 91A-096, 91A-097, 91A-098, 91A-099 as recorded
during the disassembly procedure.
(c) Install the shims 91A-090, 91A-091, 91A-092, 91A-093, 91A-094, 91A-095, 91A-096,
91A-097, 91A-098, 91A-099, the end fitting 90A-010, the screws 91A-100, the
washers 91A-110 and the nuts 91A-120.

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(d) Apply the Material No. 06AAB1 Polysulfide Sealant-General Purpose Fillet - to the
space between the end fitting 91A-080, see PMS 01-05-47.
(e) Let the Material No. 06AAB1 Polysulfide Sealant-General Purpose Fillet - dry.
(f) Apply the Material No. 04QAB2 Coating-- Flexible Structure to the Material No.
06AAB1 Polysulfide Sealant-General Purpose Fillet -, see PMS 01-02-41.
(g) Let the Material No. 04QAB2 Coating-- Flexible Structure dry.
(2) Install the hinge assemblies 91A-010 and 91A-050 as follows:
(a) Clean the mating surfaces of the hinge shims, the hinge assemblies 91A-010 and
91A-050 and the door structure with a clean Material No. 14SBA1 Textile-Lint free
Cotton -made moist with the Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-
Ethyl-Ketone -.
(b) Apply the Material No. 06AAA1 Polysulfide Sealant-General Purpose Brushable - to
the mating surfaces of the hinge shims and the hinge assemblies 91A-010 and
91A-050, see PMS 01-02-36

NOTE : Use the thickness of the hinge shims as recorded during the disassembly
procedure.
(c) Put the hinge shims and the hinge assemblies 91A-010 and 91A-050 in position on the
door structure.
(d) Apply the Material No. 06AAA1 Polysulfide Sealant-General Purpose Brushable - to
the shaft of the screws 91A-100, 91A-130, 91A-160, 91A-165, 91A-170, 91A-175,
91A-180, 91A-190, 91A-200, see PMS 01-02-36.
(e) Install the screws 91A-100, 91A-130, 91A-160, 91A-165, 91A-170, 91A-175, 91A-180,
91A-190, 91A-200, the washers 91A-110, 91A-140 and 91A-145 and the nuts
91A-120, 91A-150 and 91A-155.
(f) Tighten the nuts 91A-120, 91A-150 and 91A-155.
(g) Torque the screws 91A-200 to 2.0 m.daN (14.751 lbf.ft).
(h) Put marks on the screws 91A-200 and the door structure with the Material No.
04SAB2 Varnish Polyurethane-- Marking Structure for identification as torqued, see
PMS 01-05-67.

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**For PN’s ALL

TASK 52-32-17-400-818-A01
Installation of the Door Fairing
1. General
A. See REPAIR section for the component parts which have a permanent connection.
B. Make sure that the drain valves and the drain holes are clean and have no blockages.
C. When no torque value is specified, a standard torque value is applicable.
-

NOTE : For the standard torque values, see PMS 01-05-66.

NOTE : Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to all surfaces of parts which move.
2. Job Set-up Information
A. Referenced Information
REFERENCE DESIGNATION
PMS 01-05-66
Referenced Information
TABLE 1

3. Procedure

WARNING : BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

CAUTION : USE ONLY THE SPECIFIED MATERIALS. MATERIALS WHICH ARE NOT
SPECIFIED, CAN CAUSE DAMAGE.

Subtask 52-32-17-400-018-A01
A. Installation of the Door Fairing

NOTE : See IPL_FIGURE_70, IPL_FIGURE_71.

(1) Install the section assemblies 71-100, 71-170, 71-200 and 71-210 as follows:

NOTE : Use the marks on the door structure and the door web assemblies 71-100,
71-170, 71-200 and 71-210 made during the disassembly procedure.
(a) Put the edge section assembly 71-210 in position and tighten the studs 71-140.

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(b) Put the lower L-section 71-100 and the L-section assembly 71-200 in position and
install the washers 71-120 and the screws 71-110.
(c) Put the Z-section assembly 71-170 in position and install the washers 71-120 and the
screws 71-240.
(2) Install the fairing door web assemblies 71-130 and 71-160 as follows:

NOTE : Use the marks on the door structure and the door web assemblies 71-130 and
71-160 made during the disassembly procedure.
(a) Install the door web assembly 71-130 with the washers 71-120, the screws 71-110 and
the studs 71-140.
(b) Put the door web assembly 71-160 in position and install the washers 71-120 and the
screws 71-110.
(c) If removed, install the support plate 71-190 with the washers 71-120 and the screws
71-110.
(3) Install the fairings 70-010 and 70-020 as follows:
(a) If removed, install the sight glass 70-022 as follows:
1 Put the sight glass 70-022 in position on the fairing 70-020 and install the
screws 70-024, the washers 70-026 and the nuts 70-028.
2 Tighten the nuts 70-028.
(b) Put the fairings 70-010 and 70-020 in position on the fairing structure 70-060 and
install the washers 70-040 and the screws 70-030 and 70-050.

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**For PN’s ALL

TASK 52-32-17-800-801-A01
Adjustment
1. General
A. See REPAIR section for the component parts which have a permanent connection.
B. Make sure that the drain valves and the drain holes are clean and have no blockages.
C. When no torque value is specified, a standard torque value is applicable.
-

NOTE : For the standard torque values, see PMS 01-05-66.

NOTE : Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose Low
Temp - to all surfaces of parts which move.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
14QFB1 Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -
Consumable Materials
TABLE 1

B. Fixtures, Tools, Test and Support Equipment

REFERENCE DESIGNATION
98D52307525200 Rigging Pin
98D52307525000 Adjustment Tool - Cargo Doors
98D52307525100 Rigging Pin
98D52308309000 Rigging Pin
Fixtures, Tools, Test and Support Equipment
TABLE 2

C. Referenced Information
REFERENCE DESIGNATION
PMS 01-05-66
PMS 01-05-01
PMS 01-05-03
FIGURE 52-32-17-991-014-A FIGURE 52-32-17-991-014-A-Adjustment of the Hand Lever Assembly
FIGURE 52-32-17-991-015-A FIGURE 52-32-17-991-015-A-Adjustment of the Latching Mechanism

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REFERENCE DESIGNATION
FIGURE 52-32-17-991-016-A FIGURE 52-32-17-991-016-A-Adjustment of the Locking Mechanism
FIGURE 52-32-17-991-017-A FIGURE 52-32-17-991-017-A-Adjustment of the Drift Pin Mechanism
FIGURE 52-32-17-991-018-A FIGURE 52-32-17-991-018-A-Adjustment of the Interlock Mechanism
FIGURE 52-32-17-991-019-A FIGURE 52-32-17-991-019-A-Adjustment of the Vent Door Assembly
FIGURE 52-32-17-991-020-A FIGURE 52-32-17-991-020-A-Adjustment of the Proximity Sensors
Referenced Information
TABLE 3

3. Procedure

WARNING : BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

CAUTION : USE ONLY THE SPECIFIED MATERIALS. MATERIALS WHICH ARE NOT
SPECIFIED, CAN CAUSE DAMAGE.

Subtask 52-32-17-820-001-A01
A. Adjustment of the Hand Lever Assembly

NOTE : See FIGURE 52-32-17-991-014-A.

NOTE : The hand lever assembly (1) must be in the LOCKED position.
(1) Adjust the hand lever assembly (1) as follows:
(a) Adjust the clearance ’A’ as follows:
1 Do a check that the clearances ’A’ have the same dimension and are between
1.0 and 3.0 mm (0.0394 and 0.1181 in) between the hand lever assembly (1)
and the door structure.
2 If the clearances ’A’ are not in the limits, change the positions and/or the
quantity of the spacer washers (2) to make the necessary adjustment.
(b) Adjust the offset ’B’ (flush clearance) between the hand lever assembly (1) and the
installed access cover as follows:
1 Make sure that the offset ’B’ is between 0.0 and -1.0 mm (0.000 and -0.0393
in).
2 If the offset ’B’ is not correct, then do the subsequent steps.
3 Loosen the nut (4).
4 Adjust the offset ’B’ with the bolt (3).

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5 Tighten the nut (4).

(c) Adjust the catching hook (7) as follows:
1 Make sure that the bearing bolt (5) does not touch the catching hook (7).
2 Make sure that the clearance ’C’ is between 0.3 and 0.7 mm (0.0119 and 0.0275
in) while the hand lever assembly (1) is flush with the door structure.
3 If the clearance ’C’ is not correct, then do the subsequent steps.
4 Remove the bolts (9), the washers (8), the catching hook (7) and the shim (6).
5 Adjust the clearance ’C’ with the shim (6).
6 Install the shim (6), the catching hook (7), the washers (8) and the bolts (9).

Subtask 52-32-17-820-002-A01
B. Adjustment of the Latching Mechanism

NOTE : See FIGURE 52-32-17-991-015-A.

(1) Adjust the latching mechanism as follows:
(a) Make sure that the latching mechanism assemblies (1), see FIGURE
52-32-17-991-016-A are in the LOCKED position.
(b) Make sure that the hand lever assembly (1), see FIGURE 52-32-17-991-014-A is flush
with the door structure during the adjustment procedure.
(c) Install the 98D52307525200 Rigging Pin (1) of the adjustment tool 98D52307525000
Adjustment Tool - Cargo Doors through the rigging holes. These are in the door
structure and the bolts (6), (upper dead center).
(d) If you cannot install the 98D52307525200 Rigging Pin (1) easily, adjust the length of
the control rod (2) as follows:

WARNING : USE GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE.

EACH TIME YOU CUT LOCKWIRE DURING THE TASK, REMOVE
AND DISCARD IT (THE UNWANTED LOCKWIRE) IMMEDIATELY.
LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND.
1 If necessary, cut, remove and discard the lockwire from the safety devices (4) of
the control rod (2).
2 Loosen the two jam nuts (3).
3 Turn the turnbuckle (5) until you can install the 98D52307525200 Rigging Pin
(1) in the bolts (6) without force.
4 Tighten and safety the jam nuts (3) with the Material No. 14QFB1 Wire-
Locking Dia: 0.8 mm CRES Nickel Alloy - to the safety devices (4), see PMS
01-05-01.

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(e) Adjust the length of the six connecting rods (7) make sure that the lower over-
centering is correct:

WARNING : USE GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE.

EACH TIME YOU CUT LOCKWIRE DURING THE TASK, REMOVE
AND DISCARD IT (THE UNWANTED LOCKWIRE) IMMEDIATELY.
LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND.
1 If necessary, cut, remove and discard the lockwire from the safety devices (9) of
the connecting rod (7).
2 Loosen the two jam nuts (8).
3 Turn the turnbuckle (10) until the rear of the bellcrank assembly (11) touches
the bolt (14).
4 Turn the turnbuckle (10) 10 degrees back until you can move the connecting rod
(7) easily.
5 Make sure that you can install the 98D52307525100 Rigging Pin (13) of the
98D52307525000 Adjustment Tool - Cargo Doors easily through the rigging
holes. These are in the door structure and the bolt (12).
6 If not, turn the turnbuckle (10) until you can install the 98D52307525100
Rigging Pin (13) of the 98D52307525000 Adjustment Tool - Cargo Doors easily.
7 Tighten and safety the jam nuts (8) with the Material No. 14QFB1 Wire-
Locking Dia: 0.8 mm CRES Nickel Alloy - to the safety devices (9), see PMS
01-05-01.
8 Make sure that you can turn the connection rods (7).
9 Remove the 98D52307525200 Rigging Pin (1) and the 98D52307525100 Rigging
Pin (13) of the 98D52307525000 Adjustment Tool - Cargo Doors.

Subtask 52-32-17-820-003-A01
C. Adjustment of the Locking Mechanism

NOTE : See FIGURE 52-32-17-991-016-A.

(1) Adjust the locking mechanism as follows:
(a) Move the hand lever assembly away from the door structure up to a 65 degree
position.
(b) Make sure that the latching mechanism assemblies (1) stay in the LATCHED
position.
(c) Measure the clearance ’C’ between the locking cam (6) and the latching hook (7), see
Detail B.

NOTE : The dimension of the clearance ’C’ must be more than 2.0 mm (0.0788 in).

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(d) If the dimension is less than 2.0 mm (0.0788 in), adjust the control rod (5) as follows:

WARNING : USE GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE.

EACH TIME YOU CUT LOCKWIRE DURING THE TASK, REMOVE
AND DISCARD IT (THE UNWANTED LOCKWIRE) IMMEDIATELY.
LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND.
1 Cut, remove and discard the lockwire from the safety devices (3), see Detail A.
2 Loosen the two jam nuts (2).
3 Turn the turnbuckle (4) until the dimension is correct.
4 Tighten and safety the jam nuts (2) with the Material No. 14QFB1 Wire-
Locking Dia: 0.8 mm CRES Nickel Alloy - to the safety devices (3), see PMS
01-05-01.

Subtask 52-32-17-820-004-A01
D. Adjustment of the Drift Pin Mechanism

NOTE : See FIGURE 52-32-17-991-017-A.

(1) Adjust the drift pin mechanism as follows:
(a) Make sure that the hand lever assembly is in the LOCKED position and in the recess
of the door structure.
(b) Install the 98D52308309000 Rigging Pin (2) through the door structure and the link
lever assemblies (1).

NOTE : This position gives an over-centering height of approx. 1.5 mm (0.0590 in)
at the link lever assemblies (1).
(c) If you cannot install the 98D52308309000 Rigging Pin (2) easily into the link lever
assemblies (1), adjust the length of the fixed rod (3) and the adjustable rod (4) as
follows:

WARNING : USE GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE.

EACH TIME YOU CUT LOCKWIRE DURING THE TASK, REMOVE
AND DISCARD IT (THE UNWANTED LOCKWIRE) IMMEDIATELY.
LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND.
1 Cut, remove and discard the lockwire from the safety devices (6) and the
turnbuckle (7).
2 Loosen the two jam nuts (5).
3 Turn the turnbuckle (7) until you can install the 98D52308309000 Rigging Pin
(2) easily in the link lever assemblies (1).

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WARNING : USE GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE.

EACH TIME YOU CUT LOCKWIRE DURING THE TASK, REMOVE
AND DISCARD IT (THE UNWANTED LOCKWIRE) IMMEDIATELY.
LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND.
4 Tighten and safety the jam nuts (5) with the Material No. 14QFB1 Wire-
Locking Dia: 0.8 mm CRES Nickel Alloy - to the safety devices (6), see PMS
01-05-01.
(d) Measure the distance ’Y’ between the end of the extended drift pins and the edge
members of the door structure.

NOTE : The distance ’Y’ must be between 34.7 and 37.7 mm (1.3662 and 1.4842
in).
(e) Move the hand lever assembly to the UNLOCKED position.
(f) Make sure that the retracted drift pins are behind the skin edge of the door, see
Detail A, B Section A-A.

Subtask 52-32-17-820-005-A01
E. Adjustment of the Interlock Mechanism

NOTE : See FIGURE 52-32-17-991-018-A.

(1) Adjust the interlock mechanism as follows:
(a) Make sure that the hand lever assembly is in the UNLOCKED position.
(b) Measure the clearance ’Z’ between the adjusting screw (2) and the stop cam (1) of
the latching shaft assembly, see Detail A.

NOTE : The clearance ’Z’ must be between 1.0 and 1.4 mm (0.0394 and 0.0551 in).
(c) If the clearance ’Z’ is not in the limits, adjust as follows:
1 Bend and release the lock plate (4), see Detail B.
2 Loosen the nut (3) and remove the adjusting screw (2) from the lever (5).
3 Discard the lock plate (4).
4 Install the new lock plate (4) with the adjusting screw (2) and the nut (3) on
the lever (5).
5 Adjust the adjusting screw (2) until the clearance ’Z’ is correct, see Detail A.

NOTE : The clearance ’Z’ must be between 1.0 and 1.4 mm (0.0394 and
0.0551 in).
6 Tighten the nut (3) and safety it with the lock plate (4).

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Subtask 52-32-17-820-006-A01
F. Adjustment of the Skin Offset of the Vent Door Assembly

NOTE : See FIGURE 52-32-17-991-019-A.

(1) Adjust the skin offset of the vent door assembly (9) as follows:
(a) Make sure that the hand lever assembly is in the LOCKED position and in the recess
of the door structure.
(b) Measure the clearance ’A’ between the external contour of the vent door assembly (9)
and the door skin.
(c) Make sure that the clearance ’A’ is between 0.5 and 1.5 mm (0.0197 and 0.0590 in).
(d) If the skin offset is not correct, adjust the length of the adjustable rod (4) as follows:

WARNING : USE GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE.

EACH TIME YOU CUT LOCKWIRE DURING THE TASK, REMOVE
AND DISCARD IT (THE UNWANTED LOCKWIRE) IMMEDIATELY.
LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND.
1 Cut and remove the lockwire from the safety devices (2), see Detail C.
2 Loosen the jam nuts (1) to release the turnbuckle (3).
3 Turn the turnbuckle (3) until the skin offset is correctly adjusted.
4 Tighten and safety the jam nuts (1) with the Material No. 14QFB1 Wire-
Locking Dia: 0.8 mm CRES Nickel Alloy - to the safety devices, see PMS
01-05-01.
(e) Measure the clearance ’B’ between the bolts (5) and the stop (10) of the vent door
frame, see Detail B.
(f) Make sure that the clearance ’B’ is between 0.2 and 0.6 mm (0.0079 and 0.0236 in).
(g) If the clearance ’B’ is not correct, adjust the clearance as follows:
1 Pull the hand lever assembly out of the recess until it is in the position (65
degrees) to open the vent door assembly (9).
2 Bend the tab washers (7) to release the nuts (6), see Detail A.
3 Loosen the nuts (6) to release the bolts (5).
4 Remove the bolts (5), the nuts (6) and the tab washers (7) from the actuator
arms (8).
5 Discard the tab washers (7).
6 Install the bolts (5) with the nuts (6) and the new tab washers (7) on the
actuator arms (8).

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7 Make sure that the tab washers (7) are correctly installed on the actuator arms
(8).
8 Close the vent door assembly (9) as follows:
a Push the roller lever of the interlock mechanism to the outer side of the
door to release the latching shaft.
b Move the hand lever assembly down to the LOCKED position and push it
into the recess of the door structure.
9 Adjust the bolts (5) until the clearance ’B’ is between 0.2 and 0.6 mm (0.0079
and 0.0236 in).
10 Tighten the nuts (6) and safety them with the tab washers (7), see PMS
01-05-03.

Subtask 52-32-17-820-007-A01
G. Adjustment of the Proximity Sensors

NOTE : See FIGURE 52-32-17-991-020-A.

(1) Adjust the proximity sensors 12MJ and 34WV as follows:
(a) Adjust the proximity sensor 12MJ installed near the locking shaft as follows:
1 Make sure that the hand lever assembly (2) is in the UNLOCKED position, see
Detail A.
2 Move the hand lever assembly (2) and measure the clearance ’C’ between the
adjusting screw (5) and the stop cam (4), see Detail A,B.
3 Make sure that the clearance ’C’ is between 1.0 and 1.4 mm (0.0394 and 0.0551
in)
4 Measure the clearance ’B’ between the target (3) and the proximity sensor 12MJ
that is installed on the door structure.
5 Make sure that the clearance ’B’ is between 1.60 and 2.00 mm (0.0630 and
0.0787 in).
6 If the clearance is not correct, adjust the target (3) until you get the correct
clearance.
7 If the adjusting screw (5) touches the stop cam (4), adjust the clearance ’B’
between the proximity sensor 12MJ and the target (3) to a maximum of 3.0 mm
(0.1181 in).
(b) Adjust the proximity sensor 34WV installed near the hand lever assembly (2) as
follows:
1 Make sure that the hand lever assembly (2) is in the LOCKED position.

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2 Measure the clearance ’A’ between the proximity sensor 34WV and the target
(1) installed on the hand lever assembly (2).
3 The clearance ’A’ must be between 1.60 and 2.00 mm (0.0630 and 0.0787 in).
4 If the clearance is not correct, adjust the target (1) until you get the correct
clearance.

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**For PN’s ALL

DOOR SKIN
B C
ADJUSTMENT OF
1 CLEARANCE "A"

C CLEARANCE "A"

CLEARANCE "A"
"C"
2
"C"
F
E
10
ADJUSTMENT OF
HAND OFFSET
FOR THE MEASURE
POINTS 3, 4 AND 5
11

D
"B"

5 1

D
ADJUSTMENT OF
6 HAND OFFSET
FOR THE MEASURE
7 POINTS 1, 2 AND 6
F
8
9
1

BEAM4

1 4

HAND 3
OFFSET

ACCESS
COVER DIMENSION IN mm (in)
"A" 1.0 TO 3.0 (0.0394 TO 0.1181)
"B" 0.0 TO −1.0 (0.0000 TO −0.0393)
"C" 0.3 TO 0.7 (0.0119 TO 0.0275)

F_CM_523217_1_0140101_01_04

Adjustment of the Hand Lever Assembly

FIGURE-52-32-17-991-014-A01

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**For PN’s ALL

A
LATCHING UNIT
EXAMPLE

3
4
5 2

4
3

LATCHING SHAFT

6
1 1
8
9
10 7

9
8
14
11
LOCKING SHAFT
12

13 FR59A

NOTE:
1 THE RIGGING PIN (1) IS
ON AFT DOOR AT FR 59A ONLY

F_CM_523217_1_0150101_01_01

Adjustment of the Latching Mechanism

FIGURE-52-32-17-991-015-A01

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**For PN’s ALL

2
3

A
LATCHING
SHAFT
5

B
EXAMPLE LOCKING
SHAFT

CLEARANCE "C"
B

1
7

F_CM_523217_1_0160101_01_01

Adjustment of the Locking Mechanism

FIGURE-52-32-17-991-016-A01

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A B
DETAIL B MIRROR
IMAGE OF DETAIL A

A
C
D B
DRIFT PIN

A
A

SECTION

EXTENDED
A−A
E
DISTANCE "Y"
TYPICAL

IN RETRACTED CONDITION
THE DRIFT PIN MUST BE
BEHIND THE SKIN EDGE
5
6
4

7 SKIN EDGE
5.0 mm (0.1968 in)

C
D E
E

1
BELOW DEAD
CENTER ON THE
EXTENDED
DRIFT PIN

2
E
ABOVE DEAD CENTER
3 2 ON THE EXTENDED
DRIFT PIN

F_CM_523217_1_0170101_01_02

Adjustment of the Drift Pin Mechanism

FIGURE-52-32-17-991-017-A01

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A
LATCHING
SHAFT ASSEMBLY

CLEARANCE "Z"

B
B

F_CM_523217_1_0180101_01_01

Adjustment of the Interlock Mechanism

FIGURE-52-32-17-991-018-A01

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A A

8 C C
1
7

6 1

5
2
3
2 4
B

7
B
CLEARANCE "A" AND "B"
6 OF THE VENT DOOR STOP
AND SKIN OFFSET CHECK

CLEARANCE "B"
5
9
5

DIMENSION IN mm (in.)
10 VENT DOOR CONTOUR
"A" 0.5 TO 1.5 (0.0197 TO 0.0590)
CARGO DOOR CONTOUR
"B" 0.2 TO 0.6 (0.0079 TO 0.0236) CLEARANCE "A"
F_CM_523217_1_0190101_01_02

Adjustment of the Vent Door Assembly

FIGURE-52-32-17-991-019-A01

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A
CLEARANCE "A"

A
B

2
PROXIMITY SENSOR
34WV
1

B
PROXIMITY SENSOR
12MJ

CLEARANCE "B"

CLEARANCE "C" 4

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_523217_1_0200101_01_01

Adjustment of the Proximity Sensors

FIGURE-52-32-17-991-020-A01

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FITS AND CLEARANCES

**For PN’s ALL

TASK 52-32-17-820-807-A01
General
1. General
A. How to use the Fits and Clearances Table (See Sample 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

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**For PN’s ALL

TASK 52-32-17-820-808-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 Tables

NOTE : See FIGURE 52-32-17-991-021-A.

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MFR LIMITS IN-SERVICE WEAR LIMITS

MATING MAX
IPL ASSEMBLY DIMENSION ALLOWABLE
FIGURE DIMENSION CLEARANCE LIMITS CLEARANCES
AND millimeters millimeters millimeters millimeters
ITEM NO. (inches) (inches) (inches) (inches)
MIN MAX MIN MAX MIN MAX
B1 OD 08-250 15.976 15.994 15.951
(0.6290) (0.6296) 0.006 0.042 (0.6280) 0.092
B2 ID 09-020 16.000 16.018 (0.0003) (0.0016) 16.043 (0.0036)
(0.6300) (0.6306) (0.6316)
C1 OD 08-360 19.972 19.993 19.941
(0.7863) (0.7871) 0.007 0.049 (0.7851) 0.111
C2 ID 08-390 20.000 20.021 (0.0003) (0.0019) 20.052 (0.0043)
(0.7875) (0.7882) (0.7894)
C1 OD 08-360 19.972 19.993 19.941
(0.7863) (0.7871) 0.007 0.049 (0.7851) 0.111
C3 ID 08-530 20.000 20.021 (0.0003) (0.0019) 20.052 (0.0043)
(0.7875) (0.7882) (0.7894)
Fits and Clearances Table
TABLE 2

NOTE : See FIGURE 52-32-17-991-022-A.

