@AIRBUS

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

FAPE3

COMPONENT MAINTENANCE MANUAL

WITH
ILLUSTRATED PART LIST

MLG DOOR - TWO WHEEL BOGIE

PN : D5288000800000 D5288000800094
D5288000800095 D5288000800098
D5288000800100 D5288000800194
D5288000800195 D5288000800198
D5288000900000 D5288000900094
D5288000900095 D5288000900098
D5288000900100 D5288000900194
D5288000900195 D5288000900198
D5288001000000 D5288001000094
D5288001000095 D5288001000098
D5288001000100 D5288001000194
D5288001000195 D5288001000198

Issue: Aug 01/94 52-81-14 Rev: Jan 01/17

 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

HIGHLIGHTS

Revision No. 21 - Jan 01/17

LOCATIONS CHG DESCRIPTIONS OF CHANGE

CODE

HIGHLIGHTS
Page 1
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COMPONENT MAINTENANCE MANUAL
D5288000800000

LIST OF EFFECTIVE CONTENT

Revision No. 21 - Jan 01/17

CONTENT CHG LAST REVISION

CODE DATE
INTRODUCTION
TASK 52-81-14-871-802-A01 Jan 01/17

DESCRIPTION AND OPERATION

TASK 52-81-14-870-804-A01 Jan 01/17
FIGURE 52-81-14-991-010-A01 Jan 01/17
FIGURE 52-81-14-991-011-A01 Jan 01/17
TASK 52-81-14-870-804-B01 Jul 01/16
FIGURE 52-81-14-991-012-A01 Jul 01/16
FIGURE 52-81-14-991-013-A01 Jul 01/16
FIGURE 52-81-14-991-014-A01 Jul 01/16

TESTING AND FAULT ISOLATION

TASK 52-81-14-810-801-A01 Jan 01/17
Subtask 52-81-14-810-001-A01 Jan 01/17
Subtask 52-81-14-810-002-A01 Jan 01/17
FIGURE 52-81-14-991-003-A01 Jan 01/17
FIGURE 52-81-14-991-004-A01 Jan 01/17

DISASSEMBLY
TASK 52-81-14-000-801-A01 Jan 01/17
Subtask 52-81-14-000-015-A01 Jan 01/17
TASK 52-81-14-000-801-B01 Jan 01/17
Subtask 52-81-14-000-016-A01 Jan 01/17
Subtask 52-81-14-000-016-B01 Jan 01/17
TASK 52-81-14-000-804-A01 Jan 01/17
Subtask 52-81-14-000-001-A01 Jan 01/17
TASK 52-81-14-000-806-A01 Jan 01/17

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CONTENT CHG LAST REVISION

CODE DATE
Subtask 52-81-14-000-003-A01 Jan 01/17
TASK 52-81-14-000-807-A01 Jan 01/17
Subtask 52-81-14-000-004-A01 Jan 01/17
Subtask 52-81-14-000-004-B01 Jan 01/17
TASK 52-81-14-000-808-A01 Jan 01/17
Subtask 52-81-14-000-021-A01 Jan 01/17
TASK 52-81-14-000-809-A01 Jan 01/17
Subtask 52-81-14-000-023-A01 Jan 01/17
TASK 52-81-14-000-810-A01 Jan 01/17
Subtask 52-81-14-000-022-A01 Jan 01/17
TASK 52-81-14-000-811-A01 Jan 01/17
Subtask 52-81-14-000-018-A01 Jan 01/17
Subtask 52-81-14-000-019-A01 Jan 01/17
Subtask 52-81-14-000-019-B01 Jan 01/17
Subtask 52-81-14-000-019-C01 Jan 01/17
TASK 52-81-14-000-812-A01 Jan 01/17
Subtask 52-81-14-000-020-A01 Jan 01/17

CLEANING
TASK 52-81-14-100-801-A01 Jan 01/17
Subtask 52-81-14-100-001-A01 Jan 01/17
TASK 52-81-14-100-802-A01 Jan 01/17
Subtask 52-81-14-100-003-A01 Jan 01/17
Subtask 52-81-14-100-004-A01 Jan 01/17

INSPECTION/CHECK
TASK 52-81-14-210-801-A01 Jan 01/17
Subtask 52-81-14-210-002-A01 Jan 01/17
TASK 52-81-14-210-802-A01 Jan 01/17
Subtask 52-81-14-210-004-A01 Jan 01/17

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CONTENT CHG LAST REVISION

CODE DATE
Subtask 52-81-14-210-012-A01 Jan 01/17
Subtask 52-81-14-210-013-A01 Jan 01/17
Subtask 52-81-14-210-013-B01 Jan 01/17
Subtask 52-81-14-210-013-C01 Jan 01/17
Subtask 52-81-14-210-014-A01 Jan 01/17
TASK 52-81-14-210-803-A01 Jan 01/17
Subtask 52-81-14-210-006-A01 Jan 01/17
TASK 52-81-14-210-804-A01 Jan 01/17
Subtask 52-81-14-210-008-A01 Jan 01/17
Subtask 52-81-14-210-008-B01 Jan 01/17
Subtask 52-81-14-210-011-A01 Jan 01/17
TASK 52-81-14-210-805-A01 Jan 01/17
Subtask 52-81-14-210-010-A01 Jan 01/17
TASK 52-81-14-200-801-A01 Jan 01/17
Subtask 52-81-14-220-001-A01 Jan 01/17
TASK 52-81-14-200-802-A01 Jan 01/17
Subtask 52-81-14-220-003-A01 Jan 01/17
TASK 52-81-14-200-803-A01 Jan 01/17
Subtask 52-81-14-220-004-A01 Jan 01/17
TASK 52-81-14-200-804-A01 Jan 01/17
Subtask 52-81-14-200-001-A01 Jan 01/17

REPAIR
TASK 52-81-14-300-801-A01 Jan 01/17
Subtask 52-81-14-300-002-A01 Jan 01/17
TASK 52-81-14-300-807-A01 Jan 01/17
Subtask 52-81-14-350-001-A01 Jan 01/17
Subtask 52-81-14-350-002-A01 Jan 01/17
Subtask 52-81-14-350-003-A01 Jan 01/17

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CONTENT CHG LAST REVISION

CODE DATE
Subtask 52-81-14-350-004-A01 Jan 01/17
TASK 52-81-14-300-807-B01 Jan 01/17
Subtask 52-81-14-350-005-A01 Jan 01/17
Subtask 52-81-14-350-006-A01 Jan 01/17
Subtask 52-81-14-350-007-A01 Jan 01/17
Subtask 52-81-14-350-008-A01 Jan 01/17
TASK 52-81-14-300-807-C01 Jan 01/17
Subtask 52-81-14-350-009-A01 Jan 01/17
Subtask 52-81-14-350-010-A01 Jan 01/17
Subtask 52-81-14-350-011-A01 Jan 01/17
Subtask 52-81-14-350-012-A01 Jan 01/17
TASK 52-81-14-300-807-D01 Jan 01/17
Subtask 52-81-14-350-019-A01 Jan 01/17
Subtask 52-81-14-350-020-A01 Jan 01/17
TASK 52-81-14-300-810-A01 Jan 01/17
Subtask 52-81-14-300-039-A01 Jan 01/17
TASK 52-81-14-300-810-B01 Jan 01/17
Subtask 52-81-14-300-040-A01 Jan 01/17
TASK 52-81-14-300-810-C01 Jul 01/16
Subtask 52-81-14-300-035-A01 Jul 01/16
Subtask 52-81-14-300-035-B01 Jul 01/16
Subtask 52-81-14-300-035-C01 Jul 01/16
Subtask 52-81-14-300-035-D01 Jul 01/16
Subtask 52-81-14-300-035-E01 Jul 01/16
Subtask 52-81-14-300-035-F01 Jul 01/16
TASK 52-81-14-300-811-A01 Jan 01/17
Subtask 52-81-14-300-022-A01 Jan 01/17
TASK 52-81-14-300-812-A01 Jan 01/17
Subtask 52-81-14-300-024-A01 Jan 01/17

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COMPONENT MAINTENANCE MANUAL
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CONTENT CHG LAST REVISION

CODE DATE

ASSEMBLY
TASK 52-81-14-400-801-A01 Jan 01/17
Subtask 52-81-14-400-024-A01 Jan 01/17
TASK 52-81-14-400-802-A01 Jan 01/17
Subtask 52-81-14-400-025-A01 Jan 01/17
TASK 52-81-14-400-803-A01 Jan 01/17
Subtask 52-81-14-400-023-A01 Jan 01/17
TASK 52-81-14-400-804-A01 Jan 01/17
Subtask 52-81-14-410-004-A01 Jan 01/17
Subtask 52-81-14-410-004-B01 Jan 01/17
TASK 52-81-14-400-805-A01 Jan 01/17
Subtask 52-81-14-400-001-A01 Jan 01/17
FIGURE 52-81-14-991-005-A01 Jan 01/17
TASK 52-81-14-400-807-A01 Jan 01/17
Subtask 52-81-14-400-003-A01 Jan 01/17
TASK 52-81-14-400-808-A01 Jan 01/17
Subtask 52-81-14-400-016-A01 Jan 01/17
FIGURE 52-81-14-991-015-A01 Jan 01/17
FIGURE 52-81-14-991-016-A01 Jan 01/17
FIGURE 52-81-14-991-017-A01 Jan 01/17
TASK 52-81-14-400-808-B01 Jan 01/17
Subtask 52-81-14-400-022-A01 Jan 01/17
Subtask 52-81-14-400-022-B01 Jan 01/17
FIGURE 52-81-14-991-018-A01 Jan 01/17
FIGURE 52-81-14-991-019-A01 Jan 01/17
FIGURE 52-81-14-991-020-A01 Jan 01/17
FIGURE 52-81-14-991-021-A01 Jan 01/17
FIGURE 52-81-14-991-022-A01 Jan 01/17

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CONTENT CHG LAST REVISION

CODE DATE
TASK 52-81-14-400-809-A01 Jan 01/17
Subtask 52-81-14-400-012-A01 Jan 01/17
Subtask 52-81-14-400-012-B01 Jan 01/17
TASK 52-81-14-400-810-A01 Jan 01/17
Subtask 52-81-14-400-019-A01 Jan 01/17
Subtask 52-81-14-400-020-A01 Jan 01/17
Subtask 52-81-14-400-020-B01 Jan 01/17
Subtask 52-81-14-400-020-C01 Jan 01/17
FIGURE 52-81-14-991-023-A01 Jan 01/17
TASK 52-81-14-400-811-A01 Jan 01/17
Subtask 52-81-14-400-021-A01 Jan 01/17

FITS AND CLEARANCES

TASK 52-81-14-820-806-A01 Jan 01/17
FIGURE 52-81-14-991-006-A01 Jan 01/17
FIGURE 52-81-14-991-007-A01 Jan 01/17

STORAGE INCLUDING TRANSPORTATION

TASK 52-81-14-500-801-A01 Jan 01/17
Subtask 52-81-14-550-004-A01 Jan 01/17

ILLUSTRATED PARTS LIST

IPL Introduction
TASK 52-81-14-872-801-A01 Jan 01/17
VENDOR LIST Jan 01/17
Figure 01
FIGURE 52-81-14-991-801-001 Jan 01/17
Parts List Jan 01/17
Figure 01A
FIGURE 52-81-14-991-801-A01 Jan 01/17
Parts List Jan 01/17

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COMPONENT MAINTENANCE MANUAL
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CONTENT CHG LAST REVISION

CODE DATE
Figure 01B
FIGURE 52-81-14-991-801-B01 Jan 01/17
Parts List Jan 01/17
Figure 01C
FIGURE 52-81-14-991-801-C01 Jan 01/17
Parts List Jan 01/17
Figure 01D
FIGURE 52-81-14-991-801-D01 Jan 01/17
Parts List Jan 01/17
Figure 01E
FIGURE 52-81-14-991-801-E01 Jan 01/17
Parts List Jan 01/17
Figure 01F
FIGURE 52-81-14-991-801-F01 Jan 01/17
Parts List Jan 01/17
Figure 02
FIGURE 52-81-14-991-802-001 Jan 01/17
Parts List Jan 01/17
Figure 02A
FIGURE 52-81-14-991-802-A01 Jan 01/17
Parts List Jan 01/17
Figure 02B
FIGURE 52-81-14-991-802-B01 Jan 01/17
Parts List Jan 01/17
Figure 03
FIGURE 52-81-14-991-803-001 Jul 01/15
Parts List Jan 01/17
Figure 03B
FIGURE 52-81-14-991-803-B01 Jul 01/15

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COMPONENT MAINTENANCE MANUAL
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CONTENT CHG LAST REVISION

CODE DATE
Parts List Jan 01/17
Figure 03C
FIGURE 52-81-14-991-803-C01 Jul 01/15
Parts List Jan 01/17
Figure 04
FIGURE 52-81-14-991-804-001 Jan 01/17
Parts List Jan 01/17
Figure 04A
FIGURE 52-81-14-991-804-A01 Jul 01/15
Parts List Jan 01/17
Figure 04B
FIGURE 52-81-14-991-804-B01 Jul 01/15
Parts List Jan 01/17
Figure 04C
FIGURE 52-81-14-991-804-C01 Jul 01/15
Parts List Jan 01/17
Figure 04D
FIGURE 52-81-14-991-804-D01 Jan 01/17
Parts List Jan 01/17
Figure 05
FIGURE 52-81-14-991-805-001 Jan 01/17
Parts List Jan 01/17
Figure 05A
FIGURE 52-81-14-991-805-A01 Jul 01/15
Parts List Jan 01/17
Figure 05B
FIGURE 52-81-14-991-805-B01 Jan 01/17
Parts List Jan 01/17
Figure 05C

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COMPONENT MAINTENANCE MANUAL
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CONTENT CHG LAST REVISION

CODE DATE
FIGURE 52-81-14-991-805-C01 Jan 01/17
Parts List Jan 01/17
Figure 05D
FIGURE 52-81-14-991-805-D01 Jul 01/15
Parts List Jan 01/17
Figure 05E
FIGURE 52-81-14-991-805-E01 Jan 01/17
Parts List Jan 01/17
Figure 05F
FIGURE 52-81-14-991-805-F01 Jul 01/16
Parts List Jan 01/17
Figure 05G
FIGURE 52-81-14-991-805-G01 Jan 01/17
Parts List Jan 01/17
Figure 06
FIGURE 52-81-14-991-806-001 Jul 01/15
Parts List Jan 01/17
Figure 06A
FIGURE 52-81-14-991-806-A01 Jul 01/15
Parts List Jan 01/17
Figure 07
FIGURE 52-81-14-991-807-001 Jan 01/17
Parts List Jan 01/17
Figure 08
FIGURE 52-81-14-991-808-001 Jul 01/15
Parts List Jan 01/17

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COMPONENT MAINTENANCE MANUAL
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TABLE OF CONTENTS

INTRODUCTION
52-81-14-871-802-A01 Introduction

DESCRIPTION AND OPERATION

52-81-14-870-804-A01 Description and Operation
52-81-14-870-804-B01 Description and Operation

TESTING AND FAULT ISOLATION

52-81-14-810-801-A01 Fault Isolation of the Rear and Forward Fittings

DISASSEMBLY
52-81-14-000-801-A01 Disassembly of the FWD Fitting Assy
52-81-14-000-801-B01 Disassembly of the FWD Fitting Assy
52-81-14-000-804-A01 Disassembly of the Rear Fitting
52-81-14-000-806-A01 Disassembly of the Uplock Assy
52-81-14-000-807-A01 Disassembly of the Step Assy
52-81-14-000-808-A01 Disassembly of the Sensor Target
52-81-14-000-809-A01 Disassembly of the Tip Seal
52-81-14-000-810-A01 Disassembly of the Sealing Strips
52-81-14-000-811-A01 Disassembly of the Bushes
52-81-14-000-812-A01 Disassembly of the Bearings

CLEANING
52-81-14-100-801-A01 Cleaning of the Painted Components
52-81-14-100-802-A01 Cleaning of the Components Which Are Not Painted

INSPECTION/CHECK
52-81-14-210-801-A01 Check of the MLG Door Structure
52-81-14-210-802-A01 Check of the Fittings, the Uplock Assembly and the Lateral Ramp
52-81-14-210-803-A01 Check of the Step Assemblies
52-81-14-210-804-A01 Check of the Central Ramp and the Sensor-Support Assy
52-81-14-210-805-A01 Check of the Protective Treatment
52-81-14-200-801-A01 Check of the Tip Seal
52-81-14-200-802-A01 Check of the Sealing Strips
52-81-14-200-803-A01 Check of the Stops
52-81-14-200-804-A01 Check of the Identification Plates

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REPAIR
52-81-14-300-801-A01 Repair of the Surface Protection and Paint Coating
52-81-14-300-807-A01 Replacement of the Lateral Ramp and the Ramp Assy
52-81-14-300-807-B01 Replacement of the Lateral Ramp and the Ramp Assy
52-81-14-300-807-C01 Replacement of the Lateral Ramp and the Ramp Assy
52-81-14-300-807-D01 Replacement of the Lateral Ramp and the Ramp Assy
52-81-14-300-810-A01 Replacement of the Central Ramp
52-81-14-300-810-B01 Replacement of the Central Ramp
52-81-14-300-810-C01 Replacement of the Central Ramp
52-81-14-300-811-A01 Replacement of the Sensor-Support Assy
52-81-14-300-812-A01 Replacement of the Stops

ASSEMBLY
52-81-14-400-801-A01 Assembly of the Sealing Strips
52-81-14-400-802-A01 Assembly of the Tip Seal
52-81-14-400-803-A01 Assembly of the Sensor Targets
52-81-14-400-804-A01 Assembly of the Step Assemblies
52-81-14-400-805-A01 Assembly of the Uplock Assy
52-81-14-400-807-A01 Assembly of the Rear Fitting
52-81-14-400-808-A01 Assembly of the FWD Fitting Assy
52-81-14-400-808-B01 Assembly of the FWD Fitting Assy
52-81-14-400-809-A01 Assembly of the Identification Plates
52-81-14-400-810-A01 Assembly of the Bushes
52-81-14-400-811-A01 Assembly of the Bearings

FITS AND CLEARANCES

52-81-14-820-806-A01 Fits and Clearances

STORAGE INCLUDING TRANSPORTATION

52-81-14-500-801-A01 Material Storage Data

ILLUSTRATED PARTS LIST

52-81-14-872-801-A01 Introduction Illustrated Parts List (IPL)
VENDOR LIST
DETAILED PARTS LIST

T.O.C.
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COMPONENT MAINTENANCE MANUAL
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LIST OF SERVICE BULLETINS

SB No. REV MOD No. INCORP. DATE TITLE
No.
52-1022 02 22065G0112 may-1997 REINFORCEMENT OF MLG DOORS
52-1025 02 22140G0092, jul-2015 DOORS - MLG DOORS - COMMON
22141G0093, RAMP DEFINITION FOR 45, 46 AND 49
36642G0490 TIRE DIAMETERS
52-1073 05 24903G0258 jul-2015 MLG DOORS- INTRODUCE MODIFIED
ACTUATOR FITTING
52-1140 01 36997G0497 jul-2016 DOORS - MAIN GEAR DOORS -
REPLACE THE CENTRAL FREE FALL
RAMP TEFLON WITH TEFLON PAINT
TABLE 1

SBL
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COMPONENT MAINTENANCE MANUAL
D5288000800000

INTRODUCTION

**For PN’s ALL

TASK 52-81-14-871-802-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
ABP Airbus Process
ACMM Abbreviated Component Maintenance Manual
AEB Airline Engineering Bulletin
ASD Aero Space and Defence Industries Association of Europe
ATA Air Transport Association of America
ATLAS Abbreviated Test Language for All Systems
CMM Component Maintenance Manual
CMS Component Maintenance Sheet

INTRO
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COMPONENT MAINTENANCE MANUAL
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FIN Functional Item Number

IPC Illustrated Parts Catalog
IPL Illustrated Parts List
ID Inside Diameter
MFG Manufacturing
MFR Manufacturer
MOD Modification
MTOSS Maintenance Task Oriented Support System
NTF Non Textile Floor
OD Outside Diameter
PA Poly-Amide
PARA Paragraph
PC Poly-Carbonate
PMS Process and Materials Specification
PN Part Number
PTFE Polytetrafluoroethylene
PU Poly-Urethane
PV Poly-Venyl-Fluorite
SB Service Bulletin
SER NO Serial Number
SIL Service Information Letter
STE Simplified Technical English
SRM Structural Repair Manual
TBD To Be Determined
List of Abbreviations
TABLE 2

INTRO
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COMPONENT MAINTENANCE MANUAL
D5288000800000

DESCRIPTION AND OPERATION

**For PN’s D5288000800000 D5288000800100 D5288000900000 D5288000900100 D5288001000000

D5288001000100

TASK 52-81-14-870-804-A01
Description and Operation
1. General
A. This section tells you what the two wheel boogie main gear door is and what it does.
B. This section is about the left hand main gear door. The left hand main gear door and the right
hand main gear door are not interchangeable.
C. Technical Data APPROX:
Length 1712 mm (67.04 in)
Width 1826 mm (71.89 in)
Height 844.5 mm (33.248 in)
Weight 50.2 kg (110.672 lb)
Dimensions and Weight
TABLE 1

2. Description
The two wheel boogie main gear door has the primary components that follow:
PRE SB 52-1022
A. The two wheel boogie main gear door has the primary components that follow:

NOTE : See FIGURE 52-81-14-991-010-A.

- forward fitting with a hinge assy and the actuator fitting
- rear fitting with a hinge
- uplock assembly
- step assemblies
- lateral ramp with its supports
- central ramp with its supports
- sensor targets and supports
- cover assembly.
POST SB 52-1022
A. The two wheel boogie main gear door has the primary components that follow:

NOTE : See FIGURE 52-81-14-991-011-A.

- forward fitting with a hinge assy, the actuator fitting and a reinforcement plate
- rear fitting with a hinge

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- uplock assembly
- step assemblies
- lateral ramp with its supports
- central ramp with its supports
- sensor targets and supports
- cover assembly.
ALL VARIANTS
B. Not apply.
PRE SB 52-1022
C. The forward fitting assembly includes the actuator fitting and a hinge assy. They are made of
aluminum alloy. The forward fitting is attached to the cover assembly with nuts, washers,
screws, bolts and inserts. The hinge assy is attached to the forward fitting with nuts, washers
and screws. A spherical bearing is installed into the hinge assy. Two bushes are installed into the
actuator fitting.

NOTE : See FIGURE 52-81-14-991-010-A.

POST SB 52-1022
C. The forward fitting assembly includes the actuator fitting, a hinge assy and a reinforcement
plate. They are made of aluminum alloy. The forward fitting is attached to the cover assembly
with nuts, washers, screws, bolts and inserts. The hinge assy is attached to the forward fitting
with nuts, washers and screws. A spherical bearing is installed into the hinge assy. Two bushes
are installed into the actuator fitting. The reinforcement plate is attached to the cover assembly
and forward fitting with blind bolts and pin rivets.

NOTE : See FIGURE 52-81-14-991-011-A.

ALL VARIANTS
D. The rear fitting and the hinge are made of aluminum alloy. The fitting is attached to the cover
assembly with nuts, washers, screws, bolts and inserts. The hinge is attached to the rear fitting
with nuts, washers and screws. A bush is installed into the hinge. A lubrication fitting and a
flexible bearing are installed into the bush.
E. The uplock assembly has a fitting, a fluted plate and a mounting base which are made of
aluminum alloy and are attached with nuts, washers and screws. The uplock assembly is
attached to the cover assembly with bolts and inserts. A fluted plate is installed between the
uplock assembly and the cover assembly. The uplock mechanism has an arm with a roller that
turn around a torque shaft.
F. The step assembly and step are made of stainless steel and is attached to the cover assembly
with bolts and inserts. Protection plates are installed between the steps and the cover assembly.
G. The lateral ramp and its supports are made of aluminum alloy, TEFLON Sheets are bonded and
riveted to the ramp and HI-LOK fasteners attach the ramp to its supports. The lateral ramp and
its supports are attached to the cover assembly with rivets, bolts and inserts.

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H. The central ramp and its support are made of aluminum alloy. A TEFLON sheet is bonded and
riveted to the runout tip and HI-LOK fasteners attach the tip to its support. The runout tip and
its support are attached to the cover assembly with rivets, screws and inserts.
J. The two sensor targets are installed over supports. The supports are made of aluminum alloy
and are attached to the cover assembly with HI-LOK fasteners.
K. The cover assembly is made of honeycomb cores which have carbon fiber reinforced plastic
(CFRP) layers on both sides. The cover assembly has tip seals and sealing strips on the upper
and lower edges are attached to the cover with nuts, washers, screws and U-sections. The cover
assembly also has stops on the outer edges. The stops are made of polytetrafluoroethylene
(PTFE) and are attached to the cover with rivets.

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COMPONENT MAINTENANCE MANUAL
D5288000800000

**For PN’s D5288000800000 D5288000800100 D5288000900000 D5288000900100 D5288001000000

D5288001000100

HINGE

SENSOR TARGETS REAR FITTING

AND SUPPORT ASSEMBLIES

HINGE ASSY

STEPS ASSEMBLIES

FORWARD FITTING

LATERAL RAMP
WITH TEFLON SHEETS

CENTRAL RAMP
WITH TEFLON SHEETS

UPLOCK ASSEMBLY

COVER ASSEMBLY

L_CM_528114_1_0100101_01_00

Two Wheel Bogie Main Landing Gear Door

Two Wheel Bogie Main Landing Gear Door Components
FIGURE-52-81-14-991-010-A01

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COMPONENT MAINTENANCE MANUAL
D5288000800000

**For PN’s D5288000800000 D5288000800100 D5288000900000 D5288000900100 D5288001000000

D5288001000100

HINGE

SENSOR TARGETS REAR FITTING

AND SUPPORT ASSEMBLIES

HINGE ASSY

STEPS ASSEMBLIES

FORWARD FITTING

REINFORCEMENT
PLATE

LATERAL RAMP
WITH TEFLON SHEETS

CENTRAL RAMP
WITH TEFLON SHEETS

UPLOCK ASSEMBLY

COVER ASSEMBLY

L_CM_528114_1_0110101_01_00

Two Wheel Bogie Main Landing Gear Door

Two Wheel Bogie Main Landing Gear Door Components
FIGURE-52-81-14-991-011-A01

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COMPONENT MAINTENANCE MANUAL
D5288000800000

**For PN’s D5288000800094 D5288000800095 D5288000800098 D5288000800194 D5288000800195

D5288000800198 D5288000900094 D5288000900095 D5288000900098 D5288000900194 D5288000900195
D5288000900198 D5288001000094 D5288001000095 D5288001000098 D5288001000194 D5288001000195
D5288001000198

TASK 52-81-14-870-804-B01
Description and Operation
1. General
A. This section tells you what the two wheel boogie main gear door is and what it does.
B. This section is about the left hand main gear door. The left hand main gear door and the right
hand main gear door are not interchangeable.
C. Technical Data APPROX:
Length 1712 mm (67.04 in)
Width 1826 mm (71.89 in)
Height 844.5 mm (33.248 in)
Weight 50.2 kg (110.672 lb)
Dimensions and Weight
TABLE 1

2. Description

NOTE : See FIGURE 52-81-14-991-012-A.

PRE SB 52-1025 AND 52-1140
A. The two wheel boogie main gear door has the primary components that follow:
- forward fitting with a hinge assy, the actuator fitting and a reinforcement plate
- rear fitting with a hinge
- uplock assembly
- step assemblies
- lateral ramp with its supports
- central ramp with its supports
- sensor targets and supports
- cover assembly
B. The forward fitting assembly includes the actuator fitting, a hinge assy and a reinforcement
plate. They are made of aluminum alloy except the reinforcement plate, it is made of titanium.
The forward fitting is attached to the cover assembly with nuts, washers, screws, bolts and
inserts. The hinge assy is attached to the forward fitting with nuts, washers and screws. A
spherical bearing is installed into the hinge assy. Two bushes are installed into the actuator
fitting. The reinforcement plate is attached to the cover assembly and forward fitting with blind
bolts and pin rivets.

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C. The rear fitting and the hinge are made of aluminum alloy. The fitting is attached to the cover
assembly with nuts, washers, screws, bolts and inserts. The hinge is attached to the rear fitting
with nuts, washers and screws. A bush is installed into the hinge. A lubrication fitting and a
flexible bearing are installed into the bush.
D. The uplock assembly has a fitting, a fluted plate and a mounting base which are made of
aluminum alloy and are attached with nuts, washers and screws. The uplock assembly is
attached to the cover assembly with bolts and inserts. A fluted plate is installed between the
uplock assembly and the cover assembly. The uplock mechanism has an arm with a roller that
turn around a torque shaft.
E. The step assembly and step are made of stainless steel and is attached to the cover assembly
with bolts and inserts. Protection plates are installed between the steps and the cover assembly.
F. The lateral ramp and its supports are made of aluminum alloy, TEFLON Sheets are bonded and
riveted to the ramp and HI-LOK fasteners attach the ramp to its supports. The lateral ramp and
its supports are attached to the cover assembly with rivets, bolts and inserts.
G. The central ramp and its support are made of aluminum alloy. A TEFLON sheet is bonded and
riveted to the central ramp. The central ramp is attached to the cover assembly with rivets,
screws and inserts.
H. The two sensor targets are installed over supports. The supports are made of aluminum alloy
and are attached to the cover assembly with HI-LOK fasteners.
J. The cover assembly is made of honeycomb cores which have carbon fiber reinforced plastic
(CFRP) layers on both sides. The cover assembly has tip seals and sealing strips on the upper
and lower edges are attached to the cover with nuts, washers, screws and U-sections. The cover
assembly also has stops on the outer edges. The stops are made of polytetrafluoroethylene
(PTFE) and are attached to the cover with rivets.
K. Not apply.
POST SB 52-1025
A. The two wheel boogie main gear door has the primary components that follow:
- forward fitting with a hinge assy, the actuator fitting and a reinforcement plate
- rear fitting with a hinge
- uplock assembly
- step assemblies
- lateral ramp with its supports
- central ramp with its supports
- sensor targets and supports
- cover assembly
- podger assembly.

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B. The forward fitting assembly includes the actuator fitting, a hinge assy and a reinforcement
plate. They are made of aluminum alloy except the reinforcement plate, it is made of titanium.
The forward fitting is attached to the cover assembly with nuts, washers, screws, bolts and
inserts. The hinge assy is attached to the forward fitting with nuts, washers and screws. A
spherical bearing is installed into the hinge assy. Two bushes are installed into the actuator
fitting. The reinforcement plate is attached to the cover assembly and forward fitting with blind
bolts and pin rivets.
C. The rear fitting and the hinge are made of aluminum alloy. The fitting is attached to the cover
assembly with nuts, washers, screws, bolts and inserts. The hinge is attached to the rear fitting
with nuts, washers and screws. A bush is installed into the hinge. A lubrication fitting and a
flexible bearing are installed into the bush.
D. The uplock assembly has a fitting, a fluted plate and a mounting base which are made of
aluminum alloy and are attached with nuts, washers and screws. The uplock assembly is
attached to the cover assembly with bolts and inserts. A fluted plate is installed between the
uplock assembly and the cover assembly. The uplock mechanism has an arm with a roller that
turn around a torque shaft.
E. The step assembly and step are made of stainless steel and is attached to the cover assembly
with bolts and inserts. Protection plates are installed between the steps and the cover assembly.
F. The lateral ramp and its supports are made of aluminum alloy. The lateral ramp and its
supports are attached to the cover assembly with rivets, bolts and inserts.
G. The central ramp and its support are made of aluminum alloy. A TEFLON sheet is bonded and
riveted to the central ramp. The central ramp is attached to the cover assembly with rivets,
screws and inserts.
H. The two sensor targets are installed over supports. The supports are made of aluminum alloy
and are attached to the cover assembly with HI-LOK fasteners.
J. The cover assembly is made of honeycomb cores which have carbon fiber reinforced plastic
(CFRP) layers on both sides. The cover assembly has tip seals and sealing strips on the upper
and lower edges are attached to the cover with nuts, washers, screws and U-sections. The cover
assembly also has stops on the outer edges. The stops are made of polytetrafluoroethylene
(PTFE) and are attached to the cover with rivets.
K. The podger is a device made of alloy aluminum attached to the cover assembly. The Podger
may have to be adjusted when tires of a different size are fitted to the aircraft. A legend is
writing below the podger to indicated the correct height of the podger depending the tire
dimension installed on the aircraft.
POST SB 52-1140
A. The two wheel boogie main gear door has the primary components that follow:
- forward fitting with a hinge assy, the actuator fitting and a reinforcement plate
- rear fitting with a hinge
- uplock assembly

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- step assemblies
- lateral ramp with its supports
- central ramp with its supports
- sensor targets and supports
- cover assembly
- podger assembly.
B. The forward fitting assembly includes the actuator fitting, a hinge assy and a reinforcement
plate. They are made of aluminum alloy except the reinforcement plate, it is made of titanium.
The forward fitting is attached to the cover assembly with nuts, washers, screws, bolts and
inserts. The hinge assy is attached to the forward fitting with nuts, washers and screws. A
spherical bearing is installed into the hinge assy. Two bushes are installed into the actuator
fitting. The reinforcement plate is attached to the cover assembly and forward fitting with blind
bolts and pin rivets.
C. The rear fitting and the hinge are made of aluminum alloy. The fitting is attached to the cover
assembly with nuts, washers, screws, bolts and inserts. The hinge is attached to the rear fitting
with nuts, washers and screws. A bush is installed into the hinge. A lubrication fitting and a
flexible bearing are installed into the bush.
D. The uplock assembly has a fitting, a fluted plate and a mounting base which are made of
aluminum alloy and are attached with nuts, washers and screws. The uplock assembly is
attached to the cover assembly with bolts and inserts. A fluted plate is installed between the
uplock assembly and the cover assembly. The uplock mechanism has an arm with a roller that
turn around a torque shaft.
E. The step assembly and step are made of stainless steel and is attached to the cover assembly
with bolts and inserts. Protection plates are installed between the steps and the cover assembly.
F. The lateral ramp and its supports are made of aluminum alloy. The lateral ramp and its
supports are attached to the cover assembly with rivets, bolts and inserts.
G. The central ramp and its support are made of aluminum alloy. A TEFLON paint is applied to
the central ramp. The central ramp is attached to the cover assembly with rivets, screws and
inserts.
H. The two sensor targets are installed over supports. The supports are made of aluminum alloy
and are attached to the cover assembly with HI-LOK fasteners.
J. The cover assembly is made of honeycomb cores which have carbon fiber reinforced plastic
(CFRP) layers on both sides. The cover assembly has tip seals and sealing strips on the upper
and lower edges are attached to the cover with nuts, washers, screws and U-sections. The cover
assembly also has stops on the outer edges. The stops are made of polytetrafluoroethylene
(PTFE) and are attached to the cover with rivets.
K. The podger is a device made of alloy aluminum attached to the cover assembly. The Podger
may have to be adjusted when tires of a different size are fitted to the aircraft. A legend is
writing below the podger to indicated the correct height of the podger depending the tire
dimension installed on the aircraft.

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ALL VARIANTS
L. Not apply.

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**For PN’s D5288000800094 D5288000800095 D5288000800098 D5288000800194 D5288000800195

D5288000800198 D5288000900094 D5288000900095 D5288000900098 D5288000900194 D5288000900195
D5288000900198 D5288001000094 D5288001000095 D5288001000098 D5288001000194 D5288001000195
D5288001000198

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D5288000800000

HINGE

SENSOR TARGETS REAR FITTING

AND SUPPORT ASSEMBLIES

STEPS ASSEMBLIES

FORWARD FITTING

REINFORCEMENT
PLATE

LATERAL RAMP
WITH TEFLON SHEETS

CENTRAL RAMP
WITH TEFLON SHEETS

UPLOCK ASSEMBLY

COVER ASSEMBLY

L_CM_528114_1_0120101_01_00

Two Wheel Bogie Main Landing Gear Door

Two Wheel Bogie Main Landing Gear Door Components
FIGURE-52-81-14-991-012-A01

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D5288000800000

**For PN’s D5288000800094 D5288000800095 D5288000800098 D5288000800194 D5288000800195

D5288000800198 D5288000900094 D5288000900095 D5288000900098 D5288000900194 D5288000900195
D5288000900198 D5288001000094 D5288001000095 D5288001000098 D5288001000194 D5288001000195
D5288001000198

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D5288000800000

HINGE

SENSOR TARGETS REAR FITTING

AND SUPPORT ASSEMBLIES

HINGE ASSY
STEPS ASSEMBLIES

FORWARD FITTING

REINFORCEMENT
PLATE

LATERAL RAMP

DODGER ASSY

CENTRAL RAMP
WITH TEFLON SHEET

UPLOCK ASSEMBLY

L_CM_528114_1_0130101_01_00

Two Wheel Bogie Main Landing Gear Door

Two Wheel Bogie Main Landing Gear Door Components
FIGURE-52-81-14-991-013-A01

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D5288000800000

**For PN’s D5288000800094 D5288000800095 D5288000800098 D5288000800194 D5288000800195

D5288000800198 D5288000900094 D5288000900095 D5288000900098 D5288000900194 D5288000900195
D5288000900198 D5288001000094 D5288001000095 D5288001000098 D5288001000194 D5288001000195
D5288001000198

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D5288000800000

HINGE

SENSOR TARGETS REAR FITTING

AND SUPPORT ASSEMBLIES

HINGE ASSY
STEPS ASSEMBLIES

FORWARD FITTING

REINFORCEMENT
PLATE

LATERAL RAMP

DODGER ASSY

CENTRAL RAMP
WITH TEFLON PAINT

UPLOCK ASSEMBLY

L_CM_528114_1_0140101_01_00

Two Wheel Bogie Main Landing Gear Door

Two Wheel Bogie Main Landing Gear Door Components
FIGURE-52-81-14-991-014-A01

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TESTING AND FAULT ISOLATION

**For PN’s ALL

TASK 52-81-14-810-801-A01
Fault Isolation of the Rear and Forward Fittings
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A.
Referenced Information
REFERENCE DESIGNATION
TASK 52-81-14-000-806-A01 Disassembly of the Uplock Assembly
TASK 52-81-14-400-805-A01 Assembly of the Uplock Assembly
FIGURE 52-81-14-991-003-A FIGURE 52-81-14-991-003-A-Fittings
FIGURE 52-81-14-991-004-A FIGURE 52-81-14-991-004-A-Uplock Assembly
Referenced Information
TABLE 1

3. Procedure

Subtask 52-81-14-810-001-A01
A. Fault Isolation of the Rear and Forward Fittings

NOTE : See FIGURE 52-81-14-991-003-A.

(1) Fault Isolation of the rear and forward fittings .
FAULT POSSIBLE CAUSE CORRECTION
Remove and examine the
The rear hinge does not The flexible bearing (3) is flexible bearing (3) and the
(1) a
work correctly blocked bush (2). Replace the defective
parts. See TBD.
The forward hinge does The spherical bearing (1) is Remove and replace the
(2) a
not work correctly blocked spherical bearing (1). See TBD.
Fault Isolation of the Fittings Table
TABLE 2

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Subtask 52-81-14-810-002-A01
B. Fault Isolation of the Uplock Assembly

NOTE : See FIGURE 52-81-14-991-004-A.

NOTE : See TASK 52-81-14-000-806-A01 and TASK 52-81-14-400-805-A01 for the

replacement of the uplock assembly.
(1) Fault Isolation Table.
FAULT POSSIBLE CAUSE CORRECTION
Remove and examine the roller
The roller (4) does not
(1) (a) The roller (4) is blocked. (4) and the bushes (5). Replace
move smoothly.
the defective parts.
(a) The torque shaft (6) is bent. Replace the torque shaft (6).
The arm of the uplock Remove and examine the side
(2) assembly does not return The arm is blocked in the fittings (8 and 9) and the
to the neutral position. (b)
bushes (7). bushes (7). Replace the
defective parts.
The arm of the uplock (a) The torque shaft (6) is bent. Replace the torque shaft (6).
assembly does not move
(3)
10˚ from the neutral (b) The pin (10) is bent. Replace the pin (10).
position (under load),
Fault Isolation of the Uplock Assembly Table
TABLE 3

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**For PN’s ALL

3 2

F_CM_528114_1_0030101_01_00

Fittings
Fault Isolation of the Fittings
FIGURE-52-81-14-991-003-A01

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**For PN’s ALL

A
10

10

A
A

SECTION
A A
7 9

10 4

8 6 7

F_CM_528114_1_0040101_01_00

Uplock Assembly
Fault Isolation of the Uplock Assembly
FIGURE-52-81-14-991-004-A01

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DISASSEMBLY

**For PN’s D5288000800000 D5288000800095 D5288000800100 D5288000800195 D5288000900000

D5288000900095 D5288000900100 D5288000900195 D5288001000000 D5288001000095 D5288001000100
D5288001000195

TASK 52-81-14-000-801-A01
Disassembly of the FWD Fitting Assy
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
14QJB1 Wire-Locking diameter: 1.6 mm CRES Nickel Alloy -
Consumable Materials
TABLE 1

B. Fixtures, Tools, Test and Support Equipment

REFERENCE DESIGNATION
98D52109001000 Fitting Replacement Tool
Fixtures, Tools, Test and Support Equipment
TABLE 2

3. 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.

Subtask 52-81-14-000-015-A01
A. Disassembly of the FWD Fitting Assy
PRE SB 52-1022
(1) Disassembly of the hinge assy.

NOTE : See IPL_FIGURE_02.

NOTE : This procedure is applicable to the hinge assy 02-340.

(a) Install and calibrate the 98D52109001000 Fitting Replacement Tool on the door.

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(b) Remove and discard the cotter pins 02-240.

(c) Remove the nuts 02-250, the washers 02-260 and the bolt 02-270 from the FWD
fitting assy 02-200.
(d) Make sure that the diameter of the bolt 02-270, is in the limits between 6.32 and 6.34
mm (0.2490 and 0.2495 in), and that the diameter of the holes in the hinge assy
02-340 is in the limits between 6.31 and 6.35 mm (0.2484 and 0.2500 in).
(e) Remove the nuts 02-280, the washers 02-290 and the bolts 02-300, from the FWD
fitting assy 02-200.
(f) Make sure that the diameter of the bolts 02-300 is in the limits between 7.91 and
7.93 mm (0.3115 and 0.3120 in), and that the diameter of the holes in the hinge assy
02-340 is in the limits between 7.90 and 7.94 mm (0.3110 and 0.3126 in).
(g) Remove the nuts 02-310, the washers 02-320, the bolts 02-330 and the hinge assy
02-340, from the FWD fitting assy 02-200.
(h) Make sure that the diameter of the bolts 02-330 is in the limits between 9.50 and
9.51 mm (0.3740 and 0.3745 in), and that the diameter of the holes in the hinge assy
02-340 is in the limits between 9.49 and 9.53 mm (0.3736 and 0.3752 in). For
replacement for a new hinge assy 02-340, please contact AIRBUS.
(2) Disassembly of the FWD fitting assy.

NOTE : See IPL_FIGURE_02.

NOTE : This procedure is applicable to the FWD fitting assy 02-200.

(a) Remove and discard the cotter pins 02-010.
(b) Remove and discard the Material No. 14QJB1 Wire-Locking diameter: 1.6 mm CRES
Nickel Alloy - from the bolts 02-170.
(c) Remove the nut 02-020, the washer 02-030, the screw 02-040 and the bonding strap
02-050.
(d) Remove the nut 02-020, the washer 02-030, the bolt 02-150 and the profile 02-160.
(e) Remove the nuts 02-020, the washers 02-030, the bolts 02-170, the screws 02-190,
and the FWD fitting assy 02-200 from the cover assembly.
(f) Make sure that the diameter of the bolts 02-170 is in the limits between 6.32 and
6.34 mm (0.2490 and 0.2495 in), and that the diameter of the holes in the FWD
fitting assy 02-200 is 6.5 mm (0.256 in).
(g) Make sure that the diameter of the screws 02-190 is in the limits between 6.31 and
6.34 mm (0.2484 and 0.2495 in), and that the diameter of the holes in the FWD
fitting assy 02-200 is 6.6 mm (0.260 in). For replacement for a new FWD fitting assy
02-200, please contact AIRBUS.
POST SB 52-1022

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(1) Disassembly of the hinge assy.

NOTE : See IPL_FIGURE_02A.

NOTE : This procedure is applicable to the hinge assy 02A-610.

(a) Install and calibrate the 98D52109001000 Fitting Replacement Tool on the door.
(b) Remove and discard the cotter pins 02A-510.
(c) Remove the nuts 02A-520, the washers 02A-530 and the bolt 02A-540 from the FWD
fitting assy 02A-480.
(d) Make sure that the diameter of the bolt 02A-540, is in the limits between 6.32 and
6.34 mm (0.2490 and 0.2495 in), and that the diameter of the holes in the hinge assy
02A-610 is in the limits between 6.31 and 6.35 mm (0.2484 and 0.2500 in).
(e) Remove the nuts 02A-550, the washers 02A-560 and the bolts 02A-570 from the
FWD fitting assy 02A-480.
(f) Make sure that the diameter of the bolts 02A-570 is in the limits between 7.91 and
7.93 mm (0.3115 and 0.3120 in), and that the diameter of the holes in the hinge assy
02A-610 is in the limits between 7.90 and 7.94 mm (0.3110 and 0.3126 in).
(g) Remove the nuts 02A-580, the washers 02A-590, the bolt 02A-600 and the hinge assy
02A-610, from the FWD fitting assy 02A-480.
(h) Make sure that the diameter of the bolts 02A-600 is in the limits between 9.50 and
9.51 mm (0.3740 and 0.3745 in), and that the diameter of the holes in the hinge assy
02A-610 is in the limits between 9.49 and 9.53 mm (0.3736 and 0.3752 in). For
replacement for a new hinge assy 02A-610 , please contact AIRBUS.
(2) Disassembly of the FWD fitting assy.

NOTE : See IPL_FIGURE_02A.

NOTE : This procedure is applicable to the FWD fitting assy 02A-480.

(a) Remove and discard the cotter pins 02A-010.
(b) Remove and discard the Material No. 14QJB1 Wire-Locking diameter: 1.6 mm CRES
Nickel Alloy - from the bolts 02A-170.
(c) Remove the nut 02A-020, the washer 02A-030, the screw 02A-040 and the bonding
strap 02A-050.
(d) Remove the nut 02A-020, the washer 02A-030, the bolt 02A-150 and the profile
02A-160.
(e) Remove the nuts 02A-020, 02A-710, the washers 02A-030, the screws 02A-190 and
the bolts 02A-170, 02A-720, 02A-730, 02A-740, 02A-750.
(f) Remove the FWD fitting assy 02A-480 from the cover assembly.

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(g) Make sure that the diameter of the bolts 02A-170 is in the limits between 6.32 and
6.34 mm (0.2490 and 0.2495 in), and that the diameter of the holes in the FWD
fitting assy 02A-480 is 6.5 mm (0.256 in).
(h) Make sure that the diameter of the screws 02A-190 and the bolts 02A-720, 02A-730,
02A-740, 02A-750 is in the limits between 6.32 and 6.34 mm (0.2490 and 0.2495 in),
and that the diameter of the holes in the FWD fitting assy 02A-480 is 6.6 mm (0.260
in). For replacement for a new FWD fitting assy 02A-480, please contact AIRBUS.
ALL VARIANTS
(3) Not apply.

Page 3004
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COMPONENT MAINTENANCE MANUAL
D5288000800000

**For PN’s D5288000800094 D5288000800098 D5288000800194 D5288000800198 D5288000900094

D5288000900098 D5288000900194 D5288000900198 D5288001000094 D5288001000098 D5288001000194
D5288001000198

TASK 52-81-14-000-801-B01
Disassembly of the FWD Fitting Assy
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
14QJB1 Wire-Locking diameter: 1.6 mm CRES Nickel Alloy -
Consumable Materials
TABLE 1

B. Fixtures, Tools, Test and Support Equipment

REFERENCE DESIGNATION
98D52109001000 Fitting Replacement Tool
Fixtures, Tools, Test and Support Equipment
TABLE 2

C. Referenced Information
REFERENCE DESIGNATION
SRM 51-42-21
Referenced Information
TABLE 3

3. 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.

**For PN’s D5288000800094 D5288000800194 D5288000900094 D5288000900194 D5288001000094

Page 3005
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COMPONENT MAINTENANCE MANUAL
D5288000800000

D5288001000194

Subtask 52-81-14-000-016-A01
A. Disassembly of the FWD Fitting Assy
PRE SB 52-1022 AND SB 52-1073
(1) Disassembly of the hinge assy.

NOTE : See IPL_FIGURE_02.

NOTE : This procedure is applicable to the hinge assy 02-340.

(a) Install and calibrate the 98D52109001000 Fitting Replacement Tool on the door.
(b) Remove and discard the cotter pins 02-240.
(c) Remove the nuts 02-250, the washers 02-260 and the bolt 02-270 from the FWD
fitting assy 02-200.
(d) Make sure that the diameter of the bolt 02-270, is in the limits between 6.32 and 6.34
mm (0.2490 and 0.2495 in), and that the diameter of the holes in the hinge assy
02-340 is in the limits between 6.31 and 6.35 mm (0.2484 and 0.2500 in).
(e) Remove the nuts 02-280, the washers 02-290 and the bolts 02-300, from the FWD
fitting assy 02-200.
(f) Make sure that the diameter of the screws 02-300 is in the limits between 7.91 and
7.93 mm (0.3115 and 0.3120 in), and that the diameter of the holes in the hinge assy
02-340 is in the limits between 7.90 and 7.94 mm (0.3110 and 0.3126 in).
(g) Remove the nuts 02-310, the washers 02-320, the screws 02-330 and the hinge assy
02-340, from the FWD fitting assy 02-200.
(h) Make sure that the diameter of the screws 02-330 is in the limits between 9.50 and
9.51 mm (0.3740 and 0.3745 in), and that the diameter of the holes in the hinge assy
02-340 is in the limits between 9.49 and 9.53 mm (0.3736 and 0.3752 in). For
replacement for a new hinge assy 02-340, please contact AIRBUS.
(2) Disassembly of the FWD fitting assy.

NOTE : See IPL_FIGURE_02.

NOTE : This procedure is applicable to the FWD fitting assy 02-200.

(a) Remove and discard the cotter pins 02-010.
(b) Remove and discard the Material No. 14QJB1 Wire-Locking diameter: 1.6 mm CRES
Nickel Alloy - from the bolts 02-170.
(c) Remove the nut 02-020, the washer 02-030, the screw 02-040 and the bonding strap
02-050.
(d) Remove the nut 02-020, the washer 02-030, the bolt 02-150 and the profile 02-160.

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(e) Remove the nuts 02-020, the washers 02-030, the bolts 02-170, the screws 02-190,
and the FWD fitting assy 02-200 from the cover assembly.
(f) Make sure that the diameter of the bolts 02-170 is in the limits between 6.32 and
6.34 mm (0.2490 and 0.2495 in), and that the diameter of the holes in the FWD
fitting assy 02-200 is 6.5 mm (0.256 in).
(g) Make sure that the diameter of the screws 02-190 is in the limits between 6.31 and
6.34 mm (0.2484 and 0.2495 in), and that the diameter of the holes in the FWD
fitting assy 02-200 is 6.6 mm (0.260 in). For replacement for a new FWD fitting assy
02-200, please contact AIRBUS.
POST SB 52-1022
(1) Disassembly of the hinge assy.

NOTE : See IPL_FIGURE_02A.

NOTE : This procedure is applicable to the hinge assy 02A-610.

(a) Install and calibrate the 98D52109001000 Fitting Replacement Tool on the door.
(b) Remove and discard the cotter pins 02A-510.
(c) Remove the nuts 02A-520, the washers 02A-530 and the bolt 02A-540 from the FWD
fitting assy 02A-480.
(d) Make sure that the diameter of the bolt 02A-540, is in the limits between 6.32 and
6.34 mm (0.2490 and 0.2495 in), and that the diameter of the holes in the hinge assy
02A-610 is in the limits between 6.31 and 6.35 mm (0.2484 and 0.2500 in). For
replacement for a new hinge assy 02A-610, please contact AIRBUS.
(e) Remove the nuts 02A-550, the washers 02A-560 and the bolts 02A-570 from the
FWD fitting assy 02A-480.
(f) Make sure that the diameter of the bolts 02A-570 is in the limits between 7.91 and
7.93 mm (0.3115 and 0.3120 in), and that the diameter of the holes in the hinge assy
02A-610 is in the limits between 7.90 and 7.94 mm (0.3110 and 0.3126 in). For
replacement for a new hinge assy 02A-610, please contact AIRBUS.
(g) Remove the nuts 02A-580, the washers 02A-590, the screws 02A-600 and the hinge
assy 02A-610, from the FWD fitting assy 02A-480.
(h) Make sure that the diameter of the screws 02A-600 is in the limits between 9.50 and
9.51 mm (0.3740 and 0.3745 in), and that the diameter of the holes in the hinge assy
02A-610 is in the limits between 9.49 and 9.53 mm (0.3736 and 0.3752 in). For
replacement for a new hinge assy 02A-610, please contact AIRBUS.
(2) Disassembly of the FWD fitting assy.

NOTE : See IPL_FIGURE_02A.

NOTE : This procedure is applicable to the FWD fitting assy 02A-480.

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(a) Remove and discard the cotter pins 02A-010.

(b) Remove and discard the Material No. 14QJB1 Wire-Locking diameter: 1.6 mm CRES
Nickel Alloy - from the bolts 02A-170.
(c) Remove the nut 02A-020, the washer 02A-030, the screw 02A-040 and the bonding
strap 02A-050.
(d) Remove the nut 02A-020, the washer 02A-030, the bolt 02A-150 and the profile
02A-160.
(e) Remove the nuts 02A-020, 02A-710, the washers 02A-030, the screws 02A-190 and
the bolts 02A-170, 02A-720, 02A-730, 02A-740, 02A-750.
(f) Remove the FWD fitting assy 02A-480 from the cover assembly.
(g) Make sure that the diameter of the bolts 02A-170 is in the limits between 6.32 and
6.34 mm (0.2490 and 0.2495 in), and that the diameter of the holes in FWD fitting
assy 02A-480 is 6.5 mm (0.256 in).
(h) Make sure that the diameter of the screws 02A-190 and the bolts 02A-720, 02A-730,
02A-740, 02A-750 is in the limits between 6.32 and 6.34 mm (0.2490 and 0.2495 in),
and that the diameter of the holes in the FWD fitting assy 02A-480 is 6.6 mm (0.260
in). For replacement for a new FWD fitting assy 02A-480, please contact AIRBUS.
POST SB 52-1073
(1) Disassembly of the hinge assy.

NOTE : See IPL_FIGURE_02B.

NOTE : This procedure is applicable to the hinge assy 02B-340.

(a) Install and calibrate the 98D52109001000 Fitting Replacement Tool on the door.
(b) Remove and discard the cotter pins 02B-240.
(c) Remove the nuts 02B-260, the washers 02B-250, the bolts 02B-270, 02B-300, and the
hinge assy 02B-340 from the FWD fitting assy 02B-200.
(d) Make sure that the diameter of the bolts 02B-270, 02B-300, is in the limits between
9.50 and 9.54 mm (0..3740 and 0.3754 in), and that the diameter of the holes in the
hinge assy 02B-340 is in the limits between 9.49 and 9.53 mm (0.3736 and 0.3752
in). For replacement for a new hinge assy 02B-340, please contact AIRBUS.
(2) Disassembly of the FWD fitting assy.

NOTE : See IPL_FIGURE_02B.

NOTE : This procedure is applicable to the FWD fitting assy 02B-200.

(a) Remove and discard the cotter pins 02B-010.

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(b) Remove and discard the Material No. 14QJB1 Wire-Locking diameter: 1.6 mm CRES
Nickel Alloy - from the bolts 02B-170.
(c) Remove the nut 02B-020, the washer 02B-030, the screw 02B-040 and the bonding
strap 02B-050.
(d) Remove the rivet 02B-280 and the profile 02B-290 from the FWD fitting assy
02B-200. See SRM 51-42-21 for removal of the rivet 02B-280.
(e) Remove the bolts 02B-170.
(f) Remove the nuts 02B-020, the washer 02B-030 and the screws 02B-190.
(g) Remove the collar 02B-695 and the pin-rivets 02B-725, 02B-735, 02B-755. See SRM
51-42-21 for removal of the collar 02B-695 and the pin-rivets 02B-725, 02B-735,
02B-755.
(h) Make sure that the diameter of the bolts 02B-170 is in the limits between 6.32 and
6.34 mm (0.2490 and 0.2495 in), and that the diameter of the holes in the FWD
fitting assy 02B-200 is 6.5 mm (0.256 in).
(i) Make sure that the diameter of the screws 02B-190 is in the limits between 6.32 and
6.34 mm (0.2490 and 0.2495 in), and that the diameter of the holes in the FWD
fitting assy 02B-200 is 6.6 mm (0.260 in).
(j) Make sure that the diameter of the pin-rivets 02B-725, 02B-735, 02B-755 is in the
limits between 6.33 and 6.34 mm (0.2492 and 0.2495 in), and that the diameter of
the holes in the FWD fitting assy 02B-200 is 6.6 mm (0.260 in). For replacement for
a new FWD fitting assy 02B-200, please contact AIRBUS.
ALL VARIANTS
(3) Not apply.

**For PN’s D5288000800098 D5288000800198 D5288000900098 D5288000900198 D5288001000098

D5288001000198

Subtask 52-81-14-000-016-B01
B. Disassembly of the FWD Fitting Assy

NOTE : See IPL_FIGURE_02B.

(1) Disassembly of the hinge assy.

NOTE : This procedure is applicable to the hinge assy 02B-340.

(a) Install and calibrate the 98D52109001000 Fitting Replacement Tool on the door.
(b) Remove and discard the cotter pins 02B-240.
(c) Remove the nuts 02B-260, the washers 02B-250, the bolts 02B-270, 02B-300, and the
hinge assy 02B-340 from the FWD fitting assy 02B-200.

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(d) Make sure that the diameter of the bolts 02B-270, 02B-300, is in the limits between
9.50 and 9.54 mm (0..3740 and 0.3754 in), and that the diameter of the holes in the
hinge assy 02B-340 is in the limits between 9.49 and 9.53 mm (0.3736 and 0.3752
in). For replacement for a new hinge assy 02B-340, please contact AIRBUS.
(2) Disassembly of the FWD fitting assy.

NOTE : See IPL_FIGURE_02B.

NOTE : This procedure is applicable to the FWD fitting assy 02B-200..

(a) Remove and discard the cotter pins 02B-010.
(b) Remove and discard the Material No. 14QJB1 Wire-Locking diameter: 1.6 mm CRES
Nickel Alloy - from the bolts 02B-170.
(c) Remove the nut 02B-020, the washer 02B-030, the screw 02B-040 and the bonding
strap 02B-050.
(d) Remove the rivet 02B-280 and the profile 02B-290 from the FWD fitting assy
02B-200. See SRM 51-42-21 for removal of the rivet 02B-280..
(e) Remove the bolts 02B-170.
(f) Remove the nuts 02B-020, the washers 02B-030 and the screws 02B-190.
(g) Remove the collars 02B-695 and the pin-rivets 02B-725, 02B-735, 02B-755. See SRM
51-42-21 for removal of the collar 02B-695 and the pin-rivets 02B-725, 02B-735,
02B-755.
(h) Make sure that the diameter of the bolts 02B-170 is in the limits between 6.32 and
6.34 mm (0.2490 and 0.2495 in), and that the diameter of the holes in the FWD
fitting assy 02B-200 is 6.5 mm (0.256 in).
(i) Make sure that the diameter of the screws 02B-190 is in the limits between 6.32 and
6.34 mm (0.2490 and 0.2495 in), and that the diameter of the holes in the FWD
fitting assy 02B-200 is 6.6 mm (0.260 in).
(j) Make sure that the diameter of the pin-rivets 02B-725, 02B-735, 02B-755 is in the
limits between 6.33 and 6.34 mm (0.2492 and 0.2495 in), and that the diameter of
the holes in the FWD fitting assy 02B-200 is 6.6 mm (0.260 in). For replacement for
a new FWD fitting assy 02B-200, please contact AIRBUS.

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COMPONENT MAINTENANCE MANUAL
D5288000800000

**For PN’s ALL

TASK 52-81-14-000-804-A01
Disassembly of the Rear Fitting
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
14QJB1 Wire-Locking diameter: 1.6 mm CRES Nickel Alloy -
Consumable Materials
TABLE 1

B. Fixtures, Tools, Test and Support Equipment

REFERENCE DESIGNATION
98D52109001000 Fitting Replacement Tool
Fixtures, Tools, Test and Support Equipment
TABLE 2

C. Referenced Information
REFERENCE DESIGNATION
SRM 51-42-21
Referenced Information
TABLE 3

3. 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.

Subtask 52-81-14-000-001-A01
A. Disassembly of the Rear Fitting

NOTE : See IPL_FIGURE_07.

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(1) Disassembly of the hinge.

NOTE : This procedure is applicable to the hinge 07-250.

(a) Install and calibrate the 98D52109001000 Fitting Replacement Tool on the door.
(b) Remove and discard the cotter pins 07-210.
(c) Remove the nuts 07-220, the washers 07-230, the bolts 07-240 and the hinge 07-250
from the fitting 07-270.
(d) Make sure that the holes of the hinge 07-250 are in correct condition and the
diameter is between 6.31 mm (0.2484 in) and 6.35 mm (0.2500 in). For replacement
for a new hinge 07-250, please contact AIRBUS.
(e) Make sure that the diameter of the bolts 07-240 are in correct conditions between
6.32 mm (0.2490 in) and 6.34 mm (0.2495 in).
(2) Disassembly of the fitting.

NOTE : This procedure is applicable to the fitting 07-270.

(a) Remove and discard the cotter pins 07-010
(b) Remove and discard the Material No. 14QJB1 Wire-Locking diameter: 1.6 mm CRES
Nickel Alloy - from the bolts 07-150.
(c) Remove the nut 07-020, the washer 07-030, the bolt 07-040 and the bonding strap
07-050.
(d) Remove the nut 07-020, the washer 07-030, the bolt 07-130, the rivet 07-045 and the
profile 07-140. See SRM 51-42-21 for removal of the rivet 07-045.
(e) Remove the nuts 07-020, the washer 07-030, the screws 07-170, the bolts 07-150 and
the fitting 07-270 from the cover assembly.
(f) Make sure that the holes of the fitting 07-270 for the bolts 07-150 and 07-160 are in
correct conditions and the diameter is 6.5 mm (0.256 in). For replacement for a new
fitting 07-270, please contact AIRBUS.
(g) Make sure that the holes of the fitting 07-270 for the screws 07-170 are in correct
conditions and the diameter is 6.6 mm (0.260 in). For replacement for a new fitting
07-270, please contact AIRBUS.
(h) Make sure that the diameter of the bolts 07-150 and 07-160 are in correct conditions
between 6.32 mm (0.2488 in) and 6.34 mm (0.2496 in).
(i) Make sure that the diameter of the screws 07-170 are in correct conditions between
6.31 mm (0.2484 in) and 6.34 mm (0.2496 in).
(j) Make sure that the supplements between the fitting 07-270 and the cover assembly
are in correct condition.

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COMPONENT MAINTENANCE MANUAL
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**For PN’s ALL

TASK 52-81-14-000-806-A01
Disassembly of the Uplock Assy
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A.Referenced Information
REFERENCE DESIGNATION
TASK 52-81-14-210-802-A01 Check of the Fittings, the Uplock Assembly and the Lateral Ramp
TASK 52-81-14-810-801-A01 Fault Isolation of the Rear and Forward Fittings
Referenced Information
TABLE 1

3. 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.

Subtask 52-81-14-000-003-A01
A. Disassembly of the Uplock Assy

NOTE : See IPL_FIGURE_03, IPL_FIGURE_03B and IPL_FIGURE_03C.

NOTE : This procedure is applicable to the uplock assies 03-040, 03B-040 and 03C-040.

NOTE : See TASK 52-81-14-210-802-A01 and TASK 52-81-14-810-801-A01 for the necessary
level of the disassembly.
(1) Removal of the Roller 03-100.
(a) Remove and discard the cotter pin 03-060.
(b) Remove the nut 03-070, the washer 03-080, the bolt 03-090, and the roller with the
bushes.
(c) Remove the bushes 03-110 from the roller 03-100.
(d) Remove the lubrication fitting 03-050 from the bolt 03-090.
(2) Removal of the Torque Shaft 03-240.
(a) Remove the cotter pins 03-170 and discard.

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(b) Remove the nuts 03-180, the washers 03-190 and the protector cap 03-220 together
with the assembled torque shaft 03-240 from the mounting base 03-340.
(c) Remove and discard the cotter pin 03-060.
(d) Remove the torque shaft 03-240 from the protective cap 03-220.
(e) Remove the pin 03-210 from the mounting base 03-240.
(3) Removal of the Side Fittings 03-260 and 03-270.
(a) Remove and discard the cotter pins 03-120.
(b) Remove the nuts 03-130, the washers 03-140 and the screws 03-150 and 03-160.
(c) Remove the distance piece 03-250 from between the side fittings 03-260 and 03-270.
(d) Remove the side fittings 03-260 and 03-270 and the bushes 03-230, 03-280 from the
mounting base 03-340.
(4) Removal of the Fitting 03-320.
(a) Remove and discard the cotter pins 03-120.
(b) Remove the nuts 03-290, the washers 03-300, the bolts 03-310, the mounting base
03-340 and the fluted plate 03-330 from the fitting 03-320.
(c) Remove and discard the lockwire from the bolts 03-010.
(d) Remove the bolts 03-010, the fitting 03-320 and the fluted plate 03-030 from the
cover assembly.

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**For PN’s ALL

TASK 52-81-14-000-807-A01
Disassembly of the Step Assy
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
14QJB1 Wire-Locking diameter: 1.6 mm CRES Nickel Alloy -
Consumable Materials
TABLE 1

3. 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.

**For PN’s D5288000800000 D5288000800098 D5288000800100 D5288000800198 D5288000900000

D5288000900098 D5288000900100 D5288000900198 D5288001000000 D5288001000098
D5288001000100 D5288001000198

Subtask 52-81-14-000-004-A01
A. Disassembly of the Step Assy

NOTE : See IPL_FIGURE_03 and IPL_FIGURE_03B.

NOTE : This procedure is applicable to the step assies 03-370, 03B-370, 03-390 and 03B-390.
(1) Removal of the step assy 03-370.
(a) Remove and discard the Material No. 14QJB1 Wire-Locking diameter: 1.6 mm CRES
Nickel Alloy -.
(b) Remove the bolts 03-350 and 03-360.
(c) Remove the step assembly 03-370 and the protector 03-380 from the cover assembly.
(2) Removal of the step assy 03-390.
(a) Remove and discard the Material No. 14QJB1 Wire-Locking diameter: 1.6 mm CRES
Nickel Alloy -.
(b) Remove the bolts 03-360.

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(c) Remove the step 03-390 and the protection plate 03-400 from the cover assembly.

**For PN’s D5288000800094 D5288000800095 D5288000800194 D5288000800195 D5288000900094

D5288000900095 D5288000900194 D5288000900195 D5288001000094 D5288001000095
D5288001000194 D5288001000195

Subtask 52-81-14-000-004-B01
B. Disassembly of the Step Assy

NOTE : See IPL_FIGURE_03C.

NOTE : This procedure is applicable to the step assies 03C-370, 03C-390 and 03C-410.
(1) Removal of the step assy 03C-370.
(a) Remove and discard the Material No. 14QJB1 Wire-Locking diameter: 1.6 mm CRES
Nickel Alloy -.
(b) Remove the bolts 03C-350 and 03C-360.
(c) Remove the step assembly 03C-370 and the protector 03C-380 from the cover
assembly.
(2) Removal of the step assy 03C-390.
(a) Remove and discard the Material No. 14QJB1 Wire-Locking diameter: 1.6 mm CRES
Nickel Alloy -.
(b) Remove the bolts 03C-360.
(c) Remove the step 03C-390 and the protection plate 03C-400 from the cover assembly.
(3) Removal of the step assembly 03C-410.
(a) Remove and discard the Material No. 14QJB1 Wire-Locking diameter: 1.6 mm CRES
Nickel Alloy -.
(b) Remove the bolts 03C-360.
(c) Remove the step 03C-410 from the cover assembly.

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**For PN’s ALL

TASK 52-81-14-000-808-A01
Disassembly of the Sensor Target
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
REFERENCE DESIGNATION
non-metallic scraper
Fixtures, Tools, Test and Support Equipment
TABLE 1

3. Procedure

Subtask 52-81-14-000-021-A01
A. Disassembly of the Sensor Target

NOTE : See IPL_FIGURE_06 and IPL_FIGURE_06A.

NOTE : This procedure is applicable to the target 06-070 and 06A-070.

(1) Remove the nuts 06-040, the washers 06-050 and the screws 06-060.
(2) Remove the target 06-070.
(3) Remove the shim 06-080 from the sensor-support assy 06-030 with a non-metallic scraper.

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**For PN’s ALL

TASK 52-81-14-000-809-A01
Disassembly of the Tip Seal
1. Reason for the Job
This procedure is self-explanatory.
2. Procedure

Subtask 52-81-14-000-023-A01
A. Disassembly of the Tip Seal
PRE MOD 21295G0066
(1) Removal of the tip seal.

NOTE : See IPL_FIGURE_06.

NOTE : This procedure is applicable to the tip seal 06-290.

(a) Remove the nuts 06-240, the washers 06-250 and the screws 06-260.
(b) Remove the profile 06-270.
(c) Remove the tip seal 06-290 from the cover assy.
POST MOD 21295G0066
(1) Removal of the tip seal.

NOTE : See IPL_FIGURE_06A.

NOTE : This procedure is applicable to the tip seal 06A-290.

(a) Remove the nuts 06A-240, the washers 06A-250 and the screws 06A-260.
(b) Remove the profile 06A-270 and the shim 06A-285.
(c) Remove the tip seal 06A-290 from the cover assy.
ALL VARIANTS
(2) Not apply.

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**For PN’s ALL

TASK 52-81-14-000-810-A01
Disassembly of the Sealing Strips
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Referenced Information
REFERENCE DESIGNATION
SRM 51-42-21
Referenced Information
TABLE 1

3. Procedure

Subtask 52-81-14-000-022-A01
A. Disassembly of the Sealing Strips
PRE MOD 21295G0066
(1) Removal of the sealing strip.

NOTE : See IPL_FIGURE_06.

NOTE : This procedure is applicable to the sealing strips 06-130, 06-140 and 06-220.
(a) Remove the rivets 06-100. See SRM 51-42-21 for removal of the rivets 06-100.
(b) Remove the profile 06-110 and the sealing strip 06-130 from the cover assy.
POST MOD 21295G0066
(1) Removal of the sealing strip.

NOTE : See IPL_FIGURE_06A.

NOTE : This procedure is applicable to the sealing strips 06A-130, 06A-140 and 06A-220.
(a) Remove the nuts 06A-240, the washers 06A-250 and the screws 06A-260.
(b) Remove the profile 06A-110 and the sealing strip 06A-130 from the cover assy.
ALL VARIANTS
(2) Not apply.

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**For PN’s ALL

TASK 52-81-14-000-811-A01
Disassembly of the Bushes
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
REFERENCE DESIGNATION
non metallic scraper
Fixtures, Tools, Test and Support Equipment
TABLE 1

B. Referenced Information
REFERENCE DESIGNATION
TASK 52-81-14-000-804-A01 Disassembly of the Rear Fitting
TASK 52-81-14-000-806-A01 Disassembly of the Uplock Assembly
TASK 52-81-14-300-807-A01 Replacement of the Lateral Ramp and the Ramp Assy
TASK 52-81-14-300-807-B01 Replacement of the Lateral Ramp and the Ramp Assy
TASK 52-81-14-300-807-C01 Replacement of the Lateral Ramp and the Ramp Assy
Referenced Information
TABLE 2

3. Procedure

CAUTION : DO NOT STRESS THE FITTINGS WHEN YOU REMOVE THE OLD BUSHES.
STRESS WILL DAMAGE THE FITTING.

Subtask 52-81-14-000-018-A01
A. Disassembly of the Bushes
(1) Removal of the bushes of the FWD fitting assy.

NOTE : See IPL_FIGURE_02, IPL_FIGURE_02A and IPL_FIGURE_02B

NOTE : This procedure is applicable to the bushes 02-220, 02-230, 02A-495, 02A-500,
02B-220 and 02B-230.
(a) Remove the unwanted sealant from the bush 02-220 with a non metallic scraper.
(b) Push out the bush 02-220 from the FWD fitting assy 02-200 with a suitable tool.

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(2) Removal of the bushes of the rear fitting.

NOTE : See IPL_FIGURE_07.

NOTE : This procedure is applicable to the bush 07-260.

(a) If necessary remove the hinge 07-250. See TASK 52-81-14-000-804-A01.
(b) Remove the unwanted sealant from the bush 07-260 with a non metallic scraper .
(c) Push out the bush 07-260 from the hinge 07-250 with a suitable tool.
(3) Removal of the bushes of the uplock assy.

NOTE : See IPL_FIGURE_03, IPL_FIGURE_03B and IPL_FIGURE_03C.

NOTE : This procedure is applicable to the bushes 03-110, 03-230, 03-280, 03B-110,
03B-230, 03B-280, 03C-110, 03C-230 and 03C-280.
(a) Disassemble the uplock assy 03-040. See TASK 52-81-14-000-806-A01.
(b) Disassembly of the bushes of the base-mounting.

NOTE : This procedure is applicable to the bushes 03-230, 03-280, 03B-230,

03B-280, 03C-230 and 03C-280.
1 Remove the unwanted sealant from the bushes 03-230 and 03-280 with a non
metallic scraper .
2 Push out the bushes 03-230 and 03-280 from the from the base-mounting
03-340 with a suitable tool.
(c) Disassembly of the bushes of the roller.

NOTE : This procedure is applicable to the bushes 03-110, 03B-110 and 03C-110.
1 Remove the bushes 03-110 from the roller 03-100 with a suitable tool.

**For PN’s D5288000800098 D5288000800198 D5288000900098 D5288000900198 D5288001000098

D5288001000198

Subtask 52-81-14-000-019-A01
B. Disassembly of the Bushes of the Lateral Ramp
PRE SB 52-1025
(1) Not apply.
POST SB 52-1025
(1) Removal of the bushes.

NOTE : See IPL_FIGURE_04D.

