@AIRBUS

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

COMPONENT MAINTENANCE MANUAL

WITH
ILLUSTRATED PART LIST

INBOARD LINK AND OUTBOARD

PN : A5351021320001 A5351021320101
A5351021320201 A5351021320301
A5351021320401 A5351021320402
A5351021320403 A5351021320501
A5351021320502 A5351021320503
A5351021420001 A5351021420201
A5351021420401 A5351021420402
A5351021420403

Issue: Dec 01/90 27-81-03 Rev: Jul 01/09

 @AIRBUS
COMPONENT MAINTENANCE MANUAL
A5351021320001

HIGHLIGHTS

Revision No. 3 - Jul 01/09

LOCATIONS CHG DESCRIPTIONS OF CHANGE

CODE
INSPECTION/CHECK
TASK 27-81-03-210-801-A01 R

REPAIR
TASK 27-81-03-300-801-A01 R CONSUMABLE MATERIAL DATA
UPDATED

HIGHLIGHTS
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COMPONENT MAINTENANCE MANUAL
A5351021320001

LIST OF EFFECTIVE CONTENT

Revision No. 3 - Jul 01/09

CONTENT CHG LAST REVISION

CODE DATE
INTRODUCTION
TASK 27-81-03-871-801-A01 Mar 01/09

DESCRIPTION AND OPERATION

TASK 27-81-03-870-802-A01 Mar 01/09

INSPECTION/CHECK
TASK 27-81-03-210-801-A01 R Jul 01/09
Subtask 27-81-03-210-001-A01 Mar 01/09
FIGURE 27-81-03-991-001-A01 Mar 01/09
FIGURE 27-81-03-991-002-A01 Mar 01/09

REPAIR
TASK 27-81-03-300-801-A01 R Jul 01/09
Subtask 27-81-03-300-001-A01 Mar 01/09
FIGURE 27-81-03-991-003-A01 Mar 01/09

ILLUSTRATED PARTS LIST

L.E.C.
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COMPONENT MAINTENANCE MANUAL
A5351021320001

LIST OF SERVICE BULLETINS

SB No REV No MOD No INCORP. TITLE

DATE
*** NO SB ***

SBL
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 @AIRBUS
COMPONENT MAINTENANCE MANUAL
A5351021320001

INTRODUCTION

**For PN’s ALL

TASK 27-81-03-871-801-A01
Introduction
1. General
A. This manual is written to the iSpec 2200. The international SI units of measurement are used in
this manual, with imperial units shown in parentheses.
B. The manual contains data about maintenance on the component in a workshop. It does not
contain data about maintenance on the component when it is installed in the aircraft.
C. Only approved persons with the necessary skills are permitted to do the maintenance procedures
in this manual.
D. Maintenance Task Oriented Support System (MTOSS) task and subtask identification is used in
this manual. The maintenance tasks and other data have special MTOSS numbers for Electronic
Data Processing (EDP). The user of the manual can ignore the MTOSS numbers.
E. This manual contains:
- Technical data for the component
- Maintenance and repair procedures about the component
- An Illustrated Parts List (IPL) with data for the component parts. Parts are identified in all
sections of the manual by the IPL-Figure and item number.
F. We verified the DISASSEMBLY, TESTING and ASSEMBLY procedures by simulation.
2. How to use the Manual
A. Make sure that the manual contains the information applicable to your component.
B. If you need to identify a part or find a part number, use the search function.
C. You must use the instructions in this manual for all the component maintenance. Read all the
applicable WARNINGS and CAUTIONS before you do the work on the component.
3. List of Abbreviations
ACM Abbreviated Component Maintenance Manual
AEB Airline Engineering Bulletin
ASD Aero Space and Defence Industries Association of Europe
ATA Air Transport Association of America
ATLAS Abbreviated Test Language for All Systems
CMM Component Maintenance Manual
CMS Component Maintenance Sheet
FIN Functional Item Number
IPC Illustrated Parts Catalog

INTRO
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COMPONENT MAINTENANCE MANUAL
A5351021320001

IPL Illustrated Parts List

ID Inside Diameter
MFG Manufacturing
MFR Manufacturer
MOD Modification
MTOSS Maintenance Task Oriented Support System
NTF Non Textile Floor
OD Outside Diameter
PA Poly-Amide
PARA Paragraph
PC Poly-Carbonate
PMS Process and Materials Specification
PN Part Number
PU Poly-Urethane
PV Poly-Venyl-Fluorite
SB Service Bulletin
SERNO Serial Number
STE Simplified Technical English
TBD To Be Determined
List of Abbreviations
TABLE 1

INTRO
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COMPONENT MAINTENANCE MANUAL
A5351021320001

DESCRIPTION AND OPERATION

**For PN’s ALL

TASK 27-81-03-870-802-A01
Description
1. The inboard and outboard link permit actuation of Krueger flap located an wing leading edge, near
fuselage.