MFR LIMITS IN-SERVICE WEAR LIMITS
MATING MAX
IPL ASSEMBLY DIMENSION ALLOWABLE
FIGURE DIMENSION CLEARANCE LIMITS CLEARANCES
AND millimeters millimeters millimeters millimeters
ITEM NO. (inches) (inches) (inches) (inches)
MIN MAX MIN MAX MIN MAX
D2 OD 30-210 13.966 13.984 13.941
(0.5499) (0.5505) 0.016 0.052 (0.5489) 0.102
D1 ID 33-180, 14.000 14.018 (0.0007) (0.0020) 14.043 (0.0040)
34-180 (0.5512) (0.5518) (0.5528)
E1 OD 30-120 22.959 22.980 22.928
(0.9039) (0.9047) 0.020 0.062 (0.9027) 0.124
E2 ID 33-040, 23.000 23.021 (0.0008) (0.0024) 23.052 (0.0048)
34-040 (0.9056) (0.9063) (0.9075)

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MFR LIMITS IN-SERVICE WEAR LIMITS

MATING MAX
IPL ASSEMBLY DIMENSION ALLOWABLE
FIGURE DIMENSION CLEARANCE LIMITS CLEARANCES
AND millimeters millimeters millimeters millimeters
ITEM NO. (inches) (inches) (inches) (inches)
MIN MAX MIN MAX MIN MAX
F1 OD 33-060, 12.983 12.994 12.967
34-060 (0.5112) (0.5115) 0.006 0.035 (0.5106) 0.076
F2 ID 33-190, 13.000 13.018 (0.0003) (0.0013) 13.043 (0.0029)
34-190 (0.5119) (0.5125) (0.5135)
G1 OD 33-060, 12.983 12.994 12.967
34-060 (0.5112) (0.5115) 0.006 0.035 (0.5106) 0.076
G2 ID 33-050, 13.000 13.018 (0.0003) (0.0013) 13.043 (0.0029)
34-050 (0.5119) (0.5125) (0.5135)
Fits and Clearances Table
TABLE 3

NOTE : See FIGURE 52-32-17-991-023-A.

MFR LIMITS IN-SERVICE WEAR LIMITS
MATING MAX
IPL ASSEMBLY DIMENSION ALLOWABLE
FIGURE DIMENSION CLEARANCE LIMITS CLEARANCES
AND millimeters millimeters millimeters millimeters
ITEM NO. (inches) (inches) (inches) (inches)
MIN MAX MIN MAX MIN MAX
B1 OD 40-060 19.980 19.993 19.960
(0.7867) (0.7871) 0.007 0.041 (0.7859) 0.092
B2 ID 40-050 20.000 20.021 (0.0003) (0.0016) 20.052 (0.0036)
(0.7875) (0.7882) (0.7894)
Fits and Clearances Table
TABLE 4

NOTE : See FIGURE 52-32-17-991-024-A.

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MFR LIMITS IN-SERVICE WEAR LIMITS

MATING MAX
IPL ASSEMBLY DIMENSION ALLOWABLE
FIGURE DIMENSION CLEARANCE LIMITS CLEARANCES
AND millimeters millimeters millimeters millimeters
ITEM NO. (inches) (inches) (inches) (inches)
MIN MAX MIN MAX MIN MAX
C1 OD FUSELAGE 10.857 10.900 10.400
HINGE (0.4275) (0.4291) (0.4095)
BOLT 0.300 0.386 1.100
C2 ID 90-080, 11.200 11.243 (0.0119) (0.0151) 11.500 (0.0433)
90A-080 (0.4410) (0.4426) (0.4527)
91-040,
91A-040
D1 OD FUSELAGE 10.857 10.900 10.400
HINGE (0.4275) (0.4291) (0.4095)
BOLT
D2 ID 90-040, 11.200 11.243 0.300 0.386 11.500 1.100
90A-040,90-070,
(0.4410) (0.4426) (0.0119) (0.0151) (0.4527) (0.0433)
90A-070
91-030,91A-030,
91-070,
91A-070
Fits and Clearances Table
TABLE 5

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**For PN’s ALL

A A

B C

SECTION
B2 B−B
B2

B1

SECTION
C−C

C1

C2 C3
F_CM_523217_1_0210101_01_00

Hand Lever Mechanism

FIGURE-52-32-17-991-021-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_523217_1_0220101_01_00

Latching Hook Assembly

FIGURE-52-32-17-991-022-A01

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**For PN’s ALL

A
A

B2 B1 SECTION B2
B−B

F_CM_523217_1_0230101_01_00

Sequence Shaft
FIGURE-52-32-17-991-023-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_523217_1_0240101_01_00

Door Hinge
FIGURE-52-32-17-991-024-A01

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SPECIAL TOOLS,FIXTURES,EQUIPMENT AND CONSUMABLES

**For PN’s ALL

TASK 52-32-17-940-809-A01
Special Tools, Fixtures and Equipment List
1. Special Tools, Fixtures and Equipment List
SUPPLIERS CODE
PART No. DESCRIPTION OR NAME AND WHERE USED TID
ADDRESS
355M03213000 Cable Loom TASK
52-32-17-700-801-
A01
355M03214000 Extension Cable Loom TASK
52-32-17-700-801-
A01
98D52307525000 Adjustment Tool - Cargo FAPE3 TASK
Doors 52-32-17-800-801-
A01
98D52307525100 Rigging Pin FAPE3 TASK
52-32-17-800-801-
A01
98D52307525200 Rigging Pin FAPE3 TASK
52-32-17-800-801-
A01
98D52308309000 Rigging Pin FAPE3 TASK
52-32-17-800-801-
A01
Special Tools, Fixtures and Equipment
TABLE 1

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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_523217_1_0250101_01_00

Tool Set for the Replacement of the Bushes of the Hinge Assemblies
FIGURE-52-32-17-991-025-A01

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STORAGE INCLUDING TRANSPORTATION

**For PN’s ALL

TASK 52-32-17-550-801-A01
Storage after Assembly
1. General
A. See Material Storage Data (MSD).
The MSD document is a chargeable service to support customers with inventory planning, with
specific focus on shelf life data, hazard information and other related general storage data. A
copy is provided, free of charge for the customer during the material readiness process. It is
available on CD-ROM from Airbus, or can be downloaded from the Airbus Spares Portal via
direct access of Single Sign On (SSO) in AirbusWorld.
2. Procedure

Subtask 52-32-17-620-001-A01
A. Material Storage Data
(1) Not applicable.

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ILLUSTRATED PARTS LIST

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INTRODUCTION

**For PN’s ALL

TASK 52-32-17-872-801-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

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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
70A L9247100500400 .STRAP-BONDING (V2D671) 1
80A L9247100501400 .STRAP-BONDING (V2D671) 1
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 TBIL
V04348 LAWRENCE ENGINEERING AND SUPPLY INC/”500 SO/ FLOWER ST, POB
30”/CA-91503/BURBANK/USA
V04795 TBIL
V06329 TBIL
V06383 PANDUIT CORP/17301 RIDGELAND/IL 60477-3048/TINLEY PARK/USA
V06725 TBIL
V08748 ELDEC CORPORATION/16700 13TH AVE WEST/WA 98046/LYNNWOOD/USA
V09455 TBIL
V0FKM1 TBIL
V0H380 TBIL
V0RFT4 TBIL
V0ZC92 TBIL
V10630 TBIL
V11815 TBIL
V13899 TBIL
V14283 AMPHENOL AEROSPACE/7077 CONSOLIDATED WAY/CA 92121/SAN DIEGO/USA
V15653 TBIL
V15860 TBIL
V17140 AEROSPACE PRODUCTS COMPAGNY/123 N.PINE
STREET/IN-46206/INDIANAPOLIS/USA
V17446 TBIL
V1ER65 TBIL
V1NVY1 TBIL
V1RC86 TBIL
V1V757 WESCO AIRCRAFT HARDWARE CORP/27727 AVE
SCOTT/91355/VALENCIA,CA/USA
V27238 TBIL
V29372 ALCOA GLOBAL FASTENERS INC/DBA ALCOA FASTENING SYSTEMS DIV TRIDAIR
PRODUCTS/3000 W LOMITA BLVD/CA 90505-5103/TORRANCE/USA
V2N935 TBIL
V32664 AEROMETALS INC/11362 MONIER PARK PL BLDG 3B/CA 95742/RANCHO
CORDOVA/USA
V42C51 MIDI PYRENNES PLASTIQUES/Z I ESCALQUENS/31320/CASTANET/FR

IPL INTRO
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CODE NAME AND ADDRESS

V49367 AMPHENOL CORP/AMPHENOL AEROSPACE,PYLE-NATIONAL CONNECTORS/40-60
DELAWARE AVE/13838/SIDNEY,NY/USA
V52828 TBIL
V52930 TBIL
V56563 ALATEC PRODUCTS INC/21123 NORDHOFF ST/CA
91311-2344/2344/CHATSWORTH/USA
V56878 TBIL
V57336 TBIL
V57983 GREER INDUSTRIES INC/2659 GRAVEL STREET/TX 76117-0249/14249/FORT
WORTH/USA
V58009 TBIL
V59730 THOMAS AND BETTS CORP/HWY 218 S/IA 52240/IOWA CITY/USA
V59736 TBIL
V5M902 TBIL
V5N982 BURBANK AIRCRAFT SUPPLY INC/2525 W 190TH
ST/CA-90504-6002/TORRANCE/USA
V60119 TBIL
V60360 TBIL
V60516 TBIL
V60996 TBIL
V62384 TBIL
V64381 TBIL
V65029 TBIL
V66065 W.S.WILSON CORP/24 HARBOR PARK DRIVE/NY-11050/PORT WASHINGTON/USA
V66776 TBIL
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 TBIL
V72962 TBIL
V73145 TBIL
V73197 TBIL
V75237 KAYNAR TECHNOLOGIES INC/MICRODOT DIV/190 W CROWTHER AVE/CA
92670/PLACENTIA/USA
V77445 UNITED TECHNOLOGIES CORP PRATT AND WHITNEY/400 MAIN STREET/CT
06108/EAST HARTFORD/USA
V80205 TBIL

IPL INTRO
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CODE NAME AND ADDRESS

V80539 TBIL
V81343 TBIL
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
V83324 TBIL
V84114 TBIL
V88044 TBIL
V8K160 TBIL
V8Z507 TBIL
V91345 MILLER DIAL CORP/4400 N TEMPLE CITY BLVD/CA 91734/EL MONTE/USA
V92215 TBIL
V92595 TBIL
V94931 BENDIX INTERNATIONAL/1633 BROADWAY/NY-10019/NEW YORK/USA
V952D1 SOURIAU-CLUSES/Z.I. DES GRANDS PRES/74301/CLUSES CEDEX/F
V96906 TBIL
V97464 INDUSTRIAL RETAINING RING CO/57 CORDIER ST/NJ-07111/IRVINGTON, NJ/USA
V97928 TBIL
VB0014 ADB NV/585 LEUVENSESTEENWEG/1930/ZAVENTEN/BEL
VB1395 TBIL
VC0258 TBIL
VC0259 PANDUIT GMBH/STEINMUEHL STRASSE 14/61352/BAD HOMBURG/GER
VC0506 KRUSE TECHNIK GMBH UND CO KG/GEEREN 26-28/2800/BREMEN 1/GER
VC1776 BOYSEN GMBH/STAHLGRUBERRING 49/81829/POSTFACH
820109/MUENCHEN/GER
VC3471 GLENAIR ELECTRIC GMBH/HOLZWEG 32A/61440/POSTFACH
4147/OBERURSEL/GER
VC3753 TBIL
VC3898 EUFA FASTENER GMBH/OTTO-HAHN-STRASSE.10/71083/HERRENBERG/GER
VC4293 TBIL
VC4344 FROELICH GMBH/FRIEDRICH-EBERT-STR.209/37520/OSTERODE/D
VC4863 SCHWARZ/IM UNTEREN RIED 7/75382/ALTHENGSTETT/D
VC5543 TBIL
VC5729 HONEYWELL HPG/LADEMANNBOGEN 128/22339/HAMBURG,/D

IPL INTRO
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CODE NAME AND ADDRESS

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
VC8431 TBIL
VD0680 TBIL
VD1283 HUCK INTERNATIONAL GMBH/AN DER UNTEREN SOESE
26/37520/OSTERODE/GER
VD1973 TBIL
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 TBIL
VD8518 TBIL
VD8527 HELLERMANN PAUL GMBH/SIEMENS STRASSE 5/25421/PINNEBERG/GER
VD9221 TBIL
VD9728 TBIL
VDM395 TBIL
VDM498 TBIL
VF0095 TBIL
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 TBIL
VF0224 TBIL
VF0225 SOURIAU/9 RUE DE LA PORTE DE BUC/78000/VERSAILLES/FR
VF0236 TBIL
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

IPL INTRO
Page 11
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

CODE NAME AND ADDRESS

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 TBIL
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 TBIL
VF6198 TBIL
VF7395 TBIL
VF7411 TBIL
VF7756 TBIL
VF8421 TBIL
VF8433 TBIL
VF8612 MATRIX SC FRANCE/29 CHS JULES CESAR/95300/CERGY PONTOISE CEDEX/FR
VF8982 TBIL
VF9211 TBIL
VFA3K5 TBIL
VFAFQ0 TBIL
VFAPE3 TBIL
VFAWT4 TBIL
VH1822 TBIL
VH2776 AIR PARTS INTERNATIONAL BV/KALKOVENWEG 12/2401/255/LK ALPHEN AD
RIJN/NL
VH6173 TBIL

IPL INTRO
Page 12
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

CODE NAME AND ADDRESS

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
VK1012 TBIL
VK1484 TBIL
VK1678 TBIL
VK4955 TBIL
VK4975 TBIL
VK5269 SKF (U.K) LTD AEROSPACE DIVISION/108 STRODE ROAD/BS21 6QQ/CLEVEDON
AVON/UK
VK5673 TBIL
VK6405 TBIL
VK7766 TBIL
VK8753 TBIL
VKC2C0 TBIL
VS0352 TBIL
VS5540 ULTRA PRECISION SA/MONTHEY/CH
VT0802 TBIL
VU1653 SOCIETY OF BRITISH AEROSPACE COMPANIES LTD/(STANDARDISATION
OFFICE.REFER TO OPT VENDORS)/29 KING STREET/SW1Y 6RD/LONDON/GB
VU6300 TBIL
VU7388 SMITHS AEROSPACE ACTUATION SYSTEMS/(FORMERLY DOWTY AEROSPACE
HYDRAULICS)/ARLE COURT/GL51 0TP/CHELTENHAM GLOUCESTER/GB
VU8528 TBIL

IPL INTRO
Page 13
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

DETAILED PARTS LIST

Page 10001
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

C
60 10

130
120
B
110
40
100

50

B
50
C

A
A C

70
A

30
A

80

30
35

20
40 90

F_PL_523217_01_0_01_00

DOOR ASSY-CARGO COMPARTMENT,AFT

Figure 01 / FIGURE-52-32-17-950-801-01

Page 10001-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01 - 001A D5237310000000 DOOR ASSY-CARGO COMPARTMENT,AFT VFAPE3 RF
01 - 001B D5237310000200 DOOR ASSY-CARGO COMPARTMENT,AFT VFAPE3 RF
01 - 001C D5237310000400 DOOR ASSY-CARGO COMPARTMENT,AFT VFAPE3 RF
01 - 001D D5237310000800 DOOR ASSY-CARGO COMPARTMENT,AFT VFAPE3 RF
01 - 001E D5237310000600 DOOR ASSY-CARGO COMPARTMENT,AFT VFAPE3 RF
01 - 001F D5237310001000 DOOR ASSY-CARGO COMPARTMENT,AFT VFAPE3 RF
01 - 001G D5237310001200 DOOR ASSY-CARGO COMPARTMENT,AFT VFAPE3 RF
01 - 001H D5237310001400 DOOR ASSY-CARGO COMPARTMENT,AFT VFAPE3 RF
01 - 001J D5237310002000 DOOR ASSY-CARGO COMPARTMENT,AFT VFAPE3 RF
01 010A D2587113500060 . PROTECTION INSTL-FIRE AND SEAL VFAPE3 001
INSTL-DOOR
used on 001A, 001B, 001C, 001D, 001E
SEE 52-32-17-020 FOR DET
01 010B D2587113500260 . PROTECTION INSTL-FIRE AND SEAL VFAPE3 001
INSTL-DOOR
used on 001F
SEE 52-32-17-020 FOR DET
01 010C D2587113500261 . PROTECTION INSTL-FIRE AND SEAL VFAPE3 001
INSTL-DOOR
used on 001G, 001H
SEE 52-32-17-020 FOR DET
01 010D D2557186500060 . PROTECTION INSTL-FIRE AND SEAL VFAPE3 001
INSTL-DOOR
used on 001J
SEE 52-32-17-020 FOR DET
01 020A D5237310200060 . COVER-ACCESS VFAPE3 001
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J
SEE 52-32-17-030 FOR DET
01 030A D5237311000060 . STRUCTURE ASSY VFAPE3 001
used on 001A, 001B, 001C, 001D
SEE 52-32-17-040 FOR DET
01 030B D5237311000460 . STRUCTURE ASSY VFAPE3 001
used on 001E, 001F, 001G, 001H, 001J
SEE 52-32-17-040 FOR DET
01 035A MS21209F1215P . INSERT V96906 003
Optional Vendor Code 8K160, D9728, F2094, K1012
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J
- ITEM NOT ILLUSTRATED

Page 10001-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01 040A D5237330000060 . MECHANISM ASSY-DOOR VFAPE3 001
used on 001A, 001B, 001C, 001D
SEE 52-32-17-050 FOR DET
01 040B D5237330000270 . MECHANISM ASSY-DOOR VFAPE3 001
used on 001E, 001F, 001G, 001H
SEE 52-32-17-050 FOR DET
01 040C D5237330000670 . MECHANISM ASSY-DOOR VFAPE3 001
used on 001J
SEE 52-32-17-050 FOR DET
01 050A D5237310000061 . HOUSING-VALVE VFAPE3 001
used on 001A, 001B, 001C
SEE 52-32-17-500 FOR DET
01 050B D5237310000062 . HOUSING-VALVE VFAPE3 001
used on 001D
SEE 52-32-17-500 FOR DET
01 050C D5237310000662 . HOUSING-VALVE VFAPE3 001
used on 001E, 001F, 001G, 001H, 001J
SEE 52-32-17-500 FOR DET
01 - 051A D5237310000062 . HOUSING-VALVE VFAPE3 002
POST SB 52-1124
used on 001B, 001C
SEE 52-32-17-500 FOR DET
01 060A D9209031203060 . ELECTRICAL SYSTEM VFAPE3 001
used on 001A
SEE 52-32-17-600 FOR DET
01 060B D9209031202260 . ELECTRICAL SYSTEM VFAPE3 001
used on 001B, 001C, 001D, 001E, 001F, 001G, 001H,
001J
SEE 52-32-17-600 FOR DET
01 070A D5347850100060 . FAIRING INSTL-AFT CARGO COMPT VFAPE3 001
DOOR
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J
SEE 52-32-17-700 FOR DET
01 080A NSA9117-23 . PLATE-IDENTIFICATION VF6198 001
NSA9117-23D F6198
Optional Vendor Code 04795, 2N935, C5543, D1973,
DM395, F8421, FA3K5, K1484
used on 001A, 001B
01 080B NSA9117-62 . PLATE-IDENTIFICATION VF6198 001
Optional Vendor Code 04795, 2N935, C5543, DM395,
F8421, FA3K5, K1484
- ITEM NOT ILLUSTRATED

Page 10001-2
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 001C, 001D
01 080C NSA9117-63 . PLATE-IDENTIFICATION VF6198 001
Optional Vendor Code 04795, 2N935, C5543, D1973,
DM395, F8421, FA3K5, K1484
used on 001E, 001F, 001G, 001H
01 080D NSA9117-69 . PLATE-IDENTIFICATION VF6198 001
Optional Vendor Code 04795, 2N935, C5543, DM395,
F8421, FA3K5, K1484
used on 001J
01 090A D5237121720000 . PLUG VFAPE3 003
OPT TO ABS0411PF1210 FAPE3
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J
01 100A D5237113420000 . SCREW-ADJUSTING VFAPE3 004
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H
01 100B D5237113420800 . SCREW-ADJUSTING VFAPE3 004
used on 001J
01 110A NAS509-5C . NUT V80205 004
Optional Vendor Code 01673, 56878, 60119, 8K160,
92595, F2094, FAWT4, T0802
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J
01 120A SP112G . WASHER-TAB VK7766 004
OPT TO 5310999480982 K4975
Optional Vendor Code F7395, F7756, FAWT4, K4955,
KC2C0, U8528
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J
01 130A NSA5054-5 . INSERT VF6198 004
OPT TO K8000-5 K6405
OPT TO SR314L0036 83324
Optional Vendor Code 04795, 2N935, 5M902, 83324,
C5543
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J
- ITEM NOT ILLUSTRATED

Page 10001-3
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

10

A
D
C C 90

C C

B E C

C
C C

C C

C
C
20

C
60
100
40 A

50 100
20 30

85
110

B C D E
TYPICAL
F_PL_523217_02_0_01_01

PROTECTION INSTL-FIRE AND SEAL INSTL-DOOR

Figure 02 / FIGURE-52-32-17-950-802-01

Page 10002-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
02 - 001A D2587113500060 PROTECTION INSTL-FIRE AND SEAL VFAPE3 RF
INSTL-DOOR
used on 010A (523217010)
SEE 52-32-17-010 FOR NHA
02 - 001B D2587113500260 PROTECTION INSTL-FIRE AND SEAL VFAPE3 RF
INSTL-DOOR
used on 010B (523217010)
SEE 52-32-17-010 FOR NHA
02 - 001C D2587113500261 PROTECTION INSTL-FIRE AND SEAL VFAPE3 RF
INSTL-DOOR
used on 010C (523217010)
SEE 52-32-17-010 FOR NHA
02 - 001D D2557186500060 PROTECTION INSTL-FIRE AND SEAL VFAPE3 RF
INSTL-DOOR
used on 010D (523217010)
SEE 52-32-17-010 FOR NHA
02 010A D2587113600000 . LINING ASSY-FIRE PROTECTION VFAPE3 001
used on 001A
SIL 25-135 ((FAR 25-856))
02 010B D2587113600200 . LINING ASSY-FIRE PROTECTION VFAPE3 001
used on 001B, 001C, 001D
02 010C D2557186700000 . LINING-FIRE PROTECTION VFAPE3 001
used on 001B, 001C, 001D
02 020A D2587113321200 .. INSULATION VFAPE3 016
Optional Vendor Code 1NVY1
used on 010A
SIL 25-135 ((FAR 25-856))
02 020B D2587114322200 .. MAT-INSULATION VFAPE3 016
used on 010B, 010C
02 030A NSA55131-007 .. STUD VF6198 018
OPT TO 2700-7S K1678
OPT TO J710-7N F9211
Optional Vendor Code 04795, 2N935, 71286, C5543,
D0680, DM498
used on 010A, 010B, 010C
02 040A D2587115820200 .. SPACER VFAPE3 018
used on 010A, 010B, 010C
02 050A NAS1149C0532R .. WASHER V80205 018
Optional Vendor Code 10630, 1ER65, 58009, 65029,
8K160
used on 010A, 010B, 010C
- ITEM NOT ILLUSTRATED

Page 10002-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
02 060A NSA55144-001 .. WASHER-LOCK VF6198 018
OPT TO 1127722 60119
OPT TO 2600SW K1678
Optional Vendor Code 04795, 2N935, 5M902, 60119,
71286, C5543, D0680, DM498
used on 010A, 010B, 010C
02 085A DAN98S1B .. TAPE-LOOP VD8518 AR
USE AS REQUIRED
ABS1133D020 FAPE3
OPT TO 6TBD501284 C0258
Optional Vendor Code 04795, 2N935, C3753, C5543,
D8518
used on 010A
02 085B ABS1133D020 .. TAPE VFAPE3 AR
USE AS REQUIRED
OPT TO APLIX840AP55L20 C3753
Optional Vendor Code 04795, 2N935, 64381, C5543
used on 010B, 010C
02 090A D5237300120000 . SEAL-DOOR VFAPE3 001
used on 001A, 001B
02 090B D5237300120200 . SEAL-DOOR VFAPE3 001
used on 001A, 001B, 001C, 001D
02 100A D5237112720000 . BUSHING VFAPE3 004
used on 001A, 001B, 001C, 001D
02 110A DAN98S1A . TAPE-HOOK VD8518 AR
USE AS REQUIRED, REQUIRED LENGTH 100 MM
ABS1133C020 FAPE3
OPT TO 6TBD501282 C0258
Optional Vendor Code 04795, 2N935, C3753, C5543,
D8518
used on 001A
02 110B ABS1133C020 . TAPE VFAPE3 AR
USE AS REQUIRED
OPT TO APLIX840AP55H20 C3753
Optional Vendor Code 04795, 2N935, 64381, C5543
used on 001B, 001C, 001D
- ITEM NOT ILLUSTRATED

Page 10002-2
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

110
A B

10

A D

120
F F
F
H
A G C
B F
F
H F H
F
100 C
C 30
F E
F C
20
D
C E 15

E E 40

E
G 140
150

D TO F

50 D
60 E
70 F 160

132 90 170

130
135 80
F_PL_523217_03_0_01_00

COVER-ACCESS
Figure 03 / FIGURE-52-32-17-950-803-01

Page 10003-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
03 - 001A D5237310200060 COVER-ACCESS VFAPE3 RF
used on 020A (523217010)
SEE 52-32-17-010 FOR NHA
03 010A D5237310200000 . COVER ASSY-ACCESS VFAPE3 001
used on 001A
03 015A D5237124220000 .. SHEET VFAPE3 004
used on 010A
03 020A D5237124120200 .. GLASS-SIGHT VFAPE3 004
used on 010A
03 030A NAS1102-06-6 .. SCREW V80205 008
Optional Vendor Code 04795, C5543, C5729, F0188,
K8753
used on 010A
03 040A 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
Optional Vendor Code 04795, 06329, 60996, 8K160,
C5543, C5729
used on 010A
03 050A ABS0691-015 .. STUD VFAPE3 002
OPT TO 1604S41-015BP D0680
OPT TO DV691-015 C4863
Optional Vendor Code 04795, C5543, C5729
used on 010A
03 060A ABS0691-020 .. STUD VFAPE3 005
OPT TO 1604S41-020BP D0680
OPT TO DV691-020 C4863
Optional Vendor Code 04795, C5543, C5729
used on 010A
03 070A ABS0691-030 .. STUD VFAPE3 010
OPT TO 1604S41-030BP D0680
OPT TO DV691-030 C4863
Optional Vendor Code 04795, C5543, C5729
used on 010A
03 080A ABS0604-4 .. WASHER VFAPE3 017
OPT TO CA21077-4 D0680
OPT TO SS604-4 C4863
Optional Vendor Code 04795, C5543, C5729
- ITEM NOT ILLUSTRATED