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NOTE : This procedure is applicable to the bushes 04D-203.

(a) Remove the ramp assy 04D-190. See TASK 52-81-14-300-807-A01TASK
52-81-14-300-807-B01TASK 52-81-14-300-807-C01.
(b) Remove the unwanted sealant from the bush 04D-203 with a non metallic scraper.
(c) Push out the bush 04D-203 from the glider 04D-202 with a suitable tool.
ALL VARIANTS
(2) Not apply.

**For PN’s D5288000800094 D5288000800095 D5288000800194 D5288000800195 D5288000900094

D5288000900095 D5288000900194 D5288000900195 D5288001000094 D5288001000095
D5288001000194 D5288001000195

Subtask 52-81-14-000-019-B01
C. Disassembly of the Bushes of the Lateral Ramp
(1) Removal of the bushes.

NOTE : See IPL_FIGURE_04D.

NOTE : This procedure is applicable to the bushes 04D-203.

(a) Remove the ramp assy 04D-190. See TASK 52-81-14-300-807-D01.
(b) Remove the unwanted sealant from the bush 04D-203 with a non metallic scraper.
(c) Push out the bush 04D-203 from the glider 04D-202 with a suitable tool.

**For PN’s D5288000800000 D5288000800100 D5288000900000 D5288000900100 D5288001000000

D5288001000100

Subtask 52-81-14-000-019-C01
D. Disassembly of the Bushes of the Lateral Ramp
(1) Not apply.

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**For PN’s ALL

TASK 52-81-14-000-812-A01
Disassembly of the Bearings
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
REFERENCE DESIGNATION
98D52109001000 Fitting Replacement Tool
Fixtures, Tools, Test and Support Equipment
TABLE 1

B. Referenced Information
REFERENCE DESIGNATION
TASK 52-81-14-000-801-A01 Disassembly of the FWD Fitting Assy
TASK 52-81-14-000-801-B01 Disassembly of the FWD Fitting Assy
PMS 01-05-26
Referenced Information
TABLE 2

3. Procedure

Subtask 52-81-14-000-020-A01
A. Disassembly of the Bearings

NOTE : See IPL_FIGURE_02, IPL_FIGURE_02A and IPL_FIGURE_02B.

NOTE : This procedure is applicable to the spherical bearing 02-360, 02A-630 and 02B-360.
(1) Disassembly of the spherical bearing with the hinge assy.
(a) Install and calibrate the 98D52109001000 Fitting Replacement Tool on the door.
(b) Disassemble the hinge assy 02-340 from the forward fitting assy 02-200. See TASK
52-81-14-000-801-A01TASK 52-81-14-000-801-B01.
(c) Press out the spherical bearing 02-360 from the hinge assy 02-340. See PMS 01-05-26
for the replacement of the spherical bearing 02-360.

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CLEANING

**For PN’s ALL

TASK 52-81-14-100-801-A01
Cleaning of the Painted Components
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
14SBA1 Textile-Lint free Cotton -
08ABC1 Aqueous Cleaner-Aircraft Exterior Pressure Spraying -
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 SPECIFIED CLEANING MATERIALS AND SOLUTIONS OR THEIR

EQUIVALENTS. THE SURFACE PROTECTION COULD BE DAMAGED IF
UNSPECIFIED MATERIALS ARE USED. IT IS IMPORTANT THAT THE
MANUFACTURER’S MIXING, APPLICATION AND TREATMENT INSTRUCTIONS
ARE FOLLOWED.

Subtask 52-81-14-100-001-A01
A. Cleaning of the Painted Components
(1) Remove all loose dirt with a vacuum cleaner or a soft brush.
(2) Carefully remove the remaining sealant and dirt with a non-metallic scraper .

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(3) Clean the component with a soft brush or with a Material No. 14SBA1 Textile-Lint free
Cotton - soaked with Material No. 08ABC1 Aqueous Cleaner-Aircraft Exterior Pressure
Spraying -.
(4) Flush the component with clean water to remove the detergent.
(5) Dry the component with a hot-air blower or with a Material No. 14SBA1 Textile-Lint free
Cotton -.

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**For PN’s ALL

TASK 52-81-14-100-802-A01
Cleaning of the Components Which Are Not Painted
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
14SBA1 Textile-Lint free Cotton -
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
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 SPECIFIED CLEANING MATERIALS AND SOLUTIONS OR THEIR

EQUIVALENTS. THE SURFACE PROTECTION COULD BE DAMAGED IF
UNSPECIFIED MATERIALS ARE USED. IT IS IMPORTANT THAT THE
MANUFACTURER’S MIXING, APPLICATION AND TREATMENT INSTRUCTIONS
ARE FOLLOWED.

Subtask 52-81-14-100-003-A01
A. Cleaning of the Components Which Are Not Painted
(1) Remove the loose dirt from the component with a vacuum cleaner or a soft brush.
(2) Carefully remove the remaining dirt with a non-metallic scraper .
(3) Clean the components which are not painted with a soft brush or with a Material No.
14SBA1 Textile-Lint free Cotton - soaked with Material No. 08BBF1 Non Aqueous
Cleaner-- Methyl-Ethyl-Ketone -.

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(4) Dry the component with a hot-air blower or with a Material No. 14SBA1 Textile-Lint free
Cotton -.

Subtask 52-81-14-100-004-A01
B. Cleaning of the Bonding Points
(1) Remove the unwanted grease, oil or other contamination from the mating surfaces as
follows:
(a) Remove the loose dirt from the components with a vacuum cleaner or a soft brush.
(b) Carefully remove the remaining dirt with a non-metallic scraper.
(c) Clean the components which are not painted with a soft brush or with a Material No.
14SBA1 Textile-Lint free Cotton - soaked with Material No. 08BBF1 Non Aqueous
Cleaner-- Methyl-Ethyl-Ketone -.
(d) Dry the components with a hot-air blower or with a Material No. 14SBA1 Textile-Lint
free Cotton -.
(2) Make sure that the bonding area is between 2 mm (0.08 in) and 4 mm (0.16 in) larger
than the diameter of the mating surfaces.
(3) Abrade the bonding area with abrasive cloth, 120 grade .
(4) Clean the working area with a vacuum cleaner.

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INSPECTION/CHECK

**For PN’s ALL

TASK 52-81-14-210-801-A01
Check of the MLG Door Structure
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Referenced Information
REFERENCE DESIGNATION
SRM 52-81-14
Referenced Information
TABLE 1

3. Procedure

Subtask 52-81-14-210-002-A01
A. Check of the MLG Door Structure
(1) Examine the cover assembly for damage.
(2) See SRM 52-81-14, Page Block 101 Config. 1, 2 and 3 for allowable damage limits.

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**For PN’s ALL

TASK 52-81-14-210-802-A01
Check of the Fittings, the Uplock Assembly and the Lateral Ramp
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Referenced Information
REFERENCE DESIGNATION
TASK 52-81-14-000-801-A01 Disassembly of the FWD Fitting Assy
TASK 52-81-14-000-801-B01 Disassembly of the FWD Fitting Assy
TASK 52-81-14-400-808-A01 Assembly of the FWD Fitting Assy
TASK 52-81-14-400-808-B01 Assembly of the FWD Fitting Assy
TASK 52-81-14-000-804-A01 Disassembly of the Rear Fitting
TASK 52-81-14-400-807-A01 Assembly of the Rear Fitting
TASK 52-81-14-000-811-A01 Disassembly of the Bushes
TASK 52-81-14-400-810-A01 Assembly of the Bushes
TASK 52-81-14-000-812-A01 Disassembly of the Bearings
TASK 52-81-14-400-811-A01 Assembly of the Bearings
TASK 52-81-14-300-807-A01 Replacement of the Lateral Ramp and the Ramp Assy
TASK 52-81-14-300-807-B01 Replacement of the Lateral Ramp and the Ramp Assy
TASK 52-81-14-300-807-C01 Replacement of the Lateral Ramp and the Ramp Assy
TASK 52-81-14-300-807-D01 Replacement of the Lateral Ramp and the Ramp Assy
TASK 52-81-14-000-806-A01 Disassembly of the Uplock Assembly
TASK 52-81-14-400-805-A01 Assembly of the Uplock Assembly
TASK 52-81-14-820-806-A01 Fits and Clearances
NTM 52-81-14
SRM 51-22-00
SRM 51-11-00
Referenced Information
TABLE 1

3. Procedure

Subtask 52-81-14-210-004-A01
A. Check of the FWD Fitting Assy

NOTE : See IPL_FIGURE_02, IPL_FIGURE_02A and IPL_FIGURE_02B.

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(1) Examine the FWD fitting assy.

NOTE : This procedure is applicable to the FWD fitting assies 02-200, 02A-480, 02B-200.
- Cracks
- Corrosion
- Lockwire
- Other damages.
(a) Do an approved non-destructive test if you think that there is a crack that you cannot
see clearly. See NTM 52-81-14.
(b) Cracks are not permitted. For replacement for a new FWD fitting assy 02-200, please
contact AIRBUS.
(c) For the removal of the corrosion on the FWD fitting assy 02-200, see SRM 51-22-00.
(d) Examine the lockwire of the screws. In case it has lost its use, replace it. See TASK
52-81-14-000-801-A01TASK 52-81-14-000-801-B01 and TASK 52-81-14-400-808-
A01TASK 52-81-14-400-808-B01.
(e) Other damages. See SRM 51-11-00 for damage classification.
(f) See TASK 52-81-14-000-801-A01TASK 52-81-14-000-801-B01 and TASK
52-81-14-400-808-A01TASK 52-81-14-400-808-B01 for the disassembly and assembly
of the FWD fitting assy 02-200.
(g) Examine the bushes 02-220 and 02-230 for damages.
1 See TASK 52-81-14-820-806-A01 for the permitted limits.
2 For the removal of the corrosion, see SRM 51-22-00.
3 Other damage is not permitted on the bushes 02-220 and 02-230.
4 See TASK 52-81-14-000-811-A01 and TASK 52-81-14-400-810-A01 for the
disassembly and assembly of the bushes 02-220 and 02-230.
(2) Examine the hinge assy.

NOTE : This procedure is applicable to the hinge assy 02-340, 02A-610 and 02B-340.
- Cracks
- Corrosion
- Other damages.
(a) Do an approved non-destructive test if you think that there is a crack that you cannot
see clearly. See NTM 52-81-14.
(b) Cracks are not permitted. For replacement for a new hinge assy 02-340, please
contact AIRBUS.
(c) For the removal of the corrosion on the hinge assy 02-340, see SRM 51-22-00.
(d) Other damages. See SRM 51-11-00 for damage classification.

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(e) See TASK 52-81-14-000-801-A01TASK 52-81-14-000-801-B01 and TASK

52-81-14-400-808-A01TASK 52-81-14-400-808-B01 for the disassembly and assembly
of the hinge assy 02-340.
(f) Examine the bearing 02-360 for damage.
1 Examine the correct installation of the bearing 02-360 in the hinge assy 02-340.
2 See TASK 52-81-14-820-806-A01 for the permitted limits.
3 For the removal of the corrosion, see SRM 51-22-00.
4 Other damage is not permitted on the bearings.
5 See TASK 52-81-14-000-812-A01 and TASK 52-81-14-400-811-A01 for the
disassembly and assembly of the bearing 02-360.
(3) Examine the bonding strap 02-050 for lacquer layer, incorrect attachment, torsion or
corrosion.
(a) Lacquer layer, incorrect attachment, torsion or corrosion are not permitted.
(b) For the replacement of the damaged bonding strap 02-050, see TASK
52-81-14-000-801-A01TASK 52-81-14-000-801-B01 and TASK 52-81-14-400-808-
A01TASK 52-81-14-400-808-B01.

Subtask 52-81-14-210-012-A01
B. Check of the Rear Fitting

NOTE : See IPL_FIGURE_07.

(1) Examine the fitting.

NOTE : This procedure is applicable to the fitting 07-270.

- Cracks
- Corrosion
- Lockwire
- Other damages.
(a) Do an approved non-destructive test if you think that there is a crack that you cannot
see clearly. See NTM 52-81-14.
(b) Cracks are not permitted. For replacement for a new fitting 07-270, please contact
AIRBUS.
(c) Remove the corrosion on the fitting 07-270. See SRM 51-22-00.
(d) Examine the lockwire of the screws. In case it has lost its use, replace it. See TASK
52-81-14-000-804-A01 and TASK 52-81-14-400-807-A01.
(e) Other damages. See SRM 51-11-00 for damage classifications.
(f) See TASK 52-81-14-000-804-A01 and TASK 52-81-14-400-807-A01 for the
disassembly and assembly of the fitting 07-270.

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(2) Examine the hinge.

NOTE : This procedure is applicable to the hinge 07-250.

- Cracks
- Corrosion
- Other damages.
(a) Do an approved non-destructive test if you think that there is a crack that you cannot
see clearly. See NTM 52-81-14.
(b) Cracks are not permitted. For replacement for a new hinge 07-250, please contact
AIRBUS.
(c) For the removal of the corrosion on the hinge 07-250. See SRM 51-22-00.
(d) Other damages. See SRM 51-11-00 for damage classifications.
(e) See TASK 52-81-14-000-804-A01 and TASK 52-81-14-400-807-A01 for the
disassembly and assembly of the hinge 07-250.
(f) Examine the bush 07-260 for damage.
1 Examine the correct installation of the bush 07-260 in the hinge 07-250.
2 See TASK 52-81-14-820-806-A01 for the permitted limits.
3 For the removal of the corrosion. See SRM 51-22-00.
4 Other damage is not permitted on the bushes.
5 See TASK 52-81-14-000-811-A01 and TASK 52-81-14-400-810-A01 for the
disassembly and assembly of the bush 07-260.
(3) Examine the bonding strap 07-050 for lacquer layer, incorrect attachment, torsion or
corrosion.
(a) Lacquer layer, incorrect attachment, torsion or corrosion are not permitted.
(b) Replace the damaged bonding strap 07-050. See TASK 52-81-14-000-811-A01 and
TASK 52-81-14-400-810-A01.

**For PN’s D5288000800000 D5288000800100 D5288000900000 D5288000900100 D5288001000000

D5288001000100

Subtask 52-81-14-210-013-A01
C. Check of the Lateral Ramp and the Ramp Assy
(1) Examine the lateral ramp for:

NOTE : See IPL_FIGURE_04, IPL_FIGURE_04A, IPL_FIGURE_04B and

IPL_FIGURE_04C.

NOTE : This procedure is applicable to the lateral ramp.

- Cracks

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- Corrosion
- Lockwire
- Other damages.
(a) Cracks, corrosion and other damages.
1 Do an approved non-destructive test if you think that there is a crack that you
cannot see clearly. See NTM 52-81-14.
2 Cracks are not permitted. For replacement for a new lateral ramp, please contact
AIRBUS.
3 For the removal of the corrosion on the fittings of the lateral ramp, see SRM
51-22-00.
4 Examine the lockwire of the screws. In case it has lost its use, replace it. See
TASK 52-81-14-300-807-A01TASK 52-81-14-300-807-B01TASK
52-81-14-300-807-C01TASK 52-81-14-300-807-D01.
5 Other damages see SRM 51-11-00 for damage classification.
6 See TASK 52-81-14-300-807-A01TASK 52-81-14-300-807-B01TASK
52-81-14-300-807-C01TASK 52-81-14-300-807-D01 for assembly and
disassembly of the lateral ramp.
7 Examine the teflon sheets of the lateral ramp for cracks and incorrect
attachment.

NOTE : This procedure is applicable to the teflon sheets 04-050, 04-070,

04A-050, 04A-070, 04B-050, 04B-070, 04C-050 and 04C-070.
a Cracks and incorrect attachment are not permitted on the teflon sheets.
b See TASK 52-81-14-300-807-A01TASK 52-81-14-300-807-B01TASK
52-81-14-300-807-C01TASK 52-81-14-300-807-D01 for assembly and
disassembly of the teflon sheets.
(2) Examine the ramp assy for:
(a) Not apply.

**For PN’s D5288000800094 D5288000800095 D5288000800194 D5288000800195 D5288000900094

D5288000900095 D5288000900194 D5288000900195 D5288001000094 D5288001000095
D5288001000194 D5288001000195

Subtask 52-81-14-210-013-B01
D. Check of the Lateral Ramp and the Ramp Assy
(1) Examine the lateral ramp for:
(a) Not apply.

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(2) Examine the ramp assy for:

NOTE : See IPL_FIGURE_04D.

NOTE : This procedure is applicable to the ramp assy 04D-190.

- Cracks
- Lockwire
- Corrosion
- Other damages.
(a) Cracks, corrosion and other damages.
1 Do an approved non-destructive test if you think that there is a crack that you
cannot see clearly. See NTM 52-81-14.
2 Cracks are not permitted. For replacement for a new ramp assy 04D-190, please
contact AIRBUS.
3 For the removal of the corrosion on the fittings of the ramp assy 04D-190, see
SRM 51-22-00.
4 Examine the lockwire of the screws. In case it has lost its use, replace it. See
TASK 52-81-14-300-807-D01.
5 Other damages see SRM 51-11-00 for damage classification.
6 See TASK 52-81-14-300-807-D01 for assembly and disassembly of the ramp assy
04D-190.

**For PN’s D5288000800098 D5288000800198 D5288000900098 D5288000900198 D5288001000098

D5288001000198

Subtask 52-81-14-210-013-C01
E. Check of the Lateral Ramp and the Ramp Assy
PRE SB 52-1025
(1) Examine the lateral ramp for:

NOTE : See IPL_FIGURE_04, IPL_FIGURE_04A, IPL_FIGURE_04B and

IPL_FIGURE_04C.

NOTE : This procedure is applicable to the lateral ramp.

- Cracks
- Corrosion
- Lockwire
- Other damages.

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(a) Cracks, corrosion and other damages.

1 Do an approved non-destructive test if you think that there is a crack that you
cannot see clearly. See NTM 52-81-14.
2 Cracks are not permitted. For replacement for a new lateral ramp, please contact
AIRBUS.
3 For the removal of the corrosion on the fittings of the lateral ramp, see SRM
51-22-00.
4 Examine the lockwire of the screws. In case it has lost its use, replace it. See
TASK 52-81-14-300-807-A01TASK 52-81-14-300-807-B01TASK
52-81-14-300-807-C01TASK 52-81-14-300-807-D01.
5 Other damages see SRM 51-11-00 for damage classification.
6 See TASK 52-81-14-300-807-A01TASK 52-81-14-300-807-B01TASK
52-81-14-300-807-C01TASK 52-81-14-300-807-D01 for assembly and
disassembly of the lateral ramp.
7 Examine the teflon sheets of the lateral ramp for cracks and incorrect
attachment.

NOTE : This procedure is applicable to the teflon sheets 04-050, 04-070,

04A-050, 04A-070, 04B-050, 04B-070, 04C-050 and 04C-070.
a Cracks and incorrect attachment are not permitted on the teflon sheets.
b See TASK 52-81-14-300-807-A01TASK 52-81-14-300-807-B01TASK
52-81-14-300-807-C01TASK 52-81-14-300-807-D01 for assembly and
disassembly of the teflon sheets.
(2) Examine the ramp assy for:
(a) Not apply.
POST SB 52-1025
(1) Examine the lateral ramp for:
(a) Not apply.
(2) Examine the ramp assy for:

NOTE : See IPL_FIGURE_04D.

NOTE : This procedure is applicable to the ramp assy 04D-190.

- Cracks
- Lockwire
- Corrosion
- Other damages.

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(a) Cracks, corrosion and other damages.

1 Do an approved non-destructive test if you think that there is a crack that you
cannot see clearly. See NTM 52-81-14.
2 Cracks are not permitted. For replacement for a new ramp assy 04D-190, please
contact AIRBUS.
3 For the removal of the corrosion on the fittings of the ramp assy 04D-190, see
SRM 51-22-00.
4 Examine the lockwire of the screws. In case it has lost its use, replace it. See
TASK 52-81-14-300-807-A01TASK 52-81-14-300-807-B01TASK
52-81-14-300-807-C01TASK 52-81-14-300-807-D01.
5 Other damages see SRM 51-11-00 for damage classification.
6 See TASK 52-81-14-300-807-A01TASK 52-81-14-300-807-B01TASK
52-81-14-300-807-C01TASK 52-81-14-300-807-D01 for assembly and
disassembly of the ramp assy 04D-190.
ALL VARIANTS
(3) Not apply.

**For PN’s ALL

Subtask 52-81-14-210-014-A01
F. Check of the Uplock Assy
(1) Examine the uplock assy for:

NOTE : See IPL_FIGURE_03, IPL_FIGURE_03B and IPL_FIGURE_03C.

NOTE : This procedure is applicable to the uplock assy 03-040, 03B-040 and 03C-040.
- Cracks
- Corrosion
- Lockwire
- Other damages.
(a) Cracks, corrosion and other damages.
1 Do an approved non-destructive test if you think that there is a crack that you
cannot see clearly. See NTM 52-81-14.
2 Cracks are not permitted. For replacement for a new uplock assy 03-040, please
contact AIRBUS.
3 For the removal of the corrosion on the uplock assy 03-040, see SRM 51-22-00.
4 Examine the lockwire of the screws. In case it has lost its use, replace it. See
TASK 52-81-14-000-806-A01 and TASK 52-81-14-400-805-A01.

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5 Other damages, see SRM 51-11-00 for damage classification.

6 See TASK 52-81-14-000-806-A01 and TASK 52-81-14-400-805-A01 for assembly
and disassembly of the uplock assy 03-040.
(b) Examine the bushes 03-110, 03-230 and 03-280 for damages.
1 See TASK 52-81-14-820-806-A01 for the permitted limits.
2 Damage is not permitted on the bushes 03-110, 03-230 and 03-280.
3 See TASK 52-81-14-000-811-A01 and TASK 52-81-14-400-810-A01 for the
disassembly and assembly of the bushes 03-110, 03-230 and 03-280.

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**For PN’s ALL

TASK 52-81-14-210-803-A01
Check of the Step Assemblies
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Referenced Information
REFERENCE DESIGNATION
TASK 52-81-14-000-807-A01 Disassembly of the Step Assemblies
TASK 52-81-14-400-804-A01 Assembly of the Step Assemblies
SRM 51-22-00
SRM 51-11-00
Referenced Information
TABLE 1

3. Procedure

Subtask 52-81-14-210-006-A01
A. Check of the Step Assemblies
(1) Examine the step assemblies for:
- Cracks
- Corrosion
- Lockwire
- Other damages.
(a) Cracks, corrosion and other damages.
1 Do an approved non-destructive test if you think there is a crack that you
cannot see clearly.
2 Cracks are not permitted. See TASK 52-81-14-000-807-A01 and TASK
52-81-14-400-804-A01 for replacement of the step assemblies.
3 For removal of the corrosion, see SRM 51-22-00.
4 Examine the lockwire of the screws. In case it has lost its use, replace it. See
TASK 52-81-14-000-807-A01 and TASK 52-81-14-400-804-A01.
5 Other damages, see SRM 51-11-00 for damage classification.

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**For PN’s ALL

TASK 52-81-14-210-804-A01
Check of the Central Ramp and the Sensor-Support Assy
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Referenced Information
REFERENCE DESIGNATION
TASK 52-81-14-300-810-A01 Replacement of the Central Ramp
TASK 52-81-14-300-810-B01 Replacement of the Central Ramp
TASK 52-81-14-300-810-C01 Replacement of the Central Ramp
TASK 52-81-14-300-811-A01 Replacement of the Sensor-Support Assy
TASK 52-81-14-000-808-A01 Disassembly of the Sensor Target
TASK 52-81-14-400-803-A01 Assembly of the Sensor Target
NTM 52-81-14
SRM 51-22-00
SRM 51-11-00
Referenced Information
TABLE 1

3. Procedure

**For PN’s D5288000800000 D5288000800095 D5288000800098 D5288000800100 D5288000800195

D5288000800198 D5288000900000 D5288000900095 D5288000900098 D5288000900100
D5288000900195 D5288000900198 D5288001000000 D5288001000095 D5288001000098
D5288001000100 D5288001000195 D5288001000198

Subtask 52-81-14-210-008-A01
A. Check of the Central Ramp

NOTE : See IPL_FIGURE_05, IPL_FIGURE_05A, IPL_FIGURE_05B, IPL_FIGURE_05C and

IPL_FIGURE_05E.

NOTE : This procedure is applicable to the central ramp.

(1) Examine the central ramp for:
- Cracks
- Corrosion
- Other damages.

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(a) Cracks, corrosion and other damages.

1 Do an approved non-destructive test if you think that there is a crack that you
cannot see clearly. See NTM 52-81-14.
2 Cracks are not permitted. For replacement for a new central ramp, please
contact AIRBUS.
3 For the removal of the corrosion on the fittings of the central ramp, see SRM
51-22-00.
4 Other damages see SRM 51-11-00 for damage classification.
5 See TASK 52-81-14-300-810-A01TASK 52-81-14-300-810-B01TASK
52-81-14-300-810-C01 for removal and installation of the central ramp.
6 Examine the teflon sheets of the central ramp for cracks and incorrect
attachment.

NOTE : This procedure is applicable to the teflon sheets .

a Cracks and incorrect attachment are not permitted on the teflon sheets.
b See TASK 52-81-14-300-810-A01TASK 52-81-14-300-810-B01TASK
52-81-14-300-810-C01 for removal and installation of the teflon sheets.

**For PN’s D5288000800094 D5288000800194 D5288000900094 D5288000900194 D5288001000094

D5288001000194

Subtask 52-81-14-210-008-B01
B. Check of the Central Ramp

NOTE : See IPL_FIGURE_05F and IPL_FIGURE_05G.

NOTE : This procedure is applicable to the central ramp.

(1) Examine the central ramp for:
- Cracks
- Corrosion
- Other damages.
(a) Cracks, corrosion and other damages.
1 Do an approved non-destructive test if you think that there is a crack that you
cannot see clearly. See NTM 52-81-14.
2 Cracks are not permitted. For replacement for a new central ramp, please
contact AIRBUS.
3 For the removal of the corrosion on the fittings of the central ramp, see SRM
51-22-00.
4 Other damages see SRM 51-11-00 for damage classification.

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5 See TASK 52-81-14-300-810-C01 for removal and installation of the central

ramp.
6 Examine the teflon paint of the central ramp for damage.

NOTE : This procedure is applicable to the teflon paint.

a Damage is not permitted on the teflon paint.
b See TASK 52-81-14-300-810-C01 for repair of the teflon paint.

**For PN’s ALL

Subtask 52-81-14-210-011-A01
C. Check of the Sensor-Support Assy

NOTE : See IPL_FIGURE_06 and IPL_FIGURE_06A.

NOTE : This procedure is applicable to the sensor-support assy 06-030 and 06A-030 .
(1) Examine the sensor-support assy for:
- Cracks
- Corrosion
- Other damages
- Correct attachment of the target.
(a) Cracks, corrosion and other damages.
1 Do an approved non-destructive test if you think that there is a crack that you
cannot see clearly. See NTM 52-81-14.
2 Cracks are not permitted. For replacement for a new sensor-support assy 06-030
, please contact AIRBUS.
3 For the removal of the corrosion on the sensor-support assy 06-030 , see SRM
51-22-00.
4 Other damages see SRM 51-11-00 for damage classification.
5 Check the correct attachment of the target 06-070 for loosed and/or missing
nuts or screws.
6 See TASK 52-81-14-300-811-A01 for removal and installation of the sensor-
support assy 06-030 . See TASK 52-81-14-000-808-A01, TASK
52-81-14-400-803-A01 for the disassembly and assembly of the target 06-070 .

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**For PN’s ALL

TASK 52-81-14-210-805-A01
Check of the Protective Treatment
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A.Referenced Information
REFERENCE DESIGNATION
TASK 52-81-14-100-801-A01 Cleaning of the Painted Components
TASK 52-81-14-100-802-A01 Cleaning of the Components Which are not Painted
TASK 52-81-14-300-801-A01 Repair of the Surface Protection and Paint Coating
Referenced Information
TABLE 1

3. Procedure

Subtask 52-81-14-210-010-A01
A. Check of the Protective Treatment
(1) Examine all components, which have a protective treatment for:
(a) Damage to the surface protection:
1 Clean the component. See TASK 52-81-14-100-801-A01 and TASK
52-81-14-100-802-A01.
2 Damage of the surface protection is not permitted.
3 See TASK 52-81-14-300-801-A01 for repair of the surface protection.

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**For PN’s ALL

TASK 52-81-14-200-801-A01
Check of the Tip Seal
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A.Referenced Information
REFERENCE DESIGNATION
TASK 52-81-14-000-809-A01 Disassembly of the Tip Seal
TASK 52-81-14-400-802-A01 Assembly of the Tip Seal
Referenced Information
TABLE 1

3. Procedure

Subtask 52-81-14-220-001-A01
A. Check of the Tip Seal
(1) Examine the tip seal for:

NOTE : See IPL_FIGURE_06 and IPL_FIGURE_06A.

NOTE : This procedure is applicable to the tip seals 06-290 and 06A-290.
- Cracks
- Hardening
- Oil contamination
- Porosity
- Other damage.
(a) Hardening, cracks, oil contamination or porosity is not permitted.
(b) Other damage is not permitted on the tip seal.
(c) For the replacement of the damaged tip seal 06-290 see TASK 52-81-14-000-809-A01
and TASK 52-81-14-400-802-A01.
PRE MOD 21295G0066
(4) Examine the profile for:

NOTE : See IPL_FIGURE_06.

NOTE : This procedure is applicable to the profile 06-270.

- Attach parts

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- Damages.
(a) A loose or damaged attach part of the profile 06-270 is not permitted.
(b) Damages are not permitted.
(c) See TASK 52-81-14-000-809-A01 and TASK 52-81-14-400-802-A01 for the
disassembly and assembly of the profile 06-270.
POST MOD 21295G0066
(4) Examine the profile and the shim for:

NOTE : See IPL_FIGURE_06A.

NOTE : This procedure is applicable to the profile 06A-270 and the shim 06A-285.
- Attach parts
- Damages.
(a) A loose or damaged attach part of the profile 06-270 and the shim 06A-285 is not
permitted.
(b) Damages are not permitted.
(c) See TASK 52-81-14-000-809-A01 and TASK 52-81-14-400-802-A01 for the
disassembly and assembly of the profile 06-270 and the shim 06A-285.
ALL VARIANTS
(5) Not apply.

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**For PN’s ALL

TASK 52-81-14-200-802-A01
Check of the Sealing Strips
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A.Referenced Information
REFERENCE DESIGNATION
TASK 52-81-14-000-810-A01 Disassembly of the Sealing Strips
TASK 52-81-14-400-801-A01 Assembly of the Sealing Strips
Referenced Information
TABLE 1

3. Procedure

Subtask 52-81-14-220-003-A01
A. Check of the Sealing Strips
(1) Examine the sealing strips for:

NOTE : See IPL_FIGURE_06 and IPL_FIGURE_06A.

NOTE : This procedure is applicable to the sealing strips 06-130, 06A-130 ,06-140,
06A-140 ,06-220 and 06A-220.
- Cracks
- Hardening
- Oil contamination
- Porosity
- Other damage.
(a) Hardening, cracks, oil contamination or porosity is not permitted.
(b) Other damage is not permitted on the sealing strip 06-130.
(c) For the replacement of the damaged sealing strip 06-130 see TASK
52-81-14-000-810-A01 and TASK 52-81-14-400-801-A01
(2) Examine the profile for:

NOTE : See IPL_FIGURE_06 and IPL_FIGURE_06A.

NOTE : This procedure is applicable to the profiles 06-110, 06A-110, 06-120, 06A-120,
06-150, 06A-150, 06-170, 06A-18006-180, 06-190, 06A-190, 06-200 and
06A-200.

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- Attach parts
- Damages.
(a) A loose or damaged attach part of the profile is not permitted.
(b) Damages are not permitted.
(c) See TASK 52-81-14-000-810-A01 and TASK 52-81-14-400-801-A01 for the
disassembly and assembly of the profile 06-110.

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**For PN’s ALL

TASK 52-81-14-200-803-A01
Check of the Stops
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A.Referenced Information
REFERENCE DESIGNATION
TASK 52-81-14-300-812-A01 Replacement of the Stops
Referenced Information
TABLE 1

3. Procedure

Subtask 52-81-14-220-004-A01
A. Check of the Stops
(1) Examine the stops for:
- Attach parts
- Damages.
(a) A loose or damaged attach part of the stop is not permitted.
(b) Damages are not permitted.
(c) See TASK 52-81-14-300-812-A01 for replacement of the stops.

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**For PN’s ALL

TASK 52-81-14-200-804-A01
Check of the Identification Plates
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A.Referenced Information
REFERENCE DESIGNATION
TASK 52-81-14-400-809-A01 Assembly of the Identification Plates
Referenced Information
TABLE 1

3. Procedure

Subtask 52-81-14-200-001-A01
A. Check of the Identification Plates
(1) Do a visual inspection of the identification plate for:
(a) Damaged readability is not permitted.
(b) A loose or damaged attachment of the identification plate is not permitted.
(c) A loose or damaged identification plate is not permitted.
(d) No other damage is not permitted.
(e) See TASK 52-81-14-400-809-A01 for the replacement of the damaged identification
plate.

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REPAIR

**For PN’s ALL

TASK 52-81-14-300-801-A01
Repair of the Surface Protection and Paint Coating
1. Reason for the Job
This section tells you how to repair the component parts.
2. Job Set-up Information
A. Referenced Information
REFERENCE DESIGNATION
TASK 52-81-14-210-805-A01 Check of the Protective Treatment
PMS 01-02-27
PMS 01-02-31
SRM 51-73-00
SRM 51-74-00
SRM 51-75-12
Referenced Information
TABLE 1

3. Procedure

WARNING : BE CAREFUL WHEN YOU USE SOLVENTS/CLEANING AGENTS, SEALANTS AND

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

CAUTION : USE ONLY SPECIFIED CLEANING MATERIALS AND SOLUTIONS OR THEIR

EQUIVALENTS. THE SURFACE PROTECTION COULD BE DAMAGED IF
UNSPECIFIED MATERIALS ARE USED. IT IS IMPORTANT THAT THE
MANUFACTURER’S MIXING, APPLICATION AND TREATMENT INSTRUCTIONS
ARE FOLLOWED.

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Subtask 52-81-14-300-002-A01
A. Repair of the Surface Protection and Paint Coating

CAUTION : DO NOT APPLY THESE STEPS TO THE COVER ASSEMBLY, FITTINGS,

UPLOCK ASSEMBLY, STEP ASSEMBLY, RAMP AND SENSOR TARGET
ASSEMBLIES.

NOTE : See TASK 52-81-14-210-805-A01 for check the surface protection.

NOTE : See PMS 01-02-27 for application of primer.

NOTE : See PMS 01-02-31 for pretreatment of P. T. F. E. surfaces.

(1) Repair of minor damage.
(a) See SRM 51-73-00 for repair of minor damage.
(2) Repair of corroded areas.
(a) See SRM 51-74-00 for repair of corroded areas.
(3) Repair of minor damaged paint coatings.
(a) See SRM 51-75-12 for repair of damaged paint coatings.

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**For PN’s D5288000800000 D5288000800098 D5288000800100 D5288000800198

TASK 52-81-14-300-807-A01
Replacement of the Lateral Ramp and the Ramp Assy
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
14QGC1 Wire-Locking Dia: 1 mm (0.041 inch) CRES -
06AAC1 Polysulfide Sealant-General Purpose Interfay -
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
13AEC1 Dry glass fabric-8H Satin 293 gsm - 181 style SRM Type 2 -
05EML7 Epoxy Adhesive-- - Legacy 3
05EJL9 Epoxy Adhesive-Metal to metal - Legacy
Consumable Materials
TABLE 1

B. Fixtures, Tools, Test and Support Equipment

REFERENCE DESIGNATION
non-metallic scraper
Fixtures, Tools, Test and Support Equipment
TABLE 2

C. Referenced Information
REFERENCE DESIGNATION
SRM 51-42-21
SRM 51-42-11
PMS 01-02-31
PMS 01-02-27
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.

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.

CAUTION : USE ONLY SPECIFIED CLEANING MATERIALS AND SOLUTIONS OR THEIR

EQUIVALENTS. THE SURFACE PROTECTION COULD BE DAMAGED IF
UNSPECIFIED MATERIALS ARE USED. IT IS IMPORTANT THAT THE
MANUFACTURER’S MIXING, APPLICATION AND TREATMENT INSTRUCTIONS
ARE FOLLOWED.

Subtask 52-81-14-350-001-A01
A. Disassembly of the Lower Lateral Ramp
PRE MOD 21516G0071
(1) Disassembly of the lower lateral ramp.

NOTE : See IPL_FIGURE_04 .

(a) Remove all Material No. 14QGC1 Wire-Locking Dia: 1 mm (0.041 inch) CRES - and
sealant from the fastener heads.
(b) Remove the bonded teflon sheet 04-070 from the plate 04-510 and the T-section
04-140.
(c) Remove the old adhesive from the component parts with a non-metallic scraper.
(d) Remove the plate 04-510 from the runout tip 04-540 by removing the hi-loks 04-435,
the collars 04-415 and the blind bolts 04-480. See SRM 51-42-11 for the removal of
the hi-loks 04-435, the collars 04-415 and the blind bolts 04-480.
(e) Remove the T-section 04-140 from the tip support 04-560 and the No. 4 moveable
support 04-420 by removing the rivets 04-040. See SRM 51-42-11 for the removal of
the rivets 04-040.
(f) Remove the tip support 04-560 from the cover assembly by removing the screws
04-210.
(g) Remove the bolts 04-400, the washers 04-410 and the No. 4 moveable support 04-420
from the isolator 04-465.
(h) Remove the runout tip 04-540 from the cover assembly by removing the screws
04-210, the hi-loks 04-030, the nuts 04-020 and the rivets 04-040, 04-500. See SRM
51-42-21 for the removal of the hi-loks 04-030 and the rivets 04-040, 04-500.

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(i) Remove the L-profile 04-580 by removing the blind bolts 04-470. See SRM 51-42-11
for the removal of the blind bolts 04-470.
POST MOD 21516G0071
(1) Disassembly of the lower lateral ramp.

NOTE : See IPL_FIGURE_04B.

(a) Remove all Material No. 14QGC1 Wire-Locking Dia: 1 mm (0.041 inch) CRES - and
sealant from the fastener heads.
(b) Remove the bonded teflon sheet 04B-070 from the plate 04B-510 and the T-section
04B-140.
(c) Remove the old adhesive from the component parts with a non-metallic scraper.
(d) Remove the plate 04B-510 from the runout tip 04B-540 by removing the blind bolts
04B-480, the screw 04B-505, and the nuts 04B-490. See SRM 51-42-11 for the
removal of the blind bolts 04B-480.
(e) Remove the T-section 04B-140 from the tip support 04B-560 and the No. 4 moveable
support 04B-420 by removing the rivets 04B-040. See SRM 51-42-11 for the removal
of the rivets 04B-040.
(f) Remove the tip support 04B-560 from the cover assembly by removing the screws
04B-210.
(g) Remove the bolts 04B-400, the washers 04B-410 and the No. 4 moveable support
04B-420 from the isolator 04B-470.
(h) Remove the runout tip 04B-540 from the cover assembly by removing the screws
04B-210, the hi-loks 04B-030, the nuts 04B-020 and the rivets 04B-040, 04B-530. See
SRM 51-42-21 for the removal of the hi-loks 04B-030 and the rivets 04B-040,
04B-530.
ALL VARIANTS
(2) Not apply.

Subtask 52-81-14-350-002-A01
B. Disassembly of the Upper Lateral Ramp

NOTE : See IPL_FIGURE_04 and IPL_FIGURE_04B.

(1) Remove all Material No. 14QGC1 Wire-Locking Dia: 1 mm (0.041 inch) CRES - and
sealant from the fastener heads.
(2) Remove the bolts 04-010 from the teflon sheet 04-050. See SRM 51-42-21 for the removal
of the bolts 04-010.
(3) Remove the bonded teflon sheet 04-050 from the T-sections 04-100 and 04-120.
(4) Remove the old adhesive from the component parts with a non-metallic scraper.

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(5) Remove the T-section 04-120 from the No. 4 support assembly 04-440, the No. 3 fwd
support assembly 04-600, the No. 3 aft support assembly 04-620, the No. 2 fwd support
assembly 04-220 and the No. 2 aft support assembly 04-240 by removing the hi-loks
04-030, the collar 04-020 and the rivets 04-040. See SRM 51-42-11 for the removal of the
hi-loks 04-030, the collar 04-020 and the rivets 04-040.
(6) Remove the T-section 04-100 from the No. 2 fwd support assembly 04-220, the No. 2 aft
support assembly 04-240 and the No. 1 support 04-190 by removing the rivets 04-040 and
the screws 04-090. See SRM 51-42-11 for the removal of the rivets 04-040.
(7) Remove the No. 4 support assembly 04-440 by removing the bolts 04-260 and 04-270.
(8) Remove the isolators 04-46504-470 by removing the rivets 04-460. See SRM 51-42-11 for
the removal of the rivets 04-460.
(9) Remove the No. 3 fwd support 04-600 by removing the bolts 04-260.
(10) Remove the No. 3 aft support 04-620 by removing the bolts 04-260.
(11) Remove the No. 2 fwd support 04-220 by removing the screws 04-210.
(12) Remove the No. 2 aft support 04-240 by removing the screws 04-210.
(13) Remove the No. 1 support 04-190 by removing the screws 04-160 and 04-170.

Subtask 52-81-14-350-003-A01
C. Installation of the Lower Lateral Ramp

NOTE : Unless indicated, all fasteners and mating surfaces are to be wet installed with
Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay -.

NOTE : Where necessary use oversize fasteners.

PRE MOD 21516 G0071
(1) Installation of the lower lateral ramp.

NOTE : See IPL_FIGURE_04.

(a) Remove all old sealant from the cover assembly and any components that were
previously removed.
(b) Clean the surface of the cover assembly with Material No. 08BBF1 Non Aqueous
Cleaner-- Methyl-Ethyl-Ketone -.
(c) Cut a piece of Material No. 13AEC1 Dry glass fabric-8H Satin 293 gsm - 181 style
SRM Type 2 - to the shape of the runout tip 04-540 and the tip support 04-560.
(d) Apply Material No. 05EML7 Epoxy Adhesive-- - Legacy 3 to the glass fabric pieces
and put them in position on the cover assembly.
(e) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surfaces of the runout tip 04-540 and the tip support 04-560.

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CAUTION : MAKE SURE THAT THE SCREWS HAVE A MINIMUM THREADED

LENGTH OF 5 MM (0.20 IN).
(f) Install the tip support 04-560 with the screws 04-210.
(g) Install the L-profile 04-580 to the runout tip 04-540 with the blind bolts 04-470. See
SRM 51-42-11 for the installation of the blind bolts 04-470.
(h) Install the runout tip 04-540 to the cover assembly with the screws 04-210, the hi-loks
04-030, the collar 04-020 and the rivets 04-040, 04-500. See SRM 51-42-21 for the
installation of the hi-loks 04-030, the collar 04-020 and the rivets 04-040, 04-500.
(i) Install the plate 04-510 to the runout tip 04-540 with the blind bolts 04-480, the hi-
loks 04-435 and the collars 04-415. See SRM 51-42-11 for the installation of the blind
bolts 04-480, the hi-loks 04-435 and the collars 04-415.
(j) Install the No. 4 support 04-440 to the cover assembly with the bolts 04-260 and
04-270.
(k) Safety the bolts 04-260 and 04-270 with Material No. 14QGC1 Wire-Locking Dia: 1
mm (0.041 inch) CRES - .
(l) Install the No. 4 moveable support 04-420 to the isolators 04-465 with the bolts
04-400 and the washers 04-410.
(m) Install the T-section 04-140 to the tip support 04-560 and the No. 4 moveable
support 04-420 with the rivets 04-040. See SRM 51-42-11 for the installation of the
rivets 04-040.
(n) Identify the mating surfaces of the teflon sheet 04-070 with the T-section 04-140 and
the plate 04-510. On the mating surfaces of the teflon sheet 04-070 only, do a pre-
treatment according to ABP5-1148 PMS 01-02-31 Pre-Treatment of the P. T. F. E.
Surfaces.
(o) Identify the mating surfaces of the T-section 04-140 and the plate 04-510 with the
teflon sheet 04-070. On the mating surfaces of the T-section 04-140 and the plate
04-510 only, examine the condition of the bonding primer.
(p) If the bonding primer of the T-section 04-100, 04-120 and 04-140, and the plate
04-510 is damaged, do the subsequent steps.
1 Remove the bonding primer with emery cloth Grade 240 to 440 .
2 Clean the mating surfaces of the T-section 04-100, 04-120 and 04-140, and the
plate 04-510 with Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-
Ketone -.
3 Apply bonding primer to the mating surfaces of the T-section 04-100, 04-120
and 04-140, and the plate 04-510, according to ABP4-1123. See PMS 01-02-27
Application of Primer.
(q) Rub lightly the mating surfaces of the T-section 04-140 and the plate 04-510 with
emery cloth Grade 240 to 440.

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(r) Clean the mating surfaces of the T-section 04-140 and the plate 04-510 with Material
No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(s) Apply Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy to the mating
surfaces of the T-section 04-140, the teflon sheet 04-070 and the plate 04-510.
(t) Install the teflon sheet 04-070 on the T-section 04-140 and the plate 04-510. Apply
pressure and let the adhesive cure.
(u) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to all
fastener heads.
POST MOD 21516 G0071
(1) Installation of the lower lateral ramp.

NOTE : See IPL_FIGURE_04B.

(a) Remove all old sealant from the cover assembly and any components that were
previously removed.
(b) Clean the surface of the cover assembly with Material No. 08BBF1 Non Aqueous
Cleaner-- Methyl-Ethyl-Ketone -.
(c) Cut a piece of Material No. 13AEC1 Dry glass fabric-8H Satin 293 gsm - 181 style
SRM Type 2 - to the shape of the runout tip 04B-540 and the tip support 04B-560.
(d) Apply Material No. 05EML7 Epoxy Adhesive-- - Legacy 3 to the glass fabric pieces
and put them in position on the cover assembly.
(e) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surfaces of the runout tip 04B-540 and the tip support 04B-560.

CAUTION : MAKE SURE THAT THE SCREWS HAVE A MINIMUM THREADED

LENGTH OF 5 MM (0.20 IN).
(f) Install the tip support 04B-560 with the screws 04B-210.
(g) Install the runout tip 04B-540 to the cover assembly with the screws 04B-210, the hi-
loks 04B-030, the nuts 04B-020 and the rivets 04B-040, 04B-530. See SRM 51-42-21
for the installation of the hi-loks 04B-030 and the rivets 04B-040, 04B-530.
(h) Install the plate 04B-510 to the runout tip 04B-540 with the blind bolts 04B-480, the
screws 04B-505 and the nuts 04B-490. See SRM 51-42-11 for the installation of the
blind bolts 04B-480.
(i) Install the No. 4 support 04B-440 to the cover assembly with the bolts 04B-260 and
04B-270.
(j) Safety the bolts 04B-260 and 04B-270 with Material No. 14QGC1 Wire-Locking Dia:
1 mm (0.041 inch) CRES - .
(k) Install the No. 4 moveable support 04B-420 to the isolators 04B-470 with the bolts
04B-400, the washers 04B-410.

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(l) Install the T-section 04B-140 to the tip support 04B-560 and the No. 4 moveable
support 04B-420 with the rivets 04B-040. See SRM 51-42-11 for the installation of
the rivets 04B-040.
(m) Identify the mating surfaces of the teflon sheet 04B-470 with the T-section 04B-140
and the plate 04B-510. On the mating surfaces of the teflon sheet 04B-470 only, do a
pre-treatment according to ABP5-1148 PMS 01-02-31 Pre-Treatment of the P. T. F.
E. Surfaces.
(n) Identify the mating surfaces of the T-section 04B-140 and the plate 04B-510 with the
teflon sheet 04B-470. On the mating surfaces of the T-section 04B-140 and the plate
04B-510 only, examine the condition of the bonding primer.
(o) If the bonding primer of the T-section 04B-100, 04B-120 and 04B-140, and the plate
04B-510 is damaged, do the subsequent steps.
1 Remove the bonding primer with emery cloth Grade 240 to 440 .
2 Clean the mating surfaces of the T-section 04B-100, 04B-120 and 04B-140, and
the plate 04B-510 with Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-
Ethyl-Ketone -.
3 Apply bonding primer to the mating surfaces of the T-section 04B-100, 04B-120
and 04B-140, and the plate 04B-510, according to ABP4-1123. See PMS
01-02-27 Application of Primer.
(p) Rub lightly the mating surfaces of the T-section 04B-140 and the plate
04B-51004B-510 with emery cloth Grade 240 to 440.
(q) Clean the mating surfaces of the T-section 04B-140 and the plate 04B-510 with
Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(r) Apply Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy to the mating
surfaces of the T-section 04B-140, the teflon sheet 04B-470 and the plate 04B-510.
(s) Install the teflon sheet 04B-470 on the T-section 04B-140 and the plate 04B-510.
Apply pressure and let the adhesive cure.
(t) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to all
fastener heads.
ALL VARIANTS
(2) Not apply.

Subtask 52-81-14-350-004-A01
D. Assembly of the Upper Lateral Ramp

NOTE : See IPL_FIGURE_04 and IPL_FIGURE_04B.

NOTE : Unless indicated, all fasteners and mating surfaces are to be wet installed with
Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay -.

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NOTE : Where necessary use oversize fasteners.

(1) Remove all old sealant from the cover assembly and any components that were previously
removed.
(2) Clean the surface of the cover assembly with Material No. 08BBF1 Non Aqueous Cleaner--
Methyl-Ethyl-Ketone -.
(3) Cut some pieces of Material No. 13AEC1 Dry glass fabric-8H Satin 293 gsm - 181 style
SRM Type 2 - to the shape of the No. 3 and No. 2 supports.
(4) Apply Material No. 05EML7 Epoxy Adhesive-- - Legacy 3 to the glass fabric pieces and put
them in position on the cover assembly.
(5) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the mating
surfaces of the No. 3, No. 2 and No. 1 supports.
(6) Install the No. 3 fwd and aft supports 04-600 and 04-620 to the cover assembly with the
bolts 04-260.
(7) Safety the bolts 04-260 with Material No. 14QGC1 Wire-Locking Dia: 1 mm (0.041 inch)
CRES - .
(8) Install the No. 2 fwd and aft supports 04-220 and 04-240 with the screws 04-210.
(9) Install the No. 1 support 04-190 with the screws 04-160 and 04-170.
(10) Cut some pieces of Material No. 13AEC1 Dry glass fabric-8H Satin 293 gsm - 181 style
SRM Type 2 - to the upper shape of the No. 3 and No. 2 supports.
(11) Apply Material No. 05EML7 Epoxy Adhesive-- - Legacy 3 to the glass fabric pieces and put
them over the supports.
(12) Install the T-section 04-120 to the No. 4 support 04-440, the No. 3 fwd Support 04-600,
the No. 3 aft support 04-620, the No. 2 fwd support 04-220 and the No. 2 aft support
04-240 with the hi-loks 04-030 and the collar 04-020. See SRM 51-42-11 for the
installation of the hi-loks 04-030 and the collar 04-020.
(13) Install the T-section 04-100 to the No. 2 fwd support 04-220, the No. 2 aft support 04-240
and the No. 1 support 04-190 with the rivets 04-040 and the screws 04-090. See SRM
51-42-11 for the installation of the rivets 04-040.
(14) Identify the mating surfaces of the teflon sheet 04-050 with the T-sections 04-100 and
04-120, On the mating surfaces of the teflon sheet 04-050 only, do a pre-treatment
according to ABP51148. See PMS 01-02-31 Pre-Treatment of the P. T. F. E. Surfaces.
(15) Identify the mating surfaces of the T-sections 04-100 and 04-120 with the teflon sheet
04-050. On the mating surfaces of the T-sections 04-100 and 04-120 only, examine the
condition of the bonding primer.
(16) If the bonding primer of the T-section 04-100, 04-120 and 04-140, and the plate 04-510 is
damaged, do the subsequent steps.
(a) Remove the bonding primer with emery cloth Grade 240 to 440 .

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(b) Clean the mating surfaces of the T-section 04-100, 04-120 and 04-140, and the plate
04-510 with Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(c) Apply bonding primer to the mating surfaces of the T-section 04-100, 04-120 and
04-140, and the plate 04-510, according to ABP4-1123. See PMS 01-02-27
Application of Primer.
(17) Rub lightly the mating surfaces of the T-sections 04-100 and 04-120 with emery cloth
Grade 240 to 440.
(18) Clean the mating surfaces of the T-sections 04-100 and 04-120 with Material No. 08BBF1
Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(19) Apply Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy to the mating surfaces
of the T-sections 04-100 and 04-120 and the teflon sheet 04-050.
(20) Install the teflon sheet 04-050 on the T-sections 04-100 and 04-120. Install the bolts
04-010 thru the teflon sheet 04-050, the T-section 04-120 and the No. 4 support 04-440.
Apply pressure and let the adhesive cure. See SRM 51-42-21 for the installation of the bolts
04-010.
(21) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to all fastener
heads.

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**For PN’s D5288000900000 D5288000900098 D5288000900100 D5288000900198

TASK 52-81-14-300-807-B01
Replacement of the Lateral Ramp and the Ramp Assy
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
14QGC1 Wire-Locking Dia: 1 mm (0.041 inch) CRES -
06AAC1 Polysulfide Sealant-General Purpose Interfay -
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
13AEC1 Dry glass fabric-8H Satin 293 gsm - 181 style SRM Type 2 -
05EML7 Epoxy Adhesive-- - Legacy 3
05EJL9 Epoxy Adhesive-Metal to metal - Legacy
Consumable Materials
TABLE 1

B. Fixtures, Tools, Test and Support Equipment

REFERENCE DESIGNATION
non-metallic scraper
Fixtures, Tools, Test and Support Equipment
TABLE 2

C. Referenced Information
REFERENCE DESIGNATION
SRM 51-42-11
SRM 51-42-21
PMS 01-02-31
PMS 01-02-27
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.

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.

CAUTION : USE ONLY SPECIFIED CLEANING MATERIALS AND SOLUTIONS OR THEIR

EQUIVALENTS. THE SURFACE PROTECTION COULD BE DAMAGED IF
UNSPECIFIED MATERIALS ARE USED. IT IS IMPORTANT THAT THE
MANUFACTURER’S MIXING, APPLICATION AND TREATMENT INSTRUCTIONS
ARE FOLLOWED.

Subtask 52-81-14-350-005-A01
A. Disassembly of the Lower Lateral Ramp

NOTE : See IPL_FIGURE_04A.

(1) Remove all Material No. 14QGC1 Wire-Locking Dia: 1 mm (0.041 inch) CRES - and
sealant from the fastener heads.
(2) Remove the bonded teflon sheet 04A-070 from the plate 04A-510 and the T-section
04A-140.
(3) Remove the old adhesive from the component parts with a non-metallic scraper.
(4) Remove the plate 04A-510 from the runout tip 04A-540 by removing the screw 04A-500,
the blind bolts 04A-480 and the nut 04A-490. See SRM 51-42-11 for the removal of the
blind bolts 04A-480.
(5) Remove the T-section 04A-140 from the tip support 04A-560 and the No. 4 moveable
support 04A-420 by removing the rivets 04A-040. See SRM 51-42-11 for the removal of the
rivets 04A-040.
(6) Remove the tip support 04A-560 from the cover assembly by removing the screws 04A-210.
(7) Remove the bolts 04A-400, the washers 04A-410 and the No. 4 moveable support 04A-420
from the isolator 04A-470.
(8) Remove the runout tip 04A-540 from the cover assembly by removing the screws 04A-210,
the hi-loks 04A-030, the collar 04A-020 and the rivets 04A-040 and 04A-530. See SRM
51-42-21 for the removal of the hi-loks 04B-030 and the rivets 04B-040, 04B-530.

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Subtask 52-81-14-350-006-A01
B. Disassembly of the Upper Lateral Ramp

NOTE : See IPL_FIGURE_04A.

(1) Remove all Material No. 14QGC1 Wire-Locking Dia: 1 mm (0.041 inch) CRES - and
sealant from the fastener heads.
(2) Remove the bolts 04A-010 from the teflon sheet 04A-050. See SRM 51-42-21 for the
removal of the bolts 04A-010.
(3) Remove the teflon sheet 04A-050 from the T-sections 04A-100 and 04A-120.
(4) Remove the old adhesive from the component parts with a non-metallic scraper.
(5) Remove the T-section 04A-120 from the No. 4 support assembly 04A-440, the No. 3 fwd
support assembly 04A-360, the No. 3 aft support assembly 04A-380, the No. 2 fwd support
assembly 04A-220 and the No. 2 aft support assembly 04A-240 by removing the hi-loks
04A-030, the collar 04A-020 and the rivets 04A-040. See SRM 51-42-11 for the removal of
the hi-loks 04A-030, the collar 04A-020 and the rivets 04A-040.
(6) Remove the T-section 04A-100 from the No. 2 fwd support assembly 04A-220, the No. 2
aft support assembly 04A-240 and the No. 1 support 04A-190 by removing the rivets
04A-040 and the screws 04A-090. See SRM 51-42-11 for the removal of the rivets 04A-040.
(7) Remove the No. 4 support assembly 04A-440 by removing the bolts 04A-260 and 04A-270.
(8) Remove the isolators 04A-470 by removing the rivets 04A-460. See SRM 51-42-11 for the
removal of the rivets 04A-460.
(9) Remove the No. 3 support 04A-290 by removing the bolts 04A-260.
(10) Remove the No. 2 fwd support 04A-220 by removing the screws 04A-210.
(11) Remove the No. 2 aft support 04A-240 by removing the screws 04A-210.
(12) Remove the No. 1 support 04A-190 by removing the screws 04A-160 and 04A-170.
(13) Remove the reinforcements 04A-320 and 04A-340 from the No. 3 fwd and aft supports
04A-360 and 04A-380 by removing the rivets 04A-310. See SRM 51-42-11 for the removal
of the rivets 04A-310.

Subtask 52-81-14-350-007-A01
C. Installation of the Lower Lateral Ramp

NOTE : See IPL_FIGURE_04A.

NOTE : Unless indicated, all fasteners and mating surfaces are to be wet installed with
Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay -.

NOTE : Where necessary use oversize fasteners.

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(1) Remove all old sealant from the cover assembly and any components that were previously
removed.
(2) Clean the surface of the cover assembly with Material No. 08BBF1 Non Aqueous Cleaner--
Methyl-Ethyl-Ketone -.
(3) Cut a piece of Material No. 13AEC1 Dry glass fabric-8H Satin 293 gsm - 181 style SRM
Type 2 - to the shape of the runout tip 04A-540 and the tip support 04A-560.
(4) Apply Material No. 05EML7 Epoxy Adhesive-- - Legacy 3 to the glass fabric pieces and put
them in position on the cover assembly.
(5) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the mating
surfaces of the runout tip 04A-540, and the tip support 04A-560.

CAUTION : MAKE SURE THAT THE SCREWS HAVE A MINIMUM THREADED LENGTH
OF 5 MM (0.20 IN).
(6) Install the tip support 04A-560 with the screws 04A-210.
(7) Install the runout tip 04A-540 to the cover assembly with the screws 04A-210, the hi-loks
04A-030, the collar 04A-020 and the rivets 04A-040, 04A-530. See SRM 51-42-21 for the
installation of the hi-loks 04A-030, the collar 04A-020 and the rivets 04A-040, 04A-530.
(8) Install the plate 04A-510 to the runout tip 04A-540 with the blind bolts 04A-480, the screw
04A-500 and the nut 04A-490. See SRM 51-42-11 for the installation of the blind bolts
04A-480.
(9) Install the No. 4 support 04A-440 to the cover assembly with the bolts 04A-260 and
04A-270.
(10) Safety the bolts 04A-260 and 04A-270 with Material No. 14QGC1 Wire-Locking Dia: 1 mm
(0.041 inch) CRES - .
(11) Install the No. 4 moveable support 04A-420 to the isolators 04A-470 with the bolts
04A-400 and the washers 04A-410.
(12) Install the T-section 04A-140 to the tip support 04A-560 and the No. 4 moveable support
04A-420 with the rivets 04A-040. See SRM 51-42-11 for the installation of the rivets
04A-040.
(13) Identify the mating surfaces of the teflon sheet 04A-070 with the T-section 04A-140 and
the plate 04A-510. On the mating surfaces of the teflon sheet 04A-070 only, do a pre-
treatment according to ABP5-1148 PMS 01-02-31 Pre-Treatment of the P. T. F. E.
Surfaces.
(14) Identify the mating surfaces of the T-section 04A-140 and the plate 04A-510 with the
teflon sheet 04A-070. On the mating surfaces of the T-section 04A-140 and the plate
04A-510 only, examine the condition of the bonding primer.

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(15) If the bonding primer of the T-section 04A-100, 04A-120 and 04A-140, and the plate
04A-510 is damaged, do the subsequent steps.
(a) Remove the bonding primer with emery cloth Grade 240 to 400 .
(b) Clean the mating surfaces of the T-section 04A-100, 04A-120 and 04A-140, and the
plate 04A-510 with Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-
Ketone -.
(c) Apply bonding primer to the mating surfaces of the T-section 04A-100, 04A-120 and
04A-140, and the plate 04A-510, according to ABP4-1123. See PMS 01-02-27
Application of Primer.
(16) Rub lightly the mating surfaces of the T-section 04A-140 and the plate 04A-510 with
emery cloth Grade 240 to 400 .
(17) Clean the mating surfaces of the T-section 04A-140 and the plate 04A-510 with Material
No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(18) Apply Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy to the mating surfaces
of the T-section 04A-140, the teflon sheet 04A-070 and the plate 04A-510.
(19) Install the teflon sheet 04A-070 on the T-section 04A-140 and the plate 04A-510. Apply
pressure and let the adhesive cure.
(20) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to all fastener
heads.

Subtask 52-81-14-350-008-A01
D. Installation of the Upper Lateral Ramp

NOTE : See IPL_FIGURE_04A

NOTE : Unless indicated, all fasteners and mating surfaces are to be wet installed with
Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay -.

NOTE : Where necessary use oversize fasteners.

(1) Remove all old sealant from the cover assembly and any components that were previously
removed.
(2) Clean the surface of the cover assembly with Material No. 08BBF1 Non Aqueous Cleaner--
Methyl-Ethyl-Ketone -.
(3) Install the reinforcement plates 04A-320 and 04A-340 to the No. 3 fwd support 04A-360
and the No. 3 aft support 04A-380 with the rivets 04A-310. See SRM 51-42-11 for the
installation of the rivets 04A-310.
(4) Cut some pieces of Material No. 13AEC1 Dry glass fabric-8H Satin 293 gsm - 181 style
SRM Type 2 - to the shape of the No. 3 and No. 2 supports.

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(5) Apply Material No. 05EML7 Epoxy Adhesive-- - Legacy 3 to the glass fabric pieces and put
them in position on the cover assembly.
(6) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the mating
surfaces of the No. 3, No. 2 and No. 1 supports.
(7) Install the No. 3 support assembly 04A-290 to the cover assembly with the bolts 04A-260.
(8) Safety the bolts 04A-260 with Material No. 14QGC1 Wire-Locking Dia: 1 mm (0.041 inch)
CRES - .
(9) Install the No. 2 fwd and aft supports 04A-220 and 04A-240 with the screws 04A-210.
(10) Install the No. 1 support 04A-190 with the screws 04A-160 and 04A-170.
(11) Cut some pieces of Material No. 13AEC1 Dry glass fabric-8H Satin 293 gsm - 181 style
SRM Type 2 - to the upper shape of the No. 3 and No. 2 supports.
(12) Apply Material No. 05EML7 Epoxy Adhesive-- - Legacy 3 to the glass fabric pieces and put
them on the supports.
(13) Install the T-section 04A-120 to the No. 4 support 04A-440, the No. 3 fwd support
04A-360, the No. 3 aft support 04A-380, the No. 2 fwd support 04A-220 and the No, 2 aft
support 04A-240 with the hi-loks 04A-030 and the collar 04A-020. See SRM 51-42-11 for
the installation of the hi-loks 04A-030 and the collar 04A-020.
(14) Install the T-section 04A-100 to the No. 2 fwd support 04A-220, the No. 2 aft support
04A-240 and the No. 1 support 04A-190 with the rivets 04A-040 and the screws 04A-090.
See SRM 51-42-11 for the installation of the rivets 04-040.
(15) Identify the mating surfaces of the teflon sheet 04A-050 with the T-sections 04A-100 and
04A-120. On the mating surfaces of the teflon sheet 04A-050 only, do a pre-treatment
according to ABP51148, See PMS 01-02-31 Pre-Treatment of the P. T. F. E. Surfaces.
(16) Identify the mating surfaces of the T-sections 04A-100 and 04A-120 with the teflon sheet
04A-050. On the mating surfaces of the T-sections 04A-100 and 04A-120 only, examine the
condition of the bonding primer.
(17) If the bonding primer of the T-section 04A-100, 04A-120 and 04A-140, and the plate
04A-510 is damaged, do the subsequent steps.
(a) Remove the bonding primer with emery cloth Grade 240 to 400 .
(b) Clean the mating surfaces of the T-section 04A-100, 04A-120 and 04A-140, and the
plate 04A-510 with Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-
Ketone -.
(c) Apply bonding primer to the mating surfaces of the T-section 04A-100, 04A-120 and
04A-140, and the plate 04A-510, according to ABP4-1123. See PMS 01-02-27
Application of Primer.
(18) Rub lightly the mating surfaces of the T-sections 04A-100 and 04A-120 with emery cloth
Grade 240 to 400.

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(19) Clean the mating surfaces of the T-sections 04A-100 and 04A-120 with Material No.
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(20) Apply Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy to the mating surfaces
of the T-sections 04A-100 and 04A-120 and the teflon sheet 04A-050.
(21) Install the teflon sheet 04A-050 on the T-sections 04A-100 and 04A-120. Install the bolts
04A-010 thru the teflon sheet 04A-050 the T-section 04A-120 and the No. 4 support
04A-440. Apply pressure and let the adhesive cure. See SRM 51-42-21 for the installation
of the bolts 04A-010.
(22) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to all fastener
heads.

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D5288000800000

**For PN’s D5288001000000 D5288001000098 D5288001000100 D5288001000198

TASK 52-81-14-300-807-C01
Replacement of the Lateral Ramp and the Ramp Assy
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
14QGC1 Wire-Locking Dia: 1 mm (0.041 inch) CRES -
06AAC1 Polysulfide Sealant-General Purpose Interfay -
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
13AEC1 Dry glass fabric-8H Satin 293 gsm - 181 style SRM Type 2 -
05EML7 Epoxy Adhesive-- - Legacy 3
05EJL9 Epoxy Adhesive-Metal to metal - Legacy
Consumable Materials
TABLE 1

B. Fixtures, Tools, Test and Support Equipment

REFERENCE DESIGNATION
non-metallic scraper
Fixtures, Tools, Test and Support Equipment
TABLE 2

C. Referenced Information
REFERENCE DESIGNATION
SRM 51-42-11
SRM 51-42-21
PMS 01-02-31
PMS 01-02-27
Referenced Information
TABLE 3

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COMPONENT MAINTENANCE MANUAL
D5288000800000

3. Procedure

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

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

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.

CAUTION : USE ONLY SPECIFIED CLEANING MATERIALS AND SOLUTIONS OR THEIR

EQUIVALENTS. THE SURFACE PROTECTION COULD BE DAMAGED IF
UNSPECIFIED MATERIALS ARE USED. IT IS IMPORTANT THAT THE
MANUFACTURER’S MIXING, APPLICATION AND TREATMENT INSTRUCTIONS
ARE FOLLOWED.

Subtask 52-81-14-350-009-A01
A. Disassembly of the Lower Lateral Ramp

NOTE : See IPL_FIGURE_04C.

(1) Remove all Material No. 14QGC1 Wire-Locking Dia: 1 mm (0.041 inch) CRES - and
sealant from the fastener heads.
(2) Remove the bonded teflon sheet 04C-070 from the plate 04C-510 and the T-section
04C-140.
(3) Remove the old adhesive from the component parts with a non-metallic scraper.
(4) Remove the plate 04C-510 from the runout tip 04C-540 by removing the screw 04C-500,
the blind bolts 04C-480 and the nut 04C-490. See SRM 51-42-11 for the removal of the
blind bolts 04C-480.
(5) Remove the T-section 04C-140 from the tip support 04C-560 and the No. 4 moveable
support 04C-420 by removing the rivets 04C-040. See SRM 51-42-11 for the removal of the
rivets 04C-040.
(6) Remove the tip support 04C-560 from the cover assembly by removing the screws 04C-210.
(7) Remove the bolts 04C-400, the washer 04C-410 and the No. 4 moveable support 04C-420
from the isolator 04C-470.
(8) Remove the runout tip 04C-540 from the cover assembly by removing the screws 04C-210,
the hi-loks 04C-030, the collar 04C-020 and the rivets 04C-040 and 04C-530. See SRM
51-42-11 for the removal of the hi-loks 04C-030, the collar 04C-020 and the rivets 04C-040
and 04C-530.

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Subtask 52-81-14-350-010-A01
B. Disassembly of the Upper Lateral Ramp

NOTE : See IPL_FIGURE_04C.

(1) Remove all Material No. 14QGC1 Wire-Locking Dia: 1 mm (0.041 inch) CRES - and
sealant from the fastener heads.
(2) Remove the bolts 04C-010 from the teflon sheet 04C-050 and remove the bonded teflon
sheet 04C-050 from the T-sections 04C-100 and 04C-120. See SRM 51-42-21 for the
removal of the bolts 04C-010.
(3) Remove the old adhesive from the component parts with a non-metallic scraper.
(4) Remove the T-section 04C-120 from the No. 4 support assembly 04C-440, the No. 3 fwd
support assembly 04C-600, the No. 3 aft support assembly 04C-620, the No. 2 fwd support
assembly 04C-220 and the No. 2 aft support assembly 04C-240 by removing the hi-loks
04C-030, the collar 04C-020 and the rivets 04C-040. See SRM 51-42-11 for the removal of
the hi-loks 04C-030, the collar 04C-020 and the rivets 04C-040.
(5) Remove the T-section 04C-100 from the No. 2 fwd support assembly 04C-220, the No. 2
aft support assembly 04C-240 and the No. 1 support 04C-190 by removing the rivets
04C-040 and the screws 04C-090.
(6) Remove the No. 4 support assembly 04C-440 by removing the bolts 04C-260 and 04C-270.
See SRM 51-42-11 for the removal of the rivets 04C-040.
(7) Remove the isolators 04C-470 by removing the rivets 04C-460. See SRM 51-42-11 for the
removal of the rivets 04C-460.
(8) Remove the No. 3 fwd support 04C-600 by removing the bolts 04C-260.
(9) Remove the No. 3 aft support 04C-620 by removing the bolts 04C-260.
(10) Remove the No. 2 fwd support 04C-220 by removing the screws 04C-210.
(11) Remove the No. 2 aft support 04C-240 by removing the screws 04C-210.
(12) Remove the No. 1 support 04C-190 by removing the screws 04C-160 and 04C-170.

Subtask 52-81-14-350-011-A01
C. Installation of the Lower Lateral Ramp

NOTE : See IPL_FIGURE_04C.

NOTE : Unless indicated, all fasteners and mating surfaces are to be wet installed with
Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay -.

NOTE : Where necessary use oversize fasteners.

(1) Remove all old sealant from the cover assembly and any components that were previously
removed.

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(2) Clean the surface of the cover assembly with Material No. 08BBF1 Non Aqueous Cleaner--
Methyl-Ethyl-Ketone -.
(3) Cut a piece of Material No. 13AEC1 Dry glass fabric-8H Satin 293 gsm - 181 style SRM
Type 2 - to the shape of the runout tip 04C-540 and the tip support 04C-560.
(4) Apply Material No. 05EML7 Epoxy Adhesive-- - Legacy 3 to the glass fabric pieces and put
them in position on the cover assembly.
(5) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the mating
surfaces of the runout tip 04C-540, and the tip support 04C-560.

CAUTION : MAKE SURE THAT THE SCREWS HAVE A MINIMUM THREADED LENGTH
OF 5 MM (0.20 IN).
(6) Install the tip support 04C-560 with the screws 04C-210.
(7) Install the runout tip 04C-540 to the cover assembly with the screws 04C-210, the hi-loks
04C-030, the collar 04C-020 and the rivets 04C-040 and 04C-530. See SRM 51-42-21 for
the installation of the hi-loks 04C-030, the collar 04C-020 and the rivets 04C-040 and
04C-530.
(8) Install the plate 04C-510 to the runout tip 04C-540 with the blind bolts 04C-480, the screw
04C-500 and the nut 04C-490. See SRM 51-42-11 for the installation of the blind bolts
04C-480.
(9) Install the No. 4 support 04C-440 to the cover assembly with the bolts 04C-260 and
04C-270.
(10) Safety the bolts 04C-260 and 04C-270 with Material No. 14QGC1 Wire-Locking Dia: 1 mm
(0.041 inch) CRES - .
(11) Install the No. 4 movable support 04C-420 to the isolators 04C-470 with the bolts 04C-400
and the washers 04C-410.
(12) Install the T-section 04C-140 to the tip support 04C-560 and the No. 4 moveable support
04C-420 with the rivets 04C-040. See SRM 51-42-11 for the installation of the rivets
04C-040.
(13) Identify the mating surfaces of the teflon sheet 04C-070 with the T-section 04C-140 and
the plate 04C-510. On the mating surfaces of the teflon sheet 04C-070 only, do a pre-
treatment according to ABP5-1148 PMS 01-02-31 Pre-Treatment of the P. T. F. E.
Surfaces.
(14) Identify the mating surfaces of the T-section 04C-140 and the plate 04C-510 with the
teflon sheet 04C-070. On the mating surfaces of the T-section 04C-140 and the plate
04C-510 only, examine the condition of the bonding primer.
(15) If the bonding primer of the T-section 04C-100, 04C-120 and 04C-140, and the plate
04C-510 is damaged, do the subsequent steps.
(a) Remove the bonding primer with emery cloth Grade 240 to 400.