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COMPONENT MAINTENANCE MANUAL
A5351021320001

INSPECTION/CHECK

**For PN’s ALL

TASK 27-81-03-210-801-A01
Check
1. Reason for the Job
Self explanatory.
2. Job Set-up Information
A. Referenced Information
REFERENCE DESIGNATION
TASK 27-81-03-300-801-A01 TASK 27-81-03-300-801-A01-Repair
FIGURE 27-81-03-991-001-A FIGURE 27-81-03-991-001-A-Check for Damage on Inboard
Link
FIGURE 27-81-03-991-002-A FIGURE 27-81-03-991-002-A-Check for Damage on Inboard
Link
Referenced Information
TABLE 1

3. Procedure

Subtask 27-81-03-210-001-A01
A. Check
(1) Check for Wear (Refer to FIGURE 27-81-03-991-001-A and FIGURE 27-81-03-991-002-A).
(a) Measure depth of damaged part (X) (see details A and B)
(b) If X is less or equal to 0.4 mm (0.0157 in.), refer to REPAIR TASK
27-81-03-300-801-A01. Maximum wear per face is 0.4 mm (0.0157 in.).
(c) If X is more than 0.4 mm (0.0157 in.). per face contact AIRBUS INDUSTRIE.

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**For PN’s ALL

F_CM_278103_1_0010101_01_00

Check for Damage on Inboard Link

FIGURE-27-81-03-991-001-A01

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F_CM_278103_1_0020101_01_00

Check for Damage on Inboard Link

FIGURE-27-81-03-991-002-A01

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COMPONENT MAINTENANCE MANUAL
A5351021320001

REPAIR

**For PN’s ALL

TASK 27-81-03-300-801-A01
Repair
1. General
A. This repair principle for wear corrosion covers up to a total wear depth of 0.8 mm (0.0315 in.).
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
16-020 Wash Primer
16-001 Anti Corrosion Primer (Polyurethane)
09-025 Corrosion Inhibiting Sealant, sprayable
Consumable Materials
TABLE 1

B. Referenced Information
REFERENCE DESIGNATION
FIGURE 27-81-03-991-003-A FIGURE 27-81-03-991-003-A-Repair of the Inboard or
Outboard Link
Referenced Information
TABLE 2

3. Procedure

Subtask 27-81-03-300-001-A01
A. Reworking

NOTE : Refer to FIGURE 27-81-03-991-003-A.

(1) Fabricate a titanium washer (TA6V alloy) 0.6 mm (0.0236 in.) thick, internal diameter 33
mm (1.2992 in.) and external diameter 44 mm (1.7322 in.).
(2) Machine damaged part of inboard or outboard link to a depth of 0.6 mm (0.0236 in.) over
a diameter of 48 mm (1.88971 in.) coaxial with bore.

WARNING : BE CAREFUL WHEN YOU USE MATERIAL NO. 16-020 WASH PRIMER.
OBEY THE MATERIAL MANUFACTURER’S INSTRUCTIONS.

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WARNING : BE CAREFUL WHEN YOU USE MATERIAL NO. 16-001 ANTI CORROSION
PRIMER (POLYURETHANE). OBEY THE MATERIAL MANUFACTURER’S
INSTRUCTIONS.
(3) Protect the reworked area with Material No. 16-020 Wash Primer and Material No. 16-001
Anti Corrosion Primer (Polyurethane).

WARNING : BE CAREFUL WHEN YOU USE MATERIAL NO. 09-025 CORROSION

INHIBITING SEALANT, SPRAYABLE. OBEY THE MATERIAL
MANUFACTURER’S INSTRUCTIONS.
(4) Install washer with Material No. 09-025 Corrosion Inhibiting Sealant, sprayable.

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COMPONENT MAINTENANCE MANUAL
A5351021320001

**For PN’s ALL

F_CM_278103_1_0030101_01_00

Repair of the Inboard or Outboard Link

FIGURE-27-81-03-991-003-A01

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