Page 10003-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 010A
03 090A ABS0692-01 .. WASHER-TAB VFAPE3 017
OPT TO 1604W50-1BP D0680
OPT TO H200S C4863
Optional Vendor Code 04795, C5543, C5729
used on 010A
03 100A NAS1791C3-1 .. NUT-PLATE V80205 004
OPT TO F50732-3-1 15653
OPT TO LACR53M1 F0224
OPT TO RF260C3M1 52828
Optional Vendor Code 04795, C5543, C5729
used on 010A
03 - 105A DIN65399-2400BF .. RIVET VD8286 AR
USE AS REQUIRED
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 D5237310500000 . COVER ASSY-ACCESS VFAPE3 001
used on 001A
03 132A D5237310520000 .. COVER-ACCESS VFAPE3 001
used on 130A
03 135A D5347504521800 .. SECTION-SEALING VFAPE3 002
used on 130A
03 140A NAS1100E3-8 . SCREW V80205 020
Optional Vendor Code 1ER65, 8Z507, F0188, F7411,
K8753
used on 001A
03 150A NAS1149C0332R . WASHER V80205 020
Optional Vendor Code 04795, 5N982, 60996, 8K160,
C5543, C5729
used on 001A
03 160A 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 170A DIN65399-2400BF . RIVET VD8286 034
used on 001A
- ITEM NOT ILLUSTRATED

Page 10003-2
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

10 A
70
90
60
70

50

50
B 80

40

130 50 30
50
100
B

120 130

50
70
90

110 60
70
20

130

F_PL_523217_04_0_01_00

STRUCTURE ASSY
Figure 04 / FIGURE-52-32-17-950-804-01

Page 10004-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
04 - 001A D5237311000060 STRUCTURE ASSY VFAPE3 RF
used on 030A (523217010)
SEE 52-32-17-010 FOR NHA
04 - 001B D5237311000460 STRUCTURE ASSY VFAPE3 RF
used on 030B (523217010)
SEE 52-32-17-010 FOR NHA
04 010A D5237311000061 . HINGE INSTL VFAPE3 001
used on 001A
SEE 52-32-17-900 FOR DET
04 010B D5237311000061 . HINGE INSTL VFAPE3 001
used on 001B
SEE 52-32-17-90A FOR DET
04 020A D5237127620800 . PLUG-PROTECTIVE VFAPE3 001
used on 001A, 001B
04 030A D5237310420000 . STOP-X VFAPE3 001
used on 001A, 001B
04 040A D5237310320600 . PLATE-ADJUSTING VFAPE3 001
selfrom, 1.20MM (0.047IN) THICK
used on 001A, 001B
04 - 041A D5237310320400 . PLATE-ADJUSTING VFAPE3 AR
selfrom, USE AS REQUIRED, 0.80MM (0.031IN)
THICK
used on 001A, 001B
04 - 042A D5237310320000 . PLATE-ADJUSTING VFAPE3 AR
selfrom, USE AS REQUIRED, 0.40MM (0.016IN)
THICK
used on 001A, 001B
04 - 043A D5237310320800 . PLATE-ADJUSTING VFAPE3 AR
selfrom, USE AS REQUIRED, 1.60MM (0.063IN)
THICK
used on 001A, 001B
04 050A NAS1102E3-10 . SCREW V80205 012
Optional Vendor Code 04795, 06329, 1ER65, C5543,
C5729, F0188, K8753
used on 001A, 001B
04 060A NAS1149C0332R . WASHER V80205 008
Optional Vendor Code 04795, 5N982, 60996, 8K160,
C5543, C5729
used on 001A, 001B
04 070A NAS1291C3M . NUT V80205 014
OPT TO H42-3 15653
- ITEM NOT ILLUSTRATED

Page 10004-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
Optional Vendor Code 04795, 60119, C5543, C5729,
F0224
used on 001A, 001B
04 080A NAS1102E3-14 . SCREW V80205 002
Optional Vendor Code F0188, K8753
used on 001A, 001B
04 090A ASNA0113-48CA . WASHER VF5442 006
Optional Vendor Code 04795, C1776, C5543, C5729,
F2094, F7395
used on 001A, 001B
04 100A D5237310420200 . STOP-X VFAPE3 001
used on 001A, 001B
04 110A D5237310321200 . PLATE-ADJUSTING VFAPE3 001
selfrom, 1.20MM (0.047IN) THICK
used on 001A, 001B
04 - 111A D5237310321000 . PLATE-ADJUSTING VFAPE3 AR
selfrom, USE AS REQUIRED, 0.80MM (0.031IN)
THICK
used on 001A, 001B
04 - 112A D5237310320200 . PLATE-ADJUSTING VFAPE3 AR
selfrom, USE AS REQUIRED, 0.40MM (0.016IN)
THICK
used on 001A, 001B
04 - 113A D5237310321400 . PLATE-ADJUSTING VFAPE3 AR
selfrom, USE AS REQUIRED, 1.60MM (0.063IN)
THICK
used on 001A, 001B
04 120A D5237127620000 . PLUG-PROTECTIVE VFAPE3 001
used on 001A, 001B
04 130A D5237127620200 . PLUG-PROTECTIVE VFAPE3 003
used on 001A, 001B
04 - 140A D5237311000063 . BUSHING INSTL-DOOR STRUCTURE VFAPE3 001
used on 001A, 001B
SEE 52-32-17-960 FOR DET
- ITEM NOT ILLUSTRATED

Page 10004-2
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

30

20

60

10

40
50

F_PL_523217_05_0_01_00

MECHANISM ASSY-DOOR
Figure 05 / FIGURE-52-32-17-950-805-01

Page 10005-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
05 - 001A D5237330000060 MECHANISM ASSY-DOOR VFAPE3 RF
used on 040A (523217010)
SEE 52-32-17-010 FOR NHA
05 - 001B D5237330000270 MECHANISM ASSY-DOOR VFAPE3 RF
used on 040B (523217010)
SEE 52-32-17-010 FOR NHA
05 - 001C D5237330000670 MECHANISM ASSY-DOOR VFAPE3 RF
used on 040C (523217010)
SEE 52-32-17-010 FOR NHA
05 010A D5237330000061 . HANDLE ASSY VFAPE3 001
used on 001A
SEE 52-32-17-080 FOR DET
05 010B D5237330000261 . HANDLE ASSY VFAPE3 001
used on 001B
SEE 52-32-17-080 FOR DET
05 010C D5237330000661 . HANDLE ASSY VFAPE3 001
used on 001C
SEE 52-32-17-080 FOR DET
05 - 013A D5237330000067 . HANDLE ASSY VFAPE3 001
used on 001A, 001B, 001C
SEE 52-32-17-080 FOR DET
05 - 015A D5237330000068 . HANDLE ASSY VFAPE3 001
used on 001A, 001B, 001C
SEE 52-32-17-080 FOR DET
05 020A D5237330000062 . ROD-ADJUSTABLE AND DRIFT PIN VFAPE3 001
used on 001A
SEE 52-32-17-130 FOR DET
05 020B D5237330000062 . ROD-ADJUSTABLE AND DRIFT PIN VFAPE3 001
used on 001B, 001C
SEE 52-32-17-130 FOR DET
05 - 023A D5237330000069 . ROD-ADJUSTABLE AND DRIFT PIN VFAPE3 001
used on 001A, 001B, 001C
SEE 52-32-17-130 FOR DET
05 - 025A D5237330000070 . ROD-ADJUSTABLE AND DRIFT PIN VFAPE3 001
used on 001A, 001B, 001C
SEE 52-32-17-130 FOR DET
05 030A D5237330000063 . DOOR ASSY-VENT VFAPE3 001
used on 001A
SEE 52-32-17-200 FOR DET
05 030B D5237330000063 . DOOR ASSY-VENT VFAPE3 001
used on 001B, 001C
SEE 52-32-17-200 FOR DET
- ITEM NOT ILLUSTRATED

Page 10005-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
05 - 033A D5237330000071 . DOOR ASSY-VENT VFAPE3 001
used on 001A, 001B, 001C
SEE 52-32-17-200 FOR DET
05 - 035A D5237330000072 . DOOR ASSY-VENT VFAPE3 001
used on 001A, 001B, 001C
SEE 52-32-17-200 FOR DET
05 040A D5237330000064 . MECHANISM ASSY-LATCHING VFAPE3 001
used on 001A
SEE 52-32-17-300 FOR DET
05 040B D5237330000064 . MECHANISM ASSY-LATCHING VFAPE3 001
used on 001B
SEE 52-32-17-300 FOR DET
05 040C D5237330000664 . MECHANISM ASSY-LATCHING VFAPE3 001
used on 001C
SEE 52-32-17-300 FOR DET
05 - 043A D5237330000075 . MECHANISM ASSY-LATCHING VFAPE3 001
used on 001A, 001B, 001C
SEE 52-32-17-300 FOR DET
05 - 045A D5237330000076 . MECHANISM ASSY-LATCHING VFAPE3 001
used on 001A, 001B, 001C
SEE 52-32-17-300 FOR DET
05 050A D5237330000065 . MECHANISM-INTERLOCK VFAPE3 001
used on 001A
SEE 52-32-17-440 FOR DET
05 050B D5237330000065 . MECHANISM-INTERLOCK VFAPE3 001
used on 001B, 001C
SEE 52-32-17-440 FOR DET
05 060A D5237330000066 . SHAFT-SEQUENCE VFAPE3 001
used on 001A
SEE 52-32-17-400 FOR DET
05 060B D5237330000066 . SHAFT-SEQUENCE VFAPE3 001
used on 001B
SEE 52-32-17-400 FOR DET
05 060C D5237330000666 . SHAFT-SEQUENCE VFAPE3 001
used on 001C
SEE 52-32-17-400 FOR DET
05 - 063A D5237330000073 . SHAFT-SEQUENCE VFAPE3 001
used on 001A, 001B, 001C
SEE 52-32-17-400 FOR DET
05 - 065A D5237330000074 . SHAFT-SEQUENCE VFAPE3 001
used on 001A, 001B, 001C
SEE 52-32-17-400 FOR DET
- ITEM NOT ILLUSTRATED

Page 10005-2
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

120
30 130
60
70 110
120
A 20 80 60
350 50 70
80
140
250 40
A
150 80
50
260 80
360
230 60
510 70
90
520 530
260
270
530 60
370 100
410 70
420 110
400 220
570 200
240 580
270 380 210

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

120 200
500 210

470

10

170
180
110 190
220
440
F_PL_523217_08_0_01_00

HANDLE ASSY
Figure 08 / FIGURE-52-32-17-950-808-01

Page 10008-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
08 - 001A D5237330000061 HANDLE ASSY VFAPE3 RF
used on 010A (523217050)
SEE 52-32-17-050 FOR NHA
08 - 001B D5237330000067 HANDLE ASSY VFAPE3 RF
used on 013A (523217050)
SEE 52-32-17-050 FOR NHA
08 - 001C D5237330000068 HANDLE ASSY VFAPE3 RF
used on 015A (523217050)
SEE 52-32-17-050 FOR NHA
08 - 001D D5237330000261 HANDLE ASSY VFAPE3 RF
used on 010B (523217050)
SEE 52-32-17-050 FOR NHA
08 - 001E D5237330000661 HANDLE ASSY VFAPE3 RF
used on 010C (523217050)
SEE 52-32-17-050 FOR NHA
08 010A D5237177000200 . LEVER ASSY-HAND VFAPE3 001
used on 001A, 001B, 001C, 001D, 001E
SEE 52-32-17-090 FOR DET
08 020A D5237178000200 . LEVER ASSY-SERRATED VFAPE3 001
used on 001A, 001B, 001C, 001D, 001E
08 020B D5237178000000 . LEVER ASSY VFAPE3 001
used on 001D, 001E
08 030A D5237177620000 .. BRACKET VFAPE3 001
used on 020A, 020B
08 040A ASNA2151-08 .. ACTUATING UNIT VF6198 001
OPT TO 192953 D8485
Optional Vendor Code 04795, 2N935, C5543, D8485,
F8433
used on 020A, 020B
08 050A F5237136720200 .. PIN-LOCATING VFAPE3 002
used on 020A, 020B
08 060A MS24665-86 .. PIN-COTTER V96906 004
Optional Vendor Code 11815, 65029, 73145, 84114,
8K160
used on 020A, 020B
08 070A NAS1149C0463R .. WASHER V80205 004
Optional Vendor Code 10630, 1ER65, 58009, 65029,
8K160
used on 020A, 020B
- ITEM NOT ILLUSTRATED

Page 10008-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
08 080A NAS1149C0432R .. WASHER V80205 004
Optional Vendor Code 10630, 1ER65, 58009, 65029,
8K160
used on 020A, 020B
08 090A D5237179620200 .. LEVER-SERRATED VFAPE3 001
used on 020A
08 090B D5237179620000 .. LEVER VFAPE3 001
used on 020B
08 100A MS14103-4K .. BEARING V96906 001
Optional Vendor Code 09455, 15860, F0222, S0352
used on 020A
08 100B MS14102-4K .. BEARING V96906 001
Optional Vendor Code 15860, S0352
used on 020B
08 110A NAS1291C3M . NUT V80205 007
OPT TO H42-3 15653
Optional Vendor Code 15653, 27238, 52828, F0224
used on 001A, 001B, 001C, 001D, 001E
08 120A NAS1149C0332R . WASHER V80205 009
Optional Vendor Code 10630, 58009, 65029, 8K160
used on 001A, 001B, 001C, 001D, 001E
08 130A NSA5031-3-5 . BOLT VF6198 003
Optional Vendor Code 04795, 2N935, C4293, C5543,
F6167, F7411, FAWT4, T0802
used on 001A, 001B, 001C, 001D, 001E
08 140A NSA5031-3-2 . BOLT VF6198 002
ABS0114T3-2 FAPE3
Optional Vendor Code 04795, 2N935, C4293, C5543,
F6167, F7411, FAWT4, K8753, T0802
used on 001A, 001B, 001C, 001D, 001E
08 150A D5237179820000 . WASHER-LOCK VFAPE3 001
used on 001A, 001B, 001C, 001D, 001E
08 160A D5237176820000 . ROD ASSY VFAPE3 001
OPT TO B322104-003 F0222
OPT TO R24359 B1395
used on 001A, 001D, 001E
08 160B R24359 . ROD ASSY VB1395 001
OPT TO D5237176820000 FAPE3
used on 001B
SEE 52-32-17-950 FOR DET
08 160C B322104-003 . ROD ASSY VF0222 001
OPT TO D5237176820000 FAPE3
- ITEM NOT ILLUSTRATED

Page 10008-2
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 001C
08 170A MS24665-151 . PIN-COTTER V96906 003
Optional Vendor Code 10630, 65029, 73145, 84114,
8K160
used on 001A, 001B, 001C, 001D, 001E
08 180A NSA5059C4 . NUT VF6198 003
OPT TO TE9925-4 72962
OPT TO THCR54 F0224
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 001A
08 180B NSA5059E4 . NUT VF6198 003
OPT TO 73783CM8-428 56878
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 001D, 001E
08 190A NAS1149C0463R . WASHER V80205 003
Optional Vendor Code 10630, 1ER65, 58009, 65029,
8K160
used on 001A, 001B, 001C, 001D, 001E
08 200A NSA5031-4D11 . BOLT VF6198 003
Optional Vendor Code 04795, 2N935, C4293, C5543,
FAWT4, K8753, T0802
used on 001A, 001B, 001C, 001D, 001E
08 210A NAS1149C0432R . WASHER V80205 003
Optional Vendor Code 10630, 1ER65, 58009, 65029,
8K160
used on 001A, 001B, 001C, 001D, 001E
08 220A NAS1149C0363R . WASHER V80205 003
Optional Vendor Code 10630, 1ER65, 58009, 65029,
8K160
used on 001A, 001B, 001C, 001D, 001E
08 230A NSA5031-3-17 . BOLT VF6198 002
Optional Vendor Code 04795, 2N935, C4293, C5543,
F6167, F7411, FAWT4, K5673, K8753, T0802
used on 001A, 001B, 001C, 001D, 001E
08 240A D5237179120000 . LOCK-UNIVERSAL JOINT VFAPE3 001
used on 001A, 001B, 001C, 001D, 001E
08 250A D5237179720200 . SHAFT VFAPE3 001
used on 001A, 001B, 001C, 001D, 001E
08 260A D5237179922000 . WASHER-SPACER VFAPE3 002
used on 001A, 001B, 001C, 001D, 001E
- ITEM NOT ILLUSTRATED

Page 10008-3
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
08 270A D5237179920800 . WASHER-SPACER VFAPE3 002
selfrom, THICKNESS 3.8 MM
used on 001A, 001B, 001C, 001D, 001E
08 - 271A D5237179920600 . WASHER-SPACER VFAPE3 AR
selfrom, USE AS REQUIRED, THICKNESS 3.6 MM
used on 001A, 001B, 001C, 001D, 001E
08 - 272A D5237179921000 . WASHER-SPACER VFAPE3 AR
selfrom, USE AS REQUIRED, THICKNESS 4.0 MM
used on 001A, 001B, 001C, 001D, 001E
08 - 273A D5237179921200 . WASHER-SPACER VFAPE3 AR
selfrom, USE AS REQUIRED, THICKNESS 4.2 MM
used on 001A, 001B, 001C, 001D, 001E
08 - 274A D5237179921400 . WASHER-SPACER VFAPE3 AR
selfrom, USE AS REQUIRED, THICKNESS 4.4 MM
used on 001A, 001B, 001C, 001D, 001E
08 - 275A D5237179921600 . WASHER-SPACER VFAPE3 AR
selfrom, USE AS REQUIRED, THICKNESS 4.6 MM
used on 001A, 001B, 001C, 001D, 001E
08 - 276A D5237179921800 . WASHER-SPACER VFAPE3 AR
selfrom, USE AS REQUIRED, THICKNESS 4.8 MM
used on 001A, 001B, 001C, 001D, 001E
08 - 277A D5237179922200 . WASHER-SPACER VFAPE3 AR
selfrom, USE AS REQUIRED, THICKNESS 5.4 MM
used on 001A, 001B, 001C, 001D, 001E
08 350A MS15001-1 . FITTING-LUBRICATION V96906 001
AS15001-1 81343
AS15001-1P 81343
Optional Vendor Code 0FKM1, 13899, 52930, 57336,
59736
used on 001A, 001B, 001C, 001D, 001E
08 360A D5237179520000 . SHAFT VFAPE3 001
used on 001A, 001B, 001C, 001D, 001E
08 370A D5237178500000 . LEVER ASSY-ROLLER VFAPE3 001
used on 001A, 001B, 001C
08 370B D5237178500200 . LEVER ASSY-ROLLER VFAPE3 001
used on 001A, 001B, 001C, 001D, 001E
08 380A D5237178420000 .. LEVER-ROLLER VFAPE3 001
used on 370A, 370B
08 390A D5237178320000 .. BUSHING-SHOULDERED VFAPE3 002
used on 370A, 370B
- ITEM NOT ILLUSTRATED

Page 10008-4
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
08 400A D5237178620000 .. ROLLER VFAPE3 001
used on 370A, 370B
08 410A NAS1291C3M .. NUT V80205 001
OPT TO H42-3 15653
Optional Vendor Code 15653, 27238, 52828, F0224
used on 370A
08 410B NSA5059E3 .. NUT VF6198 001
OPT TO 73783CM8-328 56878
Optional Vendor Code 04795, 15653, 2N935, C5543,
F0224, FAWT4
used on 370B
08 420A NAS1149C0332R .. WASHER V80205 001
Optional Vendor Code 10630, 58009, 65029, 8K160
used on 370A, 370B
08 430A NSA5042C04-150 .. BOLT VF6198 001
Optional Vendor Code 04795, 2N935, C4293, C5543,
C8431, F0095, F7411, FAWT4, K5673, K8753
used on 370A, 370B
08 440A NAS428C3A7 . BOLT V80205 001
OPT TO D5237164820000 FAPE3
Optional Vendor Code 1ER65, 62384
used on 001A, 001B, 001C, 001D, 001E
08 450A NSA5042C04-185 . BOLT VF6198 001
Optional Vendor Code 04795, 2N935, C4293, C5543,
C8431, F0095, F7411, FAWT4, K5673, K8753
used on 001A, 001B, 001C, 001D, 001E
08 460A D5237178920200 . BOLT-SPRING VFAPE3 001
used on 001A, 001B, 001C, 001D, 001E
08 470A D5237178820200 . SPRING-COMPRESSION VFAPE3 001
used on 001A, 001B, 001C, 001D, 001E
08 480A A5217236820000 . SHEET VFAPE3 001
used on 001A, 001B, 001C, 001D, 001E
08 490A D5237176320000 . HOOK-CATCHING VFAPE3 001
used on 001A, 001B, 001C, 001D, 001E
08 500A NAS6703-4 . BOLT V80205 002
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, 1RC86,
5M902, 62384, 8K160, 8Z507, F7411, FAWT4, K5673,
K8753
used on 001A, 001B, 001C, 001D, 001E
08 510A D5237179000400 . JOINT ASSY-UNIVERSAL VFAPE3 001
used on 001A, 001D
- ITEM NOT ILLUSTRATED

Page 10008-5
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
08 510B D5237179000400 . JOINT ASSY-UNIVERSAL VFAPE3 001
used on 001B, 001D
08 510C D5237179000400 . JOINT ASSY-UNIVERSAL VFAPE3 001
used on 001C, 001D
08 510D D5237179000200 . JOINT ASSY-UNIVERSAL VFAPE3 001
used on 001D
08 510E D5237179000600 . JOINT ASSY-UNIVERSAL VFAPE3 001
used on 001E
08 520A D5237179220200 .. LATCH-UNIVERSAL JOINT VFAPE3 001
used on 510A
08 520B D5237179220000 .. LATCH-UNIVERSAL JOINT VFAPE3 001
used on 510D
08 520C D5237179220400 .. LATCH-UNIVERSAL JOINT VFAPE3 001
used on 510E
08 530A D5237178320000 .. BUSHING-SHOULDERED VFAPE3 002
used on 510A, 510B, 510C, 510D, 510E
08 540A MS24665-153 .. PIN-COTTER V96906 001
Optional Vendor Code 04795, 06329, 2N935, 60996,
84114, 8K160, C5543
used on 510A, 510B, 510C, 510D, 510E
08 550A NSA5059C4 .. NUT VF6198 001
OPT TO TE9925-4 72962
OPT TO THCR54 F0224
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 510A, 510B, 510C, 510D
08 550B NSA5059E4 .. NUT VF6198 001
OPT TO 73783CM8-428 56878
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 510E
08 560A NAS1149C0463R .. WASHER V80205 001
Optional Vendor Code 10630, 1ER65, 58009, 65029,
8K160
used on 510A, 510B, 510C, 510D, 510E
08 570A NAS1149C0432R .. WASHER V80205 001
Optional Vendor Code 10630, 1ER65, 58009, 65029,
8K160
used on 510A, 510B, 510C, 510D, 510E
08 580A NSA5031-4D11 .. BOLT VF6198 001
Optional Vendor Code 04795, 2N935, C4293, C5543,
FAWT4, K8753, T0802
- ITEM NOT ILLUSTRATED

Page 10008-6
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 510A, 510B, 510C, 510D, 510E
08 590A MS14103-4K .. BEARING V96906 001
Optional Vendor Code 09455, 15860, F0222, S0352
used on 510A, 510B, 510C
08 590B MS14102-4K .. BEARING V96906 001
Optional Vendor Code 15860, S0352
used on 510D, 510E
08 600A D5237176720200 .. ROD ASSY VFAPE3 001
OPT TO B322104-012 F0222
OPT TO R24358 B1395
used on 510A, 510D, 510E
08 600B R24358 .. ROD ASSY VB1395 001
OPT TO D5237176720000 FAPE3
OPT TO D5237176720200 FAPE3
OPT TO D5237176720400 FAPE3
used on 510B
SEE 52-32-17-950 FOR DET
08 600C B322104-012 .. ROD ASSY VF0222 001
OPT TO D5237176720200 FAPE3
used on 510C
- ITEM NOT ILLUSTRATED

Page 10008-7
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

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_523217_09_0_01_00

LEVER ASSY-HAND
Figure 09 / FIGURE-52-32-17-950-809-01

Page 10009-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
09 - 001A D5237177000200 LEVER ASSY-HAND VFAPE3 RF
used on 010A (523217080)
SEE 52-32-17-080 FOR NHA
09 010A D5237331120000 . 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
Optional Vendor Code 04795, C5543, C5729, F7756
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
Optional Vendor Code 04795, 06329, 60996, 84114,
8K160, C5543, C5729
used on 001A
09 130A NAS1149C0363R . WASHER V80205 002
Optional Vendor Code 04795, 06329, 60996, 70347,
8K160, C5543, C5729
used on 001A
09 140A D5237177520200 . BOLT-BEARING VFAPE3 001
used on 001A
09 150A NAS1149C0332R . WASHER V80205 008
Optional Vendor Code 04795, 5N982, 60996, 8K160,
C5543, C5729
used on 001A
- ITEM NOT ILLUSTRATED

Page 10009-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

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
Optional Vendor Code 04795, C5543, C5729, D1283,
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
- ITEM NOT ILLUSTRATED