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(b) Clean the mating surfaces of the T-section 04C-100, 04C-120 and 04C-140, and the
plate 04C-510 with Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-
Ketone -.
(c) Apply bonding primer to the mating surfaces of the T-section 04C-100, 04C-120 and
04C-140, and the plate 04C-510, according to ABP4-1123, see PMS 01-02-27
Application of Primer.
(16) Rub Lightly the mating surfaces of the T-section 04C-140 and the plate 04C-510 with
emery cloth Grade 240 to 400 .
(17) Clean the mating surfaces of the T-section 04C-140 and the plate 04C-510 with Material
No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(18) Apply Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy to the mating surfaces
of the T-section 04C-140, the teflon sheet 04C-070 and the plate 04C-510.
(19) Install the teflon sheet 04C-070 on the T-section 04C-140 and the plate 04C-510. Apply
pressure and let the adhesive cure.
(20) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to all fastener
heads.

Subtask 52-81-14-350-012-A01
D. Installation of the Upper Lateral Ramp

NOTE : See IPL_FIGURE_04C.

NOTE : Unless indicated, all fasteners and mating surfaces are to be wet installed with
Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay -.

NOTE : Where necessary use oversize fasteners.

(1) Remove all old sealant from the cover assembly and any components that were previously
removed.
(2) Clean the surface of the cover assembly with Material No. 08BBF1 Non Aqueous Cleaner--
Methyl-Ethyl-Ketone -.
(3) Cut some pieces of Material No. 13AEC1 Dry glass fabric-8H Satin 293 gsm - 181 style
SRM Type 2 - to the shape of the No. 3 and No. 2 supports.
(4) Apply Material No. 05EML7 Epoxy Adhesive-- - Legacy 3 to the glass fabric pieces and put
them in position on the cover assembly.
(5) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the mating
surfaces of the No. 3, No. 2 and No. 1 supports.
(6) Install the No. 3 fwd and aft supports 04C-600 and 04C-620 to the cover assembly with the
bolts 04C-260.

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(7) Safety the bolts 04C-260 with Material No. 14QGC1 Wire-Locking Dia: 1 mm (0.041 inch)
CRES - .
(8) Install the No. 2 fwd and aft supports 04C-220 and 04C-240 with the screws 04C-210.
(9) Install the No. 1 support 04C-190 with the screws 04C-160 and 04C-170.
(10) Cut some pieces of Material No. 13AEC1 Dry glass fabric-8H Satin 293 gsm - 181 style
SRM Type 2 - to the upper shape of the No. 3 and No. 2 supports.
(11) Apply Material No. 05EML7 Epoxy Adhesive-- - Legacy 3 to the glass fabric pieces and put
them over the supports.
(12) Install the T-section 04C-120 to the No. 4 support 04C-440, the No. 3 fwd support
04C-600, the No. 3 aft support 04C-620, the No. 2 fwd support 04C-220 and the No. 2 aft
support 04C-240 with the hi-loks 04C-030 and the collar 04C-020. See SRM 51-42-11 for
the installation of the hi-loks 04C-030 and the collar 04C-020.
(13) Install the T-section 04C-100 to the No. 2 fwd support 04C-220, the No. 2 aft support
04C-240 and the No. 1 support 04C-190 with the rivets 04C-040 and the screws 04C-090.
See SRM 51-42-11 for the installation of the rivets 04C-040.
(14) Identify the mating surfaces of the teflon sheet 04C-050 with the T-sections 04C-100 and
04C-120, On the mating surfaces of the teflon sheet 04C-050 only, do a pre-treatment
according to ABP51148 , See PMS 01-02-31 Pre-Treatment of the P. T. F. E. Surfaces.
(15) Identify the mating surfaces of the T-sections 04C-100 and 04C-120 with the teflon sheet
04C-050. On the mating surfaces of the T-sections 04C-100 and 04C-120 only, examine the
condition of the bonding primer.
(16) If the bonding primer of the T-section 04C-100, 04C-120 and 04C-140, and the plate
04C-510 is damaged, do the subsequent steps.
(a) Remove the bonding primer with emery cloth Grade 240 to 400 .
(b) Clean the mating surfaces of the T-sections 04C-100, 04C-120 and 04C-140, and the
plate 04C-510 with Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-
Ketone -.
(c) Apply bonding primer to the mating surfaces of the T-section 04C-100, 04C-120 and
04C-140, and the plate 04C-510, according to ABP4-1123, see PMS 01-02-27
Application of Primer.
(17) Rub lightly the mating surfaces of the T-sections 04C-100 and 04C-120 with emery cloth
Grade 240 to 400 .
(18) Clean the mating surfaces of the T-sections 04C-100 and 04C-120 with Material No.
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(19) Apply Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy to the mating surfaces
of the T-sections 04C-100 and 04C-120 and the teflon sheet 04C-050.

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(20) Install the teflon sheet 04C-050 on the T-sections 04C-100 and 04C-120. Install the bolts
04C-010 thru the teflon sheet 04C-050, the T-section 04C-120 and the No. 4 support
04C-440. Apply pressure and let the adhesive cure. See SRM 51-42-21 for the installation
of the bolts 04C-010.
(21) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to all fastener
heads.

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COMPONENT MAINTENANCE MANUAL
D5288000800000

**For PN’s D5288000800094 D5288000800095 D5288000800194 D5288000800195 D5288000900094

D5288000900095 D5288000900194 D5288000900195 D5288001000094 D5288001000095 D5288001000194
D5288001000195

TASK 52-81-14-300-807-D01
Replacement of the Lateral Ramp and the Ramp Assy
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
06ABC1 Polysulfide Sealant-Fuel Tank Interfay -
06AAC1 Polysulfide Sealant-General Purpose Interfay -
06PAG1 Adhesion Promoter-For Polysulfide Sealant - -
06ACB1 Polysulfide Sealant-Low Density Multi Purpose Fillet -
04QAB2 Coating-- Flexible Structure
Consumable Materials
TABLE 1

B. Referenced Information
REFERENCE DESIGNATION
TASK 52-81-14-100-801-A01 Cleaning of the Painted Components
SRM 51-42-21
SRM 51-42-11
Referenced Information
TABLE 2

3. Procedure

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

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

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.

Page 6026
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COMPONENT MAINTENANCE MANUAL
D5288000800000

CAUTION : USE ONLY SPECIFIED CLEANING MATERIALS AND SOLUTIONS OR THEIR

EQUIVALENTS. THE SURFACE PROTECTION COULD BE DAMAGED IF
UNSPECIFIED MATERIALS ARE USED. IT IS IMPORTANT THAT THE
MANUFACTURER’S MIXING, APPLICATION AND TREATMENT INSTRUCTIONS
ARE FOLLOWED.

Subtask 52-81-14-350-019-A01
A. Removal of the Ramp Assy

NOTE : See IPL_FIGURE_04D.

(1) Removal of the ramp assy.

NOTE : This procedure is applicable to the ramp assy 04D-190.

(a) Remove the nuts 04D-050, the screws 04D-060 and the blind bolts 04D-070. See
SRM 51-42-21 for the removal of the blind bolts 04D-070.
(b) Remove the pin-cotter 04D-010, the nut 04D-020, the washer 04D-030 and the bolt
04D-040.
(c) Remove the ramp assy 04D-190 from the MLG door.
(2) Removal of the glider.

NOTE : This procedure is applicable to the glider 04D-202.

(a) Remove the bolt-blind 04D-205 and 04D-207. See SRM 51-42-11 for removal of the
bolt-blind 04D-205 and 04D-207.
(b) Remove the glider 04D-202 from the ramp assy 04D-190.
(3) Removal of the support.

NOTE : This procedure is applicable to the support 04D-090.

(a) Remove the bolts 04D-080.
(b) Remove the support 04D-090 from the MLG door.
(4) Removal of the runout tip.

NOTE : This procedure is applicable to the runout tip 04D-160.

(a) Remove the collars 04D-130, the hi-loks 04D-140, the rivets 04D-150, and the screws
04D-120. See SRM 51-42-11 for removal of the hi-loks 04D-140 and the rivets
04D-150.
(b) Remove the runout tip 04D-160 from the MLG door.
(5) Removal of the angles.

NOTE : This procedure is applicable to the angles 04D-210, 04D-230 and 04D-250.

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(a) Remove the collars 04D-280 and the rivet pins 04D-270, 04D-290. See SRM 51-42-11
for removal of the the collars 04D-280 and the rivet pins 04D-270, 04D-290.
(b) Remove the angles 04D-230, 04D-210 and 04D-250 from the runout tip 04D-160.

Subtask 52-81-14-350-020-A01
B. Installation of the Ramp Assy

NOTE : See IPL_FIGURE_04D.

NOTE : This procedure is applicable to the ramp assy 04D-190.

NOTE : Unless indicated, all fasteners and mating surfaces are to be wet installed with
Material No. 06ABC1 Polysulfide Sealant-Fuel Tank Interfay -.

NOTE : Where necessary use oversize fasteners.

(1) Installation of the angles.

NOTE : This procedure is applicable to the angles 04D-210, 04D-230 and 04D-250.
(a) Clean the mating surfaces of the angles 04D-210, 04D-230, 04D-250 and the runout
tip 04D-160. See TASK 52-81-14-100-801-A01.
(b) Apply a layer of Material No. 06ABC1 Polysulfide Sealant-Fuel Tank Interfay - to the
mating surfaces of the angles 04D-210, 04D-230 and 04D-250, and the runout tip
04D-160.
(c) Put the angles 04D-210, 04D-230 and 04D-250 in the correct position on the runout
tip 04D-160.
(d) Install the rivet pins 04D-270 and 04D-290, soaked with Material No. 06ABC1
Polysulfide Sealant-Fuel Tank Interfay -, and the collars 04D-280. See SRM 51-42-11
for the installation of the collars 04D-280 and the rivet pins 04D-270, 04D-290.
(e) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
heads of the rivet pins 04D-270 and 04D-290 and the collars 04D-280.
(f) Apply a fillet of Material No. 06PAG1 Adhesion Promoter-For Polysulfide Sealant - -
to the edges of the mating surfaces of the angles 04D-210, 04D-230 and 04D-250,
and the runout tip 04D-160. Let the sealant dry.
(g) Apply a fillet of Material No. 06ACB1 Polysulfide Sealant-Low Density Multi Purpose
Fillet -on Material No. 06PAG1 Adhesion Promoter-For Polysulfide Sealant - -. Let
the sealant dry.
(h) Apply a fillet of Material No. 04QAB2 Coating-- Flexible Structure on Material No.
06ACB1 Polysulfide Sealant-Low Density Multi Purpose Fillet -.
(2) Installation of the runout tip.

NOTE : This procedure is applicable to the runout tip 04D-160.

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(a) Clean the mating surfaces of the runout tip 04D-160 and the MLG door. See TASK
52-81-14-100-801-A01.
(b) Apply a layer of Material No. 06ABC1 Polysulfide Sealant-Fuel Tank Interfay - to the
mating surfaces of the ramp assy 04D-190 and the runout tip 04D-160.
(c) Put the runout tip 04D-160 on the MLG door in the correct position.
(d) Install the hi-loks 04D-140 and the rivets 04D-150. See SRM 51-42-11 for installation
of the hi-loks 04D-140 and the rivets 04D-150.

CAUTION : MAKE SURE THAT THE SCREWS HAVE A MINIMUM THREADED

LENGTH OF 5 MM (0.20 IN).
(e) Install the screws 04D-120, soaked with Material No. 06ABC1 Polysulfide Sealant-
Fuel Tank Interfay -, and the collars 04D-130. See SRM 51-42-11 for installation of
the collars 04D-130.
(f) Tighten the collars 04D-130.
(g) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
heads of the hi-loks 04D-140, the rivets 04D-150, the screws 04D-120 and the collars
04D-130.
(h) Apply a fillet of Material No. 06PAG1 Adhesion Promoter-For Polysulfide Sealant - -
to the edges of the mating surfaces of the MLG door and the runout tip 04D-160. Let
the sealant dry.
(i) Apply a fillet of Material No. 06ACB1 Polysulfide Sealant-Low Density Multi Purpose
Fillet - on Material No. 06PAG1 Adhesion Promoter-For Polysulfide Sealant - -. Let
the sealant dry.
(j) Apply a fillet of Material No. 04QAB2 Coating-- Flexible Structure on Material No.
06ACB1 Polysulfide Sealant-Low Density Multi Purpose Fillet -.
(3) Installation of the support.

NOTE : This procedure is applicable to the support 04D-090.

(a) Clean the mating surfaces of the support 04D-090 and the MLG door. See TASK
52-81-14-100-801-A01.
(b) Put the support 04D-090 on the MLG door in the correct position.

CAUTION : MAKE SURE THAT THE BOLTS HAVE A MINIMUM THREADED

LENGHT OF 6 MM (0.23 IN).
(c) Install the support 04D-090 with the bolts 04D-040, soaked with Material No.
06ABC1 Polysulfide Sealant-Fuel Tank Interfay -. Tighten the bolts 04D-040.
(d) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
head of the bolts 04D-040.

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(e) Apply a fillet of Material No. 06PAG1 Adhesion Promoter-For Polysulfide Sealant - -
to the edges of the mating surfaces of the support 04D-090 and the MLG door. Let
the sealant dry.
(f) Apply a fillet of Material No. 06ACB1 Polysulfide Sealant-Low Density Multi Purpose
Fillet - on Material No. 06PAG1 Adhesion Promoter-For Polysulfide Sealant - -. Let
the sealant dry.
(g) Apply a fillet of Material No. 04QAB2 Coating-- Flexible Structure on Material No.
06ACB1 Polysulfide Sealant-Low Density Multi Purpose Fillet -.
(4) Installation of the glider.

NOTE : This procedure is applicable to the glider 04D-203.

(a) Clean the mating surfaces of the glider 04D-203 and the ramp assy 04D-190. See
TASK 52-81-14-100-801-A01.
(b) Apply a layer of Material No. 06ABC1 Polysulfide Sealant-Fuel Tank Interfay -
between the mating surfaces of the glider 04D-203 and the ramp assy 04D-190.
(c) Put the glider 04D-203 in the ramp assy 04D-190 in the correct position.
(d) Install the bolt-blind 04D-205 and 04D-207 to attach the glider 04D-203 in the ramp
assy 04D-190. See SRM 51-42-11 for installation of the bolt-blind 04D-205 and
04D-207.
(e) Apply a fillet of Material No. 06PAG1 Adhesion Promoter-For Polysulfide Sealant - -
to the edges of the mating surfaces of the glider 04D-203 and the ramp assy 04D-190.
Let the sealant dry.
(f) Apply a fillet of Material No. 06ACB1 Polysulfide Sealant-Low Density Multi Purpose
Fillet - on Material No. 06PAG1 Adhesion Promoter-For Polysulfide Sealant - -. Let
the sealant dry.
(g) Apply a fillet of Material No. 04QAB2 Coating-- Flexible Structure on Material No.
06ACB1 Polysulfide Sealant-Low Density Multi Purpose Fillet -.
(5) Installation of the ramp assy.

NOTE : This procedure is applicable to the ramp assy 04D-190.

(a) Clean the mating surfaces between the ramp assy 04D-190 the runout tip 04D-160
and the MLG door. See TASK 52-81-14-100-801-A01.
(b) Apply a layer of Material No. 06ABC1 Polysulfide Sealant-Fuel Tank Interfay -
between the mating surfaces between the ramp assy 04D-190 the runout tip 04D-160
and the MLG door.
(c) Put the ramp assy 04D-190 in the correct position.
(d) Install the washer 04D-030, the bolt 04D-040 and the nut 04D-020.

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(e) Install the screws 04D-060 and the blind bolts 04D-070 and the nuts 04D-050. See
SRM 51-42-21 for the installation of the blind bolts 04D-070.
(f) Tighten the nuts 04D-020 and 04D-050.
(g) Install the new pin-cotter 04D-010.
(h) Apply a fillet of Material No. 06PAG1 Adhesion Promoter-For Polysulfide Sealant - -
to the edges of the mating surfaces of the ramp assy 04D-190 and the MLG door, and
the runout tip 04D-160. Let the sealant dry.
(i) Apply a fillet of Material No. 06ACB1 Polysulfide Sealant-Low Density Multi Purpose
Fillet - on Material No. 06PAG1 Adhesion Promoter-For Polysulfide Sealant - -. Let
the sealant dry.
(j) Apply a fillet of Material No. 04QAB2 Coating-- Flexible Structure on Material No.
06ACB1 Polysulfide Sealant-Low Density Multi Purpose Fillet -.

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D5288000800000

**For PN’s D5288000800000 D5288000800100 D5288000900000 D5288000900100

TASK 52-81-14-300-810-A01
Replacement of the Central Ramp
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
06AAC1 Polysulfide Sealant-General Purpose Interfay -
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
13AEC1 Dry glass fabric-8H Satin 293 gsm - 181 style SRM Type 2 -
13FBB1 Paste Adhesive-Epoxy Composite General Use -
05EJL9 Epoxy Adhesive-Metal to metal - Legacy
Consumable Materials
TABLE 1

B. Fixtures, Tools, Test and Support Equipment

REFERENCE DESIGNATION
non-metallic scraper
Fixtures, Tools, Test and Support Equipment
TABLE 2

C. Referenced Information
REFERENCE DESIGNATION
SRM 51-42-11
PMS 01-02-31
PMS 01-02-26
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 SPECIFIED CLEANING MATERIALS AND SOLUTIONS OR THEIR

EQUIVALENTS. THE SURFACE PROTECTION COULD BE DAMAGED IF
UNSPECIFIED MATERIALS ARE USED. IT IS IMPORTANT THAT THE
MANUFACTURER’S MIXING, APPLICATION AND TREATMENT INSTRUCTIONS
ARE FOLLOWED.

Subtask 52-81-14-300-039-A01
A. Replacement of the Central Ramp
PRE MOD 21514
(1) Removal of the central ramp.

NOTE : This procedure is applicable to the central ramp 05-001.

NOTE : See IPL_FIGURE_05.

(a) Remove all sealant from the fastener heads.
(b) Remove the screws 05-120 from the teflon sheet 05-010.
(c) Remove the rivets 05-030 from the ramp blister 05-250 and the teflon sheet 05-010.
See SRM 51-42-11 for removal of the rivets 05-030.
(d) Remove the bonded teflon sheet 05-010 from the ramp blister 05-250 and the T-
sections 05-090 and 05-110.
(e) Remove the old adhesive from the component parts with a non-metallic scraper.
(f) Remove the rivets 05-040 and the blind bolts 05-080. See SRM 51-42-11 for removal
of the rivets 05-040 and the blind bolts 05-080.
(g) Remove the T-section 05-110.
(h) Remove the rivets 05-040 and the blind bolts 05-050, 05-060 and 05-070. See SRM
51-42-11 for removal of the rivets 05-040 and the blind bolts 05-050, 05-060 and
05-070.
(i) Remove the T-section 05-090.
(j) Remove the screws 05-120 and 05-240, the washers 05-230 and the nuts 05-220.
(k) Remove the ramp blister 05-250.
(l) Remove the screws 05-120.
(m) Remove the runout tip 05-200.
(n) Remove the screws 05-120.
(o) Remove the No. 2 FWD support 05-160.
(p) Remove the screws 05-120.
(q) Remove the No. 2 AFT support 05-180.

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(r) Remove the No. 1 support 05-140 from the cover assembly.
(2) Installation of the central ramp.

NOTE : This procedure is applicable to the central ramp 05-001.

NOTE : See IPL_FIGURE_05.

NOTE : Unless indicated, all fasteners and mating surfaces are to be wet installed with
Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay -.

NOTE : Where necessary use oversize fasteners.

(a) Remove all old sealant from the cover assembly and any components that were
previously removed.
(b) Clean the surface of the cover assembly with Material No. 08BBF1 Non Aqueous
Cleaner-- Methyl-Ethyl-Ketone -.
(c) Cut some pieces of Material No. 13AEC1 Dry glass fabric-8H Satin 293 gsm - 181
style SRM Type 2 - to the shape runout tip 05-200, the No. 2 FWD and AFT
supports 05-160 and 05-180, and No. 1 support 05-140.
(d) Apply Material No. 13FBB1 Paste Adhesive-Epoxy Composite General Use - to the
glass fabric pieces and put them in position on the cover assembly.
(e) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surfaces of the runout tip, the No. 2 and the No. 1 supports.
(f) Install the No. 2 AFT support 05-180 with the screws 05-120.
(g) Install the No. 2 FWD support 05-160 with the screws 05-120.
(h) Install the runout tip 05-200 with the screws 05-120.
(i) Tighten the screws 05-120.
(j) Install the T-section 05-110 to the runout tip 05-200 with the blind bolts 05-080 and
to the No. 2 FWD support 05-160 and the No. 2 AFT support 05-180 with the rivets
05-040. See SRM 51-42-11 for installation of the rivets 05-040 and the blind bolts
05-080.
(k) Install the T-section 05-090 to the No. 2 FWD support 05-160 and the No. 2 AFT
support 05-180 with the rivets 05-040 and together with the No. 1 support 05-140
with the blind bolts 05-050, 05-060 and 05-070 to the cover assembly. See SRM
51-42-11 for installation of the rivets 05-040 and the blind bolts 05-050, 05-060 and
05-070.
(l) Apply Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy to the mating
surfaces of the ramp blister 05-250 and the No. 1 support 05-140.
(m) Install the ramp blister 05-250 with the screws 05-120 and 05-240, the washers
05-230 and the nuts 05-220.

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(n) Identify the mating surfaces of the teflon sheet 05-010 with the ramp blister 05-250
and the T-sections 05-090 and 05-110. On the mating surfaces of the teflon sheet
05-010 only, do a pretreatment according to ABP5-1148 PMS 01-02-31 Pre-
Treatment of the P. T. F. E. Surfaces.
(o) Identify the mating surfaces of the ramp blister 05-250 and the T-sections 05-090 and
05-110 with the teflon sheet 05-010. On the mating surfaces of the ramp blister
05-250 of the T-sections 05-090 and 05-110 only, examine the condition of the
bonding primer.
(p) If the bonding primer of the ramp blister 05-250 and the T-sections 05-090 and
05-110 is damaged, do the subsequent steps.
1 Remove the bonding primer with emery cloth Grade 240 to 400 .
2 Clean the mating surfaces of the ramp blister 05-250 and the T-sections 05-090
and 05-110 with Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-
Ketone -.
3 Apply bonding primer to the mating surfaces of the ramp blister 05-250 and the
T-sections 05-090 and 05-110, according to ABP4-1123 PMS 01-02-26
application of primer.
(q) Rub lightly the mating surfaces of the ramp blister 05-250 and the T-sections 05-090
and 05-110 with emery cloth Grade 240 to 400 .
(r) Clean the mating surfaces of the ramp blister 05-250 and the T-sections 05-090 and
05-110 with Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(s) Apply Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy to the mating
surfaces of the T-sections 05-090 and 05-110, the ramp blister 05-250 and the teflon
sheet 05-010.
(t) Install the teflon sheet 05-010 on the T-sections 05-090, 05-110 and the ramp blister
05-250. Install the screws 05-120 and the rivets 05-030 thru the teflon sheet 05-010
and the ramp blister 05-250. Apply pressure and let the adhesive cure. See SRM
51-42-11 for installation of the rivets 05-030.
(u) Tighten the screws 05-120.
(v) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to all
fastener heads.
POST MOD 21514
(1) Removal of the central ramp.

NOTE : See IPL_FIGURE_05B.

NOTE : This procedure is applicable to the central ramp 05B-001.

(a) Remove all sealant from the fastener heads.

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(b) Remove the screws 05B-120 from the teflon sheet 05B-01005-010.
(c) Remove the rivets 05B-030 from the ramp blister 05B-250 and the teflon sheet
05B-010. See SRM 51-42-11 for removal of the rivets 05B-030.
(d) Remove the bonded teflon sheet 05B-010 from the ramp blister 05B-250 and the T-
sections 05B-090 and 05B-110.
(e) Remove the old adhesive from the component parts with a non-metallic scraper.
(f) Remove the rivets 05B-040 and the blind bolts 05B-080. See SRM 51-42-11 for
removal of the rivets 05B-040 and the blind bolts 05B-080.
(g) Remove the T-section 05B-110.
(h) Remove the rivets 05B-040 and the blind bolts 05B-050, 05B-060 and 05B-070. See
SRM 51-42-11 for removal of the rivets 05B-040 and the blind bolts 05B-050,
05B-060 and 05B-070.
(i) Remove the T-section 05B-090.
(j) Remove the screws 05B-120 and 05B-240, the washers 05B-230 and the nuts
05B-220. Remove the angles 05B-290 and 05B-310 from the ramp blister 05B-250 by
removing the rivets 05B-330.
(k) Remove the ramp blister 05B-250.
(l) Remove the screws 05B-120.
(m) Remove the runout tip 05B-200.
(n) Remove the screws 05B-120.
(o) Remove the No. 2 FWD support 05B-160.
(p) Remove the screws 05B-120.
(q) Remove the No. 2 AFT support 05B-180.
(r) Remove the No. 1 support 05B-140 from the cover assembly.
(2) Installation of the central ramp.

NOTE : See IPL_FIGURE_05B.

NOTE : This procedure is applicable to the central ramp 05B-001.

NOTE : Unless indicated, all fasteners and mating surfaces are to be wet installed with
Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay -.

NOTE : Where necessary use oversize fasteners.

(a) Remove all old sealant from the cover assembly and any components that were
previously removed.

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(b) Clean the surface of the cover assembly with Material No. 08BBF1 Non Aqueous
Cleaner-- Methyl-Ethyl-Ketone -.
(c) Cut some pieces of Material No. 13AEC1 Dry glass fabric-8H Satin 293 gsm - 181
style SRM Type 2 - to the shape runout tip 05B-200, the No. 2 FWD and AFT
supports 05B-160 and 05B-180, and No. 1 support 05B-140.
(d) Apply Material No. 13FBB1 Paste Adhesive-Epoxy Composite General Use - to the
glass fabric pieces and put them in position on the cover assembly.
(e) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surfaces of the runout tip, the No. 2 and the No. 1 supports.
(f) Install the No. 2 AFT support 05B-180 with the screws 05B-120.
(g) Install the No. 2 FWD support 05B-160 with the screws 05B-120.
(h) Install the runout tip 05B-200 with the screws 05B-120.
(i) Tighten the screws 05B-120.
(j) Install the T-section 05B-110 to the runout tip 05B-200 with the blind bolts 05B-080
and to the No. 2 FWD support 05B-160 and the No. 2 AFT support 05B-180 with
the rivets 05B-040. See SRM 51-42-11 for installation of the rivets 05B-040 and the
blind bolts 05B-080.
(k) Install the T-section 05B-090 to the No. 2 FWD support 05B-160 and the No. 2 AFT
support 05B-180 with the rivets 05B-040 and together with the No. 1 support
05B-140 with the blind bolts 05B-050, 05B-060 and 05B-070 to the cover assembly.
See SRM 51-42-11 for installation of the rivets 05B-040 and the blind bolts 05B-050,
05B-060 and 05B-070.
(l) Apply Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy to the mating
surfaces of the ramp blister 05B-250 and the No. 1 support 05B-140.
(m) Install the ramp blister 05B-250 with the screws 05B-120 and 05B-240, the washers
05B-230 and the nuts 05B-220.
(n) Install the angles 05B-290 and 05B-310 with the screws 05B-120 and the rivets
05B-330.
(o) Identify the mating surfaces of the teflon sheet 05B-010 with the ramp blister
05B-250 and the T-sections 05B-090 and 05B-110. On the mating surfaces of the
teflon sheet 05B-010 only, do a pretreatment according to ABP5-1148 PMS 01-02-31
Pre-Treatment of the P. T. F. E. Surfaces.
(p) Identify the mating surfaces of the ramp blister 05B-250 and the T-sections 05B-090
and 05B-110 with the teflon sheet 05B-010. On the mating surfaces of the ramp
blister 05B-250 of the T-sections 05B-090 and 05B-110 only, examine the condition
of the bonding primer.

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(q) If the bonding primer of the ramp blister 05B-250 and the T-sections 05B-090 and
05B-110 is damaged, do the subsequent steps.
1 Remove the bonding primer with emery cloth Grade 240 to 400 .
2 Clean the mating surfaces of the ramp blister 05B-250 and the T-sections
05B-090 and 05B-110 with Material No. 08BBF1 Non Aqueous Cleaner--
Methyl-Ethyl-Ketone -.
3 Apply bonding primer to the mating surfaces of the ramp blister 05B-250 and
the T-sections 05B-090 and 05B-110, according to ABP4-1123 PMS 01-02-26
application of primer.
(r) Rub lightly the mating surfaces of the ramp blister 05B-250 and the T-sections
05B-090 and 05B-110 with emery cloth Grade 240 to 400 .
(s) Clean the mating surfaces of the ramp blister 05B-250 and the T-sections 05B-090
and 05B-110 with Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone
-.
(t) Apply Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy to the mating
surfaces of the T-sections 05B-090 and 05B-110, the ramp blister 05B-250 and the
teflon sheet 05B-010.
(u) Install the teflon sheet 05B-010 on the T-sections 05B-090, 05B-110 and the ramp
blister 05B-250. Install the screws 05B-120 and the rivets 05B-030 thru the teflon
sheet 05B-010 and the ramp blister 05B-250. Apply pressure and let the adhesive
cure. See SRM 51-42-11 for installation of the rivets 05B-030.
(v) Tighten the screws 05B-120.
(w) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to all
fastener heads.
ALL VARIANTS
(3) Not apply.

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COMPONENT MAINTENANCE MANUAL
D5288000800000

**For PN’s D5288001000000 D5288001000100

TASK 52-81-14-300-810-B01
Replacement of the Central Ramp
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
06AAC1 Polysulfide Sealant-General Purpose Interfay -
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
13AEC1 Dry glass fabric-8H Satin 293 gsm - 181 style SRM Type 2 -
13FBB1 Paste Adhesive-Epoxy Composite General Use -
05EJL9 Epoxy Adhesive-Metal to metal - Legacy
Consumable Materials
TABLE 1

B. Fixtures, Tools, Test and Support Equipment

REFERENCE DESIGNATION
non-metallic scraper
Fixtures, Tools, Test and Support Equipment
TABLE 2

C. Referenced Information
REFERENCE DESIGNATION
SRM 51-42-11
PMS 01-02-31
PMS 01-02-26
Referenced Information
TABLE 3

3. Procedure

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

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

Page 6039
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 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

CAUTION : USE ONLY SPECIFIED CLEANING MATERIALS AND SOLUTIONS OR THEIR

EQUIVALENTS. THE SURFACE PROTECTION COULD BE DAMAGED IF
UNSPECIFIED MATERIALS ARE USED. IT IS IMPORTANT THAT THE
MANUFACTURER’S MIXING, APPLICATION AND TREATMENT INSTRUCTIONS
ARE FOLLOWED.

Subtask 52-81-14-300-040-A01
A. Replacement of the Central Ramp
PRE MOD 21514 AND PRE SB 52-1025
(1) Removal of the Central Ramp

NOTE : See IPL_FIGURE_05A.

NOTE : This procedure is applicable to the central ramp 05A-001.

(a) Remove all sealant from the fastener heads.
(b) Remove the screws 05A-120 from the teflon sheet 05A-010.
(c) Remove the bonded teflon sheet 05A-010 from the ramp blister 05A-250 and the T-
sections 05A-090 and 05A-110.
(d) Remove the old adhesive from the component parts with a non-metallic scraper.
(e) Remove the rivets 05A-040 and the blind bolts 05A-080. See SRM 51-42-11 for
removal of the rivets 05A-040 and the blind bolts 05A-080.
(f) Remove the T-section 05A-110.
(g) Remove the rivets 05A-040 and the blind bolts 05A-050, 05A-060 and 05A-070. See
SRM 51-42-11 for removal of the rivets 05A-040 and the blind bolts 05A-050,
05A-060 and 05A-070.
(h) Remove the T-section 05A-090.
(i) Remove the screws 05A-120, 05A-240 and 05A-245, the washers 05A-230 and
05A-235 and the nuts 05A-220 and 05A-225.
(j) Remove the ramp blister 05A-250.
(k) Remove the screws 05A-120.
(l) Remove the runout tip 05A-200.
(m) Remove the screws 05A-120.
(n) Remove the No. 2 fwd support 05A-160.
(o) Remove the screws 05A-120.
(p) Remove the No. 2 aft support 05A-180.
(q) Remove the No. 1 support 05A-140 from the cover assembly.

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(2) Installation of the central ramp.

NOTE : See IPL_FIGURE_05A.

NOTE : This procedure is applicable to the central ramp 05A-001.

NOTE : Unless indicated, all fasteners and mating surfaces are to be wet installed with
Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay -.

NOTE : Where necessary use oversize fasteners.

(a) Remove all old sealant from the cover assembly and any components that were
previously removed.
(b) Clean the surface of the cover assembly with Material No. 08BBF1 Non Aqueous
Cleaner-- Methyl-Ethyl-Ketone -.
(c) Cut some pieces of Material No. 13AEC1 Dry glass fabric-8H Satin 293 gsm - 181
style SRM Type 2 - to the shape runout tip 05A-200, the No. 2 fwd and aft supports
05A-160 and 05A-180 and No. 1 support 05A-140.
(d) Apply Material No. 13FBB1 Paste Adhesive-Epoxy Composite General Use - to the
glass fabric pieces and put them in position on the cover assembly.
(e) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surfaces of the runout tip, the No. 2 and the No. 1 supports.
(f) Install the No. 2 aft support 05A-180 with the screws 05A-120.
(g) Install the No. 2 fwd support 05A-160 with the screws 05A-120.
(h) Install the runout tip 05A-200 with the screws 05A-120.
(i) Tighten the screws 05A-120.
(j) Install the T-section 05A-110 to the runout tip 05A-200 with the blind bolts 05A-080
and to the No. 2 fwd support 05A-160 and the No. 2 aft support 05A-180 with the
rivets 05A-040. See SRM 51-42-11 for installation of the rivets 05A-040 and the blind
bolts 05A-080.
(k) Install the T-section 05A-090 to the No. 2 fwd support 05A-160 and the No. 2 aft
support 05A-180 with the rivets 05A-040 and together with the No. 1 support
05A-140 with the blind bolts 05A-050, 05A-060 and 05A-070 to the cover assembly.
See SRM 51-42-11 for installation of the rivets 05A-040 and the blind bolts 05A-050,
05A-060 and 05A-070.
(l) Apply Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy to the mating
surfaces of the ramp blister 05A-250 and the No. 1 support 05A-140.
(m) Install the ramp blister 05A-250 with the screws 05A-120, 05A-240 and 05A-245, the
washers 05A-230 and 05A-235 and the nuts 05A-220 and 05A-225.

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(n) Identify the mating surfaces of the teflon sheet 05A-010 with the ramp blister
05A-250 and the T-sections 05A-090 and 05A-110. On the mating surfaces of the
teflon sheet 05A-010 only, do a pretreatment according to ABP5-1148 PMS 01-02-31
Pre-Treatment of the P. T. F. E. Surfaces.
(o) Identify the mating surfaces of the ramp blister 05A-250 and the T-sections 05A-090
and 05A-110 with the teflon sheet 05A-010. On the mating surfaces of the ramp
blister 05A-250 of the T-sections 05A-090 and 05A-110 only, examine the condition
of the bonding primer.
(p) If the bonding primer of the ramp blister 05A-250 and the T-sections 05A-090 and
05A-110 is damaged, do the subsequent steps.
1 Remove the bonding primer with emery cloth Grade 240 to 400 .
2 Clean the mating surfaces of the ramp blister 05A-250 and the T-sections
05A-090 and 05A-110 with Material No. 08BBF1 Non Aqueous Cleaner--
Methyl-Ethyl-Ketone -.
3 Apply bonding primer to the mating surfaces of the ramp blister 05A-250 and
the T-sections 05A-090 and 05A-110, according to ABP4-1123 PMS 01-02-26
application of primer.
(q) Rub lightly the mating surfaces of the ramp blister 05A-250 and the T-sections
05A-090 and 05A-110 with emery cloth Grade 240 to 400 .
(r) Clean the mating surfaces of the ramp blister 05A-250 and the T-sections 05A-090
and 05A-110 with Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone
-.
(s) Apply Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy to the mating
surfaces of the T-sections 05A-090 and 05A-110, the ramp blister 05A-250 and the
teflon sheet 05A-010.
(t) Install the teflon sheet 05A-010 on the T-sections 05A-090 and 05A-110 and the ramp
blister 05A-250. Install the screws 05A-120 and the rivets 05A-040 thru the teflon
sheet 05A-010 and the ramp blister 05A-250. Apply pressure and let the adhesive
cure. See SRM 51-42-11 for installation of the rivets05A-040.
(u) Tighten the screws 05A-120.
(v) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to all
fastener heads.
POST MOD 21514 AND PRE SB 52-1025
(1) Removal of the central ramp.

NOTE : See IPL_FIGURE_05C.

NOTE : This procedure is applicable to the central ramp 05C-001.

(a) Remove all sealant from the fastener heads.

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(b) Remove the screws 05C-120 from the teflon sheet 05C-010.
(c) Remove the bonded teflon sheet 05C-010 from the ramp blister 05C-250 and the T-
sections 05C-090 and 05C-110.
(d) Remove the old adhesive from the component parts with a non-metallic scraper.
(e) Remove the rivets 05C-040 and the blind bolts 05C-080. See SRM 51-42-11 for
removal of the rivets 05C-040 and the blind bolts 05C-080.
(f) Remove the T-section 05C-110.
(g) Remove the rivets 05C-040 and the blind bolts 05C-050, 05C-060 and 05C-070. See
SRM 51-42-11 for removal of the rivets 05C-040 and the blind bolts 05C-050,
05C-060 and 05C-070.
(h) Remove the T-section 05C-090.
(i) Remove the screws 05C-120, 05C-240 and 05C-245, the washers 05C-230 and
05C-235 and the nuts 05C-220 and 05C-225.
(j) Remove the ramp blister 05C-250.
(k) Remove the rivets 05C-330. See SRM 51-42-11 for the removal of the rivets 05C-330.
(l) Remove the angles 05C-290 and 05C-310 from the ramp blister 05C-250.
(m) Remove the screws 05C-120.
(n) Remove the runout tip 05C-200.
(o) Remove the screws 05C-120.
(p) Remove the No. 2 fwd support 05C-160.
(q) Remove the screws 05C-120.
(r) Remove the No. 2 aft support 05C-180.
(s) Remove the No. 1 support 05C-140 from the cover assembly.
(2) Installation of the central ramp.

NOTE : See IPL_FIGURE_05C.

NOTE : This procedure is applicable to the central ramp 05C-001.

NOTE : Unless indicated, all fasteners and mating surfaces are to be wet installed with
Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay -.

NOTE : Where necessary use oversize fasteners.

(a) Remove all old sealant from the cover assembly and any components that were
previously removed.
(b) Clean the surface of the cover assembly with Material No. 08BBF1 Non Aqueous
Cleaner-- Methyl-Ethyl-Ketone -.

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(c) Cut some pieces of Material No. 13AEC1 Dry glass fabric-8H Satin 293 gsm - 181
style SRM Type 2 - to the shape runout tip 05C-200, the No. 2 fwd and aft supports
05C-160 and 05C-180 and No. 1 support 05C-140.
(d) Apply Material No. 13FBB1 Paste Adhesive-Epoxy Composite General Use - to the
glass fabric pieces and put them in position on the cover assembly.
(e) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surfaces of the runout tip, the No. 2 and the No. 1 supports.
(f) Install the No. 2 aft support 05C-180 with the screws 05C-120.
(g) Install the No. 2 fwd support 05C-160 with the screws 05C-120.
(h) Install the runout tip 05C-200 with the screws 05C-120.
(i) Tighten the screws 05C-120.
(j) Install the T-section 05C-110 to the runout tip 05C-200 with the blind bolts 05C-080
and to the No. 2 fwd support 05C-160 and the No. 2 aft support 05C-180 with the
rivets 05C-040. See SRM 51-42-11 for installation of the rivets 05C-040 and the blind
bolts 05C-080.
(k) Install the T-section 05C-090 to the No. 2 fwd support 05C-160 and the No. 2 aft
support 05C-180 with the rivets 05C-040 and together with the No. 1 support
05C-140 with the blind bolts 05C-050, 05C-060 and 05C-070 to the cover assembly.
See SRM 51-42-11 for installation of the rivets 05C-040 and the blind bolts 05C-050,
05C-060 and 05C-070.
(l) Apply Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy to the mating
surfaces of the ramp blister 05C-250 and the No. 1 support 05C-140.
(m) Install the ramp blister 05C-250 with the screws 05C-120, 05C-240 and 05C-245, the
washers 05C-230 and 05C-235 and the nuts 05C-220 and 05C-225.
(n) Install the angles 05C-290 and 05C-310 with the screws 05C-120 and the rivets
05C-330. See SRM 51-42-11 for installation of the rivets05C-330.
(o) Identify the mating surfaces of the teflon sheet 05C-010 with the ramp blister
05C-250 and the T-sections 05C-090 and 05C-110. On the mating surfaces of the
teflon sheet 05C-010 only, do a pretreatment according to ABP5-1148 PMS 01-02-31
Pre-Treatment of the P. T. F. E. Surfaces.
(p) Identify the mating surfaces of the ramp blister 05C-250 and the T-sections 05C-090
and 05C-110 with the teflon sheet 05C-010. On the mating surfaces of the ramp
blister 05C-250 of the T-sections 05C-090 and 05C-110 only, examine the condition of
the bonding primer.
(q) If the bonding primer of the ramp blister 05C-250 and the T-sections 05C-090 and
05C-110 is damaged, do the subsequent steps.
1 Remove the bonding primer with emery cloth Grade 240 to 400 .

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2 Clean the mating surfaces of the ramp blister 05C-250 and the T-sections
05C-090 and 05C-110 with Material No. 08BBF1 Non Aqueous Cleaner--
Methyl-Ethyl-Ketone -.
3 Apply bonding primer to the mating surfaces of the ramp blister 05C-250 and
the T-sections 05C-090 and 05C-110, according to ABP4-1123 PMS 01-02-26
application of primer.
(r) Rub lightly the mating surfaces of the ramp blister 05C-250 and the T-sections
05C-090 and 05C-110 with emery cloth Grade 240 to 400 .
(s) Clean the mating surfaces of the ramp blister 05C-250 and the T-sections 05C-090
and 05C-110 with Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone
-.
(t) Apply Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy to the mating
surfaces of the T-sections 05C-090 and 05C-110, the ramp blister 05C-250 and the
teflon sheet 05C-010.
(u) Install the teflon sheet 05C-010 on the T-sections 05C-090 and 05C-110 and the ramp
blister 05C-250. Install the screws 05C-120 and the rivets 05C-040 thru the teflon
sheet 05C-010 and the ramp blister 05C-250. Apply pressure and let the adhesive
cure. See SRM 51-42-11 for installation of the rivets 05C-040.
(v) Tighten the screws 05C-120.
(w) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to all
fastener heads.
ALL VARIANTS
(3) Not apply.

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**For PN’s D5288000800094 D5288000800095 D5288000800098 D5288000800194 D5288000800195

D5288000800198 D5288000900094 D5288000900095 D5288000900098 D5288000900194 D5288000900195
D5288000900198 D5288001000094 D5288001000095 D5288001000098 D5288001000194 D5288001000195
D5288001000198

TASK 52-81-14-300-810-C01
Replacement of the Central Ramp
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
06ADB1 Polysulfide Sealant-Fuel Contaminated Area Fillet -
06ABC1 Polysulfide Sealant-Fuel Tank Interfay -
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
05EJL9 Epoxy Adhesive-Metal to metal - Legacy
06ADA1 Polysulfide Sealant-Fuel Contaminated Area Brushable -
06AAC1 Polysulfide Sealant-General Purpose Interfay -
13AEC1 Dry glass fabric-8H Satin 293 gsm - 181 style SRM Type 2 -
13FBB1 Paste Adhesive-Epoxy Composite General Use -
04PAD2 Polyurethane Coating-- Abrasion Resistant Structure
Consumable Materials
TABLE 1

B. Fixtures, Tools, Test and Support Equipment

REFERENCE DESIGNATION
non-metallic scraper
Fixtures, Tools, Test and Support Equipment
TABLE 2

C. Referenced Information
REFERENCE DESIGNATION
SRM 51-42-11
PMS 01-02-31
SRM 51-75-11
SRM 51-75-12

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REFERENCE DESIGNATION
PMS 01-02-26
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 SPECIFIED CLEANING MATERIALS AND SOLUTIONS OR THEIR

EQUIVALENTS. THE SURFACE PROTECTION COULD BE DAMAGED IF
UNSPECIFIED MATERIALS ARE USED. IT IS IMPORTANT THAT THE
MANUFACTURER’S MIXING, APPLICATION AND TREATMENT INSTRUCTIONS
ARE FOLLOWED.

**For PN’s D5288000800095 D5288000800195 D5288000900095 D5288000900195

Subtask 52-81-14-300-035-A01
A. Replacement of the Central Ramp

NOTE : See IPL_FIGURE_05D.

NOTE : This procedure is applicable to the central ramp 05D-001.

(1) Removal of the central ramp.
(a) Remove the sealant from all the heads of the fasteners with a non-metallic scraper.
(b) Remove the nuts 05D-220, the washers 05D-230 and the screws 05D-120 and
05D-240.
(c) Remove the ramp blister 05D-250 from the MLG door.
(d) Remove the rivets 05D-030. See SRM 51-42-11 for removal of the rivets 05D-030.
(e) Remove the teflon sheet 05D-010 from the ramp blister 05D-250 and the T-sections
05D-090 and 05D-110.
(f) Remove the angles 05D-290, 05D-310, 05D-340 and 05D-350 from the ramp blister
05D-250.
(g) Loosen the screws 05D-120.
(h) Removal of the support 05D-140 and the T-sections 05D-090 and 05D-110.
1 Remove the blind bolts 05D-080 and the rivets 05D-040 from the T-section
05D-110. See SRM 51-42-11 for removal of the rivets 05D-040 and blind bolts
05D-080.

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2 Remove the T-section 05D-110.

3 Remove the blind bolts 05D-050, 05D-060 and 05D-070, and the rivets 05D-040
from the support 05D-140 and the T-section 05D-090. See SRM 51-42-11 for
removal of the rivets 05D-040 and blind bolts 05D-050, 05D-060 and 05D-070.
4 Remove the support 05D-140 and the T-section 05D-090.
5 Make sure that the shim between the support 05D-140 and the MLG door is in
correct conditions.
(i) Removal of the runout tip 05D-200 and the supports 05D-160 and 05D-180.
1 Remove the screws 05D-120 from the runout tip 05D-200 and the supports
05D-160 and 05D-180.
2 Remove the runout tip 05D-200 and the supports 05D-160 and 05D-180.
3 Make sure that the shim between the supports 05D-160 and 05D-180 and the
MLG door is in correct conditions.
(2) Installation of the central ramp.

NOTE : For mixing and curing details refer to the manufacturer’s instructions.

NOTE : Where necessary use oversize fasteners.

(a) Installation of the supports 05D-160 and 05D-180, and the runout tip 05D-200.
1 Make sure that the shim between the supports 05D-160 and 05D-180 and the
MLG door is in correct conditions.
2 Put the supports 05D-160 and 05D-180 on the MLG door in the correct
position.
3 Clean the mating surfaces of the supports 05D-160 and 05D-180, the runout tip
05D-200 and the MLG door with Material No. 08BBF1 Non Aqueous Cleaner--
Methyl-Ethyl-Ketone -.
4 Apply a layer of Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy
on the mating surfaces of the supports 05D-160 and 05D-180, the runout tip
05D-200.

CAUTION : MAKE SURE THAT THE BOLTS HAVE A MINIMUM THREADED

LENGHT OF 6 MM (0.23 IN).
5 Install the supports 05D-160 and 05D-180, the runout tip 05D-200 in the correct
position on the MLG door with the screws 05D-120 soaked with Material No.
06ABC1 Polysulfide Sealant-Fuel Tank Interfay -. Lightly tighten the screws
05D-120.

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(b) Installation of the T-sections 05D-090 and 05D-110, and the support 05D-140.
1 Make sure that the shim between the support 05D-140 and the MLG door is in
correct conditions.
2 Put the support 05D-140 on the MLG door in the correct position.
3 Clean the mating surfaces of the T-sections 05D-090 and 05D-110, and the
support 05D-140 with Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-
Ethyl-Ketone -.
4 Apply a layer of Material No. 06ABC1 Polysulfide Sealant-Fuel Tank Interfay -
on the mating surfaces of the T-sections 05D-090 and 05D-110, and the support
05D-140.
5 Install the support 05D-140 and the T-section 05D-090 in the correct position
with the blind bolts 05D-050, 05D-060 and 05D-070, and the rivets 05D-040
soaked with Material No. 06ABC1 Polysulfide Sealant-Fuel Tank Interfay -.
6 Install the T-section 05D-110 in the correct position with the bolts 05D-080 and
the rivets 05D-040 soaked with Material No. 06ABC1 Polysulfide Sealant-Fuel
Tank Interfay -. See SRM 51-42-11 for removal of the rivets 05D-040 and the
blind bolts 05D-080.
(c) Tighten the screws 05D-120.
(d) Apply a layer of Material No. 06ADB1 Polysulfide Sealant-Fuel Contaminated Area
Fillet - on the heads of the screws 05D-120, the blind bolts 05D-050, 05D-060,
05D-070 and 05D-080, and the rivets 05D-040. Let the sealant dry. See SRM
51-42-11 for removal of the rivets 05D-040 and the blind bolts 05D-050, 05D-060,
05D-070.
(e) Install the angles 05D-290, 05D-310, 05D-340 and 05D-350 on the ramp blister in the
correct position with the rivets 05D-330 soaked with Material No. 06ABC1 Polysulfide
Sealant-Fuel Tank Interfay -. See SRM 51-42-11 for removal of the rivets05D-330.
(f) Apply a layer of Material No. 06ADB1 Polysulfide Sealant-Fuel Contaminated Area
Fillet - on the heads of the rivets 05D-330. Let the sealant dry.
(g) Clean the surface of the ramp blister 05D-250 and the T-sections 05D-090 and
05D-110 that will be in contact with the teflon sheet 05D-010 with Material No.
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(h) Apply a layer of Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy on the
mating surfaces of the ramp blister 05D-250, the T-sections 05D-090 and 05D-110,
and the teflon sheet 05D-010.
(i) Install the teflon sheet 05D-010 on the ramp blister 05D-250 and the T-sections
05D-090 and 05D-110.
(j) Install the rivets 05D-030 on the teflon sheet 05D-010 and the ramp blister 05D-250.
See SRM 51-42-11 for removal of the rivets 05D-030.

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(k) Make sure that the mating surfaces of the teflon sheet 05D-010, the ramp blister
05D-250 and the T-sections 05D-090 and 05D-110 are in good contact.
(l) Remove any excess of Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy.
(m) Apply Material No. 06ADA1 Polysulfide Sealant-Fuel Contaminated Area Brushable -
to the surface of the new ramp blister 05D-250 and the angles 05D-290, 05D-310,
05D-340 and 05D-350 that will be in contact with the MLG door.

CAUTION : MAKE SURE THAT THE BOLTS HAVE A MINIMUM THREADED

LENGHT OF 6 MM (0.23 IN).
(n) Install the new ramp blister 05D-250 on the MLG door in the correct position with
the screws 05D-120 and 05D-240, soaked with Material No. 06ABC1 Polysulfide
Sealant-Fuel Tank Interfay -, the washers 05D-230 and the nuts 05D-220.
(o) Tighten the nuts 05D-220.
(p) Apply a layer of Material No. 06ADB1 Polysulfide Sealant-Fuel Contaminated Area
Fillet - on the heads of the screws 05D-120 and 05D-240, and the nuts 05D-220. Let
the sealant dry.

**For PN’s D5288001000095 D5288001000195

Subtask 52-81-14-300-035-B01
B. Replacement of the Central Ramp

NOTE : See IPL_FIGURE_05E.

NOTE : This procedure is applicable to the central ramps 05E-001.

(1) Removal of the central ramp.
(a) Remove all sealant from the fastener heads.
(b) Remove the screws 05E-120 from the teflon sheet 05E-010.
(c) Remove the bonded teflon sheet 05E-010 from the ramp blister 05E-250 and the T-
sections 05E-090 and 05E-110.
(d) Remove the old adhesive from the component parts with a non-metallic scraper.
(e) Remove the rivets 05E-040 and the blind bolts 05E-080. See SRM 51-42-11 for
removal of the rivets 05E-040 and the blind bolts 05E-080.
(f) Remove the T-section 05E-110.
(g) Remove the rivets 05E-040 and the blind bolts 05E-050, 05E-060 and 05E-070. See
SRM 51-42-11 for removal of the rivets 05E-040 and blind bolts 05E-050, 05E-060
and 05E-070.
(h) Remove the T-section 05E-090.

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(i) Remove the screws 05E-120 , 05E-240, 05E-245, the washers 05E-230, 05E-235, the
nuts 05E-220, 05E-225 and the rivets 05E-340. See SRM 51-42-11 for removal of the
rivets 05E-340.
(j) Remove ramp blister 05E-250.
(k) Remove the rivets 05E-330. See SRM 51-42-11 for removal of the rivets 05E-330.
(l) Remove the angles 05E-290 and 05E-310 from the ramp blister 05E-250.
(m) Remove the rivets 05E-330. See SRM 51-42-11 for removal of the rivets 05E-330.
(n) Remove the runout tip 05E-200.
(o) Remove the screws 05E-120.
(p) Remove the No. 2 fwd support 05E-160.
(q) Remove the screws 05E-120.
(r) Remove the No. 2 aft support 05E-180.
(s) Remove the No. 1 support 05E-140 from the cover assembly.
(2) Installation of the central ramp.

NOTE : Unless indicated, all fasteners and mating surfaces are to be wet installed with
Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay -.

NOTE : Where necessary use oversize fasteners.

(a) Remove all old sealant from the cover assembly and any components that were
previously removed.
(b) Clean the surface of the cover assembly with Material No. 08BBF1 Non Aqueous
Cleaner-- Methyl-Ethyl-Ketone -.
(c) Cut some pieces of Material No. 13AEC1 Dry glass fabric-8H Satin 293 gsm - 181
style SRM Type 2 - to the shape runout tip 05E-200, the No. 2 fwd and aft supports
05E-160 and 05E-180 and No. 1 support 05E-140.
(d) Apply Material No. 13FBB1 Paste Adhesive-Epoxy Composite General Use - to the
glass fabric pieces and put them in position on the cover assembly.
(e) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surfaces of the runout tip, the No. 2 and the No. 1 supports.
(f) Install the No. 2 aft support 05E-180 with the screws 05E-120.
(g) Install the No. 2 fwd support 05E-160 with the screws 05E-120.
(h) Install the runout tip 05E-200 with the screws 05E-120.
(i) Install the T-section 05E-110 to the runout tip 05E-200 with the blind bolts 05E-080
and to the No. 2 fwd support 05E-160 and the No. 2 aft support 05E-180 with the
rivets 05E-040. See SRM 51-42-11 for installation of the rivets 05E-040 and blind
bolts 05E-080.

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(j) Install the T-section 05E-090 to the No. 2 fwd support 05E-160 and the No. 2 aft
support 05E-180 with the rivets 05E-040 and together with the No. 1 support
05E-140 with the blind bolts 05E-050, 05E-060 and 05E-070 to the cover assembly.
See SRM 51-42-11 for installation of the rivets 05E-040 and blind bolts 05E-050,
05E-060 and 05E-070.
(k) Apply Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy to the mating
surfaces of the ramp blister 05E-250 and the No. 1 support 05A-140.
(l) Install the ramp blister 05E-250 with the screws 05E-120, 05E-240, 05E-245, the
washers 05E-230 and 05E-235, the nuts 05E-220, 05E-225 and the rivets 05E-340.
See SRM 51-42-11 for installation of the rivets 05E-340.
(m) Install the angles 05E-290 and 05E-310 with the screws 05E-120 and the rivets
05E-330. See SRM 51-42-11 for installation of the rivets 05E-330.
(n) Identify the mating surfaces of the teflon sheet 05E-010 with the ramp blister 05E-250
and the T-sections 05E-090 and 05E-110. On the mating surfaces of the teflon sheet
05A-010 only, do a pretreatment according to ABP5-1148 PMS 01-02-31 Pre-
Treatment of the P. T. F. E. Surfaces.
(o) Identify the mating surfaces of the ramp blister 05E-250 and the T-sections 05E-090
and 05E-110 with the teflon sheet 05E-010. On the mating surfaces of the ramp
blister 05E-250 of the T-sections 05A-090 and 05A-110 only, examine the condition of
the bonding primer.
(p) If the bonding primer of the ramp blister 05E-250 and the T-sections 05E-090 and
05E-110 is damaged, do the subsequent steps.
1 Remove the bonding primer with emery cloth Grade 240 to 400 .
2 Clean the mating surfaces of the ramp blister 05E-250 and the T-sections
05E-090 and 05E-110 with Material No. 08BBF1 Non Aqueous Cleaner--
Methyl-Ethyl-Ketone -.
3 Apply bonding primer to the mating surfaces of the ramp blister 05E-250 and
the T-sections 05E-090 and 05E-110, according to ABP4-1123 PMS 01-02-26
Application of Primer.
(q) Rub lightly the mating surfaces of the ramp blister 05E-250 and the T-sections
05E-090 and 05E-110 with emery cloth Grade 240 to 400 .
(r) Clean the mating surfaces of the ramp blister 05E-250 and the T-sections 05E-090
and 05E-110 with Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone
-.
(s) Apply Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy to the mating
surfaces of the T-sections 05E-090 and 05E-110 and the ramp blister 05E-250 and the
teflon sheet 05E-010.

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(t) Install the teflon sheet 05E-010 on the T-sections 05E-090 and 05E-110 and the ramp
blister 05E-250.
(u) Install the screws 05E-120 and the rivets 05E-040 through the teflon sheet 05E-010
and the ramp blister 05E-250. Apply pressure and let the adhesive cure. See SRM
51-42-11 for installation of the rivets 05E-040.
(v) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to all
fastener heads.

**For PN’s D5288000800094 D5288000800194 D5288000900094 D5288000900194

Subtask 52-81-14-300-035-C01
C. Replacement of the Central Ramp

NOTE : See IPL_FIGURE_05F.

NOTE : This procedure is applicable to the central ramp 05F-001.

(1) Removal of the central ramp.
(a) Remove the sealant from all the heads of the fasteners with a non-metallic scraper.
(b) Remove the nuts 05F-220, the washers 05F-230 and the screws 05F-120 and 05F-240.
(c) Remove the ramp blister 05F-250 from the MLG door.
(d) Remove the rivets 05F-330. See SRM 51-42-11 for removal of the rivets05D-330.
(e) Remove the angles 05F-290, 05F-310, 05F-340 and 05F-350 from the ramp blister
05F-250.
(f) Loosen the screws 05F-120.
(g) Removal of the support 05F-140 and the T-sections 05F-090 and 05F-110.
1 Remove the blind bolts 05F-080 and the rivets 05F-040 from the T-section
05F-110. See SRM 51-42-11 for removal of the rivets 05F-040 and blind bolts
05F-080.
2 Remove the T-section 05F-110.
3 Remove the blind bolts 05F-050, 05F-060 and 05F-070, and the rivets 05F-040
from the support 05F-140 and the T-section 05F-090. See SRM 51-42-11 for
removal of the rivets 05F-040 and blind bolts 05F-050, 05F-060 and 05F-070.
4 Remove the support 05F-140 and the T-section 05F-090.
5 Make sure that the shim between the support 05F-140 and the MLG door is in
correct conditions.
(h) Removal of the runout tip 05F-200 and the supports 05F-160 and 05F-180.
1 Remove the screws 05F-120 from the runout tip 05F-200 and the supports
05F-160 and 05F-180.

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2 Remove the runout tip 05F-200 and the supports 05F-160 and 05F-180.
3 Make sure that the shim between the supports 05F-160 and 05F-180 and the
MLG door is in correct conditions.
(i) If necessary remove the Material No. 04PAD2 Polyurethane Coating-- Abrasion
Resistant Structurefrom the ramp blister 05F-250 See SRM 51-75-11 for removal of
the coating.
(2) Installation of the central ramp.

NOTE : For mixing and curing details refer to the manufacturer’s instructions.

NOTE : Where necessary use oversize fasteners.

(a) Installation of the supports 05F-160 and 05F-180, and the runout tip 05F-200.
1 Make sure that the shim between the supports 05F-160 and 05F-180 and the
MLG door is in correct conditions.
2 Put the supports 05F-160 and 05F-180 on the MLG door in the correct position.
3 Clean the mating surfaces of the supports 05F-160 and 05F-180, the runout tip
05F-200 and the MLG door with Material No. 08BBF1 Non Aqueous Cleaner--
Methyl-Ethyl-Ketone -.
4 Apply a layer of Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy
on the mating surfaces of the supports 05F-160 and 05F-180, the runout tip
05F-200.

CAUTION : MAKE SURE THAT THE BOLTS HAVE A MINIMUM THREADED

LENGHT OF 6 MM (0.23 IN).
5 Install the supports 05F-160 and 05F-180, the runout tip 05F-200 in the correct
position on the MLG door with the screws 05F-120 soaked with Material No.
06ABC1 Polysulfide Sealant-Fuel Tank Interfay -. Lightly tighten the screws
05F-120.
(b) Installation of the T-sections 05F-090 and 05F-110, and the support 05F-140.
1 Make sure that the shim between the support 05F-140 and the MLG door is in
correct conditions.
2 Put the support 05F-140 on the MLG door in the correct position.
3 Clean the mating surfaces of the T-sections 05F-090 and 05F-110, and the
support 05F-140 with Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-
Ethyl-Ketone -.
4 Apply a layer of Material No. 06ABC1 Polysulfide Sealant-Fuel Tank Interfay -
on the mating surfaces of the T-sections 05F-090 and 05F-110, and the support
05F-140.

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5 Install the support 05F-140 and the T-section 05F-090 in the correct position
with the blind bolts 05F-050, 05F-060 and 05F-070, and the rivets 05F-040
soaked with Material No. 06ABC1 Polysulfide Sealant-Fuel Tank Interfay -.
6 Install the T-section 05F-110 in the correct position with the blind bolts 05F-080
and the rivets 05F-040 soaked with Material No. 06ABC1 Polysulfide Sealant-
Fuel Tank Interfay -. See SRM 51-42-11 for installation of the rivets 05F-040
and the blind bolts 05F-080.
(c) Tighten the screws 05F-120.
(d) Apply a layer of Material No. 06ADB1 Polysulfide Sealant-Fuel Contaminated Area
Fillet - on the heads of the screws 05F-120, the blind bolts 05F-050, 05F-060,
05F-070, and the rivets 05F-040. Let the sealant dry. See SRM 51-42-11 for removal
of the rivets 05F-040 and the blind bolts 05F-050, 05F-060 and 05F-070.
(e) Install the angles 05F-290, 05F-310, 05F-340 and 05F-350 on the ramp blister in the
correct position with the rivets 05F-330 soaked with Material No. 06ABC1 Polysulfide
Sealant-Fuel Tank Interfay -. See SRM 51-42-11 for installation of the rivets 05F-330.
(f) If necessary apply the Material No. 04PAD2 Polyurethane Coating-- Abrasion
Resistant Structurefrom the ramp blister 05F-250 See SRM 51-75-12 for repair of the
coating.
(g) Apply a layer of Material No. 06ADB1 Polysulfide Sealant-Fuel Contaminated Area
Fillet - on the heads of the rivets 05F-330. Let the sealant dry.
(h) Apply Material No. 06ADA1 Polysulfide Sealant-Fuel Contaminated Area Brushable -
to the surface of the new ramp blister 05F-250 and the angles 05F-290, 05F-310,
05F-340 and 05F-350 that will be in contact with the MLG door.

CAUTION : MAKE SURE THAT THE BOLTS HAVE A MINIMUM THREADED

LENGHT OF 6 MM (0.23 IN).
(i) Install the new ramp blister 05F-250 on the MLG door in the correct position with the
screws 05F-120 and 05F-240, soaked with Material No. 06ABC1 Polysulfide Sealant-
Fuel Tank Interfay -, the washers 05F-230 and the nuts 05F-220.
(j) Tighten the nuts 05F-220.
(k) Apply a layer of Material No. 06ADB1 Polysulfide Sealant-Fuel Contaminated Area
Fillet - on the heads of the screws 05F-120 and 05F-240, and the nuts 05F-220. Let
the sealant dry.

**For PN’s D5288001000094 D5288001000194

Subtask 52-81-14-300-035-D01
D. Replacement of the Central Ramp

NOTE : See IPL_FIGURE_05G.

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NOTE : This procedure is applicable to the central ramp 05G-001.

(1) Removal of the central ramp.
(a) Remove all sealant from the fastener heads.
(b) Remove the rivets 05G-040 and the blind bolts 05G-080. See SRM 51-42-11 for
removal of the rivets 05G-040 and the blind bolts 05G-080.
(c) Remove the T-section 05G-110.
(d) Remove the rivets 05G-040 and the blind bolts 05G-050, 05G-060 and 05G-070. See
SRM 51-42-11 for removal of the rivets 05G-040 and blind bolts 05G-050, 05G-060
and 05G-070.
(e) Remove the T-section 05G-090.
(f) Remove the screws 05G-120 , 05G-240, 05G-245, the washers 05G-230, 05G-235, the
nuts 05G-220, 05G-225 and the rivets 05G-340. See SRM 51-42-11 for removal of the
rivets 05G-340.
(g) Remove ramp blister 05G-250.
(h) Remove the rivets 05G-330. See SRM 51-42-11 for removal of the rivets 05G-330.
(i) Remove the angles 05G-290 and 05G-310 from the ramp blister 05G-250.
(j) Remove the rivets 05G-330. See SRM 51-42-11 for removal of the rivets 05G-330.
(k) Remove the runout tip 05G-200.
(l) Remove the screws 05G-120.
(m) Remove the No. 2 fwd support 05G-160.
(n) Remove the screws 05G-120.
(o) Remove the No. 2 aft support 05G-180.
(p) Remove the No. 1 support 05G-140 from the cover assembly.
(q) If necessary remove the Material No. 04PAD2 Polyurethane Coating-- Abrasion
Resistant Structurefrom the ramp blister 05G-250See SRM 51-75-11 for removal of
the coating.
(2) Installation of the central ramp.

NOTE : For mixing and curing details refer to the manufacturer’s instructions.

NOTE : Where necessary use oversize fasteners.

(a) Remove all old sealant from the cover assembly and any components that were
previously removed.
(b) Clean the surface of the cover assembly with Material No. 08BBF1 Non Aqueous
Cleaner-- Methyl-Ethyl-Ketone -.

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(c) Cut some pieces of Material No. 13AEC1 Dry glass fabric-8H Satin 293 gsm - 181
style SRM Type 2 - to the shape runout tip 05G-200, the No. 2 fwd and aft supports
05G-160 and 05G-180 and No. 1 support 05G-140.
(d) Apply Material No. 13FBB1 Paste Adhesive-Epoxy Composite General Use - to the
glass fabric pieces and put them in position on the cover assembly.
(e) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surfaces of the runout tip, the No. 2 and the No. 1 supports.
(f) Install the No. 2 aft support 05G-180 with the screws 05G-120.
(g) Install the No. 2 fwd support 05G-160 with the screws 05G-120.
(h) Install the runout tip 05G-200 with the screws 05G-120.
(i) Install the T-section 05G-110 to the runout tip 05G-200 with the blind bolts 05G-080
and to the No. 2 fwd support 05G-160 and the No. 2 aft support 05G-180 with the
rivets 05G-040. See SRM 51-42-11 for installation of the rivets 05G-040 and blind
bolts 05G-080.
(j) Install the T-section 05G-090 to the No. 2 fwd support 05G-160 and the No. 2 aft
support 05G-180 with the rivets 05G-040 and together with the No. 1 support
05G-140 with the blind bolts 05G-050, 05G-060 and 05G-070 to the cover assembly.
See SRM 51-42-11 for installation of the rivets 05G-040 and blind bolts 05G-050,
05G-060 and 05G-070.
(k) Apply Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy to the mating
surfaces of the ramp blister 05G-250 and the No. 1 support 05G-140.
(l) Install the ramp blister 05G-250 with the screws 05G-120, 05G-240, 05G-245, the
washers 05G-230 and 05G-235, the nuts 05G-220, 05G-225 and the rivets 05G-340.
See SRM 51-42-11 for installation of the rivets 05G-340.
(m) Install the angles 05G-290 and 05G-310 with the screws 05G-120 and the rivets
05G-330 . See SRM 51-42-11 for installation of the rivets 05G-330.
(n) If necessary apply the Material No. 04PAD2 Polyurethane Coating-- Abrasion
Resistant Structurefrom the ramp blister 05G-250. See SRM 51-75-12 for repair of the
coating.
(o) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to all
fastener heads.

**For PN’s D5288000800098 D5288000800198 D5288000900098 D5288000900198

Subtask 52-81-14-300-035-E01
E. Replacement of the Central Ramp
PRE MOD 21514 AND PRE SB 52-1025

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(1) Removal of the Central Ramp

NOTE : This procedure is applicable to the central ramp 05-001.

NOTE : See IPL_FIGURE_05.

(a) Remove all sealant from the fastener heads.
(b) Remove the screws 05-120 from the teflon sheet 05-010.
(c) Remove the rivets 05-030 from the ramp blister 05-250 and the teflon sheet 05-010.
See SRM 51-42-11 for removal of the rivets 05-030.
(d) Remove the bonded teflon sheet 05-010 from the ramp blister 05-250 and the T-
sections 05-090 and 05-110.
(e) Remove the old adhesive from the component parts with a non-metallic scraper.
(f) Remove the rivets 05-040 and the blind bolts 05-080. See SRM 51-42-11 for removal
of the rivets 05-040 and the blind bolts 05-080.
(g) Remove the T-section 05-110.
(h) Remove the rivets 05-040 and the blind bolts 05-050, 05-060 and 05-070. See SRM
51-42-11 for removal of the rivets 05-040 and the blind bolts 05-050, 05-060 and
05-070.
(i) Remove the T-section 05-090.
(j) Remove the screws 05-120 and 05-240, the washers 05-230 and the nuts 05-220.
(k) Remove the ramp blister 05-250.
(l) Remove the screws 05-120.
(m) Remove the runout tip 05-200.
(n) Remove the screws 05-120.
(o) Remove the No. 2 FWD support 05-160.
(p) Remove the screws 05-120.
(q) Remove the No. 2 AFT support 05-180.
(r) Remove the No. 1 support 05-140 from the cover assembly.
(2) Installation of the central ramp.

NOTE : This procedure is applicable to the central ramp 05-001.

NOTE : See IPL_FIGURE_05.

NOTE : Unless indicated, all fasteners and mating surfaces are to be wet installed with
Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay -.

NOTE : Where necessary use oversize fasteners.

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(a) Remove all old sealant from the cover assembly and any components that were
previously removed.
(b) Clean the surface of the cover assembly with Material No. 08BBF1 Non Aqueous
Cleaner-- Methyl-Ethyl-Ketone -.
(c) Cut some pieces of Material No. 13AEC1 Dry glass fabric-8H Satin 293 gsm - 181
style SRM Type 2 - to the shape runout tip 05-200, the No. 2 FWD and AFT
supports 05-160 and 05-180, and No. 1 support 05-140.
(d) Apply Material No. 13FBB1 Paste Adhesive-Epoxy Composite General Use - to the
glass fabric pieces and put them in position on the cover assembly.
(e) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surfaces of the runout tip, the No. 2 and the No. 1 supports.
(f) Install the No. 2 AFT support 05-180 with the screws 05-120.
(g) Install the No. 2 FWD support 05-160 with the screws 05-120.
(h) Install the runout tip 05-200 with the screws 05-120.
(i) Tighten the screws 05-120.
(j) Install the T-section 05-110 to the runout tip 05-200 with the blind bolts 05-080 and
to the No. 2 FWD support 05-160 and the No. 2 AFT support 05-180 with the rivets
05-040. See SRM 51-42-11 for installation of the rivets 05-040 and the blind bolts
05-080.
(k) Install the T-section 05-090 to the No. 2 FWD support 05-160 and the No. 2 AFT
support 05-180 with the rivets 05-040 and together with the No. 1 support 05-140
with the blind bolts 05-050, 05-060 and 05-070 to the cover assembly. See SRM
51-42-11 for installation of the rivets 05-040 and the blind bolts 05-050, 05-060 and
05-070.
(l) Apply Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy to the mating
surfaces of the ramp blister 05-250 and the No. 1 support 05-140.
(m) Install the ramp blister 05-250 with the screws 05-120 and 05-240, the washers
05-230 and the nuts 05-220.
(n) Identify the mating surfaces of the teflon sheet 05-010 with the ramp blister 05-250
and the T-sections 05-090 and 05-110. On the mating surfaces of the teflon sheet
05-010 only, do a pretreatment according to ABP5-1148 PMS 01-02-31 Pre-
Treatment of the P. T. F. E. Surfaces.
(o) Identify the mating surfaces of the ramp blister 05-250 and the T-sections 05-090 and
05-110 with the teflon sheet 05-010. On the mating surfaces of the ramp blister
05-250 of the T-sections 05-090 and 05-110 only, examine the condition of the
bonding primer.

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(p) If the bonding primer of the ramp blister 05-250 and the T-sections 05-090 and
05-110 is damaged, do the subsequent steps.
1 Remove the bonding primer with emery cloth Grade 240 to 400 .
2 Clean the mating surfaces of the ramp blister 05-250 and the T-sections 05-090
and 05-110 with Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-
Ketone -.
3 Apply bonding primer to the mating surfaces of the ramp blister 05-250 and the
T-sections 05-090 and 05-110, according to ABP4-1123 PMS 01-02-26
application of primer.
(q) Rub lightly the mating surfaces of the ramp blister 05-250 and the T-sections 05-090
and 05-110 with emery cloth Grade 240 to 400 .
(r) Clean the mating surfaces of the ramp blister 05-250 and the T-sections 05-090 and
05-110 with Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(s) Apply Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy to the mating
surfaces of the T-sections 05-090 and 05-110, the ramp blister 05-250 and the teflon
sheet 05-010.
(t) Install the teflon sheet 05-010 on the T-sections 05-090, 05-110 and the ramp blister
05-250. Install the screws 05-120 and the rivets 05-030 thru the teflon sheet 05-010
and the ramp blister 05-250. Apply pressure and let the adhesive cure. See SRM
51-42-11 for installation of the rivets 05-030.
(u) Tighten the screws 05-120.
(v) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to all
fastener heads.
POST MOD 21514 AND PRE SB 52-1025
(1) Removal of the central ramp.

NOTE : See IPL_FIGURE_05B.

NOTE : This procedure is applicable to the central ramp 05B-001.