Page 10009-2
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

A 10

20

50
60 40
70

200
210
230
240
A 250 30
270

220
230
240 200
250 210

260

200
230 210
240
250

90 190
100 300
110
50 40 120 130
180 150
60 290 190
70 300 180 140
290

10 230
20 240
250 160
220

200
210 170
280 170
280

30
80

F_PL_523217_13_0_01_00

ROD-ADJUSTABLE AND DRIFT PIN

Figure 13 / FIGURE-52-32-17-950-813-01

Page 10013-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
13 - 001A D5237330000062 ROD-ADJUSTABLE AND DRIFT PIN VFAPE3 RF
used on 020A (523217050)
SEE 52-32-17-050 FOR NHA
13 - 001B D5237330000069 ROD-ADJUSTABLE AND DRIFT PIN VFAPE3 RF
used on 023A (523217050)
SEE 52-32-17-050 FOR NHA
13 - 001C D5237330000070 ROD-ADJUSTABLE AND DRIFT PIN VFAPE3 RF
used on 025A (523217050)
SEE 52-32-17-050 FOR NHA
13 - 001D D5237330000062 ROD-ADJUSTABLE AND DRIFT PIN VFAPE3 RF
used on 020B (523217050)
SEE 52-32-17-050 FOR NHA
13 010A D5237157120200 . PIN-DRIFT VFAPE3 002
used on 001A, 001B, 001C, 001D
13 020A NAS1303-11D . BOLT V80205 002
NAS6603D11 80205
Optional Vendor Code F0188, F7411, K8753
used on 001A, 001B, 001C, 001D
13 030A D5237156420000 . WASHER VFAPE3 002
used on 001A, 001B, 001C, 001D
13 040A D5237151620000 . BUSHING VFAPE3 002
used on 001A, 001B, 001C, 001D
13 050A NSA5059C3 . NUT VF5442 002
OPT TO H53173-3 15653
OPT TO TE9925-3 72962
OPT TO THCR53 F0224
Optional Vendor Code 04795, C5543, C5729, F0188
used on 001A
13 050B NSA5059E3 . NUT VF5442 002
OPT TO 73783CM8-328 56878
Optional Vendor Code 04795, C5543, C5729, F0188,
F2094
used on 001D
13 060A NAS1149C0332R . WASHER V80205 002
Optional Vendor Code 04795, 5N982, 60996, 8K160,
C5543, C5729
used on 001A, 001B, 001C, 001D
13 070A MS24665-88 . PIN-COTTER V96906 002
Optional Vendor Code 04795, 06329, 60996, 84114,
8K160, C5543, C5729
used on 001A, 001B, 001C, 001D
- ITEM NOT ILLUSTRATED

Page 10013-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
13 080A D5237332220000 . ROD-FIXED VFAPE3 001
used on 001A, 001D
13 080B R25257 . ROD ASSY VB1395 001
used on 001B
SEE 52-32-17-950 FOR DET
13 080C B318217-022 . ROD ASSY VF0222 001
used on 001C
13 090A D5237331800000 . BELLCRANK ASSY VFAPE3 001
used on 001A
13 090B D5237331800200 . BELLCRANK ASSY VFAPE3 001
used on 001D
13 100A D5237331700000 .. LEVER ASSY-LINK VFAPE3 001
used on 090A, 090B
13 110A D5237331720000 ... LEVER-LINK VFAPE3 001
used on 100A
13 120A MS14102-4K ... BEARING V96906 002
Optional Vendor Code 04795, C5543, C5729, C7239,
K5269, S0352
used on 100A
13 130A D5237331600000 .. LEVER ASSY-LINK VFAPE3 001
used on 090A
13 130B D5237331600200 .. LEVER-LINK VFAPE3 001
used on 090A, 090B
13 140A D5237331620000 ... LEVER-LINK VFAPE3 001
used on 130A
13 140B D5237331620200 ... LEVER-LINK VFAPE3 001
used on 130A, 130B
13 150A MS14102-4K ... BEARING V96906 001
Optional Vendor Code 04795, C5543, C5729, C7239,
K5269, S0352
used on 130A, 130B
13 160A D5237103220000 .. SHAFT-BEAM 3 VFAPE3 001
used on 090A, 090B
13 170A AN386-2-8A .. PIN-TAPER V88044 002
Optional Vendor Code 04795
used on 090A
13 180A D5237180220000 .. SLEEVE VFAPE3 002
used on 090A
13 190A NAS1291C3M .. NUT V80205 002
OPT TO H42-3 15653
Optional Vendor Code 04795, 60119, C5543, C5729,
F0224
- ITEM NOT ILLUSTRATED

Page 10013-2
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 090A
13 200A NSA5031-4D11 . BOLT VF5442 004
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001A, 001B, 001C, 001D
13 210A NAS1149C0432R . WASHER V80205 004
Optional Vendor Code 04795, 60996, 8K160, C5543,
C5729
used on 001A, 001B, 001C, 001D
13 220A NAS1149C0632R . WASHER V80205 002
Optional Vendor Code 04795, 60996, 8K160, C5543,
C5729
used on 001A, 001B, 001C, 001D
13 230A NSA5059C4 . NUT VF5442 004
OPT TO TE9925-4 72962
OPT TO THCR54 F0224
Optional Vendor Code 04795, C5543, C5729, F0188
used on 001A
13 230B NSA5059E4 . NUT VF5442 004
OPT TO 73783CM8-428 56878
Optional Vendor Code 04795, 92215, C5543, C5729,
F0188
used on 001D
13 240A NAS1149C0463R . WASHER V80205 004
Optional Vendor Code 04795, 60996, 8K160, C5543,
C5729
used on 001A, 001B, 001C, 001D
13 250A MS24665-151 . PIN-COTTER V96906 004
Optional Vendor Code 04795, 06329, 60996, 84114,
8K160, C5543, C5729
used on 001A, 001B, 001C, 001D
13 260A D5237332320000 . ROD-ADJUSTABLE VFAPE3 001
used on 001A, 001D
13 260B R25258 . ROD ASSY VB1395 001
used on 001B
SEE 52-32-17-950 FOR DET
13 260C B318217-023 . ROD ASSY VF0222 001
used on 001C
13 270A D5237305720000 . ROD VFAPE3 001
used on 001A, 001D
- ITEM NOT ILLUSTRATED

Page 10013-3
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
13 270B R25259 . ROD ASSY VB1395 001
used on 001B
SEE 52-32-17-950 FOR DET
13 280A AN386-2-8A . PIN-TAPER V88044 002
Optional Vendor Code 04795
used on 001D
13 290A D5237180220000 . SLEEVE VFAPE3 002
used on 001D
13 300A NAS1291C3M . NUT V80205 002
OPT TO H42-3 15653
Optional Vendor Code 04795, 60119, C5543, C5729,
F0224
used on 001D
- ITEM NOT ILLUSTRATED

Page 10013-4
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

A
250
B

260
270
280

240
10

A
B
120 100 20
290 30
105 107
70
80

30
40
50
60

130
110 300
120
290 140 30
130 310 40
90 105 50
100 300140
107 310

70
30 80
40
50
150
70
80
30 30
40 70 210 40 210
50 80 310 50 310
200 200
300 300

230
187
180
185 190
290
190
290
227 225
160
170 220

F_PL_523217_20_0_01_00

DOOR ASSY-VENT
Figure 20 / FIGURE-52-32-17-950-820-01

Page 10020-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
20 - 001A D5237330000063 DOOR ASSY-VENT VFAPE3 RF
used on 030A (523217050)
SEE 52-32-17-050 FOR NHA
20 - 001B D5237330000071 DOOR ASSY-VENT VFAPE3 RF
used on 033A (523217050)
SEE 52-32-17-050 FOR NHA
20 - 001C D5237330000072 DOOR ASSY-VENT VFAPE3 RF
used on 035A (523217050)
SEE 52-32-17-050 FOR NHA
20 - 001D D5237330000063 DOOR ASSY-VENT VFAPE3 RF
used on 030B (523217050)
SEE 52-32-17-050 FOR NHA
20 010A D5237335000060 . DOOR ASSY-VENT VFAPE3 001
used on 001A
SEE 52-32-17-210 FOR DET
20 010B D5237335000060 . DOOR ASSY-VENT VFAPE3 001
used on 001D
SEE 52-32-17-210 FOR DET
20 020A NSA5031-4D16 . BOLT VF5442 001
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001A, 001B, 001C, 001D
20 030A NAS1149C0463R . WASHER V80205 006
Optional Vendor Code 04795, 60996, 8K160, C5543,
C5729
used on 001A, 001B, 001C, 001D
20 040A MS24665-151 . PIN-COTTER V96906 005
Optional Vendor Code 04795, 06329, 60996, 84114,
8K160, C5543, C5729
used on 001A, 001B, 001C, 001D
20 050A NSA5059C4 . NUT VF5442 005
OPT TO TE9925-4 72962
OPT TO THCR54 F0224
Optional Vendor Code 04795, C5543, C5729, F0188
used on 001A
20 050B NSA5059E4 . NUT VF5442 005
OPT TO 73783CM8-428 56878
Optional Vendor Code 04795, 92215, C5543, C5729,
F0188
used on 001D
20 060A D5237333120000 . ROD-ADJUSTABLE VFAPE3 001
used on 001A, 001D
- ITEM NOT ILLUSTRATED

Page 10020-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
20 060B R25261 . ROD ASSY VB1395 001
used on 001B
SEE 52-32-17-950 FOR DET
20 060C B318217-031 . ROD ASSY VF0222 001
used on 001C
20 070A NAS1149C0432R . WASHER V80205 004
Optional Vendor Code 04795, 60996, 8K160, C5543,
C5729
used on 001A, 001B, 001C, 001D
20 080A NSA5031-4D11 . BOLT VF5442 004
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001A, 001B, 001C, 001D
20 090A D5237334000000 . BELLCRANK ASSY VFAPE3 001
used on 001A
20 090B D5237334000200 . BELLCRANK ASSY VFAPE3 001
used on 001D
20 100A D5237331200000 .. LEVER ASSY-LINK VFAPE3 002
used on 090A, 090B
20 105A D5237331220000 ... LEVER-LINK VFAPE3 001
used on 100A
20 107A MS14102-4K ... BEARING V96906 001
Optional Vendor Code 04795, C5543, C5729, C7239,
K5269, S0352
used on 100A
20 110A D5237103220600 .. SHAFT-BEAM 3 VFAPE3 001
used on 090A, 090B
20 120A AN386-2-8A .. PIN-TAPER V88044 002
Optional Vendor Code 04795
used on 090A
20 130A D5237180220000 .. SLEEVE VFAPE3 002
used on 090A
20 140A NAS1291C3M .. NUT V80205 002
OPT TO H42-3 15653
Optional Vendor Code 04795, 60119, C5543, C5729,
F0224
used on 090A
20 150A D5237333020000 . ROD-FIXED VFAPE3 001
used on 001A, 001D
20 150B R25260 . ROD ASSY VB1395 001
used on 001B
SEE 52-32-17-950 FOR DET
- ITEM NOT ILLUSTRATED

Page 10020-2
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
20 150C B318217-030 . ROD ASSY VF0222 001
used on 001C
20 160A D5237331400000 . BELLCRANK ASSY VFAPE3 001
used on 001A
20 160B D5237331400200 . BELLCRANK ASSY VFAPE3 001
used on 001D
20 170A D5237103220800 .. SHAFT-BEAM 3 VFAPE3 001
used on 160A, 160B
20 180A D5237331200000 .. LEVER ASSY-LINK VFAPE3 001
used on 160A, 160B
20 185A D5237331220000 ... LEVER-LINK VFAPE3 001
used on 180A
20 187A MS14102-4K ... BEARING V96906 001
Optional Vendor Code 04795, C5543, C5729, C7239,
K5269, S0352
used on 180A
20 190A AN386-2-8A .. PIN-TAPER V88044 002
Optional Vendor Code 04795
used on 160A
20 200A D5237180220000 .. SLEEVE VFAPE3 002
used on 160A
20 210A NAS1291C3M .. NUT V80205 002
OPT TO H42-3 15653
Optional Vendor Code 04795, 60119, C5543, C5729,
F0224
used on 160A
20 220A D5237331300000 .. LEVER ASSY-LINK VFAPE3 001
used on 160A, 160B
20 225A D5237331320000 ... LEVER-LINK VFAPE3 001
used on 220A
20 227A MS14102-4K ... BEARING V96906 002
Optional Vendor Code 04795, C5543, C5729, C7239,
K5269, S0352
used on 220A
20 230A D5237331520000 . BUSH VFAPE3 001
used on 001A, 001B, 001C, 001D
20 240A D5237166120200 . COVER VFAPE3 001
used on 001A, 001B, 001C, 001D
20 250A NAS1100E3-8 . SCREW V80205 004
Optional Vendor Code 1ER65, 8Z507, F0188, F7411,
K8753
used on 001A, 001B, 001C, 001D
- ITEM NOT ILLUSTRATED

Page 10020-3
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
20 260A NAS1149C0332R . WASHER V80205 004
Optional Vendor Code 04795, 5N982, 60996, 8K160,
C5543, C5729
used on 001A, 001B, 001C, 001D
20 270A NAS1291C3M . NUT V80205 004
OPT TO H42-3 15653
Optional Vendor Code 04795, 60119, C5543, C5729,
F0224
used on 001A, 001B, 001C, 001D
20 280A D2587115820000 . SPACER VFAPE3 004
used on 001A, 001B, 001C, 001D
20 290A AN386-2-8A . PIN-TAPER V88044 004
Optional Vendor Code 04795
used on 001D
20 300A D5237180220000 . SLEEVE VFAPE3 004
used on 001D
20 310A NAS1291C3M . NUT V80205 004
OPT TO H42-3 15653
Optional Vendor Code 04795, 60119, C5543, C5729,
F0224
used on 001D
- ITEM NOT ILLUSTRATED

Page 10020-4
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

A
170 130 430

410
420

140

330
340 350
380
30 160
110 400
370
100 150
160
140 320
360

310

370
270
320 300
390

60

150
160 210
90
10 220 230
10 20 280 260
20 30
390
30 290
40
250
50
240
120 60 180
150
30 160
40 250
190
200 70 160
80 400
F_PL_523217_21_0_01_00

DOOR ASSY-VENT
Figure 21 / FIGURE-52-32-17-950-821-01

Page 10021-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
21 - 001A D5237335000060 DOOR ASSY-VENT VFAPE3 RF
used on 010A (523217200)
SEE 52-32-17-200 FOR NHA
21 - 001B D5237335000060 DOOR ASSY-VENT VFAPE3 RF
used on 010B (523217200)
SEE 52-32-17-200 FOR NHA
21 010A MS24665-300 . PIN-COTTER V96906 002
Optional Vendor Code 04795, 06329, 60996, 84114,
8K160, C5543, C5729
used on 001A, 001B
21 020A NSA5059C6 . NUT VF5442 002
OPT TO TE9925-6 72962
OPT TO THCR56 F0224
Optional Vendor Code 04795, C5543, C5729, F0188
used on 001A
21 020B NSA5059E6 . NUT VF5442 002
OPT TO 73783CM8-624 56878
Optional Vendor Code 04795, 92215, C5543, C5729,
F0188
used on 001B
21 030A NAS1149C0632R . WASHER V80205 004
Optional Vendor Code 04795, 60996, 8K160, C5543,
C5729
used on 001A, 001B
21 - 031A NAS1149C0632R . WASHER V80205 AR
USE AS REQUIRED
Optional Vendor Code 04795, 60996, 8K160, C5543,
C5729
used on 001A, 001B
21 040A NAS1149C0616R . WASHER V80205 AR
USE AS REQUIRED
Optional Vendor Code 04795, 60996, 8K160, C5543,
C5729
used on 001A, 001B
21 050A D5237166620100 . SPRING VFAPE3 001
used on 001A, 001B
21 060A D5237166320200 . SLEEVE VFAPE3 002
used on 001A, 001B
21 070A NAS1149C0463R . WASHER V80205 001
Optional Vendor Code 04795, 60996, 8K160, C5543,
C5729
used on 001A, 001B
- ITEM NOT ILLUSTRATED

Page 10021-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
21 080A NSA5031-4D16 . BOLT VF5442 001
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001A, 001B
21 090A D5237166620000 . SPRING VFAPE3 001
used on 001A, 001B
21 100A D5237166320400 . SLEEVE VFAPE3 001
used on 001A, 001B
21 110A NSA5031-6D38 . BOLT VF5442 001
Optional Vendor Code 04795, C5543, D1283, F0188,
F6167, F7411, K5673, K8753
used on 001A, 001B
21 120A D5237335000000 . DOOR ASSY-VENT VFAPE3 001
used on 001A, 001B
21 130A D5237334920000 .. DOOR-VENT VFAPE3 001
used on 120A
21 140A NSA5030-4-27 .. SCREW VF5442 004
ASNA2001V4-27 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 120A
21 150A NAS1291C4M .. NUT V80205 006
OPT TO 180003-5 60119
OPT TO PLH504M F0224
Optional Vendor Code 04795, C5543, C5729
used on 120A
21 160A NAS1149C0463R .. WASHER V80205 010
Optional Vendor Code 04795, 60996, 8K160, C5543,
C5729
used on 120A
21 170A NSA5030-4-26 .. SCREW VF5442 002
ASNA2001V4-26 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 120A
21 180A D5237334600000 .. ARM ASSY-ACTUATOR VFAPE3 001
used on 120A
21 190A D5237165620200 ... BUSHING VFAPE3 001
used on 180A
21 200A D5237165420200 ... BUSHING-SHOULDERED VFAPE3 001
used on 180A
- ITEM NOT ILLUSTRATED

Page 10021-2
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
21 210A NAS428C3A7 ... BOLT V80205 001
OPT TO D5237164820000 FAPE3
Optional Vendor Code 04795, C5543, C5729
used on 180A
21 220A MS35650-304 ... NUT V96906 001
Optional Vendor Code 04795, 06329, 1V757, 57983,
69289, C5543, C5729
used on 180A
21 230A SP108D ... WASHER-TAB VK7766 001
Optional Vendor Code 04795, C5543, C5729, K4975
used on 180A
21 240A D5237334720000 ... ARM-ACTUATOR VFAPE3 001
used on 180A
21 250A D5237165320000 ... BUSHING-SHOULDERED VFAPE3 002
used on 180A
21 260A MS21209F1-20 ... INSERT V96906 001
Optional Vendor Code 04795, 06329, 60996, 8K160,
C4293, C5543, C5729, K6405
used on 180A
21 270A D5237334400000 .. BRACKET ASSY VFAPE3 001
used on 120A
21 280A D5237164220000 ... BUSHING-SHOULDERED VFAPE3 001
used on 270A
21 290A D5237164320000 ... BUSHING VFAPE3 001
used on 270A
21 300A D5237334320000 ... BRACKET VFAPE3 001
used on 270A
21 310A D5237334800000 .. ARM ASSY-ACTUATOR VFAPE3 001
used on 120A
21 320A D5237165620200 ... BUSHING VFAPE3 002
used on 310A
21 330A NAS428C3A7 ... BOLT V80205 001
OPT TO D5237164820000 FAPE3
Optional Vendor Code 04795, C5543, C5729
used on 310A
21 340A MS35650-304 ... NUT V96906 001
Optional Vendor Code 04795, 06329, 1V757, 57983,
69289, C5543, C5729
used on 310A
21 350A SP108D ... WASHER-TAB VK7766 001
Optional Vendor Code 04795, C5543, C5729, K4975
used on 310A
- ITEM NOT ILLUSTRATED

Page 10021-3
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
21 360A D5237334720000 ... ARM-ACTUATOR VFAPE3 001
used on 310A
21 370A D5237165320000 ... BUSHING-SHOULDERED VFAPE3 002
used on 310A
21 380A MS21209F1-20 ... INSERT V96906 001
Optional Vendor Code 04795, 06329, 60996, 8K160,
C4293, C5543, C5729, K6405
used on 310A
21 390A D5237165220200 .. BOLT-SPRING VFAPE3 002
used on 120A
21 400A MS24665-86 .. PIN-COTTER V96906 002
Optional Vendor Code 04795, 06329, 60996, 84114,
8K160, C5543, C5729
used on 120A
21 410A D5237163920200 .. SEAL-PRESSURE RELIEF FLAP VFAPE3 001
used on 120A
21 420A D5237163820600 .. RETAINER VFAPE3 001
used on 120A
21 430A D5237163820700 .. RETAINER VFAPE3 001
used on 120A
21 - 440A NAS1097KE4-00 .. RIVET V80205 AR
USE AS REQUIRED
EN6069KE4 I9005
used on 120A
- ITEM NOT ILLUSTRATED

Page 10021-4
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

40
10
B A TO C
A
A
170
C 180
190
240
270 140
280 150
260

200
C 230
AB 290 210

240
250
220 B

220 B 110
160
120
80 B
170
90 B

130
140 AC 90
100

50
20 AC 60 AC
50 30 B 70
60 B
70

80 AC
F_PL_523217_30_0_01_00

MECHANISM ASSY-LATCHING
Figure 30 / FIGURE-52-32-17-950-830-01

Page 10030-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
30 - 001A D5237330000064 MECHANISM ASSY-LATCHING VFAPE3 RF
used on 040A (523217050)
SEE 52-32-17-050 FOR NHA
30 - 001B D5237330000064 MECHANISM ASSY-LATCHING VFAPE3 RF
used on 040B (523217050)
SEE 52-32-17-050 FOR NHA
30 - 001C D5237330000075 MECHANISM ASSY-LATCHING VFAPE3 RF
used on 043A (523217050)
SEE 52-32-17-050 FOR NHA
30 - 001D D5237330000076 MECHANISM ASSY-LATCHING VFAPE3 RF
used on 045A (523217050)
SEE 52-32-17-050 FOR NHA
30 - 001E D5237330000664 MECHANISM ASSY-LATCHING VFAPE3 RF
used on 040C (523217050)
SEE 52-32-17-050 FOR NHA
30 010A D5237330200000 . SHAFT ASSY-LOCKING VFAPE3 001
used on 001A
SEE 52-32-17-310 FOR DET
30 010B D5237330000260 . SHAFT ASSY-LOCKING VFAPE3 001
used on 001B
SEE 52-32-17-31A FOR DET
30 010C D5237330000660 . SHAFT ASSY-LOCKING VFAPE3 001
used on 001E
SEE 52-32-17-31B FOR DET
30 020A D5237149000000 . LATCHING MECHANISM ASSY VFAPE3 003
used on 001A, 001B, 001C, 001D, 001E
SEE 52-32-17-330 FOR DET
30 - 023A D5237149000062 . MECHANISM ASSY-LATCHING VFAPE3 001
used on 001A, 001B, 001C, 001D, 001E
SEE 52-32-17-330 FOR DET
30 - 025A D5237149000063 . MECHANISM ASSY-LATCHING VFAPE3 001
used on 001A, 001B, 001C, 001D, 001E
SEE 52-32-17-330 FOR DET
30 030A D5237149000200 . LATCHING MECHANISM ASSY VFAPE3 001
used on 001A, 001B, 001C, 001D, 001E
SEE 52-32-17-340 FOR DET
30 040A D5237330500000 . SHAFT ASSY-LATCHING VFAPE3 001
used on 001A
SEE 52-32-17-320 FOR DET
30 040B D5237330500260 . SHAFT ASSY-LATCHING VFAPE3 001
used on 001B, 001E
SEE 52-32-17-32A FOR DET
- ITEM NOT ILLUSTRATED

Page 10030-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
30 050A MS24665-370 . PIN-COTTER V96906 004
Optional Vendor Code 65029, 73145, 84114
used on 001A, 001B, 001C, 001D, 001E
30 060A NSA5059C10 . NUT VF6198 004
OPT TO TE9925-10 72962
OPT TO THCR510 F0224
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 001A
30 060B NSA5059E10 . NUT VF6198 004
OPT TO 73783CM8-1018 56878
Optional Vendor Code 04795, 15653, 2N935, C5543,
F0224
used on 001B, 001E
30 070A NAS1149C1032R . WASHER V80205 004
Optional Vendor Code 10630, 1ER65, 58009, 65029,
8K160
used on 001A, 001B, 001C, 001D, 001E
30 080A D5237144120000 . BOLT VFAPE3 004
used on 001A, 001B, 001C, 001D, 001E
30 090A D5237140120000 . WASHER VFAPE3 004
used on 001A, 001B, 001C, 001D, 001E
30 100A D5237145220000 . BUSHING-SHOULDERED VFAPE3 004
used on 001A, 001B, 001C, 001D, 001E
30 110A D5237145220200 . BUSHING-SHOULDERED VFAPE3 004
used on 001A, 001B, 001C, 001D, 001E
30 120A D5237144220200 . SLEEVE VFAPE3 004
used on 001A, 001B, 001C, 001D, 001E
30 130A NAS6705U42 . BOLT V80205 004
Optional Vendor Code 06725, 0RFT4, 0ZC92, 1ER65,
1RC86, 62384, 8Z507, F7411, K8753
used on 001A, 001B, 001C, 001D, 001E
30 140A NAS1149C0532R . WASHER V80205 008
Optional Vendor Code 10630, 1ER65, 58009, 65029,
8K160
used on 001A, 001B, 001C, 001D, 001E
30 150A NAS1291C5M . NUT V80205 004
OPT TO H42-5 15653
OPT TO PLH55M F0224
OPT TO VN300D054 92215
Optional Vendor Code 15653, 27238, 52828, 60119,
F0224
- ITEM NOT ILLUSTRATED

Page 10030-2
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 001A, 001B, 001C, 001D, 001E
30 160A NSA5031-7D42 . BOLT VF6198 004
Optional Vendor Code 04795, 2N935, C4293, C5543,
FAWT4, K8753, T0802
used on 001A, 001B, 001C, 001D, 001E
30 170A NAS1149C0763R . WASHER V80205 008
OPT TO AN960C716 88044
Optional Vendor Code 10630, 1ER65, 58009, 65029,
8K160
used on 001A, 001B, 001C, 001D, 001E
30 180A MS24665-300 . PIN-COTTER V96906 004
Optional Vendor Code 58009, 65029, 73145, 84114,
8K160
used on 001A, 001B, 001C, 001D, 001E
30 190A NSA5059C7 . NUT VF6198 004
OPT TO TE9925-7 72962
OPT TO THCR57 F0224
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 001A
30 190B NSA5059E7 . NUT VF6198 004
OPT TO 73783CM8-720 56878
Optional Vendor Code 04795, 15653, 2N935, C5543,
F0224, FAWT4
used on 001B, 001E
30 200A D5237145120600 . BUSHING-SHOULDERED VFAPE3 004
used on 001A, 001B, 001C, 001D, 001E
30 210A D5237144420400 . SLEEVE VFAPE3 004
used on 001A, 001B, 001C, 001D, 001E
30 220A D5237140120400 . WASHER VFAPE3 002
used on 001A
30 220B F5237139820200 . WASHER VFAPE3 002
used on 001B, 001E
30 230A D5237144520200 . BOLT VFAPE3 001
used on 001A, 001B, 001C, 001D, 001E
30 240A NAS1149C0432R . WASHER V80205 008
Optional Vendor Code 10630, 1ER65, 58009, 65029,
8K160
used on 001A, 001B, 001C, 001D, 001E
30 250A D5237141320400 . BUSHING VFAPE3 004
used on 001A, 001B, 001C, 001D, 001E
- ITEM NOT ILLUSTRATED

Page 10030-3
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
30 260A D5237141420000 . BUSHING VFAPE3 004
used on 001A, 001B, 001C, 001D, 001E
30 270A MS24665-151 . PIN-COTTER V96906 004
Optional Vendor Code 10630, 65029, 73145, 84114,
8K160
used on 001A, 001B, 001C, 001D, 001E
30 280A NSA5059C4 . NUT VF6198 004
OPT TO TE9925-4 72962
OPT TO THCR54 F0224
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 001A
30 280B NSA5059E4 . NUT VF6198 004
OPT TO 73783CM8-428 56878
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 001B, 001E
30 290A NSA5031-4D16 . BOLT VF6198 003
Optional Vendor Code 04795, 2N935, C4293, C5543,
FAWT4, K8753, T0802
used on 001A, 001B, 001C, 001D, 001E
- ITEM NOT ILLUSTRATED

Page 10030-4
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

A
80
30
40

80
30 70
40
70
20

20

70
10
30
70 30 40
40
110 50
50
50
30
100 40
50
90 80
30
40
60

20
20

80
30 70
40

70

70

70

F_PL_523217_31_0_01_00

SHAFT ASSY-LOCKING
Figure 31 / FIGURE-52-32-17-950-831-01

Page 10031-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
31 - 001A D5237330200000 SHAFT ASSY-LOCKING VFAPE3 RF
used on 010A (523217300)
SEE 52-32-17-300 FOR NHA
31 010A D5237305220000 . SHAFT-LOCKING VFAPE3 001
used on 001A
31 020A AN386-1-10A . PIN-TAPER V88044 004
Optional Vendor Code 0H380, 60360
used on 001A
31 030A NAS1291C3M . NUT V80205 012
OPT TO H42-3 15653
Optional Vendor Code 15653, 27238, 52828, F0224
used on 001A
31 040A NAS1149C0332R . WASHER V80205 012
Optional Vendor Code 10630, 58009, 65029, 8K160
used on 001A
31 050A D5237167320000 . SLEEVE VFAPE3 004
used on 001A
31 060A D5237176920000 . LEVER VFAPE3 001
used on 001A
31 070A DAN15-6-18 . PIN-RIVET VD8518 008
OPT TO HL20PB6-18 73197
Optional Vendor Code 04795, 2N935, C4293, C5543,
K5673
used on 001A
31 080A D5237151221000 . CAM-LOCKING VFAPE3 004
used on 001A
31 090A D5237150300000 . LEVER ASSY-HINGED VFAPE3 001
used on 001A
31 100A D5237150320000 .. LEVER-HINGED VFAPE3 001
used on 090A
31 110A MS14102-4K .. BEARING V96906 001
Optional Vendor Code 15860, S0352
used on 090A
- ITEM NOT ILLUSTRATED

Page 10031-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

A
70
90
100

70
90 120
100

120
80

80

120

120 90
90 100
100 110
50
110
110
10 60
90
100 20
40
110 70
30
90
100

80
80

70
90 120
100

120

120

120

F_PL_523217_31_A_01_00

SHAFT ASSY-LOCKING
Figure 31A / FIGURE-52-32-17-950-831-A01

Page 10031A-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
31A - 001A D5237330000260 SHAFT ASSY-LOCKING VFAPE3 RF
used on 010B (523217300)
SEE 52-32-17-300 FOR NHA
31A 010A D5237330200200 . SHAFT ASSY-LOCKING VFAPE3 001
used on 001A
31A 020A D5237305220000 .. SHAFT-LOCKING VFAPE3 001
used on 010A
31A 030A D5237150300000 .. LEVER ASSY-HINGED VFAPE3 001
used on 010A
31A 040A D5237150320000 ... LEVER-HINGED VFAPE3 001
used on 030A
31A 050A MS14102-4K ... BEARING V96906 001
Optional Vendor Code 15860, S0352
used on 030A
31A 060A D5237176920000 .. LEVER VFAPE3 001
used on 010A
31A 070A D5237151221000 .. CAM-LOCKING VFAPE3 004
used on 010A
31A 080A AN386-1-10A . PIN-TAPER V88044 004
Optional Vendor Code 0H380, 60360
used on 001A
31A 090A NAS1291C3M . NUT V80205 012
OPT TO H42-3 15653
Optional Vendor Code 15653, 27238, 52828, F0224
used on 001A
31A 100A NAS1149C0332R . WASHER V80205 012
Optional Vendor Code 10630, 58009, 65029, 8K160
used on 001A
31A 110A D5237167320000 . SLEEVE VFAPE3 004
used on 001A
31A 120A DAN15-6-18 . PIN-RIVET VD8518 008
OPT TO HL20PB6-18 73197
Optional Vendor Code 04795, 2N935, C4293, C5543,
K5673
used on 001A
- ITEM NOT ILLUSTRATED

Page 10031A-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

A
70
130

10
20

70
130
120
120
80
80
90
100
120 90 110
120 100
110
50
60
40
30
70
110
110 130
90
100
80
80

70
130
120
120

120
120
A
F_PL_523217_31_B_01_00

SHAFT ASSY-LOCKING
Figure 31B / FIGURE-52-32-17-950-831-B01

Page 10031B-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
31B - 001A D5237330000660 SHAFT ASSY-LOCKING VFAPE3 RF
used on 010C (523217300)
SEE 52-32-17-300 FOR NHA
31B 010A D5237330200200 . SHAFT ASSY-LOCKING VFAPE3 001
used on 001A
31B 020A D5237305220000 .. SHAFT-LOCKING VFAPE3 001
used on 010A
31B 030A D5237150300000 .. LEVER ASSY-HINGED VFAPE3 001
used on 010A
31B 040A D5237150320000 ... LEVER-HINGED VFAPE3 001
used on 030A
31B 050A MS14102-4K ... BEARING V96906 001
Optional Vendor Code 15860, S0352
used on 030A
31B 060A D5237176920000 .. LEVER VFAPE3 001
used on 010A
31B 070A D5237152920200 .. CAM-LOCKING VFAPE3 004
used on 010A
31B 080A AN386-1-10A . PIN-TAPER V88044 004
Optional Vendor Code 0H380, 60360
used on 001A
31B 090A NAS1291C3M . NUT V80205 004
OPT TO H42-3 15653
Optional Vendor Code 15653, 27238, 52828, F0224
used on 001A
31B 100A NAS1149C0332R . WASHER V80205 004
Optional Vendor Code 10630, 58009, 65029, 8K160
used on 001A
31B 110A D5237167320000 . SLEEVE VFAPE3 004
used on 001A
31B 120A DAN15-6-18 . PIN-RIVET VD8518 008
OPT TO HL20PB6-18 73197
Optional Vendor Code 04795, 2N935, C4293, C5543,
K5673
used on 001A
31B 130A NAS1726C3PE . NUT V80205 008
Optional Vendor Code 15653, 27238, 66776, F0224
used on 001A
- ITEM NOT ILLUSTRATED

Page 10031B-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

A
A
100
50 40 110
120

50
40
30

30

70
30 80
40
40 30
50
30
50
30
90
40
50

30 10
70
40 60
50
20
40
50

30 40
50
40
50 30
30
40
70
50

40
50

30

40
50
F_PL_523217_32_0_01_00

SHAFT ASSY-LATCHING
Figure 32 / FIGURE-52-32-17-950-832-01

Page 10032-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
32 - 001A D5237330500000 SHAFT ASSY-LATCHING VFAPE3 RF
used on 040A (523217300)
SEE 52-32-17-300 FOR NHA
32 010A D5237305520000 . SHAFT-LATCHING VFAPE3 001
used on 001A
32 020A D5237150620200 . LEVER-SHAFT VFAPE3 001
used on 001A
32 030A AN386-2-13A . PIN-TAPER V88044 011
Optional Vendor Code 04795, 70347, C5543, C5729,
F0434
used on 001A
32 040A D5237180220000 . SLEEVE VFAPE3 012
used on 001A
32 050A NAS1291C3M . NUT V80205 012
OPT TO H42-3 15653
Optional Vendor Code 04795, 60119, C5543, C5729,
F0224
used on 001A
32 060A AN386-2-12A . PIN-TAPER V88044 001
Optional Vendor Code 04795, 70347, C5543, C5729,
F0434
used on 001A
32 070A D5237150620000 . LEVER-SHAFT VFAPE3 003
used on 001A
32 080A D5237141920400 . CAM-STOP VFAPE3 001
used on 001A
32 090A D5237143220200 . LEVER-SWITCH VFAPE3 001
used on 001A
32 100A D5237150500000 . LEVER ASSY-HINGED VFAPE3 001
used on 001A
32 110A D5237150520000 .. LEVER-HINGED VFAPE3 001
used on 100A
32 120A MS14102-4K .. BEARING V96906 001
Optional Vendor Code 04795, C5543, C5729, C7239,
K5269, S0352
used on 100A
- ITEM NOT ILLUSTRATED

Page 10032-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

A A
70
130 120
130 80

120

90

100 100

40
100 50
120
120 100
130
100
130
100
60
120
130

10

100 20
40
120 110
130
120 30
130

120
100 130

120
130 100
100

40 120
130

120
130

100

120
130
F_PL_523217_32_A_01_00

SHAFT ASSY-LATCHING
Figure 32A / FIGURE-52-32-17-950-832-A01

Page 10032A-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
32A - 001A D5237330500260 SHAFT ASSY-LATCHING VFAPE3 RF
used on 040B (523217300)
SEE 52-32-17-300 FOR NHA
32A 010A D5237330500200 . SHAFT ASSY-LATCHING VFAPE3 001
used on 001A
32A 020A D5237305520000 .. SHAFT-LATCHING VFAPE3 001
used on 010A
32A 030A D5237150620200 .. LEVER-SHAFT VFAPE3 001
used on 010A
32A 040A D5237150620000 .. LEVER-SHAFT VFAPE3 003
used on 010A
32A 050A D5237141920400 .. CAM-STOP VFAPE3 001
used on 010A
32A 060A D5237143220200 .. LEVER-SWITCH VFAPE3 001
used on 010A
32A 070A D5237150500000 .. LEVER ASSY-HINGED VFAPE3 001
used on 010A
32A 080A D5237150520000 ... LEVER-HINGED VFAPE3 001
used on 070A
32A 090A MS14102-4K ... BEARING V96906 001
Optional Vendor Code 04795, C5543, C5729, C7239,
K5269, S0352
used on 070A
32A 100A AN386-2-13A . PIN-TAPER V88044 011
Optional Vendor Code 04795, 70347, C5543, C5729,
F0434
used on 001A
32A 110A AN386-2-12A . PIN-TAPER V88044 001
Optional Vendor Code 04795, 70347, C5543, C5729,
F0434
used on 001A
32A 120A D5237180220000 . SLEEVE VFAPE3 012
used on 001A
32A 130A NAS1291C3M . NUT V80205 012
OPT TO H42-3 15653
Optional Vendor Code 04795, 60119, C5543, C5729,
F0224
used on 001A
- ITEM NOT ILLUSTRATED

Page 10032A-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

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_523217_33_0_01_00

LATCHING MECHANISM ASSY

Figure 33 / FIGURE-52-32-17-950-833-01

Page 10033-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
33 - 001A D5237149000000 LATCHING MECHANISM ASSY VFAPE3 RF
used on 020A (523217300)
SEE 52-32-17-300 FOR NHA
33 - 001B D5237149000062 MECHANISM ASSY-LATCHING VFAPE3 RF
used on 023A (523217300)
SEE 52-32-17-300 FOR NHA
33 - 001C D5237149000063 MECHANISM ASSY-LATCHING VFAPE3 RF
used on 025A (523217300)
SEE 52-32-17-300 FOR NHA
33 010A D5237143500000 . HOOK ASSY-LATCHING VFAPE3 001
used on 001A, 001B, 001C
33 020A D5237143620000 .. HOOK-LATCHING VFAPE3 001
used on 010A
33 030A MS15001-1 .. FITTING-LUBRICATION V96906 001
AS15001-1 81343
Optional Vendor Code 06329, 13899, 5N982, 60996,
8K160, C5543, C5729
used on 010A
33 040A D5237143820000 .. BUSHING-SHOULDERED VFAPE3 001
used on 010A
33 050A D5237143920000 .. BUSHING-SHOULDERED VFAPE3 002
used on 010A
33 060A D5237140320200 . SLEEVE VFAPE3 002
used on 001A, 001B, 001C
33 070A D5237185320000 . LINK-CONNECTING VFAPE3 001
used on 001A, 001B, 001C
33 080A D5237140420200 . BOLT VFAPE3 001
used on 001A, 001B, 001C
33 090A NAS1149C0732R . WASHER V80205 002
Optional Vendor Code 04795, 60996, 8K160, C5543,
C5729
used on 001A, 001B, 001C
33 100A D5237140920200 . BUSHING-SHOULDERED VFAPE3 002
used on 001A, 001B, 001C
33 110A D5237140920400 . BUSHING-SHOULDERED VFAPE3 002
used on 001A, 001B, 001C
33 120A NSA5059C5 . NUT VF5442 002
OPT TO TE9925-5 72962
OPT TO THCR55 F0224
Optional Vendor Code 04795, C5543, C5729, F0188
used on 001A, 001B, 001C
- ITEM NOT ILLUSTRATED

Page 10033-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
33 130A NAS1149C0532R . WASHER V80205 002
Optional Vendor Code 04795, 60996, 8K160, C5543,
C5729
used on 001A, 001B, 001C
33 140A MS24665-153 . PIN-COTTER V96906 003
Optional Vendor Code 04795, 06329, 60996, 84114,
8K160, C5543, C5729
used on 001A, 001B, 001C
33 150A D5237140420000 . BOLT VFAPE3 001
used on 001A, 001B, 001C
33 160A D5237185600000 . BELLCRANK ASSY VFAPE3 001
used on 001A, 001B, 001C
33 170A D5237185520000 .. BELLCRANK VFAPE3 001
used on 160A
33 180A D5237142320200 .. BUSHING VFAPE3 001
used on 160A
33 190A D5237143920000 .. BUSHING-SHOULDERED VFAPE3 002
used on 160A
33 200A MS15001-1 .. FITTING-LUBRICATION V96906 001
AS15001-1 81343
Optional Vendor Code 06329, 13899, 5N982, 60996,
8K160, C5543, C5729
used on 160A
33 210A NSA5031-4D16 . BOLT VF5442 001
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001A, 001B, 001C
33 220A NAS1149C0432R . WASHER V80205 002
Optional Vendor Code 04795, 60996, 8K160, C5543,
C5729
used on 001A, 001B, 001C
33 230A D5237141320400 . BUSHING VFAPE3 001
used on 001A, 001B, 001C
33 240A D5237141420000 . BUSHING VFAPE3 001
used on 001A, 001B, 001C
33 250A NSA5059C4 . NUT VF5442 001
OPT TO TE9925-4 72962
OPT TO THCR54 F0224
Optional Vendor Code 04795, C5543, C5729, F0188
used on 001A, 001B, 001C
- ITEM NOT ILLUSTRATED

Page 10033-2
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
33 260A D5237180120000 . ROD-CONNECTING VFAPE3 001
OPT TO B322104-013 F0222
OPT TO R24225 B1395
used on 001A
33 260B R24225 . ROD ASSY VB1395 001
OPT TO D5237180120000 FAPE3
used on 001B
33 260C B322104-013 . ROD ASSY VF0222 001
OPT TO D5237180120000 FAPE3
used on 001C
- ITEM NOT ILLUSTRATED

Page 10033-3
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

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_523217_34_0_01_00

LATCHING MECHANISM ASSY

Figure 34 / FIGURE-52-32-17-950-834-01

Page 10034-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
34 - 001A D5237149000200 LATCHING MECHANISM ASSY VFAPE3 RF
used on 030A (523217300)
SEE 52-32-17-300 FOR NHA
34 010A D5237143500000 . HOOK ASSY-LATCHING VFAPE3 001
used on 001A
34 020A D5237143620000 .. HOOK-LATCHING VFAPE3 001
used on 010A
34 030A MS15001-1 .. FITTING-LUBRICATION V96906 001
AS15001-1 81343
Optional Vendor Code 06329, 13899, 5N982, 60996,
8K160, C5543, C5729
used on 010A
34 040A D5237143820000 .. BUSHING-SHOULDERED VFAPE3 001
used on 010A
34 050A D5237143920000 .. BUSHING-SHOULDERED VFAPE3 002
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
Optional Vendor Code 04795, 60996, 8K160, C5543,
C5729
used on 001A
34 100A D5237140920200 . BUSHING-SHOULDERED VFAPE3 002
used on 001A
34 110A D5237140920400 . BUSHING-SHOULDERED VFAPE3 002
used on 001A
34 120A NSA5059C5 . NUT VF5442 002
OPT TO TE9925-5 72962
OPT TO THCR55 F0224
Optional Vendor Code 04795, C5543, C5729, F0188
used on 001A
34 130A NAS1149C0532R . WASHER V80205 002
Optional Vendor Code 04795, 60996, 8K160, C5543,
C5729
used on 001A
34 140A MS24665-153 . PIN-COTTER V96906 003
Optional Vendor Code 04795, 06329, 60996, 84114,
8K160, C5543, C5729
- ITEM NOT ILLUSTRATED

Page 10034-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 001A
34 150A D5237140420000 . BOLT VFAPE3 001
used on 001A
34 160A D5237185600000 . BELLCRANK ASSY VFAPE3 001
used on 001A
34 170A D5237185520000 .. BELLCRANK VFAPE3 001
used on 160A
34 180A D5237142320200 .. BUSHING VFAPE3 001
used on 160A
34 190A D5237143920000 .. BUSHING-SHOULDERED VFAPE3 002
used on 160A
34 200A MS15001-1 .. FITTING-LUBRICATION V96906 001
AS15001-1 81343
Optional Vendor Code 06329, 13899, 5N982, 60996,
8K160, C5543, C5729
used on 160A
34 210A NSA5031-4D16 . BOLT VF5442 001
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001A
34 220A NAS1149C0432R . WASHER V80205 002
Optional Vendor Code 04795, 60996, 8K160, C5543,
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
Optional Vendor Code 04795, C5543, C5729, F0188
used on 001A
34 260A D5237180120000 . ROD-CONNECTING VFAPE3 001
OPT TO B322104-013 F0222
OPT TO R24225 B1395
used on 001A
- ITEM NOT ILLUSTRATED

Page 10034-2
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

240
250

210
220
230
A

10

240
250

A 210
220
230
160

190 90 70
200 80
20 50
30
40
180

170

50

170
180
60 70
80
90

110
120
130 160
140
150

100
240
250

210
220
230

F_PL_523217_40_0_01_00

SHAFT-SEQUENCE
Figure 40 / FIGURE-52-32-17-950-840-01

Page 10040-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
40 - 001A D5237330000066 SHAFT-SEQUENCE VFAPE3 RF
used on 060A (523217050)
SEE 52-32-17-050 FOR NHA
40 - 001B D5237330000073 SHAFT-SEQUENCE VFAPE3 RF
used on 063A (523217050)
SEE 52-32-17-050 FOR NHA
40 - 001C D5237330000074 SHAFT-SEQUENCE VFAPE3 RF
used on 065A (523217050)
SEE 52-32-17-050 FOR NHA
40 - 001D D5237330000066 SHAFT-SEQUENCE VFAPE3 RF
used on 060B (523217050)
SEE 52-32-17-050 FOR NHA
40 - 001E D5237330000666 SHAFT-SEQUENCE VFAPE3 RF
used on 060C (523217050)
SEE 52-32-17-050 FOR NHA
40 010A D5237332120000 . ROD-FIXED VFAPE3 001
used on 001A, 001D, 001E
40 010B R25256 . ROD ASSY VB1395 001
used on 001B
SEE 52-32-17-950 FOR DET
40 010C B318217-021 . ROD ASSY VF0222 001
used on 001C
40 020A D5237333500000 . HOUSING ASSY-BELLCRANK VFAPE3 001
used on 001A
40 020B D5237333500000 . HOUSING ASSY-BELLCRANK VFAPE3 001
used on 001B
40 020C D5237333500000 . HOUSING ASSY-BELLCRANK VFAPE3 001
used on 001C
40 020D D5237333500200 . HOUSING ASSY-BELLCRANK VFAPE3 001
used on 001A, 001B, 001C, 001D, 001E
40 030A D5237294000000 .. COVER-BEAM 4 VFAPE3 001
used on 020A, 020B, 020C, 020D
40 040A D5237294020000 ... COVER VFAPE3 001
used on 030A
40 050A D5237162320000 ... BUSHING-SHOULDERED VFAPE3 002
used on 030A
40 060A D5237294120000 .. SHAFT-BEAM 4 VFAPE3 001
used on 020A, 020B, 020C, 020D
40 070A D5237294200000 .. LEVER VFAPE3 002
used on 020A, 020B, 020C, 020D
- ITEM NOT ILLUSTRATED

Page 10040-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
40 080A D5237294220000 ... LEVER VFAPE3 001
used on 070A
40 090A MS14102-4K ... BEARING V96906 001
Optional Vendor Code 15860, S0352
used on 070A
40 100A D5237332020000 .. ROD-FIXED VFAPE3 001
OPT TO 44910 B1395
OPT TO R25255 B1395
used on 020A
40 100B R25255 .. ROD ASSY VB1395 001
OPT TO D5237332020000 FAPE3
used on 020B
40 100C 44910 .. ROD END VB1395 001
OPT TO D5237332020000 FAPE3
used on 020C
40 100D D5237332020200 .. ROD-FIXED VFAPE3 001
OPT TO R26229 B1395
used on 020A, 020D
40 110A MS24665-151 .. PIN-COTTER V96906 001
Optional Vendor Code 10630, 65029, 73145, 84114,
8K160
used on 020A, 020B, 020C, 020D
40 120A NSA5059E4 .. NUT VF6198 001
OPT TO 73783CM8-428 56878
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 020A, 020B, 020C, 020D
40 130A NAS1149C0463R .. WASHER V80205 001
Optional Vendor Code 10630, 1ER65, 58009, 65029,
8K160
used on 020A, 020B, 020C, 020D
40 140A NSA5031-4D11 .. BOLT VF6198 001
Optional Vendor Code 04795, 2N935, C4293, C5543,
FAWT4, K8753, T0802
used on 020A, 020B, 020C, 020D
40 150A NAS1149C0432R .. WASHER V80205 001
Optional Vendor Code 10630, 1ER65, 58009, 65029,
8K160
used on 020A, 020B, 020C, 020D
40 160A AN386-2-8A .. PIN-TAPER V88044 002
Optional Vendor Code 0H380, 60360
used on 020A, 020B, 020C, 020D
- ITEM NOT ILLUSTRATED

Page 10040-2
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
40 170A NAS1291C3M .. NUT V80205 002
OPT TO H42-3 15653
Optional Vendor Code 15653, 27238, 52828, F0224
used on 020A, 020B, 020C, 020D
40 180A D5237180220000 .. SLEEVE VFAPE3 002
used on 020A, 020B, 020C, 020D
40 190A NSA5031-3-3 . BOLT VF6198 004
Optional Vendor Code 04795, 2N935, C4293, C5543,
F6167, F7411, FAWT4, T0802
used on 001A, 001B, 001C, 001D, 001E
40 200A NAS1149C0332R . WASHER V80205 004
Optional Vendor Code 10630, 58009, 65029, 8K160
used on 001A, 001B, 001C, 001D, 001E
40 210A NSA5059C4 . NUT VF6198 003
OPT TO TE9925-4 72962
OPT TO THCR54 F0224
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 001A
40 210B NSA5059E4 . NUT VF6198 003
OPT TO 73783CM8-428 56878
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 001D, 001E
40 220A NAS1149C0463R . WASHER V80205 003
Optional Vendor Code 10630, 1ER65, 58009, 65029,
8K160
used on 001A, 001B, 001C, 001D, 001E
40 230A MS24665-151 . PIN-COTTER V96906 003
Optional Vendor Code 10630, 65029, 73145, 84114,
8K160
used on 001A, 001B, 001C, 001D, 001E
40 240A NAS1149C0432R . WASHER V80205 003
Optional Vendor Code 10630, 1ER65, 58009, 65029,
8K160
used on 001A, 001B, 001C, 001D, 001E
40 250A NSA5031-4D11 . BOLT VF6198 003
Optional Vendor Code 04795, 2N935, C4293, C5543,
FAWT4, K8753, T0802
used on 001A, 001B, 001C, 001D, 001E
- ITEM NOT ILLUSTRATED