(a) Remove all sealant from the fastener heads.
(b) Remove the screws 05B-120 from the teflon sheet 05B-01005-010.
(c) Remove the rivets 05B-030 from the ramp blister 05B-250 and the teflon sheet
05B-010. See SRM 51-42-11 for removal of the rivets 05B-030.
(d) Remove the bonded teflon sheet 05B-010 from the ramp blister 05B-250 and the T-
sections 05B-090 and 05B-110.
(e) Remove the old adhesive from the component parts with a non-metallic scraper.
(f) Remove the rivets 05B-040 and the blind bolts 05B-080. See SRM 51-42-11 for
removal of the rivets 05B-040 and the blind bolts 05B-080.

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(g) Remove the T-section 05B-110.

(h) Remove the rivets 05B-040 and the blind bolts 05B-050, 05B-060 and 05B-070. See
SRM 51-42-11 for removal of the rivets 05B-040 and the blind bolts 05B-050,
05B-060 and 05B-070.
(i) Remove the T-section 05B-090.
(j) Remove the screws 05B-120 and 05B-240, the washers 05B-230 and the nuts
05B-220. Remove the angles 05B-290 and 05B-310 from the ramp blister 05B-250 by
removing the rivets 05B-330.
(k) Remove the ramp blister 05B-250.
(l) Remove the screws 05B-120.
(m) Remove the runout tip 05B-200.
(n) Remove the screws 05B-120.
(o) Remove the No. 2 FWD support 05B-160.
(p) Remove the screws 05B-120.
(q) Remove the No. 2 AFT support 05B-180.
(r) Remove the No. 1 support 05B-140 from the cover assembly.
(2) Installation of the central ramp.

NOTE : See IPL_FIGURE_05B.

NOTE : This procedure is applicable to the central ramp 05B-001.

NOTE : Unless indicated, all fasteners and mating surfaces are to be wet installed with
Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay -.

NOTE : Where necessary use oversize fasteners.

(a) Remove all old sealant from the cover assembly and any components that were
previously removed.
(b) Clean the surface of the cover assembly with Material No. 08BBF1 Non Aqueous
Cleaner-- Methyl-Ethyl-Ketone -.
(c) Cut some pieces of Material No. 13AEC1 Dry glass fabric-8H Satin 293 gsm - 181
style SRM Type 2 - to the shape runout tip 05B-200, the No. 2 FWD and AFT
supports 05B-160 and 05B-180, and No. 1 support 05B-140.
(d) Apply Material No. 13FBB1 Paste Adhesive-Epoxy Composite General Use - to the
glass fabric pieces and put them in position on the cover assembly.
(e) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surfaces of the runout tip, the No. 2 and the No. 1 supports.
(f) Install the No. 2 AFT support 05B-180 with the screws 05B-120.

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(g) Install the No. 2 FWD support 05B-160 with the screws 05B-120.
(h) Install the runout tip 05B-200 with the screws 05B-120.
(i) Tighten the screws 05B-120.
(j) Install the T-section 05B-110 to the runout tip 05B-200 with the blind bolts 05B-080
and to the No. 2 FWD support 05B-160 and the No. 2 AFT support 05B-180 with
the rivets 05B-040. See SRM 51-42-11 for installation of the rivets 05B-040 and the
blind bolts 05B-080.
(k) Install the T-section 05B-090 to the No. 2 FWD support 05B-160 and the No. 2 AFT
support 05B-180 with the rivets 05B-040 and together with the No. 1 support
05B-140 with the blind bolts 05B-050, 05B-060 and 05B-070 to the cover assembly.
See SRM 51-42-11 for installation of the rivets 05B-040 and the blind bolts 05B-050,
05B-060 and 05B-070.
(l) Apply Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy to the mating
surfaces of the ramp blister 05B-250 and the No. 1 support 05B-140.
(m) Install the ramp blister 05B-250 with the screws 05B-120 and 05B-240, the washers
05B-230 and the nuts 05B-220.
(n) Install the angles 05B-290 and 05B-310 with the screws 05B-120 and the rivets
05B-330.
(o) Identify the mating surfaces of the teflon sheet 05B-010 with the ramp blister
05B-250 and the T-sections 05B-090 and 05B-110. On the mating surfaces of the
teflon sheet 05B-010 only, do a pretreatment according to ABP5-1148 PMS 01-02-31
Pre-Treatment of the P. T. F. E. Surfaces.
(p) Identify the mating surfaces of the ramp blister 05B-250 and the T-sections 05B-090
and 05B-110 with the teflon sheet 05B-010. On the mating surfaces of the ramp
blister 05B-250 of the T-sections 05B-090 and 05B-110 only, examine the condition
of the bonding primer.
(q) If the bonding primer of the ramp blister 05B-250 and the T-sections 05B-090 and
05B-110 is damaged, do the subsequent steps.
1 Remove the bonding primer with emery cloth Grade 240 to 400 .
2 Clean the mating surfaces of the ramp blister 05B-250 and the T-sections
05B-090 and 05B-110 with Material No. 08BBF1 Non Aqueous Cleaner--
Methyl-Ethyl-Ketone -.
3 Apply bonding primer to the mating surfaces of the ramp blister 05B-250 and
the T-sections 05B-090 and 05B-110, according to ABP4-1123 PMS 01-02-26
application of primer.
(r) Rub lightly the mating surfaces of the ramp blister 05B-250 and the T-sections
05B-090 and 05B-110 with emery cloth Grade 240 to 400 .

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(s) Clean the mating surfaces of the ramp blister 05B-250 and the T-sections 05B-090
and 05B-110 with Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone
-.
(t) Apply Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy to the mating
surfaces of the T-sections 05B-090 and 05B-110, the ramp blister 05B-250 and the
teflon sheet 05B-010.
(u) Install the teflon sheet 05B-010 on the T-sections 05B-090, 05B-110 and the ramp
blister 05B-250. Install the screws 05B-120 and the rivets 05B-030 thru the teflon
sheet 05B-010 and the ramp blister 05B-250. Apply pressure and let the adhesive
cure. See SRM 51-42-11 for installation of the rivets 05B-030.
(v) Tighten the screws 05B-120.
(w) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to all
fastener heads.
POST MOD 21514 AND POST SB 52-1025
(1) Removal of the central ramp.

NOTE : See IPL_FIGURE_05D.

NOTE : This procedure is applicable to the central ramp 05D-001.

(a) Remove the sealant from all the heads of the fasteners with a non-metallic scraper.
(b) Remove the nuts 05D-220, the washers 05D-230 and the screws 05D-120 and
05D-240.
(c) Remove the ramp blister 05D-250 from the MLG door.
(d) Remove the rivets 05D-030. See SRM 51-42-11 for removal of the rivets 05D-030.
(e) Remove the teflon sheet 05D-010 from the ramp blister 05D-250 and the T-sections
05D-090 and 05D-110.
(f) Remove the angles 05D-290, 05D-310, 05D-340 and 05D-350 from the ramp blister
05D-250.
(g) Loosen the screws 05D-120.
(h) Removal of the support 05D-140 and the T-sections 05D-090 and 05D-110.
1 Remove the blind bolts 05D-080 and the rivets 05D-040 from the T-section
05D-110. See SRM 51-42-11 for removal of the rivets 05D-040 and blind bolts
05D-080.
2 Remove the T-section 05D-110.
3 Remove the blind bolts 05D-050, 05D-060 and 05D-070, and the rivets 05D-040
from the support 05D-140 and the T-section 05D-090. See SRM 51-42-11 for
removal of the rivets 05D-040 and blind bolts 05D-050, 05D-060 and 05D-070.

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4 Remove the support 05D-140 and the T-section 05D-090.

5 Make sure that the shim between the support 05D-140 and the MLG door is in
correct conditions.
(i) Removal of the runout tip 05D-200 and the supports 05D-160 and 05D-180.
1 Remove the screws 05D-120 from the runout tip 05D-200 and the supports
05D-160 and 05D-180.
2 Remove the runout tip 05D-200 and the supports 05D-160 and 05D-180.
3 Make sure that the shim between the supports 05D-160 and 05D-180 and the
MLG door is in correct conditions.
(2) Installation of the central ramp.

NOTE : See IPL_FIGURE_05D.

NOTE : This procedure is applicable to the central ramp 05D-001.

NOTE : For mixing and curing details refer to the manufacturer’s instructions.

NOTE : Where necessary use oversize fasteners.

(a) Installation of the supports 05D-160 and 05D-180, and the runout tip 05D-200.
1 Make sure that the shim between the supports 05D-160 and 05D-180 and the
MLG door is in correct conditions.
2 Put the supports 05D-160 and 05D-180 on the MLG door in the correct
position.
3 Clean the mating surfaces of the supports 05D-160 and 05D-180, the runout tip
05D-200 and the MLG door with Material No. 08BBF1 Non Aqueous Cleaner--
Methyl-Ethyl-Ketone -.
4 Apply a layer of Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy
on the mating surfaces of the supports 05D-160 and 05D-180, the runout tip
05D-200.

CAUTION : MAKE SURE THAT THE BOLTS HAVE A MINIMUM THREADED

LENGHT OF 6 MM (0.23 IN).
5 Install the supports 05D-160 and 05D-180, the runout tip 05D-200 in the correct
position on the MLG door with the screws 05D-120 soaked with Material No.
06ABC1 Polysulfide Sealant-Fuel Tank Interfay -. Lightly tighten the screws
05D-120.
(b) Installation of the T-sections 05D-090 and 05D-110, and the support 05D-140.
1 Make sure that the shim between the support 05D-140 and the MLG door is in
correct conditions.

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2 Put the support 05D-140 on the MLG door in the correct position.
3 Clean the mating surfaces of the T-sections 05D-090 and 05D-110, and the
support 05D-140 with Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-
Ethyl-Ketone -.
4 Apply a layer of Material No. 06ABC1 Polysulfide Sealant-Fuel Tank Interfay -
on the mating surfaces of the T-sections 05D-090 and 05D-110, and the support
05D-140.
5 Install the support 05D-140 and the T-section 05D-090 in the correct position
with the blind bolts 05D-050, 05D-060 and 05D-070, and the rivets 05D-040
soaked with Material No. 06ABC1 Polysulfide Sealant-Fuel Tank Interfay -.
6 Install the T-section 05D-110 in the correct position with the bolts 05D-080 and
the rivets 05D-040 soaked with Material No. 06ABC1 Polysulfide Sealant-Fuel
Tank Interfay -. See SRM 51-42-11 for removal of the rivets 05D-040 and the
blind bolts 05D-080.
(c) Tighten the screws 05D-120.
(d) Apply a layer of Material No. 06ADB1 Polysulfide Sealant-Fuel Contaminated Area
Fillet - on the heads of the screws 05D-120, the blind bolts 05D-050, 05D-060,
05D-070 and 05D-080, and the rivets 05D-040. Let the sealant dry. See SRM
51-42-11 for removal of the rivets 05D-040 and the blind bolts 05D-050, 05D-060,
05D-070.
(e) Install the angles 05D-290, 05D-310, 05D-340 and 05D-350 on the ramp blister in the
correct position with the rivets 05D-330 soaked with Material No. 06ABC1 Polysulfide
Sealant-Fuel Tank Interfay -. See SRM 51-42-11 for removal of the rivets05D-330.
(f) Apply a layer of Material No. 06ADB1 Polysulfide Sealant-Fuel Contaminated Area
Fillet - on the heads of the rivets 05D-330. Let the sealant dry.
(g) Clean the surface of the ramp blister 05D-250 and the T-sections 05D-090 and
05D-110 that will be in contact with the teflon sheet 05D-010 with Material No.
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(h) Apply a layer of Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy on the
mating surfaces of the ramp blister 05D-250, the T-sections 05D-090 and 05D-110,
and the teflon sheet 05D-010.
(i) Install the teflon sheet 05D-010 on the ramp blister 05D-250 and the T-sections
05D-090 and 05D-110.
(j) Install the rivets 05D-030 on the teflon sheet 05D-010 and the ramp blister 05D-250.
See SRM 51-42-11 for removal of the rivets 05D-030.
(k) Make sure that the mating surfaces of the teflon sheet 05D-010, the ramp blister
05D-250 and the T-sections 05D-090 and 05D-110 are in good contact.
(l) Remove any excess of Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy.

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(m) Apply Material No. 06ADA1 Polysulfide Sealant-Fuel Contaminated Area Brushable -
to the surface of the new ramp blister 05D-250 and the angles 05D-290, 05D-310,
05D-340 and 05D-350 that will be in contact with the MLG door.

CAUTION : MAKE SURE THAT THE BOLTS HAVE A MINIMUM THREADED

LENGHT OF 6 MM (0.23 IN).
(n) Install the new ramp blister 05D-250 on the MLG door in the correct position with
the screws 05D-120 and 05D-240, soaked with Material No. 06ABC1 Polysulfide
Sealant-Fuel Tank Interfay -, the washers 05D-230 and the nuts 05D-220.
(o) Tighten the nuts 05D-220.
(p) Apply a layer of Material No. 06ADB1 Polysulfide Sealant-Fuel Contaminated Area
Fillet - on the heads of the screws 05D-120 and 05D-240, and the nuts 05D-220. Let
the sealant dry.

**For PN’s D5288001000098 D5288001000198

Subtask 52-81-14-300-035-F01
F. Replacement of the Central Ramp
PRE MOD 21514 AND PRE SB 52-1025
(2) Removal of the Central Ramp

NOTE : See IPL_FIGURE_05A.

NOTE : This procedure is applicable to the central ramp 05A-001.

(a) Remove all sealant from the fastener heads.
(b) Remove the screws 05A-120 from the teflon sheet 05A-010.
(c) Remove the bonded teflon sheet 05A-010 from the ramp blister 05A-250 and the T-
sections 05A-090 and 05A-110.
(d) Remove the old adhesive from the component parts with a non-metallic scraper.
(e) Remove the rivets 05A-040 and the blind bolts 05A-080. See SRM 51-42-11 for
removal of the rivets 05A-040 and the blind bolts 05A-080.
(f) Remove the T-section 05A-110.
(g) Remove the rivets 05A-040 and the blind bolts 05A-050, 05A-060 and 05A-070. See
SRM 51-42-11 for removal of the rivets 05A-040 and the blind bolts 05A-050,
05A-060 and 05A-070.
(h) Remove the T-section 05A-090.
(i) Remove the screws 05A-120, 05A-240 and 05A-245, the washers 05A-230 and
05A-235 and the nuts 05A-220 and 05A-225.
(j) Remove the ramp blister 05A-250.

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(k) Remove the screws 05A-120.

(l) Remove the runout tip 05A-200.
(m) Remove the screws 05A-120.
(n) Remove the No. 2 fwd support 05A-160.
(o) Remove the screws 05A-120.
(p) Remove the No. 2 aft support 05A-180.
(q) Remove the No. 1 support 05A-140 from the cover assembly.
(3) Installation of the central ramp.

NOTE : See IPL_FIGURE_05A.

NOTE : This procedure is applicable to the central ramp 05A-001.

NOTE : Unless indicated, all fasteners and mating surfaces are to be wet installed with
Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay -.

NOTE : Where necessary use oversize fasteners.

(a) Remove all old sealant from the cover assembly and any components that were
previously removed.
(b) Clean the surface of the cover assembly with Material No. 08BBF1 Non Aqueous
Cleaner-- Methyl-Ethyl-Ketone -.
(c) Cut some pieces of Material No. 13AEC1 Dry glass fabric-8H Satin 293 gsm - 181
style SRM Type 2 - to the shape runout tip 05A-200, the No. 2 fwd and aft supports
05A-160 and 05A-180 and No. 1 support 05A-140.
(d) Apply Material No. 13FBB1 Paste Adhesive-Epoxy Composite General Use - to the
glass fabric pieces and put them in position on the cover assembly.
(e) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surfaces of the runout tip, the No. 2 and the No. 1 supports.
(f) Install the No. 2 aft support 05A-180 with the screws 05A-120.
(g) Install the No. 2 fwd support 05A-160 with the screws 05A-120.
(h) Install the runout tip 05A-200 with the screws 05A-120.
(i) Tighten the screws 05A-120.
(j) Install the T-section 05A-110 to the runout tip 05A-200 with the blind bolts 05A-080
and to the No. 2 fwd support 05A-160 and the No. 2 aft support 05A-180 with the
rivets 05A-040. See SRM 51-42-11 for installation of the rivets 05A-040 and the blind
bolts 05A-080.

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(k) Install the T-section 05A-090 to the No. 2 fwd support 05A-160 and the No. 2 aft
support 05A-180 with the rivets 05A-040 and together with the No. 1 support
05A-140 with the blind bolts 05A-050, 05A-060 and 05A-070 to the cover assembly.
See SRM 51-42-11 for installation of the rivets 05A-040 and the blind bolts 05A-050,
05A-060 and 05A-070.
(l) Apply Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy to the mating
surfaces of the ramp blister 05A-250 and the No. 1 support 05A-140.
(m) Install the ramp blister 05A-250 with the screws 05A-120, 05A-240 and 05A-245, the
washers 05A-230 and 05A-235 and the nuts 05A-220 and 05A-225.
(n) Identify the mating surfaces of the teflon sheet 05A-010 with the ramp blister
05A-250 and the T-sections 05A-090 and 05A-110. On the mating surfaces of the
teflon sheet 05A-010 only, do a pretreatment according to ABP5-1148 PMS 01-02-31
Pre-Treatment of the P. T. F. E. Surfaces.
(o) Identify the mating surfaces of the ramp blister 05A-250 and the T-sections 05A-090
and 05A-110 with the teflon sheet 05A-010. On the mating surfaces of the ramp
blister 05A-250 of the T-sections 05A-090 and 05A-110 only, examine the condition
of the bonding primer.
(p) If the bonding primer of the ramp blister 05A-250 and the T-sections 05A-090 and
05A-110 is damaged, do the subsequent steps.
1 Remove the bonding primer with emery cloth Grade 240 to 400 .
2 Clean the mating surfaces of the ramp blister 05A-250 and the T-sections
05A-090 and 05A-110 with Material No. 08BBF1 Non Aqueous Cleaner--
Methyl-Ethyl-Ketone -.
3 Apply bonding primer to the mating surfaces of the ramp blister 05A-250 and
the T-sections 05A-090 and 05A-110, according to ABP4-1123 PMS 01-02-26
application of primer.
(q) Rub lightly the mating surfaces of the ramp blister 05A-250 and the T-sections
05A-090 and 05A-110 with emery cloth Grade 240 to 400 .
(r) Clean the mating surfaces of the ramp blister 05A-250 and the T-sections 05A-090
and 05A-110 with Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone
-.
(s) Apply Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy to the mating
surfaces of the T-sections 05A-090 and 05A-110, the ramp blister 05A-250 and the
teflon sheet 05A-010.
(t) Install the teflon sheet 05A-010 on the T-sections 05A-090 and 05A-110 and the ramp
blister 05A-250. Install the screws 05A-120 and the rivets 05A-040 thru the teflon
sheet 05A-010 and the ramp blister 05A-250. Apply pressure and let the adhesive
cure. See SRM 51-42-11 for installation of the rivets05A-040.

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(u) Tighten the screws 05A-120.

(v) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to all
fastener heads.
POST MOD 21514 AND PRE SB 52-1025
(2) Removal of the central ramp.

NOTE : See IPL_FIGURE_05C.

NOTE : This procedure is applicable to the central ramp 05C-001.

(a) Remove all sealant from the fastener heads.
(b) Remove the screws 05C-120 from the teflon sheet 05C-010.
(c) Remove the bonded teflon sheet 05C-010 from the ramp blister 05C-250 and the T-
sections 05C-090 and 05C-110.
(d) Remove the old adhesive from the component parts with a non-metallic scraper.
(e) Remove the rivets 05C-040 and the blind bolts 05C-080. See SRM 51-42-11 for
removal of the rivets 05C-040 and the blind bolts 05C-080.
(f) Remove the T-section 05C-110.
(g) Remove the rivets 05C-040 and the blind bolts 05C-050, 05C-060 and 05C-070. See
SRM 51-42-11 for removal of the rivets 05C-040 and the blind bolts 05C-050,
05C-060 and 05C-070.
(h) Remove the T-section 05C-090.
(i) Remove the screws 05C-120, 05C-240 and 05C-245, the washers 05C-230 and
05C-235 and the nuts 05C-220 and 05C-225.
(j) Remove the ramp blister 05C-250.
(k) Remove the rivets 05C-330. See SRM 51-42-11 for the removal of the rivets 05C-330.
(l) Remove the angles 05C-290 and 05C-310 from the ramp blister 05C-250.
(m) Remove the screws 05C-120.
(n) Remove the runout tip 05C-200.
(o) Remove the screws 05C-120.
(p) Remove the No. 2 fwd support 05C-160.
(q) Remove the screws 05C-120.
(r) Remove the No. 2 aft support 05C-180.
(s) Remove the No. 1 support 05C-140 from the cover assembly.
(3) Installation of the central ramp.

NOTE : See IPL_FIGURE_05C.

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NOTE : This procedure is applicable to the central ramp 05C-001.

NOTE : Unless indicated, all fasteners and mating surfaces are to be wet installed with
Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay -.

NOTE : Where necessary use oversize fasteners.

(a) Remove all old sealant from the cover assembly and any components that were
previously removed.
(b) Clean the surface of the cover assembly with Material No. 08BBF1 Non Aqueous
Cleaner-- Methyl-Ethyl-Ketone -.
(c) Cut some pieces of Material No. 13AEC1 Dry glass fabric-8H Satin 293 gsm - 181
style SRM Type 2 - to the shape runout tip 05C-200, the No. 2 fwd and aft supports
05C-160 and 05C-180 and No. 1 support 05C-140.
(d) Apply Material No. 13FBB1 Paste Adhesive-Epoxy Composite General Use - to the
glass fabric pieces and put them in position on the cover assembly.
(e) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surfaces of the runout tip, the No. 2 and the No. 1 supports.
(f) Install the No. 2 aft support 05C-180 with the screws 05C-120.
(g) Install the No. 2 fwd support 05C-160 with the screws 05C-120.
(h) Install the runout tip 05C-200 with the screws 05C-120.
(i) Tighten the screws 05C-120.
(j) Install the T-section 05C-110 to the runout tip 05C-200 with the blind bolts 05C-080
and to the No. 2 fwd support 05C-160 and the No. 2 aft support 05C-180 with the
rivets 05C-040. See SRM 51-42-11 for installation of the rivets 05C-040 and the blind
bolts 05C-080.
(k) Install the T-section 05C-090 to the No. 2 fwd support 05C-160 and the No. 2 aft
support 05C-180 with the rivets 05C-040 and together with the No. 1 support
05C-140 with the blind bolts 05C-050, 05C-060 and 05C-070 to the cover assembly.
See SRM 51-42-11 for installation of the rivets 05C-040 and the blind bolts 05C-050,
05C-060 and 05C-070.
(l) Apply Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy to the mating
surfaces of the ramp blister 05C-250 and the No. 1 support 05C-140.
(m) Install the ramp blister 05C-250 with the screws 05C-120, 05C-240 and 05C-245, the
washers 05C-230 and 05C-235 and the nuts 05C-220 and 05C-225.
(n) Install the angles 05C-290 and 05C-310 with the screws 05C-120 and the rivets
05C-330. See SRM 51-42-11 for installation of the rivets05C-330.

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(o) Identify the mating surfaces of the teflon sheet 05C-010 with the ramp blister
05C-250 and the T-sections 05C-090 and 05C-110. On the mating surfaces of the
teflon sheet 05C-010 only, do a pretreatment according to ABP5-1148 PMS 01-02-31
Pre-Treatment of the P. T. F. E. Surfaces.
(p) Identify the mating surfaces of the ramp blister 05C-250 and the T-sections 05C-090
and 05C-110 with the teflon sheet 05C-010. On the mating surfaces of the ramp
blister 05C-250 of the T-sections 05C-090 and 05C-110 only, examine the condition of
the bonding primer.
(q) If the bonding primer of the ramp blister 05C-250 and the T-sections 05C-090 and
05C-110 is damaged, do the subsequent steps.
1 Remove the bonding primer with emery cloth Grade 240 to 400 .
2 Clean the mating surfaces of the ramp blister 05C-250 and the T-sections
05C-090 and 05C-110 with Material No. 08BBF1 Non Aqueous Cleaner--
Methyl-Ethyl-Ketone -.
3 Apply bonding primer to the mating surfaces of the ramp blister 05C-250 and
the T-sections 05C-090 and 05C-110, according to ABP4-1123 PMS 01-02-26
application of primer.
(r) Rub lightly the mating surfaces of the ramp blister 05C-250 and the T-sections
05C-090 and 05C-110 with emery cloth Grade 240 to 400 .
(s) Clean the mating surfaces of the ramp blister 05C-250 and the T-sections 05C-090
and 05C-110 with Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone
-.
(t) Apply Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy to the mating
surfaces of the T-sections 05C-090 and 05C-110, the ramp blister 05C-250 and the
teflon sheet 05C-010.
(u) Install the teflon sheet 05C-010 on the T-sections 05C-090 and 05C-110 and the ramp
blister 05C-250. Install the screws 05C-120 and the rivets 05C-040 thru the teflon
sheet 05C-010 and the ramp blister 05C-250. Apply pressure and let the adhesive
cure. See SRM 51-42-11 for installation of the rivets 05C-040.
(v) Tighten the screws 05C-120.
(w) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to all
fastener heads.
POST MOD 21514 AND POST SB 52-1025
(2) Removal of the central ramp.

NOTE : See IPL_FIGURE_05E.

NOTE : This procedure is applicable to the central ramps 05E-001.

(a) Remove all sealant from the fastener heads.

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(b) Remove the screws 05E-120 from the teflon sheet 05E-010.
(c) Remove the bonded teflon sheet 05E-010 from the ramp blister 05E-250 and the T-
sections 05E-090 and 05E-110.
(d) Remove the old adhesive from the component parts with a non-metallic scraper.
(e) Remove the rivets 05E-040 and the blind bolts 05E-080. See SRM 51-42-11 for
removal of the rivets 05E-040 and the blind bolts 05E-080.
(f) Remove the T-section 05E-110.
(g) Remove the rivets 05E-040 and the blind bolts 05E-050, 05E-060 and 05E-070. See
SRM 51-42-11 for removal of the rivets 05E-040 and blind bolts 05E-050, 05E-060
and 05E-070.
(h) Remove the T-section 05E-090.
(i) Remove the screws 05E-120 , 05E-240, 05E-245, the washers 05E-230, 05E-235, the
nuts 05E-220, 05E-225 and the rivets 05E-340. See SRM 51-42-11 for removal of the
rivets 05E-340.
(j) Remove ramp blister 05E-250.
(k) Remove the rivets 05E-330. See SRM 51-42-11 for removal of the rivets 05E-330.
(l) Remove the angles 05E-290 and 05E-310 from the ramp blister 05E-250.
(m) Remove the rivets 05E-330. See SRM 51-42-11 for removal of the rivets 05E-330.
(n) Remove the runout tip 05E-200.
(o) Remove the screws 05E-120.
(p) Remove the No. 2 fwd support 05E-160.
(q) Remove the screws 05E-120.
(r) Remove the No. 2 aft support 05E-180.
(s) Remove the No. 1 support 05E-140 from the cover assembly.
(3) Installation of the central ramp.

NOTE : See IPL_FIGURE_05E.

NOTE : This procedure is applicable to the central ramps 05E-001.

NOTE : Unless indicated, all fasteners and mating surfaces are to be wet installed with
Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay -.

NOTE : Where necessary use oversize fasteners.

(a) Remove all old sealant from the cover assembly and any components that were
previously removed.

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(b) Clean the surface of the cover assembly with Material No. 08BBF1 Non Aqueous
Cleaner-- Methyl-Ethyl-Ketone -.
(c) Cut some pieces of Material No. 13AEC1 Dry glass fabric-8H Satin 293 gsm - 181
style SRM Type 2 - to the shape runout tip 05E-200, the No. 2 fwd and aft supports
05E-160 and 05E-180 and No. 1 support 05E-140.
(d) Apply Material No. 13FBB1 Paste Adhesive-Epoxy Composite General Use - to the
glass fabric pieces and put them in position on the cover assembly.
(e) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surfaces of the runout tip, the No. 2 and the No. 1 supports.
(f) Install the No. 2 aft support 05E-180 with the screws 05E-120.
(g) Install the No. 2 fwd support 05E-160 with the screws 05E-120.
(h) Install the runout tip 05E-200 with the screws 05E-120.
(i) Install the T-section 05E-110 to the runout tip 05E-200 with the blind bolts 05E-080
and to the No. 2 fwd support 05E-160 and the No. 2 aft support 05E-180 with the
rivets 05E-040. See SRM 51-42-11 for installation of the rivets 05E-040 and blind
bolts 05E-080.
(j) Install the T-section 05E-090 to the No. 2 fwd support 05E-160 and the No. 2 aft
support 05E-180 with the rivets 05E-040 and together with the No. 1 support
05E-140 with the blind bolts 05E-050, 05E-060 and 05E-070 to the cover assembly.
See SRM 51-42-11 for installation of the rivets 05E-040 and blind bolts 05E-050,
05E-060 and 05E-070.
(k) Apply Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy to the mating
surfaces of the ramp blister 05E-250 and the No. 1 support 05A-140.
(l) Install the ramp blister 05E-250 with the screws 05E-120, 05E-240, 05E-245, the
washers 05E-230 and 05E-235, the nuts 05E-220, 05E-225 and the rivets 05E-340.
See SRM 51-42-11 for installation of the rivets 05E-340.
(m) Install the angles 05E-290 and 05E-310 with the screws 05E-120 and the rivets
05E-330. See SRM 51-42-11 for installation of the rivets 05E-330.
(n) Identify the mating surfaces of the teflon sheet 05E-010 with the ramp blister 05E-250
and the T-sections 05E-090 and 05E-110. On the mating surfaces of the teflon sheet
05A-010 only, do a pretreatment according to ABP5-1148 PMS 01-02-31 Pre-
Treatment of the P. T. F. E. Surfaces.
(o) Identify the mating surfaces of the ramp blister 05E-250 and the T-sections 05E-090
and 05E-110 with the teflon sheet 05E-010. On the mating surfaces of the ramp
blister 05E-250 of the T-sections 05A-090 and 05A-110 only, examine the condition of
the bonding primer.

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(p) If the bonding primer of the ramp blister 05E-250 and the T-sections 05E-090 and
05E-110 is damaged, do the subsequent steps.
1 Remove the bonding primer with emery cloth Grade 240 to 400 .
2 Clean the mating surfaces of the ramp blister 05E-250 and the T-sections
05E-090 and 05E-110 with Material No. 08BBF1 Non Aqueous Cleaner--
Methyl-Ethyl-Ketone -.
3 Apply bonding primer to the mating surfaces of the ramp blister 05E-250 and
the T-sections 05E-090 and 05E-110, according to ABP4-1123 PMS 01-02-26
Application of Primer.
(q) Rub lightly the mating surfaces of the ramp blister 05E-250 and the T-sections
05E-090 and 05E-110 with emery cloth Grade 240 to 400 .
(r) Clean the mating surfaces of the ramp blister 05E-250 and the T-sections 05E-090
and 05E-110 with Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone
-.
(s) Apply Material No. 05EJL9 Epoxy Adhesive-Metal to metal - Legacy to the mating
surfaces of the T-sections 05E-090 and 05E-110 and the ramp blister 05E-250 and the
teflon sheet 05E-010.
(t) Install the teflon sheet 05E-010 on the T-sections 05E-090 and 05E-110 and the ramp
blister 05E-250.
(u) Install the screws 05E-120 and the rivets 05E-040 through the teflon sheet 05E-010
and the ramp blister 05E-250. Apply pressure and let the adhesive cure. See SRM
51-42-11 for installation of the rivets 05E-040.
(v) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to all
fastener heads.
ALL VARIANTS
(4) Not apply.

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**For PN’s ALL

TASK 52-81-14-300-811-A01
Replacement of the Sensor-Support Assy
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
06AAC1 Polysulfide Sealant-General Purpose Interfay -
Consumable Materials
TABLE 1

B. Referenced Information
REFERENCE DESIGNATION
TASK 52-81-14-100-801-A01 Cleaning of the Painted Components
TASK 52-81-14-100-802-A01 Cleaning of the Components Which are not Painted
SRM 51-42-21
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 SPECIFIED CLEANING MATERIALS AND SOLUTIONS OR THEIR

EQUIVALENTS. THE SURFACE PROTECTION COULD BE DAMAGED IF
UNSPECIFIED MATERIALS ARE USED. IT IS IMPORTANT THAT THE
MANUFACTURER’S MIXING, APPLICATION AND TREATMENT INSTRUCTIONS
ARE FOLLOWED.

Subtask 52-81-14-300-022-A01
A. Replacement of the Sensor-Support Assy

NOTE : See IPL_FIGURE_06 and IPL_FIGURE_06A.

NOTE : This procedure is applicable to the sensor-support assy 06-030 and 06A-030.

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(1) Removal of the sensor-support assy.

(a) Remove the collars 06-020, the fasteners HI-LOK 06-010. See SRM 51-42-21 for
removal of the collars 06-020 and the fasteners HI-LOK 06-010.
(b) Remove the sensor-support assy 06-030 from the cover assy.
(2) Installation of the sensor-support assy.
(a) Clean the mating surfaces of the cover assembly and the sensor-support assy 06-030.
See TASK 52-81-14-100-801-A01 and TASK 52-81-14-100-802-A01.
(b) Apply the Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surface of the sensor-support assy 06-030 and the cover assy.
(c) Put the sensor-support assy 06-030 in the correct position on the cover assy.
(d) Install the fasteners HI-LOK 06-010 and the collars 06-020. See SRM 51-42-21 for
installation of the collars 06-020 and the fasteners HI-LOK 06-010.

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**For PN’s ALL

TASK 52-81-14-300-812-A01
Replacement of the Stops
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Referenced Information
REFERENCE DESIGNATION
TASK 52-81-14-100-801-A01 Cleaning of the Painted Components
TASK 52-81-14-100-802-A01 Cleaning of the Components Which are not Painted
SRM 51-42-21
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 SPECIFIED CLEANING MATERIALS AND SOLUTIONS OR THEIR

EQUIVALENTS. THE SURFACE PROTECTION COULD BE DAMAGED IF
UNSPECIFIED MATERIALS ARE USED. IT IS IMPORTANT THAT THE
MANUFACTURER’S MIXING, APPLICATION AND TREATMENT INSTRUCTIONS
ARE FOLLOWED.

Subtask 52-81-14-300-024-A01
A. Replacement of the Stops

NOTE : See IPL_FIGURE_06 and IPL_FIGURE_06A.

NOTE : This procedure is applicable to the stops 06-320, 06-330, 06-340, 06A-320, 06A-330
and 06A-340.
(1) Removal of the stop.
(a) Remove the rivets 06-310. See SRM 51-42-21 for removal of the rivets 06-310.
(b) Remove and discard the stop 06-320 from the cover assy.
(2) Installation of the stop.
(a) Clean the mating surfaces of the cover assembly and the stop 06-320. See TASK
52-81-14-100-801-A01 and TASK 52-81-14-100-802-A01.

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(b) Put the new stop 06-320 in the correct position on the cover assy.
(c) Install the rivets 06-310 . See SRM 51-42-21 for installation of the rivets 06-310.

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ASSEMBLY

**For PN’s ALL

TASK 52-81-14-400-801-A01
Assembly of the Sealing Strips
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Referenced Information
REFERENCE DESIGNATION
TASK 52-81-14-100-801-A01 Cleaning of the Painted Components
TASK 52-81-14-100-802-A01 Cleaning of the Components Which are not Painted
SRM 51-42-21
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 SPECIFIED CLEANING MATERIALS AND SOLUTIONS OR THEIR

EQUIVALENTS. THE SURFACE PROTECTION COULD BE DAMAGED IF
UNSPECIFIED MATERIALS ARE USED. IT IS IMPORTANT THAT THE
MANUFACTURER’S MIXING, APPLICATION AND TREATMENT INSTRUCTIONS
ARE FOLLOWED.

Subtask 52-81-14-400-024-A01
A. Assembly of the Sealing Strips
PRE MOD 21295G0066
(1) Installation of the sealing strip.

NOTE : See IPL_FIGURE_06.

NOTE : This procedure is applicable to the sealing strips 06-130, 06-140 and 06-220.
(a) Clean the mating surfaces of the cover assy and the sealing strip 06-130. See TASK
52-81-14-100-801-A01 and TASK 52-81-14-100-802-A01.
(b) Install the sealing strip 06-130 in correct place on the cover assy.

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(c) Install the profile 06-110 on sealing strip 06-130.

(d) Install the rivets 06-100. See SRM 51-42-21 for installation of the rivets 06-100.
POST MOD 21295G0066
(1) Installation of the sealing strip.

NOTE : See IPL_FIGURE_06A.

NOTE : This procedure is applicable to the sealing strips 06A-130, 06A-140 and 06A-220.
(a) Clean the mating surfaces of the cover assy and the sealing strip 06A-130. See TASK
52-81-14-100-801-A01 and TASK 52-81-14-100-802-A01.
(b) Install the sealing strip 06A-130 in correct place on the cover assy.
(c) Install the profile 06A-110 on sealing strip 06A-130.
(d) Install the screws 06A-260, the washers 06A-250 and the nuts 06A-240. Tighten the
nuts 06A-240.
ALL VARIANTS
(2) Not apply.

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**For PN’s ALL

TASK 52-81-14-400-802-A01
Assembly of the Tip Seal
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A.Referenced Information
REFERENCE DESIGNATION
TASK 52-81-14-100-801-A01 Cleaning of the Painted Components
TASK 52-81-14-100-802-A01 Cleaning of the Components Which are not Painted
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 SPECIFIED CLEANING MATERIALS AND SOLUTIONS OR THEIR

EQUIVALENTS. THE SURFACE PROTECTION COULD BE DAMAGED IF
UNSPECIFIED MATERIALS ARE USED. IT IS IMPORTANT THAT THE
MANUFACTURER’S MIXING, APPLICATION AND TREATMENT INSTRUCTIONS
ARE FOLLOWED.

Subtask 52-81-14-400-025-A01
A. Assembly of the Tip Seal
PRE MOD 21295G0066
(1) Installation of the tip seal.

NOTE : See IPL_FIGURE_06.

NOTE : This procedure is applicable to the tip seal 06-290.

(a) Clean the mating surfaces of the cover assy and the tip seal 06-290. See TASK
52-81-14-100-801-A01 and TASK 52-81-14-100-802-A01.
(b) Put the tip seal 06-290 in the correct place on the cover assy.
(c) Put the profile 06-270 on the tip seal 06-290.

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(d) Install the screws 06-260, the washers 06-250 and the nuts 06-240. Tighten the nuts
06-240.
POST MOD 21295G0066
(1) Installation of the tip seal .

NOTE : See IPL_FIGURE_06A.

NOTE : This procedure is applicable to the tip seal 06A-290.

(a) Clean the mating surfaces of the cover assy and the tip seal 06-290. See TASK
52-81-14-100-801-A01 and TASK 52-81-14-100-802-A01.
(b) Put the tip seal 06A-290 in the correct place on the cover assy.
(c) Put the profile 06A-270 and the shim 06A-285 on the tip seal 06A-290 .
(d) Install the screws 06A-260, the washers 06A-250 and the nuts 06A-240. Tighten the
nuts 06A-240.
ALL VARIANTS
(2) Not apply.

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**For PN’s ALL

TASK 52-81-14-400-803-A01
Assembly of the Sensor Targets
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
05EML9 Epoxy Adhesive-- - Legacy 1
Consumable Materials
TABLE 1

B.Referenced Information
REFERENCE DESIGNATION
TASK 52-81-14-100-801-A01 Cleaning of the Painted Components
TASK 52-81-14-100-802-A01 Cleaning of the Components Which are not Painted
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 SPECIFIED CLEANING MATERIALS AND SOLUTIONS OR THEIR

EQUIVALENTS. THE SURFACE PROTECTION COULD BE DAMAGED IF
UNSPECIFIED MATERIALS ARE USED. IT IS IMPORTANT THAT THE
MANUFACTURER’S MIXING, APPLICATION AND TREATMENT INSTRUCTIONS
ARE FOLLOWED.

Subtask 52-81-14-400-023-A01
A. Assembly of the Sensor Targets

NOTE : See IPL_FIGURE_06 and IPL_FIGURE_06A.

NOTE : This procedure is applicable to the target 06-070 and 06A-070.

(1) Clean the mating surfaces of the sensor-support 06-090 and the shim 06-080. See TASK
52-81-14-100-801-A01 and TASK 52-81-14-100-802-A01.

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(2) Apply the Material No. 05EML9 Epoxy Adhesive-- - Legacy 1 to the mating surfaces of the
sensor-support 06-090 and the shim 06-080.
(3) Install the shim 06-080 and the target 06-070 with the screws 06-060, the washers 06-050
and the nuts 06-040 to the sensor-support 06-090. Tighten the nuts 06-040.

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**For PN’s ALL

TASK 52-81-14-400-804-A01
Assembly of the Step Assemblies
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
06AAC1 Polysulfide Sealant-General Purpose Interfay -
14QJB1 Wire-Locking Dia: 1.6 mm CRES Nickel Alloy -
Consumable Materials
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 SPECIFIED CLEANING MATERIALS AND SOLUTIONS OR THEIR

EQUIVALENTS. THE SURFACE PROTECTION COULD BE DAMAGED IF
UNSPECIFIED MATERIALS ARE USED. IT IS IMPORTANT THAT THE
MANUFACTURER’S MIXING, APPLICATION AND TREATMENT INSTRUCTIONS
ARE FOLLOWED.

**For PN’s D5288000800000 D5288000800098 D5288000800100 D5288000800198 D5288000900000

D5288000900098 D5288000900100 D5288000900198 D5288001000000 D5288001000098
D5288001000100 D5288001000198

Subtask 52-81-14-410-004-A01
A. Assembly of the Step Assy

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.

NOTE : See IPL_FIGURE_03 and IPL_FIGURE_03B.

NOTE : This procedure is applicable to the step assies 03-370 and 03B-370.

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(1) Assembly of the step assy 03-370.

(a) Apply a layer of Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay -
to the mating surfaces of the protector 03-380, the step assembly 03-370 and the
cover assembly.
(b) Install the protector 03-380 and the step assembly 03-370 with the bolts 03-350 and
03-360 to the cover assembly.
(c) Safety the bolts 03-350 and 03-360 with Material No. 14QJB1 Wire-Locking Dia: 1.6
mm CRES Nickel Alloy -.
(2) Assembly of the step assy 03-390.
(a) Apply a layer of Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay -
to the mating surfaces of the protection plate 03-400, the step 03-390 and the cover
assembly.
(b) Install the protection plate 03-400 and the step 03-390 with the bolts 03-360 to the
cover assembly.
(c) Safety the bolts 03-360 with Material No. 14QJB1 Wire-Locking Dia: 1.6 mm CRES
Nickel Alloy -.

**For PN’s D5288000800094 D5288000800095 D5288000800194 D5288000800195 D5288000900094

D5288000900095 D5288000900194 D5288000900195 D5288001000094 D5288001000095
D5288001000194 D5288001000195

Subtask 52-81-14-410-004-B01
B. Assembly of the Step Assy

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.

NOTE : See IPL_FIGURE_03C.

NOTE : This procedure is applicable to the step assy 03C-370, 03C-390 and 03C-410.
(1) Assembly of the step assy 03C-370.
(a) Apply a layer of Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay -
to the mating surfaces of the protector 03C-380, the step assembly 03C-370 and the
cover assembly.
(b) Install the protector 03C-380 and the step assembly 03C-370 with the bolts 03C-350
and 03C-360 to the cover assembly.
(c) Safety the bolts 03C-350 and 03C-360 with Material No. 14QJB1 Wire-Locking Dia:
1.6 mm CRES Nickel Alloy -.

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(2) Assembly of the step assy 03C-390.

NOTE : This procedure is applicable to the step assy 03C-410.

(a) Apply a layer of Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay -
to the mating surfaces of the protection plate 03C-400, the step 03C-390 and the
cover assembly.
(b) Install the protection plate 03C-400 and the step 03C-390 with the bolts 03C-360 to
the cover assembly.
(c) Safety the bolts 03C-360 with Material No. 14QJB1 Wire-Locking Dia: 1.6 mm CRES
Nickel Alloy -.
(3) Assembly of the step assy 03C-410.
(a) Apply a layer of Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay -
to the mating surfaces of the step 03C-410 and the cover assembly.
(b) Install the step 03C-410 with the bolts 03C-360 to the cover assembly.
(c) Safety the bolts 03C-360 with Material No. 14QJB1 Wire-Locking Dia: 1.6 mm CRES
Nickel Alloy -.

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**For PN’s ALL

TASK 52-81-14-400-805-A01
Assembly of the Uplock Assy
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
03HBD9 Synthetic Ester base Grease-General Purpose Low Temp -
06AAC1 Polysulfide Sealant-General Purpose Interfay -
19-010 Lockwire Stainless Steel annealed 0.8 mm Dia.
Consumable Materials
TABLE 1

B.Referenced Information
REFERENCE DESIGNATION
FIGURE 52-81-14-991-005-A FIGURE 52-81-14-991-005-A-Arm, Neutral Position
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 SPECIFIED CLEANING MATERIALS AND SOLUTIONS OR THEIR

EQUIVALENTS. THE SURFACE PROTECTION COULD BE DAMAGED IF
UNSPECIFIED MATERIALS ARE USED. IT IS IMPORTANT THAT THE
MANUFACTURER’S MIXING, APPLICATION AND TREATMENT INSTRUCTIONS
ARE FOLLOWED.

Subtask 52-81-14-400-001-A01
A. Assembly of the Uplock Assy

NOTE : See IPL_FIGURE_03, IPL_FIGURE_03B and IPL_FIGURE_03C.

NOTE : This procedure is applicable to the uplock assies 03-040, 03B-040 and 03C-040.

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(1) Assembly of the Fitting 03-320.

NOTE : Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose
Low Temp - to all movable parts.
(a) Apply Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surface of the fluted plate 03-330 and the cover assembly.
(b) Install the fluted plate 03-030 and the fitting 03-320 with the bolts 03-010 to the
door.
(c) Safety the bolts 03-010 with Material No. 19-010 Lockwire Stainless Steel annealed
0.8 mm Dia..
(d) Assemble the fluted plate 03-330 and the mounting base 03-340 with the bolts
03-310, the washers 03-300 and the nuts 03-290 to the fitting 03-320.
(e) Safety the nuts 03-290 with the cotter pins 03-120. Do not safety the bolts 03-310 as
final adjustment is made on the aircraft.
(2) Assembly of the Side Fittings 03-260 and 03-270.

NOTE : Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose
Low Temp - to all movable parts.
(a) Install the bushes 03-230 and 03-280 and the side fittings 03-260 and 03-270 to the
mounting base 03-340.
(b) Install the distance piece 03-250 between the side fittings 03-260 and 03-270 with the
screws 03-150 and 03-160, the washers 03-140 and the nuts 03-130.
(c) Safety the nuts 03-130 with the cotter pins 03-120.
(d) Install the pin 03-210 and the screw 03-200 in the mounting base 03-340.

NOTE : The pin 03-210 must be between the fork end of the side fitting 03-270.
(3) Assembly of the Torque Shaft 03-240.

NOTE : Apply the Material No. 03HBD9 Synthetic Ester base Grease-General Purpose
Low Temp - to all movable parts.
(a) Install the torque shaft 03-240 in the protector cap 03-220 and secure with the cotter
pin 03-060.

NOTE : Drill a 2.7 mm (0.106 in) diameter hole through the assembled torque shaft
03-240 and the protector cap 03-220 if you use a new torque shaft 03-240.

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(b) Install the protector cap 03-220 together with the assembled torque shaft 03-240 with
the screw 03-200, the pin 03-210, the washers 03-190 and the nuts 03-180 to the
mounting base 03-340.

NOTE : Make sure that the neutral position is correct. See FIGURE
52-81-14-991-005-A.
(c) Safety the nuts 03-180 with the cotter pins 03-170.
(4) Assembly of the Roller 03-100.
(a) Install the lubrication fitting 03-050 in the bolt 03-090.
(b) Install the roller 03-100 and the bushes 03-110 with the bolt 03-090, the washer
03-080 and the nut 03-070.
(c) Safety the nut 03-070 with the cotter pin 03-060.
(d) Fill the lubrication fitting 03-050 with Material No. 03HBD9 Synthetic Ester base
Grease-General Purpose Low Temp -.

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**For PN’s ALL

14.09 1

F_CM_528114_1_0050101_01_00

Arm, Neutral Position

FIGURE-52-81-14-991-005-A01

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**For PN’s ALL

TASK 52-81-14-400-807-A01
Assembly of the Rear Fitting
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
14SBA1 Textile-Lint free Cotton -
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
13FBB2 Paste Adhesive-Epoxy Composite General Use Structure
14QJB1 Wire-Locking Dia: 1.6 mm CRES Nickel Alloy -
04TMB2 Varnish-- Electrical Bonding Structure
06ABA1 Polysulfide Sealant-Fuel Tank Brushable -
06AAC1 Polysulfide Sealant-General Purpose Interfay -
03HBD9 Synthetic Ester base Grease-General Purpose Low Temp -
Consumable Materials
TABLE 1

B. Fixtures, Tools, Test and Support Equipment

REFERENCE DESIGNATION
98D52109001000 Fitting Replacement Tool
soft brush
Fixtures, Tools, Test and Support Equipment
TABLE 2

C. Referenced Information
REFERENCE DESIGNATION
TASK 52-81-14-100-802-A01 Cleaning of the Components Which are not Painted
SRM 51-42-21
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.

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.

CAUTION : USE ONLY SPECIFIED CLEANING MATERIALS AND SOLUTIONS OR THEIR

EQUIVALENTS. THE SURFACE PROTECTION COULD BE DAMAGED IF
UNSPECIFIED MATERIALS ARE USED. IT IS IMPORTANT THAT THE
MANUFACTURER’S MIXING, APPLICATION AND TREATMENT INSTRUCTIONS
ARE FOLLOWED.

Subtask 52-81-14-400-003-A01
A. Assembly of the Rear Fitting

NOTE : See IPL_FIGURE_07.

(1) Assembly of the fitting.

NOTE : This procedure is applicable to the fitting 07-270.

(a) Clean the matting surfaces of the fitting 07-270 and the cover assembly with a soft
brush or with a Material No. 14SBA1 Textile-Lint free Cotton - soaked with Material
No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(b) Before the installation of the fitting 07-270, make sure that the shim on the cover
assembly is not damaged.
(c) Make sure that the diameter of the bolts 07-150 and 07-160 are in correct conditions
between 6.32 mm (0.2488 in) and 6.34 mm (0.2496 in).
(d) Make sure that the diameter of the screws 07-170 are in correct conditions between
6.31 mm (0.2484 in) and 6.34 mm (0.2496 in).
(e) Make sure that the holes of the fitting 07-270 for the bolts 07-150 and 07-160 are in
correct conditions and the diameter is 6.5 mm (0.256 in). For replacement for a new
fitting 07-270, please contact AIRBUS.
(f) Make sure that the holes of the fitting 07-270 for the screws 07-170 are in correct
conditions and the diameter is 6.6 mm (0.260 in). For replacement for a new fitting
07-270, please contact AIRBUS.
(g) Apply the Material No. 13FBB2 Paste Adhesive-Epoxy Composite General Use
Structure to the mating surface of the fitting 07-270 and the cover assembly.

Page 7015
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COMPONENT MAINTENANCE MANUAL
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(h) Make sure that the bolts 07-150 and 07-160 engaged a minimum of 6 mm (0.23 in) in
the inserts 07-180.
(i) Install the fitting 07-270 with the bolts 07-150 and 07-160, the screws 07-170, the
washers 07-030 and the nuts 07-020 to the cover assembly.
(j) Safety the nuts 07-020 with the new cotter pins 07-010, the bolts 07-150 and 07-160
with Material No. 14QJB1 Wire-Locking Dia: 1.6 mm CRES Nickel Alloy -.
(k) Remove the unwanted Material No. 13FBB2 Paste Adhesive-Epoxy Composite
General Use Structure with a Material No. 14SBA1 Textile-Lint free Cotton -.
(l) Apply the Material No. 04TMB2 Varnish-- Electrical Bonding Structure on the edges
between the fitting 07-270 and the cover assembly.
(m) Clean the mating surfaces of the profile 07-140 and the fitting 07-270, and the mating
surfaces of the profile 07-140 and the bonding strap 07-050. See TASK
52-81-14-100-802-A01.
(n) Put the profile 07-140 in the correct position in the fitting 07-270 and the cover
assembly.
(o) Install the rivet 07-045 and the bolt 07-130 , the washer 07-030 and the nut 07-020.
See SRM 51-42-21 for the installation of the rivet 07-045.
(p) Safety the nut 07-020 with the new cotter pin 07-010.
(q) Put the bonding strap 07-050 in the correct position on the profile 07-140.
(r) Install the bonding strap 07-050 with the bolt 07-040 , the washer 07-030 and the nut
07-020.
(s) Safety the nut 07-020 with the new cotter pin 07-010.
(t) Apply the Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable - on the
bolts 07-040 and 07-130, the washers 07-030 and the nuts 07-020 and the new cotter
pin 07-010.
1 The layer of Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable -
must cover a minimum area around the mating surfaces of 10 mm (0.39 in).
(u) Apply the Material No. 04TMB2 Varnish-- Electrical Bonding Structure on the
Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable - around to between 2
(0.08 in) and 3 mm (0.12 in).
(2) Assembly of the hinge.

NOTE : This procedure is applicable to the hinge 07-250.

(a) Clean the matting surfaces of the hinge 07-250 with a soft brush or with a Material
No. 14SBA1 Textile-Lint free Cotton - soaked with Material No. 08BBF1 Non
Aqueous Cleaner-- Methyl-Ethyl-Ketone -.

Page 7016
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(b) Make sure that the 98D52109001000 Fitting Replacement Tool is installed and
calibrated on the door.
(c) Make sure that the holes of the hinge 07-250 are in correct condition and the
diameter is between 6.31 mm (0.2484 in) and 6.35 mm (0.2500 in). For replacement
for a new hinge 07-250, please contact AIRBUS.
(d) Make sure that the diameter of the bolts 07-240 is in correct conditions between 6.32
mm (0.2490 in) and 6.34 mm (0.2495 in).
(e) Apply the Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surfaces between the hinge 07-250 and the fitting 07-270.
(f) Put the hinge 07-250 in the correct position on the fitting 07-270.
(g) Install the bolts 07-240, the washers 07-230 and the nuts 07-220. Tighten the nuts
07-220.
(h) Safety the nuts 07-220 with the new cotter pins 07-210.
(i) Remove the unwanted Material No. 06AAC1 Polysulfide Sealant-General Purpose
Interfay - with a Material No. 14SBA1 Textile-Lint free Cotton -.
(j) Apply the Material No. 04TMB2 Varnish-- Electrical Bonding Structure on the edges
between the hinge 07-250 and the fitting 07-270.
(k) Fill the lubrication fitting 07-100 with the Material No. 03HBD9 Synthetic Ester base
Grease-General Purpose Low Temp -.
(l) Disassemble the 98D52109001000 Fitting Replacement Tool from the door.

Page 7017
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COMPONENT MAINTENANCE MANUAL
D5288000800000

**For PN’s D5288000800000 D5288000800095 D5288000800100 D5288000800195 D5288000900000

D5288000900095 D5288000900100 D5288000900195 D5288001000000 D5288001000095 D5288001000100
D5288001000195

TASK 52-81-14-400-808-A01
Assembly of the FWD Fitting Assy
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
06AAC1 Polysulfide Sealant-General Purpose Interfay -
14QJB1 Wire-Locking Dia: 1.6 mm CRES Nickel Alloy -
06ABA1 Polysulfide Sealant-Fuel Tank Brushable -
04TMB2 Varnish-- Electrical Bonding Structure
14SBA1 Textile-Lint free Cotton -
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
Consumable Materials
TABLE 1

B. Fixtures, Tools, Test and Support Equipment

REFERENCE DESIGNATION
98D52109001000 FWD fitting assy Replacement Tool
soft brush
Fixtures, Tools, Test and Support Equipment
TABLE 2

C.Referenced Information
REFERENCE DESIGNATION
TASK 52-81-14-100-801-A01 Cleaning of the Painted Components
TASK 52-81-14-100-802-A01 Cleaning of the Components Which are not Painted
FIGURE 52-81-14-991-016-A FIGURE 52-81-14-991-016-A-Bolts and Holes in the FWD Fitting
Assy
FIGURE 52-81-14-991-015-A FIGURE 52-81-14-991-015-A-Bolts and Holes in the Hinge Assy

Page 7018
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COMPONENT MAINTENANCE MANUAL
D5288000800000

REFERENCE DESIGNATION
FIGURE 52-81-14-991-017-A FIGURE 52-81-14-991-017-A-Bolts and Holes in the FWD Fitting
Assy
Referenced Information
TABLE 3

3. Procedure

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

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

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.

CAUTION : USE ONLY SPECIFIED CLEANING MATERIALS AND SOLUTIONS OR THEIR

EQUIVALENTS. THE SURFACE PROTECTION COULD BE DAMAGED IF
UNSPECIFIED MATERIALS ARE USED. IT IS IMPORTANT THAT THE
MANUFACTURER’S MIXING, APPLICATION AND TREATMENT INSTRUCTIONS
ARE FOLLOWED.

Subtask 52-81-14-400-016-A01
A. Assembly of the FWD Fitting Assy
PRE SB 52-1022
(1) Assembly of the FWD fitting assy.

NOTE : See IPL_FIGURE_02.

NOTE : This procedure is applicable to the FWD fitting assy 02-200.

(a) Make sure that the diameters of the holes in the FWD fitting assy 02-200 are in the
limits, see TABLE 4 and FIGURE 52-81-14-991-016-A. For replacement for a new
FWD fitting assy 02-200, please contact AIRBUS.
(b) Make sure that the diameters of the bolts 02-170 and the screws 02-190 are in the
limits. See TABLE 4 and FIGURE 52-81-14-991-016-A.
(c) Clean the matting surfaces of the FWD fitting assy 02-200 and the cover assembly.
See TASK 52-81-14-100-801-A01 and TASK 52-81-14-100-802-A01.
(d) Apply the Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surface of the FWD fitting assy 02-200 and the cover assembly.

Page 7019
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(e) Make sure that the bolts 02-170 are engaged a minimum of 6 mm (0.23 in) in the
inserts 02-180.
(f) Install the FWD fitting assy 02-200 on the cover assembly in the correct position.
(g) Install the bolts 02-170, the screws 02-190, the washers 02-030 and the nuts 02-020.
Tighten the bolts 02-170 and nuts 02-020.
(h) Safety the nuts 02-020 with the new cotter pins 02-010.
(i) Safety the bolts 02-170 with Material No. 14QJB1 Wire-Locking Dia: 1.6 mm CRES
Nickel Alloy -.
(j) Clean the mating surfaces of the bracket 02-160 and the FWD fitting assy 02-200 and
the mating surfaces of the bracket 02-160 and the bonding strap 02-050. See TASK
52-81-14-100-802-A01 for cleaning of the bonding points.
(k) Install the bracket 02-160 with the bolt 02-150, the washer 02-030 and the nut
02-020. Tighten the nut 02-020.
(l) Safety the nut02-020 with the new cotter pin 02-010.
(m) Apply the Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable - on the
bolt 02-150, the washer 02-030 and the nut 02-020 and the new cotter pin 02-010.
1 The layer of Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable -
must cover a minimum area around the mating surfaces of 10 mm (0.39 in).
(n) Apply a layer of Material No. 04TMB2 Varnish-- Electrical Bonding Structure on the
Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable -.
(o) Make sure that the layer of Material No. 04TMB2 Varnish-- Electrical Bonding
Structure covers an area around the Material No. 06ABA1 Polysulfide Sealant-Fuel
Tank Brushable - between 3 and 5 mm (0.12 and 0.20 in).
(p) Install the bonding strap 02-050 with the screw 02-040, the washer 02-030 and the
nut 02-020.
(q) Safety the nut 02-020 with the new cotter pin 02-010.
(r) Apply the Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable - on the
screw 02-040, the washer 02-030 and the nut 02-020 and the new cotter pin 02-010.
1 The layer of Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable -
must cover a minimum area around the mating surfaces of 10 mm (0.39 in).
(s) Apply a layer of Material No. 04TMB2 Varnish-- Electrical Bonding Structure on the
Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable -.

Page 7020
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(t) Make sure that the layer of Material No. 04TMB2 Varnish-- Electrical Bonding
Structure covers an area around the Material No. 06ABA1 Polysulfide Sealant-Fuel
Tank Brushable - between 3 and 5 mm (0.12 and 0.20 in).
SCREWS AND BOLTS FWD FITTING ASSY HOLES
LOC NO. IPL ITEM NO. DIAMETERS DIMENSIONS DIAMETERS DIMENSIONS
MIN MAX MIN MAX
A 02-170 6.32 mm 6.34 mm 6.5 mm (0.256 6.5 mm (0.256
(0.2490 in) (0.2495 in) in) in)
B 02-190 6.31 mm 6.34 mm 6.6 mm (0.260 6.6 mm (0.260
(0.2484 in) (0.2495 in) in) in)
Screws, Bolts and Holes Diameters Dimensions
TABLE 4

(2) Assembly of the hinge assy.

NOTE : This procedure is applicable to the hinge assy 02-340.

(a) Make sure that the 98D52109001000 FWD fitting assy Replacement Tool is installed
and calibrated on the door.
(b) Make sure that the diameters of the holes in the hinge assy 02-340 are in the limits,
see TABLE 5 and FIGURE 52-81-14-991-015-A. For replacement for a new hinge assy
02-340, please contact AIRBUS.
(c) Make sure that the diameters of the bolts 02-270, 02-300 and 02-330 are in the
limits. See TABLE 5 and FIGURE 52-81-14-991-015-A.
(d) Clean the matting surfaces of the hinge assy 02-340 and the FWD fitting assy 02-200
with a soft brush or with a Material No. 14SBA1 Textile-Lint free Cotton - soaked
with Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
(e) Apply the Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surfaces between the hinge assy 02-340 and the FWD fitting assy 02-200.
(f) Install the hinge assy 02-340 in the correct position on the FWD fitting assy 02-200.
(g) Install the bolt 02-270, the washer 02-260 and the nut 02-250. Tighten the nut
02-250.
(h) Install the bolts 02-300, the washers 02-290 and the nuts 02-280. Tighten the nuts
02-280.
(i) Install the bolts 02-330, the washers 02-320, and the nuts 02-310. Tighten the nuts
02-310.
(j) Safety the nuts 02-250, 02-280, 02-310, with the new cotter pins 02-240.
(k) Remove the excess of Material No. 06AAC1 Polysulfide Sealant-General Purpose
Interfay - with a Material No. 14SBA1 Textile-Lint free Cotton -.

Page 7021
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COMPONENT MAINTENANCE MANUAL
D5288000800000

(l) Apply the Material No. 04TMB2 Varnish-- Electrical Bonding Structure on the edges
between the hinge assy 02-340 and the FWD fitting assy 02-200.
FWD FITTING ASSY AND
BOLTS DIAMETERS
HINGE ASSY HOLES
LOC NO. IPL ITEM NO. DIMENSIONS
DIAMETERS DIMENSIONS
MIN MAX MIN MAX
A 02-270 6.32 m (0.2490 6.34 m (0.2495 6.31 mm 6.35 mm
in) in) (0.2484 in) (0.2500 in)
B 02-330 9.50 mm 9.51 mm 9.49 mm 9.53 mm
(0.3740 in) (0.3745 in) (0.3736 in) (0.3752 in)
C 02-300 7.91 mm 7.93 mm 7.90 mm 7.94 mm
(0.3115 in) (0.3120 in) (0.3110 in) (0.3126 in)
Bolts and Holes Diameters Dimensions
TABLE 5

(m) Disassemble the 98D52109001000 FWD fitting assy Replacement Tool from the door.
POST SB 52-1022
(1) Assembly of the FWD fitting assy.

NOTE : See IPL_FIGURE_02A.

NOTE : This procedure is applicable to the FWD fitting assy 02A-480.

(a) Make sure that the diameters of the holes in the FWD fitting assy 02A-480 are in the
limits, see TABLE 6 and FIGURE 52-81-14-991-017-A. For replacement for a new
FWD fitting assy 02A-480, please contact AIRBUS.
(b) Make sure that the diameters of the screws 02A-190 and the bolts 02A-170, 02A-720,
02A-730, 02A-740, 02A-750 are in the limits. See TABLE 6 and FIGURE
52-81-14-991-017-A.
(c) Clean the matting surfaces of the FWD fitting assy 02A-480 and the cover assembly.
See and .
(d) Apply the Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surface of the FWD fitting assy 02A-480 and the cover assembly.
(e) Make sure that the bolts 02A-170 are engaged a minimum of 6 mm (0.23 in) in the
inserts 02A-180.
(f) Install the FWD fitting assy 02A-480 on the cover assembly in the correct position.
(g) Install the screws 02A-190 , the bolts 02A-170, 02A-720, 02A-730, 02A-740, 02A-750,
the washers 02A-030 and the nuts 02A-020, 02A-710. Tighten the bolts 02A-170 and
the nuts 02A-020, 02A-710.

Page 7022
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 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

(h) Safety the nuts 02A-020 with the new cotter pins 02A-010.
(i) Safety the bolts 02A-170 with Material No. 14QJB1 Wire-Locking Dia: 1.6 mm CRES
Nickel Alloy -.
(j) Clean the mating surfaces of the bracket 02A-160 and the FWD fitting assy 02A-480
and the mating surfaces of the bracket 02A-160 and the bonding strap 02A-050. See
TASK 52-81-14-100-802-A01 for cleaning of the bonding points.
(k) Install the bracket 02A-160 with the bolt 02A-150, the washer 02A-030 and the nut
02A-020. Tighten the nut 02A-020.
(l) Safety the nut 02A-020 with the new cotter pin 02A-010.
(m) Apply the Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable - on the
bolt 02A-150, the washer 02A-030, the nut 02A-020 and the new cotter pin 02A-010.
1 The layer of Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable -
must cover a minimum area around the mating surfaces of 10 mm (0.39 in).
(n) Apply a layer of Material No. 04TMB2 Varnish-- Electrical Bonding Structure on the
Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable -.
(o) Make sure that the layer of Material No. 04TMB2 Varnish-- Electrical Bonding
Structure covers an area around the Material No. 06ABA1 Polysulfide Sealant-Fuel
Tank Brushable - between 3 and 5 mm (0.12 and 0.20 in).
(p) Install the bonding strap 02A-050 with the screw 02A-040, the washer 02A-030 and
the nut 02A-020.
(q) Safety the nut 02A-020 with the new cotter pin 02A-010.
(r) Apply the Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable - on the
screw 02A-040 , the washer 02A-030 and the nut 02A-020 and the new cotter pin
02A-010.
1 The layer of Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable -
must cover a minimum area around the mating surfaces of 10 mm (0.39 in).
(s) Apply a layer of Material No. 04TMB2 Varnish-- Electrical Bonding Structure on the
Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable -.
(t) Make sure that the layer of Material No. 04TMB2 Varnish-- Electrical Bonding
Structure covers an area around the Material No. 06ABA1 Polysulfide Sealant-Fuel
Tank Brushable - between 3 and 5 mm (0.12 and 0.20 in).
SCREWS AND BOLTS FWD FITTING ASSY HOLES
LOC NO. IPL ITEM NO. DIAMETERS DIMENSIONS DIAMETERS DIMENSIONS
MIN MAX MIN MAX
6.32 mm 6.34 mm 6.5 mm (0.256 6.5 mm (0.256
A 02A-170 (0.2490 in) (0.2495 in) in) in)

Page 7023
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COMPONENT MAINTENANCE MANUAL
D5288000800000

SCREWS AND BOLTS FWD FITTING ASSY HOLES

LOC NO. IPL ITEM NO. DIAMETERS DIMENSIONS DIAMETERS DIMENSIONS
MIN MAX MIN MAX
02A-190,
02A-720, 6.31 mm 6.34 mm 6.6 mm (0.260 6.6 mm (0.260
B 02A-730, (0.2484 in) (0.2495 in) in) in)
02A-740,
02A-750
Screws, Bolts and Holes Diameters Dimensions
TABLE 6

(2) Assembly of the hinge assy.

NOTE : This procedure is applicable to the hinge assy 02A-610.

(a) Make sure that the 98D52109001000 FWD fitting assy Replacement Tool is installed
and calibrated on the door.
(b) Make sure that the diameters of the holes in the hinge assy 02A-610 are in the limits,
see TABLE 7 and FIGURE 52-81-14-991-015-A. For replacement for a new hinge assy
02A-610, please contact AIRBUS.
(c) Make sure that the diameters of the bolts 02A-540, 02A-570, 02A-600 are in the
limits. See TABLE 7 and FIGURE 52-81-14-991-015-A.
(d) Clean the matting surfaces of the hinge assy 02A-610 and the FWD fitting assy
02A-480 with a soft brush or with a Material No. 14SBA1 Textile-Lint free Cotton -
soaked with Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
(e) Apply the Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surfaces between the hinge assy 02A-610 and the FWD fitting assy 02A-480.
(f) Install the hinge assy 02A-610 in the correct position on the FWD fitting assy
02A-480.
(g) Install the bolt 02A-540, the washer 02A-530 and the nut 02A-520. Tighten the nut
02A-520.
(h) Install the bolts 02A-570, the washers 02A-560 and the nuts 02A-550. Tighten the
nuts 02A-550.
(i) Install the bolts 02A-600, the washers 02A-590, and the nuts 02A-580. Tighten the
nuts 02A-580.
(j) Safety the nuts 02A-520, 02A-550, 02A-580 with the new cotter pins 02A-510.
(k) Remove the excess of Material No. 06AAC1 Polysulfide Sealant-General Purpose
Interfay - with a Material No. 14SBA1 Textile-Lint free Cotton -.

Page 7024
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 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

(l) Apply the Material No. 04TMB2 Varnish-- Electrical Bonding Structure on the edges
between the hinge assy 02A-610 and the FWD fitting assy 02A-480.
FWD FITTING ASSY AND
BOLTS DIAMETERS
HINGE ASSY HOLES
LOC NO. IPL ITEM NO. DIMENSIONS
DIAMETERS DIMENSIONS
MIN MAX MIN MAX
A 02A-540 6.32 m (0.2490 6.34 m (0.2495 6.31 mm 6.35 mm
in) in) (0.2484 in) (0.2500 in)
B 02A-600 9.50 mm 9.51 mm 9.49 mm 9.53 mm
(0.3740 in) (0.3745 in) (0.3736 in) (0.3752 in)
C 02A-570 7.91 mm 7.93 mm 7.90 mm 7.94 mm
(0.3115 in) (0.3120 in) (0.3110 in) (0.3126 in)
Bolts and Holes Diameters Dimensions
TABLE 7

(m) Disassemble the 98D52109001000 FWD fitting assy Replacement Tool from the door.
ALL VARIANTS
(3) Not apply.

Page 7025
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

**For PN’s D5288000800000 D5288000800095 D5288000800100 D5288000800195 D5288000900000

D5288000900095 D5288000900100 D5288000900195 D5288001000000 D5288001000095 D5288001000100
D5288001000195

A HINGE ASSY

L_CM_528114_1_0150101_01_00

Bolts and Holes in the Hinge Assy

FIGURE-52-81-14-991-015-A01

Page 7026
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

**For PN’s D5288000800000 D5288000800095 D5288000800100 D5288000800195 D5288000900000

D5288000900095 D5288000900100 D5288000900195 D5288001000000 D5288001000095 D5288001000100
D5288001000195

A
B

FITTING

L_CM_528114_1_0160101_01_00

Bolts and Holes in the FWD Fitting Assy

FIGURE-52-81-14-991-016-A01

Page 7027
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 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

**For PN’s D5288000800000 D5288000800095 D5288000800100 D5288000800195 D5288000900000

D5288000900095 D5288000900100 D5288000900195 D5288001000000 D5288001000095 D5288001000100
D5288001000195
B

B FITTING

A
L_CM_528114_1_0170101_01_00

Bolts and Holes in the FWD Fitting Assy

FIGURE-52-81-14-991-017-A01

Page 7028
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

**For PN’s D5288000800094 D5288000800098 D5288000800194 D5288000800198 D5288000900094

D5288000900098 D5288000900194 D5288000900198 D5288001000094 D5288001000098 D5288001000194
D5288001000198

TASK 52-81-14-400-808-B01
Assembly of the FWD Fitting Assy
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
06AAC1 Polysulfide Sealant-General Purpose Interfay -
14QJB1 Wire-Locking Dia: 1.6 mm CRES Nickel Alloy -
06ABA1 Polysulfide Sealant-Fuel Tank Brushable -
04TMB2 Varnish-- Electrical Bonding Structure
14SBA1 Textile-Lint free Cotton -
Consumable Materials
TABLE 1

B. Fixtures, Tools, Test and Support Equipment

REFERENCE DESIGNATION
98D52109001000 FWD fitting assy Replacement Tool
Fixtures, Tools, Test and Support Equipment
TABLE 2

C. Referenced Information
REFERENCE DESIGNATION
TASK 52-81-14-100-801-A01 Cleaning of the Painted Components
TASK 52-81-14-100-802-A01 Cleaning of the Components Which are not Painted
SRM 51-42-21
FIGURE 52-81-14-991-020-A FIGURE 52-81-14-991-020-A-Bolts and Holes in the FWD Fitting
Assy
FIGURE 52-81-14-991-018-A FIGURE 52-81-14-991-018-A-Bolts and Holes in the Hinge Assy
FIGURE 52-81-14-991-021-A FIGURE 52-81-14-991-021-A-Bolts and Holes in the FWD Fitting
Assy
FIGURE 52-81-14-991-022-A FIGURE 52-81-14-991-022-A-Bolts and Holes in the FWD Fitting
Assy

Page 7029
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 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

REFERENCE DESIGNATION
FIGURE 52-81-14-991-019-A FIGURE 52-81-14-991-019-A-Bolts and Holes in the Hinge Assy
FIGURE 52-81-14-991-022-A FIGURE 52-81-14-991-022-A-Bolts and Holes in the FWD Fitting
Assy
FIGURE 52-81-14-991-019-A FIGURE 52-81-14-991-019-A-Bolts and Holes in the Hinge Assy
Referenced Information
TABLE 3

3. Procedure

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

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

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.

CAUTION : USE ONLY SPECIFIED CLEANING MATERIALS AND SOLUTIONS OR THEIR

EQUIVALENTS. THE SURFACE PROTECTION COULD BE DAMAGED IF
UNSPECIFIED MATERIALS ARE USED. IT IS IMPORTANT THAT THE
MANUFACTURER’S MIXING, APPLICATION AND TREATMENT INSTRUCTIONS
ARE FOLLOWED.