Page 10040-3
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
40 - 260A D52373300000CTD . SHAFT-SEQUENCE,CONTINUED VFAPE3 001
used on 001A, 001B, 001C
SEE 52-32-17-410 FOR DET
40 - 260B D52373300000CTD . SHAFT-SEQUENCE,CONTINUED VFAPE3 001
used on 001D
SEE 52-32-17-41A FOR DET
40 - 260C D5237330000671 . SHAFT-SEQUENCE,CONTINUED VFAPE3 001
used on 001E
SEE 52-32-17-41B FOR DET
- ITEM NOT ILLUSTRATED

Page 10040-4
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

390
400
290 410
A 290
300

300 280 420

430
335
310
290
300
240 330
250 280
260
360 460
370 440
20 380
450
320
335
340
320
270

210 270
180
200 170
30
40
130
150
230 220
140 460
350
150 190
390
400
10 410
120

420
430
70
160 390
400
40 410
50

60

90
100
110
80

F_PL_523217_41_0_01_00

SHAFT-SEQUENCE,CONTINUED
Figure 41 / FIGURE-52-32-17-950-841-01

Page 10041-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
41 - 001A D52373300000CTD SHAFT-SEQUENCE,CONTINUED VFAPE3 RF
used on 260A (523217400)
SEE 52-32-17-400 FOR NHA
41 010A D5237330600000 . LINK ASSY VFAPE3 001
used on 001A
41 020A D5237153120200 .. FORK VFAPE3 001
used on 010A
41 030A NAS509L3C .. NUT V80205 001
Optional Vendor Code 60119, 92595, F2094, FAWT4
used on 010A
41 040A SP108D .. WASHER-TAB VK4955 002
Optional Vendor Code 04795, 2N935, C5543, K4975
used on 010A
41 050A NAS509-3C .. NUT V80205 001
Optional Vendor Code 01673, 04795, 06329, 2N935,
60996, 8K160, 92595, C5543
used on 010A
41 060A D5237152620200 .. FORK VFAPE3 001
used on 010A
41 070A D5237153420200 .. SLEEVE VFAPE3 001
used on 010A
41 080A NSA5031-3D7 .. BOLT VF6198 001
Optional Vendor Code 04795, 2N935, C4293, C5543,
F6167, F7411, FAWT4, K5673, K8753, T0802
used on 010A
41 090A NAS1149C0332R .. WASHER V80205 001
Optional Vendor Code 10630, 58009, 65029, 8K160
used on 010A
41 100A NSA5059E3 .. NUT VF6198 001
OPT TO 73783CM8-328 56878
Optional Vendor Code 04795, 15653, 2N935, C5543,
F0224, FAWT4
used on 010A
41 110A MS24665-88 .. PIN-COTTER V96906 001
Optional Vendor Code 10630, 58009, 65029, 73145,
84114, 8K160
used on 010A
41 120A D5237152820000 .. ROD VFAPE3 001
used on 010A
41 130A D5237336800000 .. LEVER ASSY VFAPE3 001
used on 010A
- ITEM NOT ILLUSTRATED

Page 10041-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
41 140A D5237330720000 ... LEVER VFAPE3 001
used on 130A
41 150A D5237153720000 ... BUSHING-SHOULDERED VFAPE3 002
used on 130A
41 160A D5237153320000 ... BUSHING VFAPE3 001
used on 130A
41 170A D5237111920200 . SUPPORT-FITTING VFAPE3 001
used on 001A
41 180A 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, 06725, 17446, 2N935,
56878, 73197, C4293, C5543, K5673, U6300
used on 001A
41 190A NSA5075-5 . COLLAR VF6198 002
OPT TO DAN11-5 D8518
OPT TO F0N2-1181-5 H1822
OPT TO HL70AA5 92215
Optional Vendor Code 04795, 2N935, 56878, 5M902,
73197, 80539, C5543, U6300
used on 001A
41 200A D5237336000000 . SHAFT ASSY-SEQUENCE VFAPE3 001
used on 001A
41 210A D5237336120000 .. SHAFT-SEQUENCE VFAPE3 001
used on 200A
41 220A D5237336320000 .. LEVER VFAPE3 001
used on 200A
41 230A D5237153320000 .. BUSHING VFAPE3 001
used on 200A
41 240A D5237336200000 .. LEVER ASSY VFAPE3 001
used on 200A
41 250A D5237336220000 ... LEVER VFAPE3 001
used on 240A
41 260A MS14102-4K ... BEARING V96906 001
Optional Vendor Code 15860, S0352
used on 240A
41 270A AN386-1-10A .. PIN-TAPER V88044 004
Optional Vendor Code 0H380, 60360
used on 200A
41 280A D5237167320000 .. SLEEVE VFAPE3 004
used on 200A
- ITEM NOT ILLUSTRATED

Page 10041-2
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
41 290A NAS1149C0332R .. WASHER V80205 006
Optional Vendor Code 10630, 58009, 65029, 8K160
used on 200A
41 300A NAS1291C3M .. NUT V80205 006
OPT TO H42-3 15653
Optional Vendor Code 15653, 27238, 52828, F0224
used on 200A
41 310A D5237151220800 .. CAM-LOCKING VFAPE3 001
used on 200A
41 320A DAN15-6-18 .. PIN-RIVET VD8518 002
OPT TO HL20PB6-18 73197
Optional Vendor Code 04795, 2N935, C4293, C5543,
K5673
used on 200A
41 330A D5237176920000 .. LEVER VFAPE3 001
used on 200A
41 335A F5237139820200 . WASHER VFAPE3 002
used on 001A
41 340A NSA5031-3D7 . BOLT VF6198 001
Optional Vendor Code 04795, 2N935, C4293, C5543,
F6167, F7411, FAWT4, K5673, K8753, T0802
used on 001A
41 350A D5237153420200 . SLEEVE VFAPE3 001
used on 001A
41 360A NSA5059C3 . NUT VF6198 001
OPT TO H53173-3 15653
OPT TO TE9925-3 72962
OPT TO THCR53 F0224
Optional Vendor Code 04795, 15653, 2N935, 56878,
C4293, C5543, F0224, FAWT4
used on 001A
41 370A NAS1149C0332R . WASHER V80205 001
Optional Vendor Code 10630, 58009, 65029, 8K160
used on 001A
41 380A MS24665-88 . PIN-COTTER V96906 001
Optional Vendor Code 10630, 58009, 65029, 73145,
84114, 8K160
used on 001A
41 390A NSA5059C4 . NUT VF6198 003
OPT TO TE9925-4 72962
OPT TO THCR54 F0224
- ITEM NOT ILLUSTRATED

Page 10041-3
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 001A
41 400A NAS1149C0463R . WASHER V80205 003
Optional Vendor Code 10630, 1ER65, 58009, 65029,
8K160
used on 001A
41 410A MS24665-151 . PIN-COTTER V96906 003
Optional Vendor Code 10630, 65029, 73145, 84114,
8K160
used on 001A
41 420A NAS1149C0432R . WASHER V80205 002
Optional Vendor Code 10630, 1ER65, 58009, 65029,
8K160
used on 001A
41 430A NSA5031-4D11 . BOLT VF6198 002
Optional Vendor Code 04795, 2N935, C4293, C5543,
FAWT4, K8753, T0802
used on 001A
41 440A D5237180300400 . ROD ASSY-CONNECTING VFAPE3 001
used on 001A
41 450A D5237180320400 .. ROD-CONNECTING VFAPE3 001
used on 440A
41 460A MS14103-4K .. BEARING V96906 002
Optional Vendor Code 09455, 15860, F0222, S0352
used on 440A
- ITEM NOT ILLUSTRATED

Page 10041-4
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

A 420
350 400
430 410
200
290
300 210
250

310
290 240 370 460
340 220 380
360 390 440
20 230
450
320

280
280
180
170
290
300
130
30 150
40 140
260
270 460
190
330 370 150
380
10 390
120

400
410
70
160 370
380
40 390
50

60

90
100
110
80

F_PL_523217_41_A_01_00

SHAFT-SEQUENCE,CONTINUED
Figure 41A / FIGURE-52-32-17-950-841-A01

Page 10041A-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
41A - 001A D52373300000CTD SHAFT-SEQUENCE,CONTINUED VFAPE3 RF
used on 260B (523217400)
SEE 52-32-17-400 FOR NHA
41A 010A D5237330600000 . LINK ASSY VFAPE3 001
used on 001A
41A 020A D5237153120200 .. FORK VFAPE3 001
used on 010A
41A 030A NAS509L3C .. NUT V80205 001
Optional Vendor Code 60119, 92595, F2094, FAWT4
used on 010A
41A 040A SP108D .. WASHER-TAB VK4955 002
Optional Vendor Code 04795, 2N935, C5543, K4975
used on 010A
41A 050A NAS509-3C .. NUT V80205 001
Optional Vendor Code 01673, 04795, 06329, 2N935,
60996, 8K160, 92595, C5543
used on 010A
41A 060A D5237152620200 .. FORK VFAPE3 001
used on 010A
41A 070A D5237153420200 .. SLEEVE VFAPE3 001
used on 010A
41A 080A NSA5031-3D7 .. BOLT VF6198 001
Optional Vendor Code 04795, 2N935, C4293, C5543,
F6167, F7411, FAWT4, K5673, K8753, T0802
used on 010A
41A 090A NAS1149C0332R .. WASHER V80205 001
Optional Vendor Code 10630, 58009, 65029, 8K160
used on 010A
41A 100A NSA5059E3 .. NUT VF6198 001
OPT TO 73783CM8-328 56878
Optional Vendor Code 04795, 15653, 2N935, C5543,
F0224, FAWT4
used on 010A
41A 110A MS24665-88 .. PIN-COTTER V96906 001
Optional Vendor Code 10630, 58009, 65029, 73145,
84114, 8K160
used on 010A
41A 120A D5237152820000 .. ROD VFAPE3 001
used on 010A
41A 130A D5237336800000 .. LEVER ASSY VFAPE3 001
used on 010A
- ITEM NOT ILLUSTRATED

Page 10041A-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
41A 140A D5237330720000 ... LEVER VFAPE3 001
used on 130A
41A 150A D5237153720000 ... BUSHING-SHOULDERED VFAPE3 002
used on 130A
41A 160A D5237153320000 ... BUSHING VFAPE3 001
used on 130A
41A 170A D5237111920200 . SUPPORT-FITTING VFAPE3 001
used on 001A
41A 180A 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, 06725, 17446, 2N935,
56878, 73197, C4293, C5543, K5673, U6300
used on 001A
41A 190A NSA5075-5 . COLLAR VF6198 002
OPT TO DAN11-5 D8518
OPT TO F0N2-1181-5 H1822
OPT TO HL70AA5 92215
Optional Vendor Code 04795, 2N935, 56878, 5M902,
73197, 80539, C5543, U6300
used on 001A
41A 200A D5237186400400 . SHAFT ASSY-SEQUENCE VFAPE3 001
used on 001A
41A 210A D5237186520000 .. SHAFT-SEQUENCE VFAPE3 001
used on 200A
41A 220A D5237186700200 .. LEVER ASSY-SERRATED VFAPE3 001
used on 200A
41A 230A D5237186720200 ... LEVER-SERRATED VFAPE3 001
used on 220A
41A 240A MS14102-4K ... BEARING V96906 001
Optional Vendor Code 15860, S0352
used on 220A
41A 250A D5237151220800 .. CAM-LOCKING VFAPE3 001
used on 200A
41A 260A D5237186820000 .. LEVER-LINK VFAPE3 001
used on 200A
41A 270A D5237153320000 .. BUSHING VFAPE3 001
used on 200A
41A 280A DAN15-6-18 . PIN-RIVET VD8518 002
OPT TO HL20PB6-18 73197
- ITEM NOT ILLUSTRATED

Page 10041A-2
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
Optional Vendor Code 04795, 2N935, C4293, C5543,
K5673
used on 001A
41A 290A NAS1149C0332R . WASHER V80205 004
Optional Vendor Code 10630, 58009, 65029, 8K160
used on 001A
41A 300A NAS1291C3M . NUT V80205 003
OPT TO H42-3 15653
Optional Vendor Code 15653, 27238, 52828, F0224
used on 001A
41A 310A DAN15-6-16 . PIN-RIVET VD8518 001
OPT TO HL20PB6-16 92215
Optional Vendor Code 04795, 2N935, C4293, C5543,
K5673
used on 001A
41A 320A NSA5031-3D7 . BOLT VF6198 001
Optional Vendor Code 04795, 2N935, C4293, C5543,
F6167, F7411, FAWT4, K5673, K8753, T0802
used on 001A
41A 330A D5237153420200 . SLEEVE VFAPE3 001
used on 001A
41A 340A NSA5059E3 . NUT VF6198 001
OPT TO 73783CM8-328 56878
Optional Vendor Code 04795, 15653, 2N935, C5543,
F0224, FAWT4
used on 001A
41A 350A D5237186620000 . LEVER-SERRATED VFAPE3 001
used on 001A
41A 360A MS24665-88 . PIN-COTTER V96906 001
Optional Vendor Code 10630, 58009, 65029, 73145,
84114, 8K160
used on 001A
41A 370A NSA5059E4 . NUT VF6198 003
OPT TO 73783CM8-428 56878
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 001A
41A 380A NAS1149C0463R . WASHER V80205 003
Optional Vendor Code 10630, 1ER65, 58009, 65029,
8K160
used on 001A
- ITEM NOT ILLUSTRATED

Page 10041A-3
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
41A 390A MS24665-151 . PIN-COTTER V96906 003
Optional Vendor Code 10630, 65029, 73145, 84114,
8K160
used on 001A
41A 400A NSA5031-4D11 . BOLT VF6198 002
Optional Vendor Code 04795, 2N935, C4293, C5543,
FAWT4, K8753, T0802
used on 001A
41A 410A NAS1149C0432R . WASHER V80205 002
Optional Vendor Code 10630, 1ER65, 58009, 65029,
8K160
used on 001A
41A 420A A5227148120200 . SCREW VFAPE3 001
used on 001A
41A 430A NSA5355-4CA . WASHER-LOCK VF6198 001
Optional Vendor Code 04795, 2N935, 58009, C5543,
F2094, F7395, F7756
used on 001A
41A 440A D5237180300200 . ROD ASSY-CONNECTING VFAPE3 001
used on 001A
41A 450A D5237180320200 .. ROD-CONNECTING VFAPE3 001
used on 440A
41A 460A MS14102-4K .. BEARING V96906 002
Optional Vendor Code 15860, S0352
used on 440A
- ITEM NOT ILLUSTRATED

Page 10041A-4
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

420
A 350
400
430 410
200

470 210
250
460
440
370 450
220 380
390
230
310

260
270
330 300
480 280
240 180 460

290 400
340 190 410
360 30 170
40 130
320
20
140 150
150
190
370
380 370
390 380
120 390
10

70
160
40
50 90
100
60 110 A
80
F_PL_523217_41_B_01_00

SHAFT-SEQUENCE,CONTINUED
Figure 41B / FIGURE-52-32-17-950-841-B01

Page 10041B-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
41B - 001A D5237330000671 SHAFT-SEQUENCE,CONTINUED VFAPE3 RF
used on 260C (523217400)
SEE 52-32-17-400 FOR NHA
41B 010A D5237330600000 . LINK ASSY VFAPE3 001
used on 001A
41B 020A D5237153120200 .. FORK VFAPE3 001
used on 010A
41B 030A NAS509L3C .. NUT V80205 001
Optional Vendor Code 60119, 92595, F2094, FAWT4
used on 010A
41B 040A SP108D .. WASHER-TAB VK4955 002
Optional Vendor Code 04795, 2N935, C5543, K4975
used on 010A
41B 050A NAS509-3C .. NUT V80205 001
Optional Vendor Code 01673, 04795, 06329, 2N935,
60996, 8K160, 92595, C5543
used on 010A
41B 060A D5237152620200 .. FORK VFAPE3 001
used on 010A
41B 070A D5237153420200 .. SLEEVE VFAPE3 001
used on 010A
41B 080A NSA5031-3D7 .. BOLT VF6198 001
Optional Vendor Code 04795, 2N935, C4293, C5543,
F6167, F7411, FAWT4, K5673, K8753, T0802
used on 010A
41B 090A NAS1149C0332R .. WASHER V80205 001
Optional Vendor Code 10630, 58009, 65029, 8K160
used on 010A
41B 100A NSA5059E3 .. NUT VF6198 001
OPT TO 73783CM8-328 56878
Optional Vendor Code 04795, 15653, 2N935, C5543,
F0224, FAWT4
used on 010A
41B 110A MS24665-88 .. PIN-COTTER V96906 001
Optional Vendor Code 10630, 58009, 65029, 73145,
84114, 8K160
used on 010A
41B 120A D5237152820000 .. ROD VFAPE3 001
used on 010A
41B 130A D5237336800000 .. LEVER ASSY VFAPE3 001
used on 010A
- ITEM NOT ILLUSTRATED

Page 10041B-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
41B 140A D5237330720000 ... LEVER VFAPE3 001
used on 130A
41B 150A D5237153720000 ... BUSHING-SHOULDERED VFAPE3 002
used on 130A
41B 160A D5237153320000 ... BUSHING VFAPE3 001
used on 130A
41B 170A D5237111920200 . SUPPORT-FITTING VFAPE3 001
used on 001A
41B 180A 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, 06725, 17446, 2N935,
56878, 73197, C4293, C5543, K5673, U6300
used on 001A
41B 190A NSA5075-5 . COLLAR VF6198 002
OPT TO DAN11-5 D8518
OPT TO F0N2-1181-5 H1822
OPT TO HL70AA5 92215
Optional Vendor Code 04795, 2N935, 56878, 5M902,
73197, 80539, C5543, U6300
used on 001A
41B 200A D5237186401000 . SHAFT ASSY-SEQUENCE VFAPE3 001
used on 001A
41B 210A D5237186520000 .. SHAFT-SEQUENCE VFAPE3 001
used on 200A
41B 220A D5237186700200 .. LEVER ASSY-SERRATED VFAPE3 001
used on 200A
41B 230A D5237186720200 ... LEVER-SERRATED VFAPE3 001
used on 220A
41B 240A MS14102-4K ... BEARING V96906 001
Optional Vendor Code 15860, S0352
used on 220A
41B 250A D5237152920000 .. CAM-LOCKING VFAPE3 001
used on 200A
41B 260A D5237186820000 .. LEVER-LINK VFAPE3 001
used on 200A
41B 270A D5237153320000 .. BUSHING VFAPE3 001
used on 200A
41B 280A DAN15-6-18 . PIN-RIVET VD8518 002
OPT TO HL20PB6-18 73197
- ITEM NOT ILLUSTRATED

Page 10041B-2
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
Optional Vendor Code 04795, 2N935, C4293, C5543,
K5673
used on 001A
41B 290A NAS1149C0332R . WASHER V80205 001
Optional Vendor Code 10630, 58009, 65029, 8K160
used on 001A
41B 300A NAS1291C3M . NUT V80205 001
OPT TO H42-3 15653
Optional Vendor Code 15653, 27238, 52828, F0224
used on 001A
41B 310A NSA5031-3-17 . BOLT VF6198 001
Optional Vendor Code 04795, 2N935, C4293, C5543,
F6167, F7411, FAWT4, K5673, K8753, T0802
used on 001A
41B 320A NSA5031-3D7 . BOLT VF6198 001
Optional Vendor Code 04795, 2N935, C4293, C5543,
F6167, F7411, FAWT4, K5673, K8753, T0802
used on 001A
41B 330A D5237153420200 . SLEEVE VFAPE3 001
used on 001A
41B 340A NSA5059E3 . NUT VF6198 001
OPT TO 73783CM8-328 56878
Optional Vendor Code 04795, 15653, 2N935, C5543,
F0224, FAWT4
used on 001A
41B 350A D5237186620000 . LEVER-SERRATED VFAPE3 001
used on 001A
41B 360A MS24665-88 . PIN-COTTER V96906 001
Optional Vendor Code 10630, 58009, 65029, 73145,
84114, 8K160
used on 001A
41B 370A NSA5059E4 . NUT VF6198 003
OPT TO 73783CM8-428 56878
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 001A
41B 380A NAS1149C0463R . WASHER V80205 003
Optional Vendor Code 10630, 1ER65, 58009, 65029,
8K160
used on 001A
41B 390A MS24665-151 . PIN-COTTER V96906 003
Optional Vendor Code 10630, 65029, 73145, 84114,
8K160
- ITEM NOT ILLUSTRATED

Page 10041B-3
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 001A
41B 400A NSA5031-4D11 . BOLT VF6198 002
Optional Vendor Code 04795, 2N935, C4293, C5543,
FAWT4, K8753, T0802
used on 001A
41B 410A NAS1149C0432R . WASHER V80205 002
Optional Vendor Code 10630, 1ER65, 58009, 65029,
8K160
used on 001A
41B 420A A5227148120200 . SCREW VFAPE3 001
used on 001A
41B 430A NSA5355-4CA . WASHER-LOCK VF6198 001
Optional Vendor Code 04795, 2N935, 58009, C5543,
F2094, F7395, F7756
used on 001A
41B 440A D5237180300200 . ROD ASSY-CONNECTING VFAPE3 001
used on 001A
41B 450A D5237180320200 .. ROD-CONNECTING VFAPE3 001
used on 440A
41B 460A MS14102-4K .. BEARING V96906 002
Optional Vendor Code 15860, S0352
used on 440A
41B 470A NAS1726C3PE . NUT V80205 002
Optional Vendor Code 15653, 27238, 66776, F0224
used on 001A
41B 480A NAS1149C0363R . WASHER V80205 001
Optional Vendor Code 10630, 1ER65, 58009, 65029,
8K160
used on 001A
- ITEM NOT ILLUSTRATED

Page 10041B-4
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

A
240
60 250
70 280

50

A 260 60
250 70 60
270 70
290

110

160

210
50
220
300

40

180

190
200 80
30
20
170 80 10

110 230
160 90
100
110
160

130
150
120 140

F_PL_523217_44_0_01_00

MECHANISM-INTERLOCK
Figure 44 / FIGURE-52-32-17-950-844-01

Page 10044-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
44 - 001A D5237330000065 MECHANISM-INTERLOCK VFAPE3 RF
used on 050A (523217050)
SEE 52-32-17-050 FOR NHA
44 - 001B D5237330000065 MECHANISM-INTERLOCK VFAPE3 RF
used on 050B (523217050)
SEE 52-32-17-050 FOR NHA
44 010A D5237145500000 . SLEEVE ASSY-SPRING VFAPE3 001
used on 001A, 001B
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, 001B
44 050A MS20392-3T49 . PIN V96906 002
Optional Vendor Code 04795, 06329, 6D833, 70347,
C5543, C5729, F0188, H2776
used on 001A, 001B
44 060A MS24665-151 . PIN-COTTER V96906 003
Optional Vendor Code 04795, 06329, 60996, 84114,
8K160, C5543, C5729
used on 001A, 001B
44 070A NAS1149C0463R . WASHER V80205 003
Optional Vendor Code 04795, 60996, 8K160, C5543,
C5729
used on 001A, 001B
44 080A D5237148420000 . WASHER-SPACER VFAPE3 002
used on 001A, 001B
44 090A D5237145000400 . MECHANISM-INTERLOCK VFAPE3 001
used on 001A, 001B
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
Optional Vendor Code 04795, 70347, 97464, C5543,
C5729
used on 090A
44 130A D5237147820000 .. PIN VFAPE3 001
used on 090A
- ITEM NOT ILLUSTRATED

Page 10044-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
44 140A D5237147720000 .. ROLLER VFAPE3 001
used on 090A
44 150A D5237179420000 .. ROD-CONNECTING VFAPE3 001
used on 090A
44 160A NSA5321-6 .. RING-RETAINING VF5442 003
OPT TO ST6 D8090
Optional Vendor Code 04795, C5543, C5729, F7756
used on 090A
44 170A D5237146620400 .. LEVER VFAPE3 001
used on 090A
44 180A D5237113420600 .. SCREW-ADJUSTING VFAPE3 001
used on 090A
44 190A NAS509-5C .. NUT V80205 001
Optional Vendor Code 92595
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
Optional Vendor Code 04795, 60996, 8K160, C5543,
C5729
used on 001A, 001B
44 230A D5237145821000 . BUSHING VFAPE3 001
used on 001A, 001B
44 240A NSA5059C6 . NUT VF5442 001
OPT TO TE9925-6 72962
OPT TO THCR56 F0224
Optional Vendor Code 04795, C5543, C5729, F0188
used on 001A
44 240B NSA5059E6 . NUT VF5442 001
OPT TO 73783CM8-624 56878
Optional Vendor Code 04795, 92215, C5543, C5729,
F0188
used on 001B
44 250A NAS1149C0663R . WASHER V80205 002
Optional Vendor Code 04795, 10630, 56563, 60996,
70347, 8K160, C5543, C5729
used on 001A, 001B
44 260A D5237145821200 . BUSHING VFAPE3 001
used on 001A, 001B
- ITEM NOT ILLUSTRATED

Page 10044-2
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
44 270A NAS1306-22D . BOLT V80205 001
NAS6606D22 80205
Optional Vendor Code 04348, 04795, 06329, C5543,
C5729, F0188, K8753
used on 001A, 001B
44 280A MS24665-300 . PIN-COTTER V96906 001
Optional Vendor Code 04795, 06329, 60996, 84114,
8K160, C5543, C5729
used on 001A, 001B
44 290A NSA5059C4 . NUT VF5442 001
OPT TO TE9925-4 72962
OPT TO THCR54 F0224
Optional Vendor Code 04795, C5543, C5729, F0188
used on 001A
44 290B NSA5059E4 . NUT VF5442 001
OPT TO 73783CM8-428 56878
Optional Vendor Code 04795, 92215, C5543, C5729,
F0188
used on 001B
44 300A NAS1304-23D . BOLT V80205 001
NAS6604D23 80205
Optional Vendor Code F0188, F7411, K8753
used on 001A, 001B
- ITEM NOT ILLUSTRATED