**For PN’s D5288000800094 D5288000800194 D5288000900094 D5288000900194 D5288001000094

D5288001000194

Subtask 52-81-14-400-022-A01
A. Assembly of the FWD Fitting Assy
PRE SB 52-1022 AND 52-1073
(1) Assembly of the FWD fitting assy.

NOTE : See IPL_FIGURE_02.

NOTE : This procedure is applicable to the FWD fitting assy 02-200.

(a) Make sure that the diameters of the holes in the FWD fitting assy 02-200 are in the
limits, see TABLE 4 and FIGURE 52-81-14-991-020-A. For replacement for a new
fitting TBD, please contact AIRBUS.
(b) Make sure that the diameters of the bolts 02-170 and the screws 02-190 are in the
limits. See TABLE 4 and FIGURE 52-81-14-991-020-A.

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(c) Clean the matting surfaces of the FWD fitting assy 02-200 and the cover assembly.
See TASK 52-81-14-100-801-A01 and TASK 52-81-14-100-802-A01.
(d) Apply the Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surface of the FWD fitting assy 02-200 and the cover assembly.
(e) Make sure that the bolts 02-170 are engaged a minimum of 6 mm (0.23 in) in the
inserts 02-180.
(f) Install the FWD fitting assy 02-200 on the cover assembly in the correct position.
(g) Install the bolts 02-170, the screws 02-190, the washers 02-030 and the nuts 02-020 .
Tighten the bolts 02-170 and nuts 02-020.
(h) Safety the nuts 02-020 with the new cotter pins 02-010.
(i) Safety the bolts 02-170 with Material No. 14QJB1 Wire-Locking Dia: 1.6 mm CRES
Nickel Alloy -.
(j) Clean the mating surfaces of the profile 02-160 and the FWD fitting assy 02-200 and
the mating surfaces of the profile 02-160 and the bonding strap 02-050. See TASK
52-81-14-100-802-A01 for cleaning of the bonding points.
(k) Install the profile 02-160 with the bolt 02-150, the washer 02-030 and the nut 02-020.
Tighten the nut 02-020.
(l) Safety the nut 02-020 with the new cotter pin 02-010.
(m) Apply the Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable - on the
bolt 02-150, the washer 02-030 and the nut 02-020 and the new cotter pin 02-010.
1 The layer of Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable -
must cover a minimum area around the mating surfaces of 10 mm (0.39 in).
(n) Apply a layer of Material No. 04TMB2 Varnish-- Electrical Bonding Structure on the
Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable -.
(o) Make sure that the layer of Material No. 04TMB2 Varnish-- Electrical Bonding
Structure covers an area around the Material No. 06ABA1 Polysulfide Sealant-Fuel
Tank Brushable - between 3 and 5 mm (0.12 and 0.20 in).
(p) Install the bonding strap 02-050 with the screw 02-040, the washer 02-030 and the
nut 02-020.
(q) Safety the nut 02-020 with the new cotter pin 02-010.
(r) Apply the Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable - on the
screw 02-040, the washer 02-030 and the nut 02-020 and the new cotter pin 02-010.
1 The layer of Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable -
must cover a minimum area around the mating surfaces of 10 mm (0.39 in).
(s) Apply a layer of Material No. 04TMB2 Varnish-- Electrical Bonding Structure on the
Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable -.

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(t) Make sure that the layer of Material No. 04TMB2 Varnish-- Electrical Bonding
Structure covers an area around the Material No. 06ABA1 Polysulfide Sealant-Fuel
Tank Brushable - between 3 and 5 mm (0.12 and 0.20 in).
SCREWS AND BOLTS FWD FITTING ASSY HOLES
LOC NO. IPL ITEM NO. DIAMETERS DIMENSIONS DIAMETERS DIMENSIONS
MIN MAX MIN MAX
A 02-170 6.32 mm 6.34 mm 6.5 mm (0.256 6.5 mm (0.256
(0.2490 in) (0.2495 in) in) in)
B 02-190 6.31 mm 6.34 mm 6.6 mm (0.260 6.6 mm (0.260
(0.2484 in) (0.2495 in) in) in)
Screws, Bolts and Holes Diameters Dimensions
TABLE 4

(2) Assembly of the hinge assy.

NOTE : This procedure is applicable to the hinge assy 02-340.

(a) Make sure that the 98D52109001000 FWD fitting assy Replacement Tool is installed
and calibrated on the door.
(b) Make sure that the diameters of the holes in the hinge assy 02-340 are in the limits,
see TABLE 5 and FIGURE 52-81-14-991-018-A. For replacement for a new hinge assy
02-340, please contact AIRBUS.
(c) Make sure that the diameters of the bolts 02-270, 02-300 02-330 and are in the
limits. See TABLE 5 and FIGURE 52-81-14-991-018-A.
(d) Clean the matting surfaces of the hinge assy 02-340 and the FWD fitting assy 02-200.
See TASK 52-81-14-100-801-A01 and TASK 52-81-14-100-802-A01.
(e) Apply the Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surfaces between the hinge assy 02-340 and the FWD fitting assy 02-200.
(f) Install the hinge assy 02-340 in the correct position on the FWD fitting assy 02-200.
(g) Install the bolt 02-270, the washer 02-260 and the nut 02-250. Tighten the nut
02-250.
(h) Install the bolts 02-300, the washers 02-290 and the nuts 02-280. Tighten the nuts
02-280.
(i) Install the bolts 02-330, the washers 02-320, and the nuts 02-310. Tighten the nuts
02-310.
(j) Safety the nuts 02-250, 02-280, 02-310, with the new cotter pins 02-240.
(k) Remove the excess of Material No. 06AAC1 Polysulfide Sealant-General Purpose
Interfay - with a Material No. 14SBA1 Textile-Lint free Cotton -.

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(l) Apply the Material No. 04TMB2 Varnish-- Electrical Bonding Structure on the edges
between the hinge assy 02-340 and the FWD fitting assy 02-200.
FWD FITTING ASSY AND
BOLTS DIAMETERS
HINGE ASSY HOLES
LOC NO. IPL ITEM NO. DIMENSIONS
DIAMETERS DIMENSIONS
MIN MAX MIN MAX
A 02-270 6.32 m (0.2490 6.34 m (0.2495 6.31 mm 6.35 mm
in) in) (0.2484 in) (0.2500 in)
B 02-330 9.50 mm 9.51 mm 9.49 mm 9.53 mm
(0.3740 in) (0.3745 in) (0.3736 in) (0.3752 in)
C 02-300 7.91 mm 7.93 mm 7.90 mm 7.94 mm
(0.3115 in) (0.3120 in) (0.3110 in) (0.3126 in)
Bolts and Holes Diameters Dimensions
TABLE 5

(m) Disassemble the 98D52109001000 FWD fitting assy Replacement Tool from the door.
POST SB 52-1022
(1) Assembly of the FWD fitting assy.

NOTE : See IPL_FIGURE_02A.

NOTE : This procedure is applicable to the FWD fitting assy 02A-480.

(a) Make sure that the diameters of the holes in the FWD fitting assy 02A-480 are in the
limits, see TABLE 6 and FIGURE 52-81-14-991-021-A. For replacement for a new
FWD fitting assy 02A-480, please contact AIRBUS.
(b) Make sure that the diameters of the screws 02A-190 and the bolts 02A-170, 02A-720,
02A-730, 02A-740, 02A-750 are in the limits. See TABLE 6 and FIGURE
52-81-14-991-021-A.
(c) Clean the matting surfaces of the FWD fitting assy 02A-480 and the cover assembly.
See TASK 52-81-14-100-801-A01 and TASK 52-81-14-100-802-A01.
(d) Apply the Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surface of the FWD fitting assy 02A-480 and the cover assembly.
(e) Make sure that the bolts 02A-170 are engaged a minimum of 6 mm (0.23 in) in the
inserts 02A-180.
(f) Install the FWD fitting assy 02A-480 on the cover assembly in the correct position.
(g) Install the screws 02A-190 , the bolts 02A-170, 02A-720, 02A-730, 02A-740, 02A-750,
the washers 02A-030 and the nuts 02A-020, 02A-710. Tighten the bolts 02A-170 and
the nuts 02A-020, 02A-710.

Page 7033
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(h) Safety the nuts 02A-020 with the new cotter pins 02A-010.
(i) Safety the bolts 02A-170 with Material No. 14QJB1 Wire-Locking Dia: 1.6 mm CRES
Nickel Alloy -.
(j) Clean the mating surfaces of the profile 02A-160 and the FWD fitting assy 02A-480
and the mating surfaces of the profile 02A-160 and the bonding strap 02A-050. See
TASK 52-81-14-100-802-A01 for cleaning of the bonding points.
(k) Install the profile 02A-160 with the bolt 02A-150, the washer 02A-030 and the nut
02A-020. Tighten the nut 02A-020.
(l) Safety the nut 02A-020 with the new cotter pin 02A-010.
(m) Apply the Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable - on the
bolt 02A-150, the washer 02A-030, the nut 02A-020 and the new cotter pin 02A-010.
1 The layer of Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable -
must cover a minimum area around the mating surfaces of 10 mm (0.39 in).
(n) Apply a layer of Material No. 04TMB2 Varnish-- Electrical Bonding Structure on the
Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable -.
(o) Make sure that the layer of Material No. 04TMB2 Varnish-- Electrical Bonding
Structure covers an area around the Material No. 06ABA1 Polysulfide Sealant-Fuel
Tank Brushable - between 3 and 5 mm (0.12 and 0.20 in).
(p) Install the bonding strap 02A-050 with the screw 02A-040, the washer 02A-030 and
the nut 02A-020.
(q) Safety the nut 02A-020 with the new cotter pin 02A-010.
(r) Apply the Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable - on the
screw 02A-040 , the washer 02A-030 and the nut 02A-020 and the new cotter pin
02A-010.
1 The layer of Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable -
must cover a minimum area around the mating surfaces of 10 mm (0.39 in).
(s) Apply a layer of Material No. 04TMB2 Varnish-- Electrical Bonding Structure on the
Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable -.
(t) Make sure that the layer of Material No. 04TMB2 Varnish-- Electrical Bonding
Structure covers an area around the Material No. 06ABA1 Polysulfide Sealant-Fuel
Tank Brushable - between 3 and 5 mm (0.12 and 0.20 in).
SCREWS AND BOLTS FWD FITTING ASSY HOLES
LOC NO. IPL ITEM NO. DIAMETERS DIMENSIONS DIAMETERS DIMENSIONS
MIN MAX MIN MAX
6.32 mm 6.34 mm 6.5 mm (0.256 6.5 mm (0.256
A 02A-170 (0.2490 in) (0.2495 in) in) in)

Page 7034
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SCREWS AND BOLTS FWD FITTING ASSY HOLES

LOC NO. IPL ITEM NO. DIAMETERS DIMENSIONS DIAMETERS DIMENSIONS
MIN MAX MIN MAX
02A-190,
02A-720, 6.31 mm 6.34 mm 6.6 mm (0.260 6.6 mm (0.260
B 02A-730, (0.2484 in) (0.2495 in) in) in)
02A-740,
02A-750
Screws, Bolts and Holes Diameters Dimensions
TABLE 6

(2) Assembly of the hinge assy.

NOTE : This procedure is applicable to the hinge assy 02A-610.

(a) Make sure that the 98D52109001000 FWD fitting assy Replacement Tool is installed
and calibrated on the door.
(b) Make sure that the diameters of the holes in the hinge assy 02A-610 are in the limits,
see TABLE 7 and FIGURE 52-81-14-991-018-A. For replacement for a new hinge assy
02A-610, please contact AIRBUS.
(c) Make sure that the diameters of the bolts 02A-540, 02A-570, 02A-600 are in the
limits. See TABLE 7 and FIGURE 52-81-14-991-018-A.
(d) Clean the matting surfaces of the hinge assy 02A-610 and the FWD fitting assy
02A-480. See TASK 52-81-14-100-801-A01 and TASK 52-81-14-100-802-A01.
(e) Apply the Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surfaces between the hinge assy 02A-610 and the FWD fitting assy 02A-480.
(f) Install the hinge assy 02A-610 in the correct position on the FWD fitting assy
02A-480.
(g) Install the bolt 02A-540, the washer 02A-530 and the nut 02A-520. Tighten the nut
02A-520.
(h) Install the bolts 02A-570, the washers 02A-560 and the nuts 02A-550. Tighten the
nuts 02A-550.
(i) Install the bolts 02A-600, the washers 02A-590, and the nuts 02A-580. Tighten the
nuts 02A-580.
(j) Safety the nuts 02A-520, 02A-550, 02A-580 with the new cotter pins 02A-510.
(k) Remove the excess of Material No. 06AAC1 Polysulfide Sealant-General Purpose
Interfay - with a Material No. 14SBA1 Textile-Lint free Cotton -.

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(l) Apply the Material No. 04TMB2 Varnish-- Electrical Bonding Structure on the edges
between the hinge assy 02A-610 and the FWD fitting assy 02A-480.
FWD FITTING ASSY AND
BOLTS DIAMETERS
HINGE ASSY HOLES
LOC NO. IPL ITEM NO. DIMENSIONS
DIAMETERS DIMENSIONS
MIN MAX MIN MAX
A 02A-540 6.32 m (0.2490 6.34 m (0.2495 6.31 mm 6.35 mm
in) in) (0.2484 in) (0.2500 in)
B 02A-600 9.50 mm 9.51 mm 9.49 mm 9.53 mm
(0.3740 in) (0.3745 in) (0.3736 in) (0.3752 in)
C 02A-570 7.91 mm 7.93 mm 7.90 mm 7.94 mm
(0.3115 in) (0.3120 in) (0.3110 in) (0.3126 in)
Bolts and Holes Diameters Dimensions
TABLE 7

(m) Disassemble the 98D52109001000 FWD fitting assy Replacement Tool from the door.
POST SB 52-1073
(1) Assembly of the FWD fitting assy.

NOTE : See IPL_FIGURE_02B.

NOTE : This procedure is applicable to the FWD fitting assy 02B-200.

(a) Make sure that the diameters of the holes in the FWD fitting assy 02B-200 are in the
limits, see TABLE 8 and FIGURE 52-81-14-991-022-A. For replacement for a new
FWD fitting assy 02B-200, please contact AIRBUS.
(b) Make sure that the diameters of the bolts 02B-170 and the pin-rivets 02B-725,
02B-735, 02B-755 are in the limits. See TABLE 8 and FIGURE 52-81-14-991-022-A.
(c) Clean the matting surfaces of the FWD fitting assy 02B-200 and the cover assembly.
See TASK 52-81-14-100-801-A01 and TASK 52-81-14-100-802-A01.
(d) Apply the Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surface of the FWD fitting assy 02B-200 and the cover assembly.
(e) Make sure that the bolts 02B-170 are engaged a minimum of 6 mm (0.23 in) in the
inserts 02B-180.
(f) Install the FWD fitting assy 02B-200 on the cover assembly in the correct position.
(g) Install the bolts 02B-170 , the screws 02B-190, the washers 02B-030 and the nuts
02B-020. Tighten the bolts 02B-170 and the nuts 02B-020.

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(h) Install the pin-rivets 02B-725, 02B-735, 02B-755 and the collars 02B-695. See SRM
51-42-21 for installation of the collars 02B-695 and the pin-rivets 02B-725, 02B-735,
02B-755.
(i) Safety the nuts 02B-020 with the new cotter pins 02B-010.
(j) Safety the bolts 02B-170 with Material No. 14QJB1 Wire-Locking Dia: 1.6 mm CRES
Nickel Alloy -.
SCREWS AND BOLTS FWD FITTING ASSY HOLES
LOC NO. IPL ITEM NO. DIAMETERS DIMENSIONS DIAMETERS DIMENSIONS
MIN MAX MIN MAX
6.32 mm 6.34 mm 6.5 mm (0.256 6.5 mm (0.256
A 02B-170 (0.2490 in) (0.2495 in) in) in)
02B-190,
02B-725, 6.31 mm 6.34 mm 6.6 mm (0.260 6.6 mm (0.260
B (0.2484 in) (0.2495 in)
02B-735, in) in)
02B-755
Screws, Bolts and Holes Diameters Dimensions
TABLE 8

(2) Assembly of the hinge assy.

NOTE : See IPL_FIGURE_02B.

NOTE : This procedure is applicable to the hinge assy 02B-340.

(a) Make sure that the 98D52109001000 FWD fitting assy Replacement Tool is installed
and calibrated on the door.
(b) Make sure that the diameters of the holes in the hinge assy 02B-340 are in the limits,
see TABLE 9 and FIGURE 52-81-14-991-019-A. For replacement for a new hinge assy
02B-340, please contact AIRBUS.
(c) Make sure that the diameters of the bolts 02B-270, 02B-300, are in the limits. See
TABLE 9 and FIGURE 52-81-14-991-019-A.
(d) Clean the matting surfaces of the hinge assy 02B-340 and the FWD fitting assy
02B-200. See TASK 52-81-14-100-801-A01 and TASK 52-81-14-100-802-A01.
(e) Apply the Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surfaces between the hinge assy 02B-340 and the FWD fitting assy 02B-200.
(f) Install the hinge assy 02B-340 in the correct position on the FWD fitting assy
02B-200.
(g) Clean the mating surfaces of the profile 02B-290 and the FWD fitting assy 02B-200
and the mating surfaces of the profile 02B-290 and the bonding strap 02B-050. See
TASK 52-81-14-100-802-A01 for cleaning of the bonding points.

Page 7037
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(h) Install the bolts 02B-300, the washers 02B-250 and the nuts 02B-260. Tighten the
nuts 02B-260.
(i) Safety the nuts 02B-260, with the new cotter pins 02B-240.
(j) Remove the excess of Material No. 06AAC1 Polysulfide Sealant-General Purpose
Interfay - with a Material No. 14SBA1 Textile-Lint free Cotton -.
(k) Apply the Material No. 04TMB2 Varnish-- Electrical Bonding Structure on the edges
between the hinge assy 02B-340 and the FWD fitting assy 02B-200.
(l) Install the profile 02B-290, with the bolt 02B-270, the washer 02B-250, the nut
02B-260 and the rivet 02B-280. See SRM 51-42-21 for installation of the rivet
02B-280.
(m) Tighten the nut 02B-260.
(n) Safety the nut 02B-260 with the new cotter pin 02B-240.
(o) Apply a layer of Material No. 04TMB2 Varnish-- Electrical Bonding Structure on the
Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable -.
1 The layer of Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable -
must cover a minimum area around the mating surfaces of 10 mm (0.39 in).
(p) Apply a layer of Material No. 04TMB2 Varnish-- Electrical Bonding Structure on the
Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable -.
(q) Make sure that the layer of Material No. 04TMB2 Varnish-- Electrical Bonding
Structure covers an area around the Material No. 06ABA1 Polysulfide Sealant-Fuel
Tank Brushable - between 3 and 5 mm (0.12 and 0.20 in).
(r) Install the bonding strap 02B-050 with the screw 02B-040 , the washer 02B-030 and
the nut 02B-020. Tighten the nut 02B-020.
(s) Safety the nuts 02B-020 with the new cotter pin 02B-010.

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(t) Apply the Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable - on the
screw 02B-040, the washer 02B-030 and the nut 02B-020 and the new cotter pin
02B-010.
1 The layer of Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable -
must cover a minimum area around the mating surfaces of 10 mm (0.39 in).
FWD FITTING ASSY AND
BOLTS DIAMETERS
HINGE ASSY HOLES
LOC NO. IPL ITEM NO. DIMENSIONS
DIAMETERS DIMENSIONS
MIN MAX MIN MAX
02B-270, 9.50 mm 9.54 mm 9.49 mm 9.53 mm
A (0.3740 in) (0.3756 in) (0.3736 in) (0.3752 in)
02B-300
Bolts and Holes Diameters Dimensions
TABLE 9

(u) Disassemble the 98D52109001000 FWD fitting assy Replacement Tool from the door.
ALL VARIANTS
(3) Not apply.

**For PN’s D5288000800098 D5288000800198 D5288000900098 D5288000900198 D5288001000098

D5288001000198

Subtask 52-81-14-400-022-B01
B. Assembly of the Forward Fitting Assy
(1) Assembly of the fitting.

NOTE : See IPL_FIGURE_02B.

NOTE : This procedure is applicable to the FWD fitting assy 02B-200.

(a) Make sure that the diameters of the holes in the FWD fitting assy 02B-200 are in the
limits, see TABLE 10 and FIGURE 52-81-14-991-022-A. For replacement for a new
FWD fitting assy 02B-200, please contact AIRBUS.
(b) Make sure that the diameters of the bolts 02B-170 and the pin-rivets 02B-725,
02B-735, 02B-755 are in the limits. See TABLE 10 and FIGURE 52-81-14-991-022-A.
(c) Clean the matting surfaces of the FWD fitting assy 02B-200 and the cover assembly.
See TASK 52-81-14-100-801-A01 and TASK 52-81-14-100-802-A01.
(d) Apply the Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surface of the FWD fitting assy 02B-200 and the cover assembly.
(e) Make sure that the bolts 02B-170 are engaged a minimum of 6 mm (0.23 in) in the
inserts 02B-180.

Page 7039
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(f) Install the FWD fitting assy 02B-200 on the cover assembly in the correct position.
(g) Install the bolts 02B-170 , the screws 02B-190, the washers 02B-030 and the nuts
02B-020. Tighten the bolts 02B-170 and the nuts 02B-020.
(h) Install the pin-rivets 02B-725, 02B-735, 02B-755 and the collars 02B-695. See SRM
51-42-21 for installation of the collars 02B-695 and the pin-rivets 02B-725, 02B-735,
02B-755.
(i) Safety the nuts 02B-020 with the new cotter pins 02B-010.
(j) Safety the bolts 02B-170 with Material No. 14QJB1 Wire-Locking Dia: 1.6 mm CRES
Nickel Alloy -.
SCREWS AND BOLTS FWD FITTING ASSY HOLES
LOC NO. IPL ITEM NO. DIAMETERS DIMENSIONS DIAMETERS DIMENSIONS
MIN MAX MIN MAX
6.32 mm 6.34 mm 6.5 mm (0.256 6.5 mm (0.256
A 02B-170 (0.2490 in) (0.2495 in) in) in)
02B-190,
02B-725, 6.31 mm 6.34 mm 6.6 mm (0.260 6.6 mm (0.260
B (0.2484 in) (0.2495 in)
02B-735, in) in)
02B-755
Screws, Bolts and Holes Diameters Dimensions
TABLE 10

(2) Assembly of the hinge assy.

NOTE : See IPL_FIGURE_02B.

NOTE : This procedure is applicable to the hinge assy 02B-340.

(a) Make sure that the 98D52109001000 FWD fitting assy Replacement Tool is installed
and calibrated on the door.
(b) Make sure that the diameters of the holes in the hinge assy 02B-340 are in the limits,
see TABLE 11 and FIGURE 52-81-14-991-019-A. For replacement for a new hinge
assy 02B-340, please contact AIRBUS.
(c) Make sure that the diameters of the bolts 02B-270, 02B-300, are in the limits. See
TABLE 11 and FIGURE 52-81-14-991-019-A.
(d) Clean the matting surfaces of the hinge assy 02B-340 and the FWD fitting assy
02B-200. See TASK 52-81-14-100-801-A01 and TASK 52-81-14-100-802-A01.
(e) Apply the Material No. 06AAC1 Polysulfide Sealant-General Purpose Interfay - to the
mating surfaces between the hinge assy 02B-340 and the FWD fitting assy 02B-200.
(f) Install the hinge assy 02B-340 in the correct position on the FWD fitting assy
02B-200.

Page 7040
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COMPONENT MAINTENANCE MANUAL
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(g) Clean the mating surfaces of the profile 02B-290 and the FWD fitting assy 02B-200
and the mating surfaces of the profile 02B-290 and the bonding strap 02B-050. See
TASK 52-81-14-100-802-A01 for cleaning of the bonding points.
(h) Install the bolts 02B-300, the washers 02B-250 and the nuts 02B-260. Tighten the
nuts 02B-260.
(i) Safety the nuts 02B-260 with the new cotter pins 02B-240.
(j) Remove the excess of Material No. 06AAC1 Polysulfide Sealant-General Purpose
Interfay - with a Material No. 14SBA1 Textile-Lint free Cotton -.
(k) Apply the Material No. 04TMB2 Varnish-- Electrical Bonding Structure on the edges
between the hinge assy 02B-340 and the FWD fitting assy 02B-200.
(l) Install the profile 02B-290, with the bolt 02B-270, the washer 02B-250, the nut
02B-260 and the rivet 02B-280. See SRM 51-42-21 for installation of the rivet
02B-280.
(m) Tighten the nut 02B-260.
(n) Safety the nut 02B-260 with the new cotter pin 02B-240.
(o) Apply a layer of Material No. 04TMB2 Varnish-- Electrical Bonding Structure on the
Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable -.
1 The layer of Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable -
must cover a minimum area around the mating surfaces of 10 mm (0.39 in).
(p) Apply a layer of Material No. 04TMB2 Varnish-- Electrical Bonding Structure on the
Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable -.
(q) Make sure that the layer of Material No. 04TMB2 Varnish-- Electrical Bonding
Structure covers an area around the Material No. 06ABA1 Polysulfide Sealant-Fuel
Tank Brushable - between 3 and 5 mm (0.12 and 0.20 in).
(r) Install the bonding strap 02B-050 with the screw 02B-040 , the washer 02B-030 and
the nut 02B-020. Tighten the nut 02B-020.
(s) Safety the nuts 02B-020 with the new cotter pin 02B-010.

Page 7041
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(t) Apply the Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable - on the
screw 02B-040, the washer 02B-030 and the nut 02B-020 and the new cotter pin
02B-010.
1 The layer of Material No. 06ABA1 Polysulfide Sealant-Fuel Tank Brushable -
must cover a minimum area around the mating surfaces of 10 mm (0.39 in).
FWD FITTING ASSY AND
BOLTS DIAMETERS
HINGE ASSY HOLES
LOC NO. IPL ITEM NO. DIMENSIONS
DIAMETERS DIMENSIONS
MIN MAX MIN MAX
02B-270, 9.50 mm 9.54 mm 9.49 mm 9.53 mm
A (0.3740 in) (0.3756 in) (0.3736 in) (0.3752 in)
02B-300
Bolts and Holes Diameters Dimensions
TABLE 11

(u) Disassemble the 98D52109001000 FWD fitting assy Replacement Tool from the door.

Page 7042
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COMPONENT MAINTENANCE MANUAL
D5288000800000

**For PN’s D5288000800094 D5288000800098 D5288000800194 D5288000800198 D5288000900094

D5288000900098 D5288000900194 D5288000900198 D5288001000094 D5288001000098 D5288001000194
D5288001000198

A
HINGE ASSY

L_CM_528114_1_0180101_01_00

Bolts and Holes in the Hinge Assy

FIGURE-52-81-14-991-018-A01

Page 7043
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COMPONENT MAINTENANCE MANUAL
D5288000800000

**For PN’s D5288000800094 D5288000800098 D5288000800194 D5288000800198 D5288000900094

D5288000900098 D5288000900194 D5288000900198 D5288001000094 D5288001000098 D5288001000194
D5288001000198

HINGE ASSY

L_CM_528114_1_0190101_01_00

Bolts and Holes in the Hinge Assy

FIGURE-52-81-14-991-019-A01

Page 7044
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COMPONENT MAINTENANCE MANUAL
D5288000800000

**For PN’s D5288000800094 D5288000800098 D5288000800194 D5288000800198 D5288000900094

D5288000900098 D5288000900194 D5288000900198 D5288001000094 D5288001000098 D5288001000194
D5288001000198

A
B

FITTING

L_CM_528114_1_0200101_01_00

Bolts and Holes in the FWD Fitting Assy

FIGURE-52-81-14-991-020-A01

Page 7045
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COMPONENT MAINTENANCE MANUAL
D5288000800000

**For PN’s D5288000800094 D5288000800098 D5288000800194 D5288000800198 D5288000900094

D5288000900098 D5288000900194 D5288000900198 D5288001000094 D5288001000098 D5288001000194
D5288001000198
B

B FITTING

A
L_CM_528114_1_0210101_01_00

Bolts and Holes in the FWD Fitting Assy

FIGURE-52-81-14-991-021-A01

Page 7046
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COMPONENT MAINTENANCE MANUAL
D5288000800000

**For PN’s D5288000800094 D5288000800098 D5288000800194 D5288000800198 D5288000900094

D5288000900098 D5288000900194 D5288000900198 D5288001000094 D5288001000098 D5288001000194
D5288001000198

FITTING

A
L_CM_528114_1_0220101_01_00

Bolts and Holes in the FWD Fitting Assy

FIGURE-52-81-14-991-022-A01

Page 7047
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COMPONENT MAINTENANCE MANUAL
D5288000800000

**For PN’s ALL

TASK 52-81-14-400-809-A01
Assembly of the Identification Plates
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
14SBA1 Textile-Lint free Cotton -
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
05JBB9 Contact Adhesive-Rubber & Plastic Bonding Nitrile base -
04SBA3 Varnish Polyurethane-Low VOC - External Structure
08ABC1 Aqueous Cleaner-Aircraft Exterior Pressure Spraying -
Consumable Materials
TABLE 1

B. Fixtures, Tools, Test and Support Equipment

REFERENCE DESIGNATION
non-metallic scraper
Fixtures, Tools, Test and Support Equipment
TABLE 2

C. Referenced Information
REFERENCE DESIGNATION
SRM 51-42-21
Referenced Information
TABLE 3

3. Procedure

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

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

Page 7048
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COMPONENT MAINTENANCE MANUAL
D5288000800000

CAUTION : USE ONLY SPECIFIED CLEANING MATERIALS AND SOLUTIONS OR THEIR

EQUIVALENTS. THE SURFACE PROTECTION COULD BE DAMAGED IF
UNSPECIFIED MATERIALS ARE USED. IT IS IMPORTANT THAT THE
MANUFACTURER’S MIXING, APPLICATION AND TREATMENT INSTRUCTIONS
ARE FOLLOWED.

**For PN’s D5288000800000 D5288000800100 D5288000900000 D5288000900100 D5288001000000

D5288001000100

Subtask 52-81-14-400-012-A01
A. Assembly of the Identification Plates

NOTE : See IPL_FIGURE_01, IPL_FIGURE_01A, and IPL_FIGURE_01B.

NOTE : This procedure is applicable to the identification plates 01-190, 01A-210 and 01B-190.
(1) Removal of the bonded identification plates.
(a) Make a copy of the data from the old identification plate 01-190.
(b) Put the data on the new identification plate 01-190.
(c) Remove the old identification plate 01-190 with a non-metallic scraper.
(2) Installation of the bonded identification plates.
(a) Clean the work area with Material No. 14SBA1 Textile-Lint free Cotton - soaked with
Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(b) Apply a layer of Material No. 05JBB9 Contact Adhesive-Rubber & Plastic Bonding
Nitrile base - on the reverse side of the new identification plate 01-190.
(c) Install the new identification plate 01-190 in the correct position.
(d) Remove the remaining adhesive, around the identification plate 01-190, with Material
No. 14SBA1 Textile-Lint free Cotton - soaked with Material No. 08BBF1 Non
Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(e) Let the Material No. 05JBB9 Contact Adhesive-Rubber & Plastic Bonding Nitrile base
- cure.
(f) Apply a layer of Material No. 04SBA3 Varnish Polyurethane-Low VOC - External
Structure on the new identification plate.
(g) Let the Material No. 04SBA3 Varnish Polyurethane-Low VOC - External Structure
cure.

**For PN’s D5288000800094 D5288000800095 D5288000800098 D5288000800194 D5288000800195

D5288000800198 D5288000900094 D5288000900095 D5288000900098 D5288000900194
D5288000900195 D5288000900198 D5288001000094 D5288001000095 D5288001000098

Page 7049
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COMPONENT MAINTENANCE MANUAL
D5288000800000

D5288001000194 D5288001000195 D5288001000198

Subtask 52-81-14-400-012-B01
B. Assembly of the Identification Plates

NOTE : See IPL_FIGURE_01, IPL_FIGURE_01A, IPL_FIGURE_01B, IPL_FIGURE_01C,

IPL_FIGURE_01D , IPL_FIGURE_01E and IPL_FIGURE_01F.

NOTE : This procedure is applicable to the identification plates 01-190, 01A-210, 01B-190,
01C-190, 01C-230, 01D-190, 01D-210, 01E-190, 01E-230 and 01F-190.
(1) Removal of the riveted identification plates.
(a) Make a copy of the data from the old identification plate 01-190.
(b) Put the data on the new identification plate 01-190.
(c) Remove the rivets 01-200 from the identification plate 01-190. See SRM 51-42-21 for
the removal of the rivets 01-200.
(d) Remove the identification plate 01-190 with a non-metallic scraper.
(2) Installation of the riveted identification plates.
(a) Clean the work area with a Material No. 14SBA1 Textile-Lint free Cotton - soaked
with Material No. 08ABC1 Aqueous Cleaner-Aircraft Exterior Pressure Spraying -.
(b) Put the new identification plate 01-190 in the correct position.
(c) Install the new rivets 01-200 on the identification plate 01-190. See SRM 51-42-21 for
the installation of the new rivets 01-200.

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COMPONENT MAINTENANCE MANUAL
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**For PN’s ALL

TASK 52-81-14-400-810-A01
Assembly of the Bushes
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
05ABM1 Retaining adhesive-Cylindrical fitting High strength High viscosity -
05XAB1 Adhesive Activator-- Anaerobic -
Consumable Materials
TABLE 1

B. Fixtures, Tools, Test and Support Equipment

REFERENCE DESIGNATION
suitable tool
Fixtures, Tools, Test and Support Equipment
TABLE 2

C.Referenced Information
REFERENCE DESIGNATION
FIGURE 52-81-14-991-023-A FIGURE 52-81-14-991-023-A-Bushes Installation
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 SPECIFIED CLEANING MATERIALS AND SOLUTIONS OR THEIR

EQUIVALENTS. THE SURFACE PROTECTION COULD BE DAMAGED IF
UNSPECIFIED MATERIALS ARE USED. IT IS IMPORTANT THAT THE
MANUFACTURER’S MIXING, APPLICATION AND TREATMENT INSTRUCTIONS
ARE FOLLOWED.

Page 7051
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D5288000800000

CAUTION : DO NOT STRESS THE HINGE OR THE FITTING WHEN INSTALLING THE
BUSHES. STRESS WILL DAMAGE THE HINGE OR THE FITTING.

Subtask 52-81-14-400-019-A01
A. Assembly of the Bushes
(1) Installation of the bushes of the FWD fitting assy.

NOTE : See IPL_FIGURE_02, IPL_FIGURE_02A, IPL_FIGURE_02B and FIGURE

52-81-14-991-023-A.

NOTE : This procedure is applicable to the bushes 02-220, 02-230, 02A-495, 02A-500,
02B-220 and 02B-230.
(a) Clean the mating surfaces of the bushes 02-220 and 02-230, and the FWD fitting assy
02-200 with the Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(b) Make sure that the internal diameter of the FWD fitting assy 02-200 is in correct
condition.
(c) Apply Material No. 05ABM1 Retaining adhesive-Cylindrical fitting High strength High
viscosity - to the bushes 02-220 and 02-230.

CAUTION : DO NOT STRESS THE HINGE OR THE FITTING WHEN INSTALLING

THE BUSHES. STRESS WILL DAMAGE THE HINGE OR THE FITTING.
(d) Press in the bushes 02-220 and 02-230 into the FWD fitting assy 02-200, with a
suitable tool .
(e) Make sure that the bushes 02-220 and 02-230 are flushed with the external surfaces
of the FWD fitting assy 02-200.
(f) Make sure that the dimensions of the assembly of the bushes 02-220 and 02-230, are
correct. See FIGURE 52-81-14-991-023-A.
(2) Installation of the bushes of the rear fitting.

NOTE : See IPL_FIGURE_07.

NOTE : This procedure is applicable to the bush 07-260 .

(a) Clean the mating surfaces of the bush 07-260 and the hinge 07-250 with the Material
No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(b) Make sure that the internal diameter of the hinge 07-250 is in correct condition.

CAUTION : MAKE SURE THAT THE INTERNAL DIAMETER OF THE HINGE DOES
NOT EXCEED 44.964 MM (1.7702 IN), OTHERWISE THE HINGE MUST
BE REPLACED.
(c) If the internal diameter of the hinge 07-250 has corrosion, wear or distortion, ream
the internal diameter to the next oversize diameter.

Page 7052
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(d) For oversize bushes and internal diameter of the hinge 07-250. See TABLE 4.
(e) To make the bond better, make the surface rough, using an abrasive cloth grade 220.
(f) Clean the grease on the internal diameter of the hinge 07-250 and the bush 07-260
with the Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.

CAUTION : DO NOT TOUCH THE SURFACES AFTER THE GREASE IS REMOVED,

BECAUSE THIS WILL DAMAGE THE BOND.
(g) Apply an uniform, thin coat of Material No. 05XAB1 Adhesive Activator-- Anaerobic -
to the surfaces to be bonded.
(h) After the pretreatment apply Material No. 05ABM1 Retaining adhesive-Cylindrical
fitting High strength High viscosity - evenly to the new bush and the internal diameter
of the hinge 07-250.

CAUTION : DO NOT STRESS THE HINGE OR THE FITTING WHEN INSTALLING

THE BUSHES. STRESS WILL DAMAGE THE HINGE OR THE FITTING.
(i) Push the bush 07-260 into the internal diameter of the hinge 07-250 with a suitable
tool and check for correct seating. Remove the remaining bonding compound Material
No. 05ABM1 Retaining adhesive-Cylindrical fitting High strength High viscosity -.
(j) Let the bonded component parts cure at room temperature for a minimum of 30
minutes or at 40 ˚C (104.00 ˚F) for a minimum of 10 minutes.
ITEM OVERSIZE BUSH REAMING OF THE INTERNAL
millimeters (inches) DIAMETER
millimeters (inches)
07-261 42.68 to 42.69 42.73 to 42.76
(1.6803 to 1.6807) (1.6823 to 1.6835)
07-262 42.88 to 42.89 42.93 to 42.96
(1.6882 to 1.6886) (1.6902 to 1.6913)
07-263 43.08 to 43.09 43.13 to 43.16
(1.6961 to 1.6964) (1.6980 to 1.6992)
07-264 43.28 to 43.29 43.33 to 43.36
(1.7037 to 1.7043) (1.7059 to 1.7071)
07-265 43.48 to 43.49 43.53 to 43.56
(1.7118 to 1.7122) (1.7138 to 1.7150)
07-266 43.88 to 43.89 43.93 to 43.96
(1.7276 to 1.7280) (1.7295 to 1.7307)
07-267 44.48 to 44.49 44.53 to 44.56
(1.7512 to 1.7516) (1.7531 to 1.7543)

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07-268 44.88 to 44.89 44.93 to 44.96

(1.7669 to 1.7673) (1.7689 to 1.7701)
Oversize of Bush and Internal Diameter of the Fitting
TABLE 4

(3) Installation of the bushes of the uplock assy.

NOTE : See IPL_FIGURE_03, IPL_FIGURE_03B and IPL_FIGURE_03C.

(a) Installation of the bushes of the base-mounting.

NOTE : This procedure is applicable to the bushes 03-230, 03-280, 03B-230,

03B-280, 03C-230 and 03C-280.
1 Clean the mating surfaces of the bushes 03-230, 03-280 and the base-mounting
03-340 with the Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-
Ketone -.
2 Make sure that the internal diameter of the base-mounting 03-340 is in correct
condition.
3 Apply Material No. 05ABM1 Retaining adhesive-Cylindrical fitting High strength
High viscosity - to the bushes 03-230, 03-280.

CAUTION : DO NOT STRESS THE HINGE OR THE FITTING WHEN

INSTALLING THE BUSHES. STRESS WILL DAMAGE THE HINGE
OR THE FITTING.
4 Press in the bushes 03-230, 03-280 in the base-mounting 03-340 with a suitable
tool.
5 Make sure that the bushes 03-230, 03-280 are correctly installed in the base-
mounting 03-340.
(b) Installation of the bushes of the roller.

NOTE : This procedure is applicable to the bushes 03-110, 03B-110 and 03C-110.
1 Clean the mating surfaces of the bushes 03-110 and the roller 03-100 with the
Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
2 Press in the bushes 03-110 into the roller 03-100.

**For PN’s D5288000800098 D5288000800198 D5288000900098 D5288000900198 D5288001000098

Page 7054
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COMPONENT MAINTENANCE MANUAL
D5288000800000

D5288001000198

Subtask 52-81-14-400-020-A01
B. Assembly of the Bushes of the Lateral Ramp
PRE SB 52-1025
(1) Not apply.
POST SB 52-1025
(1) Installation of the bushes.

NOTE : See IPL_FIGURE_04D.

NOTE : This procedure is applicable to the bushes 04D-203.

(a) Clean the mating surfaces of the bushes 04D-203 and the glider 04D-202 with the
Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(b) Make sure that the internal diameter of the glider 04D-202 is in correct condition.
(c) Apply Material No. 05ABM1 Retaining adhesive-Cylindrical fitting High strength High
viscosity - to the bushes 04D-203.

CAUTION : DO NOT STRESS THE HINGE OR THE FITTING WHEN INSTALLING

THE BUSHES. STRESS WILL DAMAGE THE HINGE OR THE FITTING.
(d) Press in the bushes 04D-203 into the glider 04D-202, with a suitable tool.
(e) Make sure that the bushes are flushed with the external surfaces of the glider
04D-202.
ALL VARIANTS
(2) Not apply.

**For PN’s D5288000800094 D5288000800095 D5288000800194 D5288000800195 D5288000900094

D5288000900095 D5288000900194 D5288000900195 D5288001000094 D5288001000095
D5288001000194 D5288001000195

Subtask 52-81-14-400-020-B01
C. Assembly of the Bushes of the Lateral Ramp
(1) Installation of the bushes.

NOTE : See IPL_FIGURE_04D.

NOTE : This procedure is applicable to the bushes 04D-203.

(a) Clean the mating surfaces of the bushes 04D-203 and the glider 04D-202 with the
Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.

Page 7055
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D5288000800000

(b) Make sure that the internal diameter of the glider 04D-202 is in correct condition.
(c) Apply Material No. 05ABM1 Retaining adhesive-Cylindrical fitting High strength High
viscosity - to the bushes 04D-203.

CAUTION : DO NOT STRESS THE HINGE OR THE FITTING WHEN INSTALLING

THE BUSHES. STRESS WILL DAMAGE THE HINGE OR THE FITTING.
(d) Press in the bushes 04D-203 into the glider 04D-202, with a suitable tool.
(e) Make sure that the bushes are flushed with the external surfaces of the glider
04D-202.

**For PN’s D5288000800000 D5288000800100 D5288000900000 D5288000900100 D5288001000000

D5288001000100

Subtask 52-81-14-400-020-C01
D. Assembly of the Bushes of the Lateral Ramp
(1) Not apply.

Page 7056
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COMPONENT MAINTENANCE MANUAL
D5288000800000

**For PN’s ALL

20.20 mm (0.795 in)

19.80 mm (0.780 in)

18.20 mm (0.717 in)

17.80 mm (0.701 in)

BUSH
BUSH

FITTING

A A

L_CM_528114_1_0230101_01_00

Bushes Installation
Dimension of the Bushes Installation
FIGURE-52-81-14-991-023-A01

Page 7057
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COMPONENT MAINTENANCE MANUAL
D5288000800000

**For PN’s ALL

TASK 52-81-14-400-811-A01
Assembly of the Bearings
1. Reason for the Job
This procedure is self-explanatory.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -
06LCG9 Non Hardening Jointing Putty-Medium Temp. Area - -
Consumable Materials
TABLE 1

B. Fixtures, Tools, Test and Support Equipment

REFERENCE DESIGNATION
98D52109001000 Fitting Replacement Tool
Fixtures, Tools, Test and Support Equipment
TABLE 2

C. Referenced Information
REFERENCE DESIGNATION
TASK 52-81-14-000-801-A01 Disassembly of the FWD Fitting Assy
TASK 52-81-14-000-801-B01 Disassembly of the FWD Fitting Assy
TASK 52-81-14-400-808-A01 Assembly of the FWD Fitting Assy
PMS 01-05-26
Referenced Information
TABLE 3

3. Procedure

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

MATERIAL MANUFACTURER’S INSTRUCTIONS AND YOUR LOCAL
REGULATIONS.

Page 7058
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COMPONENT MAINTENANCE MANUAL
D5288000800000

CAUTION : USE ONLY SPECIFIED CLEANING MATERIALS AND SOLUTIONS OR THEIR

EQUIVALENTS. THE SURFACE PROTECTION COULD BE DAMAGED IF
UNSPECIFIED MATERIALS ARE USED. IT IS IMPORTANT THAT THE
MANUFACTURER’S MIXING, APPLICATION AND TREATMENT INSTRUCTIONS
ARE FOLLOWED.

Subtask 52-81-14-400-021-A01
A. Assembly of the Bearings

NOTE : See IPL_FIGURE_02, IPL_FIGURE_02A and IPL_FIGURE_02B.

NOTE : This procedure is applicable to the spherical bearing 02-360, 02A-630 and 02B-360.
(1) Assembly of the spherical bearing with the hinge assy.
(a) Make sure that the 98D52109001000 Fitting Replacement Tool is installed and
calibrated on the door.
(b) Make sure that the hinge assy 02-340 is in correct conditions. See TASK
52-81-14-000-801-A01TASK 52-81-14-000-801-B01, and TBD.
(c) Clean the mating surfaces of the spherical bearing02-360 and the hinge assy 02-340
with Material No. 08BBF1 Non Aqueous Cleaner-- Methyl-Ethyl-Ketone -.
(d) Apply Material No. 06LCG9 Non Hardening Jointing Putty-Medium Temp. Area - - to
the mating surface of the spherical bearing 02-360 and the hinge assy 02-340.
(e) Press the spherical bearing 02-360 into the hinge assy 02-340. See PMS 01-05-26 for
the installation of the spherical bearing 02-360.
(f) Make sure that the spherical bearing 02-360 is flush with the external surfaces of the
hinge assy 02-340.
(g) Do a check of the installation of the spherical bearing 02-360. See PMS 01-05-26.
(h) Assemble the hinge assy 02-340 on the forward fitting assy 02-200. See TASK
52-81-14-400-808-A01.
(i) Disassemble the 98D52109001000 Fitting Replacement Tool from the door.

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FITS AND CLEARANCES

**For PN’s ALL

TASK 52-81-14-820-806-A01
Fits and Clearances
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

2. Fits and clearances.

NOTE : See IPL_FIGURE_02, IPL_FIGURE_02A, IPL_FIGURE_02B, IPL_FIGURE_07 and FIGURE

52-81-14-991-006-A.

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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
02-360, 30.15 30.16
A2 OD 02A-630, (1.1870) (1.1874)
02B-360 0.00 0.01 NO WEAR
02-340, 30.16 (0.0000) (0.0004) ALLOWED
30.16
A1 ID 02A-610, (1.1874) (1.1874)
02B-340
02-360, 15.86 15.88
A2 ID 02A-630, (0.6244) (0.6252)
02B-360
02-230, 21.96 21.98
---
B2 OD (0.8646) (0.8654)
02A-50002B-230 0.02 0.06 NO WEAR
02-200, 22.00 22.02 (0.0008) (0.0024) ALLOWED
B1 ID 02A-480, (0.8661) ---
(0.8669)
02B-200
02-230, 15.88 15.89
B2 ID (0.6252) (0.6256)
02A-50002B-230
02-220, 22.04 22.06
B3 OD 02A-495, (0.8677) (0.8685)
02B-220 -0.06 -0.02 NO WEAR
02-200, 22.00 (-0.0024) (-0.0008) ALLOWED
22.02
B1 ID 02A-480, (0.8661) (0.8669)
02B-200
02-220, 19.00 19.02
B3 ID (0.7480) (0.7488)
02A-495,02B-220
42.48 42.49
OD 07-260 (1.6724)
C2FOOTNOTE ---
(1.6728) 0.04 0.08 NO WEAR
42.53 42.56 (0.0016) (0.0031) ALLOWED
ID 07-250 (1.6744)
C1FOOTNOTE ---
(1.6756)
32.00 32.03
C2 ID 07-260 (1.2598) (1.2610)

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For oversize bushes see TASK 52-81-14-000-811-A01 and .

Fits and Clearances Table
TABLE 2

NOTE : See IPL_FIGURE_03, IPL_FIGURE_03B, IPL_FIGURE_03C and FIGURE

52-81-14-991-007-A.
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
03-090, 11.50 11.86 11.09
A1 OD 03B-090,(0. 4528) (0.4670) (0.4366)
03C-090 0.14 0.68 1.50
03-110, 12.00 12.18 (0. 0055) (0.0268) (0.0591)
12.59
A2 ID 03B-110,(0. 4724) (0.
(0.4957)
03C-110 4795)
03-110, 16.20 16.30
A2 OD 03B-110,(0.6378) (0.6417) ---
03C-110 -0.50 -0.30 NO WEAR
03-100, 15.80 (-0.0197) (-0.0118) ALLOWED
15.90
A3 ID 03B-100,(0.6220) (0.6260) ---
03C-100
03-090, 11.50 11.86
11.09
A1 OD 03B-090,(0.4528) (0.
(0. 4366)
03C-090 4669) 0.14 0.68 1.50
03-110, 12.00 (0.0055) (0.0268) (0.0591)
12.18 12.59
A4 ID 03B-110,(0.4724) (0.4795) (0. 4957)
03C-110
03-090, 13.66 13.84 13.32
A4 OD 03B-090,(0.5378) (0.5449) (0. 5244)
03C-090 0.16 0.52 1.20
03-280, 14.00 (0. 0063) (0.0205) (0.0472)
14.18 14.52
A7 ID 03B-280,(0. 5512) (0.5583) (0. 5717)
03C-280

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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
03-090, 11.50 11.86 11.09
A1 OD 03B-090,(0. 4528) (0.4670) (0. 4366)
03C-090 0.14 0.68 1.50
12.18 (0.0055) (0.0268) (0.0591)
12.00
03-27003B-270, 12.59
A5 ID (0.
03C-270 (0.4724) 4795) (0.4957)

13.66
03-27003B-270, 13.84 13.32
A5 OD
03C-270 (0.5378) (0.4670) 0.16 0.52
(0.5244)
1.20
03-280, 14.00 14.18 (0.0063) (0.0205) 14.52 (0.0472)
A6 ID 03B-280,(0.5512) (0.5583) (0.5717)
03C-280
03-230, 17.89 18.00 17.83
A7 OD 03B-230,(0.7043) (0.7087) (0.7020)
03C-230 0.00 0.12 0.24
03-340, 18.00 18.01 (0.0000) (0.0048) (0.0094)
18.07
A8 ID 03C-340,(0.7087) (0.
(0.7114)
03C-340 7091)
03-280, 17.89 18.00 17.83
A6 OD 03B-280,(0. 7043) (0.7087) (0.7020)
03C-280 0.00 0.12 0.24
03-340, 18.00 (0.0000) (0.0048) (0.0094)
18.01 18.07
A8 ID 03C-340,(0.7087) (0.0791) (0.7114)
03C-340
Fits and Clearances Table
TABLE 3

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**For PN’s ALL

C
SECTION

C A A

B
B

A2 A1

SECTION

C C SECTION

B B

B1

B3 B2
C1 C2

F_CM_528114_1_0060101_01_00

Fits and Clearances of the Main Landing Door

FIGURE-52-81-14-991-006-A01

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**For PN’s ALL

A5 A2 A3 A2 A4
A

A1

A7

A6

A8

F_CM_528114_1_0070101_01_00

Fits and Clearances for the Main Landing Door

FIGURE-52-81-14-991-007-A01

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STORAGE INCLUDING TRANSPORTATION

**For PN’s ALL

TASK 52-81-14-500-801-A01
Material Storage Data
1. General
A. See Material Storage Data (MSD)
The MSD document is a chargeable service to support customers with inventory planning, with
a 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, or SSO (Single Sign On) in Airbus World.
2. Procedure

Subtask 52-81-14-550-004-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 52-81-14-872-801-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

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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.

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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

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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

V00779 TBIL
V04795 TBIL
V05939 TBIL
V06329 TBIL
V06725 TBIL
V08748 TBIL
V0FKM1 TBIL
V0RFT4 TBIL
V0ZC92 TBIL
V10630 TBIL
V11815 TBIL
V13257 TBIL
V13899 TBIL
V15653 TBIL
V17446 TBIL
V1BGN6 TBIL
V1ER65 TBIL
V1RC86 TBIL
V27238 TBIL
V2N935 TBIL
V32664 TBIL
V52828 TBIL
V52930 TBIL
V53551 TBIL
V56878 TBIL
V57336 TBIL
V58009 TBIL
V58845 TBIL
V59736 TBIL
V5M902 TBIL
V60119 TBIL
V60516 TBIL
V60996 TBIL
V62384 TBIL
V65029 TBIL
V66776 TBIL

IPL INTRO
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CODE NAME AND ADDRESS

V70347 TBIL
V72962 TBIL
V73145 TBIL
V73197 TBIL
V75237 TBIL
V80205 TBIL
V80539 TBIL
V81343 TBIL
V83324 TBIL
V84114 TBIL
V88044 TBIL
V8848B TBIL
V8K160 TBIL
V8Z507 TBIL
V92215 TBIL
V96906 TBIL
V97393 TBIL
V97613 TBIL
V97928 TBIL
V98524 TBIL
VA3856 TBIL
VB1103 TBIL
VC3898 TBIL
VC4293 TBIL
VC5543 TBIL
VC5973 TBIL
VC6488 TBIL
VC7009 TBIL
VC7239 TBIL
VC7839 TBIL
VD1227 TBIL
VD3279 TBIL
VD7103 TBIL
VD8442 TBIL
VD8518 TBIL
VD9221 TBIL
VDM395 TBIL
VDM498 TBIL

IPL INTRO
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CODE NAME AND ADDRESS

VF0095 TBIL
VF0188 TBIL
VF0222 TBIL
VF0224 TBIL
VF0234 TBIL
VF0236 TBIL
VF0286 TBIL
VF0296 TBIL
VF2094 TBIL
VF4291 TBIL
VF5442 TBIL
VF6167 TBIL
VF6198 TBIL
VF7395 TBIL
VF7411 TBIL
VF7756 TBIL
VF8421 TBIL
VF8982 TBIL
VFA3K5 TBIL
VFAPE3 TBIL
VFAWT4 TBIL
VH1822 TBIL
VH6173 TBIL
VI9005 TBIL
VK0018 TBIL
VK0653 TBIL
VK0654 TBIL
VK1484 TBIL
VK5269 TBIL
VK5673 TBIL
VK8753 TBIL
VR1120 TBIL
VS0352 TBIL
VSBF11 TBIL
VSHS69 TBIL
VSS822 TBIL
VT0802 TBIL
VU1653 TBIL

IPL INTRO
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CODE NAME AND ADDRESS

VU6300 TBIL

IPL INTRO
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DETAILED PARTS LIST

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D5288000800000

110
(120)

30
(40)

10
(20)

50
(60)

30
(40) 90 70
(100) (80)

F_PL_528114_01_0_01_01

DOOR ASSY-MLG
Figure 01 / FIGURE-52-81-14-950-801-01

Page 10001-0
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01 - 001A D5288000800000 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01 - 001B D5288000800000 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01 - 001C D5288000800000 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01 - 001D D5288000800000 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01 - 001E D5288000800000 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01 - 001F D5288000800000 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01 - 001G D5288000800000 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01 - 001H D5288000800000 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01 - 001J D5288000800000 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01 - 001K D5288000800000 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01 - 001L D5288000800000 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01 - 001M D5288000800098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01 - 001N D5288000800098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01 - 001P D5288000800098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01 - 001Q D5288000800098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01 - 001R D5288000800098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01 - 001S D5288000800098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01 - 001T D5288000800098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01 - 001U D5288000800098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01 - 001V D5288000800098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
- ITEM NOT ILLUSTRATED

Page 10001-1
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01 - 001W D5288000800098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01 - 001X D5288000800098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01 - 002A D5288000800100 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01 - 002B D5288000800100 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01 - 002C D5288000800100 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01 - 002D D5288000800100 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01 - 002E D5288000800100 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01 - 002F D5288000800100 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01 - 002G D5288000800100 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01 - 002H D5288000800100 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01 - 002J D5288000800100 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01 - 002K D5288000800100 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01 - 002L D5288000800100 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01 - 002M D5288000800198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01 - 002N D5288000800198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01 - 002P D5288000800198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01 - 002Q D5288000800198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01 - 002R D5288000800198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01 - 002S D5288000800198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01 - 002T D5288000800198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
- ITEM NOT ILLUSTRATED

Page 10001-2
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01 - 002U D5288000800198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01 - 002V D5288000800198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01 - 002W D5288000800198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01 - 002X D5288000800198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01 010A D5288010000063 . FITTING INSTL-FORWARD VFAPE3 001
used on 001A
SEE 52-81-14-020 FOR DET
01 010B D5288010000066 . FITTING INSTL-FORWARD VFAPE3 001
used on 001B, 001C, 001D, 001E, 001F, 001G, 001H,
001J
SEE 52-81-14-020 FOR DET
01 010C D5288010000066 . FITTING INSTL-FORWARD VFAPE3 001
POST SB 52-1022
used on 001K, 001L
SEE 52-81-14-02A FOR DET
01 010D D5288010000066 . FITTING INSTL-FORWARD VFAPE3 001
POST SB 52-1073
used on 001M, 001N, 001P, 001Q, 001R, 001S, 001T,
001U, 001V, 001W, 001X
SEE 52-81-14-02B FOR DET
01 020A D5288010000163 . FITTING INSTL-FORWARD VFAPE3 001
used on 002A
SEE 52-81-14-020 FOR DET
01 020B D5288010000166 . FITTING INSTL-FORWARD VFAPE3 001
used on 002B, 002C, 002D, 002E, 002F, 002G, 002H,
002J
SEE 52-81-14-020 FOR DET
01 020C D5288010000166 . FITTING INSTL-FORWARD VFAPE3 001
POST SB 52-1022
used on 002K, 002L
SEE 52-81-14-02A FOR DET
01 020D D5288010000166 . FITTING INSTL-FORWARD VFAPE3 001
POST SB 52-1073
used on 002M, 002N, 002P, 002Q, 002R, 002S, 002T,
002U, 002V, 002W, 002X
SEE 52-81-14-02B FOR DET
01 030A D5288010000073 . UPLOCK AND STEP ASSY VFAPE3 001
used on 001A, 001B, 001D, 001M, 001N, 001Q
SEE 52-81-14-030 FOR DET
- ITEM NOT ILLUSTRATED

Page 10001-3
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01 030B D5288010000075 . UPLOCK AND STEP ASSY VFAPE3 001
used on 001C, 001E, 001P, 001R
SEE 52-81-14-03B FOR DET
01 030C D5288010000073 . UPLOCK AND STEP ASSY VFAPE3 001
used on 001F, 001G, 001H, 001J, 001K, 001L, 001S,
001T, 001U, 001V, 001W, 001X
SEE 52-81-14-03B FOR DET
01 040A D5288010000173 . UPLOCK AND STEP ASSY VFAPE3 001
used on 002A, 002B, 002D, 002M, 002N, 002Q
SEE 52-81-14-030 FOR DET
01 040B D5288010000175 . UPLOCK AND STEP ASSY VFAPE3 001
used on 002C, 002E, 002P, 002R
SEE 52-81-14-03B FOR DET
01 040C D5288010000173 . UPLOCK AND STEP ASSY VFAPE3 001
used on 002F, 002G, 002H, 002J, 002K, 002L, 002S,
002T, 002U, 002V, 002W, 002X
SEE 52-81-14-03B FOR DET
01 050A D5288000800065 . RAMP INSTL-LATERAL VFAPE3 001
used on 001A, 001B, 001C, 001D, 001G, 001L, 001M,
001N, 001P, 001Q, 001T, 001X
SEE 52-81-14-040 FOR DET
01 050B D5288000800065 . RAMP INSTL-LATERAL VFAPE3 001
used on 001E, 001F, 001H, 001J, 001K, 001R, 001S,
001U, 001V, 001W
SEE 52-81-14-04B FOR DET
01 060A D5288000800165 . RAMP INSTL-LATERAL VFAPE3 001
used on 002A, 002B, 002C, 002D, 002G, 002L, 002M,
002N, 002P, 002Q, 002T, 002X
SEE 52-81-14-040 FOR DET
01 060B D5288000800165 . RAMP INSTL-LATERAL VFAPE3 001
used on 002E, 002F, 002H, 002J, 002K, 002R, 002S,
002U, 002V, 002W
SEE 52-81-14-04B FOR DET
01 070A D5288000800064 . RAMP INSTL-CENTRAL VFAPE3 001
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J, 001M, 001N, 001P, 001Q, 001R, 001S,
001T, 001U, 001V
SEE 52-81-14-050 FOR DET
01 070B D5288000800064 . RAMP INSTL-CENTRAL VFAPE3 001
used on 001K, 001L, 001W, 001X
SEE 52-81-14-05B FOR DET
- ITEM NOT ILLUSTRATED

Page 10001-4
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01 080A D5288000800164 . RAMP INSTL-CENTRAL VFAPE3 001
used on 002A, 002B, 002C, 002D, 002E, 002F, 002G,
002H, 002J, 002M, 002N, 002P, 002Q, 002R, 002S,
002T, 002U, 002V
SEE 52-81-14-050 FOR DET
01 080B D5288000800164 . RAMP INSTL-CENTRAL VFAPE3 001
used on 002K, 002L, 002W, 002X
SEE 52-81-14-05B FOR DET
01 090A D5288010000074 . COVER ASSY VFAPE3 001
used on 001A, 001B, 001D, 001M, 001N, 001Q
SEE 52-81-14-060 FOR DET
01 090B D5288010000074 . COVER ASSY VFAPE3 001
used on 001C, 001E, 001P, 001R
SEE 52-81-14-060 FOR DET
01 090C D5288010000074 . COVER ASSY VFAPE3 001
used on 001F, 001G, 001H, 001J, 001S, 001T, 001U,
001V
SEE 52-81-14-06A FOR DET
01 090D D5288010000074 . COVER ASSY VFAPE3 001
used on 001K, 001L, 001W, 001X
SEE 52-81-14-06A FOR DET
01 100A D5288010000174 . COVER ASSY VFAPE3 001
used on 002A, 002B, 002D, 002M, 002N, 002Q
SEE 52-81-14-060 FOR DET
01 100B D5288010000174 . COVER ASSY VFAPE3 001
used on 002C, 002E, 002P, 002R
SEE 52-81-14-060 FOR DET
01 100C D5288010000174 . COVER ASSY VFAPE3 001
used on 002F, 002G, 002H, 002J, 002S, 002T, 002U,
002V
SEE 52-81-14-06A FOR DET
01 100D D5288010000174 . COVER ASSY VFAPE3 001
used on 002K, 002L, 002W, 002X
SEE 52-81-14-06A FOR DET
01 110A D5288010000068 . FITTING INSTL-REAR VFAPE3 001
used on 001A, 001M
SEE 52-81-14-070 FOR DET
01 110B D5288010000068 . FITTING INSTL-REAR VFAPE3 001
used on 001B, 001C, 001D, 001E, 001F, 001G, 001H,
001J, 001K, 001L, 001N, 001P, 001Q, 001R, 001S,
001T, 001U, 001V, 001W, 001X
SEE 52-81-14-070 FOR DET
- ITEM NOT ILLUSTRATED

Page 10001-5
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01 120A D5288010000168 . FITTING INSTL-REAR VFAPE3 001
used on 002A, 002M
SEE 52-81-14-070 FOR DET
01 120B D5288010000168 . FITTING INSTL-REAR VFAPE3 001
used on 002B, 002C, 002D, 002E, 002F, 002G, 002H,
002J, 002K, 002L, 002N, 002P, 002Q, 002R, 002S,
002T, 002U, 002V, 002W, 002X
SEE 52-81-14-070 FOR DET
01 - 130A D5288010700000 . BOLT ASSY VFAPE3 001
used on 001A, 001M, 002A, 002M
01 - 130B D5288010700000 . BOLT ASSY VFAPE3 001
used on 001B, 001C, 001D, 001E, 001F, 001G, 001H,
001J, 001K, 001L, 001N, 001P, 001Q, 001R, 001S,
001T, 001U, 001V, 001W, 001X, 002B, 002C, 002D,
002E, 002F, 002G, 002H, 002J, 002K, 002L, 002N,
002P, 002Q, 002R, 002S, 002T, 002U, 002V, 002W,
002X
01 - 140A MS24665-300 .. PIN-COTTER V96906 001
Optional Vendor Code 58009, 65029, 73145, 84114,
8K160
used on 130A, 130B
01 - 150A NSA5059-8 .. NUT VF6198 001
OPT TO H53173-8 15653
OPT TO MS14145L8 96906
OPT TO RMTE9868-8 72962
OPT TO THCR358M F0224
Optional Vendor Code 04795, 15653, 2N935, 56878,
A3856, C5543, F0224, FAWT4
used on 130A, 130B
01 - 160A NSA5305-8 .. WASHER VF6198 001
Optional Vendor Code 04795, 10630, 2N935, 58009,
C5543, F2094, F7395, F7756
used on 130A, 130B
01 - 170A D5288014020000 .. SPACER VFAPE3 001
used on 130A, 130B
01 - 180A D5288014120000 .. BOLT VFAPE3 001
used on 130A, 130B
01 - 180B D5288014120200 .. BOLT VFAPE3 001
used on 130A, 130B
01 - 190A NSA9117-22S . PLATE-IDENTIFICATION VF6198 001
NSA9117-62S F6198
- ITEM NOT ILLUSTRATED

Page 10001-6
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
Optional Vendor Code 04795, 2N935, C5543, D9221,
DM395, F0286, F8421, FA3K5, K1484
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J, 001K, 001L, 002A, 002B, 002C, 002D,
002E, 002F, 002G, 002H, 002J, 002K, 002L
01 - 190B NSA9117-20S . PLATE-IDENTIFICATION VF6198 001
Optional Vendor Code 04795, 2N935, C5543, DM395,
F8421, FA3K5, K1484
used on 001M, 001N, 001P, 001Q, 001R, 001S, 001T,
001U, 001V, 001W, 001X, 002M, 002N, 002P, 002Q,
002R, 002S, 002T, 002U, 002V, 002W, 002X
01 - 200A ABS0214-3-3 . RIVET VFAPE3 002
OPT TO CSR902B3W03 11815
OPT TO CSR902T3W3 11815
Optional Vendor Code 04795, 11815, 2N935, 53551,
C5543, F0095
used on 001M, 001N, 001P, 001Q, 001R, 001S, 001T,
001U, 001V, 001W, 001X, 002M, 002N, 002P, 002Q,
002R, 002S, 002T, 002U, 002V, 002W, 002X
- ITEM NOT ILLUSTRATED

Page 10001-7
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

110
(120)

30
(40)

10
(20)

50
(60)

30
(40) 90 70
(100) (80)

F_PL_528114_01_A_01_01

DOOR ASSY-MLG
Figure 01A / FIGURE-52-81-14-950-801-A01

Page 10001A-0
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01A - 001A D5288000900000 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01A - 001B D5288000900000 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01A - 001C D5288000900000 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01A - 001D D5288000900000 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01A - 001E D5288000900000 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01A - 001F D5288000900000 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01A - 001G D5288000900098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01A - 001H D5288000900098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01A - 001J D5288000900098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01A - 001K D5288000900098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01A - 001L D5288000900098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01A - 001M D5288000900098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01A - 002A D5288000900100 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01A - 002B D5288000900100 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01A - 002C D5288000900100 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01A - 002D D5288000900100 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01A - 002E D5288000900100 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01A - 002F D5288000900100 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01A - 002G D5288000900198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01A - 002H D5288000900198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
- ITEM NOT ILLUSTRATED

Page 10001A-1
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01A - 002J D5288000900198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01A - 002K D5288000900198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01A - 002L D5288000900198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01A - 002M D5288000900198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01A 010A D5288010000063 . FITTING INSTL-FORWARD VFAPE3 001
used on 001A
SEE 52-81-14-020 FOR DET
01A 010B D5288010000066 . FITTING INSTL-FORWARD VFAPE3 001
used on 001B, 001C, 001D, 001E
SEE 52-81-14-020 FOR DET
01A 010C D5288010000066 . FITTING INSTL-FORWARD VFAPE3 001
POST SB 52-1022
used on 001F
SEE 52-81-14-02A FOR DET
01A 010D D5288010000066 . FITTING INSTL-FORWARD VFAPE3 001
POST SB 52-1073
used on 001G, 001H, 001J, 001K, 001L, 001M
SEE 52-81-14-02B FOR DET
01A 020A D5288010000163 . FITTING INSTL-FORWARD VFAPE3 001
used on 002A
SEE 52-81-14-020 FOR DET
01A 020B D5288010000166 . FITTING INSTL-FORWARD VFAPE3 001
used on 002B, 002C, 002D, 002E
SEE 52-81-14-020 FOR DET
01A 020C D5288010000166 . FITTING INSTL-FORWARD VFAPE3 001
POST SB 52-1022
used on 002F
SEE 52-81-14-02A FOR DET
01A 020D D5288010000166 . FITTING INSTL-FORWARD VFAPE3 001
POST SB 52-1073
used on 002G, 002H, 002J, 002K, 002L, 002M
SEE 52-81-14-02B FOR DET
01A 030A D5288010000073 . UPLOCK AND STEP ASSY VFAPE3 001
used on 001A, 001B, 001G, 001H
SEE 52-81-14-030 FOR DET
01A 030B D5288010000075 . UPLOCK AND STEP ASSY VFAPE3 001
used on 001C, 001J
SEE 52-81-14-03B FOR DET
- ITEM NOT ILLUSTRATED

Page 10001A-2
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01A 030C D5288010000073 . UPLOCK AND STEP ASSY VFAPE3 001
used on 001D, 001E, 001F, 001K, 001L, 001M
SEE 52-81-14-03B FOR DET
01A 040A D5288010000173 . UPLOCK AND STEP ASSY VFAPE3 001
used on 002A, 002B, 002G, 002H
SEE 52-81-14-030 FOR DET
01A 040B D5288010000175 . UPLOCK AND STEP ASSY VFAPE3 001
used on 002C, 002J
SEE 52-81-14-03B FOR DET
01A 040C D5288010000173 . UPLOCK AND STEP ASSY VFAPE3 001
used on 002D, 002E, 002F, 002K, 002L, 002M
SEE 52-81-14-03B FOR DET
01A 050A D5288000900063 . RAMP INSTL-LATERAL VFAPE3 001
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J, 001K, 001L, 001M
SEE 52-81-14-04A FOR DET
01A 060A D5288000900163 . RAMP INSTL-LATERAL VFAPE3 001
used on 002A, 002B, 002C, 002D, 002E, 002F, 002G,
002H, 002J, 002K, 002L, 002M
SEE 52-81-14-04A FOR DET
01A 070A D5288000900064 . RAMP INSTL-CENTRAL VFAPE3 001
used on 001A, 001B, 001C, 001D, 001E, 001G, 001H,
001J, 001K, 001L
SEE 52-81-14-050 FOR DET
01A 070B D5288000900064 . RAMP INSTL-CENTRAL VFAPE3 001
used on 001F, 001M
SEE 52-81-14-05B FOR DET
01A 080A D5288000900164 . RAMP INSTL-CENTRAL VFAPE3 001
used on 002A, 002B, 002C, 002D, 002E, 002G, 002H,
002J, 002K, 002L
SEE 52-81-14-050 FOR DET
01A 080B D5288000900164 . RAMP INSTL-CENTRAL VFAPE3 001
used on 002F, 002M
SEE 52-81-14-05B FOR DET
01A 090A D5288010000074 . COVER ASSY VFAPE3 001
used on 001A, 001B, 001G, 001H
SEE 52-81-14-060 FOR DET
01A 090B D5288010000074 . COVER ASSY VFAPE3 001
used on 001C, 001J
SEE 52-81-14-060 FOR DET
- ITEM NOT ILLUSTRATED

Page 10001A-3
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01A 090C D5288010000074 . COVER ASSY VFAPE3 001
used on 001D, 001E, 001K, 001L
SEE 52-81-14-06A FOR DET
01A 090D D5288010000074 . COVER ASSY VFAPE3 001
used on 001F, 001M
SEE 52-81-14-06A FOR DET
01A 100A D5288010000174 . COVER ASSY VFAPE3 001
used on 002A, 002B, 002G, 002H
SEE 52-81-14-060 FOR DET
01A 100B D5288010000174 . COVER ASSY VFAPE3 001
used on 002C, 002J
SEE 52-81-14-060 FOR DET
01A 100C D5288010000174 . COVER ASSY VFAPE3 001
used on 002D, 002E, 002K, 002L
SEE 52-81-14-06A FOR DET
01A 100D D5288010000174 . COVER ASSY VFAPE3 001
used on 002F, 002M
SEE 52-81-14-06A FOR DET
01A 110A D5288010000068 . FITTING INSTL-REAR VFAPE3 001
used on 001A, 001G
SEE 52-81-14-070 FOR DET
01A 110B D5288010000068 . FITTING INSTL-REAR VFAPE3 001
used on 001B, 001C, 001D, 001E, 001F, 001H, 001J,
001K, 001L, 001M
SEE 52-81-14-070 FOR DET
01A 120A D5288010000168 . FITTING INSTL-REAR VFAPE3 001
used on 002A, 002G
SEE 52-81-14-070 FOR DET
01A 120B D5288010000168 . FITTING INSTL-REAR VFAPE3 001
used on 002B, 002C, 002D, 002E, 002F, 002H, 002J,
002K, 002L, 002M
SEE 52-81-14-070 FOR DET
01A - 130A D5288010700000 . BOLT ASSY VFAPE3 001
used on 001A, 001G, 002A, 002G
01A - 130B D5288010700000 . BOLT ASSY VFAPE3 001
used on 001B, 001C, 001D, 001E, 001F, 001H, 001J,
001K, 001L, 001M, 002B, 002C, 002D, 002E, 002F,
002H, 002J, 002K, 002L, 002M
01A - 140A MS24665-300 .. PIN-COTTER V96906 001
Optional Vendor Code 58009, 65029, 73145, 84114,
8K160
used on 130A, 130B
- ITEM NOT ILLUSTRATED

Page 10001A-4
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01A - 150A NSA5059-8 .. NUT VF6198 001
OPT TO H53173-8 15653
OPT TO MS14145L8 96906
OPT TO RMTE9868-8 72962
OPT TO THCR358M F0224
Optional Vendor Code 04795, 15653, 2N935, 56878,
A3856, C5543, F0224, FAWT4
used on 130A, 130B
01A - 160A NSA5305-8 .. WASHER VF6198 001
Optional Vendor Code 04795, 10630, 2N935, 58009,
C5543, F2094, F7395, F7756
used on 130A, 130B
01A - 170A D5288014020000 .. SPACER VFAPE3 001
used on 130A, 130B
01A - 180A D5288014120000 .. BOLT VFAPE3 001
used on 130A, 130B
01A - 180B D5288014120200 .. BOLT VFAPE3 001
used on 130A, 130B
01A - 210A NSA9117-22S . PLATE-IDENTIFICATION VF6198 001
NSA9117-62S F6198
Optional Vendor Code 04795, 2N935, C5543, D9221,
DM395, F0286, F8421, FA3K5, K1484
used on 001A, 001B, 001C, 001D, 001E, 001F, 002A,
002B, 002C, 002D, 002E, 002F
01A - 210B NSA9117-20S . PLATE-IDENTIFICATION VF6198 001
Optional Vendor Code 04795, 2N935, C5543, DM395,
F8421, FA3K5, K1484
used on 001G, 001H, 001J, 001K, 001L, 001M, 002G,
002H, 002J, 002K, 002L, 002M
01A - 220A ABS0214-3-3 . RIVET VFAPE3 002
OPT TO CSR902B3W03 11815
OPT TO CSR902T3W3 11815
Optional Vendor Code 04795, 11815, 2N935, 53551,
C5543, F0095
used on 001G, 001H, 001J, 001K, 001L, 001M, 002G,
002H, 002J, 002K, 002L, 002M
- ITEM NOT ILLUSTRATED

Page 10001A-5
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

110
(120)

30
(40)

10
(20)

50
(60)

30
(40) 90 70
(100) (80)

F_PL_528114_01_B_01_01

DOOR ASSY-MLG
Figure 01B / FIGURE-52-81-14-950-801-B01

Page 10001B-0
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01B - 001A D5288001000000 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01B - 001B D5288001000000 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01B - 001C D5288001000000 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01B - 001D D5288001000098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01B - 001E D5288001000098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01B - 001F D5288001000098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01B - 002A D5288001000100 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01B - 002B D5288001000100 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01B - 002C D5288001000100 DOOR ASSY-MLG VFAPE3 RF
PRE SB 52-1073, PRE SB 52-1025, PRE SB 52-1140
01B - 002D D5288001000198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01B - 002E D5288001000198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01B - 002F D5288001000198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073
01B 010A D5288010000066 . FITTING INSTL-FORWARD VFAPE3 001
used on 001A, 001B
SEE 52-81-14-020 FOR DET
01B 010B D5288010000066 . FITTING INSTL-FORWARD VFAPE3 001
POST SB 52-1022
used on 001C
SEE 52-81-14-02A FOR DET
01B 010C D5288010000066 . FITTING INSTL-FORWARD VFAPE3 001
POST SB 52-1073
used on 001D, 001E, 001F
SEE 52-81-14-02B FOR DET
01B 020A D5288010000166 . FITTING INSTL-FORWARD VFAPE3 001
used on 002A, 002B
SEE 52-81-14-020 FOR DET
01B 020B D5288010000166 . FITTING INSTL-FORWARD VFAPE3 001
POST SB 52-1022
used on 002C
SEE 52-81-14-02A FOR DET
- ITEM NOT ILLUSTRATED

Page 10001B-1
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01B 020C D5288010000166 . FITTING INSTL-FORWARD VFAPE3 001
POST SB 52-1073
used on 002D, 002E, 002F
SEE 52-81-14-02B FOR DET
01B 030A D5288010000073 . UPLOCK AND STEP ASSY VFAPE3 001
used on 001A, 001B, 001D, 001E
SEE 52-81-14-030 FOR DET
01B 030B D5288010000073 . UPLOCK AND STEP ASSY VFAPE3 001
used on 001C, 001F
SEE 52-81-14-03B FOR DET
01B 040A D5288010000173 . UPLOCK AND STEP ASSY VFAPE3 001
used on 002A, 002B, 002D, 002E
SEE 52-81-14-030 FOR DET
01B 040B D5288010000173 . UPLOCK AND STEP ASSY VFAPE3 001
used on 002C, 002F
SEE 52-81-14-03B FOR DET
01B 050A D5288001000064 . RAMP INSTL-LATERAL VFAPE3 001
used on 001A, 001D
SEE 52-81-14-04C FOR DET
01B 050B D5288001000064 . RAMP INSTL-LATERAL VFAPE3 001
used on 001B, 001C, 001E, 001F
SEE 52-81-14-04C FOR DET
01B 060A D5288001000164 . RAMP INSTL-LATERAL VFAPE3 001
used on 002A, 002D
SEE 52-81-14-04C FOR DET
01B 060B D5288001000164 . RAMP INSTL-LATERAL VFAPE3 001
used on 002B, 002C, 002E, 002F
SEE 52-81-14-04C FOR DET
01B 070A D5288001000063 . RAMP INSTL-CENTRAL VFAPE3 001
used on 001A, 001B, 001D, 001E
SEE 52-81-14-05A FOR DET
01B 070B D5288001000063 . RAMP INSTL-CENTRAL VFAPE3 001
used on 001C, 001F
SEE 52-81-14-05C FOR DET
01B 080A D5288001000163 . RAMP INSTL-CENTRAL VFAPE3 001
used on 002A, 002B, 002D, 002E
SEE 52-81-14-05A FOR DET
01B 080B D5288001000163 . RAMP INSTL-CENTRAL VFAPE3 001
used on 002C, 002F
SEE 52-81-14-05C FOR DET
- ITEM NOT ILLUSTRATED

Page 10001B-2
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01B 090A D5288010000074 . COVER ASSY VFAPE3 001
used on 001A, 001B, 001D, 001E
SEE 52-81-14-060 FOR DET
01B 090B D5288010000074 . COVER ASSY VFAPE3 001
used on 001C, 001F
SEE 52-81-14-06A FOR DET
01B 100A D5288010000174 . COVER ASSY VFAPE3 001
used on 002A, 002B, 002D, 002E
SEE 52-81-14-060 FOR DET
01B 100B D5288010000174 . COVER ASSY VFAPE3 001
used on 002C, 002F
SEE 52-81-14-06A FOR DET
01B 110A D5288010000068 . FITTING INSTL-REAR VFAPE3 001
used on 001A, 001D
SEE 52-81-14-070 FOR DET
01B 110B D5288010000068 . FITTING INSTL-REAR VFAPE3 001
used on 001B, 001C, 001E, 001F
SEE 52-81-14-070 FOR DET
01B 120A D5288010000168 . FITTING INSTL-REAR VFAPE3 001
used on 002A, 002D
SEE 52-81-14-070 FOR DET
01B 120B D5288010000168 . FITTING INSTL-REAR VFAPE3 001
used on 002B, 002C, 002E, 002F
SEE 52-81-14-070 FOR DET
01B - 130A D5288010700000 . BOLT ASSY VFAPE3 001
used on 001A, 001D, 002A, 002D
01B - 130B D5288010700000 . BOLT ASSY VFAPE3 001
used on 001B, 001C, 001E, 001F, 002B, 002C, 002E,
002F
01B - 140A MS24665-300 .. PIN-COTTER V96906 001
Optional Vendor Code 58009, 65029, 73145, 84114,
8K160
used on 130A, 130B
01B - 150A NSA5059-8 .. NUT VF6198 001
OPT TO H53173-8 15653
OPT TO MS14145L8 96906
OPT TO RMTE9868-8 72962
OPT TO THCR358M F0224
Optional Vendor Code 04795, 15653, 2N935, 56878,
A3856, C5543, F0224, FAWT4
used on 130A, 130B
- ITEM NOT ILLUSTRATED

Page 10001B-3
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01B - 160A NSA5305-8 .. WASHER VF6198 001
Optional Vendor Code 04795, 10630, 2N935, 58009,
C5543, F2094, F7395, F7756
used on 130A, 130B
01B - 170A D5288014020000 .. SPACER VFAPE3 001
used on 130A, 130B
01B - 180A D5288014120000 .. BOLT VFAPE3 001
used on 130A, 130B
01B - 180B D5288014120200 .. BOLT VFAPE3 001
used on 130A, 130B
01B - 190A NSA9117-22S . PLATE-IDENTIFICATION VF6198 001
NSA9117-62S F6198
Optional Vendor Code 04795, 2N935, C5543, D9221,
DM395, F0286, F8421, FA3K5, K1484
used on 001A, 001B, 001C, 002A, 002B, 002C
01B - 190B NSA9117-20S . PLATE-IDENTIFICATION VF6198 001
Optional Vendor Code 04795, 2N935, C5543, DM395,
F8421, FA3K5, K1484
used on 001D, 001E, 001F, 002D, 002E, 002F
01B - 200A ABS0214-3-3 . RIVET VFAPE3 002
OPT TO CSR902B3W03 11815
OPT TO CSR902T3W3 11815
Optional Vendor Code 04795, 11815, 2N935, 53551,
C5543, F0095
used on 001D, 001E, 001F, 002D, 002E, 002F
- ITEM NOT ILLUSTRATED

Page 10001B-4
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

A
110
(120)

30
(40)

10
(20)

50
(60)
210
(220)

30
(40) 90 70
(100) (80)

A
F_PL_528114_01_C_01_00

DOOR ASSY-MLG
Figure 01C / FIGURE-52-81-14-950-801-C01

Page 10001C-0
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01C - 001A D5288000800095 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01C - 001B D5288000800095 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01C - 001C D5288000800095 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01C - 001D D5288000800095 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01C - 001E D5288000800095 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01C - 001F D5288000800095 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01C - 001G D5288000800095 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01C - 001H D5288000800095 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01C - 001J D5288000800095 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01C - 001K D5288000800095 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01C - 001L D5288000800095 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01C - 001M D5288000800098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01C - 001N D5288000800098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01C - 001P D5288000800098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01C - 001Q D5288000800098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01C - 001R D5288000800098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01C - 001S D5288000800098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
- ITEM NOT ILLUSTRATED

Page 10001C-1
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01C - 001T D5288000800098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01C - 001U D5288000800098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01C - 001V D5288000800098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01C - 001W D5288000800098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01C - 001X D5288000800098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01C - 002A D5288000800195 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01C - 002B D5288000800195 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01C - 002C D5288000800195 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01C - 002D D5288000800195 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01C - 002E D5288000800195 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01C - 002F D5288000800195 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01C - 002G D5288000800195 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01C - 002H D5288000800195 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01C - 002J D5288000800195 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01C - 002K D5288000800195 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01C - 002L D5288000800195 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01C - 002M D5288000800198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
- ITEM NOT ILLUSTRATED

Page 10001C-2
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01C - 002N D5288000800198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01C - 002P D5288000800198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01C - 002Q D5288000800198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01C - 002R D5288000800198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01C - 002S D5288000800198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01C - 002T D5288000800198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01C - 002U D5288000800198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01C - 002V D5288000800198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01C - 002W D5288000800198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01C - 002X D5288000800198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01C 010A D5288010000063 . FITTING INSTL-FORWARD VFAPE3 001
used on 001A
SEE 52-81-14-020 FOR DET
01C 010B D5288010000066 . FITTING INSTL-FORWARD VFAPE3 001
used on 001B, 001C, 001D, 001E, 001F, 001G, 001H,
001J
SEE 52-81-14-020 FOR DET
01C 010C D5288010000066 . FITTING INSTL-FORWARD VFAPE3 001
POST SB 52-1022
used on 001K, 001L
SEE 52-81-14-02A FOR DET
- ITEM NOT ILLUSTRATED

Page 10001C-3
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01C 010D D5288010000066 . FITTING INSTL-FORWARD VFAPE3 001
POST SB 52-1073
used on 001M, 001N, 001P, 001Q, 001R, 001S, 001T,
001U, 001V, 001W, 001X
SEE 52-81-14-02B FOR DET
01C 020A D5288010000163 . FITTING INSTL-FORWARD VFAPE3 001
used on 002A
SEE 52-81-14-020 FOR DET
01C 020B D5288010000166 . FITTING INSTL-FORWARD VFAPE3 001
used on 002B, 002C, 002D, 002E, 002F, 002G, 002H,
002J
SEE 52-81-14-020 FOR DET
01C 020C D5288010000166 . FITTING INSTL-FORWARD VFAPE3 001
POST SB 52-1022
used on 002K, 002L
SEE 52-81-14-02A FOR DET
01C 020D D5288010000166 . FITTING INSTL-FORWARD VFAPE3 001
POST SB 52-1073
used on 002M, 002N, 002P, 002Q, 002R, 002S, 002T,
002U, 002V, 002W, 002X
SEE 52-81-14-02B FOR DET
01C 030A D5288010000073 . UPLOCK AND STEP ASSY VFAPE3 001
POST SB 52-1025
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J, 001K, 001L, 001M, 001N, 001P, 001Q,
001R, 001S, 001T, 001U, 001V, 001W, 001X
SEE 52-81-14-03C FOR DET
01C 040A D5288010000173 . UPLOCK AND STEP ASSY VFAPE3 001
used on 002A, 002B, 002C, 002D, 002E, 002F, 002G,
002H, 002J, 002K, 002L, 002M, 002N, 002P, 002Q,
002R, 002S, 002T, 002U, 002V, 002W, 002X
SEE 52-81-14-03C FOR DET
01C 050A D5288000800063 . RAMP INSTL-CENTRAL LH VFAPE3 001
POST SB 52-1025
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J, 001K, 001L, 001M, 001N, 001P, 001Q,
001R, 001S, 001T, 001U, 001V, 001W, 001X
SEE 52-81-14-04D FOR DET
01C 060A D5288000800163 . RAMP INSTL-CENTRAL RH VFAPE3 001
POST SB 52-1025
- ITEM NOT ILLUSTRATED

Page 10001C-4
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 002A, 002B, 002C, 002D, 002E, 002F, 002G,
002H, 002J, 002K, 002L, 002M, 002N, 002P, 002Q,
002R, 002S, 002T, 002U, 002V, 002W, 002X
SEE 52-81-14-04D FOR DET
01C 070A D5288000800064 . RAMP INSTL-CENTRAL VFAPE3 001
POST SB 52-1025
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J, 001K, 001L, 001M, 001N, 001P, 001Q,
001R, 001S, 001T, 001U, 001V, 001W, 001X
SEE 52-81-14-05D FOR DET
01C 080A D5288000800164 . RAMP INSTL-CENTRAL VFAPE3 001
POST SB 52-1025
used on 002A, 002B, 002C, 002D, 002E, 002F, 002G,
002H, 002J, 002K, 002L, 002M, 002N, 002P, 002Q,
002R, 002S, 002T, 002U, 002V, 002W, 002X
SEE 52-81-14-05D FOR DET
01C 090A D5288010000074 . COVER ASSY VFAPE3 001
used on 001A, 001B, 001D, 001M, 001N, 001Q
SEE 52-81-14-060 FOR DET
01C 090B D5288010000074 . COVER ASSY VFAPE3 001
used on 001C, 001E, 001P, 001R
SEE 52-81-14-060 FOR DET
01C 090C D5288010000074 . COVER ASSY VFAPE3 001
used on 001F, 001G, 001H, 001J, 001S, 001T, 001U,
001V
SEE 52-81-14-06A FOR DET
01C 090D D5288010000074 . COVER ASSY VFAPE3 001
used on 001K, 001L, 001W, 001X
SEE 52-81-14-06A FOR DET
01C 100A D5288010000174 . COVER ASSY VFAPE3 001
used on 002A, 002B, 002D, 002M, 002N, 002Q
SEE 52-81-14-060 FOR DET
01C 100B D5288010000174 . COVER ASSY VFAPE3 001
used on 002C, 002E, 002P, 002R
SEE 52-81-14-060 FOR DET
01C 100C D5288010000174 . COVER ASSY VFAPE3 001
used on 002F, 002G, 002H, 002J, 002S, 002T, 002U,
002V
SEE 52-81-14-06A FOR DET
01C 100D D5288010000174 . COVER ASSY VFAPE3 001
used on 002K, 002L, 002W, 002X
SEE 52-81-14-06A FOR DET
- ITEM NOT ILLUSTRATED

Page 10001C-5
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01C 110A D5288010000068 . FITTING INSTL-REAR VFAPE3 001
used on 001A, 001M
SEE 52-81-14-070 FOR DET
01C 110B D5288010000068 . FITTING INSTL-REAR VFAPE3 001
used on 001B, 001C, 001D, 001E, 001F, 001G, 001H,
001J, 001K, 001L, 001N, 001P, 001Q, 001R, 001S,
001T, 001U, 001V, 001W, 001X
SEE 52-81-14-070 FOR DET
01C 120A D5288010000168 . FITTING INSTL-REAR VFAPE3 001
used on 002A, 002M
SEE 52-81-14-070 FOR DET
01C 120B D5288010000168 . FITTING INSTL-REAR VFAPE3 001
used on 002B, 002C, 002D, 002E, 002F, 002G, 002H,
002J, 002K, 002L, 002N, 002P, 002Q, 002R, 002S,
002T, 002U, 002V, 002W, 002X
SEE 52-81-14-070 FOR DET
01C - 130A D5288010700000 . BOLT ASSY VFAPE3 001
used on 001A, 001M, 002A, 002M
01C - 130B D5288010700000 . BOLT ASSY VFAPE3 001
used on 001B, 001C, 001D, 001E, 001F, 001G, 001H,
001J, 001K, 001L, 001N, 001P, 001Q, 001R, 001S,
001T, 001U, 001V, 001W, 001X, 002B, 002C, 002D,
002E, 002F, 002G, 002H, 002J, 002K, 002L, 002N,
002P, 002Q, 002R, 002S, 002T, 002U, 002V, 002W,
002X
01C - 140A MS24665-300 .. PIN-COTTER V96906 001
Optional Vendor Code 58009, 65029, 73145, 84114,
8K160
used on 130A, 130B
01C - 150A NSA5059-8 .. NUT VF6198 001
OPT TO H53173-8 15653
OPT TO MS14145L8 96906
OPT TO RMTE9868-8 72962
OPT TO THCR358M F0224
Optional Vendor Code 04795, 15653, 2N935, 56878,
A3856, C5543, F0224, FAWT4
used on 130A, 130B
01C - 160A NSA5305-8 .. WASHER VF6198 001
Optional Vendor Code 04795, 10630, 2N935, 58009,
C5543, F2094, F7395, F7756
used on 130A, 130B
- ITEM NOT ILLUSTRATED

Page 10001C-6
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01C - 170A D5288014020000 .. SPACER VFAPE3 001
used on 130A, 130B
01C - 180A D5288014120000 .. BOLT VFAPE3 001
used on 130A, 130B
01C - 180B D5288014120200 .. BOLT VFAPE3 001
used on 130A, 130B
01C - 190A NSA9117-22S . PLATE-IDENTIFICATION VF6198 001
NSA9117-62S F6198
Optional Vendor Code 04795, 2N935, C5543, D9221,
DM395, F0286, F8421, FA3K5, K1484
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J, 001K, 001L, 002A, 002B, 002C, 002D,
002E, 002F, 002G, 002H, 002J, 002K, 002L
01C - 190B NSA9117-20S . PLATE-IDENTIFICATION VF6198 001
Optional Vendor Code 04795, 2N935, C5543, DM395,
F8421, FA3K5, K1484
used on 001M, 001N, 001P, 001Q, 001R, 001S, 001T,
001U, 001V, 001W, 001X, 002M, 002N, 002P, 002Q,
002R, 002S, 002T, 002U, 002V, 002W, 002X
01C - 200A ABS0214-3-3 . RIVET VFAPE3 002
OPT TO CSR902B3W03 11815
OPT TO CSR902T3W3 11815
Optional Vendor Code 04795, 11815, 2N935, 53551,
C5543, F0095
used on 001M, 001N, 001P, 001Q, 001R, 001S, 001T,
001U, 001V, 001W, 001X, 002M, 002N, 002P, 002Q,
002R, 002S, 002T, 002U, 002V, 002W, 002X
01C 210A D5288000800078 . PODGER INSTL VFAPE3 001
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J, 001K, 001L, 001M, 001N, 001P, 001Q,
001R, 001S, 001T, 001U, 001V, 001W, 001X
SEE 52-81-14-080 FOR DET
01C 220A D5288000800178 . PODGER INSTL VFAPE3 001
used on 002A, 002B, 002C, 002D, 002E, 002F, 002G,
002H, 002J, 002K, 002L, 002M, 002N, 002P, 002Q,
002R, 002S, 002T, 002U, 002V, 002W, 002X
SEE 52-81-14-080 FOR DET
01C - 230A NSA9117M5S . PLATE-IDENTIFICATION VF6198 001
POST SB 52-1025
Optional Vendor Code 04795, 2N935, C5543, DM395,
F8421, FA3K5, K1484
- ITEM NOT ILLUSTRATED

Page 10001C-7
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J, 001K, 001L, 001M, 001N, 001P, 001Q,
001R, 001S, 001T, 001U, 001V, 001W, 001X, 002A,
002B, 002C, 002D, 002E, 002F, 002G, 002H, 002J,
002K, 002L, 002M, 002N, 002P, 002Q, 002R, 002S,
002T, 002U, 002V, 002W, 002X
01C - 240A ABS0214-3-3 . RIVET VFAPE3 002
POST SB 52-1025
OPT TO CSR902B3W03 11815
OPT TO CSR902T3W3 11815
Optional Vendor Code 04795, 11815, 2N935, 53551,
C5543, F0095
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J, 001K, 001L, 001M, 001N, 001P, 001Q,
001R, 001S, 001T, 001U, 001V, 001W, 001X, 002A,
002B, 002C, 002D, 002E, 002F, 002G, 002H, 002J,
002K, 002L, 002M, 002N, 002P, 002Q, 002R, 002S,
002T, 002U, 002V, 002W, 002X
- ITEM NOT ILLUSTRATED

Page 10001C-8
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

A
110
(120)

30
(40)

10
(20)

50
(60)
230
(240)

30
(40) 90 70
(100) (80)

A
F_PL_528114_01_D_01_00

DOOR ASSY-MLG
Figure 01D / FIGURE-52-81-14-950-801-D01

Page 10001D-0
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01D - 001A D5288000900095 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01D - 001B D5288000900095 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01D - 001C D5288000900095 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01D - 001D D5288000900095 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01D - 001E D5288000900095 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01D - 001F D5288000900095 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01D - 001G D5288000900098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01D - 001H D5288000900098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01D - 001J D5288000900098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01D - 001K D5288000900098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01D - 001L D5288000900098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01D - 001M D5288000900098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01D - 001N D5288000900094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, POST SB 52-1140
01D - 001P D5288000900094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01D - 001Q D5288000900094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01D - 001R D5288000900094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01D - 001S D5288000900094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
- ITEM NOT ILLUSTRATED

Page 10001D-1
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01D - 001T D5288000900094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01D - 001U D5288000900094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01D - 001V D5288000900094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01D - 001W D5288000900094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01D - 001X D5288000900094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01D - 001Y D5288000900094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01D - 001Z D5288000900094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01D - 002A D5288000900195 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01D - 002B D5288000900195 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01D - 002C D5288000900195 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01D - 002D D5288000900195 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01D - 002E D5288000900195 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01D - 002F D5288000900195 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01D - 002G D5288000900198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01D - 002H D5288000900198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01D - 002J D5288000900198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
- ITEM NOT ILLUSTRATED

Page 10001D-2
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01D - 002K D5288000900198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01D - 002L D5288000900198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01D - 002M D5288000900198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01D - 002N D5288000900194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01D - 002P D5288000900194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01D - 002Q D5288000900194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01D - 002R D5288000900194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, POST SB 52-1140
01D - 002S D5288000900194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01D - 002T D5288000900194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01D - 002U D5288000900194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01D - 002V D5288000900194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01D - 002W D5288000900194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01D - 002X D5288000900194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, POST SB 52-1140, POST SB
52-1073
01D - 002Y D5288000900194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01D - 002Z D5288000900194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
- ITEM NOT ILLUSTRATED

Page 10001D-3
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01D 010A D5288010000063 . FITTING INSTL-FORWARD VFAPE3 001
used on 001A, 001N
SEE 52-81-14-020 FOR DET
01D 010B D5288010000066 . FITTING INSTL-FORWARD VFAPE3 001
used on 001B, 001C, 001D, 001E, 001P, 001Q, 001R,
001S
SEE 52-81-14-020 FOR DET
01D 010C D5288010000066 . FITTING INSTL-FORWARD VFAPE3 001
POST SB 52-1022
used on 001F, 001T
SEE 52-81-14-02A FOR DET
01D 010D D5288010000066 . FITTING INSTL-FORWARD VFAPE3 001
POST SB 52-1073
used on 001G, 001H, 001J, 001K, 001L, 001M, 001U,
001V, 001W, 001X, 001Y, 001Z
SEE 52-81-14-02B FOR DET
01D 020A D5288010000163 . FITTING INSTL-FORWARD VFAPE3 001
used on 002A, 002N
SEE 52-81-14-020 FOR DET
01D 020B D5288010000166 . FITTING INSTL-FORWARD VFAPE3 001
used on 002B, 002C, 002D, 002E, 002P, 002Q, 002R,
002S
SEE 52-81-14-020 FOR DET
01D 020C D5288010000166 . FITTING INSTL-FORWARD VFAPE3 001
POST SB 52-1022
used on 002F, 002T
SEE 52-81-14-02A FOR DET
01D 020D D5288010000166 . FITTING INSTL-FORWARD VFAPE3 001
POST SB 52-1073
used on 002G, 002H, 002J, 002K, 002L, 002M, 002U,
002V, 002W, 002X, 002Y, 002Z
SEE 52-81-14-02B FOR DET
01D 030A D5288010000073 . UPLOCK AND STEP ASSY VFAPE3 001
POST SB 52-1025
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J, 001K, 001L, 001M, 001N, 001P, 001Q,
001R, 001S, 001T, 001U, 001V, 001W, 001X, 001Y,
001Z
SEE 52-81-14-03C FOR DET
01D 040A D5288010000173 . UPLOCK AND STEP ASSY VFAPE3 001
POST SB 52-1025
- ITEM NOT ILLUSTRATED

Page 10001D-4
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 002A, 002B, 002C, 002D, 002E, 002F, 002G,
002H, 002J, 002K, 002L, 002M, 002N, 002P, 002Q,
002R, 002S, 002T, 002U, 002V, 002W, 002X, 002Y,
002Z
SEE 52-81-14-03C FOR DET
01D 050B D5288000900063 . RAMP INSTL-LATERAL VFAPE3 001
POST SB 52-1025
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J, 001K, 001L, 001M, 001N, 001P, 001Q,
001R, 001S, 001T, 001U, 001V, 001W, 001X, 001Y,
001Z
SEE 52-81-14-04D FOR DET
01D 060A D5288000900163 . RAMP INSTL-LATERAL VFAPE3 001
POST SB 52-1025
used on 002A, 002B, 002C, 002D, 002E, 002F, 002G,
002H, 002J, 002K, 002L, 002M, 002N, 002P, 002Q,
002R, 002S, 002T, 002U, 002V, 002W, 002X, 002Y,
002Z
SEE 52-81-14-04D FOR DET
01D 070A D5288000900064 . RAMP INSTL-CENTRAL VFAPE3 001
POST SB 52-1025
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J, 001K, 001L, 001M
SEE 52-81-14-05D FOR DET
01D 070B D5288000900064 . RAMP INSTL-CENTRAL VFAPE3 001
POST SB 52-1140
used on 001N, 001P, 001Q, 001R, 001S, 001T, 001U,
001V, 001W, 001X, 001Y, 001Z
SEE 52-81-14-05F FOR DET
01D 080A D5288000900164 . RAMP INSTL-CENTRAL VFAPE3 001
POST SB 52-1025
used on 002A, 002B, 002C, 002D, 002E, 002F, 002G,
002H, 002J, 002K, 002L, 002M
SEE 52-81-14-05D FOR DET
01D 080B D5288000900164 . RAMP INSTL-CENTRAL VFAPE3 001
POST SB 52-1140
used on 002N, 002P, 002Q, 002R, 002S, 002T, 002U,
002V, 002W, 002X, 002Y, 002Z
SEE 52-81-14-05F FOR DET
01D 090A D5288010000074 . COVER ASSY VFAPE3 001
used on 001A, 001B, 001G, 001H, 001N, 001P, 001U,
001V
SEE 52-81-14-060 FOR DET
- ITEM NOT ILLUSTRATED

Page 10001D-5
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01D 090B D5288010000074 . COVER ASSY VFAPE3 001
used on 001C, 001J, 001Q, 001W
SEE 52-81-14-060 FOR DET
01D 090C D5288010000074 . COVER ASSY VFAPE3 001
used on 001D, 001E, 001K, 001L, 001R, 001S, 001X,
001Y
SEE 52-81-14-06A FOR DET
01D 090D D5288010000074 . COVER ASSY VFAPE3 001
used on 001F, 001M, 001T, 001Z
SEE 52-81-14-06A FOR DET
01D 100A D5288010000174 . COVER ASSY VFAPE3 001
used on 002A, 002B, 002G, 002H, 002N, 002P, 002U,
002V
SEE 52-81-14-060 FOR DET
01D 100B D5288010000174 . COVER ASSY VFAPE3 001
used on 002C, 002J, 002Q, 002W
SEE 52-81-14-060 FOR DET
01D 100C D5288010000174 . COVER ASSY VFAPE3 001
used on 002D, 002E, 002K, 002L, 002R, 002S, 002X,
002Y
SEE 52-81-14-06A FOR DET
01D 100D D5288010000174 . COVER ASSY VFAPE3 001
used on 002F, 002M, 002T, 002Z
SEE 52-81-14-06A FOR DET
01D 110A D5288010000068 . FITTING INSTL-REAR VFAPE3 001
used on 001A, 001G, 001N, 001U
SEE 52-81-14-070 FOR DET
01D 110B D5288010000068 . FITTING INSTL-REAR VFAPE3 001
used on 001B, 001C, 001D, 001E, 001F, 001H, 001J,
001K, 001L, 001M, 001P, 001Q, 001R, 001S, 001T,
001V, 001W, 001X, 001Y, 001Z
SEE 52-81-14-070 FOR DET
01D 120A D5288010000168 . FITTING INSTL-REAR VFAPE3 001
used on 002A, 002G, 002N, 002U
SEE 52-81-14-070 FOR DET
01D 120B D5288010000168 . FITTING INSTL-REAR VFAPE3 001
used on 002B, 002C, 002D, 002E, 002F, 002H, 002J,
002K, 002L, 002M, 002P, 002Q, 002R, 002S, 002T,
002V, 002W, 002X, 002Y, 002Z
SEE 52-81-14-070 FOR DET
- ITEM NOT ILLUSTRATED

Page 10001D-6
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01D - 130A D5288010700000 . BOLT ASSY VFAPE3 001
used on 001A, 001G, 001N, 001U, 002A, 002G, 002N,
002U
01D - 130B D5288010700000 . BOLT ASSY VFAPE3 001
used on 001B, 001C, 001D, 001E, 001F, 001H, 001J,
001K, 001L, 001M, 001P, 001Q, 001R, 001S, 001T,
001V, 001W, 001X, 001Y, 001Z, 002B, 002C, 002D,
002E, 002F, 002H, 002J, 002K, 002L, 002M, 002P,
002Q, 002R, 002S, 002T, 002V, 002W, 002X, 002Y,
002Z
01D - 140A MS24665-300 .. PIN-COTTER V96906 001
Optional Vendor Code 58009, 65029, 73145, 84114,
8K160
used on 130A, 130B
01D - 150A NSA5059-8 .. NUT VF6198 001
OPT TO H53173-8 15653
OPT TO MS14145L8 96906
OPT TO RMTE9868-8 72962
OPT TO THCR358M F0224
Optional Vendor Code 04795, 15653, 2N935, 56878,
A3856, C5543, F0224, FAWT4
used on 130A, 130B
01D - 160A NSA5305-8 .. WASHER VF6198 001
Optional Vendor Code 04795, 10630, 2N935, 58009,
C5543, F2094, F7395, F7756
used on 130A, 130B
01D - 170A D5288014020000 .. SPACER VFAPE3 001
used on 130A, 130B
01D - 180A D5288014120000 .. BOLT VFAPE3 001
used on 130A, 130B
01D - 180B D5288014120200 .. BOLT VFAPE3 001
used on 130A, 130B
01D - 190A NSA9117M5S . PLATE-IDENTIFICATION VF6198 001
POST SB 52-1025
Optional Vendor Code 04795, 2N935, C5543, DM395,
F8421, FA3K5, K1484
- ITEM NOT ILLUSTRATED

Page 10001D-7
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J, 001K, 001L, 001M, 001N, 001P, 001Q,
001R, 001S, 001T, 001U, 001V, 001W, 001X, 001Y,
001Z, 002A, 002B, 002C, 002D, 002E, 002F, 002G,
002H, 002J, 002K, 002L, 002M, 002N, 002P, 002Q,
002R, 002S, 002T, 002U, 002V, 002W, 002X, 002Y,
002Z
01D - 200A ABS0214-3-3 . RIVET VFAPE3 002
POST SB 52-1025
OPT TO CSR902B3W03 11815
OPT TO CSR902T3W3 11815
Optional Vendor Code 04795, 11815, 2N935, 53551,
C5543, F0095
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J, 001K, 001L, 001M, 001N, 001P, 001Q,
001R, 001S, 001T, 001U, 001V, 001W, 001X, 001Y,
001Z, 002A, 002B, 002C, 002D, 002E, 002F, 002G,
002H, 002J, 002K, 002L, 002M, 002N, 002P, 002Q,
002R, 002S, 002T, 002U, 002V, 002W, 002X, 002Y,
002Z
01D - 210A NSA9117-22S . PLATE-IDENTIFICATION VF6198 001
NSA9117-62S F6198
Optional Vendor Code 04795, 2N935, C5543, D9221,
DM395, F0286, F8421, FA3K5, K1484
used on 001A, 001B, 001C, 001D, 001E, 001F, 001N,
001P, 001Q, 001R, 001S, 001T, 002A, 002B, 002C,
002D, 002E, 002F, 002N, 002P, 002Q, 002R, 002S,
002T
01D - 210B NSA9117-20S . PLATE-IDENTIFICATION VF6198 001
Optional Vendor Code 04795, 2N935, C5543, DM395,
F8421, FA3K5, K1484
used on 001G, 001H, 001J, 001K, 001L, 001M, 001U,
001V, 001W, 001X, 001Y, 001Z, 002G, 002H, 002J,
002K, 002L, 002M, 002U, 002V, 002W, 002X, 002Y,
002Z
01D - 220A ABS0214-3-3 . RIVET VFAPE3 002
OPT TO CSR902B3W03 11815
OPT TO CSR902T3W3 11815
Optional Vendor Code 04795, 11815, 2N935, 53551,
C5543, F0095
- ITEM NOT ILLUSTRATED

Page 10001D-8
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 001G, 001H, 001J, 001K, 001L, 001M, 001U,
001V, 001W, 001X, 001Y, 001Z, 002G, 002H, 002J,
002K, 002L, 002M, 002U, 002V, 002W, 002X, 002Y,
002Z
01D 230A D5288000900086 . PODGER INSTL VFAPE3 001
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J, 001K, 001L, 001M, 001N, 001P, 001Q,
001R, 001S, 001T, 001U, 001V, 001W, 001X, 001Y,
001Z
SEE 52-81-14-080 FOR DET
01D 240A D5288000900186 . PODGER INSTL VFAPE3 001
used on 002A, 002B, 002C, 002D, 002E, 002F, 002G,
002H, 002J, 002K, 002L, 002M, 002N, 002P, 002Q,
002R, 002S, 002T, 002U, 002V, 002W, 002X, 002Y,
002Z
SEE 52-81-14-080 FOR DET
- ITEM NOT ILLUSTRATED

Page 10001D-9
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

A
110
(120)

30
(40)

10
(20)

50
(60)
210
(220)

30
(40) 90 70
(100) (80)

A
F_PL_528114_01_E_01_00

DOOR ASSY-MLG
Figure 01E / FIGURE-52-81-14-950-801-E01

Page 10001E-0
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01E - 001A D5288001000095 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01E - 001B D5288001000095 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01E - 001C D5288001000095 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01E - 001D D5288001000098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01E - 001E D5288001000098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01E - 001F D5288001000098 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01E - 001G D5288001000094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01E - 001H D5288001000094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01E - 001J D5288001000094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01E - 001K D5288001000094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01E - 001L D5288001000094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01E - 001M D5288001000094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01E - 002A D5288001000195 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01E - 002B D5288001000195 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01E - 002C D5288001000195 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
01E - 002D D5288001000198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
- ITEM NOT ILLUSTRATED

Page 10001E-1
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01E - 002E D5288001000198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01E - 002F D5288001000198 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1073, POST SB 52-1025, PRE SB
52-1140
01E - 002G D5288001000194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01E - 002H D5288001000194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01E - 002J D5288001000194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01E - 002K D5288001000194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01E - 002L D5288001000194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01E - 002M D5288001000194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01E 010A D5288010000066 . FITTING INSTL-FORWARD VFAPE3 001
used on 001A, 001B, 001G, 001H
SEE 52-81-14-020 FOR DET
01E 010B D5288010000066 . FITTING INSTL-FORWARD VFAPE3 001
POST SB 52-1022
used on 001C, 001J
SEE 52-81-14-02A FOR DET
01E 010C D5288010000066 . FITTING INSTL-FORWARD VFAPE3 001
POST SB 52-1073
used on 001D, 001E, 001F, 001K, 001L, 001M
SEE 52-81-14-02B FOR DET
01E 020A D5288010000166 . FITTING INSTL-FORWARD VFAPE3 001
used on 002A, 002B, 002G, 002H
SEE 52-81-14-020 FOR DET
01E 020B D5288010000166 . FITTING INSTL-FORWARD VFAPE3 001
POST SB 52-1022
used on 002C, 002J
SEE 52-81-14-02A FOR DET
01E 020C D5288010000166 . FITTING INSTL-FORWARD VFAPE3 001
POST SB 52-1073
- ITEM NOT ILLUSTRATED

Page 10001E-2
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 002D, 002E, 002F, 002K, 002L, 002M
SEE 52-81-14-02B FOR DET
01E 030A D5288010000073 . UPLOCK AND STEP ASSY VFAPE3 001
POST SB 52-1025
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J, 001K, 001L, 001M
SEE 52-81-14-03C FOR DET
01E 040A D5288010000173 . UPLOCK AND STEP ASSY VFAPE3 001
POST SB 52-1025
used on 002A, 002B, 002C, 002D, 002E, 002F, 002G,
002H, 002J, 002K, 002L, 002M
SEE 52-81-14-03C FOR DET
01E 050A D5288001000063 . RAMP INSTL-CENTRAL VFAPE3 001
POST SB 52-1025
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J, 001K, 001L, 001M
SEE 52-81-14-04D FOR DET
01E 060A D5288001000163 . RAMP INSTL-CENTRAL VFAPE3 001
POST SB 52-1025
used on 002A, 002B, 002C, 002D, 002E, 002F, 002G,
002H, 002J, 002K, 002L, 002M
SEE 52-81-14-04D FOR DET
01E 070A D5288001000063 . RAMP INSTL-CENTRAL VFAPE3 001
POST SB 52-1025
used on 001A, 001B, 001C, 001D, 001E, 001F
SEE 52-81-14-05E FOR DET
01E 070B D5288001000063 . RAMP INSTL-CENTRAL VFAPE3 001
POST SB 52-1140
used on 001G, 001H, 001J, 001K, 001L, 001M
SEE 52-81-14-05G FOR DET
01E 080A D5288001000163 . RAMP INSTL-CENTRAL VFAPE3 001
POST SB 52-1025
used on 002A, 002B, 002C, 002D, 002E, 002F
SEE 52-81-14-05E FOR DET
01E 080B D5288001000163 . RAMP INSTL-CENTRAL VFAPE3 001
POST SB 52-1140
used on 002G, 002H, 002J, 002K, 002L, 002M
SEE 52-81-14-05G FOR DET
01E 090A D5288010000074 . COVER ASSY VFAPE3 001
used on 001A, 001B, 001D, 001E, 001G, 001H, 001K,
001L
SEE 52-81-14-060 FOR DET
- ITEM NOT ILLUSTRATED

Page 10001E-3
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01E 090B D5288010000074 . COVER ASSY VFAPE3 001
used on 001C, 001F, 001J, 001M
SEE 52-81-14-06A FOR DET
01E 100A D5288010000174 . COVER ASSY VFAPE3 001
used on 002A, 002B, 002D, 002E, 002G, 002H, 002K,
002L
SEE 52-81-14-060 FOR DET
01E 100B D5288010000174 . COVER ASSY VFAPE3 001
used on 002C, 002F, 002J, 002M
SEE 52-81-14-06A FOR DET
01E 110A D5288010000068 . FITTING INSTL-REAR VFAPE3 001
used on 001A, 001D, 001G, 001K
SEE 52-81-14-070 FOR DET
01E 110B D5288010000068 . FITTING INSTL-REAR VFAPE3 001
used on 001B, 001C, 001E, 001F, 001H, 001J, 001L,
001M
SEE 52-81-14-070 FOR DET
01E 120A D5288010000168 . FITTING INSTL-REAR VFAPE3 001
used on 002A, 002D, 002G, 002K
SEE 52-81-14-070 FOR DET
01E 120B D5288010000168 . FITTING INSTL-REAR VFAPE3 001
used on 002B, 002C, 002E, 002F, 002H, 002J, 002L,
002M
SEE 52-81-14-070 FOR DET
01E - 130A D5288010700000 . BOLT ASSY VFAPE3 001
used on 001A, 001D, 001G, 001K, 002A, 002D, 002G,
002K
01E - 130B D5288010700000 . BOLT ASSY VFAPE3 001
used on 001B, 001C, 001E, 001F, 001H, 001J, 001L,
001M, 002B, 002C, 002E, 002F, 002H, 002J, 002L,
002M
01E - 140A MS24665-300 .. PIN-COTTER V96906 001
Optional Vendor Code 58009, 65029, 73145, 84114,
8K160
used on 130A, 130B
01E - 150A NSA5059-8 .. NUT VF6198 001
OPT TO H53173-8 15653
OPT TO MS14145L8 96906
OPT TO RMTE9868-8 72962
OPT TO THCR358M F0224
Optional Vendor Code 04795, 15653, 2N935, 56878,
A3856, C5543, F0224, FAWT4
- ITEM NOT ILLUSTRATED

Page 10001E-4
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 130A, 130B
01E - 160A NSA5305-8 .. WASHER VF6198 001
Optional Vendor Code 04795, 10630, 2N935, 58009,
C5543, F2094, F7395, F7756
used on 130A, 130B
01E - 170A D5288014020000 .. SPACER VFAPE3 001
used on 130A, 130B
01E - 180A D5288014120000 .. BOLT VFAPE3 001
used on 130A, 130B
01E - 180B D5288014120200 .. BOLT VFAPE3 001
used on 130A, 130B
01E - 190A NSA9117-22S . PLATE-IDENTIFICATION VF6198 001
NSA9117-62S F6198
Optional Vendor Code 04795, 2N935, C5543, D9221,
DM395, F0286, F8421, FA3K5, K1484
used on 001A, 001B, 001C, 001G, 001H, 001J, 002A,
002B, 002C, 002G, 002H, 002J
01E - 190B NSA9117-20S . PLATE-IDENTIFICATION VF6198 001
Optional Vendor Code 04795, 2N935, C5543, DM395,
F8421, FA3K5, K1484
used on 001D, 001E, 001F, 001K, 001L, 001M, 002D,
002E, 002F, 002K, 002L, 002M
01E - 200A ABS0214-3-3 . RIVET VFAPE3 002
OPT TO CSR902B3W03 11815
OPT TO CSR902T3W3 11815
Optional Vendor Code 04795, 11815, 2N935, 53551,
C5543, F0095
used on 001D, 001E, 001F, 001K, 001L, 001M, 002D,
002E, 002F, 002K, 002L, 002M
01E 210A D5288001000066 . PODGER INSTL VFAPE3 001
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J, 001K, 001L, 001M
SEE 52-81-14-080 FOR DET
01E 220A D5288001000166 . PODGER INSTL VFAPE3 001
used on 002A, 002B, 002C, 002D, 002E, 002F, 002G,
002H, 002J, 002K, 002L, 002M
SEE 52-81-14-080 FOR DET
01E - 230A NSA9117M5S . PLATE-IDENTIFICATION VF6198 001
POST SB 52-1025
Optional Vendor Code 04795, 2N935, C5543, DM395,
F8421, FA3K5, K1484
- ITEM NOT ILLUSTRATED

Page 10001E-5
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J, 001K, 001L, 001M, 002A, 002B, 002C,
002D, 002E, 002F, 002G, 002H, 002J, 002K, 002L,
002M
01E - 240A ABS0214-3-3 . RIVET VFAPE3 002
POST SB 52-1025
OPT TO CSR902B3W03 11815
OPT TO CSR902T3W3 11815
Optional Vendor Code 04795, 11815, 2N935, 53551,
C5543, F0095
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J, 001K, 001L, 001M, 002A, 002B, 002C,
002D, 002E, 002F, 002G, 002H, 002J, 002K, 002L,
002M
- ITEM NOT ILLUSTRATED

Page 10001E-6
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

A
110
(120)

30
(40)

10
(20)

50
(60)
210
(220)

30
(40) 90 70
(100) (80)

A
F_PL_528114_01_F_01_00

DOOR ASSY-MLG
Figure 01F / FIGURE-52-81-14-950-801-F01

Page 10001F-0
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01F - 001A D5288000800094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01F - 001B D5288000800094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01F - 001C D5288000800094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01F - 001D D5288000800094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01F - 001E D5288000800094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01F - 001F D5288000800094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01F - 001G D5288000800094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01F - 001H D5288000800094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01F - 001J D5288000800094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01F - 001K D5288000800094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01F - 001L D5288000800094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01F - 001M D5288000800094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01F - 001N D5288000800094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01F - 001P D5288000800094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01F - 001Q D5288000800094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01F - 001R D5288000800094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, POST SB 52-1140, POST SB
52-1073
01F - 001S D5288000800094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
- ITEM NOT ILLUSTRATED

Page 10001F-1
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01F - 001T D5288000800094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01F - 001U D5288000800094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01F - 001V D5288000800094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01F - 001W D5288000800094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01F - 001X D5288000800094 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01F - 002A D5288000800194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01F - 002B D5288000800194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01F - 002C D5288000800194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01F - 002D D5288000800194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01F - 002E D5288000800194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01F - 002F D5288000800194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01F - 002G D5288000800194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01F - 002H D5288000800194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01F - 002J D5288000800194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01F - 002K D5288000800194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01F - 002L D5288000800194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
01F - 002M D5288000800194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
- ITEM NOT ILLUSTRATED

Page 10001F-2
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01F - 002N D5288000800194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01F - 002P D5288000800194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01F - 002Q D5288000800194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01F - 002R D5288000800194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01F - 002S D5288000800194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01F - 002T D5288000800194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1025, POST SB 52-1140, POST SB
52-1073
01F - 002U D5288000800194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01F - 002V D5288000800194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01F - 002W D5288000800194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01F - 002X D5288000800194 DOOR ASSY-MLG VFAPE3 RF
POST SB 52-1140, POST SB 52-1025, POST SB
52-1073
01F 010A D5288010000063 . FITTING INSTL-FORWARD VFAPE3 001
used on 001A
SEE 52-81-14-020 FOR DET
01F 010B D5288010000066 . FITTING INSTL-FORWARD VFAPE3 001
used on 001B, 001C, 001D, 001E, 001F, 001G, 001H,
001J
SEE 52-81-14-020 FOR DET
01F 010C D5288010000066 . FITTING INSTL-FORWARD VFAPE3 001
POST SB 52-1022
used on 001K, 001L
SEE 52-81-14-02A FOR DET
- ITEM NOT ILLUSTRATED

Page 10001F-3
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01F 010D D5288010000066 . FITTING INSTL-FORWARD VFAPE3 001
POST SB 52-1073
used on 001M, 001N, 001P, 001Q, 001R, 001S, 001T,
001U, 001V, 001W, 001X
SEE 52-81-14-02B FOR DET
01F 020A D5288010000163 . FITTING INSTL-FORWARD VFAPE3 001
used on 002A
SEE 52-81-14-020 FOR DET
01F 020B D5288010000166 . FITTING INSTL-FORWARD VFAPE3 001
used on 002B, 002C, 002D, 002E, 002F, 002G, 002H,
002J
SEE 52-81-14-020 FOR DET
01F 020C D5288010000166 . FITTING INSTL-FORWARD VFAPE3 001
used on 002K, 002L
SEE 52-81-14-02A FOR DET
01F 020D D5288010000166 . FITTING INSTL-FORWARD VFAPE3 001
used on 002M, 002N, 002P, 002Q, 002R, 002S, 002T,
002U, 002V, 002W, 002X
SEE 52-81-14-02B FOR DET
01F 030A D5288010000073 . UPLOCK AND STEP ASSY VFAPE3 001
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J, 001K, 001L, 001M, 001N, 001P, 001Q,
001R, 001S, 001T, 001U, 001V, 001W, 001X
SEE 52-81-14-030 FOR DET
01F 040A D5288010000173 . UPLOCK AND STEP ASSY VFAPE3 001
used on 002A, 002B, 002C, 002D, 002E, 002F, 002G,
002H, 002J, 002K, 002L, 002M, 002N, 002P, 002Q,
002R, 002S, 002T, 002U, 002V, 002W, 002X
SEE 52-81-14-03C FOR DET
01F 050A D5288000800063 . RAMP INSTL-CENTRAL LH VFAPE3 001
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J, 001K, 001L, 001M, 001N, 001P, 001Q,
001R, 001S, 001T, 001U, 001V, 001W, 001X
SEE 52-81-14-04D FOR DET
01F 060A D5288000800163 . RAMP INSTL-CENTRAL RH VFAPE3 001
used on 002A, 002B, 002C, 002D, 002E, 002F, 002G,
002H, 002J, 002K, 002L, 002M, 002N, 002P, 002Q,
002R, 002S, 002T, 002U, 002V, 002W, 002X
SEE 52-81-14-04D FOR DET
01F 070A D5288000800064 . RAMP INSTL-CENTRAL VFAPE3 001
POST SB 52-1140
- ITEM NOT ILLUSTRATED

Page 10001F-4
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J, 001K, 001L, 001M, 001N, 001P, 001Q,
001R, 001S, 001T, 001U, 001V, 001W, 001X
SEE 52-81-14-05F FOR DET
01F 080A D5288000800164 . RAMP INSTL-CENTRAL VFAPE3 001
used on 002A, 002B, 002C, 002D, 002E, 002F, 002G,
002H, 002J, 002K, 002L, 002M, 002N, 002P, 002Q,
002R, 002S, 002T, 002U, 002V, 002W, 002X
SEE 52-81-14-05F FOR DET
01F 090A D5288010000074 . COVER ASSY VFAPE3 001
used on 001A, 001B, 001D, 001M, 001N, 001Q
SEE 52-81-14-060 FOR DET
01F 090B D5288010000074 . COVER ASSY VFAPE3 001
used on 001C, 001E, 001P, 001R
SEE 52-81-14-060 FOR DET
01F 090C D5288010000074 . COVER ASSY VFAPE3 001
used on 001F, 001G, 001H, 001J, 001S, 001T, 001U,
001V
SEE 52-81-14-06A FOR DET
01F 090D D5288010000074 . COVER ASSY VFAPE3 001
used on 001K, 001L, 001W, 001X
SEE 52-81-14-06A FOR DET
01F 100A D5288010000174 . COVER ASSY VFAPE3 001
used on 002A, 002B, 002D, 002M, 002N, 002Q
SEE 52-81-14-060 FOR DET
01F 100B D5288010000174 . COVER ASSY VFAPE3 001
used on 002C, 002E, 002P, 002R
SEE 52-81-14-060 FOR DET
01F 100C D5288010000174 . COVER ASSY VFAPE3 001
used on 002F, 002G, 002H, 002J, 002S, 002T, 002U,
002V
SEE 52-81-14-06A FOR DET
01F 100D D5288010000174 . COVER ASSY VFAPE3 001
used on 002K, 002L, 002W, 002X
SEE 52-81-14-06A FOR DET
01F 110A D5288010000068 . FITTING INSTL-REAR VFAPE3 001
used on 001A, 001M
SEE 52-81-14-070 FOR DET
- ITEM NOT ILLUSTRATED

Page 10001F-5
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01F 110B D5288010000068 . FITTING INSTL-REAR VFAPE3 001
used on 001B, 001C, 001D, 001E, 001F, 001G, 001H,
001J, 001K, 001L, 001N, 001P, 001Q, 001R, 001S,
001T, 001U, 001V, 001W, 001X
SEE 52-81-14-070 FOR DET
01F 120A D5288010000168 . FITTING INSTL-REAR VFAPE3 001
used on 002A, 002M
SEE 52-81-14-070 FOR DET
01F 120B D5288010000168 . FITTING INSTL-REAR VFAPE3 001
used on 002B, 002C, 002D, 002E, 002F, 002G, 002H,
002J, 002K, 002L, 002N, 002P, 002Q, 002R, 002S,
002T, 002U, 002V, 002W, 002X
SEE 52-81-14-070 FOR DET
01F - 130A D5288010700000 . BOLT ASSY VFAPE3 001
used on 001A, 001M, 002A, 002M
01F - 130B D5288010700000 . BOLT ASSY VFAPE3 001
used on 001B, 001C, 001D, 001E, 001F, 001G, 001H,
001J, 001K, 001L, 001N, 001P, 001Q, 001R, 001S,
001T, 001U, 001V, 001W, 001X, 002B, 002C, 002D,
002E, 002F, 002G, 002H, 002J, 002K, 002L, 002N,
002P, 002Q, 002R, 002S, 002T, 002U, 002V, 002W,
002X
01F - 140A MS24665-300 .. PIN-COTTER V96906 001
Optional Vendor Code 58009, 65029, 73145, 84114,
8K160
used on 130A, 130B
01F - 150A NSA5059-8 .. NUT VF6198 001
OPT TO H53173-8 15653
OPT TO MS14145L8 96906
OPT TO RMTE9868-8 72962
OPT TO THCR358M F0224
Optional Vendor Code 04795, 15653, 2N935, 56878,
A3856, C5543, F0224, FAWT4
used on 130A, 130B
01F - 160A NSA5305-8 .. WASHER VF6198 001
Optional Vendor Code 04795, 10630, 2N935, 58009,
C5543, F2094, F7395, F7756
used on 130A, 130B
01F - 170A D5288014020000 .. SPACER VFAPE3 001
used on 130A, 130B
01F - 180A D5288014120000 .. BOLT VFAPE3 001
used on 130A, 130B
- ITEM NOT ILLUSTRATED

Page 10001F-6
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01F - 180B D5288014120200 .. BOLT VFAPE3 001
used on 130A, 130B
01F - 190A NSA9117M5S . PLATE-IDENTIFICATION VF6198 001
Optional Vendor Code 04795, 2N935, C5543, DM395,
F8421, FA3K5, K1484
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J, 001K, 001L, 001M, 001N, 001P, 001Q,
001R, 001S, 001T, 001U, 001V, 001W, 001X, 002A,
002B, 002C, 002D, 002E, 002F, 002G, 002H, 002J,
002K, 002L, 002M, 002N, 002P, 002Q, 002R, 002S,
002T, 002U, 002V, 002W, 002X
01F - 200A ABS0214-3-3 . RIVET VFAPE3 002
OPT TO CSR902B3W03 11815
OPT TO CSR902T3W3 11815
Optional Vendor Code 04795, 11815, 2N935, 53551,
C5543, F0095
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J, 001K, 001L, 001M, 001N, 001P, 001Q,
001R, 001S, 001T, 001U, 001V, 001W, 001X, 002A,
002B, 002C, 002D, 002E, 002F, 002G, 002H, 002J,
002K, 002L, 002M, 002N, 002P, 002Q, 002R, 002S,
002T, 002U, 002V, 002W, 002X
01F 210A D5288000800078 . PODGER INSTL VFAPE3 001
used on 001A, 001B, 001C, 001D, 001E, 001F, 001G,
001H, 001J, 001K, 001L, 001M, 001N, 001P, 001Q,
001R, 001S, 001T, 001U, 001V, 001W, 001X
SEE 52-81-14-080 FOR DET
01F 220A D5288000800178 . PODGER INSTL VFAPE3 001
used on 002A, 002B, 002C, 002D, 002E, 002F, 002G,
002H, 002J, 002K, 002L, 002M, 002N, 002P, 002Q,
002R, 002S, 002T, 002U, 002V, 002W, 002X
SEE 52-81-14-080 FOR DET
- ITEM NOT ILLUSTRATED

Page 10001F-7
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

10
190 20 240
30 150 280
290
A 160

10 50
20
30 240 40
250
260

300 240
310
320
270
330

360
180 x12
340
(350)

170 x12
190 x12 200
(210)

180 x7
10 x18
20 x18
30 x18
190 x6

170 x7

410
(420)

A 220
230

F_PL_528114_02_0_01_03

FITTING INSTL-FORWARD
Figure 02 / FIGURE-52-81-14-950-802-01

Page 10002-0
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
02 - 001A D5288010000063 FITTING INSTL-FORWARD VFAPE3 RF
used on 010A (528114010), 010A (52811401A), 010A
(52811401C), 010A (52811401D), 010A (52811401F)
SEE 52-81-14-010 FOR NHA, SEE 52-81-14-01A FOR
NHA, SEE 52-81-14-01C FOR NHA, SEE
52-81-14-01D FOR NHA, SEE 52-81-14-01F FOR NHA
02 - 001B D5288010000066 FITTING INSTL-FORWARD VFAPE3 RF
used on 010B (528114010), 010B (52811401A), 010A
(52811401B), 010B (52811401C), 010B (52811401D),
010A (52811401E), 010B (52811401F)
SEE 52-81-14-010 FOR NHA, SEE 52-81-14-01A FOR
NHA, SEE 52-81-14-01B FOR NHA, SEE
52-81-14-01C FOR NHA, SEE 52-81-14-01D FOR
NHA, SEE 52-81-14-01E FOR NHA, SEE 52-81-14-01F
FOR NHA
02 - 002A D5288010000163 FITTING INSTL-FORWARD VFAPE3 RF
used on 020A (528114010), 020A (52811401A), 020A
(52811401C), 020A (52811401D), 020A (52811401F)
SEE 52-81-14-010 FOR NHA, SEE 52-81-14-01A FOR
NHA, SEE 52-81-14-01C FOR NHA, SEE
52-81-14-01D FOR NHA, SEE 52-81-14-01F FOR NHA
02 - 002B D5288010000166 FITTING INSTL-FORWARD VFAPE3 RF
used on 020B (528114010), 020B (52811401A), 020A
(52811401B), 020B (52811401C), 020B (52811401D),
020A (52811401E), 020B (52811401F)
SEE 52-81-14-010 FOR NHA, SEE 52-81-14-01A FOR
NHA, SEE 52-81-14-01B FOR NHA, SEE
52-81-14-01C FOR NHA, SEE 52-81-14-01D FOR
NHA, SEE 52-81-14-01E FOR NHA, SEE 52-81-14-01F
FOR NHA
02 010A MS24665-151 . PIN-COTTER V96906 022
Optional Vendor Code 10630, 65029, 73145, 84114,
8K160
used on 001A, 001B, 002A, 002B
02 020A NSA5060C4 . NUT VF6198 022
OPT TO E9925-4 72962
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 001A, 001B, 002A, 002B
02 030A AN960C416L . WASHER V88044 022
NAS1149C0432R 80205
- ITEM NOT ILLUSTRATED

Page 10002-1
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
OPT TO ASNA2397C416L F6198
Optional Vendor Code 10630, 58009
used on 001A, 001B, 002A, 002B
02 040A NAS6704DU1 . BOLT V80205 001
Optional Vendor Code 0ZC92, 1ER65, 1RC86, 62384,
8Z507, F7411, FAWT4, K8753, T0802
used on 001A, 001B, 002A, 002B
02 050A ABS0394G210 . STRAP-BONDING VFAPE3 001
Optional Vendor Code 04795, 2N935, C5543, C5973,
D7103, D8518, F4291
used on 001A, 001B, 002A, 002B
02 150A NAS6704DU5 . BOLT V80205 001
Optional Vendor Code 1ER65, 1RC86, 62384, 8Z507,
F7411, FAWT4, K8753, T0802
used on 001A, 001B, 002A, 002B
02 160A D5288014820000 . PROFILE VFAPE3 001
used on 001A, 001B, 002A, 002B
02 170A NAS6704HU23 . BOLT V80205 019
Optional Vendor Code 0ZC92, 1ER65, 1RC86, 8Z507,
F7411, FAWT4, K8753, T0802
used on 001A, 001B, 002A, 002B
02 180A D5288013120000 . INSERT VFAPE3 019
used on 001A, 001B, 002A, 002B
02 190A NAS1154V6D . SCREW V80205 020
Optional Vendor Code 0RFT4, F7411, FAWT4, K8753
used on 001A, 001B, 002A, 002B
02 200A D5288010200000 . FITTING ASSY-FWD,MLG VFAPE3 001
used on 001A, 001B
02 210A D5288010200100 . FITTING ASSY-FWD,MLG VFAPE3 001
used on 002A, 002B
02 220A D5288012320000 .. BUSH-SHOULDERED VFAPE3 001
MODIFIED FROM D5288012320001 MADE BY
FAPE3
used on 200A, 210A
02 230A D5288012420000 .. BUSH-SHOULDERED VFAPE3 001
used on 200A, 210A
02 240A MS24665-151 .. PIN-COTTER V96906 005
Optional Vendor Code 10630, 65029, 73145, 84114,
8K160
used on 200A, 210A
- ITEM NOT ILLUSTRATED

Page 10002-2
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
02 250A NSA5060C4 .. NUT VF6198 001
OPT TO E9925-4 72962
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 200A, 210A
02 260A AN960XC416 .. WASHER V88044 001
NAS1149C0463B 80205
Optional Vendor Code 10630, 58009
used on 200A, 210A
02 270A NAS6704DU10 .. BOLT V80205 001
Optional Vendor Code 1ER65, 1RC86, 62384, 8Z507,
F7411, FAWT4, K8753, T0802
used on 200A, 210A
02 280A NSA5060C5 .. NUT VF6198 002
OPT TO E9925-5 72962
OPT TO PHCR55 F0224
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 200A, 210A
02 290A AN960XC516L .. WASHER V88044 002
NAS1149C0532B 80205
Optional Vendor Code 10630, 58009
used on 200A, 210A
02 300A NAS6705DU11 .. BOLT V80205 002
Optional Vendor Code 06725, 0RFT4, 0ZC92, 1ER65,
1RC86, 58845, 62384, 8Z507, F7411, FAWT4, K8753
used on 200A, 210A
02 310A NSA5060C6 .. NUT VF5442 002
OPT TO E9925-6 72962
OPT TO PHCR56 F0224
Optional Vendor Code 04795, 2N935, C5543, F0224
used on 200A, 210A
02 320A AN960X616 .. WASHER V88044 002
used on 200A, 210A
02 330A NAS6706DU10 .. SCREW V80205 002
Optional Vendor Code 0ZC92, 1ER65, 8Z507, F7411,
FAWT4, K8753
used on 200A, 210A
02 340A D5288011800000 .. HINGE ASSY VFAPE3 001
used on 200A
02 350A D5288011800100 .. HINGE ASSY VFAPE3 001
used on 210A
- ITEM NOT ILLUSTRATED

Page 10002-3
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
02 360A MS21230-10 ... BEARING V96906 001
OPT TO BSH20ATC38ZM K0018
OPT TO KWB7N7 97613
OPT TO NSA8137-10 F6198
Optional Vendor Code D3279, F0222, K5269, S0352,
SS822
used on 340A, 350A
02 410A D5288020520000 . REINFORCEMENT VFAPE3 001
used on 001A, 001B
02 420A D5288020520100 . REINFORCEMENT VFAPE3 001
used on 002A, 002B
- ITEM NOT ILLUSTRATED

Page 10002-4
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

430
(440)
10
190 20 510
A 30 150 550
160 560

10 50
20
30 510 40
520
530

570 510
540 580
590
600
180 x12
630
610
(620)

770 190 x14

780 760
700
740 820 170 x12
(830)
480
(490)
710
750

180 10 x14
20 x14
470 30 x14
460
740
770

730 170
810

800 450 x6
495 500

680
(690)

720
A 410
790 (420)
710

F_PL_528114_02_A_01_04

FITTING INSTL-FORWARD
Figure 02A / FIGURE-52-81-14-950-802-A01

Page 10002A-0
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
02A - 001A D5288010000066 FITTING INSTL-FORWARD VFAPE3 RF
POST SB 52-1022
used on 010C (528114010), 010C (52811401A), 010B
(52811401B), 010C (52811401C), 010C (52811401D),
010B (52811401E), 010C (52811401F)
SEE 52-81-14-010 FOR NHA, SEE 52-81-14-01A FOR
NHA, SEE 52-81-14-01B FOR NHA, SEE
52-81-14-01C FOR NHA, SEE 52-81-14-01D FOR
NHA, SEE 52-81-14-01E FOR NHA, SEE 52-81-14-01F
FOR NHA
02A - 002A D5288010000166 FITTING INSTL-FORWARD VFAPE3 RF
POST SB 52-1022
used on 020C (528114010), 020C (52811401A), 020B
(52811401B), 020C (52811401C), 020C (52811401D),
020B (52811401E), 020C (52811401F)
SEE 52-81-14-010 FOR NHA, SEE 52-81-14-01A FOR
NHA, SEE 52-81-14-01B FOR NHA, SEE
52-81-14-01C FOR NHA, SEE 52-81-14-01D FOR
NHA, SEE 52-81-14-01E FOR NHA, SEE 52-81-14-01F
FOR NHA
02A 010A MS24665-151 . PIN-COTTER V96906 018
Optional Vendor Code 10630, 65029, 73145, 84114,
8K160
used on 001A, 002A
02A 020A NSA5060C4 . NUT VF6198 018
OPT TO E9925-4 72962
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 001A, 002A
02A 030A AN960C416L . WASHER V88044 018
NAS1149C0432R 80205
OPT TO ASNA2397C416L F6198
Optional Vendor Code 10630, 58009
used on 001A, 002A
02A 040A NAS6704DU1 . BOLT V80205 001
Optional Vendor Code 0ZC92, 1ER65, 1RC86, 62384,
8Z507, F7411, FAWT4, K8753, T0802
used on 001A, 002A
02A 050A ABS0394G210 . STRAP-BONDING VFAPE3 001
Optional Vendor Code 04795, 2N935, C5543, C5973,
D7103, D8518, F4291
used on 001A, 002A
- ITEM NOT ILLUSTRATED

Page 10002A-1
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
02A 150A NAS6704DU5 . BOLT V80205 001
Optional Vendor Code 1ER65, 1RC86, 62384, 8Z507,
F7411, FAWT4, K8753, T0802
used on 001A, 002A
02A 160A D5288014820000 . PROFILE VFAPE3 001
used on 001A, 002A
02A 170A NAS6704HU23 . BOLT V80205 019
Optional Vendor Code 0ZC92, 1ER65, 1RC86, 8Z507,
F7411, FAWT4, K8753, T0802
used on 001A, 002A
02A 180A D5288013120000 . INSERT VFAPE3 019
used on 001A, 002A
02A 190A NAS1154V6D . SCREW V80205 016
Optional Vendor Code 0RFT4, F7411, FAWT4, K8753
used on 001A, 002A
02A 410A D5288020520000 . REINFORCEMENT VFAPE3 001
used on 001A
02A 420A D5288020520100 . REINFORCEMENT VFAPE3 001
used on 002A
02A 430A D5288022000000 . FITTING ASSY-FORWARD VFAPE3 001
used on 001A
02A 440A D5288022000100 . FITTING ASSY-FORWARD VFAPE3 001
used on 002A
02A 450A ABS0258-8B .. COLLAR VFAPE3 006
Optional Vendor Code 04795, 2N935, 56878, 5M902,
73197, C5543
used on 430A, 440A
02A 460A ABS0251-8-4 .. FASTENER-HI-LOK VFAPE3 003
DAN6-8-4 D8518
Optional Vendor Code 04795, 2N935, 56878, 73197,
C5543
used on 430A, 440A
02A 470A ABS0251-8-5 .. FASTENER-HI-LOK VFAPE3 003
DAN6-8-5 D8518
OPT TO HL11VBJ8-5 73197
Optional Vendor Code 04795, 2N935, 56878, 73197,
C5543
used on 430A, 440A
02A 480A D5288010200000 .. FITTING ASSY-FWD,MLG VFAPE3 001
used on 430A
02A 490A D5288010200100 .. FITTING ASSY-FWD,MLG VFAPE3 001
used on 440A
- ITEM NOT ILLUSTRATED

Page 10002A-2
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
02A 495A D5288012320000 ... BUSH-SHOULDERED VFAPE3 001
MODIFIED FROM D5288012320001 MADE BY
FAPE3
used on 480A, 490A
02A 500A D5288012420000 ... BUSH-SHOULDERED VFAPE3 001
used on 480A, 490A
02A 510A MS24665-151 ... PIN-COTTER V96906 005
Optional Vendor Code 10630, 65029, 73145, 84114,
8K160
used on 480A, 490A
02A 520A NSA5060C4 ... NUT VF6198 001
OPT TO E9925-4 72962
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 480A, 490A
02A 530A AN960XC416 ... WASHER V88044 001
NAS1149C0463B 80205
Optional Vendor Code 10630, 58009
used on 480A, 490A
02A 540A NAS6704DU10 ... BOLT V80205 001
Optional Vendor Code 1ER65, 1RC86, 62384, 8Z507,
F7411, FAWT4, K8753, T0802
used on 480A, 490A
02A 550A NSA5060C5 ... NUT VF6198 002
OPT TO E9925-5 72962
OPT TO PHCR55 F0224
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 480A, 490A
02A 560A AN960XC516L ... WASHER V88044 002
NAS1149C0532B 80205
Optional Vendor Code 10630, 58009
used on 480A, 490A
02A 570A NAS6705DU11 ... BOLT V80205 002
Optional Vendor Code 06725, 0RFT4, 0ZC92, 1ER65,
1RC86, 58845, 62384, 8Z507, F7411, FAWT4, K8753
used on 480A, 490A
02A 580A NSA5060C6 ... NUT VF5442 002
OPT TO E9925-6 72962
OPT TO PHCR56 F0224
Optional Vendor Code 04795, 2N935, C5543, F0224
used on 480A, 490A
- ITEM NOT ILLUSTRATED

Page 10002A-3
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
02A 590A AN960XC616 ... WASHER V88044 002
NAS1149C0663R 80205
Optional Vendor Code 10630, 58009
used on 480A, 490A
02A 600A NAS6706DU10 ... SCREW V80205 002
Optional Vendor Code 0ZC92, 1ER65, 8Z507, F7411,
FAWT4, K8753
used on 480A, 490A
02A 610A D5288011800000 ... HINGE ASSY VFAPE3 001
used on 480A
02A 620A D5288011800100 ... HINGE ASSY VFAPE3 001
used on 490A
02A 630A MS21230-10 .... BEARING V96906 001
OPT TO BSH20ATC38ZM K0018
OPT TO KWB7N7 97613
OPT TO NSA8137-10 F6198
Optional Vendor Code D3279, F0222, K5269, S0352,
SS822
used on 610A, 620A
02A 680A D5288022120000 .. FITTING VFAPE3 001
used on 430A
02A 690A D5288022120100 .. FITTING VFAPE3 001
used on 440A
02A 700A D5288113520000 . INSERT VFAPE3 006
used on 001A, 002A
02A 710A NAS1726C4P . NUT V80205 013
OPT TO DHR905-4P F0224
Optional Vendor Code 15653, 27238, 66776, F0224,
FAWT4
used on 001A, 002A
02A 720A ASNA2027V4-5 . BOLT VF6198 003
ASNA2009V4-5 F6198
OPT TO HST756JB8-5 73197
Optional Vendor Code 04795, 2N935, C4293, C5543,
F0236, K5673, U6300
used on 001A, 002A
02A 730A ASNA2027V4-7 . BOLT VF6198 002
EN6115V4-7 I9005
OPT TO HST756JB8-7 73197
Optional Vendor Code 04795, 2N935, C4293, C5543,
F0236, K5673
used on 001A, 002A
- ITEM NOT ILLUSTRATED

Page 10002A-4
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
02A 740A ASNA2027V4-8 . BOLT VF6198 004
ASNA2009V4-8 F6198
OPT TO HST756JB8-8 73197
Optional Vendor Code 04795, 2N935, C4293, C5543,
F0236, K5673, U6300
used on 001A, 002A
02A 750A ASNA2027V4-10 . BOLT VF6198 004
EN6115V4-10 I9005
OPT TO HST756JB8-10 73197
Optional Vendor Code 04795, 2N935, C4293, C5543,
F0236, K5673
used on 001A, 002A
02A 760A ABS0256-5-200 . BOLT-BLIND VFAPE3 022
OPT TO ABS0256-5-200Y FAPE3
OPT TO ABS0256-5-200Z FAPE3
OPT TO MBF2112S5-200 98524
Optional Vendor Code 04795, 2N935, 98524, C5543
used on 001A, 002A
02A 770A ABS0256-5-250 . BOLT VFAPE3 003
OPT TO ABS0256-5-250Z FAPE3
OPT TO MBF2012S5-250 98524
OPT TO MBF2112S5-250 92215
Optional Vendor Code 04795, 2N935, 98524, C5543
used on 001A, 002A
02A 780A ABS0256-5-300 . BOLT-BLIND VFAPE3 009
OPT TO ABS0256-5-300Z FAPE3
OPT TO MBF2012S5-300 98524
OPT TO MBF2112S5-300 98524
Optional Vendor Code 04795, 2N935, 98524, C5543
used on 001A, 002A
02A 790A ABS0258-5A . COLLAR VFAPE3 029
OPT TO HL94TB5 92215
Optional Vendor Code 04795, 2N935, 56878, 5M902,
73197, C5543, K5673, SBF11, U6300
used on 001A, 002A
02A 800A ABS0251-5-4 . FASTENER-HI-LOK VFAPE3 007
DAN6-5-4 D8518
OPT TO HL11VBJ5-4 92215
Optional Vendor Code 04795, 2N935, 56878, 73197,
C5543
used on 001A, 002A
- ITEM NOT ILLUSTRATED