Page 10044-3
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

A
40

20

30

90

80

120
50
60
130
B 140
70

100
20

100

110

50 10
60
30

F_PL_523217_50_0_01_00

HOUSING-VALVE
Figure 50 / FIGURE-52-32-17-950-850-01

Page 10050-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
50 - 001A D5237310000061 HOUSING-VALVE VFAPE3 RF
used on 050A (523217010)
SEE 52-32-17-010 FOR NHA
50 - 001B D5237310000062 HOUSING-VALVE VFAPE3 RF
used on 050B (523217010)
SEE 52-32-17-010 FOR NHA
50 - 001C D5237310000662 HOUSING-VALVE VFAPE3 RF
used on 050C (523217010)
SEE 52-32-17-010 FOR NHA
50 - 001D D5237310000062 HOUSING-VALVE VFAPE3 RF
used on 051A (523217010)
POST SB 52-1124
SEE 52-32-17-010 FOR NHA
50 010A DAN79-07 . HOSE VFAPE3 001
REQUIRED LENGTH 400 MM
Optional Vendor Code C5543
used on 001A, 001B, 001C, 001D
50 020A ABS0341-1-01 . RETAINER-VALVE VFAPE3 002
OPT TO 140N2021-1H 57336
Optional Vendor Code 04795, C5543, C5729
used on 001A, 001B, 001C, 001D
50 030A ABS0341-2-01 . VALVE-BASIC VFAPE3 002
OPT TO 140N2022S2 57336
Optional Vendor Code 04795, C5543, C5729
used on 001A
50 030B ABS0341-2-02 . VALVE VFAPE3 002
OPT TO 140N2022S1 57336
Optional Vendor Code 04795, C5543, C5729
used on 001B, 001C
50 - 031A ABS0341-2-02 . VALVE VFAPE3 002
OPT TO 140N2022S1 57336
Optional Vendor Code 04795, C5543, C5729
used on 001D
POST SB 52-1124
50 040A NAS1100E08-12 . SCREW V80205 002
Optional Vendor Code F0188, F7411, K8753
used on 001A, 001B, 001C, 001D
50 050A NAS1149CN832R . WASHER V80205 004
OPT TO 7283A04-230 B0014
Optional Vendor Code 04795, 60996, 8K160, C5543,
C5729
- ITEM NOT ILLUSTRATED

Page 10050-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 001A, 001B, 001C, 001D
50 060A NAS1291C08M . NUT V80205 004
OPT TO 180003-08 60119
OPT TO FN1014M832 56878
OPT TO H42L08 K6405
OPT TO PLH508M F0224
OPT TO RMLH3858-82 72962
OPT TO T99C832M 11815
OPT TO VN300D82 92215
Optional Vendor Code 04795, 06329, 60996, 8K160,
C5543, C5729, H2776
used on 001A, 001B, 001C, 001D
50 070A NAS1100E08-8 . SCREW V80205 002
Optional Vendor Code F0188, F7411, K8753
used on 001A, 001B, 001C, 001D
50 080A D5237127320000 . FLANGE VFAPE3 001
used on 001A, 001B, 001D
50 080B D5237183120000 . FLANGE VFAPE3 001
used on 001C
50 090A D5237127200000 . TUBE ASSY VFAPE3 001
used on 001A, 001B, 001D
50 090B D5237183020000 . TUBE VFAPE3 001
used on 001C
50 100A 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, 001D
50 110A NSA935504-01 . MOUNT VF5442 001
OPT TO 00326110059 F0394
Optional Vendor Code 04795, 42C51, C5543, C5729
used on 001A, 001B, 001C, 001D
50 120A NAS6703-4 . BOLT V80205 001
Optional Vendor Code 04795, 06329, 32664, 60996,
8K160, C5543, C5729, K8753
used on 001A, 001B, 001C, 001D
50 130A NAS1149C0332R . WASHER V80205 001
Optional Vendor Code 04795, 5N982, 60996, 8K160,
C5543, C5729
- ITEM NOT ILLUSTRATED

Page 10050-2
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 001A, 001B, 001C, 001D
50 140A NAS1291C3M . NUT V80205 001
OPT TO H42-3 15653
Optional Vendor Code 04795, 60119, C5543, C5729,
F0224
used on 001A, 001B, 001C, 001D
- ITEM NOT ILLUSTRATED

Page 10050-3
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 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

20
A B
A
230
50 240

10 200

C 210
190
B 220
270
280

280 220
60 C 240

280
260 250
G
320 320
D
280 E
F
320
150

80
290 140
300

184

F G D
182

80
110 F
E 70

120 F
170 G

80 G 110
180

F_PL_523217_60_0_01_00

ELECTRICAL SYSTEM
Figure 60 / FIGURE-52-32-17-950-860-01

Page 10060-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
60 - 001A D9209031203060 ELECTRICAL SYSTEM VFAPE3 RF
used on 060A (523217010)
SEE 52-32-17-010 FOR NHA
60 - 001B D9209031202260 ELECTRICAL SYSTEM VFAPE3 RF
used on 060B (523217010)
SEE 52-32-17-010 FOR NHA
60 010A D9299741300000 . HARNESS-CABLE,4613VB VFAPE3 001
used on 001A
60 010B D9299741300200 . HARNESS-CABLE,4613VB VFAPE3 001
used on 001B
60 020A EN2997SE61624CN .. CONNECTOR-PLUG VI9005 001
OPT TO 85333ES1624PN08 F0225
OPT TO 9836SE16-24PN F1983
OPT TO E0442SE16-24PN F5442
OPT TO HTAMF05-16-24PN K0316
Optional Vendor Code 04795, C5543, C5729
used on 010A, 010B
60 - 030A NSA938151PA2000 .. CONTACT-PIN VF5442 014
EN3155-018M2018 I9005
OPT TO 004-0141-20 F1983
OPT TO 006-0044-20A F1983
OPT TO 050-0001-2018 14283
OPT TO 330-7587-000 F3132
OPT TO 6TBD100462 49367
OPT TO 8522-2349A F0225
Optional Vendor Code 04795, C5543, C5729
used on 010A, 010B
60 - 040A E0616BB2000 .. PLUG-SEALING VF5442 010
OPT TO 8522-389A F0225
OPT TO NSA938153BB2000 F5442
OPT TO SB2034 F0225
Optional Vendor Code 04795, C5543, C5729
used on 010A, 010B
60 050A E0115A12-16-3 .. ELBOW VF5442 001
OPT TO T9312-12 K0685
Optional Vendor Code 04795, C5543, C5729
used on 010A, 010B
- ITEM NOT ILLUSTRATED

Page 10060-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
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 SST1M39 06383
OPT TO T18RHS D8527
Optional Vendor Code 04795, C0259, C5543, C5729,
D8527
used on 010A
60 - 054A NSA935805-12 .. ELECTRICAL CONDUIT VF5442 AR
USE AS REQUIRED, DETERMINE LENGTH ON
INSTALLATION
OPT TO C10000-0-0-24 81482
OPT TO GC100-12 F0564
OPT TO SF001-00-00-12 F6101
Optional Vendor Code C5543
used on 010A, 010B
60 - 056A DAN79-05 .. HOSE VFAPE3 AR
USE AS REQUIRED, DETERMINE LENGTH ON
INSTALLATION
Optional Vendor Code C4344, C5543
used on 010A, 010B
60 060A D9299741200000 . HARNESS-CABLE,4612VB VFAPE3 001
used on 001A
60 060B D9299741200200 . HARNESS-CABLE,4612VB VFAPE3 001
used on 001B
60 070A EN3646A6083ADN .. CONNECTOR-PLUG VI9005 001
OPT TO 6TBD101465 F0225
OPT TO 6TBD101466 F1983
OPT TO 7TBD101554 F1983
OPT TO 7TBD102262 F0225
OPT TO E0052R8B3ASNE F5442
Optional Vendor Code 04795, C5543, C5729
used on 060A, 060B
60 080A ABS0638A08 .. BACKSHELL-CONNECTOR VFAPE3 004
OPT TO GK5430 C3471
Optional Vendor Code 04795, C5543, C5729
used on 060A, 060B
60 - 090A NSA938152SA2000 .. CONTACT-SOCKET VF5442 006
EN3155-019F2018 I9005
- ITEM NOT ILLUSTRATED

Page 10060-2
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
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, 060B
60 - 100A E0616BB2000 .. PLUG-SEALING VF5442 024
OPT TO 8522-389A F0225
OPT TO NSA938153BB2000 F5442
OPT TO SB2034 F0225
Optional Vendor Code 04795, C5543, C5729
used on 060A, 060B
60 110A ABS0638B08 .. BACKSHELL-CONNECTOR VFAPE3 002
OPT TO GK5440 C3471
Optional Vendor Code 04795, C5543, C5729
used on 060A, 060B
60 120A E0073-8-3AT .. SEAL-PRESSURE VF5442 001
OPT TO DTP07-8-3AK F1983
OPT TO PVW77-8-98-57 K0316
Optional Vendor Code 04795, C5543, C5729
used on 060A, 060B
60 - 130A NSA934701BU2000 .. PLUG-BLIND VF5442 002
OPT TO DF90-006-20 F1983
Optional Vendor Code D8518
used on 060A, 060B
60 140A A5217240234400 .. WASHER-SPECIAL VFAPE3 002
used on 060A, 060B
60 - 142A NSA935401-03 .. TIE-CABLE VF5442 030
OPT TO 32012 F2693
OPT TO 32251 F2693
OPT TO PLT1M30 06383
OPT TO SST1M30 06383
OPT TO SST1M39 06383
OPT TO T18RHS D8527
Optional Vendor Code 04795, C0259, C5543, C5729,
D8527
used on 060A, 060B
- ITEM NOT ILLUSTRATED

Page 10060-3
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
60 150A D9269000400200 .. BLOCK-TERMINAL VFAPE3 001
used on 060A, 060B
SEE 52-32-17-630 FOR DET
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
Optional Vendor Code 04795, C5543, C5729, F0225,
F0394, F1983
used on 060A, 060B
60 170A E0073-8-3AT .. SEAL-PRESSURE VF5442 001
OPT TO DTP07-8-3AK F1983
OPT TO PVW77-8-98-57 K0316
Optional Vendor Code 04795, C5543, C5729
used on 060A, 060B
60 180A EN3646A6083ADN .. CONNECTOR-PLUG VI9005 001
OPT TO 6TBD101465 F0225
OPT TO 6TBD101466 F1983
OPT TO 7TBD101554 F1983
OPT TO 7TBD102262 F0225
OPT TO E0052R8B3ASNE F5442
Optional Vendor Code 04795, C5543, C5729
used on 060A, 060B
60 182A D9249550220000 .. WASHER VFAPE3 002
used on 060A, 060B
60 184A D9249550120000 .. PLATE-MOUNTING VFAPE3 002
used on 060A, 060B
60 - 186A NSA935805-04 .. ELECTRICAL CONDUIT VF5442 AR
USE AS REQUIRED, DETERMINE LENGTH ON
INSTALLATION
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, 060B
- ITEM NOT ILLUSTRATED

Page 10060-4
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
60 190A NSA935807-12 . CLAMP VF5442 001
OPT TO 50011-12 F6101
Optional Vendor Code 04795, C5543, C5729, F0215,
F0355
used on 001A, 001B
60 200A NSA5527-03-04 . SPACER VF5442 001
Optional Vendor Code 04795, C0506, C5543, C5729,
F8982
used on 001A, 001B
60 210A NAS1096-2-29 . SCREW V80205 001
NAS1801-08-29 80205
Optional Vendor Code 04795, C5543, C5729, F0188,
K8753
used on 001A, 001B
60 220A NAS1149DN816K . WASHER V80205 003
Optional Vendor Code 04795, 60996, 8K160, C5543,
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
Optional Vendor Code 04795, C5543, C5729, 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 PLH3508M F0224
OPT TO RH30A08 52828
OPT TO RM52LH3324-82 72962
OPT TO T98S832 11815
OPT TO VN300A82 92215
Optional Vendor Code 04795, 06329, 60996, 75237,
8K160, C5543, C5729
used on 001A, 001B
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
- ITEM NOT ILLUSTRATED

Page 10060-5
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
Optional Vendor Code 04795, C5543, C5729, F0188,
K8753
used on 001A, 001B
60 270A NSA935513-07 . MOUNT VF5442 001
OPT TO TY5K7HS D8527
Optional Vendor Code 04795, C5543, C5729
used on 001A, 001B
60 280A NSA935513-05 . MOUNT VF5442 007
OPT TO TY5K5HS D8527
Optional Vendor Code 04795, C5543, C5729
used on 001A, 001B
60 290A NAS1096-2-7 . SCREW V80205 004
NAS1801-08-7 80205
Optional Vendor Code F0188, K8753
used on 001A, 001B
60 300A NAS1149CN832R . WASHER V80205 004
OPT TO 7283A04-230 B0014
Optional Vendor Code 04795, 60996, 8K160, C5543,
C5729
used on 001A, 001B
60 - 310A D9239125000860 . SENSOR-DOOR VFAPE3 001
used on 001A
SEE 52-32-17-620 FOR DET
60 - 310B D9239125001460 . SENSOR-DOOR VFAPE3 001
used on 001B
SEE 52-32-17-620 FOR DET
60 320A NSA931025-03A . LABEL VF5442 004
Optional Vendor Code 04795, 91345, C5543, C5729,
F0347, F4240
used on 001A, 001B
60 - 330A NSA935401-03 .. TIE-CABLE VF5442 050
OPT TO 32012 F2693
OPT TO 32251 F2693
OPT TO PLT1M30 06383
OPT TO SST1M30 06383
OPT TO SST1M39 06383
OPT TO T18RHS D8527
Optional Vendor Code 04795, C0259, C5543, C5729,
D8527
used on 320A
- ITEM NOT ILLUSTRATED

Page 10060-6
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

A 20

C
50
A

60
70

C
50
B

10
10

20

30
60
70 60
70 30
60 70
70 20

40

F_PL_523217_62_0_01_00

SENSOR-DOOR
Figure 62 / FIGURE-52-32-17-950-862-01

Page 10062-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
62 - 001A D9239125000860 SENSOR-DOOR VFAPE3 RF
used on 310A (523217600)
SEE 52-32-17-600 FOR NHA
62 - 001B D9239125001460 SENSOR-DOOR VFAPE3 RF
used on 310B (523217600)
SEE 52-32-17-600 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
Optional Vendor Code 04795, C5543, C5729
used on 001A
REFER TO SIL 32-093
62 010B 8-933-01 . SENSOR-PROXIMITY,RECTANGULAR V08748 002
OPT TO 201655069 K0654
OPT TO ABS0121-40 FAPE3
OPT TO H10468642SC U7388
Optional Vendor Code 04795, C5543, C5729
used on 001B
62 020A 8-368-04 . TARGET V08748 003
OPT TO 666000078 K0654
OPT TO ABS0121-11 FAPE3
Optional Vendor Code 04795, C5543, C5729, K0653
used on 001A, 001B
62 030A NAS1096-3-10 . SCREW V80205 004
NAS1801-3-10 80205
Optional Vendor Code 04795, C5543, C5729, F0188,
F7411, K8753
used on 001A, 001B
62 040A NAS1096-3-8 . SCREW V80205 002
NAS1801-3-8 80205
Optional Vendor Code 04795, C5543, C5729, F0188,
F7411, K8753
used on 001A, 001B
62 050A NAS1096-3-7 . SCREW V80205 004
NAS1801-3-7 80205
Optional Vendor Code F0188, K8753
used on 001A, 001B
62 060A NAS1291C3M . NUT V80205 008
OPT TO H42-3 15653
- ITEM NOT ILLUSTRATED

Page 10062-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
Optional Vendor Code 04795, 60119, C5543, C5729,
F0224
used on 001A, 001B
62 070A NAS1149C0332R . WASHER V80205 010
Optional Vendor Code 04795, 5N982, 60996, 8K160,
C5543, C5729
used on 001A, 001B
- ITEM NOT ILLUSTRATED

Page 10062-2
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

20 10

40

30

20

F_PL_523217_63_0_01_00

BLOCK-TERMINAL
Figure 63 / FIGURE-52-32-17-950-863-01

Page 10063-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
63 - 001A D9269000400200 BLOCK-TERMINAL VFAPE3 RF
used on 150A (523217600)
SEE 52-32-17-600 FOR NHA
63 010A NSA937901RB0100 . RAIL VF5442 001
Optional Vendor Code 04795, C5543, C5729, F0394,
F1983
used on 001A
63 020A NSA937901S . END-CLAMPS VF5442 002
OPT TO 00110201060 F0394
OPT TO 020-0020-00 F1983
Optional Vendor Code 04795, C5543, C5729
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
Optional Vendor Code 04795, C5543, C5729
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
Optional Vendor Code 04795, C5543, C5729
used on 001A
- ITEM NOT ILLUSTRATED

Page 10063-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

30
40

60

40
50

10

26
28

40 60
50
22

24
30
20 40

F_PL_523217_70_0_01_00

FAIRING INSTL-AFT CARGO COMPT DOOR

Figure 70 / FIGURE-52-32-17-950-870-01

Page 10070-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
70 - 001A D5347850100060 FAIRING INSTL-AFT CARGO COMPT DOOR VFAPE3 RF
used on 070A (523217010)
SEE 52-32-17-010 FOR NHA
70 010A D5347851400000 . FAIRING VFAPE3 001
used on 001A
70 020A D5347851200000 . FAIRING VFAPE3 001
used on 001A
70 022A D5347851720000 .. GLASS-SIGHT VFAPE3 001
used on 020A
70 024A NAS1102E08-8 .. SCREW V80205 004
Optional Vendor Code F0188, K8753
used on 020A
70 026A ABS0382C42 .. WASHER VFAPE3 004
Optional Vendor Code 04795, C5543, C5729, F7395,
F7756
used on 020A
70 028A NAS1291C08M .. NUT V80205 004
OPT TO 180003-08 60119
OPT TO FN1014M832 56878
OPT TO H42L08 K6405
OPT TO PLH508M F0224
OPT TO RMLH3858-82 72962
OPT TO T99C832M 11815
OPT TO VN300D82 92215
Optional Vendor Code 04795, 06329, 60996, 8K160,
C5543, C5729, H2776
used on 020A
70 030A NSA5030-3-3 . SCREW VF5442 021
ASNA2001V3-3 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001A
70 040A NAS1169C10 . WASHER V80205 030
Optional Vendor Code 04795, C5543, C5729
used on 001A
70 050A NSA5030-3-6 . SCREW VF5442 009
ASNA2001V3-6 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001A
- ITEM NOT ILLUSTRATED

Page 10070-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
70 060A D5347850300060 . STRUCTURE-FAIRING VFAPE3 001
used on 001A
SEE 52-32-17-710 FOR DET
- ITEM NOT ILLUSTRATED

Page 10070-2
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

110
120

230

130

20
110 10
120 230

250

140
150

190
110
160 120
230

120 180
30 70 140
240
80 220
230
170 90
50 210
40 60
50 270
260
110
90 120
110 100
120 200

F_PL_523217_71_0_01_00

STRUCTURE-FAIRING
Figure 71 / FIGURE-52-32-17-950-871-01

Page 10071-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
71 - 001A D5347850300060 STRUCTURE-FAIRING VFAPE3 RF
used on 060A (523217700)
SEE 52-32-17-700 FOR NHA
71 010A D5347853600000 . SECTION ASSY-L VFAPE3 001
used on 001A
71 020A D5347854400000 . SECTION ASSY-L VFAPE3 001
used on 001A
71 030A D5347854600000 . SECTION ASSY-L VFAPE3 001
used on 001A
71 040A DAN5-5-8 . PIN-RIVET VD8518 001
OPT TO ABS0250A5-8 FAPE3
OPT TO HL10VDF5-8 92215
Optional Vendor Code 04795, 56878, 73197, C5543,
C5729, D1283, F0188, K5673
used on 001A
71 050A NSA5076-5 . COLLAR VF5442 003
OPT TO F0N2-1208-5 H1822
OPT TO HL82-5APBW 92215
OPT TO HL82AA5APBW 92215
Optional Vendor Code 04795, 56878, 73197, C5543,
C5729, H6173
used on 001A
71 060A DAN5-5-9 . PIN-RIVET VD8518 002
OPT TO ABS0250A5-9 FAPE3
OPT TO HL10VDF5-9 92215
Optional Vendor Code 04795, 56878, 73197, C5543,
C5729, D1283, F0188, K5673
used on 001A
71 070A DAN5-6-9 . PIN-RIVET VD8518 001
OPT TO F0N2-1196-6-9 H1822
OPT TO HL10VDF6-9 92215
Optional Vendor Code 04795, 56878, 73197, C5543,
C5729, D1283, F0188, K5673
used on 001A
71 080A NSA5075-6 . COLLAR VF5442 001
OPT TO DAN11-6 D8518
OPT TO F0N2-1181-6 H1822
OPT TO HL70AA6 92215
Optional Vendor Code 04795, 56878, 73197, C5543,
C5729
used on 001A
- ITEM NOT ILLUSTRATED

Page 10071-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
71 090A DIN65399-4000BF . RIVET VD8286 AR
USE AS REQUIRED, DETERMINE LENGTH ON
INSTALLATION
used on 001A
71 100A D5347853920000 . SECTION-L,LWR VFAPE3 001
used on 001A
71 110A NSA5030-3-3 . SCREW VF5442 032
ASNA2001V3-3 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001A
71 120A DAN125-5 . WASHER-COUNTERSUNK VD8518 034
OPT TO EF3023A5 C3898
Optional Vendor Code 04795, C5543, C5729
used on 001A
71 130A D5347850400000 . WEB ASSY-DOOR VFAPE3 001
used on 001A
71 140A ABS0691-015 . STUD VFAPE3 006
OPT TO 1604S41-015BP D0680
OPT TO DV691-015 C4863
Optional Vendor Code 04795, C5543, C5729
used on 001A
71 150A D5347854920000 . WASHER VFAPE3 002
used on 001A
71 160A D5347850800000 . WEB ASSY-DOOR VFAPE3 001
used on 001A
71 170A D5347851900000 . SECTION ASSY-Z VFAPE3 001
used on 001A
71 180A D5347853200000 . ANGLE ASSY-CONNECTING VFAPE3 001
used on 001A
71 190A D5347851820000 . PLATE-SUPPORT VFAPE3 001
used on 001A
71 200A D5347853800000 . SECTION ASSY-L VFAPE3 001
used on 001A
71 210A D5347850600000 . SECTION ASSY-EDGE VFAPE3 001
used on 001A
71 220A D5347854920000 . WASHER VFAPE3 004
used on 001A
71 230A LN9198-4000CF . RIVET VD8442 AR
USE AS REQUIRED, DETERMINE LENGTH ON
INSTALLATION
EN6081D5 I9005
- ITEM NOT ILLUSTRATED

Page 10071-2
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 001A
71 240A NSA5030-3-4 . SCREW VF5442 002
ASNA2001V3-4 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001A
71 250A D5347854200000 . SECTION ASSY-L VFAPE3 001
used on 001A
71 260A D5347851620000 . PLATE VFAPE3 001
used on 001A
71 270A NAS1097KE5-00 . RIVET V80205 004
EN6069KE5 I9005
used on 001A
- ITEM NOT ILLUSTRATED

Page 10071-3
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

20
40 30 130
C
A 180 160
A 170
170

B
190

160
140
150
C
100

110
100 120
140 140
150 150
10
140 110
150 120
90

110 190
120
70 80
50
210 130
60

200

110
120

140 100
150

140 110
150 120

F_PL_523217_90_0_01_00

HINGE INSTL
Figure 90 / FIGURE-52-32-17-950-890-01

Page 10090-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
90 - 001A D5237311000061 HINGE INSTL VFAPE3 RF
used on 010A (523217040)
SEE 52-32-17-040 FOR NHA
90 010A D5237114720600 . FITTING-END VFAPE3 001
used on 001A
90 020A D5237311500200 . HINGE ASSY-OUTER VFAPE3 001
used on 001A
90 030A D5237311720200 .. HINGE-OUTER VFAPE3 001
used on 020A
90 040A D5237113820600 .. BUSHING VFAPE3 005
used on 020A
90 050A D5237311600000 . HINGE ASSY-MID VFAPE3 001
used on 001A
90 060A D5237311820000 .. HINGE-MID VFAPE3 001
used on 050A
90 070A D5237113820600 .. BUSHING VFAPE3 008
used on 050A
90 080A D5237113720600 .. BUSHING-SHOULDERED VFAPE3 004
used on 050A
90 090A D5237277421800 . SHIM VFAPE3 001
selfrom, 01.60 MM (000.063 IN) THICK
used on 001A
90 - 091A D5237277420000 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 00.30 MM
(000.012 IN) THICK
used on 001A
90 - 092A D5237277420200 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 00.40 MM
(000.016 IN) THICK
used on 001A
90 - 093A D5237277420400 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 00.50 MM
(000.020 IN) THICK
used on 001A
90 - 094A D5237277420600 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 00.60 MM
(000.024 IN) THICK
used on 001A
90 - 095A D5237277420800 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 00.80 MM
(000.032 IN) THICK
- ITEM NOT ILLUSTRATED