Page 10002A-5
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
02A 810A ABS0251-5-5 . FASTENER-HI-LOK VFAPE3 022
DAN6-5-5 D8518
OPT TO HL11VBJ5-5 92215
Optional Vendor Code 04795, 2N935, 56878, 73197,
C5543
used on 001A, 002A
02A 820A D5288022220000 . PLATE VFAPE3 001
used on 001A
02A 830A D5288022220100 . PLATE VFAPE3 001
used on 002A
- ITEM NOT ILLUSTRATED

Page 10002A-6
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

10
280 20
30 290
190 50
A 40

270

240
250
340 360 260
(350)

300
180 x12

715 820
(830)
705
190 x14
735 410 170 x12
190 180
(420)
775 200
(210)
765
170 x7
10
20
30
695 x12
755

755

725

230
745 220

A 695
F_PL_528114_02_B_01_03

FITTING INSTL-FORWARD
Figure 02B / FIGURE-52-81-14-950-802-B01

Page 10002B-0
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
02B - 001A D5288010000066 FITTING INSTL-FORWARD VFAPE3 RF
POST SB 52-1073
used on 010D (528114010), 010D (52811401A), 010C
(52811401B), 010D (52811401C), 010D (52811401D),
010C (52811401E), 010D (52811401F)
SEE 52-81-14-010 FOR NHA, SEE 52-81-14-01A FOR
NHA, SEE 52-81-14-01B FOR NHA, SEE
52-81-14-01C FOR NHA, SEE 52-81-14-01D FOR
NHA, SEE 52-81-14-01E FOR NHA, SEE 52-81-14-01F
FOR NHA
02B - 002A D5288010000166 FITTING INSTL-FORWARD VFAPE3 RF
POST SB 52-1073
used on 020D (528114010), 020D (52811401A), 020C
(52811401B), 020D (52811401C), 020D (52811401D),
020C (52811401E), 020D (52811401F)
SEE 52-81-14-010 FOR NHA, SEE 52-81-14-01A FOR
NHA, SEE 52-81-14-01B FOR NHA, SEE
52-81-14-01C FOR NHA, SEE 52-81-14-01D FOR
NHA, SEE 52-81-14-01E FOR NHA, SEE 52-81-14-01F
FOR NHA
02B 010A MS24665-151 . PIN-COTTER V96906 018
POST SB 52-1073
Optional Vendor Code 10630, 65029, 73145, 84114,
8K160
used on 001A, 002A
02B 020A NSA5060C4 . NUT VF6198 018
POST SB 52-1073
OPT TO E9925-4 72962
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 001A, 002A
02B 030A AN960C416L . WASHER V88044 018
POST SB 52-1073
NAS1149C0432R 80205
OPT TO ASNA2397C416L F6198
Optional Vendor Code 10630, 58009
used on 001A, 002A
02B 040A NAS6704DU1 . BOLT V80205 001
Optional Vendor Code 0ZC92, 1ER65, 1RC86, 62384,
8Z507, F7411, FAWT4, K8753, T0802
used on 001A, 002A
- ITEM NOT ILLUSTRATED

Page 10002B-1
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
02B 050A ABS0394G210 . STRAP-BONDING VFAPE3 001
Optional Vendor Code 04795, 2N935, C5543, C5973,
D7103, D8518, F4291
used on 001A, 002A
02B 170A NAS6704HU23 . BOLT V80205 019
POST SB 52-1073
Optional Vendor Code 0ZC92, 1ER65, 1RC86, 8Z507,
F7411, FAWT4, K8753, T0802
used on 001A, 002A
02B 180A D5288013120000 . INSERT VFAPE3 013
used on 001A, 002A
02B 190A NAS1154V6D . SCREW V80205 017
POST SB 52-1073
Optional Vendor Code 0RFT4, F7411, FAWT4, K8753
used on 001A, 002A
02B 200A D5288024600001 . FITTING ASSY-FWD,MLG VFAPE3 001
POST SB 52-1073
used on 001A
02B 210A D5288024600101 . FITTING ASSY-FWD,MLG VFAPE3 001
used on 002A
02B 220A D5288012320000 .. BUSH-SHOULDERED VFAPE3 001
MODIFIED FROM D5288012320001 MADE BY
FAPE3
used on 200A, 210A
02B 230A D5288012420000 .. BUSH-SHOULDERED VFAPE3 001
used on 200A, 210A
02B 240A MS24665-151 .. PIN-COTTER V96906 005
Optional Vendor Code 10630, 65029, 73145, 84114,
8K160
used on 200A, 210A
02B 250A AN960C616 .. WASHER V88044 005
NAS1149C0663R 80205
OPT TO ASNA2397C616 F6198
Optional Vendor Code 10630, 58009
used on 200A, 210A
02B 260A NSA5060C6 .. NUT VF5442 005
OPT TO E9925-6 72962
OPT TO PHCR56 F0224
Optional Vendor Code 04795, 2N935, C5543, F0224
used on 200A, 210A
- ITEM NOT ILLUSTRATED

Page 10002B-2
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
02B 270A NAS6706DU12 .. BOLT V80205 001
Optional Vendor Code 0ZC92, 1ER65, 8Z507, F7411,
FAWT4, K8753
used on 200A, 210A
02B 280A ABS0214-4-4 .. RIVET VFAPE3 001
OPT TO CSR902B4W04 11815
OPT TO CSR902B4W4 11815
OPT TO CSR902T4W4 11815
Optional Vendor Code 04795, 11815, 2N935, 53551,
C5543
used on 200A, 210A
02B 290A D5288023920000 .. PROFILE VFAPE3 001
used on 200A, 210A
02B 300A NAS6706DU11 .. BOLT V80205 004
Optional Vendor Code 1ER65, 8Z507, F7411, FAWT4,
K8753
used on 200A, 210A
02B 340A D5288023700201 .. HINGE ASSY VFAPE3 001
used on 200A
02B 350A D5288023700301 .. HINGE ASSY VFAPE3 001
used on 210A
02B 360A MS21230-10 ... BEARING V96906 001
OPT TO BSH20ATC38ZM K0018
OPT TO KWB7N7 97613
OPT TO NSA8137-10 F6198
Optional Vendor Code D3279, F0222, K5269, S0352,
SS822
used on 340A, 350A
02B 410A D5288020520000 . REINFORCEMENT VFAPE3 001
used on 001A
02B 420A D5288020520100 . REINFORCEMENT VFAPE3 001
used on 002A
02B 695A ABS0259-8A . COLLAR-HI-LOK VFAPE3 013
POST SB 52-1073
OPT TO HL175-8AWU 92215
Optional Vendor Code 04795, 2N935, 56878, 5M902,
73197, C5543
used on 001A, 002A
02B 705A D5288113520000 . INSERT VFAPE3 006
used on 001A, 002A
- ITEM NOT ILLUSTRATED

Page 10002B-3
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
02B 715A ABS0257-5-300 . RIVET VFAPE3 015
OPT TO ABS0257-5-300Z FAPE3
OPT TO MBF2013S5-300 98524
OPT TO MBF2113S5-300 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 002A
02B 725A DAN7-8-6 . PIN-RIVET VD8518 003
POST SB 52-1073
HL1012VF8-6 73197
OPT TO HL12VDF8-6 92215
Optional Vendor Code 04795, 06725, 2N935, 56878,
73197, C4293, C5543, K5673, U6300
used on 001A, 002A
02B 735A DAN7-8-8 . PIN-RIVET VD8518 005
POST SB 52-1073
HL1012VF8-8 73197
OPT TO HL12VDF8-8 92215
Optional Vendor Code 04795, 06725, 2N935, 56878,
73197, C4293, C5543, K5673, U6300
used on 001A, 002A
02B 745A DAN7-8-3 . PIN-RIVET VD8518 001
POST SB 52-1073
HL1012VF8-3 73197
OPT TO HL12VDF8-3 92215
Optional Vendor Code 04795, 06725, 2N935, 56878,
73197, C4293, C5543, K5673, U6300
used on 001A, 002A
02B 755A DAN7-8-7 . PIN-RIVET VD8518 004
MODIFIED FROM HL12VF8-7 MADE BY 92215
POST SB 52-1073
HL1012VF8-7 73197
OPT TO HL12VDF8-7 92215
Optional Vendor Code 04795, 06725, 17446, 2N935,
56878, 73197, C4293, C5543, K5673, U6300
used on 001A, 002A
02B 765A ABS0259-5A . COLLAR-HI-LOK VFAPE3 015
OPT TO HL175-5AWU 92215
Optional Vendor Code 04795, 2N935, 56878, 5M902,
73197, C4293, C5543, K5673
used on 001A, 002A
02B 775A ABS0251-5-5 . FASTENER-HI-LOK VFAPE3 015
DAN6-5-5 D8518
- ITEM NOT ILLUSTRATED

Page 10002B-4
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
OPT TO HL11VBJ5-5 92215
Optional Vendor Code 04795, 2N935, 56878, 73197,
C5543
used on 001A, 002A
02B 820A D5288022720000 . PLATE VFAPE3 001
used on 001A
02B 830A D5288022720100 . PLATE VFAPE3 001
used on 002A
- ITEM NOT ILLUSTRATED

Page 10002B-5
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

B
C 40
120 x4
10
290 x4 320
300 x4 210

330
240
120
20 130
140 50
270 280
250
B 30
220 340
310 x4 90
200
150
170 60 110
A 180
190 230 100
20 60 110
160 70 260
80

A
20

350

360

380

370
360

B
TYPICAL 400

390

F_PL_528114_03_0_01_01

UPLOCK AND STEP ASSY

Figure 03 / FIGURE-52-81-14-950-803-01

Page 10003-0
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
03 - 001A D5288010000073 UPLOCK AND STEP ASSY VFAPE3 RF
used on 030A (528114010), 030A (52811401A), 030A
(52811401B), 030A (52811401F)
SEE 52-81-14-010 FOR NHA, SEE 52-81-14-01A FOR
NHA, SEE 52-81-14-01B FOR NHA, SEE 52-81-14-01F
FOR NHA
03 - 002A D5288010000173 UPLOCK AND STEP ASSY VFAPE3 RF
used on 040A (528114010), 040A (52811401A), 040A
(52811401B)
SEE 52-81-14-010 FOR NHA, SEE 52-81-14-01A FOR
NHA, SEE 52-81-14-01B FOR NHA
03 010A NAS6704HU22 . BOLT V80205 010
Optional Vendor Code 0ZC92, 1ER65, 1RC86, 8Z507,
F7411, K8753, T0802
used on 001A, 002A
03 020A D5288013120000 . INSERT VFAPE3 030
used on 001A, 002A
03 030A D5288020220000 . PLATE-FLUTED VFAPE3 001
MODIFIED FROM D5288020220001 MADE BY
FAPE3
MODIFIED FROM D5288020220002 MADE BY
FAPE3
used on 001A, 002A
03 040A D5288010800000 . UPLOCK ASSY VFAPE3 001
MODIFIED FROM D5288010800051 MADE BY
FAPE3
used on 001A, 002A
03 050A MS15001-1 .. FITTING-LUBRICATION V96906 001
AS15001-1 81343
AS15001-1P 81343
Optional Vendor Code 0FKM1, 13899, 52930, 57336,
59736
used on 040A
03 060A MS24665-302 .. PIN-COTTER V96906 002
Optional Vendor Code 58009, 65029, 73145, 84114,
8K160
used on 040A
03 070A NSA5060-7 .. NUT VF6198 001
OPT TO RME9868-7 72962
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 040A
- ITEM NOT ILLUSTRATED

Page 10003-1
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
03 080A AN960-716L .. WASHER V88044 001
NAS1149F0732P 80205
OPT TO ASNA2397-716L F6198
Optional Vendor Code 10630, 58009
used on 040A
03 090A A5283005520200 .. BOLT VFAPE3 001
used on 040A
03 100A A5283005620200 .. ROLLER VFAPE3 001
used on 040A
03 110A A5283005720200 .. BUSH VFAPE3 002
used on 040A
03 120A MS24665-153 .. PIN-COTTER V96906 006
Optional Vendor Code 04795, 06329, 2N935, 60996,
84114, 8K160, C5543
used on 040A
03 130A NSA5059-4 .. NUT VF6198 002
OPT TO H53173-4 15653
OPT TO RMTE9868-4 72962
OPT TO THCR354M F0224
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 040A
03 140A AN960-416L .. WASHER V88044 002
NAS1149F0432P 80205
OPT TO ASNA2397-416L F6198
Optional Vendor Code 10630, 58009, 8K160, F8982
used on 040A
03 150A NAS1154-5D .. SCREW V80205 001
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, F7411,
FAWT4, K8753
used on 040A
03 160A A5283006420200 .. SCREW VFAPE3 001
MODIFIED FROM A5283006420201 MADE BY
FAPE3
used on 040A
03 170A MS24665-151 .. PIN-COTTER V96906 002
Optional Vendor Code 10630, 65029, 73145, 84114,
8K160
used on 040A
03 180A NSA5059-3 .. NUT VF6198 002
OPT TO H53173-3 15653
OPT TO RMTE9868-3 72962
OPT TO THCR353M F0224
- ITEM NOT ILLUSTRATED

Page 10003-2
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 040A
03 190A AN960-10L .. WASHER V88044 002
NAS1149F0332P 80205
OPT TO ASNA2397-10L F6198
Optional Vendor Code 10630, 58009, 8K160, F8982
used on 040A
03 200A NAS1153-8D .. SCREW V80205 001
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, F7411,
FAWT4, K8753
used on 040A
03 210A A5281008720000 .. PIN VFAPE3 001
MODIFIED FROM A5281008720001 MADE BY
FAPE3
used on 040A
03 220A A5283006020300 .. CAP-PROTECTIVE VFAPE3 001
used on 040A
03 230A A5283006120000 .. BUSH VFAPE3 001
used on 040A
03 240A A5283005420000 .. SHAFT-TORQUE VFAPE3 001
used on 040A
03 250A A5283005220400 .. SPACER VFAPE3 001
MODIFIED FROM A5283005220401 MADE BY
FAPE3
used on 040A
03 260A A5283005120000 .. FITTING-SIDE VFAPE3 001
used on 040A
03 270A A5283005020000 .. FITTING-SIDE VFAPE3 001
used on 040A
03 280A A5283005820000 .. BUSH VFAPE3 001
used on 040A
03 290A NSA5060-4 .. NUT VF6198 004
OPT TO H53174-4 15653
OPT TO PHCR354M F0224
OPT TO RME9868-4 72962
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 040A
03 300A AN960-416 .. WASHER V88044 004
NAS1149F0463P 80205
OPT TO ASNA2397-416 F6198
- ITEM NOT ILLUSTRATED

Page 10003-3
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
Optional Vendor Code 04795, 06329, 2N935, 60996,
70347, 8K160, C5543
used on 040A
03 310A NAS1304-9D .. BOLT V80205 004
NAS6604D9 80205
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, 62384,
8Z507, F7411, K8753
used on 040A
03 320A D5288020120000 .. FITTING VFAPE3 001
MODIFIED FROM D5288020120001 MADE BY
FAPE3
used on 040A
03 330A D5288012820000 .. PLATE-FLUTED VFAPE3 001
used on 040A
03 340A D5288020020000 .. BASE-MOUNTING VFAPE3 001
used on 040A
03 350A ABS0254-6-250 . BOLT VFAPE3 008
OPT TO MBF2010S6-250 92215
OPT TO MBF2110S6-250 92215
Optional Vendor Code 04795, 2N935, 98524, C4293,
C5543
used on 001A, 002A
03 360A NAS6704HU30 . BOLT V80205 012
Optional Vendor Code 0ZC92, 1ER65, 1RC86, 8Z507,
F7411, K8753, T0802
used on 001A, 002A
03 370A D5288010500000 . STEP ASSY VFAPE3 002
used on 001A, 002A
03 380A D5288013020000 . PROTECTOR VFAPE3 002
used on 001A, 002A
03 390A D5288011700000 . STEP ASSY VFAPE3 001
used on 001A, 002A
03 400A D5288020400000 . PLATE ASSY VFAPE3 001
used on 001A, 002A
- ITEM NOT ILLUSTRATED

Page 10003-4
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

C 40
120 x4
10
290 x4 320
300 x4 210
240
330
120
20 130
140 50
270 280
250
B 30
220 340
310 x4 90
200
150
170 60 110
A 180
190 230 100
20 60 110
160 70 260
80

A
20

350

360

380

370
360

B
400

390

C
TYPICAL
F_PL_528114_03_B_01_01

UPLOCK AND STEP ASSY

Figure 03B / FIGURE-52-81-14-950-803-B01

Page 10003B-0
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
03B - 001A D5288010000075 UPLOCK AND STEP ASSY VFAPE3 RF
used on 030B (528114010), 030B (52811401A)
SEE 52-81-14-010 FOR NHA, SEE 52-81-14-01A FOR
NHA
03B - 001B D5288010000073 UPLOCK AND STEP ASSY VFAPE3 RF
used on 030C (528114010), 030C (52811401A), 030B
(52811401B)
SEE 52-81-14-010 FOR NHA, SEE 52-81-14-01A FOR
NHA, SEE 52-81-14-01B FOR NHA
03B - 002A D5288010000175 UPLOCK AND STEP ASSY VFAPE3 RF
used on 040B (528114010), 040B (52811401A)
SEE 52-81-14-010 FOR NHA, SEE 52-81-14-01A FOR
NHA
03B - 002B D5288010000173 UPLOCK AND STEP ASSY VFAPE3 RF
used on 040C (528114010), 040C (52811401A), 040B
(52811401B)
SEE 52-81-14-010 FOR NHA, SEE 52-81-14-01A FOR
NHA, SEE 52-81-14-01B FOR NHA
03B 010A NAS6704HU22 . BOLT V80205 010
Optional Vendor Code 0ZC92, 1ER65, 1RC86, 8Z507,
F7411, K8753, T0802
used on 001A, 001B, 002A, 002B
03B 020A D5288013120000 . INSERT VFAPE3 026
used on 001A, 001B, 002A, 002B
03B 030A D5288020220000 . PLATE-FLUTED VFAPE3 001
MODIFIED FROM D5288020220001 MADE BY
FAPE3
MODIFIED FROM D5288020220002 MADE BY
FAPE3
used on 001A, 001B, 002A, 002B
03B 040A D5288010800000 . UPLOCK ASSY VFAPE3 001
MODIFIED FROM D5288010800051 MADE BY
FAPE3
used on 001A, 001B, 002A, 002B
03B 050A MS15001-1 .. FITTING-LUBRICATION V96906 001
AS15001-1 81343
AS15001-1P 81343
Optional Vendor Code 0FKM1, 13899, 52930, 57336,
59736
used on 040A
- ITEM NOT ILLUSTRATED

Page 10003B-1
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
03B 060A MS24665-302 .. PIN-COTTER V96906 002
Optional Vendor Code 58009, 65029, 73145, 84114,
8K160
used on 040A
03B 070A NSA5060-7 .. NUT VF6198 001
OPT TO RME9868-7 72962
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 040A
03B 080A AN960-716L .. WASHER V88044 001
NAS1149F0732P 80205
OPT TO ASNA2397-716L F6198
Optional Vendor Code 10630, 58009
used on 040A
03B 090A A5283005520200 .. BOLT VFAPE3 001
used on 040A
03B 100A A5283005620200 .. ROLLER VFAPE3 001
used on 040A
03B 110A A5283005720200 .. BUSH VFAPE3 002
used on 040A
03B 120A MS24665-153 .. PIN-COTTER V96906 006
Optional Vendor Code 04795, 06329, 2N935, 60996,
84114, 8K160, C5543
used on 040A
03B 130A NSA5059-4 .. NUT VF6198 002
OPT TO H53173-4 15653
OPT TO RMTE9868-4 72962
OPT TO THCR354M F0224
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 040A
03B 140A AN960-416L .. WASHER V88044 002
NAS1149F0432P 80205
OPT TO ASNA2397-416L F6198
Optional Vendor Code 10630, 58009, 8K160, F8982
used on 040A
03B 150A NAS1154-5D .. SCREW V80205 001
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, F7411,
FAWT4, K8753
used on 040A
03B 160A A5283006420200 .. SCREW VFAPE3 001
MODIFIED FROM A5283006420201 MADE BY
FAPE3
- ITEM NOT ILLUSTRATED

Page 10003B-2
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 040A
03B 170A MS24665-151 .. PIN-COTTER V96906 002
Optional Vendor Code 10630, 65029, 73145, 84114,
8K160
used on 040A
03B 180A NSA5059-3 .. NUT VF6198 002
OPT TO H53173-3 15653
OPT TO RMTE9868-3 72962
OPT TO THCR353M F0224
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 040A
03B 190A AN960-10L .. WASHER V88044 002
NAS1149F0332P 80205
OPT TO ASNA2397-10L F6198
Optional Vendor Code 10630, 58009, 8K160, F8982
used on 040A
03B 200A NAS1153-8D .. SCREW V80205 001
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, F7411,
FAWT4, K8753
used on 040A
03B 210A A5281008720000 .. PIN VFAPE3 001
MODIFIED FROM A5281008720001 MADE BY
FAPE3
used on 040A
03B 220A A5283006020300 .. CAP-PROTECTIVE VFAPE3 001
used on 040A
03B 230A A5283006120000 .. BUSH VFAPE3 001
used on 040A
03B 240A A5283005420000 .. SHAFT-TORQUE VFAPE3 001
used on 040A
03B 250A A5283005220400 .. SPACER VFAPE3 001
MODIFIED FROM A5283005220401 MADE BY
FAPE3
used on 040A
03B 260A A5283005120000 .. FITTING-SIDE VFAPE3 001
used on 040A
03B 270A A5283005020000 .. FITTING-SIDE VFAPE3 001
used on 040A
03B 280A A5283005820000 .. BUSH VFAPE3 001
used on 040A
- ITEM NOT ILLUSTRATED

Page 10003B-3
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
03B 290A NSA5060-4 .. NUT VF6198 004
OPT TO H53174-4 15653
OPT TO PHCR354M F0224
OPT TO RME9868-4 72962
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 040A
03B 300A AN960-416 .. WASHER V88044 004
NAS1149F0463P 80205
OPT TO ASNA2397-416 F6198
Optional Vendor Code 04795, 06329, 2N935, 60996,
70347, 8K160, C5543
used on 040A
03B 310A NAS1304-9D .. BOLT V80205 004
NAS6604D9 80205
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, 62384,
8Z507, F7411, K8753
used on 040A
03B 320A D5288020120000 .. FITTING VFAPE3 001
MODIFIED FROM D5288020120001 MADE BY
FAPE3
used on 040A
03B 330A D5288012820000 .. PLATE-FLUTED VFAPE3 001
used on 040A
03B 340A D5288020020000 .. BASE-MOUNTING VFAPE3 001
used on 040A
03B 350A ABS0254-6-250 . BOLT VFAPE3 004
OPT TO MBF2010S6-250 92215
OPT TO MBF2110S6-250 92215
Optional Vendor Code 04795, 2N935, 98524, C4293,
C5543
used on 001A, 001B, 002A, 002B
03B 360A NAS6704HU30 . BOLT V80205 012
Optional Vendor Code 0ZC92, 1ER65, 1RC86, 8Z507,
F7411, K8753, T0802
used on 001A, 001B, 002A, 002B
03B 370A D5288010500000 . STEP ASSY VFAPE3 001
used on 001A, 001B, 002A, 002B
03B 380A D5288013020000 . PROTECTOR VFAPE3 001
used on 001A, 001B, 002A, 002B
03B 380B D5288013020200 . PLATE VFAPE3 001
OPT TO D5288021300000 FAPE3
- ITEM NOT ILLUSTRATED

Page 10003B-4
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 001A, 001B, 002A, 002B
03B 390A D5288011700000 . STEP ASSY VFAPE3 002
used on 001A, 001B, 002A, 002B
03B 400A D5288020400000 . PLATE ASSY VFAPE3 002
used on 001A, 001B, 002A, 002B
- ITEM NOT ILLUSTRATED

Page 10003B-5
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

40
D C 10
120 x4
290 x4 320
300 x4 210

330
240
120
20 130
140 50
270 280
250
30
220 340
B 310 x4 90
200
150
170 60 110
A 180
190 230 100
60 110
260
20
A 160 70
80

20

350

360

380
B
370 360
20

360 400

390
410
C

D
F_PL_528114_03_C_01_01

UPLOCK AND STEP ASSY

Figure 03C / FIGURE-52-81-14-950-803-C01

Page 10003C-0
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
03C - 001A D5288010000073 UPLOCK AND STEP ASSY VFAPE3 RF
POST SB 52-1025
used on 030A (52811401C), 030A (52811401D), 030A
(52811401E)
SEE 52-81-14-01C FOR NHA, SEE 52-81-14-01D
FOR NHA, SEE 52-81-14-01E FOR NHA
03C - 002A D5288010000173 UPLOCK AND STEP ASSY VFAPE3 RF
POST SB 52-1025
used on 040A (52811401C), 040A (52811401D), 040A
(52811401E), 040A (52811401F)
SEE 52-81-14-01C FOR NHA, SEE 52-81-14-01D
FOR NHA, SEE 52-81-14-01E FOR NHA, SEE
52-81-14-01F FOR NHA
03C 010A NAS6704HU22 . BOLT V80205 010
Optional Vendor Code 0ZC92, 1ER65, 1RC86, 8Z507,
F7411, K8753, T0802
used on 001A, 002A
03C 020A D5288013120000 . INSERT VFAPE3 026
used on 001A, 002A
03C 030A D5288020220000 . PLATE-FLUTED VFAPE3 001
MODIFIED FROM D5288020220001 MADE BY
FAPE3
MODIFIED FROM D5288020220002 MADE BY
FAPE3
used on 001A, 002A
03C 040A D5288010800000 . UPLOCK ASSY VFAPE3 001
MODIFIED FROM D5288010800051 MADE BY
FAPE3
used on 001A, 002A
03C 050A MS15001-1 .. FITTING-LUBRICATION V96906 001
AS15001-1 81343
AS15001-1P 81343
Optional Vendor Code 0FKM1, 13899, 52930, 57336,
59736
used on 040A
03C 060A MS24665-302 .. PIN-COTTER V96906 002
Optional Vendor Code 58009, 65029, 73145, 84114,
8K160
used on 040A
03C 070A NSA5060-7 .. NUT VF6198 001
OPT TO RME9868-7 72962
- ITEM NOT ILLUSTRATED

Page 10003C-1
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 040A
03C 080A AN960-716L .. WASHER V88044 001
NAS1149F0732P 80205
OPT TO ASNA2397-716L F6198
Optional Vendor Code 10630, 58009
used on 040A
03C 090A A5283005520200 .. BOLT VFAPE3 001
used on 040A
03C 100A A5283005620200 .. ROLLER VFAPE3 001
used on 040A
03C 110A A5283005720200 .. BUSH VFAPE3 002
used on 040A
03C 120A MS24665-153 .. PIN-COTTER V96906 006
Optional Vendor Code 04795, 06329, 2N935, 60996,
84114, 8K160, C5543
used on 040A
03C 130A NSA5059-4 .. NUT VF6198 002
OPT TO H53173-4 15653
OPT TO RMTE9868-4 72962
OPT TO THCR354M F0224
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 040A
03C 140A AN960-416L .. WASHER V88044 002
NAS1149F0432P 80205
OPT TO ASNA2397-416L F6198
Optional Vendor Code 10630, 58009, 8K160, F8982
used on 040A
03C 150A NAS1154-5D .. SCREW V80205 001
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, F7411,
FAWT4, K8753
used on 040A
03C 160A A5283006420200 .. SCREW VFAPE3 001
MODIFIED FROM A5283006420201 MADE BY
FAPE3
used on 040A
03C 170A MS24665-151 .. PIN-COTTER V96906 002
Optional Vendor Code 10630, 65029, 73145, 84114,
8K160
used on 040A
- ITEM NOT ILLUSTRATED

Page 10003C-2
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
03C 180A NSA5059-3 .. NUT VF6198 002
OPT TO H53173-3 15653
OPT TO RMTE9868-3 72962
OPT TO THCR353M F0224
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 040A
03C 190A AN960-10L .. WASHER V88044 002
NAS1149F0332P 80205
OPT TO ASNA2397-10L F6198
Optional Vendor Code 10630, 58009, 8K160, F8982
used on 040A
03C 200A NAS1153-8D .. SCREW V80205 001
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, F7411,
FAWT4, K8753
used on 040A
03C 210A A5281008720000 .. PIN VFAPE3 001
MODIFIED FROM A5281008720001 MADE BY
FAPE3
used on 040A
03C 220A A5283006020300 .. CAP-PROTECTIVE VFAPE3 001
used on 040A
03C 230A A5283006120000 .. BUSH VFAPE3 001
used on 040A
03C 240A A5283005420000 .. SHAFT-TORQUE VFAPE3 001
used on 040A
03C 250A A5283005220400 .. SPACER VFAPE3 001
MODIFIED FROM A5283005220401 MADE BY
FAPE3
used on 040A
03C 260A A5283005120000 .. FITTING-SIDE VFAPE3 001
used on 040A
03C 270A A5283005020000 .. FITTING-SIDE VFAPE3 001
used on 040A
03C 280A A5283005820000 .. BUSH VFAPE3 001
used on 040A
03C 290A NSA5060-4 .. NUT VF6198 004
OPT TO H53174-4 15653
OPT TO PHCR354M F0224
OPT TO RME9868-4 72962
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
- ITEM NOT ILLUSTRATED

Page 10003C-3
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 040A
03C 300A AN960-416 .. WASHER V88044 004
NAS1149F0463P 80205
OPT TO ASNA2397-416 F6198
Optional Vendor Code 04795, 06329, 2N935, 60996,
70347, 8K160, C5543
used on 040A
03C 310A NAS1304-9D .. BOLT V80205 004
NAS6604D9 80205
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, 62384,
8Z507, F7411, K8753
used on 040A
03C 320A D5288020120000 .. FITTING VFAPE3 001
MODIFIED FROM D5288020120001 MADE BY
FAPE3
used on 040A
03C 330A D5288012820000 .. PLATE-FLUTED VFAPE3 001
used on 040A
03C 340A D5288020020000 .. BASE-MOUNTING VFAPE3 001
used on 040A
03C 350A ABS0254-6-250 . BOLT VFAPE3 004
OPT TO MBF2010S6-250 92215
OPT TO MBF2110S6-250 92215
Optional Vendor Code 04795, 2N935, 98524, C4293,
C5543
used on 001A, 002A
03C 360A NAS6704HU30 . BOLT V80205 012
Optional Vendor Code 0ZC92, 1ER65, 1RC86, 8Z507,
F7411, K8753, T0802
used on 001A, 002A
03C 370A D5288010500000 . STEP ASSY VFAPE3 001
used on 001A, 002A
03C 380A D5288013020200 . PLATE VFAPE3 001
OPT TO D5288021300000 FAPE3
used on 001A, 002A
03C 390A D5288011700000 . STEP ASSY VFAPE3 001
used on 001A, 002A
03C 400A D5288020400000 . PLATE ASSY VFAPE3 001
used on 001A, 002A
03C 410A D5288023400000 . STEP ASSY VFAPE3 001
POST SB 52-1025
used on 001A, 002A
- ITEM NOT ILLUSTRATED

Page 10003C-4
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

180

160
100
A 170 (110)
50
(60)
B
190
C 70 (200)
(80) 90
D A

E
210 x2

240
(250)

180 x4
210 x2
220
(230)
40

B
280

260 x2
20 x2

620
(630) 120
(130)

260 x2
20 x2
600
(610)

30
C
F_PL_528114_04_0_01_02

RAMP INSTL-LATERAL
(Sheet 1 of 2)
Figure 04 / FIGURE-52-81-14-950-804-01

Page 10004-0
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

10

280

260 x2
270 x2

420
460 x2 400 x2 (430)
440 460 x2 410 x2
(450) 465 x2

140
(150) 510
480 (520)

435 x4

210
560
(570)
180 500
210 20 x3

580
180 540 (590)
(550)
20
415 x4
30 x3 470 x4

30
E
F_PL_528114_04_0_02_00

RAMP INSTL-LATERAL
(Sheet 2 of 2)
Figure 04 / FIGURE-52-81-14-950-804-01

Page 10004-0
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
04 - 001A D5288000800065 RAMP INSTL-LATERAL VFAPE3 RF
used on 050A (528114010)
SEE 52-81-14-010 FOR NHA
04 - 002A D5288000800165 RAMP INSTL-LATERAL VFAPE3 RF
used on 060A (528114010)
SEE 52-81-14-010 FOR NHA
04 010A ABS0257-5-200 . BOLT VFAPE3 002
OPT TO ABS0257-5-200Z FAPE3
OPT TO MBF2013S5-200 92215
OPT TO MBF2113S5-200 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 002A
04 020A ABS0258-5A . COLLAR VFAPE3 008
OPT TO HL94TB5 92215
Optional Vendor Code 04795, 2N935, 56878, 5M902,
73197, C5543, K5673, SBF11, U6300
used on 001A, 002A
04 030A ABS0251A5-4 . FASTENER-HI-LOK VFAPE3 008
HL11VAP5-4 73197
used on 001A, 002A
04 040A NAS1097DD5 . RIVET V80205 004
EN6069D5 I9005
used on 001A, 002A
04 050A D5288000820600 . SHEET-TEFLON VFAPE3 001
used on 001A
04 060A D5288000820700 . SHEET-TEFLON VFAPE3 001
used on 002A
04 070A D5288000820800 . SHEET-TEFLON VFAPE3 001
used on 001A
04 080A D5288000820900 . SHEET-TEFLON VFAPE3 001
used on 002A
04 090A NAS1102-08-8 . SCREW V80205 003
Optional Vendor Code 06725, 0RFT4, 0ZC92, 1ER65,
62384, 8Z507, C4293, F7411, FAWT4, K8753
used on 001A, 002A
04 100A D5288000820000 . SECTION-T VFAPE3 001
MODIFIED FROM D5288000820001 MADE BY
FAPE3
used on 001A
04 110A D5288000820100 . SECTION-T VFAPE3 001
used on 002A
- ITEM NOT ILLUSTRATED

Page 10004-1
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
04 120A D5288000820200 . SECTION-T VFAPE3 001
used on 001A
04 130A D5288000820300 . SECTION-T VFAPE3 001
used on 002A
04 140A D5288000820400 . SECTION-T VFAPE3 001
used on 001A
04 150A D5288000820500 . SECTION-T VFAPE3 001
used on 002A
04 160A NAS1152E8R . SCREW V80205 001
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, K8753
used on 001A, 002A
04 170A NAS1152E10R . SCREW V80205 001
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, K8753
used on 001A, 002A
04 180A NAS1835C08 . INSERT V80205 010
OPT TO EF1835C08 C3898
OPT TO NSA5072-08A F6198
OPT TO SL606-08C 97393
Optional Vendor Code 83324, 97393, B1103, DM498
used on 001A, 002A
04 190A D5288017020000 . SUPPORT-NO 1 VFAPE3 001
used on 001A
04 200A D5288017020100 . SUPPORT-NO 1 VFAPE3 001
used on 002A
04 210A NAS1132E1 . SCREW V80205 008
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, 1RC86,
62384, 8Z507, C4293, F7411, FAWT4, K8753
used on 001A, 002A
04 220A D5288017120000 . SUPPORT-FWD,NO 2 VFAPE3 001
used on 001A
04 230A D5288017120100 . SUPPORT-FWD,NO 2 VFAPE3 001
used on 002A
04 240A D5288017220000 . SUPPORT-AFT,NO 2 VFAPE3 001
used on 001A
04 250A D5288017220100 . SUPPORT-AFT,NO 2 VFAPE3 001
used on 002A
04 260A NAS6704HU15 . BOLT V80205 006
Optional Vendor Code 0ZC92, 1ER65, 1RC86, 8Z507,
F7411, FAWT4, K8753, T0802
used on 001A, 002A
- ITEM NOT ILLUSTRATED

Page 10004-2
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
04 270A NAS6704HU19 . BOLT V80205 002
Optional Vendor Code 0ZC92, 1ER65, 1RC86, 8Z507,
F7411, K8753, T0802
used on 001A, 002A
04 280A D5288013120200 . INSERT VFAPE3 008
used on 001A, 002A
04 400A NAS563C11 . BOLT V80205 002
Optional Vendor Code 1ER65
used on 001A, 002A
04 410A AN960C10 . WASHER V88044 002
NAS1149C0363R 80205
OPT TO ASNA2397C10 F6198
Optional Vendor Code 10630, 58009, 8K160, F8982
used on 001A, 002A
04 415A ABS0258-5 . COLLAR VFAPE3 004
used on 001A, 002A
04 420A D5288019620000 . SUPPORT-MOVABLE,NO 4 VFAPE3 001
used on 001A
04 430A D5288019620100 . SUPPORT-MOBABLE,NO 4 VFAPE3 001
used on 002A
04 435A ABS0251-5-3 . FASTENER-HI-LOK VFAPE3 004
DAN6-5-3 D8518
OPT TO HL11VBJ5-3 73197
Optional Vendor Code 04795, 2N935, 56878, 73197,
C5543
used on 001A, 002A
04 440A D5288019200000 . SUPPORT ASSY-NO 4 VFAPE3 001
used on 001A
04 450A D5288019200100 . SUPPORT ASSY-NO 4 VFAPE3 001
used on 002A
04 460A LN9198-40B .. RIVET VD8442 004
Optional Vendor Code F0095
used on 440A, 450A
04 465A NSA5602-2 .. MOUNT-ISOLATOR VF6198 002
OPT TO SL2337-3 97393
Optional Vendor Code 04795, 2N935, 97393, B1103,
C5543
used on 440A, 450A
04 470A ABS0254-5-150 . BOLT VFAPE3 004
OPT TO ABS0254-5-150Z FAPE3
OPT TO MBF2010S5-150 98524
OPT TO MBF2110S5-150 98524
- ITEM NOT ILLUSTRATED

Page 10004-3
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 002A
04 480A ABS0256-5-150 . BOLT-BLIND VFAPE3 004
OPT TO ABS0256-5-150Z FAPE3
OPT TO MBF2112S5-150 98524
Optional Vendor Code 04795, 2N935, 98524, C5543
used on 001A, 002A
04 500A ABS0214-5-6 . RIVET VFAPE3 001
OPT TO CSR902B5W06 11815
Optional Vendor Code 04795, 11815, 2N935, 53551,
C5543
used on 001A, 002A
04 510A D5288000821200 . PLATE VFAPE3 001
used on 001A
04 520A D5288000821300 . PLATE VFAPE3 001
used on 002A
04 540A D5288019720000 . TIP-RUNOUT VFAPE3 001
used on 001A
04 550A D5288019720100 . TIP-RUNOUT VFAPE3 001
used on 002A
04 560A D5288019820000 . SUPPORT-TIP VFAPE3 001
used on 001A
04 570A D5288019820100 . SUPPORT-TIP VFAPE3 001
used on 002A
04 580A D5288000821400 . PROFILE-L VFAPE3 001
used on 001A
04 590A D5288000821500 . PROFILE-L VFAPE3 001
used on 002A
04 600A D5288019320000 . SUPPORT-FWD,NO 3 VFAPE3 001
used on 001A
04 610A D5288019320100 . SUPPORT-FWD,NO 3 VFAPE3 001
used on 002A
04 620A D5288019420000 . SUPPORT-AFT,NO 3 VFAPE3 001
used on 001A
04 630A D5288019420100 . SUPPORT-AFT,NO 3 VFAPE3 001
used on 002A
- ITEM NOT ILLUSTRATED

Page 10004-4
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

240
180 (250)
100
A (110)
170
160 40
100
(110) 210
180 x4
220
(230)

120
190
(200)
B (130)
50 310
90
B (60) 340
(350)
70 A
C (80)
D 280 380
(390)

30
E 260 20
360
(370)
320
(330)
120
290 (130)
10 (300)
140 480
510
C (150) (520)
490
120 210
280 (130)

560
(570) 180
260

270 20
210
180

460 540
(550)

440 140
(450) 420 (150)
470 30
(430) 20 500
400
410 30 530
180
D E
F_PL_528114_04_A_01_01

RAMP INSTL-LATERAL
Figure 04A / FIGURE-52-81-14-950-804-A01

Page 10004A-0
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
04A - 001A D5288000900063 RAMP INSTL-LATERAL VFAPE3 RF
used on 050A (52811401A)
SEE 52-81-14-01A FOR NHA
04A - 002A D5288000900163 RAMP INSTL-LATERAL VFAPE3 RF
used on 060A (52811401A)
SEE 52-81-14-01A FOR NHA
04A 010A ABS0257-5-200 . BOLT VFAPE3 002
OPT TO ABS0257-5-200Z FAPE3
OPT TO MBF2013S5-200 92215
OPT TO MBF2113S5-200 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 002A
04A 020A ABS0258-5A . COLLAR VFAPE3 007
OPT TO HL94TB5 92215
Optional Vendor Code 04795, 2N935, 56878, 5M902,
73197, C5543, K5673, SBF11, U6300
used on 001A, 002A
04A 030A ABS0251A5-4 . FASTENER-HI-LOK VFAPE3 007
HL11VAP5-4 73197
used on 001A, 002A
04A 040A NAS1097KE5 . RIVET V80205 004
Optional Vendor Code 11815, 53551, F0095
used on 001A, 002A
04A 050A D5288000920600 . SHEET-TEFLON VFAPE3 001
used on 001A
04A 060A D5288000920700 . SHEET-TEFLON VFAPE3 001
used on 002A
04A 070A D5288000920800 . SHEET-TEFLON VFAPE3 001
used on 001A
04A 080A D5288000920900 . SHEET-TEFLON VFAPE3 001
used on 002A
04A 090A NAS1102-08-8 . SCREW V80205 003
Optional Vendor Code 06725, 0RFT4, 0ZC92, 1ER65,
62384, 8Z507, C4293, F7411, FAWT4, K8753
used on 001A, 002A
04A 100A D5288000920000 . SECTION-T VFAPE3 001
used on 001A
04A 110A D5288000920100 . SECTION-T VFAPE3 001
used on 002A
04A 120A D5288000920200 . SECTION-T VFAPE3 001
used on 001A
- ITEM NOT ILLUSTRATED

Page 10004A-1
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
04A 130A D5288000920300 . SECTION-T VFAPE3 001
used on 002A
04A 140A D5288000920401 . SECTION-T VFAPE3 001
used on 001A
04A 150A D5288000920501 . SECTION-T VFAPE3 001
used on 002A
04A 160A NAS1152E8R . SCREW V80205 001
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, K8753
used on 001A, 002A
04A 170A NAS1152E10R . SCREW V80205 001
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, K8753
used on 001A, 002A
04A 180A NAS1835C08 . INSERT V80205 010
OPT TO EF1835C08 C3898
OPT TO NSA5072-08A F6198
OPT TO SL606-08C 97393
Optional Vendor Code 83324, 97393, B1103, DM498
used on 001A, 002A
04A 190A D5288017020000 . SUPPORT-NO 1 VFAPE3 001
used on 001A
04A 200A D5288017020100 . SUPPORT-NO 1 VFAPE3 001
used on 002A
04A 210A NAS1132E1 . SCREW V80205 008
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, 1RC86,
62384, 8Z507, C4293, F7411, FAWT4, K8753
used on 001A, 002A
04A 220A D5288017120000 . SUPPORT-FWD,NO 2 VFAPE3 001
used on 001A
04A 230A D5288017120100 . SUPPORT-FWD,NO 2 VFAPE3 001
used on 002A
04A 240A D5288017220000 . SUPPORT-AFT,NO 2 VFAPE3 001
used on 001A
04A 250A D5288017220100 . SUPPORT-AFT,NO 2 VFAPE3 001
used on 002A
04A 260A NAS6704HU15 . BOLT V80205 006
Optional Vendor Code 0ZC92, 1ER65, 1RC86, 8Z507,
F7411, FAWT4, K8753, T0802
used on 001A, 002A
04A 270A NAS6704HU19 . BOLT V80205 002
Optional Vendor Code 0ZC92, 1ER65, 1RC86, 8Z507,
F7411, K8753, T0802
- ITEM NOT ILLUSTRATED

Page 10004A-2
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 001A, 002A
04A 280A D5288013120200 . INSERT VFAPE3 008
used on 001A, 002A
04A 290A D5288016800000 . SUPPORT ASSY-NO 3 VFAPE3 001
used on 001A
04A 300A D5288016800100 . SUPPORT ASSY-NO 3 VFAPE3 001
used on 002A
04A 310A LN9198-32B .. RIVET VD8442 015
Optional Vendor Code F0095
used on 290A, 300A
04A 320A D5288017920000 .. REINFORCEMENT VFAPE3 001
used on 290A
04A 330A D5288017920100 .. REINFORCEMENT VFAPE3 001
used on 300A
04A 340A D5288018020000 .. REINFORCEMENT VFAPE3 001
used on 290A
04A 350A D5288018020100 .. REINFORCEMENT VFAPE3 001
used on 300A
04A 360A D5288017320000 .. SUPPORT-FWD,NO 3 VFAPE3 001
used on 290A
04A 370A D5288017320100 .. SUPPORT-FWD,NO 3 VFAPE3 001
used on 300A
04A 380A D5288017420000 .. SUPPORT-AFT,NO 3 VFAPE3 001
used on 290A
04A 390A D5288017420100 .. SUPPORT-AFT,NO 3 VFAPE3 001
used on 300A
04A 400A NAS563C11 . BOLT V80205 002
Optional Vendor Code 1ER65
used on 001A, 002A
04A 410A AN960C10 . WASHER V88044 002
NAS1149C0363R 80205
OPT TO ASNA2397C10 F6198
Optional Vendor Code 10630, 58009, 8K160, F8982
used on 001A, 002A
04A 420A D5288017620000 . SUPPORT-MOVABLE-NO 4 VFAPE3 001
used on 001A
04A 430A D5288017620100 . SUPPORT-MOVABLE,NO 4 VFAPE3 001
used on 002A
04A 440A D5288016900000 . SUPPORT ASSY-NO 4 VFAPE3 001
used on 001A
- ITEM NOT ILLUSTRATED

Page 10004A-3
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
04A 450A D5288016900100 . SUPPORT ASSY-NO 3 VFAPE3 001
used on 002A
04A 460A LN9198-40B .. RIVET VD8442 004
Optional Vendor Code F0095
used on 440A, 450A
04A 470A NSA5602-2 .. MOUNT-ISOLATOR VF6198 002
OPT TO SL2337-3 97393
Optional Vendor Code 04795, 2N935, 97393, B1103,
C5543
used on 440A, 450A
04A 480A ABS0256-5-150 . BOLT-BLIND VFAPE3 004
OPT TO ABS0256-5-150Z FAPE3
OPT TO MBF2112S5-150 98524
Optional Vendor Code 04795, 2N935, 98524, C5543
used on 001A, 002A
04A 490A MS21042-08 . NUT V96906 001
OPT TO H14L08CW 75237
OPT TO PLH3508 F0224
OPT TO RH30X08 52828
OPT TO T97S832CPF 11815
Optional Vendor Code 04795, 2N935, 60119, C5543
used on 001A, 002A
04A 500A NAS1152E5 . SCREW V80205 001
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, F7411,
FAWT4, K8753
used on 001A, 002A
04A 510A D5288018220000 . PLATE VFAPE3 001
used on 001A
04A 520A D5288018220100 . PLATE VFAPE3 001
used on 002A
04A 530A ABS0214-5-6 . RIVET VFAPE3 001
OPT TO CSR902B5W06 11815
Optional Vendor Code 04795, 11815, 2N935, 53551,
C5543
used on 001A, 002A
04A 540A D5288017720000 . TIP-RUNOUT VFAPE3 001
used on 001A
04A 550A D5288017720100 . TIP-RUNOUT VFAPE3 001
used on 002A
04A 560A D5288017820000 . SUPPORT-TIP VFAPE3 001
used on 001A
- ITEM NOT ILLUSTRATED

Page 10004A-4
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
04A 570A D5288017820100 . SUPPORT-TIP VFAPE3 001
used on 002A
- ITEM NOT ILLUSTRATED

Page 10004A-5
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

180
A
170 240
160 (250)
100 100
(110) (110)
40

210
180 x4
50 190 220
(60) (200) (230)
90
B
70 120
(80) A 280 B (130)
C 620
(630)
D
30

E 260 20
10

600
120 (610)
280 (130) C
120
(130)

260 480
140 510
270 (150) (520)
210 490

460
560
(570) 180
440 140
(450) 420 (150) 20
470
(430) 210
400 180
410

D 540
(550)

30
20 505
30 530
180
E
F_PL_528114_04_B_01_01

RAMP INSTL-LATERAL
Figure 04B / FIGURE-52-81-14-950-804-B01

Page 10004B-0
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
04B - 001A D5288000800065 RAMP INSTL-LATERAL VFAPE3 RF
used on 050B (528114010)
SEE 52-81-14-010 FOR NHA
04B - 002A D5288000800165 RAMP INSTL-LATERAL VFAPE3 RF
used on 060B (528114010)
SEE 52-81-14-010 FOR NHA
04B 010A ABS0257-5-200 . BOLT VFAPE3 002
OPT TO ABS0257-5-200Z FAPE3
OPT TO MBF2013S5-200 92215
OPT TO MBF2113S5-200 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 002A
04B 020A ABS0258-5A . COLLAR VFAPE3 007
OPT TO HL94TB5 92215
Optional Vendor Code 04795, 2N935, 56878, 5M902,
73197, C5543, K5673, SBF11, U6300
used on 001A, 002A
04B 030A ABS0251A5-4 . FASTENER-HI-LOK VFAPE3 007
HL11VAP5-4 73197
used on 001A, 002A
04B 040A NAS1097DD5 . RIVET V80205 004
EN6069D5 I9005
used on 001A, 002A
04B 050A D5288000820600 . SHEET-TEFLON VFAPE3 001
used on 001A
04B 060A D5288000820700 . SHEET-TEFLON VFAPE3 001
used on 002A
04B 070A D5288000820800 . SHEET-TEFLON VFAPE3 001
used on 001A
04B 080A D5288000820900 . SHEET-TEFLON VFAPE3 001
used on 002A
04B 090A NAS1102-08-8 . SCREW V80205 003
Optional Vendor Code 06725, 0RFT4, 0ZC92, 1ER65,
62384, 8Z507, C4293, F7411, FAWT4, K8753
used on 001A, 002A
04B 100A D5288000820000 . SECTION-T VFAPE3 001
MODIFIED FROM D5288000820001 MADE BY
FAPE3
used on 001A
04B 110A D5288000820100 . SECTION-T VFAPE3 001
used on 002A
- ITEM NOT ILLUSTRATED

Page 10004B-1
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
04B 120A D5288000820200 . SECTION-T VFAPE3 001
used on 001A
04B 130A D5288000820300 . SECTION-T VFAPE3 001
used on 002A
04B 140A D5288000820400 . SECTION-T VFAPE3 001
used on 001A
04B 150A D5288000820500 . SECTION-T VFAPE3 001
used on 002A
04B 160A NAS1152E8R . SCREW V80205 001
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, K8753
used on 001A, 002A
04B 170A NAS1152E10R . SCREW V80205 001
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, K8753
used on 001A, 002A
04B 180A NAS1835C08 . INSERT V80205 010
OPT TO EF1835C08 C3898
OPT TO NSA5072-08A F6198
OPT TO SL606-08C 97393
Optional Vendor Code 83324, 97393, B1103, DM498
used on 001A, 002A
04B 190A D5288017020000 . SUPPORT-NO 1 VFAPE3 001
used on 001A
04B 200A D5288017020100 . SUPPORT-NO 1 VFAPE3 001
used on 002A
04B 210A NAS1132E1 . SCREW V80205 008
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, 1RC86,
62384, 8Z507, C4293, F7411, FAWT4, K8753
used on 001A, 002A
04B 220A D5288017120000 . SUPPORT-FWD,NO 2 VFAPE3 001
used on 001A
04B 230A D5288017120100 . SUPPORT-FWD,NO 2 VFAPE3 001
used on 002A
04B 240A D5288017220000 . SUPPORT-AFT,NO 2 VFAPE3 001
used on 001A
04B 250A D5288017220100 . SUPPORT-AFT,NO 2 VFAPE3 001
used on 002A
04B 260A NAS6704HU15 . BOLT V80205 006
Optional Vendor Code 0ZC92, 1ER65, 1RC86, 8Z507,
F7411, FAWT4, K8753, T0802
used on 001A, 002A
- ITEM NOT ILLUSTRATED

Page 10004B-2
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
04B 270A NAS6704HU19 . BOLT V80205 002
Optional Vendor Code 0ZC92, 1ER65, 1RC86, 8Z507,
F7411, K8753, T0802
used on 001A, 002A
04B 280A D5288013120200 . INSERT VFAPE3 008
used on 001A, 002A
04B 400A NAS563C11 . BOLT V80205 002
Optional Vendor Code 1ER65
used on 001A, 002A
04B 410A AN960C10 . WASHER V88044 002
NAS1149C0363R 80205
OPT TO ASNA2397C10 F6198
Optional Vendor Code 10630, 58009, 8K160, F8982
used on 001A, 002A
04B 420A D5288019620000 . SUPPORT-MOVABLE,NO 4 VFAPE3 001
used on 001A
04B 430A D5288019620100 . SUPPORT-MOBABLE,NO 4 VFAPE3 001
used on 002A
04B 440A D5288019200000 . SUPPORT ASSY-NO 4 VFAPE3 001
used on 001A
04B 450A D5288019200100 . SUPPORT ASSY-NO 4 VFAPE3 001
used on 002A
04B 460A LN9198-40B .. RIVET VD8442 004
Optional Vendor Code F0095
used on 440A, 450A
04B 470A NSA5602-2 .. MOUNT-ISOLATOR VF6198 002
OPT TO SL2337-3 97393
Optional Vendor Code 04795, 2N935, 97393, B1103,
C5543
used on 440A, 450A
04B 480A ABS0256-5-150 . BOLT-BLIND VFAPE3 004
OPT TO ABS0256-5-150Z FAPE3
OPT TO MBF2112S5-150 98524
Optional Vendor Code 04795, 2N935, 98524, C5543
used on 001A, 002A
04B 490A MS21042-08 . NUT V96906 001
OPT TO H14L08CW 75237
OPT TO PLH3508 F0224
OPT TO RH30X08 52828
OPT TO T97S832CPF 11815
Optional Vendor Code 04795, 2N935, 60119, C5543
used on 001A, 002A
- ITEM NOT ILLUSTRATED

Page 10004B-3
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
04B 505A NAS1152E5 . SCREW V80205 001
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, F7411,
FAWT4, K8753
used on 001A, 002A
04B 510A D5288019920000 . PLATE VFAPE3 001
used on 001A
04B 520A D5288019920100 . PLATE VFAPE3 001
used on 002A
04B 530A ABS0214-5-6 . RIVET VFAPE3 001
OPT TO CSR902B5W06 11815
Optional Vendor Code 04795, 11815, 2N935, 53551,
C5543
used on 001A, 002A
04B 540A D5288019720000 . TIP-RUNOUT VFAPE3 001
used on 001A
04B 550A D5288019720100 . TIP-RUNOUT VFAPE3 001
used on 002A
04B 560A D5288019820000 . SUPPORT-TIP VFAPE3 001
used on 001A
04B 570A D5288019820100 . SUPPORT-TIP VFAPE3 001
used on 002A
04B 600A D5288019320000 . SUPPORT-FWD,NO 3 VFAPE3 001
used on 001A
04B 610A D5288019320100 . SUPPORT-FWD,NO 3 VFAPE3 001
used on 002A
04B 620A D5288019420000 . SUPPORT-AFT,NO 3 VFAPE3 001
used on 001A
04B 630A D5288019420100 . SUPPORT-AFT,NO 3 VFAPE3 001
used on 002A
- ITEM NOT ILLUSTRATED

Page 10004B-4
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

180
A
170 240
160 (250)
100 100
(110) (110)
40

210
180 x4
50 190 220
(60) (200) (230)
90
B
70 120
(80) A 280 B (130)
C 620
(630)
D
30

E 260 20
10

600
120 (610)
280 (130) C
120
(130)

260 480
140 510
270 (150) (520)
210 490

460
560
(570) 180
440 140
(450) 420 (150) 20
470
(430) 210
400 180
410

D 540
(550)

30
20 500
30 530
180
E
F_PL_528114_04_C_01_01

RAMP INSTL-LATERAL
Figure 04C / FIGURE-52-81-14-950-804-C01

Page 10004C-0
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
04C - 001A D5288001000064 RAMP INSTL-LATERAL VFAPE3 RF
used on 050A (52811401B)
SEE 52-81-14-01B FOR NHA
04C - 001B D5288001000064 RAMP INSTL-LATERAL VFAPE3 RF
used on 050B (52811401B)
SEE 52-81-14-01B FOR NHA
04C - 002A D5288001000164 RAMP INSTL-LATERAL VFAPE3 RF
used on 060A (52811401B)
SEE 52-81-14-01B FOR NHA
04C - 002B D5288001000164 RAMP INSTL-LATERAL VFAPE3 RF
used on 060B (52811401B)
SEE 52-81-14-01B FOR NHA
04C 010A ABS0257-5-200 . BOLT VFAPE3 002
OPT TO ABS0257-5-200Z FAPE3
OPT TO MBF2013S5-200 92215
OPT TO MBF2113S5-200 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 001B, 002A, 002B
04C 020A ABS0258-5A . COLLAR VFAPE3 007
OPT TO HL94TB5 92215
Optional Vendor Code 04795, 2N935, 56878, 5M902,
73197, C5543, K5673, SBF11, U6300
used on 001A, 001B, 002A, 002B
04C 030A ABS0251A5-4 . FASTENER-HI-LOK VFAPE3 007
HL11VAP5-4 73197
used on 001A, 001B, 002A, 002B
04C 040A NAS1097KE5 . RIVET V80205 004
Optional Vendor Code 11815, 53551, F0095
used on 001A, 001B, 002A, 002B
04C 050A D5288001020600 . SHEET-TEFLON VFAPE3 001
used on 001A, 001B
04C 060A D5288001020700 . SHEET-TEFLON VFAPE3 001
used on 002A, 002B
04C 070A D5288001020800 . SHEET-TEFLON VFAPE3 001
used on 001A, 001B
04C 080A D5288001020900 . SHEET-TEFLON VFAPE3 001
used on 002A, 002B
04C 090A NAS1102-08-8 . SCREW V80205 003
Optional Vendor Code 06725, 0RFT4, 0ZC92, 1ER65,
62384, 8Z507, C4293, F7411, FAWT4, K8753
- ITEM NOT ILLUSTRATED

Page 10004C-1
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 001A, 001B, 002A, 002B
04C 100A D5288001020000 . SECTION-T VFAPE3 001
used on 001A, 001B
04C 110A D5288001020100 . SECTION-T VFAPE3 001
used on 002A, 002B
04C 120A D5288001020200 . SECTION-T VFAPE3 001
used on 001A, 001B
04C 130A D5288001020300 . SECTION-T VFAPE3 001
used on 002A, 002B
04C 140A D5288001020400 . SECTION-T VFAPE3 001
used on 001A, 001B
04C 150A D5288001020500 . SECTION-T VFAPE3 001
used on 002A, 002B
04C 160A NAS1152E7R . SCREW V80205 001
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, K8753
used on 001A, 001B, 002A, 002B
04C 170A NAS1152E8R . SCREW V80205 001
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, K8753
used on 001A, 001B, 002A, 002B
04C 180A NAS1835C08 . INSERT V80205 010
OPT TO EF1835C08 C3898
OPT TO NSA5072-08A F6198
OPT TO SL606-08C 97393
Optional Vendor Code 83324, 97393, B1103, DM498
used on 001A, 001B, 002A, 002B
04C 190A D5288015020000 . SUPPORT-NO 1 VFAPE3 001
used on 001A
04C 190B D5288015020200 . SUPPORT NO 1 VFAPE3 001
used on 001B
04C 200A D5288015020100 . SUPPORT-NO 1 VFAPE3 001
used on 002A
04C 200B D5288015020300 . SUPPORT-NO 1 VFAPE3 001
used on 002B
04C 210A NAS1132E1 . SCREW V80205 008
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, 1RC86,
62384, 8Z507, C4293, F7411, FAWT4, K8753
used on 001A, 001B, 002A, 002B
04C 220A D5288015120000 . SUPPORT-FWD,NO 2 VFAPE3 001
used on 001A, 001B
04C 230A D5288015120100 . SUPPORT-FWD,NO 2 VFAPE3 001
used on 002A, 002B
- ITEM NOT ILLUSTRATED

Page 10004C-2
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
04C 240A D5288015220000 . SUPPORT-AFT,NO 2 VFAPE3 001
used on 001A, 001B
04C 250A D5288015220100 . SUPPORT-AFT,NO 2 VFAPE3 001
used on 002A, 002B
04C 260A NAS6704HU15 . BOLT V80205 006
Optional Vendor Code 0ZC92, 1ER65, 1RC86, 8Z507,
F7411, FAWT4, K8753, T0802
used on 001A, 001B, 002A, 002B
04C 270A NAS6704HU19 . BOLT V80205 002
Optional Vendor Code 0ZC92, 1ER65, 1RC86, 8Z507,
F7411, K8753, T0802
used on 001A, 001B, 002A, 002B
04C 280A D5288013120200 . INSERT VFAPE3 008
used on 001A, 001B, 002A, 002B
04C 400A NAS563C11 . BOLT V80205 002
Optional Vendor Code 1ER65
used on 001A, 001B, 002A, 002B
04C 410A AN960C10 . WASHER V88044 002
NAS1149C0363R 80205
OPT TO ASNA2397C10 F6198
Optional Vendor Code 10630, 58009, 8K160, F8982
used on 001A, 001B, 002A, 002B
04C 420A D5288015620000 . SUPPORT-MOVABLE,NO 4 VFAPE3 001
used on 001A, 001B
04C 430A D5288015620100 . SUPPORT-MOVABLE,NO 4 VFAPE3 001
used on 002A, 002B
04C 440A D5288014900000 . SUPPORT ASSY-NO 4 VFAPE3 001
used on 001A, 001B
04C 450A D5288014900100 . SUPPORT ASSY-NO 4 VFAPE3 001
used on 002A, 002B
04C 460A LN9198-40B .. RIVET VD8442 004
Optional Vendor Code F0095
used on 440A, 450A
04C 470A NSA5602-2 .. MOUNT-ISOLATOR VF6198 002
OPT TO SL2337-3 97393
Optional Vendor Code 04795, 2N935, 97393, B1103,
C5543
used on 440A, 450A
04C 480A ABS0256-5-150 . BOLT-BLIND VFAPE3 004
OPT TO ABS0256-5-150Z FAPE3
OPT TO MBF2112S5-150 98524
- ITEM NOT ILLUSTRATED

Page 10004C-3
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
Optional Vendor Code 04795, 2N935, 98524, C5543
used on 001A, 001B, 002A, 002B
04C 490A MS21042-08 . NUT V96906 001
OPT TO H14L08CW 75237
OPT TO PLH3508 F0224
OPT TO RH30X08 52828
OPT TO T97S832CPF 11815
Optional Vendor Code 04795, 2N935, 60119, C5543
used on 001A, 001B, 002A, 002B
04C 500A NAS1152E5 . SCREW V80205 001
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, F7411,
FAWT4, K8753
used on 001A, 001B, 002A, 002B
04C 510A D5288016020000 . PLATE VFAPE3 001
used on 001A, 001B
04C 520A D5288016020100 . PLATE VFAPE3 001
used on 002A, 002B
04C 530A ABS0214-5-6 . RIVET VFAPE3 001
OPT TO CSR902B5W06 11815
Optional Vendor Code 04795, 11815, 2N935, 53551,
C5543
used on 001A, 001B, 002A, 002B
04C 540A D5288015720000 . TIP-RUNOUT VFAPE3 001
used on 001A, 001B
04C 550A D5288015720100 . TIP-RUNOUT VFAPE3 001
used on 002A, 002B
04C 560A D5288015820000 . SUPPORT-TIP VFAPE3 001
used on 001A, 001B
04C 570A D5288015820100 . SUPPORT-TIP VFAPE3 001
used on 002A, 002B
04C 600A D5288015320000 . SUPPORT-FWD,NO 3 VFAPE3 001
used on 001A, 001B
04C 610A D5288015320100 . SUPPORT-FWD,NO 3 VFAPE3 001
used on 002A, 002B
04C 620A D5288015420000 . SUPPORT-AFT,NO 3 VFAPE3 001
used on 001A, 001B
04C 630A D5288015420100 . SUPPORT-AFT,NO 3 VFAPE3 001
used on 002A, 002B
- ITEM NOT ILLUSTRATED

Page 10004C-4
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

205 207

203
190
(210) 203
202

110

A 10
20 70
80 40 90 30 60
(100)
270
150

160
50
(170)
130
180

250
(260)
210
(220) 280
120
230 140 x3
(240) 180

290
140
A
130 F_PL_528114_04_D_01_02

RAMP INSTL-CENTRAL LH
Figure 04D / FIGURE-52-81-14-950-804-D01

Page 10004D-0
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
04D - 001A D5288000800063 RAMP INSTL-CENTRAL LH VFAPE3 RF
POST SB 52-1025
used on 050A (52811401C), 050A (52811401F)
SEE 52-81-14-01C FOR NHA, SEE 52-81-14-01F FOR
NHA
04D - 001B D5288000900063 RAMP INSTL-LATERAL VFAPE3 RF
POST SB 52-1025
used on 050B (52811401D)
SEE 52-81-14-01D FOR NHA
04D - 001C D5288001000063 RAMP INSTL-CENTRAL VFAPE3 RF
POST SB 52-1025
used on 050A (52811401E)
SEE 52-81-14-01E FOR NHA
04D - 002A D5288000800163 RAMP INSTL-CENTRAL RH VFAPE3 RF
POST SB 52-1025
used on 060A (52811401C), 060A (52811401F)
SEE 52-81-14-01C FOR NHA, SEE 52-81-14-01F FOR
NHA
04D - 002B D5288000900163 RAMP INSTL-LATERAL VFAPE3 RF
POST SB 52-1025
used on 060A (52811401D)
SEE 52-81-14-01D FOR NHA
04D - 002C D5288001000163 RAMP INSTL-CENTRAL VFAPE3 RF
POST SB 52-1025
used on 060A (52811401E)
SEE 52-81-14-01E FOR NHA
04D 010A MS24665-151 . PIN-COTTER V96906 001
Optional Vendor Code 10630, 65029, 73145, 84114,
8K160
used on 001A, 001B, 001C, 002A, 002B, 002C
04D 020A NSA5060C4 . NUT VF6198 001
OPT TO E9925-4 72962
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 001A, 001B, 001C, 002A, 002B, 002C
04D 030A AN960C416L . WASHER V88044 001
NAS1149C0432R 80205
OPT TO ASNA2397C416L F6198
Optional Vendor Code 10630, 58009
used on 001A, 001B, 001C, 002A, 002B, 002C
- ITEM NOT ILLUSTRATED

Page 10004D-1
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
04D 040A NAS6704DU30 . BOLT V80205 001
Optional Vendor Code 0ZC92, 1ER65, 1RC86, 62384,
8Z507, F7411, FAWT4, K8753, T0802
used on 001A, 001B, 001C, 002A, 002B, 002C
04D 050A MS21042-08 . NUT V96906 001
OPT TO H14L08CW 75237
OPT TO PLH3508 F0224
OPT TO RH30X08 52828
OPT TO T97S832CPF 11815
Optional Vendor Code 04795, 2N935, 60119, C5543
used on 001A, 001B, 001C, 002A, 002B, 002C
04D 060A NAS1132E2 . SCREW V80205 002
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, 1RC86,
62384, 8Z507, C4293, F7411, FAWT4, K8753
used on 001A, 001B, 001C, 002A, 002B, 002C
04D 070A ABS0257-5-150 . BOLT-BLIND VFAPE3 002
ABS0257-5-150Z FAPE3
OPT TO MBF2013S5-150 98524
OPT TO MBF2113S5-150 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 001B, 001C, 002A, 002B, 002C
04D 080A NAS6704HU15 . BOLT V80205 004
Optional Vendor Code 0ZC92, 1ER65, 1RC86, 8Z507,
F7411, FAWT4, K8753, T0802
used on 001A, 001B, 001C, 002A, 002B, 002C
04D 090A D5288018720000 . SUPPORT VFAPE3 001
used on 001A, 001B, 001C
04D 100A D5288018720100 . SUPPORT VFAPE3 001
used on 002A, 002B, 002C
04D 110A D5288013120200 . INSERT VFAPE3 004
used on 001A, 001B, 001C, 002A, 002B, 002C
04D 120A NAS1132E1 . SCREW V80205 001
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, 1RC86,
62384, 8Z507, C4293, F7411, FAWT4, K8753
used on 001A, 001B, 001C, 002A, 002B, 002C
04D 130A ABS0258-5A . COLLAR VFAPE3 004
OPT TO HL94TB5 92215
Optional Vendor Code 04795, 2N935, 56878, 5M902,
73197, C5543, K5673, SBF11, U6300
used on 001A, 001B, 001C, 002A, 002B, 002C
- ITEM NOT ILLUSTRATED

Page 10004D-2
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
04D 140A ABS0251A5-4 . FASTENER-HI-LOK VFAPE3 004
HL11VAP5-4 73197
used on 001A, 001B, 001C, 002A, 002B, 002C
04D 150A ABS0214-5-6 . RIVET VFAPE3 001
OPT TO CSR902B5W06 11815
Optional Vendor Code 04795, 11815, 2N935, 53551,
C5543
used on 001A, 001B, 001C, 002A, 002B, 002C
04D 160A D5288018625000 . TIP-RUNOUT VFAPE3 001
used on 001A, 001B, 001C
04D 170A D5288018625100 . TIP-RUNOUT VFAPE3 001
used on 002A, 002B, 002C
04D 180A NAS1835C08 . INSERT V80205 002
OPT TO EF1835C08 C3898
OPT TO NSA5072-08A F6198
OPT TO SL606-08C 97393
Optional Vendor Code 83324, 97393, B1103, DM498
used on 001A, 001B, 001C, 002A, 002B, 002C
04D 190A D5288018502000 . RAMP ASSY VFAPE3 001
POST SB 52-1025
used on 001A, 001B, 001C
04D 200A D5288018502100 . RAMP ASSY VFAPE3 001
POST SB 52-1025
used on 002A, 002B, 002C
04D 202A D5288018400000 .. GLIDER VFAPE3 001
used on 190A, 200A
04D 203A D5288018920000 ... BUSHING VFAPE3 002
used on 202A
04D 205A ABS0254-5-300 .. BOLT-BLIND VFAPE3 003
OPT TO MBF2010S5-300 98524
OPT TO MBF2110S5-300 98524
Optional Vendor Code 04795, 2N935, 98524, C5543
used on 190A, 200A
04D 207A ABS0254-5-200 .. BOLT-BLIND VFAPE3 003
OPT TO MBF2010S5-200 98524
OPT TO MBF2110S5-200 98524
Optional Vendor Code 04795, 2N935, 98524, C5543
used on 190A, 200A
04D 210A D5288018625400 . ANGLE VFAPE3 001
used on 001A, 001B, 001C
- ITEM NOT ILLUSTRATED

Page 10004D-3
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
04D 220A D5288018625500 . ANGLE VFAPE3 001
used on 002A, 002B, 002C
04D 230A D5288018625600 . ANGLE VFAPE3 001
used on 001A, 001B, 001C
04D 240A D5288018625700 . ANGLE VFAPE3 001
used on 002A, 002B, 002C
04D 250A D5288018625200 . ANGLE VFAPE3 001
used on 001A, 001B, 001C
04D 260A D5288018625300 . ANGLE VFAPE3 001
used on 002A, 002B, 002C
04D 270A DAN7-6-3 . PIN-RIVET VD8518 005
HL1012VF6-3 92215
OPT TO HL12VDF6-3 92215
Optional Vendor Code 04795, 06725, 17446, 2N935,
56878, 73197, C4293, C5543, F6167, K5673, U6300
used on 001A, 001B, 001C, 002A, 002B, 002C
04D 280A DAN12-6 . COLLAR VD8518 008
OPT TO F0N2-1207-6 H1822
OPT TO HL86GB6 92215
Optional Vendor Code 04795, 2N935, 56878, 5M902,
73197, C4293, C5543, K5673, U6300
used on 001A, 001B, 001C, 002A, 002B, 002C
04D 290A DAN7-6-4 . PIN-RIVET VD8518 003
HL1012VF6-4 92215
OPT TO HL12VDF6-4 92215
Optional Vendor Code 04795, 06725, 17446, 2N935,
56878, 73197, C4293, C5543, F6167, K5673, U6300
used on 001A, 001B, 001C, 002A, 002B, 002C
- ITEM NOT ILLUSTRATED

Page 10004D-4
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

130 130
120
240

120
220 30 x7
A 230 30 x7

10
(20)
250
(260)

240

220
230

120
120
130 x2

60
50
140 70
(150) 90
180 (100)
(190)

40
130
120
160
(170)

110

80
200
130 (210)
120
A
F_PL_528114_05_0_01_02

RAMP INSTL-CENTRAL
Figure 05 / FIGURE-52-81-14-950-805-01

Page 10005-0
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
05 - 001A D5288000800064 RAMP INSTL-CENTRAL VFAPE3 RF
used on 070A (528114010)
SEE 52-81-14-010 FOR NHA
05 - 001B D5288000900064 RAMP INSTL-CENTRAL VFAPE3 RF
used on 070A (52811401A)
SEE 52-81-14-01A FOR NHA
05 - 002A D5288000800164 RAMP INSTL-CENTRAL VFAPE3 RF
used on 080A (528114010)
SEE 52-81-14-010 FOR NHA
05 - 002B D5288000900164 RAMP INSTL-CENTRAL VFAPE3 RF
used on 080A (52811401A)
SEE 52-81-14-01A FOR NHA
05 010A D5288000821000 . SHEET-TEFLON VFAPE3 001
used on 001A
05 010B D5288000921000 . SHEET-TEFLON VFAPE3 001
used on 001B
05 020A D5288000821100 . SHEET-TEFLON VFAPE3 001
used on 002A
05 020B D5288000921100 . SHEET-TEFLON VFAPE3 001
used on 002B
05 030A LN9198-24B . RIVET VD8442 014
Optional Vendor Code F0095
used on 001A, 001B, 002A, 002B
05 040A LN9199-40C . RIVET VD8442 004
USE AS REQUIRED
LN9199-4014CF D8442
Optional Vendor Code F0095
used on 001A, 001B, 002A, 002B
05 050A ABS0257-5-400 . BOLT VFAPE3 001
OPT TO MBF2013S5-400 92215
OPT TO MBF2113S5-400 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 001B, 002A, 002B
05 060A ABS0257-5-450 . BOLT VFAPE3 001
OPT TO MBF2013S5-450 92215
OPT TO MBF2113S5-450 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 001B, 002A, 002B
- ITEM NOT ILLUSTRATED

Page 10005-1
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
05 070A ABS0257-5-500 . BOLT VFAPE3 001
OPT TO MBF2013S5-500 92215
OPT TO MBF2113S5-500 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 001B, 002A, 002B
05 080A ABS0257-5-200 . BOLT VFAPE3 003
OPT TO ABS0257-5-200Z FAPE3
OPT TO MBF2013S5-200 92215
OPT TO MBF2113S5-200 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 001B, 002A, 002B
05 090A D5288011620000 . SECTION-T VFAPE3 001
used on 001A, 001B
05 100A D5288011620100 . SECTION-T VFAPE3 001
used on 002A, 002B
05 110A D5288011620200 . SECTION-T VFAPE3 001
used on 001A, 001B, 002A, 002B
05 120A NAS1132E1 . SCREW V80205 014
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, 1RC86,
62384, 8Z507, C4293, F7411, FAWT4, K8753
used on 001A, 001B, 002A, 002B
05 130A NAS1835C08 . INSERT V80205 014
OPT TO EF1835C08 C3898
OPT TO NSA5072-08A F6198
OPT TO SL606-08C 97393
Optional Vendor Code 83324, 97393, B1103, DM498
used on 001A, 001B, 002A, 002B
05 140A D5288011020000 . SUPPORT VFAPE3 001
used on 001A, 001B
05 150A D5288011020100 . SUPPORT VFAPE3 001
used on 002A, 002B
05 160A D5288011120000 . SUPPORT- VFAPE3 001
used on 001A, 001B
05 170A D5288011120100 . SUPPORT- VFAPE3 001
used on 002A, 002B
05 180A D5288011220000 . SUPPORT VFAPE3 001
used on 001A, 001B
05 190A D5288011220100 . SUPPORT VFAPE3 001
used on 002A, 002B
- ITEM NOT ILLUSTRATED

Page 10005-2
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
05 200A D5288011320000 . TIP VFAPE3 001
used on 001A, 001B
05 210A D5288011320100 . TIP VFAPE3 001
used on 002A, 002B
05 220A MS21042-08 . NUT V96906 008
OPT TO H14L08CW 75237
OPT TO PLH3508 F0224
OPT TO RH30X08 52828
OPT TO T97S832CPF 11815
Optional Vendor Code 04795, 2N935, 60119, C5543
used on 001A, 001B, 002A, 002B
05 230A AN960C8L . WASHER V88044 008
NAS1149CN816R 80205
OPT TO ASNA2397C8L F6198
Optional Vendor Code 10630, 58009
used on 001A, 001B, 002A, 002B
05 240A NAS1152E3 . SCREW V80205 008
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, F7411,
FAWT4, K8753
used on 001A, 001B, 002A, 002B
05 250A D5288011520000 . RAMP-BLISTER VFAPE3 001
used on 001A
05 250B D5288011420000 . RAMP-BLISTER VFAPE3 001
used on 001B
05 260A D5288011520100 . RAMP-BLISTER VFAPE3 001
used on 002A
05 260B D5288011420100 . RAMP-BLISTER VFAPE3 001
used on 002B
- ITEM NOT ILLUSTRATED

Page 10005-3
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

130

130 120

240
120
A

220
230

250
(260)
10
(20)
225
235
245

240

220
230 120

130

140 60 70
(150) 90
180 (100)
(190)
50
40

120
160
(170)

110

80
200
(210)
120
A
F_PL_528114_05_A_01_01

RAMP INSTL-CENTRAL
Figure 05A / FIGURE-52-81-14-950-805-A01

Page 10005A-0
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
05A - 001A D5288001000063 RAMP INSTL-CENTRAL VFAPE3 RF
used on 070A (52811401B)
SEE 52-81-14-01B FOR NHA
05A - 002A D5288001000163 RAMP INSTL-CENTRAL VFAPE3 RF
used on 080A (52811401B)
SEE 52-81-14-01B FOR NHA
05A 010A D5288001021000 . SHEET-TEFLON VFAPE3 001
used on 001A
05A 020A D5288001021100 . SHEET-TEFLON VFAPE3 001
used on 002A
05A 040A LN9199-40C . RIVET VD8442 004
LN9199-4014CF D8442
Optional Vendor Code F0095
used on 001A, 002A
05A 050A ABS0257-5-400 . BOLT VFAPE3 001
OPT TO MBF2013S5-400 92215
OPT TO MBF2113S5-400 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 002A
05A 060A ABS0257-5-450 . BOLT VFAPE3 001
OPT TO MBF2013S5-450 92215
OPT TO MBF2113S5-450 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 002A
05A 070A ABS0257-5-500 . BOLT VFAPE3 001
OPT TO MBF2013S5-500 92215
OPT TO MBF2113S5-500 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 002A
05A 080A ABS0257-5-200 . BOLT VFAPE3 003
OPT TO ABS0257-5-200Z FAPE3
OPT TO MBF2013S5-200 92215
OPT TO MBF2113S5-200 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 002A
05A 090A D5288011620000 . SECTION-T VFAPE3 001
used on 001A
- ITEM NOT ILLUSTRATED

Page 10005A-1
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
05A 100A D5288011620100 . SECTION-T VFAPE3 001
used on 002A
05A 110A D5288011620200 . SECTION-T VFAPE3 001
used on 001A, 002A
05A 120A NAS1132E1 . SCREW V80205 006
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, 1RC86,
62384, 8Z507, C4293, F7411, FAWT4, K8753
used on 001A, 002A
05A 130A NAS1835C08 . INSERT V80205 003
OPT TO EF1835C08 C3898
OPT TO NSA5072-08A F6198
OPT TO SL606-08C 97393
Optional Vendor Code 83324, 97393, B1103, DM498
used on 001A, 002A
05A 140A D5288011020000 . SUPPORT VFAPE3 001
used on 001A
05A 150A D5288011020100 . SUPPORT VFAPE3 001
used on 002A
05A 160A D5288011120000 . SUPPORT- VFAPE3 001
used on 001A
05A 170A D5288011120100 . SUPPORT- VFAPE3 001
used on 002A
05A 180A D5288011220000 . SUPPORT VFAPE3 001
used on 001A
05A 190A D5288011220100 . SUPPORT VFAPE3 001
used on 002A
05A 200A D5288011320000 . TIP VFAPE3 001
used on 001A
05A 210A D5288011320100 . TIP VFAPE3 001
used on 002A
05A 220A MS21042-08 . NUT V96906 008
OPT TO H14L08CW 75237
OPT TO PLH3508 F0224
OPT TO RH30X08 52828
OPT TO T97S832CPF 11815
Optional Vendor Code 04795, 2N935, 60119, C5543
used on 001A, 002A
05A 225A MS21042-08 . NUT V96906 016
OPT TO H14L08CW 75237
OPT TO PLH3508 F0224
OPT TO RH30X08 52828
OPT TO T97S832CPF 11815
- ITEM NOT ILLUSTRATED

Page 10005A-2
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
Optional Vendor Code 04795, 2N935, 60119, C5543
used on 001A, 002A
05A 230A AN960C8L . WASHER V88044 008
NAS1149CN816R 80205
OPT TO ASNA2397C8L F6198
Optional Vendor Code 10630, 58009
used on 001A, 002A
05A 235A AN960C8L . WASHER V88044 016
NAS1149CN816R 80205
OPT TO ASNA2397C8L F6198
Optional Vendor Code 10630, 58009
used on 001A, 002A
05A 240A NAS1152E3 . SCREW V80205 008
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, F7411,
FAWT4, K8753
used on 001A, 002A
05A 245A NAS1152E3 . SCREW V80205 016
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, F7411,
FAWT4, K8753
used on 001A, 002A
05A 250A D5288010920000 . RAMP-BLISTER VFAPE3 001
used on 001A
05A 260A D5288010920100 . RAMP-BLISTER VFAPE3 001
used on 002A
- ITEM NOT ILLUSTRATED

Page 10005A-3
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

130 130
120
240
120
30 x7
220
A 230
30 x7

10
(20)

270 310
(280) (320) 120

250
(260) 240 330 x5
220
290 230
(300)
120

330 x5

70
130 x2 90
(100)
140
180 (150)
(190)
50
60
40

130
120
160
(170)

110

80
200
130 120 (210)
A
F_PL_528114_05_B_01_02

RAMP INSTL-CENTRAL
Figure 05B / FIGURE-52-81-14-950-805-B01

Page 10005B-0
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
05B - 001A D5288000800064 RAMP INSTL-CENTRAL VFAPE3 RF
used on 070B (528114010)
SEE 52-81-14-010 FOR NHA
05B - 001B D5288000900064 RAMP INSTL-CENTRAL VFAPE3 RF
used on 070B (52811401A)
SEE 52-81-14-01A FOR NHA
05B - 002A D5288000800164 RAMP INSTL-CENTRAL VFAPE3 RF
used on 080B (528114010)
SEE 52-81-14-010 FOR NHA
05B - 002B D5288000900164 RAMP INSTL-CENTRAL VFAPE3 RF
used on 080B (52811401A)
SEE 52-81-14-01A FOR NHA
05B 010A D5288000821000 . SHEET-TEFLON VFAPE3 001
used on 001A
05B 010B D5288000921000 . SHEET-TEFLON VFAPE3 001
used on 001B
05B 020A D5288000821100 . SHEET-TEFLON VFAPE3 001
used on 002A
05B 020B D5288000921100 . SHEET-TEFLON VFAPE3 001
used on 002B
05B 030A LN9198-24B . RIVET VD8442 014
Optional Vendor Code F0095
used on 001A, 001B, 002A, 002B
05B 040A LN9199-40C . RIVET VD8442 004
USE AS REQUIRED
LN9199-4014CF D8442
Optional Vendor Code F0095
used on 001A, 001B, 002A, 002B
05B 050A ABS0257-5-400 . BOLT VFAPE3 001
OPT TO MBF2013S5-400 92215
OPT TO MBF2113S5-400 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 001B, 002A, 002B
05B 060A ABS0257-5-450 . BOLT VFAPE3 001
OPT TO MBF2013S5-450 92215
OPT TO MBF2113S5-450 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 001B, 002A, 002B
- ITEM NOT ILLUSTRATED

Page 10005B-1
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
05B 070A ABS0257-5-500 . BOLT VFAPE3 001
OPT TO MBF2013S5-500 92215
OPT TO MBF2113S5-500 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 001B, 002A, 002B
05B 080A ABS0257-5-200 . BOLT VFAPE3 003
OPT TO ABS0257-5-200Z FAPE3
OPT TO MBF2013S5-200 92215
OPT TO MBF2113S5-200 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 001B, 002A, 002B
05B 090A D5288011620000 . SECTION-T VFAPE3 001
used on 001A, 001B
05B 100A D5288011620100 . SECTION-T VFAPE3 001
used on 002A, 002B
05B 110A D5288011620200 . SECTION-T VFAPE3 001
used on 001A, 001B, 002A, 002B
05B 120A NAS1132E1 . SCREW V80205 014
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, 1RC86,
62384, 8Z507, C4293, F7411, FAWT4, K8753
used on 001A, 001B, 002A, 002B
05B 130A NAS1835C08 . INSERT V80205 014
OPT TO EF1835C08 C3898
OPT TO NSA5072-08A F6198
OPT TO SL606-08C 97393
Optional Vendor Code 83324, 97393, B1103, DM498
used on 001A, 001B, 002A, 002B
05B 140A D5288011020000 . SUPPORT VFAPE3 001
used on 001A, 001B
05B 150A D5288011020100 . SUPPORT VFAPE3 001
used on 002A, 002B
05B 160A D5288011120000 . SUPPORT- VFAPE3 001
used on 001A, 001B
05B 170A D5288011120100 . SUPPORT- VFAPE3 001
used on 002A, 002B
05B 180A D5288011220000 . SUPPORT VFAPE3 001
used on 001A, 001B
05B 190A D5288011220100 . SUPPORT VFAPE3 001
used on 002A, 002B
- ITEM NOT ILLUSTRATED

Page 10005B-2
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
05B 200A D5288011320000 . TIP VFAPE3 001
used on 001A, 001B
05B 210A D5288011320100 . TIP VFAPE3 001
used on 002A, 002B
05B 220A MS21042-08 . NUT V96906 008
OPT TO H14L08CW 75237
OPT TO PLH3508 F0224
OPT TO RH30X08 52828
OPT TO T97S832CPF 11815
Optional Vendor Code 04795, 2N935, 60119, C5543
used on 001A, 001B, 002A, 002B
05B 230A AN960C8L . WASHER V88044 008
NAS1149CN816R 80205
OPT TO ASNA2397C8L F6198
Optional Vendor Code 10630, 58009
used on 001A, 001B, 002A, 002B
05B 240A NAS1152E3 . SCREW V80205 008
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, F7411,
FAWT4, K8753
used on 001A, 001B, 002A, 002B
05B 250A D5288011500000 . RAMP-BLISTER VFAPE3 001
used on 001A
05B 250B D5288011400000 . RAMP-BLISTER VFAPE3 001
used on 001B
05B 260A D5288011500100 . RAMP-BLISTER VFAPE3 001
used on 002A
05B 260B D5288011400100 . RAMP-BLISTER VFAPE3 001
used on 002B
05B 270A D5288011520200 .. RAMP-BLISTER VFAPE3 001
used on 250A
05B 270B D5288011420200 .. RAMP-BLISTER VFAPE3 001
used on 250B
05B 280A D5288011520300 .. RAMP-BLISTER VFAPE3 001
used on 260A
05B 280B D5288011420300 .. RAMP-BLISTER VFAPE3 001
used on 260B
05B 290A D5288011520400 .. ANGLE VFAPE3 001
MODIFIED FROM D5288011520401 MADE BY
FAPE3
used on 250A, 250B
- ITEM NOT ILLUSTRATED

Page 10005B-3
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
05B 300A D5288011520500 .. ANGLE VFAPE3 001
MODIFIED FROM D5288011520501 MADE BY
FAPE3
used on 260A, 260B
05B 310A D5288011520600 .. ANGLE VFAPE3 001
MODIFIED FROM D5288011520601 MADE BY
FAPE3
used on 250A, 250B
05B 320A D5288011520700 .. ANGLE VFAPE3 001
MODIFIED FROM D5288011520701 MADE BY
FAPE3
used on 260A, 260B
05B 330A ABS0326-5-6 .. RIVET VFAPE3 010
OPT TO CSR903T5W06 11815
Optional Vendor Code 04795, 11815, 2N935, 53551,
C5543, F0095
used on 250A, 250B, 260A, 260B
- ITEM NOT ILLUSTRATED

Page 10005B-4
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

130 130
240 120

220 120
230
225
A 235
10
(20)

245

310
(320)
250 270 330
(260) (280)

240 120
290 220
(300) 230
120
130

330

70
130 90
(100)
140
180 (150)
(190)
50
60
40

130
120
160
(170)

110

80
200
130 120 (210)
A
F_PL_528114_05_C_01_02

RAMP INSTL-CENTRAL
Figure 05C / FIGURE-52-81-14-950-805-C01

Page 10005C-0
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
05C - 001A D5288001000063 RAMP INSTL-CENTRAL VFAPE3 RF
used on 070B (52811401B)
SEE 52-81-14-01B FOR NHA
05C - 002A D5288001000163 RAMP INSTL-CENTRAL VFAPE3 RF
used on 080B (52811401B)
SEE 52-81-14-01B FOR NHA
05C 010A D5288001021000 . SHEET-TEFLON VFAPE3 001
used on 001A
05C 020A D5288001021100 . SHEET-TEFLON VFAPE3 001
used on 002A
05C 040A LN9199-40C . RIVET VD8442 004
LN9199-4014CF D8442
Optional Vendor Code F0095
used on 001A, 002A
05C 050A ABS0257-5-400 . BOLT VFAPE3 001
OPT TO MBF2013S5-400 92215
OPT TO MBF2113S5-400 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 002A
05C 060A ABS0257-5-450 . BOLT VFAPE3 001
OPT TO MBF2013S5-450 92215
OPT TO MBF2113S5-450 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 002A
05C 070A ABS0257-5-500 . BOLT VFAPE3 001
OPT TO MBF2013S5-500 92215
OPT TO MBF2113S5-500 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 002A
05C 080A ABS0257-5-200 . BOLT VFAPE3 003
OPT TO ABS0257-5-200Z FAPE3
OPT TO MBF2013S5-200 92215
OPT TO MBF2113S5-200 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 002A
05C 090A D5288011620000 . SECTION-T VFAPE3 001
used on 001A
- ITEM NOT ILLUSTRATED

Page 10005C-1
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
05C 100A D5288011620100 . SECTION-T VFAPE3 001
used on 002A
05C 110A D5288011620200 . SECTION-T VFAPE3 001
used on 001A, 002A
05C 120A NAS1132E1 . SCREW V80205 014
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, 1RC86,
62384, 8Z507, C4293, F7411, FAWT4, K8753
used on 001A, 002A
05C 130A NAS1835C08 . INSERT V80205 014
OPT TO EF1835C08 C3898
OPT TO NSA5072-08A F6198
OPT TO SL606-08C 97393
Optional Vendor Code 83324, 97393, B1103, DM498
used on 001A, 002A
05C 140A D5288011020000 . SUPPORT VFAPE3 001
used on 001A
05C 150A D5288011020100 . SUPPORT VFAPE3 001
used on 002A
05C 160A D5288011120000 . SUPPORT- VFAPE3 001
used on 001A
05C 170A D5288011120100 . SUPPORT- VFAPE3 001
used on 002A
05C 180A D5288011220000 . SUPPORT VFAPE3 001
used on 001A
05C 190A D5288011220100 . SUPPORT VFAPE3 001
used on 002A
05C 200A D5288011320000 . TIP VFAPE3 001
used on 001A
05C 210A D5288011320100 . TIP VFAPE3 001
used on 002A
05C 220A MS21042-08 . NUT V96906 008
OPT TO H14L08CW 75237
OPT TO PLH3508 F0224
OPT TO RH30X08 52828
OPT TO T97S832CPF 11815
Optional Vendor Code 04795, 2N935, 60119, C5543
used on 001A, 002A
05C 225A MS21042-08 . NUT V96906 016
OPT TO H14L08CW 75237
OPT TO PLH3508 F0224
OPT TO RH30X08 52828
OPT TO T97S832CPF 11815
- ITEM NOT ILLUSTRATED

Page 10005C-2
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
Optional Vendor Code 04795, 2N935, 60119, C5543
used on 001A, 002A
05C 230A AN960C8L . WASHER V88044 008
NAS1149CN816R 80205
OPT TO ASNA2397C8L F6198
Optional Vendor Code 10630, 58009
used on 001A, 002A
05C 235A AN960C8L . WASHER V88044 016
NAS1149CN816R 80205
OPT TO ASNA2397C8L F6198
Optional Vendor Code 10630, 58009
used on 001A, 002A
05C 240A NAS1152E3 . SCREW V80205 008
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, F7411,
FAWT4, K8753
used on 001A, 002A
05C 245A NAS1152E3 . SCREW V80205 016
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, F7411,
FAWT4, K8753
used on 001A, 002A
05C 250A D5288010900000 . RAMP-BLISTER VFAPE3 001
used on 001A
05C 260A D5288010900100 . RAMP-BLISTER VFAPE3 001
used on 002A
05C 270A D5288010920200 .. RAMP-BLISTER VFAPE3 001
used on 250A
05C 280A D5288010920300 .. RAMP-BLISTER VFAPE3 001
used on 260A
05C 290A D5288010920400 .. ANGLE VFAPE3 001
used on 250A
05C 300A D5288010920500 .. ANGLE VFAPE3 001
used on 260A
05C 310A D5288010920600 .. ANGLE VFAPE3 001
used on 250A
05C 320A D5288010920700 .. ANGLE VFAPE3 001
used on 260A
05C 330A ABS0326-5-6 .. RIVET VFAPE3 009
OPT TO CSR903T5W06 11815
Optional Vendor Code 04795, 11815, 2N935, 53551,
C5543, F0095
used on 250A, 260A
- ITEM NOT ILLUSTRATED

Page 10005C-3
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

130 350

130 130
120

120

A 340 330
330 120
30

10
(20)
240
220
230
330
360

120

310
270 (320)
(280)
240 220
230 130
330
250 120
(260)
290
(300)
70
130
140
(150)
90
(100) 180
(190) 50 60

40
130

120
160
(170)
110

200
130 (210)
120
A 80
F_PL_528114_05_D_01_01

RAMP INSTL-CENTRAL
Figure 05D / FIGURE-52-81-14-950-805-D01

Page 10005D-0
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
05D - 001A D5288000800064 RAMP INSTL-CENTRAL VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
used on 070A (52811401C)
SEE 52-81-14-01C FOR NHA
05D - 001B D5288000900064 RAMP INSTL-CENTRAL VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
used on 070A (52811401D)
SEE 52-81-14-01D FOR NHA
05D - 002A D5288000800164 RAMP INSTL-CENTRAL VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
used on 080A (52811401C)
SEE 52-81-14-01C FOR NHA
05D - 002B D5288000900164 RAMP INSTL-CENTRAL VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
used on 080A (52811401D)
SEE 52-81-14-01D FOR NHA
05D 010A D5288016520851 . SHEET-TEFLON VFAPE3 001
used on 001A, 001B
05D 020A D5288016520951 . SHEET-TEFLON VFAPE3 001
used on 002A, 002B
05D 030A LN9198-24B . RIVET VD8442 014
USE AS REQUIRED
Optional Vendor Code F0095
used on 001A, 001B, 002A, 002B
05D 040A LN9199-40C . RIVET VD8442 004
USE AS REQUIRED
LN9199-4014CF D8442
Optional Vendor Code F0095
used on 001A, 001B, 002A, 002B
05D 050A ABS0257-5-400 . BOLT VFAPE3 001
OPT TO MBF2013S5-400 92215
OPT TO MBF2113S5-400 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 001B, 002A, 002B
05D 060A ABS0257-5-450 . BOLT VFAPE3 001
OPT TO MBF2013S5-450 92215
OPT TO MBF2113S5-450 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 001B, 002A, 002B
- ITEM NOT ILLUSTRATED

Page 10005D-1
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
05D 070A ABS0257-5-500 . BOLT VFAPE3 001
OPT TO MBF2013S5-500 92215
OPT TO MBF2113S5-500 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 001B, 002A, 002B
05D 080A ABS0257-5-200 . BOLT VFAPE3 003
OPT TO ABS0257-5-200Z FAPE3
OPT TO MBF2013S5-200 92215
OPT TO MBF2113S5-200 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 001B, 002A, 002B
05D 090A D5288011620000 . SECTION-T VFAPE3 001
used on 001A, 001B
05D 100A D5288011620100 . SECTION-T VFAPE3 001
used on 002A, 002B
05D 110A D5288011620200 . SECTION-T VFAPE3 001
used on 001A, 001B, 002A, 002B
05D 120A NAS1132E1 . SCREW V80205 014
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, 1RC86,
62384, 8Z507, C4293, F7411, FAWT4, K8753
used on 001A, 001B, 002A, 002B
05D 130A NAS1835C08 . INSERT V80205 014
OPT TO EF1835C08 C3898
OPT TO NSA5072-08A F6198
OPT TO SL606-08C 97393
Optional Vendor Code 83324, 97393, B1103, DM498
used on 001A, 001B, 002A, 002B
05D 140A D5288011020000 . SUPPORT VFAPE3 001
used on 001A, 001B
05D 150A D5288011020100 . SUPPORT VFAPE3 001
used on 002A, 002B
05D 160A D5288011120000 . SUPPORT- VFAPE3 001
used on 001A, 001B
05D 170A D5288011120100 . SUPPORT- VFAPE3 001
used on 002A, 002B
05D 180A D5288011220000 . SUPPORT VFAPE3 001
used on 001A, 001B
05D 190A D5288011220100 . SUPPORT VFAPE3 001
used on 002A, 002B
- ITEM NOT ILLUSTRATED

Page 10005D-2
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
05D 200A D5288011320000 . TIP VFAPE3 001
PRE SB 52-1140
used on 001A, 001B
05D 210A D5288011320100 . TIP VFAPE3 001
PRE SB 52-1140
used on 002A, 002B
05D 220A MS21042-08 . NUT V96906 016
OPT TO H14L08CW 75237
OPT TO PLH3508 F0224
OPT TO RH30X08 52828
OPT TO T97S832CPF 11815
Optional Vendor Code 04795, 2N935, 60119, C5543
used on 001A, 001B, 002A, 002B
05D 230A AN960C8L . WASHER V88044 016
NAS1149CN816R 80205
OPT TO ASNA2397C8L F6198
Optional Vendor Code 10630, 58009
used on 001A, 001B, 002A, 002B
05D 240A NAS1152E3 . SCREW V80205 016
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, F7411,
FAWT4, K8753
used on 001A, 001B, 002A, 002B
05D 250A D5288010900200 . RAMP-BLISTER VFAPE3 001
used on 001A, 001B
05D 260A D5288010900300 . RAMP-BLISTER VFAPE3 001
POST SB 52-1025
used on 002A, 002B
05D 270A D5288010920895 .. RAMP-BLISTER VFAPE3 001
POST SB 52-1025
used on 250A
05D 280A D5288010920995 .. RAMP-BLISTER VFAPE3 001
POST SB 52-1025
used on 260A
05D 290A D5288010920495 .. ANGLE VFAPE3 001
POST SB 52-1025
used on 250A
05D 300A D5288010920595 .. ANGLE VFAPE3 001
POST SB 52-1025
used on 260A
05D 310A D5288010920695 .. ANGLE VFAPE3 001
POST SB 52-1025
used on 250A
- ITEM NOT ILLUSTRATED

Page 10005D-3
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
05D 320A D5288010920795 .. ANGLE VFAPE3 001
POST SB 52-1025
used on 260A
05D 330A ABS0326-5-6 .. RIVET VFAPE3 015
POST SB 52-1025
OPT TO CSR903T5W06 11815
Optional Vendor Code 04795, 11815, 2N935, 53551,
C5543, F0095
used on 250A, 260A
05D 340A D5288010921095 .. ANGLE VFAPE3 001
POST SB 52-1025
used on 250A, 260A
05D 350A D5288010921195 .. ANGLE VFAPE3 001
POST SB 52-1025
used on 250A, 260A
05D 360A ABS0213-5-4R .. RIVET VFAPE3 008
POST SB 52-1025
OPT TO CSR922-5WA04R 11815
Optional Vendor Code 04795, 11815, 2N935, C5543
used on 250A, 260A
- ITEM NOT ILLUSTRATED

Page 10005D-4
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

130 130

240
120
120
220
230
A

245
225 10
235 (20)
340
310
270 (320)
(280)
220 330
230
240 120
250
(260) 120
290 130
(300)

330

130 140 70
(150)

90
(100) 180
(190) 50 60

40
130

120
160
(170)
110

200
(210)
130 A 120
80 F_PL_528114_05_E_01_01

RAMP INSTL-CENTRAL
Figure 05E / FIGURE-52-81-14-950-805-E01

Page 10005E-0
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
05E - 001A D5288001000063 RAMP INSTL-CENTRAL VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
used on 070A (52811401E)
SEE 52-81-14-01E FOR NHA
05E - 002A D5288001000163 RAMP INSTL-CENTRAL VFAPE3 RF
POST SB 52-1025, PRE SB 52-1140
used on 080A (52811401E)
SEE 52-81-14-01E FOR NHA
05E 010A D5288001021000 . SHEET-TEFLON VFAPE3 001
used on 001A
05E 020A D5288001021100 . SHEET-TEFLON VFAPE3 001
used on 002A
05E 040A LN9199-40C . RIVET VD8442 004
USE AS REQUIRED
LN9199-4014CF D8442
Optional Vendor Code F0095
used on 001A, 002A
05E 050A ABS0257-5-400 . BOLT VFAPE3 001
OPT TO MBF2013S5-400 92215
OPT TO MBF2113S5-400 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 002A
05E 060A ABS0257-5-450 . BOLT VFAPE3 001
OPT TO MBF2013S5-450 92215
OPT TO MBF2113S5-450 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 002A
05E 070A ABS0257-5-500 . BOLT VFAPE3 001
OPT TO MBF2013S5-500 92215
OPT TO MBF2113S5-500 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 002A
05E 080A ABS0257-5-200 . BOLT VFAPE3 003
OPT TO ABS0257-5-200Z FAPE3
OPT TO MBF2013S5-200 92215
OPT TO MBF2113S5-200 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 002A
- ITEM NOT ILLUSTRATED

Page 10005E-1
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
05E 090A D5288011620000 . SECTION-T VFAPE3 001
used on 001A
05E 100A D5288011620100 . SECTION-T VFAPE3 001
used on 002A
05E 110A D5288011620200 . SECTION-T VFAPE3 001
used on 001A, 002A
05E 120A NAS1132E1 . SCREW V80205 014
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, 1RC86,
62384, 8Z507, C4293, F7411, FAWT4, K8753
used on 001A, 002A
05E 130A NAS1835C08 . INSERT V80205 014
OPT TO EF1835C08 C3898
OPT TO NSA5072-08A F6198
OPT TO SL606-08C 97393
Optional Vendor Code 83324, 97393, B1103, DM498
used on 001A, 002A
05E 140A D5288011020000 . SUPPORT VFAPE3 001
used on 001A
05E 150A D5288011020100 . SUPPORT VFAPE3 001
used on 002A
05E 160A D5288011120000 . SUPPORT- VFAPE3 001
used on 001A
05E 170A D5288011120100 . SUPPORT- VFAPE3 001
used on 002A
05E 180A D5288011220000 . SUPPORT VFAPE3 001
used on 001A
05E 190A D5288011220100 . SUPPORT VFAPE3 001
used on 002A
05E 200A D5288011320000 . TIP VFAPE3 001
PRE SB 52-1140
used on 001A
05E 210A D5288011320100 . TIP VFAPE3 001
PRE SB 52-1140
used on 002A
05E 220A MS21042-08 . NUT V96906 006
OPT TO H14L08CW 75237
OPT TO PLH3508 F0224
OPT TO RH30X08 52828
OPT TO T97S832CPF 11815
Optional Vendor Code 04795, 2N935, 60119, C5543
used on 001A, 002A
- ITEM NOT ILLUSTRATED

Page 10005E-2
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
05E 225A MS21042-08 . NUT V96906 010
OPT TO H14L08CW 75237
OPT TO PLH3508 F0224
OPT TO RH30X08 52828
OPT TO T97S832CPF 11815
Optional Vendor Code 04795, 2N935, 60119, C5543
used on 001A, 002A
05E 230A AN960C8L . WASHER V88044 006
NAS1149CN816R 80205
OPT TO ASNA2397C8L F6198
Optional Vendor Code 10630, 58009
used on 001A, 002A
05E 235A AN960C8L . WASHER V88044 010
NAS1149CN816R 80205
OPT TO ASNA2397C8L F6198
Optional Vendor Code 10630, 58009
used on 001A, 002A
05E 240A NAS1152E3 . SCREW V80205 006
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, F7411,
FAWT4, K8753
used on 001A, 002A
05E 245A NAS1152E3 . SCREW V80205 010
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, F7411,
FAWT4, K8753
used on 001A, 002A
05E 250A D5288010900000 . RAMP-BLISTER VFAPE3 001
used on 001A
05E 260A D5288010900100 . RAMP-BLISTER VFAPE3 001
used on 002A
05E 270A D5288010920200 .. RAMP-BLISTER VFAPE3 001
used on 250A
05E 280A D5288010920300 .. RAMP-BLISTER VFAPE3 001
used on 260A
05E 290A D5288010920400 .. ANGLE VFAPE3 001
used on 250A
05E 300A D5288010920500 .. ANGLE VFAPE3 001
used on 260A
05E 310A D5288010920600 .. ANGLE VFAPE3 001
used on 250A
05E 320A D5288010920700 .. ANGLE VFAPE3 001
used on 260A
- ITEM NOT ILLUSTRATED

Page 10005E-3
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
05E 330A ABS0326-5-6 .. RIVET VFAPE3 009
OPT TO CSR903T5W06 11815
Optional Vendor Code 04795, 11815, 2N935, 53551,
C5543, F0095
used on 250A, 260A
05E 340A ABS0213-5-4R . RIVET VFAPE3 008
POST SB 52-1025
OPT TO CSR922-5WA04R 11815
Optional Vendor Code 04795, 11815, 2N935, C5543
used on 001A, 002A
- ITEM NOT ILLUSTRATED

Page 10005E-4
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

130 350
120
130 130
120

120

340 330
A
330

240
220
230

360
330

270 120
(280)
240 220 310
230 (320)
330
250 120
(260) 130
290
(300)

130 70
140
(150)
90
(100) 180
(190) 60
50

40
130

120
160
(170)
110

200
130 (210)
120
A 80
F_PL_528114_05_F_01_00

RAMP INSTL-CENTRAL
Figure 05F / FIGURE-52-81-14-950-805-F01

Page 10005F-0
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
05F - 001A D5288000800064 RAMP INSTL-CENTRAL VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
used on 070A (52811401F)
SEE 52-81-14-01F FOR NHA
05F - 001B D5288000900064 RAMP INSTL-CENTRAL VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
used on 070B (52811401D)
SEE 52-81-14-01D FOR NHA
05F - 002A D5288000800164 RAMP INSTL-CENTRAL VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
used on 080A (52811401F)
SEE 52-81-14-01F FOR NHA
05F - 002B D5288000900164 RAMP INSTL-CENTRAL VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
used on 080B (52811401D)
SEE 52-81-14-01D FOR NHA
05F 040A LN9199-40C . RIVET VD8442 004
USE AS REQUIRED
LN9199-4014CF D8442
Optional Vendor Code F0095
used on 001A, 001B, 002A, 002B
05F 050A ABS0257-5-400 . BOLT VFAPE3 001
OPT TO MBF2013S5-400 92215
OPT TO MBF2113S5-400 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 001B, 002A, 002B
05F 060A ABS0257-5-450 . BOLT VFAPE3 001
OPT TO MBF2013S5-450 92215
OPT TO MBF2113S5-450 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 001B, 002A, 002B
05F 070A ABS0257-5-500 . BOLT VFAPE3 001
OPT TO MBF2013S5-500 92215
OPT TO MBF2113S5-500 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 001B, 002A, 002B
- ITEM NOT ILLUSTRATED

Page 10005F-1
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
05F 080A ABS0257-5-200 . BOLT VFAPE3 003
OPT TO ABS0257-5-200Z FAPE3
OPT TO MBF2013S5-200 92215
OPT TO MBF2113S5-200 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 001B, 002A, 002B
05F 090A D5288011620000 . SECTION-T VFAPE3 001
used on 001A, 001B
05F 100A D5288011620100 . SECTION-T VFAPE3 001
used on 002A, 002B
05F 110A D5288011620200 . SECTION-T VFAPE3 001
used on 001A, 001B, 002A, 002B
05F 120A NAS1132E1 . SCREW V80205 014
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, 1RC86,
62384, 8Z507, C4293, F7411, FAWT4, K8753
used on 001A, 001B, 002A, 002B
05F 130A NAS1835C08 . INSERT V80205 014
OPT TO EF1835C08 C3898
OPT TO NSA5072-08A F6198
OPT TO SL606-08C 97393
Optional Vendor Code 83324, 97393, B1103, DM498
used on 001A, 001B, 002A, 002B
05F 140A D5288011020000 . SUPPORT VFAPE3 001
used on 001A, 001B
05F 150A D5288011020100 . SUPPORT VFAPE3 001
used on 002A, 002B
05F 160A D5288011120000 . SUPPORT- VFAPE3 001
used on 001A, 001B
05F 170A D5288011120100 . SUPPORT- VFAPE3 001
used on 002A, 002B
05F 180A D5288011220000 . SUPPORT VFAPE3 001
used on 001A, 001B
05F 190A D5288011220100 . SUPPORT VFAPE3 001
used on 002A, 002B
05F 200A D5288011320295 . TIP RUNOUT VFAPE3 001
POST SB 52-1140
used on 001A, 001B
05F 210A D5288011320395 . TIP RUNOUT VFAPE3 001
POST SB 52-1140
used on 002A, 002B
- ITEM NOT ILLUSTRATED

Page 10005F-2
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
05F 220A MS21042-08 . NUT V96906 016
OPT TO H14L08CW 75237
OPT TO PLH3508 F0224
OPT TO RH30X08 52828
OPT TO T97S832CPF 11815
Optional Vendor Code 04795, 2N935, 60119, C5543
used on 001A, 001B, 002A, 002B
05F 230A AN960C8L . WASHER V88044 016
NAS1149CN816R 80205
OPT TO ASNA2397C8L F6198
Optional Vendor Code 10630, 58009
used on 001A, 001B, 002A, 002B
05F 240A NAS1152E3 . SCREW V80205 016
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, F7411,
FAWT4, K8753
used on 001A, 001B, 002A, 002B
05F 250A D5288010900200 . RAMP-BLISTER VFAPE3 001
used on 001A, 001B
05F 260A D5288010900300 . RAMP-BLISTER VFAPE3 001
POST SB 52-1025
used on 002A, 002B
05F 270A D5288010920895 .. RAMP-BLISTER VFAPE3 001
POST SB 52-1025
used on 250A
05F 280A D5288010920995 .. RAMP-BLISTER VFAPE3 001
POST SB 52-1025
used on 260A
05F 290A D5288010920495 .. ANGLE VFAPE3 001
POST SB 52-1025
used on 250A
05F 300A D5288010920595 .. ANGLE VFAPE3 001
POST SB 52-1025
used on 260A
05F 310A D5288010920695 .. ANGLE VFAPE3 001
POST SB 52-1025
used on 250A
05F 320A D5288010920795 .. ANGLE VFAPE3 001
POST SB 52-1025
used on 260A
05F 330A ABS0326-5-6 .. RIVET VFAPE3 015
POST SB 52-1025
OPT TO CSR903T5W06 11815
- ITEM NOT ILLUSTRATED

Page 10005F-3
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
Optional Vendor Code 04795, 11815, 2N935, 53551,
C5543, F0095
used on 250A, 260A
05F 340A D5288010921095 .. ANGLE VFAPE3 001
POST SB 52-1025
used on 250A, 260A
05F 350A D5288010921195 .. ANGLE VFAPE3 001
POST SB 52-1025
used on 250A, 260A
05F 360A ABS0213-5-4R .. RIVET VFAPE3 008
POST SB 52-1025
OPT TO CSR922-5WA04R 11815
Optional Vendor Code 04795, 11815, 2N935, C5543
used on 250A, 260A
- ITEM NOT ILLUSTRATED

Page 10005F-4
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

130 130 120

240 120

A 220
230

245

225
235 340

270
(280)
310
220 (320)
230
240 330
250
(260) 120
290 120
(300)
130
330

130 140
(150) 70

90
(100) 180
(190) 60
50

40
130

120
160
(170)
110

200
(210)
130 A 120 80
F_PL_528114_05_G_01_01

RAMP INSTL-CENTRAL
Figure 05G / FIGURE-52-81-14-950-805-G01

Page 10005G-0
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
05G - 001A D5288001000063 RAMP INSTL-CENTRAL VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
used on 070B (52811401E)
SEE 52-81-14-01E FOR NHA
05G - 002A D5288001000163 RAMP INSTL-CENTRAL VFAPE3 RF
POST SB 52-1140, POST SB 52-1025
used on 080B (52811401E)
SEE 52-81-14-01E FOR NHA
05G 040A LN9199-40C . RIVET VD8442 004
USE AS REQUIRED
LN9199-4014CF D8442
Optional Vendor Code F0095
used on 001A, 002A
05G 050A ABS0257-5-400 . BOLT VFAPE3 001
OPT TO MBF2013S5-400 92215
OPT TO MBF2113S5-400 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 002A
05G 060A ABS0257-5-450 . BOLT VFAPE3 001
OPT TO MBF2013S5-450 92215
OPT TO MBF2113S5-450 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 002A
05G 070A ABS0257-5-500 . BOLT VFAPE3 001
OPT TO MBF2013S5-500 92215
OPT TO MBF2113S5-500 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 002A
05G 080A ABS0257-5-200 . BOLT VFAPE3 003
OPT TO ABS0257-5-200Z FAPE3
OPT TO MBF2013S5-200 92215
OPT TO MBF2113S5-200 92215
Optional Vendor Code 04795, 2N935, 5M902, 98524,
C5543
used on 001A, 002A
05G 090A D5288011620000 . SECTION-T VFAPE3 001
used on 001A
05G 100A D5288011620100 . SECTION-T VFAPE3 001
used on 002A
- ITEM NOT ILLUSTRATED

Page 10005G-1
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
05G 110A D5288011620200 . SECTION-T VFAPE3 001
used on 001A, 002A
05G 120A NAS1132E1 . SCREW V80205 014
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, 1RC86,
62384, 8Z507, C4293, F7411, FAWT4, K8753
used on 001A, 002A
05G 130A NAS1835C08 . INSERT V80205 014
OPT TO EF1835C08 C3898
OPT TO NSA5072-08A F6198
OPT TO SL606-08C 97393
Optional Vendor Code 83324, 97393, B1103, DM498
used on 001A, 002A
05G 140A D5288011020000 . SUPPORT VFAPE3 001
used on 001A
05G 150A D5288011020100 . SUPPORT VFAPE3 001
used on 002A
05G 160A D5288011120000 . SUPPORT- VFAPE3 001
used on 001A
05G 170A D5288011120100 . SUPPORT- VFAPE3 001
used on 002A
05G 180A D5288011220000 . SUPPORT VFAPE3 001
used on 001A
05G 190A D5288011220100 . SUPPORT VFAPE3 001
used on 002A
05G 200A D5288011320295 . TIP RUNOUT VFAPE3 001
POST SB 52-1140
used on 001A
05G 210A D5288011320395 . TIP RUNOUT VFAPE3 001
POST SB 52-1140
used on 002A
05G 220A MS21042-08 . NUT V96906 006
OPT TO H14L08CW 75237
OPT TO PLH3508 F0224
OPT TO RH30X08 52828
OPT TO T97S832CPF 11815
Optional Vendor Code 04795, 2N935, 60119, C5543
used on 001A, 002A
05G 225A MS21042-08 . NUT V96906 010
OPT TO H14L08CW 75237
OPT TO PLH3508 F0224
OPT TO RH30X08 52828
OPT TO T97S832CPF 11815
- ITEM NOT ILLUSTRATED

Page 10005G-2
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
Optional Vendor Code 04795, 2N935, 60119, C5543
used on 001A, 002A
05G 230A AN960C8L . WASHER V88044 006
NAS1149CN816R 80205
OPT TO ASNA2397C8L F6198
Optional Vendor Code 10630, 58009
used on 001A, 002A
05G 235A AN960C8L . WASHER V88044 010
NAS1149CN816R 80205
OPT TO ASNA2397C8L F6198
Optional Vendor Code 10630, 58009
used on 001A, 002A
05G 240A NAS1152E3 . SCREW V80205 006
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, F7411,
FAWT4, K8753
used on 001A, 002A
05G 245A NAS1152E3 . SCREW V80205 010
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, F7411,
FAWT4, K8753
used on 001A, 002A
05G 250A D5288010900000 . RAMP-BLISTER VFAPE3 001
used on 001A
05G 260A D5288010900100 . RAMP-BLISTER VFAPE3 001
used on 002A
05G 270A D5288010920200 .. RAMP-BLISTER VFAPE3 001
used on 250A
05G 280A D5288010920300 .. RAMP-BLISTER VFAPE3 001
used on 260A
05G 290A D5288010920400 .. ANGLE VFAPE3 001
used on 250A
05G 300A D5288010920500 .. ANGLE VFAPE3 001
used on 260A
05G 310A D5288010920600 .. ANGLE VFAPE3 001
used on 250A
05G 320A D5288010920700 .. ANGLE VFAPE3 001
used on 260A
05G 330A ABS0326-5-6 .. RIVET VFAPE3 009
OPT TO CSR903T5W06 11815
Optional Vendor Code 04795, 11815, 2N935, 53551,
C5543, F0095
used on 250A, 260A
- ITEM NOT ILLUSTRATED

Page 10005G-3
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
05G 340A ABS0213-5-4R . RIVET VFAPE3 008
POST SB 52-1025
OPT TO CSR922-5WA04R 11815
Optional Vendor Code 04795, 11815, 2N935, C5543
used on 001A, 002A
- ITEM NOT ILLUSTRATED

Page 10005G-4
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

320
310
D
340
310

A 310
A B

330
B
C
C TYPICAL

220
350 E (230)
(360) C 200 140
(210)
120

10
100 190

20 40 30
50 90
80
180 70 240
60
250
170
270
150 (280)
(160)
D
110
130

290
(300)
260 E
F_PL_528114_06_0_01_01

COVER ASSY
Figure 06 / FIGURE-52-81-14-950-806-01

Page 10006-0
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
06 - 001A D5288010000074 COVER ASSY VFAPE3 RF
used on 090A (528114010), 090A (52811401A), 090A
(52811401B), 090A (52811401C), 090A (52811401D),
090A (52811401E), 090A (52811401F)
SEE 52-81-14-010 FOR NHA, SEE 52-81-14-01A FOR
NHA, SEE 52-81-14-01B FOR NHA, SEE
52-81-14-01C FOR NHA, SEE 52-81-14-01D FOR
NHA, SEE 52-81-14-01E FOR NHA, SEE 52-81-14-01F
FOR NHA
06 - 001B D5288010000074 COVER ASSY VFAPE3 RF
used on 090B (528114010), 090B (52811401A), 090B
(52811401C), 090B (52811401D), 090B (52811401F)
SEE 52-81-14-010 FOR NHA, SEE 52-81-14-01A FOR
NHA, SEE 52-81-14-01C FOR NHA, SEE
52-81-14-01D FOR NHA, SEE 52-81-14-01F FOR NHA
06 - 002A D5288010000174 COVER ASSY VFAPE3 RF
used on 100A (528114010), 100A (52811401A), 100A
(52811401B), 100A (52811401C), 100A (52811401D),
100A (52811401E), 100A (52811401F)
SEE 52-81-14-010 FOR NHA, SEE 52-81-14-01A FOR
NHA, SEE 52-81-14-01B FOR NHA, SEE
52-81-14-01C FOR NHA, SEE 52-81-14-01D FOR
NHA, SEE 52-81-14-01E FOR NHA, SEE 52-81-14-01F
FOR NHA
06 - 002B D5288010000174 COVER ASSY VFAPE3 RF
used on 100B (528114010), 100B (52811401A), 100B
(52811401C), 100B (52811401D), 100B (52811401F)
SEE 52-81-14-010 FOR NHA, SEE 52-81-14-01A FOR
NHA, SEE 52-81-14-01C FOR NHA, SEE
52-81-14-01D FOR NHA, SEE 52-81-14-01F FOR NHA
06 010A ABS0251-5-7 . FASTENER-HI-LOK VFAPE3 008
DAN6-5-7 D8518
OPT TO HL11VBJ5-7 92215
Optional Vendor Code 04795, 2N935, 56878, 73197,
C5543
used on 001A, 001B, 002A, 002B
06 020A NSA5075-5 . COLLAR VF6198 008
OPT TO DAN11-5 D8518
OPT TO F0N2-1181-5 H1822
OPT TO HL70AA5 92215
- ITEM NOT ILLUSTRATED

Page 10006-1
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
Optional Vendor Code 04795, 2N935, 56878, 5M902,
73197, 80539, C5543, U6300
used on 001A, 001B, 002A, 002B
06 030A D5288010600000 . SUPPORT ASSY-SENSOR VFAPE3 002
used on 001A, 001B, 002A, 002B
06 040A MS21042L3 .. NUT V96906 002
OPT TO AS8600D U1653
OPT TO H14-3 15653
OPT TO PLH353M F0224
OPT TO RH30A3 52828
OPT TO RM52LH3324-02 72962
OPT TO T98S1032 11815
OPT TO VN300A02 92215
Optional Vendor Code 04795, 06329, 1BGN6, 2N935,
60996, 8K160, C5543, R1120
used on 030A
06 050A AN960-10L .. WASHER V88044 002
NAS1149F0332P 80205
OPT TO ASNA2397-10L F6198
Optional Vendor Code 10630, 58009, 8K160, F8982
used on 030A
06 060A NAS1133-3W .. SCREW V80205 002
Optional Vendor Code 62384, C4293
used on 030A
06 070A ABS0121-11 .. TARGET VFAPE3 001
OPT TO 666000078 K0654
OPT TO 8-368-04 08748
Optional Vendor Code 04795, 08748, 2N935, C5543,
K0653
used on 030A
06 080A D5288014420000 .. SHIM VFAPE3 001
used on 030A
06 090A D5288014220000 .. SUPPORT-SENSOR VFAPE3 001
MODIFIED FROM D5288014220001 MADE BY
FAPE3
used on 030A
06 100A ABS0214-4-6 . RIVET VFAPE3 034
OPT TO CSR902B4W6 11815
OPT TO CSR902T4W06 11815
OPT TO CSR902T4W6 11815
Optional Vendor Code 04795, 11815, 2N935, 53551,
C5543, F0095
- ITEM NOT ILLUSTRATED

Page 10006-2
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 001A, 001B, 002A, 002B
06 110A D5288014721000 . PROFILE VFAPE3 001
MODIFIED FROM D5288014721001 MADE BY
FAPE3
MODIFIED FROM D5288014721002 MADE BY
FAPE3
used on 001A, 001B, 002A, 002B
06 120A D5288014721100 . PROFILE VFAPE3 001
MODIFIED FROM D5288014721101 MADE BY
FAPE3
MODIFIED FROM D5288014721102 MADE BY
FAPE3
used on 001A, 001B, 002A, 002B
06 130A D5288013420200 . STRIP-SEALING VFAPE3 001
used on 001A, 001B, 002A, 002B
06 140A D5288013420300 . STRIP-SEALING VFAPE3 001
used on 001A, 001B, 002A, 002B
06 150A D5288014720800 . PROFILE VFAPE3 001
MODIFIED FROM D5288014720801 MADE BY
FAPE3
used on 001A, 001B
06 160A D5288014720900 . PROFILE VFAPE3 001
MODIFIED FROM D5288014720901 MADE BY
FAPE3
MODIFIED FROM D5288014720902 MADE BY
FAPE3
used on 002A, 002B
06 170A D5288014720200 . PROFILE VFAPE3 001
MODIFIED FROM D5288014720201 MADE BY
FAPE3
used on 001A, 001B, 002A, 002B
06 180A D5288014720400 . PROFILE VFAPE3 001
MODIFIED FROM D5288014720401 MADE BY
FAPE3
MODIFIED FROM D5288014720402 MADE BY
FAPE3
used on 001A, 001B, 002A, 002B
06 190A D5288014720000 . PROFILE VFAPE3 001
MODIFIED FROM D5288014720001 MADE BY
FAPE3
MODIFIED FROM D5288014720002 MADE BY
FAPE3
- ITEM NOT ILLUSTRATED

Page 10006-3
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
used on 001A, 001B, 002A, 002B
06 200A D5288014720600 . PROFILE VFAPE3 001
MODIFIED FROM D5288014720601 MADE BY
FAPE3
MODIFIED FROM D5288014720602 MADE BY
FAPE3
used on 001A, 001B
06 210A D5288014720700 . PROFILE VFAPE3 001
MODIFIED FROM D5288014720701 MADE BY
FAPE3
MODIFIED FROM D5288014720702 MADE BY
FAPE3
used on 002A, 002B
06 220A D5288013420000 . STRIP-SEALING VFAPE3 001
used on 001A, 001B
06 230A D5288013420100 . STRIP-SEALING VFAPE3 001
used on 002A, 002B
06 240A MS21042L06 . NUT V96906 010
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 11815, 15653, 27238, 52828,
73197, 8K160, F0224
used on 001A, 001B, 002A, 002B
06 250A AN960C6 . WASHER V88044 010
NAS1149CN632R 80205
OPT TO ASNA2397C6 F6198
Optional Vendor Code 10630, 58009, 8K160, F8982
used on 001A, 001B, 002A, 002B
06 260A NAS1151E5 . SCREW V80205 010
Optional Vendor Code 0RFT4, F7411, FAWT4, K8753
used on 001A, 001B, 002A, 002B
06 270A D5288020320000 . SECTION-U VFAPE3 001
used on 001A, 001B
06 280A D5288020320100 . SECTION-U VFAPE3 001
used on 002A, 002B
06 290A D5288013320000 . SEAL-TIP VFAPE3 001
used on 001A, 001B
- ITEM NOT ILLUSTRATED

Page 10006-4
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
06 300A D5288013320100 . SEAL-TIP VFAPE3 001
used on 002A, 002B
06 310A ABS0214-4-7 . RIVET VFAPE3 008
OPT TO CSR902B4W07 11815
OPT TO CSR902B4W7 11815
Optional Vendor Code 04795, 11815, 2N935, 53551,
C5543, F0095
used on 001A, 001B, 002A, 002B
06 320A D5288010020000 . STOP VFAPE3 001
used on 001A, 001B, 002A, 002B
06 330A D5288010020200 . STOP VFAPE3 002
used on 001A, 001B, 002A, 002B
06 340A D5288010020400 . STOP VFAPE3 001
used on 001A, 001B, 002A, 002B
06 350A D5288010100000 . COVER VFAPE3 001
used on 001A
06 350B D5288010100200 . COVER VFAPE3 001
used on 001B
06 360A D5288010100100 . COVER VFAPE3 001
used on 002A
06 360B D5288010100300 . COVER VFAPE3 001
used on 002B
- ITEM NOT ILLUSTRATED

Page 10006-5
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

320
310
D
340
310

A 310
A B

330
B
C
C TYPICAL

220
350 (230)
(360)
E 200 140
C (210)
120

10
260 190

240
250
20 40 285
30
50 90
270
80 (280)
180 70
240 60
250
170
150
240
(160)
250
D 260
110
130

290 E
(300)
260

F_PL_528114_06_A_01_01

COVER ASSY
Figure 06A / FIGURE-52-81-14-950-806-A01

Page 10006A-0
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
06A - 001A D5288010000074 COVER ASSY VFAPE3 RF
used on 090C (528114010), 090C (52811401A), 090C
(52811401C), 090C (52811401D), 090C (52811401F)
SEE 52-81-14-010 FOR NHA, SEE 52-81-14-01A FOR
NHA, SEE 52-81-14-01C FOR NHA, SEE
52-81-14-01D FOR NHA, SEE 52-81-14-01F FOR NHA
06A - 001B D5288010000074 COVER ASSY VFAPE3 RF
used on 090D (528114010), 090D (52811401A), 090B
(52811401B), 090D (52811401C), 090D (52811401D),
090B (52811401E), 090D (52811401F)
SEE 52-81-14-010 FOR NHA, SEE 52-81-14-01A FOR
NHA, SEE 52-81-14-01B FOR NHA, SEE
52-81-14-01C FOR NHA, SEE 52-81-14-01D FOR
NHA, SEE 52-81-14-01E FOR NHA, SEE 52-81-14-01F
FOR NHA
06A - 002A D5288010000174 COVER ASSY VFAPE3 RF
used on 100C (528114010), 100C (52811401A), 100C
(52811401C), 100C (52811401D), 100C (52811401F)
SEE 52-81-14-010 FOR NHA, SEE 52-81-14-01A FOR
NHA, SEE 52-81-14-01C FOR NHA, SEE
52-81-14-01D FOR NHA, SEE 52-81-14-01F FOR NHA
06A - 002B D5288010000174 COVER ASSY VFAPE3 RF
used on 100D (528114010), 100D (52811401A), 100B
(52811401B), 100D (52811401C), 100D (52811401D),
100B (52811401E), 100D (52811401F)
SEE 52-81-14-010 FOR NHA, SEE 52-81-14-01A FOR
NHA, SEE 52-81-14-01B FOR NHA, SEE
52-81-14-01C FOR NHA, SEE 52-81-14-01D FOR
NHA, SEE 52-81-14-01E FOR NHA, SEE 52-81-14-01F
FOR NHA
06A 010A ABS0251-5-7 . FASTENER-HI-LOK VFAPE3 008
DAN6-5-7 D8518
OPT TO HL11VBJ5-7 92215
Optional Vendor Code 04795, 2N935, 56878, 73197,
C5543
used on 001A, 001B, 002A, 002B
06A 020A NSA5075-5 . COLLAR VF6198 008
OPT TO DAN11-5 D8518
OPT TO F0N2-1181-5 H1822
OPT TO HL70AA5 92215
- ITEM NOT ILLUSTRATED

Page 10006A-1
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
Optional Vendor Code 04795, 2N935, 56878, 5M902,
73197, 80539, C5543, U6300
used on 001A, 001B, 002A, 002B
06A 030A D5288010600000 . SUPPORT ASSY-SENSOR VFAPE3 002
used on 001A, 001B, 002A, 002B
06A 040A MS21042L03 .. NUT V96906 002
used on 030A
06A 050A AN960-10L .. WASHER V88044 002
NAS1149F0332P 80205
OPT TO ASNA2397-10L F6198
Optional Vendor Code 10630, 58009, 8K160, F8982
used on 030A
06A 060A NAS1133-3W .. SCREW V80205 002
Optional Vendor Code 62384, C4293
used on 030A
06A 070A ABS0121-11 .. TARGET VFAPE3 001
OPT TO 666000078 K0654
OPT TO 8-368-04 08748
Optional Vendor Code 04795, 08748, 2N935, C5543,
K0653
used on 030A
06A 080A D5288014420000 .. SHIM VFAPE3 001
used on 030A
06A 090A D5288014220000 .. SUPPORT-SENSOR VFAPE3 001
MODIFIED FROM D5288014220001 MADE BY
FAPE3
used on 030A
06A 110A D5288014721000 . PROFILE VFAPE3 001
MODIFIED FROM D5288014721001 MADE BY
FAPE3
MODIFIED FROM D5288014721002 MADE BY
FAPE3
used on 001A, 001B, 002A, 002B
06A 120A D5288014721100 . PROFILE VFAPE3 001
MODIFIED FROM D5288014721101 MADE BY
FAPE3
MODIFIED FROM D5288014721102 MADE BY
FAPE3
used on 001A, 001B, 002A, 002B
06A 130A D5288013420200 . STRIP-SEALING VFAPE3 001
used on 001A, 001B, 002A, 002B
- ITEM NOT ILLUSTRATED

Page 10006A-2
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
06A 140A D5288013420300 . STRIP-SEALING VFAPE3 001
used on 001A, 001B, 002A, 002B
06A 150A D5288014720800 . PROFILE VFAPE3 001
MODIFIED FROM D5288014720801 MADE BY
FAPE3
used on 001A, 001B
06A 160A D5288014720900 . PROFILE VFAPE3 001
MODIFIED FROM D5288014720901 MADE BY
FAPE3
MODIFIED FROM D5288014720902 MADE BY
FAPE3
used on 002A, 002B
06A 170A D5288014720200 . PROFILE VFAPE3 001
MODIFIED FROM D5288014720201 MADE BY
FAPE3
used on 001A, 001B, 002A, 002B
06A 180A D5288014720400 . PROFILE VFAPE3 001
MODIFIED FROM D5288014720401 MADE BY
FAPE3
MODIFIED FROM D5288014720402 MADE BY
FAPE3
used on 001A, 001B, 002A, 002B
06A 190A D5288014720000 . PROFILE VFAPE3 001
MODIFIED FROM D5288014720001 MADE BY
FAPE3
MODIFIED FROM D5288014720002 MADE BY
FAPE3
used on 001A, 001B, 002A, 002B
06A 200A D5288014720600 . PROFILE VFAPE3 001
MODIFIED FROM D5288014720601 MADE BY
FAPE3
MODIFIED FROM D5288014720602 MADE BY
FAPE3
used on 001A, 001B
06A 210A D5288014720700 . PROFILE VFAPE3 001
MODIFIED FROM D5288014720701 MADE BY
FAPE3
MODIFIED FROM D5288014720702 MADE BY
FAPE3
used on 002A, 002B
06A 220A D5288013420000 . STRIP-SEALING VFAPE3 001
used on 001A, 001B
- ITEM NOT ILLUSTRATED

Page 10006A-3
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
06A 230A D5288013420100 . STRIP-SEALING VFAPE3 001
used on 002A, 002B
06A 240A MS21042L06 . NUT V96906 043
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 11815, 15653, 27238, 52828,
73197, 8K160, F0224
used on 001A, 001B, 002A, 002B
06A 250A AN960C6 . WASHER V88044 043
NAS1149CN632R 80205
OPT TO ASNA2397C6 F6198
Optional Vendor Code 10630, 58009, 8K160, F8982
used on 001A, 001B, 002A, 002B
06A 260A NAS1151E5 . SCREW V80205 043
Optional Vendor Code 0RFT4, F7411, FAWT4, K8753
used on 001A, 001B, 002A, 002B
06A 270A D5288013520400 . SECTION-U VFAPE3 001
used on 001A
06A 270B D5288013520800 . SECTION-U VFAPE3 001
used on 001A, 001B
06A 280A D5288013520500 . SECTION-U VFAPE3 001
used on 002A
06A 280B D5288013520900 . SECTION-U VFAPE3 001
used on 002A, 002B
06A 285A D5288013520600 . SHIM VFAPE3 001
used on 001A, 001B, 002A, 002B
06A 290A D5288020600000 . SEAL-TIP VFAPE3 001
used on 001A, 001B
06A 300A D5288020600100 . SEAL-TIP VFAPE3 001
used on 002A, 002B
06A 310A ABS0214-4-7 . RIVET VFAPE3 008
OPT TO CSR902B4W07 11815
OPT TO CSR902B4W7 11815
Optional Vendor Code 04795, 11815, 2N935, 53551,
C5543, F0095
used on 001A, 001B, 002A, 002B
- ITEM NOT ILLUSTRATED

Page 10006A-4
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
06A 320A D5288010020000 . STOP VFAPE3 001
used on 001A, 001B, 002A, 002B
06A 330A D5288010020200 . STOP VFAPE3 002
used on 001A, 001B, 002A, 002B
06A 340A D5288010020400 . STOP VFAPE3 001
used on 001A, 001B, 002A, 002B
06A 350A D5288010100400 . COVER VFAPE3 001
used on 001A
06A 350B D5288010100800 . COVER VFAPE3 001
used on 001B
06A 360A D5288010100500 . COVER VFAPE3 001
used on 002A
06A 360B D5288010100900 . COVER VFAPE3 001
used on 002B
- ITEM NOT ILLUSTRATED

Page 10006A-5
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

170
10
100
20 240 x4
45 30

140

260

10 130 250
20 50
30 270
40 210 190
220 (200)
180 230

150 x4
150 x4
160

A
F_PL_528114_07_0_01_03

FITTING INSTL-REAR
Figure 07 / FIGURE-52-81-14-950-807-01

Page 10007-0
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
07 - 001A D5288010000068 FITTING INSTL-REAR VFAPE3 RF
used on 110A (528114010), 110A (52811401A), 110A
(52811401B), 110A (52811401C), 110A (52811401D),
110A (52811401E), 110A (52811401F)
SEE 52-81-14-010 FOR NHA, SEE 52-81-14-01A FOR
NHA, SEE 52-81-14-01B FOR NHA, SEE
52-81-14-01C FOR NHA, SEE 52-81-14-01D FOR
NHA, SEE 52-81-14-01E FOR NHA, SEE 52-81-14-01F
FOR NHA
07 - 001B D5288010000068 FITTING INSTL-REAR VFAPE3 RF
used on 110B (528114010), 110B (52811401A), 110B
(52811401B), 110B (52811401C), 110B (52811401D),
110B (52811401E), 110B (52811401F)
SEE 52-81-14-010 FOR NHA, SEE 52-81-14-01A FOR
NHA, SEE 52-81-14-01B FOR NHA, SEE
52-81-14-01C FOR NHA, SEE 52-81-14-01D FOR
NHA, SEE 52-81-14-01E FOR NHA, SEE 52-81-14-01F
FOR NHA
07 - 002A D5288010000168 FITTING INSTL-REAR VFAPE3 RF
used on 120A (528114010), 120A (52811401A), 120A
(52811401B), 120A (52811401C), 120A (52811401D),
120A (52811401E), 120A (52811401F)
SEE 52-81-14-010 FOR NHA, SEE 52-81-14-01A FOR
NHA, SEE 52-81-14-01B FOR NHA, SEE
52-81-14-01C FOR NHA, SEE 52-81-14-01D FOR
NHA, SEE 52-81-14-01E FOR NHA, SEE 52-81-14-01F
FOR NHA
07 - 002B D5288010000168 FITTING INSTL-REAR VFAPE3 RF
used on 120B (528114010), 120B (52811401A), 120B
(52811401B), 120B (52811401C), 120B (52811401D),
120B (52811401E), 120B (52811401F)
SEE 52-81-14-010 FOR NHA, SEE 52-81-14-01A FOR
NHA, SEE 52-81-14-01B FOR NHA, SEE
52-81-14-01C FOR NHA, SEE 52-81-14-01D FOR
NHA, SEE 52-81-14-01E FOR NHA, SEE 52-81-14-01F
FOR NHA
07 010A MS24665-151 . PIN-COTTER V96906 006
Optional Vendor Code 10630, 65029, 73145, 84114,
8K160
used on 001A, 001B, 002A, 002B
- ITEM NOT ILLUSTRATED

Page 10007-1
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
07 020A NSA5060C4 . NUT VF6198 006
OPT TO E9925-4 72962
Optional Vendor Code 04795, 15653, 2N935, 56878,
C5543, F0224, FAWT4
used on 001A, 001B, 002A, 002B
07 030A AN960C416L . WASHER V88044 006
NAS1149C0432R 80205
OPT TO ASNA2397C416L F6198
Optional Vendor Code 10630, 58009
used on 001A, 001B, 002A, 002B
07 040A NAS6704DU1 . BOLT V80205 001
Optional Vendor Code 0ZC92, 1ER65, 1RC86, 62384,
8Z507, F7411, FAWT4, K8753, T0802
used on 001A, 001B, 002A, 002B
07 045A ABS0214-4-6 . RIVET VFAPE3 001
OPT TO CSR902B4W6 11815
OPT TO CSR902T4W06 11815
OPT TO CSR902T4W6 11815
Optional Vendor Code 04795, 11815, 2N935, 53551,
C5543, F0095
used on 001A, 001B, 002A, 002B
07 050A ABS0394G210 . STRAP-BONDING VFAPE3 001
Optional Vendor Code 04795, 2N935, C5543, C5973,
D7103, D8518, F4291
used on 001A, 001B, 002A, 002B
07 100A MS15001-1 . FITTING-LUBRICATION V96906 001
AS15001-1 81343
AS15001-1P 81343
Optional Vendor Code 0FKM1, 13899, 52930, 57336,
59736
used on 001A, 001B, 002A, 002B
07 130A NAS6704DU3 . BOLT V80205 001
Optional Vendor Code 1ER65, 1RC86, 62384, 8Z507,
F7411, FAWT4, K8753, T0802
used on 001A, 001B, 002A, 002B
07 140A D5288014520000 . BRACKET VFAPE3 001
used on 001A, 001B, 002A, 002B
07 150A NAS6704HU19 . BOLT V80205 008
Optional Vendor Code 0ZC92, 1ER65, 1RC86, 8Z507,
F7411, K8753, T0802
used on 001A, 001B, 002A, 002B
- ITEM NOT ILLUSTRATED

Page 10007-2
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
07 160A NAS6704HU18 . BOLT V80205 004
Optional Vendor Code 0ZC92, 1ER65, 1RC86, 8Z507,
F7411, K8753, T0802
used on 001A, 001B, 002A, 002B
07 170A NAS1154V6D . SCREW V80205 004
Optional Vendor Code 0RFT4, F7411, FAWT4, K8753
used on 001A, 001B, 002A, 002B
07 180A D5288013120000 . INSERT VFAPE3 012
used on 001A, 001B, 002A, 002B
07 190A D5288010300000 . REAR FITTING ASSY VFAPE3 001
MODIFIED FROM D5288010300002 MADE BY
FAPE3
used on 001A, 001B
07 200A D5288010300100 . HINGE ASSY VFAPE3 001
MODIFIED FROM D5288010300102 MADE BY
FAPE3
used on 002A, 002B
07 210A MS24665-151 .. PIN-COTTER V96906 004
Optional Vendor Code 10630, 65029, 73145, 84114,
8K160
used on 190A, 200A
07 220A NSA5059C4 .. NUT VF6198 004
OPT TO TE9925-4 72962
OPT TO THCR54 F0224
Optional Vendor Code 04795, 15653, 2N935, 56878,
A3856, C5543, F0224, FAWT4
used on 190A, 200A
07 230A AN960XC416L .. WASHER V88044 004
NAS1149C0432B 80205
Optional Vendor Code 10630, 58009, 8K160
used on 190A, 200A
07 240A NAS6704DU7 .. BOLT V80205 004
Optional Vendor Code 1ER65, 1RC86, 62384, 8Z507,
F7411, FAWT4, K8753, T0802
used on 190A, 200A
07 250A D5288012620000 .. HINGE VFAPE3 001
MODIFIED FROM D5288012620001 MADE BY
FAPE3
MODIFIED FROM D5288012620052 MADE BY
FAPE3
used on 190A, 200A
- ITEM NOT ILLUSTRATED

Page 10007-3
52-81-14 Jan 01/17
 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
07 260A A5283301920000 .. BUSH VFAPE3 001
WITH OVERSIZE ITEM 261 TO 268
used on 190A, 200A
07 - 261A A52833019200001 .. BUSH VFAPE3 AR
USE AS REQUIRED, OVERSIZE OF ITEM 260
A52810110200001 FAPE3
used on 190A, 200A
07 - 262A A52833019200002 .. BUSH VFAPE3 AR
USE AS REQUIRED, OVERSIZE OF ITEM 260
A52810110200002 FAPE3
used on 190A, 200A
07 - 263A A52833019200003 .. BUSH VFAPE3 AR
USE AS REQUIRED, OVERSIZE OF ITEM 260
A52810110200003 FAPE3
used on 190A, 200A
07 - 264A A52833019200004 .. BUSH VFAPE3 AR
USE AS REQUIRED, OVERSIZE OF ITEM 260
A52810110200004 FAPE3
used on 190A, 200A
07 - 265A A52833019200005 .. BUSH VFAPE3 AR
USE AS REQUIRED, OVERSIZE OF ITEM 260
A52810110200005 FAPE3
used on 190A, 200A
07 - 266A A52833019200006 .. BUSH VFAPE3 AR
USE AS REQUIRED, OVERSIZE OF ITEM 260
A52810110200006 FAPE3
used on 190A, 200A
07 - 267A A52833019200007 .. BUSH VFAPE3 AR
USE AS REQUIRED, OVERSIZE OF ITEM 260
A52810110200007 FAPE3
used on 190A, 200A
07 - 268A A52833019200008 .. BUSH VFAPE3 AR
USE AS REQUIRED, OVERSIZE OF ITEM 260
A52810110200008 FAPE3
used on 190A, 200A
07 270A D5288012520000 .. FITTING VFAPE3 001
MODIFIED FROM D5288012520002 MADE BY
FAPE3
used on 190A, 200A
- ITEM NOT ILLUSTRATED

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COMPONENT MAINTENANCE MANUAL
D5288000800000

80
20

70

90
70

10 40

70

70

20

60

30 50 40
A

F_PL_528114_08_0_01_00

PODGER INSTL
Figure 08 / FIGURE-52-81-14-950-808-01

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 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
08 - 001A D5288000800078 PODGER INSTL VFAPE3 RF
POST SB 52-1025
used on 210A (52811401C), 210A (52811401F)
SEE 52-81-14-01C FOR NHA, SEE 52-81-14-01F FOR
NHA
08 - 001B D5288000900086 PODGER INSTL VFAPE3 RF
POST SB 52-1025
used on 230A (52811401D)
SEE 52-81-14-01D FOR NHA
08 - 001C D5288001000066 PODGER INSTL VFAPE3 RF
POST SB 52-1025
used on 210A (52811401E)
SEE 52-81-14-01E FOR NHA
08 - 002A D5288000800178 PODGER INSTL VFAPE3 RF
POST SB 52-1025
used on 220A (52811401C), 220A (52811401F)
SEE 52-81-14-01C FOR NHA, SEE 52-81-14-01F FOR
NHA
08 - 002B D5288000900186 PODGER INSTL VFAPE3 RF
POST SB 52-1025
used on 240A (52811401D)
SEE 52-81-14-01D FOR NHA
08 - 002C D5288001000166 PODGER INSTL VFAPE3 RF
POST SB 52-1025
used on 220A (52811401E)
SEE 52-81-14-01E FOR NHA
08 010A NAS1726-05E . NUT V80205 008
OPT TO DHR9035-05E F0224
OPT TO HW53097P836 15653
Optional Vendor Code 15653, 27238, F0224, FAWT4
used on 001A, 001B, 001C, 002A, 002B, 002C
08 020A NAS1132E3 . SCREW V80205 008
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, 1RC86,
62384, 8Z507, C4293, F7411, FAWT4, K8753
used on 001A, 001B, 001C, 002A, 002B, 002C
08 030A D5288021000000 . PODGER ASSY VFAPE3 001
used on 001A, 001B, 001C, 002A, 002B, 002C
08 040A MS20470AD3 .. RIVET V96906 006
used on 030A
08 050A D5288021020000 .. SHEET-TEFLON VFAPE3 001
used on 030A
- ITEM NOT ILLUSTRATED

Page 10008-1
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 @AIRBUS
COMPONENT MAINTENANCE MANUAL
D5288000800000

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
08 060A D5288021120000 .. PODGER VFAPE3 001
used on 030A
08 070A NAS1132E1 . SCREW V80205 006
Optional Vendor Code 0RFT4, 0ZC92, 1ER65, 1RC86,
62384, 8Z507, C4293, F7411, FAWT4, K8753
used on 001A, 001B, 001C, 002A, 002B, 002C
08 080A D5288021220000 . FITTING VFAPE3 001
MODIFIED FROM D5288021220001 MADE BY
FAPE3
used on 001A, 001B, 001C, 002A, 002B, 002C
08 090A NAS1835C08 . INSERT V80205 006
OPT TO EF1835C08 C3898
OPT TO NSA5072-08A F6198
OPT TO SL606-08C 97393
Optional Vendor Code 83324, 97393, B1103, DM498
used on 001A, 001B, 001C, 002A, 002B, 002C
- ITEM NOT ILLUSTRATED

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