Page 10090-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 001A
90 - 096A D5237277421000 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 01.00 MM
(000.040 IN) THICK
used on 001A
90 - 097A D5237277421200 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 01.20 MM
(000.047 IN) THICK
used on 001A
90 - 098A D5237277421400 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 01.40 MM
(000.055 IN) THICK
used on 001A
90 - 099A D5237277421600 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 01.50 MM
(000.059 IN) THICK
used on 001A
90 100A NSA5030-3-9 . SCREW VF5442 022
ASNA2001V3-9 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001A
90 105A NSA5030-3-9 . SCREW VF5442 002
ASNA2001V3-9 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001A
90 110A NAS1149C0363R . WASHER V80205 032
Optional Vendor Code 04795, 06329, 60996, 70347,
8K160, C5543, C5729
used on 001A
90 115A NAS1149C0363R . WASHER V80205 003
Optional Vendor Code 04795, 06329, 60996, 70347,
8K160, C5543, C5729
used on 001A
90 120A NAS1291C3M . NUT V80205 032
OPT TO H42-3 15653
Optional Vendor Code 04795, 60119, C5543, C5729,
F0224
used on 001A
90 125A NAS1291C3M . NUT V80205 003
OPT TO H42-3 15653
- ITEM NOT ILLUSTRATED

Page 10090-2
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
Optional Vendor Code 04795, 60119, C5543, C5729,
F0224
used on 001A
90 130A NSA5030-4-12 . SCREW VF5442 004
ASNA2001V4-12 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001A
90 140A NAS1149C0463R . WASHER V80205 020
Optional Vendor Code 04795, 60996, 8K160, C5543,
C5729
used on 001A
90 150A NAS1291C4M . NUT V80205 020
OPT TO 180003-5 60119
OPT TO PLH504M F0224
Optional Vendor Code 04795, C5543, C5729
used on 001A
90 160A NSA5030-4-11 . SCREW VF5442 006
ASNA2001V4-11 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001A
90 170A NSA5030-4-9 . SCREW VF5442 005
ASNA2001V4-9 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001A
90 180A NSA5030-4-8 . SCREW VF5442 001
ASNA2001V4-8 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001A
90 190A NSA5030-3-8 . SCREW VF5442 010
ASNA2001V3-8 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001A
90 195A NSA5030-3-8 . SCREW VF5442 001
ASNA2001V3-8 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001A
- ITEM NOT ILLUSTRATED

Page 10090-3
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
90 200A NSA5030-4-13 . SCREW VF5442 002
ASNA2001V4-13 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001A
90 210A NAS1154-11 . SCREW V80205 002
Optional Vendor Code 04795, C5543, C5729
used on 001A
90 - 220A D52373110000CTD . STRUCTURE-DOOR VFAPE3 001
used on 001A
SEE 52-32-17-910 FOR DET
- ITEM NOT ILLUSTRATED

Page 10090-4
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

20 A
40 30 130
C
170
160
A 170
160
B 180

185

C 175

100

145
155
140
150
140
10 150 145
155
110
120 90

190
B
70 80
50
210 130
60

200

110
120

140 100
150

140
150 110
120
F_PL_523217_90_A_01_01

HINGE INSTL
Figure 90A / FIGURE-52-32-17-950-890-A01

Page 10090A-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
90A - 001B D5237311000061 HINGE INSTL VFAPE3 RF
used on 010B (523217040)
SEE 52-32-17-040 FOR NHA
90A 010A D5237114720600 . FITTING-END VFAPE3 001
used on 001B
90A 020A D5237311500200 . HINGE ASSY-OUTER VFAPE3 001
used on 001B
90A 030A D5237311720200 .. HINGE-OUTER VFAPE3 001
used on 020A
90A 040A D5237113820600 .. BUSHING VFAPE3 005
used on 020A
90A 050A D5237311600000 . HINGE ASSY-MID VFAPE3 001
used on 001B
90A 060A D5237311820000 .. HINGE-MID VFAPE3 001
used on 050A
90A 070A D5237113820600 .. BUSHING VFAPE3 008
used on 050A
90A 080A D5237113720600 .. BUSHING-SHOULDERED VFAPE3 004
used on 050A
90A 090A D5237277421800 . SHIM VFAPE3 001
selfrom, 01.60 MM (000.063 IN) THICK
used on 001B
90A - 091A D5237277420000 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 00.30 MM
(000.012 IN) THICK
used on 001B
90A - 092A D5237277420200 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 00.40 MM
(000.016 IN) THICK
used on 001B
90A - 093A D5237277420400 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 00.50 MM
(000.020 IN) THICK
used on 001B
90A - 094A D5237277420600 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 00.60 MM
(000.024 IN) THICK
used on 001B
90A - 095A D5237277420800 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 00.80 MM
(000.032 IN) THICK
- ITEM NOT ILLUSTRATED

Page 10090A-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 001B
90A - 096A D5237277421000 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 01.00 MM
(000.040 IN) THICK
used on 001B
90A - 097A D5237277421200 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 01.20 MM
(000.047 IN) THICK
used on 001B
90A - 098A D5237277421400 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 01.40 MM
(000.055 IN) THICK
used on 001B
90A - 099A D5237277421600 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 01.50 MM
(000.059 IN) THICK
used on 001B
90A 100A NSA5030-3-9 . SCREW VF5442 022
ASNA2001V3-9 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001B
90A 110A NAS1149C0363R . WASHER V80205 032
Optional Vendor Code 04795, 06329, 60996, 70347,
8K160, C5543, C5729
used on 001B
90A 120A NAS1291C3M . NUT V80205 032
OPT TO H42-3 15653
Optional Vendor Code 04795, 60119, C5543, C5729,
F0224
used on 001B
90A 130A NSA5030-4-12 . SCREW VF5442 004
ASNA2001V4-12 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001B
90A 140A NAS1149C0463R . WASHER V80205 020
Optional Vendor Code 04795, 60996, 8K160, C5543,
C5729
used on 001B
- ITEM NOT ILLUSTRATED

Page 10090A-2
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
90A 145A NAS1149C0463R . WASHER V80205 003
Optional Vendor Code 04795, 60996, 8K160, C5543,
C5729
used on 001B
90A 150A NAS1291C4M . NUT V80205 020
OPT TO 180003-5 60119
OPT TO PLH504M F0224
Optional Vendor Code 04795, C5543, C5729
used on 001B
90A 155A NAS1291C4M . NUT V80205 003
OPT TO 180003-5 60119
OPT TO PLH504M F0224
Optional Vendor Code 04795, C5543, C5729
used on 001B
90A 160A NSA5030-4-11 . SCREW VF5442 006
ASNA2001V4-11 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001B
90A 170A NSA5030-4-9 . SCREW VF5442 005
ASNA2001V4-9 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001B
90A 175A NSA5030-4-9 . SCREW VF5442 002
ASNA2001V4-9 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001B
90A 180A NSA5030-4-8 . SCREW VF5442 001
ASNA2001V4-8 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001B
90A 185A NSA5030-4-8 . SCREW VF5442 001
ASNA2001V4-8 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001B
90A 190A NSA5030-3-8 . SCREW VF5442 010
ASNA2001V3-8 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
- ITEM NOT ILLUSTRATED

Page 10090A-3
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 001B
90A 200A NSA5030-4-13 . SCREW VF5442 002
ASNA2001V4-13 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001B
90A 210A NAS1154-11 . SCREW V80205 002
Optional Vendor Code 04795, C5543, C5729
used on 001B
90A - 220B D52373110000CTD . STRUCTURE-DOOR VFAPE3 001
used on 001B
SEE 52-32-17-91A FOR DET
- ITEM NOT ILLUSTRATED

Page 10090A-4
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

40
A
160

170
A
B 180

C
20
10
30

140
150
100

140
150

110
120

110
120
100
C B
185 105
200
130
70 190
50
60

170
80

90
110 115
120 125

160

140
150
115
125

140
150

F_PL_523217_91_0_01_01

STRUCTURE-DOOR
Figure 91 / FIGURE-52-32-17-950-891-01

Page 10091-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
91 - 001A D52373110000CTD STRUCTURE-DOOR VFAPE3 RF
used on 220A (523217900)
SEE 52-32-17-900 FOR NHA
91 010A D5237311600200 . HINGE ASSY-MID VFAPE3 001
used on 001A
91 020A D5237311820200 .. HINGE-MID VFAPE3 001
used on 010A
91 030A D5237113820600 .. BUSHING VFAPE3 007
used on 010A
91 040A D5237113720600 .. BUSHING-SHOULDERED VFAPE3 004
used on 010A
91 050A D5237311500000 . HINGE ASSY-OUTER VFAPE3 001
used on 001A
91 060A D5237311720200 .. HINGE-OUTER VFAPE3 001
used on 050A
91 070A D5237113820600 .. BUSHING VFAPE3 006
used on 050A
91 080A D5237114720700 . FITTING-END VFAPE3 001
used on 001A
91 090A D5237277421800 . SHIM VFAPE3 001
selfrom, 01.60 MM (000.063 IN) THICK
used on 001A
91 - 091A D5237277420000 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 00.30 MM
(000.012 IN) THICK
used on 001A
91 - 092A D5237277420200 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 00.40 MM
(000.016 IN) THICK
used on 001A
91 - 093A D5237277420400 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 00.50 MM
(000.020 IN) THICK
used on 001A
91 - 094A D5237277420600 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 00.60 MM
(000.024 IN) THICK
used on 001A
91 - 095A D5237277420800 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 00.80 MM
(000.032 IN) THICK
- ITEM NOT ILLUSTRATED

Page 10091-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 001A
91 - 096A D5237277421000 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 01.00 MM
(000.040 IN) THICK
used on 001A
91 - 097A D5237277421200 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 01.20 MM
(000.047 IN) THICK
used on 001A
91 - 098A D5237277421400 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 01.40 MM
(000.055 IN) THICK
used on 001A
91 - 099A D5237277421600 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 01.50 MM
(000.059 IN) THICK
used on 001A
91 100A NSA5030-3-9 . SCREW VF5442 020
ASNA2001V3-9 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001A
91 105A NSA5030-3-9 . SCREW VF5442 002
ASNA2001V3-9 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001A
91 110A NAS1149C0363R . WASHER V80205 029
Optional Vendor Code 04795, 06329, 60996, 70347,
8K160, C5543, C5729
used on 001A
91 115A NAS1149C0363R . WASHER V80205 003
Optional Vendor Code 04795, 06329, 60996, 70347,
8K160, C5543, C5729
used on 001A
91 120A NAS1291C3M . NUT V80205 029
OPT TO H42-3 15653
Optional Vendor Code 04795, 60119, C5543, C5729,
F0224
used on 001A
91 125A NAS1291C3M . NUT V80205 003
OPT TO H42-3 15653
- ITEM NOT ILLUSTRATED

Page 10091-2
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
Optional Vendor Code 04795, 60119, C5543, C5729,
F0224
used on 001A
91 130A NSA5030-4-12 . SCREW VF5442 002
ASNA2001V4-12 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001A
91 140A NAS1149C0463R . WASHER V80205 023
Optional Vendor Code 04795, 60996, 8K160, C5543,
C5729
used on 001A
91 150A NAS1291C4M . NUT V80205 023
OPT TO 180003-5 60119
OPT TO PLH504M F0224
Optional Vendor Code 04795, C5543, C5729
used on 001A
91 160A NSA5030-4-11 . SCREW VF5442 012
ASNA2001V4-11 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001A
91 170A NSA5030-4-9 . SCREW VF5442 005
ASNA2001V4-9 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001A
91 180A NSA5030-3-8 . SCREW VF5442 009
ASNA2001V3-8 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001A
91 185A NSA5030-3-8 . SCREW VF5442 001
ASNA2001V3-8 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001A
91 190A NSA5030-4-13 . SCREW VF5442 002
ASNA2001V4-13 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001A
- ITEM NOT ILLUSTRATED

Page 10091-3
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
91 200A NAS1154-11 . SCREW V80205 002
Optional Vendor Code 04795, C5543, C5729
used on 001A
- ITEM NOT ILLUSTRATED

Page 10091-4
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

A
40
160

170
A
B 180

C
20
10
30

140
150
100

140
150

110
120

110
120
100

C B
175 165
200
130
70 190
50
60

170
80

90
110 145
120 155

160

140
150
145
155

140
150

F_PL_523217_91_A_01_01

STRUCTURE-DOOR
Figure 91A / FIGURE-52-32-17-950-891-A01

Page 10091A-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
91A - 001B D52373110000CTD STRUCTURE-DOOR VFAPE3 RF
used on 220B (52321790A)
SEE 52-32-17-90A FOR NHA
91A 010A D5237311600200 . HINGE ASSY-MID VFAPE3 001
used on 001B
91A 020A D5237311820200 .. HINGE-MID VFAPE3 001
used on 010A
91A 030A D5237113820600 .. BUSHING VFAPE3 007
used on 010A
91A 040A D5237113720600 .. BUSHING-SHOULDERED VFAPE3 004
used on 010A
91A 050B D5237311500000 . HINGE ASSY-OUTER VFAPE3 001
used on 001B
91A 060B D5237311720000 .. HINGE-OUTER VFAPE3 001
used on 050B
91A 070A D5237113820600 .. BUSHING VFAPE3 006
used on 050B
91A 080A D5237114720700 . FITTING-END VFAPE3 001
used on 001B
91A 090A D5237277421800 . SHIM VFAPE3 001
selfrom, 01.60 MM (000.063 IN) THICK
used on 001B
91A - 091A D5237277420000 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 00.30 MM
(000.012 IN) THICK
used on 001B
91A - 092A D5237277420200 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 00.40 MM
(000.016 IN) THICK
used on 001B
91A - 093A D5237277420400 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 00.50 MM
(000.020 IN) THICK
used on 001B
91A - 094A D5237277420600 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 00.60 MM
(000.024 IN) THICK
used on 001B
91A - 095A D5237277420800 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 00.80 MM
(000.032 IN) THICK
- ITEM NOT ILLUSTRATED

Page 10091A-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 001B
91A - 096A D5237277421000 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 01.00 MM
(000.040 IN) THICK
used on 001B
91A - 097A D5237277421200 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 01.20 MM
(000.047 IN) THICK
used on 001B
91A - 098A D5237277421400 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 01.40 MM
(000.055 IN) THICK
used on 001B
91A - 099A D5237277421600 . SHIM VFAPE3 AR
selfrom, FOR ADJUSTMENT ONLY, 01.50 MM
(000.059 IN) THICK
used on 001B
91A 100A NSA5030-3-9 . SCREW VF5442 020
ASNA2001V3-9 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001B
91A 110A NAS1149C0363R . WASHER V80205 029
Optional Vendor Code 04795, 06329, 60996, 70347,
8K160, C5543, C5729
used on 001B
91A 120A NAS1291C3M . NUT V80205 029
OPT TO H42-3 15653
Optional Vendor Code 04795, 60119, C5543, C5729,
F0224
used on 001B
91A 130A NSA5030-4-12 . SCREW VF5442 002
ASNA2001V4-12 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001B
91A 140A NAS1149C0463R . WASHER V80205 023
Optional Vendor Code 04795, 60996, 8K160, C5543,
C5729
used on 001B
- ITEM NOT ILLUSTRATED

Page 10091A-2
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
91A 145A NAS1149C0463R . WASHER V80205 003
Optional Vendor Code 04795, 60996, 8K160, C5543,
C5729
used on 001B
91A 150A NAS1291C4M . NUT V80205 023
OPT TO 180003-5 60119
OPT TO PLH504M F0224
Optional Vendor Code 04795, C5543, C5729
used on 001B
91A 155A NAS1291C4M . NUT V80205 003
OPT TO 180003-5 60119
OPT TO PLH504M F0224
Optional Vendor Code 04795, C5543, C5729
used on 001B
91A 160A NSA5030-4-11 . SCREW VF5442 012
ASNA2001V4-11 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001B
91A 165A NSA5030-4-11 . SCREW VF5442 002
ASNA2001V4-11 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001B
91A 170A NSA5030-4-9 . SCREW VF5442 005
ASNA2001V4-9 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001B
91A 175A NSA5030-4-9 . SCREW VF5442 001
ASNA2001V4-9 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001B
91A 180A NSA5030-3-8 . SCREW VF5442 009
ASNA2001V3-8 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
used on 001B
91A 190A NSA5030-4-13 . SCREW VF5442 002
ASNA2001V4-13 F5442
Optional Vendor Code 04795, C5543, C5729, D1283,
F0188, F6167, F7411, K5673, K8753
- ITEM NOT ILLUSTRATED

Page 10091A-3
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 001B
91A 200A NAS1154-11 . SCREW V80205 002
Optional Vendor Code 04795, C5543, C5729
used on 001B
- ITEM NOT ILLUSTRATED

Page 10091A-4
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

001A

10A 30A 40A 20A

50A 50A

001B

10B 30A 40A 20B

50A 50A

001C
001H

10C 20C

001D
001G

10D 30B 40B 20D

50B 50B

001E

10D 30C 40C 20E

50A 50A

001F

10E 20F

F_PL_523217_95_0_01_00

ROD ASSY
Figure 95 / FIGURE-52-32-17-950-895-01

Page 10095-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
95 - 001A R24359 ROD ASSY VB1395 RF
OPT TO D5237176820000 FAPE3
OPT TO D5237176820200 FAPE3
used on 160B (523217080)
SEE 52-32-17-080 FOR NHA
95 - 001B R24358 ROD ASSY VB1395 RF
OPT TO D5237176720000 FAPE3
OPT TO D5237176720200 FAPE3
OPT TO D5237176720400 FAPE3
used on 600B (523217080)
SEE 52-32-17-080 FOR NHA
95 - 001C R25257 ROD ASSY VB1395 RF
used on 080B (523217130)
SEE 52-32-17-130 FOR NHA
95 - 001D R25258 ROD ASSY VB1395 RF
used on 260B (523217130)
SEE 52-32-17-130 FOR NHA
95 - 001E R25261 ROD ASSY VB1395 RF
used on 060B (523217200)
SEE 52-32-17-200 FOR NHA
95 - 001F R25260 ROD ASSY VB1395 RF
used on 150B (523217200)
SEE 52-32-17-200 FOR NHA
95 - 001G R25256 ROD ASSY VB1395 RF
used on 010B (523217400)
SEE 52-32-17-400 FOR NHA
95 - 001H R25259 ROD ASSY VB1395 RF
used on 270B (523217130)
SEE 52-32-17-130 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, 001H
95 010D E5072-4SPL5K111 . CLEVIS VB1395 001
used on 001D, 001E, 001G
95 010E E4116-4S5-111 . CLEVIS VB1395 001
used on 001F
95 020A E5072-4S5K111 . ROD END VB1395 001
used on 001A
- ITEM NOT ILLUSTRATED

Page 10095-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
95 020B E5990-4S5K111 . ROD END VB1395 001
used on 001B
95 020C E4144 . ROD END VB1395 001
used on 001C, 001H
95 020D E5072-4SP5K111 . CLEVIS VB1395 001
used on 001D, 001G
95 020E NSA8143-04XRK . ROD END VF5442 001
OPT TO ART4ECRXWNSA C7239
Optional Vendor Code 66065, S0352
used on 001E
95 020F E4116-4S5-111 . CLEVIS VB1395 001
used on 001F
95 030A NAS509L5C . NUT V80205 001
Optional Vendor Code 01673, 04795, 06329, 60996,
8K160, 92595, C5543, C5729
used on 001A, 001B
95 030B NAS509L5 . NUT V80205 001
Optional Vendor Code 92595
used on 001D, 001G
95 030C NAS1423C5LH . NUT V80205 001
Optional Vendor Code 04795, 06329, 60996, 8K160,
C5543, C5729
used on 001E
95 040A NAS509-5C . NUT V80205 001
Optional Vendor Code 92595
used on 001A, 001B
95 040B NAS509-5 . NUT V80205 001
Optional Vendor Code 92595
used on 001D, 001G
95 040C NAS1423C5 . NUT V80205 001
Optional Vendor Code 04795, 06329, 60996, 8K160,
C5543, C5729
used on 001E
95 050A NAS1193K5C . LOCKING DEVICE V80205 002
Optional Vendor Code 04795, 06329, 17140, 70347,
C5543, C5729, H2776
used on 001A, 001B, 001E
95 050B NAS1193K5CP . LOCKING DEVICE V80205 002
Optional Vendor Code D8518
used on 001D, 001G
- ITEM NOT ILLUSTRATED

Page 10095-2
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

A B
C 40 A
120 B
80 A 60 A
140 B
B
A

E 70 A 20 A
210 150 B 100 B

30 A
110 B
50 A 40 A
130 B 120B
20 A
100 B

D C
190

170

F_PL_523217_96_0_01_00

BUSHING INSTL-DOOR STRUCTURE

Figure 96 / FIGURE-52-32-17-950-896-01

Page 10096-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
96 - 001A D5237311000063 BUSHING INSTL-DOOR STRUCTURE VFAPE3 RF
used on 140A (523217040)
SEE 52-32-17-040 FOR NHA
96 - 010A D5237311100060 . FRAME ASSY (NP) 001
used on 001A
96 020A D5237112920200 .. BUSHING VFAPE3 002
used on 001A
96 030A D5237111820000 .. BUSHING-SHOULDERED VFAPE3 002
used on 001A
96 040A D5237111620400 .. BUSHING-SHOULDERED VFAPE3 002
used on 001A
96 050A D5237112820200 .. BUSHING VFAPE3 001
used on 001A
96 060A D5237171720000 .. BUSHING-SHOULDERED VFAPE3 001
used on 001A
96 070A D5237111720000 .. BUSHING-SHOULDERED VFAPE3 002
used on 001A
96 080A D5237111820200 .. BUSHING-SHOULDERED VFAPE3 002
used on 001A
96 - 090A D5237311200060 . FRAME ASSY (NP) 001
used on 001A
96 100A D5237112920200 .. BUSHING VFAPE3 002
used on 001A
96 110A D5237111820000 .. BUSHING-SHOULDERED VFAPE3 002
used on 001A
96 120A D5237111620400 .. BUSHING-SHOULDERED VFAPE3 002
used on 001A
96 130A D5237112820200 .. BUSHING VFAPE3 001
used on 001A
96 140A D5237171720000 .. BUSHING-SHOULDERED VFAPE3 001
used on 001A
96 150A D5237111720000 .. BUSHING-SHOULDERED VFAPE3 002
used on 001A
96 - 160A D5237317100060 . BEAM-4 (NP) 001
used on 001A
96 170A NSA5054-3 .. INSERT VF5442 004
OPT TO K8000-3 K6405
OPT TO M45932-1-9AL 81349
used on 001A
96 - 180A D5237316800060 . BEAM-2A (NP) 001
used on 001A
- ITEM NOT ILLUSTRATED

Page 10096-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
96 190A D5237162320000 .. BUSHING-SHOULDERED VFAPE3 002
used on 001A
96 - 200A D5237316100060 . BEAM-3 (NP) 001
used on 001A
96 210A D5237162320000 .. BUSHING-SHOULDERED VFAPE3 002
used on 001A
96 - 220A D5237311000064 . BUSHING INSTL-DOOR STRUCTURE VFAPE3 001
used on 001A
SEE 52-32-17-970 FOR DET
- ITEM NOT ILLUSTRATED

Page 10096-2
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

E
A B
150 B
40 A
C D 110 B

60 A
130 B
B
A

A
70 20 A
B
140 90 B
E
260 30 A
100 B
50 A A
40
120 B B
110
20 A
90 B

210
C

D
230 200

170

190
240

F_PL_523217_97_0_01_00

BUSHING INSTL-DOOR STRUCTURE

Figure 97 / FIGURE-52-32-17-950-897-01

Page 10097-0
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
97 - 001A D5237311000064 BUSHING INSTL-DOOR STRUCTURE VFAPE3 RF
used on 220A (523217960)
SEE 52-32-17-960 FOR NHA
97 - 010A D5237311300060 . FRAME ASSY (NP) 001
used on 001A
97 020A D5237112920200 .. BUSHING VFAPE3 002
used on 001A
97 030A D5237111820000 .. BUSHING-SHOULDERED VFAPE3 002
used on 001A
97 040A D5237111620400 .. BUSHING-SHOULDERED VFAPE3 002
used on 001A
97 050A D5237112820200 .. BUSHING VFAPE3 001
used on 001A
97 060A D5237171720000 .. BUSHING-SHOULDERED VFAPE3 001
used on 001A
97 070A D5237111720000 .. BUSHING-SHOULDERED VFAPE3 002
used on 001A
97 - 080A D5237311400060 . FRAME ASSY (NP) 001
used on 001A
97 090A D5237112920200 .. BUSHING VFAPE3 002
used on 001A
97 100A D5237111820000 .. BUSHING-SHOULDERED VFAPE3 002
used on 001A
97 110A D5237111620400 .. BUSHING-SHOULDERED VFAPE3 002
used on 001A
97 120A D5237112820200 .. BUSHING VFAPE3 001
used on 001A
97 130A D5237171720000 .. BUSHING-SHOULDERED VFAPE3 001
used on 001A
97 140A D5237111720000 .. BUSHING-SHOULDERED VFAPE3 002
used on 001A
97 150A D5237179320000 .. BUSHING VFAPE3 001
used on 001A
97 - 160A D5237317700060 . SEGMENT-FRAME,FWD (NP) 001
used on 001A
97 170A D5237143420000 .. BUSHING-SHOULDERED VFAPE3 002
used on 001A
97 - 180A D5237317800060 . SEGMENT-FRAME,AFT (NP) 001
used on 001A
97 190A D5237178320200 .. BUSHING-SHOULDERED VFAPE3 001
used on 001A
- ITEM NOT ILLUSTRATED

Page 10097-1
52-32-17 Jul 01/16
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5237310000000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
97 200A D5237143420000 .. BUSHING-SHOULDERED VFAPE3 001
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 D5237317300060 . 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
97 - 250A D5237316200060 . BEAM-3 (NP) 001
used on 001A
97 260A D5237162320000 .. BUSHING-SHOULDERED VFAPE3 002
used on 001A
- ITEM NOT ILLUSTRATED

Page 10097-2
52-32-17 Jul 01/16